Maintenance and Manufacturing Staff Instructions (MSI) No. 26

Subject:	Number:	MSI 26
Issuance of a Certificate of Airworthiness on the Import of Type Certified Aircraft	Revision No:	1
	Number of Pages:	37
File No: AARP-5009-3-26	Issue Date:	February 24, 2004

Word version (308 KB)

1. Purpose

1.1 The purpose of this instruction is to provide guidance and information to Air Operators and Transport Canada personnel concerning the issuance of a Canadian Certificate of Airworthiness (C of A) for type certificated aircraft imported into Canada.

2. Background

2.1 Aircraft are routinely imported into Canada, however the process to determine eligibility for import and the process for issuance of a C of A is not detailed in the Canadian Aviation Regulations or Standards.

2.2 There are many variables that must be considered for persons wishing to import an aircraft and obtain a C of A. This staff instruction, through the attached checklists, serves to detail the steps involved in determining eligibility for import and eligibility for the issuance of a C of A.

2.3 The attached checklists also include information for the addition of aircraft to various operating certificates. This information is over and above that needed for the issuance of a C of A and is included here to provide a comprehensive document outlining all the steps involved from import to operation.

2.4 This staff instruction is not intended to cover the eligibility for issuance of Special Certificates of Airworthiness in any category. Refer to MSI 14 and STD 507.03.

3. Layout of TP Document

3.1 The importation document as found on pages 3 to 37 of this MSI is made up of five parts:

Part 1 - Provides a general overview of the process.

Part 2 - Is to be completed by the operator prior to purchasing the aircraft.

Part 3 - Consists of two (2) distinct methods of verification of conformity to the Type Design.

Part 4 - Identifies the additional airworthiness requirements that must be accomplished prior to operating the aircraft under an Air Operator Certificate or a Private Operator Certificate.

Part 5 - Consists of checklists that identify specific airworthiness / operational requirements for aircraft operated under the CARs.

4. Availablity

4.1 The importation document annexed to this MSI is available on the Internet and on the Intranet as a downloadable document. Transport Canada personnel should also make copies available to the industry as required.

5. Effective date

5.1 This instruction comes into effect immediately.

6. HQ Contact

6.1 The responsible division indicated below may be contacted for information regarding this MSI:

AARPE - Standards and Procedures

D.B. Sherritt
Director,
Maintenance and Manufacturing

Aircraft Importation Checklist

Layout of the Importation Document

Part 1: The information is intended to provide a general overview of the importation process to a prospective applicant. Part 1 is composed of two pages.

Part 2: Is to be completed by the applicant and submitted to Transport Canada. This should be done prior to purchasing the aircraft to ensure it is eligible for importation. An application for Provisional Certificate of Registration (form 26-0025) may be made when Part 2 is completed and verified eligible for importation by Transport Canada or a Minister's Delegate. Please refer to Standard 507 Appendix E - Additional Guidelines respecting the application for a flight authority. Part 2 is composed of 7 pages.

Part 3: Consists of three checklists that are to be completed by the applicant. The checklists are broken into two distinct methods of verification of conformity to an approved type design. Complete only the checklist that is applicable to the method of importation. Please ensure all segments of the checklist utilized are completed. Part 3 is composed of 3 checklists that cover a total of 9 pages .

Checklist 1: This checklist will be used when:

1. conformity to an approved type design is shown by means of an Export Airworthiness Certificate issued by the civil aviation authority of a country with which Canada has entered into a bilateral airworthiness agreement or a similar arrangement, which provides for the acceptance of such certificates; or
2. conformity to an approved type design is shown by means of an Export Airworthiness Certificate issued by the civil aviation authority of a country with which Canada does not have an agreement, where a Canadian Type Certificate has been issued and the product is being exported from the country of manufacture. Checklist 1 is composed of 3 pages.

Checklist 2: This checklist will be used when conformity to an approved type design is shown by means of an airworthiness inspection to procedures detailed in the Canadian Aviation Regulations for an aircraft, which will be imported without an Export Airworthiness Certificate. Checklist 2 is composed of 4 pages.

Checklist 3: The following checklist will be used to ensure essential operating requirements are met. This checklist is applicable to aircraft imported with or without an Export Airworthiness Certificate.

Part 4: Identifies additional airworthiness inspection requirements for aeroplanes, helicopters and balloons that must be complied with prior to the aircraft being operated under the authority of an Air Operator Certificate (AOC), Private Operator Certificate (POC), Flight Training Unit Certificate (FTUOC) or Privately Operated. It is important to note that not all sections are applicable therefore it is imperative the applicant review each area of inspection for applicability against the referenced regulation and standard. This checklist will be submitted to your Principal Maintenance Inspector as part of the process to add the aircraft to the AOC or POC. Part 4 is composed of 6 pages and is optional at time of import.

Part 5: Consists of 6 checklists. Each checklist identifies specific airworthiness / operational requirements for aircraft operated under CAR Part IV Subpart 6 - Flight Training Units, Part VI Subpart 4 - Private Operator Passenger Transportation, Part VII Subpart 2 - Aerial Work, Part VII Subpart 3 - Air Taxi Operations, Part VII Subpart 4 - Commuter Operations and Part VII Subpart 5 - Airline Operations. The applicant should review and complete the applicable checklist in conjunction with applicable portions of Part 4 of this document. This checklist will be submitted to your Principal Maintenance Inspector as part of the process to add the aircraft to the AOC. Part 5 is composed of 8 pages and is optional at time of import.

Part 1: General Overview

Airworthiness Requirements:

An aircraft may be issued a Canadian C of A whether or not it is imported with an Export Airworthiness Certificate, provided it can be shown and the Minister is satisfied that the aircraft conforms to an approved type design and is in a condition for safe operation.

Note: The term "in a condition for safe operation" is intended to cover general aircraft condition and whether or not the aircraft is configured for the type of operation it will be used for.

Aircraft may conform with the basic requirements of the Type Certificate Data Sheet (TCDS) but be in poor overall condition. Maintenance may be needed to restore the aircraft and it's systems to ensure proper operation. The aircraft may also be intended for operation in a role that requires the installation of additional equipment such as medivac or fire supression or where specific operational rules require the installation of certain items of equipment such as Flight Data Recorders, survival equipment, Ground Proximity Warning Systems and so on. The combination of proper maintenance and aircraft configuration meet the intent of "in a condition for safe operation".

It is not intended that a Transport Canada Civil Aviation Safety Inspector or Minister's Delegate assume any responsibility for the condition or safe operation of any aircraft. This is the responsibility of an appropriately qualified person per CAR 571.11 and/or the operator of the aircraft.

1.1 The following requirements must be met for the aircraft to be eligible for importation:

1. The aircraft owner must be qualified to be a registered owner of a Canadian Aircraft pursuant to Canadian Aviation Regulations (CAR) Part II, Subpart 2 - Aircraft Marking and Registration, CAR 202.15; and
2. The aircraft must conform to an approved type design. This may be demonstrated by compliance with CAR Part V, Subpart 7 - Flight Authority, CAR 507.07 and STD 507.07 - Applications made in respect of Imported Aircraft.

Information Notes: There is a distinct difference between eligibility for import and eligibility for the issuance of a Certificate of Airworthiness.

1. For the aircraft type to be eligible for import, there must be a Canadian TCDS (reference CAR 507.07(6)(a)) for the aircraft type. Airworthiness Notice B038 contains additional information on aircraft that have not been issued a Canadian TCDS but are otherwise eligible for import.
2. To be eligible for the issuance of a Certificate of Airworthiness, the applicant must demonstrate that the aircraft conforms to all the requirements of the TCDS. This will include correct aircraft model and serial number, correct engine, propeller and appliance models plus any additional requirements such as Canadian configuration modifications, flight manual status, life limitations, maintenance requirements and so on. The checklists contained in this document are designed for this purpose. Importers are cautioned to ensure that the aircraft they wish to import is specifically listed in the TCDS by model and serial number. Contact Transport Canada Aircraft Certification if there is any discrepancy with the aircraft model or serial number and the TCDS.

1.2 For aircraft to be operated commercially & added onto an Air Operator Certificate:

For aircraft that will be imported and added to an Air Operator Certificate (either commercial or private), additional airworthiness and operational requirements must be met prior to operation of the aircraft. These requirements are contained in Part 4 and Part 5 of this aircraft importation checklist.

1.3 For all aircraft to be imported:

To expedite the importation process, applicants shall ensure that the aircraft conforms to all the applicable import requirements before the aircraft is subjected to a conformity inspection.

Information Notes:

1. The applicant is responsible to ensure that all major repairs and major modifications carried out prior to importation, are in accordance with approved data. Refer to CAR 571.06 and Standard 571.06(1), (2), (3), (4), (5) and (6) for definitions of approved data and Standard 571 Appendix A for criteria used to classify modifications and repairs. Aircraft Certification Staff Instruction (ACSI) 23, Acceptance and Approval of Foreign Design Changes, should also be reviewed where the aircraft incorporates design changes approved by a foreign airworthiness authority.

The applicant must provide a complete list of modifications,Supplemental Instructions for Continued Airworthiness (ICA) and Supplemental Type Certificates as early as possible during the import process. The applicant may be required to supply substantiating documentation on any or all modifications, STCs as required by Transport Canada. The applicant must ensure he has access to all information required to support the above.

ii. Canadian and Foreign Supplemental Type Certificates (STC's) will be reviewed against configuration, differences in design requirements, AFM supplements, and maintenance manual supplements.

iii. Where differences are noted between the two certificates, inform regional certification personnel who will action in accordance with ACSI 22 and/or Aircraft Certification Policy Letter (ACPL) 6.

iv. Canadian STC's must take precedence for matters relating to Canadian certification.

v. When confirming that Transport Canada has validated a foreign change (STC or FAA 337), check the conditions of that validation to ensure that they have been complied with.

vi. All major repairs and major modifications must be reported to the Minister upon importation pursuant to CAR 571.12.

vii. The applicant must ensure that the aircraft complies with the Noise Emission Standards for the type. To determine if an aircraft does or does not need to meet noise emission standards, the following documents must be consulted; the TCDS; CAR 602; CAR 516 and STD 516 or ICAO Annex 16.

viii. If the aircraft is equipped with a Mode "S" transponder, the applicant must ensure that the transponder code has been disabled and a new code applied for at the time of registration.

ix. The applicant is required to provide Transport Canada with a documentation "report" (survey) delineating proposed maintenance activities required to bring the aircraft to a condition of conformity to the certified type design and for safe operation. See Part 3 and Standard 507.07(7).

x. If any doubt exists during any importation stage, please contact your local Transport Canada Center.

1.4 Additional import requirements may be detailed in the following publications:

1. Airworthiness Notices "A" Series (White);
2. Airworthiness Notices "B" Series (Pink);
3. Aeronautical Information Publication (AIP), Licensing, Registration & Airworthiness (LRA) section;
4. Maintenance Policy Letters (MPL) or Maintenance Staff Instructions (MSI); and
5. Aircraft Certification advisory material

1.5 Conformance Statement - this section is to be completed by the aircraft Owner and/or Authorized Representative

Confirmation by the applicant that, for the aircraft to be eligible for importation and issuance of a Certificate of Airworthiness, 1.1(a) and (b) above has been satisfied and are acceptable to the Minister.
Aircraft Owners Name:
Telephone Number:				Date:
Aircraft Owners Authorized Representative Name (Importing AMO):
Telephone Number:				Date:

Part 2: must be completed by the APPLICANT, where applicable

Please ensure all applicable areas of paragraph 2.1 through to paragraph 2.15 are completed. Mail or deliver to your local Transport Canada Centre or Minister's Delegate, as applicable.

2.1 Photograph, copy (rubbing) ACTUAL airframe data plate details including location, in the space provided:

Part 2: to be completed by the APPLICANT, where applicable

2.2 Aircraft Data:

It is the applicant's responsibility to accurately record the applicable airframe, engine, propeller, main rotor, tail rotor and auxiliary power unit descriptive data from a visual inspection of the components specific data plate. Other technical information may be obtained from the aircraft journey and technical logs.

Aircraft
Manufacturer
Model Number
Serial Number
Total Time Since New (TTSN)
Total Cycles Since New (TCSN)
Type Certificate Number
Identify last major inspection and date completed:	Type:	Date:
Indicate if the Inspection was conducted in accordance with the manufacturer's requirements or other maintenance schedule
Previous foreign registration
Aircraft role prior to importation if known
Intended aircraft role
Additional Noteworthy Information: Use additional paper as required.

Part 2: to be completed by the APPLICANT, where applicable

2.2 Aircraft Data: (continued.)

ENGINE	Engine # 1	Engine # 2	Engine # 3	Engine # 4
Manufacturer
Model Number
Serial Number
Type Certificate Number
Total Time Since New (TTSN)
Total Time Since Overhaul (TTSO)
Total Cycles Since New (TCSN)
Total Cycles Since Overhaul (TCSO)
Additional Noteworthy Information:

PROPELLER	Propeller # 1	Propeller # 2	Propeller # 3	Propeller # 4
Manufacturer
Model Number
Serial Number
Type Certificate Number
Total Time Since New (TTSN)
Total Time Since Overhaul (TTSO)
Additional Noteworthy Information:

Part 2: to be completed by the APPLICANT, where applicable

2.2 Aircraft Data: (continued.)

AUXILIARY POWER UNIT (APU)
Manufacturer
Model Number
Serial Number
Type Certificate Number
Total Time Since New (TTSN)
Total Time Since Overhaul (TTSO)
Total Cycles Since New (TCSN)
Total Cycles Since Overhaul (TCSO)
Additional Noteworthy Information:

Part 2: to be completed by the APPLICANT, where applicable

2.2 Aircraft Data: (continued.)

Provide a list of all helicopter dynamic components as listed on the aircraft type certificate.
Dynamic Components	Manufacturer	Model Number	Serial Number	TTSN	TTSO
Additional Noteworthy Information:

 

Part 2: to be completed by the APPLICANT, where applicable

2.3 Is the aircraft to be operated privately?			Yes:  No: 
Who will conduct the Import?					Contact person:
Location:					Telephone:
2.4 (a) This section is to be completed if the aircraft is to be added onto a new or existing Air Operator Certificate:
Identify Air Operator Certificate: Flight Training Unit Part IV Subpart 6 Private Operator Part VI Subpart 4 Commercial Operator Part VII Subpart 6
Name of Operator Certificate Holder:
Operator Certificate Number:
Address:						Telephone:
(b) Is the aircraft to be added onto the Air Operator Certificate (AOC) or Private Operator Certificate (POC) a new aircraft type to the Company?								Yes:  No: 
Note: If Yes, additional operational requirements may be necessary. Contact the Commercial & Business Aviation or Canadian Business Aviation Association office, as applicable, for details.
2.5 Please send the preceding completed documentation to your local Transport Canada Center or Minister's Delegate as applicable, for aircraft eligibility verification.

This part is to be completed by a TRANSPORT CANADA INSPECTOR or a MINISTER'S DELEGATE

2.6 For Departmental Use Only:
(a) Does the airframe model and serial number agree with the Type Certificate?			Yes:  No: 
(b) Does the engine(s) model number agree with the Type Certificate?			Yes:  No: 
(c) Does the propeller(s) model number agree with the Type Certificate?			Yes:  No: 
(d) Does the APU model number agree with the Type Certificate?			Yes:  No: 
(e) Is the aircraft eligible for importation under the Type Certificate?			Yes:  No: 
Note: If the aircraft is not eligible for importation, identify why in the information section below. Contact the aircraft owner / applicant / representative to discuss the details preventing the aircraft importation. Provide guidance to rectify the situation.
2.7 Has the applicant been advised concerning the eligibility of the aircraft for importation?	Eligible  Not Eligible 	Date applicant contacted:
Transport Canada Inspector or Minister's Delegate name.
2.8 Has the applicant advised Transport Canada or the Minister's Delegate in writing it intends to precede with the import once it has been acknowledged that the aircraft is eligible for importation?	Yes:  No: 	Date:
Information:

Part 2: to be completed by the APPLICANT, where applicable

Section 2.9, 2.10, 2.11 and 2.12 may be completed when it is determined the aircraft meets eligibility requirements.

2.9 Means of importation: Identify the method to be utilized. Complete a, b or c.

(a) Canadian Registration:

Or

Foreign Registration:

(b) Surface Transportation:

(c) Already in Canada, Identify Location:

2.10 Importation flight route and customs clearance.

From:

(departure point in foreign country)

To:

(final destination in Canada)

Customs Clearance Point:

(first landing point in Canada)

2.11 Have Canadian registration marks been reserved:

Yes: 

Marks: C-

No: 

2.12 If the aircraft is equipped with a Mode "S" transponder, has the previous owner's code been disabled and a new code applied for? Yes:  No: 

2.13 This aircraft meets the requirements for a Provisional Certificate of Registration and Flight Permit. In accordance with CAR 507, STD 507.04 and STD 507 Appendix B & E, I hereby request a Provisional Certificate of Registration and Flight Permit for the identified aircraft.

Aircraft Owner / Applicant's Signature:

Aircraft Owner / Applicant's Address:

Telephone:

Date:

Fee Submitted:

2.14 Please send the preceding completed documentation (Section 2.9, 2.10, 2.11, 2.12, 2.13) and associated fees for flight permit and provisional registration to Transport Canada, General Aviation, Aircraft Licensing, in the region where the aircraft will normally be based.

This part is to be completed by a TRANSPORT CANADA INSPECTOR or a MINISTER'S DELEGATE

2.15 For Department Use Only:
Has a flight permit been issued or validated?	Yes:  No: 
Have registration marks been allocated?	Yes:  No: 
Have fees been submitted?	Yes:  No: 
Has Aircraft Registration been advised of eligibility?	Yes:  No: 
Has Non-Registration or De-Registration been received by a foreign aviation authority?	Yes:  No: 

Part 3: General

Note:. The following checklists are controlled, therefore it is suggested that, should copies be made, you ensure the revision status is current prior to their use. The checklists are available on the Internet at: https://tc.canada.ca/en/aviation/reference-centre/airworthiness-staff-instructions-maintenance-manufacturing-staff-instructions/maintenance-manufacturing-staff-instructions-msi-no-26

This checklist shall be used to ensure the standardization of the importation process and assure that all data necessary to validate the importation are requested and received from the applicant. The Civil Aviation Safety Inspector or Minister's Delegate as applicable will ensure compliance with the requirements stated herein.

Coordination with other Transport Canada branches, such as Aircraft Certification or Commercial & Business Aviation is recommended.

Note 1: A Civil Aviation Safety Inspector or Minister's Delegate can inspect the aircraft during the evaluation of the application and on completion of the work. See STD 507.07(12).

Note 2: Pursuant to MPL 15, Minister's Delegates shall not issue a Certificate of Airworthiness or Special Certificate of Airworthiness- Restricted, in respect of an aircraft for which he has also made an application for issue or has completed an attestation of condition and conformity, or make any recommendation relating to such application or attestation.

Enhancements or questions regarding the importation standard may be made through your local Transport Canada Centre.

It will be the responsibility of the applicant to ensure that all import requirements identified in the applicable Canadian Aviation Regulations and Standards have been complied with and validated prior to making application for a Certificate of Airworthiness. Any false claims identified by Transport Canada Inspectors during their subsequent review will be forwarded directly to the Enforcement office for further action.

This section is to be completed by the APPLICANT

APPLICATION FOR A FLIGHT AUTHORITY - GENERAL (STD 507.06) All used aircraft, or new aircraft of a type not previously registered in Canada, will be inspected by a Transport Canada Civil Aviation Safety Inspector or Minister's Delegate as soon as possible after the application for a flight authority has been received; and All new aircraft and types previously registered in Canada, can be inspected by a Transport Canada Civil Aviation Safety Inspector or Minister's Delegate when considered necessary, to verify the airworthiness of the aircraft.
METHOD OF IMPORT:
a) Aircraft imported with an Export Airworthiness Certificate from a bilateral or non-bilateral country will utilize checklist 1. Note: An Export Airworthiness Certificate is NOT a flight authorization.
b) Aircraft imported without an Export Airworthiness Certificate will utilize checklist 2.
Provide the name and telephone number of the organization / person who will be responsible for the aircraft inspection and application for the Certificate of Airworthiness.
Name:			Telephone Number:
Organization:

Part 3: Checklist 1 - to be completed by the APPLICANT

3.1	The following checklist will be used where: conformity to an approved type design is shown by means of an Export Airworthiness Certificate issued by the Civil Aviation Authority of a Country with which Canada has entered into a Bilateral Airworthiness Agreement or a similar arrangement that provides for acceptance of such certificates. STD 507.07(2)(a); or conformity to an approved type design is shown by means of an Export Airworthiness Certificate issued by the civil aviation authority of a country with which Canada does not have an agreement, provided a Canadian Type Certificate has been issued and the product is being exported from the country of manufacture.
Checklist 1 - Aircraft imported with an Export Airworthiness Certificate			Comment and initials (acceptable, accomplished, N/A .)
3.1.1 (a) Was the Export Airworthiness Certificate (EAC) issued by the civil aviation authority of a country with which Canada has entered into a Bilateral Airworthiness Agreement or a similar arrangement that provides for such acceptance of such certificates? See STD 507.07 (2)(a)
(b) Was the product manufactured in Canada by an approved manufacturer to a type design specified in a Canadian type certificate and there is a Bilateral Airworthiness Agreement or similar arrangement between Canada and the country of export?
(c) Was the product, if manufactured in a country other than the country of export, manufactured to a type design certified by both the country of export and the Minister, and is there a Bilateral Airworthiness Agreement or similar arrangement between Canada and the country of export? See STD 507.07(3)(c)
(d) Was the product designed and manufactured in the country of export, type certified by the civil aviation authority of that country, and type certified under CAR 511? See STD 507.07(3)(a)
3.1.2 Was the Export Airworthiness Certificate issued by the civil aviation authority of a country with which Canada does not have an agreement, where a Canadian type certificate has been issued and the product is being exported from the country of manufacture? See STD 507.07(2)(b)
3.1.3 (a) Is the Export Airworthiness Certificate properly signed by an authorized representative of the civil aviation authority of the country of export and does it contain the following information? see STD 507.07(4)
(b) Does the Export Airworthiness Certificate identify a certification of conformity to the type design specified in the Canadian Type Certificate? See STD 507.07(4)(a)
(c) Does the Export Airworthiness Certificate include a list of any major modifications and major repairs approved by the country of export and embodied in the product? See STD 507.07(4)(b) Note 1: Confirm if major modifications or major repairs have been embodied. See STD 571.06 for definitions of major and minor. Note 2: The services of Transport Canada, Aircraft Certification may be required to familiarize any major repairs and modifications. All major repair and major modification documentation must be available for review.
(d) Does the Export Airworthiness Certificate (make reference to) list applicable airworthiness directives or equivalent notices, issued by the country of export, indicating which have been complied with? See STD 507.07(4)(c)
(e) Have all applicable airworthiness directives (or foreign equivalents) been complied with? Note: The applicant must verify that all applicable Airworthiness directives (ADs) have been complied with. If a list identifying all applicable ADs was not supplied by the exporter please provide a list of ADs that were researched and complied with by the applicant.
3.1.4 Is the aircraft cabin in an approved configuration? Note: Review against the type design and approved drawings.
3.1.5 Is the airframe, engine(s) and propeller(s) free of corrosion or within the limits prescribed by the applicable maintenance manuals? See STD 507.07(6)(d) Note: If corrosion is within limits provide complete details of location and identify the maintenance manual standards.
3.1.6 Are all aircraft systems, engines, propellers, appliances. and controls functioning properly? See STD 507.07(6)(e)
3.1.7 Have the engines, propellers, rotors, life limited components, appliances, balloon basket and burner assemblies been identified in accordance with applicable sections of CAR 201.06 to CAR 201.11? See STD 507.07(13) Note: Aeronautical products imported from a country not requiring certain identification data will require the identification data be installed prior to acceptance. See CAR 201.05(1)(2)
3.1.8 Is the approved flight manual or approved operating limitations as applicable, available for the aircraft? See STD 507.06(13)(a)
3.1.9 Is a Weight and Balance report together with an equipment not forming part of the type design available? See STD 507.06(13)(b) Note 1: The aircraft must have a current weight and balance including an equipment list that meets the requirements of STD 571 Appendix C.
3.1.10 Have all life-limited parts been researched to determine that the time in service of each life-limited part has not exceeded its maximum permitted life? See STD 507.07(6)(f) Note 1: Each life-limited component, or any product containing a life-limited component, which has seen prior service shall be accompanied by its technical record containing details of all repairs and modifications carried out during its service life, and a record of accumulated time in flying hours or cycles, as may be applicable. See STD 507.07(14) Note 2: For installation of Life Limited Parts refer to the CAR 571.09(1) and See STD 571.09
3.1.11 Has an application for a certificate of airworthiness been submitted to the Minister in accordance with CAR 507.06? See STD 507.07 and STD 507 Appendix A - Application for a CofA.
3.1.12 Has the aircraft journey log and other technical records been established for the aircraft as required by CAR 605.92?
3.1.13 Does the aircraft technical record include a listing of all applicable "supplemental instructions for continued airworthiness"?
To the best of my knowledge the information contained in the checklists is true and accurate.
Print name of applicant / representative:
Signature of applicant / representative:
Name of the Civil Aviation Safety Inspector or Minister's Delegate who verified (sampled) the above requirements. ______________________________________________________________

This part is to be completed by a TRANSPORT CANADA INSPECTOR or a MINISTER'S DELEGATE

3.1.14 (a) Will the Canadian Certificate of Airworthiness be issued?	Yes:  No: 	Date of Issue:
(b) If no, has the importer been informed in writing identifying why the aircraft did not conform to an approved type design and was not in a condition for safe operation and issuance of a flight authority?	Yes:  No: 
3.1.15 Has the importer / Transport Canada rescheduled the inspection if necessary?	Yes:  No: 	Date Rescheduled:
Remarks:

Part 3: Checklist 2 - to be completed by the APPLICANT

3.2	The following checklist will be used where conformity to an approved type design is shown by means of an airworthiness inspection to procedures detailed in STD 507.07 (5) to (12) for an aircraft which has been imported without an Export Airworthiness Certificate.
Checklist 2 - Aircraft imported without an Export Airworthiness Certificate			Comment and initials(acceptable, accomplished, N/A .)
3.2.1 Is the technical history of the aircraft sufficient? A 100 hour inspection, or equivalent shall be carried out. Note 1: "Sufficient" in relation to technical history means, as a minimum, a maintenance release or equivalent certification for each maintenance task completed within the preceding year, and technical records in sufficient detail to enable a determination of the following: - the identity of the aircraft; - the identity of each installed engine; - the identity of each installed propeller / rotor; - the identity and airworthiness status of each installed serialized component; - the time remaining before the next scheduled task on the applicable maintenance schedule; - the permissible time in service remaining for each life-limited part installed; See STD507.07(5)(a) Note 2: The aircraft owner shall submit a report to the Minister clearly detailing the inspection conducted and all additional details of the work required to bring the aircraft to a condition of conformity to the certified type design and of safe operation. See STD 507.07(7) A Civil Aviation Safety Inspector or Minister's Delegate as applicable, will evaluate the report and inspect the aircraft to determine if the work proposed will bring the aircraft to a condition of conformity and to a condition of safe operation. STD 507.07(8)
3.2.2 Is the technical history of the aircraft continuous? Note 1: If the technical history of the aircraft lacks continuity, or does not, in the opinion of the "authorized person", contain sufficient data regarding the maintenance of the aircraft, engines, or other aeronautical products, disassembly and inspection are required in addition to that required in subsection 507.07(5)(a). See STD 507.07(5)(b) Note 2: The aircraft owner shall submit a report to the Minister detailing what portions of the aircraft, engines, aeronautical products lack continuity and will require disassembly and inspection. A Civil Aviation Safety Inspector or Minister's Delegate as applicable, will evaluate the report and inspect the aircraft to determine if the work proposed will bring the aircraft to a condition of conformity and to a condition of safe operation. STD 507.07(8)
3.2.3 Is the technical history sufficient to determine the conformity and condition of the aircraft? Note 1: If the technical history of the aircraft is not sufficient to determine the conformity and condition of the aircraft, a complete overhaul is required, except those aeronautical products for which there is documentary evidence that the product has been overhauled within one year prior to the aircraft being imported. See STD 507.07(5)(c) and 507.07 (2)(d) (i, ii, iii, iv, v) Note 2: The aircraft owner shall submit a report to the Minister detailing what portions of the technical history are not sufficient to determine the aeronautical product's conformity and condition and will be overhauled. A Civil Aviation Safety Inspector or Minister's Delegate as applicable) will evaluate the report and inspect the aircraft to determine if the work proposed will bring the aircraft to a condition of conformity and to a condition of safe operation. STD 507.07(8)
3.2.4 Is the aircraft, engine(s), propeller(s) and appliances in compliance with the applicable type certificate data sheets or aircraft specifications? See STD 507.07(6)(a)
3.2.5 Is the aircraft cabin in an approved configuration? Note: Review against the type certificate and approved drawings.
3.2.6 Have all applicable airworthiness directives been complied with? See STD 507.07 (6)(b) Note: The applicant must verify that all applicable airworthiness directives (or foreign equivalents) have been complied with. A list identifying all ADs researched and complied with must accompany the import application.
3.2.7 Have all major repairs and major modifications been carried out in accordance with data acceptable to the Minister, and certified indicating that they are of an approved type and were made in accordance with accepted standards of workmanship? See STD 507.07 (2)(d)(iii) and STD 507.07(6)(c) Note 1: Confirm and list all major modifications or major repairs embodied in the product. See STD 571.06 for definitions of major and minor. Note 2: The services of Transport Canada, Aircraft Certification may be required to familiarize any major repairs and modifications. All documentation supporting a major repair or major modification must be available for review.
3.2.8 Is the airframe, engine(s) and propeller(s) free of corrosion or within the limits prescribed by the applicable maintenance standards? See STD 507.07(6)(d) Note: If corrosion is within limits, provide complete details of location and indicate the maintenance manual standards.
3.2.9 Are all aircraft systems, engines, propellers and controls functioning properly and to manufacturer's specifications? See STD 507.07(2)(d)(iv) and STD 507.07(6)(e)
3.2.10 Have the engines, propellers, rotors, life limited components, appliances, balloon basket and burner assemblies been identified in accordance with applicable sections of CAR 201.06 to CAR 201.11? See STD 507.07(13) Note: Aeronautical products imported from a country not requiring certain identification data will require the identification data be installed prior to acceptance. See CAR 201.05(1)(2)
3.2.11 Is the approved flight manual or approved operating limitations as applicable available for the aircraft? See STD 507.06(13)(a)
3.2.12 Is a Weight and Balance report together with an equipment not forming part of the type design available? See STD 507.06(13)(b) Note: The aircraft must have a current weight and balance including an equipment list that meets the requirements of STD 571 Appendix C.
3.2.13 Have all life-limited parts been researched to determine that the time in service of each life limited part has not exceeded its maximum permitted life? See STD 507.07 (6) (f) Note 1: Each life limited component, or any product containing a life limited component, which has seen prior service shall be accompanied by its technical record containing details of all repairs and modifications carried out during its service life, and a record of accumulated time in flying hours or cycles, as may be applicable. See STD (507.07)(14) Note 2: For installation of Life Limited Parts refer to the CAR 571.09(1) and see STD 571.09.
3.2.14 If the aircraft is eligible for a certificate of airworthiness, has it been brought to the required standards through the use of applicable maintenance manuals? See STD 507.07(10) Note: Reference to "required standards" is intended to ensure that any maintenance accomplished on the aircraft is done in accordance with CAR/Standard 571 with respect to performance of work.
3.2.15 Has an application for a certificate of airworthiness been submitted in accordance with CAR 507.06 See STD 507.07(11) and STD 507 Appendix A - Application for a C of A.M.
3.2.16 Have the appropriate fees been submitted with the Certificate of Airworthiness application?
3.2.17 Has the aircraft journey log and other technical records been established for the aircraft as required by CAR 605.92? Note: Has a maintenance release been provided by a person authorized pursuant to CAR 571.10 and CAR 571.11?
3.2.18 Does the aircraft technical record include a listing of all applicable "supplemental instructions for continued airworthiness"?
To the best of my knowledge the information contained in the checklists is true and accurate.
Print name of applicant / representative:
Signature of applicant / representative:
Name of Civil Aviation Safety Inspector or Minister's Delegate who verified (sampled) the above requirements.

This part is to be completed by a TRANSPORT CANADA INSPECTOR or aMINISTER'S DELEGATE

Checklist 2 - Aircraft imported without an Export Airworthiness Certificate [continued ...]
3.2.19 (a) After evaluation of the report (survey) as required by Part 3 Check List 2, sections 3.2.2, 3.2.3, 3.2.4, and inspection of the aircraft, has the Minister`s delegate or Transport Canada inspector determined that the work proposed was adequate to bring the aircraft to a condition of conformity to the certified type design and of safe operation? See STD 507.07(8)	Yes:  No: 	Comments:
(b) If no, has the importer been informed in writing identifying why the aircraft did not conform to an approved type design and was not in a condition for safe operation and issuance of a flight authority? See STD 507.07(9)	Yes:  No: 
3.2.20 Have items not corrected in the proposed work report been entered in the aircraft journey log book? Ref: CAR 605.94 and Schedule I, Item 8. Note: It is not absolutely essential that all defects found during the import inspection be corrected before the C of A is issued. Items not corrected must be entered in the journey log book as defects and an assessment made by the pilot in command to determine if the defect will adversely affect the safe flight of the aircraft. This assessment is the same for any operational aircraft.	Yes:  No: 	Date of Issue:
3.2.21 Will the Canadian Certificate of Airworthiness be issued?	Yes:  No: 	Date of Issue:
3.2.22 Has the importer / Transport Canada rescheduled the inspection if necessary?	Yes:  No: 	Date Rescheduled:
Remarks:

Part 3: Checklist 3 - to be completed by the APPLICANT

3.3	The following checklist will be used to ensure essential operating requirements are met. This checklist is applicable to aircraft imported with or without an Export Airworthiness Certificate.
Checklist 3 - All type certificated aircraft imported into Canada			Comment and initial (acceptable, accomplished, N/A .)
3.3.1 Is there available an Aircraft Flight Manual as required by the applicable standards of airworthiness? See CAR 605.04 (1) & (2)?
3.3.2 Have all Placards required by the applicable standards of airworthiness been affixed to the aircraft or attached to the component in accordance with those standards? Note 1:If the aircraft contains signs powered by tritium, reference AN B007 Note 2: See CAR 605.05 and STD 625.05(1) (a) (b) (c) (d)?
To the best of my knowledge the information contained in the checklists is true and accurate.
Print name of applicant / representative:
Signature of applicant / representative:
Name of Civil Aviation Safety Inspector or Minister's Delegate who verified (sampled) the above requirements.

Part 4: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional Airworthiness Requirements for Aeroplanes, Helicopters, and Balloons
This part identifies additional airworthiness inspection requirements for private, private passenger carrying, flight training and commercial operators of aeroplanes, helicopters, and balloons that must be complied with prior to the aircraft being operated. Note: It is important to note that not all sections are applicable, therefore, it is imperative the applicant review each area of inspection for applicability against the referenced Regulation and Standard.
Additional Airworthiness Requirements for Aeroplanes, Helicopters, and Balloons		Comment and initial (acceptable, accomplished, N/A .)
4.1 If the operator is a Part VI subpart IV (Private Operator Passenger Transportation) has the operator established and maintained an operating manual that provides guidance to crew members and in the operation of the aircraft? Note: See CAR 604.83(1) and STD 624.83		**
4.2 Has a Master Minimum Equipment List been produced for the aircraft? If yes, has the operator of the aircraft applied for a Generated Minimum Equipment List (MEL) or submitted a MEL for Approval? Note: See CAR 605.07(1), (2), (3) and STD625.07		**
4.3 If the power driven aircraft is to be operated for Day VFR flight, has the aircraft been equipped per CAR 605.14?
4.4 If the power driven aircraft is to be operated for VFR flight Over the Top (OTT), has the aircraft been equipped per CAR 605.15?
4.5 If the power driven aircraft is to be operated for Night VFR flight, has the aircraft been equipped per CAR 605.16? See STD625.16
4.6 If the power driven aircraft is to be operated for IFR flight has the aircraft been equipped per CAR 605.18?
4.7 If a balloon is to be operated for Day VFR flight, has the balloon been equipped per CAR 605.19?
4.8 If a balloon is to be operated for Night VFR flight, has the balloon been equipped per CAR 605.20?
4.9 If a glider is to be operated for Day VFR flight, has the glider been equipped per CAR 605.21?
4.10 (a) Is the aircraft equipped with a Seat and Safety Belt for each person on board the aircraft? See CAR 605.22 (1) (2) (3) Note 1: See CAR 605.23 for aircraft operated without being in compliance with CAR 605.22.
(b) Is each front seat or flight deck seat equipped with a shoulder harness? See CAR 605.24 (1) (2) (3) (4) (5) Note 2: This is not applicable for small aeroplanes manufactured before July 18, 1978. See CAR 605.24(1)
4.11 If the aircraft is Unpressurized, does it carry sufficient Oxygen for the period of flight and cabin pressure altitude? Note: For unpressurized aircraft oxygen requirements, see CAR 605.31(1).
4.12 If the aircraft is Pressurized, is it equipped with sufficient Oxygen Dispensing Units and oxygen supply to provide, in the event of cabin pressurization failure, sufficient oxygen to continue the flight to an areodrome suitable for landing? Note: For pressurized aircraft oxygen requirements, see CAR 605.31(2).
4.13 Aircraft Weight and Balance Control, STD 571 Appendix C Except where otherwise provided under the terms of a fleet empty weight and balance program referred to in subsection CAR 706.06(3), has the large aircraft been re-weighed and an updated report prepared every 5 years? See STD 625 Appendix C(8)
4.14 (a) Is a Weight and Balance report together with an equipment not forming part of the type design available? See STD 507.06(13)(b) (b) Has the weight and balance report been certified by signing a maintenance release? See STD 571 Appendix C (1)(b) (c) Is the aircraft likely to be operated in two or more different configurations? If yes is there a separate weight and balance report addendum for each configuration? See STD 571 Appendix C (3)(a) (d) Does each addendum contain a supplementary list which clearly shows the differences from the basic aircraft? See STD 571 Appendix C (3)(a)(i) (e) Does each addendum include the empty weight and center of gravity for the applicable configuration? See STD 571 Appendix C (3)(a)(ii) (f) Is each addendum clearly identified with respect to the aircraft configuration to which it applies? See STD 571 Appendix C (3)(a)(iii) Note 1: The aircraft must have a current weight and equipment? See STD 571 Appendix C (1)(a)
4.15 If the aircraft is so equipped, has the Non-Stabilized Magnetic Direction Indicator been calibrated and a dated correction card installed for each indicator at intervals not exceeding 12 months? See STD 625 Appendix C (9)(a) Note: The annual calibration may not be required if the aircraft is equipped with two independent stabilized magnetic direction indicators in addition to the non-stabilized direct reading magnetic direction indicator. Refer to STD 625 Appendix C (9)(b)(i)(ii)
4.16 (a) Has the aircraft been fitted with the Survival and Emergency Equipment required by CAR 602.59? (b) Has the equipment been overhauled at the interval recommended by the manufacture? See STD 625 Appendix C (10) Note 1: Refer to CAR 602.61 for Survival Equipment for flight over land, CAR 602.62 for life preservers and flotation devices, and CAR 602.63 for life rafts and survival equipment.
4.17 (a) Except where powered by water activated batteries, has the Emergency Locator Transmitter (ELT) been checked at intervals not exceeding 12 months? See STD 625 Appendix C (11)(a) (b) Have ELTs powered by water activation been performance tested at intervals not exceeding 5 years? See STD 625 Appendix C (11)(b) (c) Have ELT batteries been replaced at intervals recommended by the manufacturer? See STD 625 Appendix C (11)(c) (d) Has a corrosion inspection been performed on the circuit board and battery compartment? The inspection must be done by an appropriately rated shop only. See STD 571 Appendix G (e) Has the performance of the Emergency Locator Transmitters been verified in accordance with the standards identifed in STD 571 Appendix G? Note 1:Refer to CAR 605.38 (1)(2) for the quantity and type of ELT.
4.18 Has the Altimeter, Pitot and Static Pressure Systems and other altimetry devices, where installed (for compliance with the basis of certification listed on the type certificate or required by operating rule), been calibrated at intervals not exceeding 24 months? See STD 625 Appendix C (12)
4.19 (a) Has the altimeter been tested by an approved maintenance organization in accordance with STD 571 Appendix B (b)(1) for scale error, hysteresis, after effect, friction, case leak and barometric scale error? See STD 571 Appendix B (b)1(i) (ii) (iii) (iv) (v) (vi) and CAR 605.36 - Altitude Alerting System or Device (b) Has the person who performed the altimeter tests recorded on the altimeter the date and maximum altitude to which the altimeter has been tested? See STD 571 App B (c) Has the person signing the maintenance release entered the data in the aircraft record? See STD 571 Appendix B (c) (d) Has the altimeter been tested by an appropriately rated approved maintenance organization in accordance with STD 571 Appendix B (b)(1)?
4.20 (a) Has the Static Pressure System been inspected in accordance with STD 571 Appendix B? (b) Is the static system free from moisture or sources of restriction? See STD 571 Appendix B (a) (1) (c) If a static port heater is installed, is it operative? See STD 571 Appendix B(2) (d) Is there any alteration or deformity to the airframe surface that would affect the relationship between air pressure in the static pressure system and the true ambient air pressure? Refer to modifications if airframe is altered. See STD 571 App B (a) (3) (e) Has the static system been leak tested? Does it fall within the tolerances of STD 571 Appendix B (a) (4)(i)(ii)?
4.21 (a) Have air traffic control (ATC) Transponders, including any associated altitude sensing reporting mechanisms installed, been tested every 24 calendar months in accordance with STD 571 Appendix F? See CAR 605.35 and STD 625 Appendix C (13) (b) Has the performance of (ATC) transponders been verified in accordance with the standards identifed in STD 571 Appendix F? Note 1: Traffic Advisory and Collision Avoidance System (TACAS) is a requirement for flight in American airspace. Calibration of the intergrated systems may be required. Note 2: The mode S ident code can be requested through Transport Canada aircraft licensing.
4.22 If the aircraft is a turbo-jet-powered aircraft, has a Altitude Alerting System or device been installed that conforms to the Aircraft Equipment and Maintenance Standards? See CAR 605.36 and STD 625.36
4.23 Has the turbo-jet-powered aeroplane with a MCTOW of more than 33,069 pounds and operating under Subpart 4 or 5 of Part VII (Commuter or Airline Operations) been equipped with a Ground Proximity Warning System? See CAR 605.37 (1) (2) (3)
4.24 Has the turbo-jet-powered aeroplane operating under Part VII been equipped with a Standby Attitude Indicator that meets the Aircraft Equipment and Maintenance Standards. See CAR 605.41 and STD 625.41 Note: After July 31, 1997 no person shall conduct a take off in a transport category aircraft unless that aircraft is equipped with a standby attitude indicator.
4.25 (a) This section is applicable if the aircraft is a multi-engined, turbine powered, pressurized aeroplane, >12500 lb MCTOW, with passenger seating of 10 or more, manufactured after October 11, 1991. Does the aircraft have aFlight Data Recorder (FDR) installed in accordance with CAR 605.33(1)(a) (i) (ii) (iii) (b) (c)? See CAR 605.34 and STD 625.33(I)
(b) Has the FDR been maintained in accordance with a maintenance schedule, meeting the requirements identified in STD 625 Appendix C (16)? Note 1: Refer to STD 571 Appendix I for manufacturer's recommendation.
(c) Has a correlation check been conducted to ensure all required parameters are being recorded and usable at 3000 flight hours, or 12 months, whichever occurs first? See STD 625 Appendix C (16) for FDR maintenance schedule chart Note 2: See STD 625 Appendic (C) (16) for inspection and test requirements and STD 571 Appendix I for maintenance of Flight Data Recorders.
4.26 (a) This section is applicable if the aircraft is a multi-engined, turbine powered, pressurized aeroplane, >12500 lb MCTOW, with passenger seating of six or more. Does the aircraft have a Cockpit Voice Recorder (CVR) installed on board the aeroplanes or helicopters in accordance with CAR 605.33 (2)(a) (i) (ii) (iii) (b) (c)? See CAR 605.34 and STD 625.33 (II) for CVR
(b) Has the CVR been maintained in accordance with a maintenance schedule meeting the requirements identified in STD 625 Appendix C (14)?
(c) Has a functional and intelligibility check been completed in accordance with manufacturers maintenance instructions or at 3,000 hours, or 12 months, whichever comes first? See STD 625 Appendix C (14) (c) (d) (i) (ii)
4.27(a) Have the Underwater Locating Devices (ULDs) had an operational check performed once a year after initial installation? See STD 625 Appendix C (15) (b)
(b) Has the ULD been recertified at 12 month intervals? See STD 625 Appendix C (15)(c)(ii)?
(c) Has the maintenance of ULDs been performed in accordance with the recommendation of the ULD manufacturer? See STD 625 Appendix C (15)(a)
4.28 (a) Has the aircraft been maintained in accordance with a Maintenance Schedule that conforms to the Aircraft Equipment Standards and Maintenance Schedule? See CAR 605.86 (1)(a) and STD 625.86 Note: Identify the maintenance schedule used. Was the previous maintenance schedule approved? Identify approval Number and Region.		**
(b) Has the maintenance schedule been approved by the Minister where the aircraft is to be operated under Subpart 6 of IV (Flight Training Units) or under Part VII (Commercial Air Services) or is a large turbine-powered, pressurized aircraft or an airship? See CAR 605.86 (b) and STD 625.86		**
4.29 Is the maintenance schedule the aircraft will be maintained to, the same as the previous maintenance schedule? Note: If no, review CAR 605.87 - Transfer of Aeronautical Products between Maintenance Schedules, and STD 625 Appendix F		**
4.30 If the previous maintenance schedule was different from the maintenance schedule the aircraft will be maintained to, have the aeronautical products been transferred in accordance with CAR 605.87 and STD 625 Appendix F?
4.31 Have the propellers been inspected for condition at the times specified in the appropriate maintenance schedule? See STD 571 Appendix D
4.32 Have Aircraft Wooden Components been inspected in accordance with STD 571 Appendix E?
4.33 Inspect seat breakover force. Reference FAR 25.785. AC 25-17 recommends a minium horizontal breakover load of 25 lbs.
4.34 Have registration marks been affixed and are they in accordance with CAR 202.01 STD 222.01?
4.35 Has the Air Operator submitted an acceptable amendment to Transport Canada for the Air Operator Maintenance Control Manual for addition of the aircraft?		**
4.36 Has the Approved Maintenance Organization submitted an acceptable amendment to Transport Canada for the Maintenance Policy Manual?		**
4.37(a) Have Technical Records been established in accordance with CAR 605.92? Note: Journey log, separate technical record for airframe, each installed engine, and each variable pitch propeller and an empty weight and balance report. For balloons or gliders all entries in respect of the technical records may be kept in the journey log.
(b) Have entries into the technical records been accurate, legible and permanent? See CAR 605.93 (1)(a)
(c) Where a person has altered an entry on the technical record for the purpose of correcting the entry, has it been done in a manner that the underlining information remains legible? See CAR 605.93 (1) (5)
(d) If the owner of the aircraft keeps the technical records as electronic data, has the owner ensured that the electronic data system used complies with CAR 103.04 and the Aircraft Equipment and Maintenance Standards? See CAR 605.93 (2) and STD 625.93
(e) Have Technical records for the airframe, engine, propeller or component been initiated in accordance with CAR 605.96 Schedule II? See STD 625.96
(f) At the time of transfer, did the previous owner deliver to the new owner all of the technical records that related to the aeronautical product? See CAR 605.97
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements
Note: The ** items of this Part 4 may require the applicant to contact the nearest Transport Canada Center for specific approvals.
Remarks: (continued.)

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated.

Part 5 consists of 6 checklists which pinpoint specific airworthiness / operational requirements for aircraft operated under CAR Part IV Subpart 6 - Flight Training Units, Part VI Subpart 4 - Private Operator Passenger, Part VII Subpart 2 - Aerial Work, Part VII Subpart 3 - Air Taxi Operations, Part VII Subpart 4 - Commuter Operations and Part VII Subpart 5 - Airline Operations, that should be reviewed.

Additional requirements for Flight Training Units (Part IV Subpart 6)
Checklist 1, in conjunction with other applicable requirements, will apply in respect of an aeroplane, helicopter, glider, balloon, gyroplane or ultra light aeroplane used for flight training. See CAR 406.02		Comment and initial (acceptable, accomplished, N/A .)
5.1.1 Does the aircraft to be used for flight training meet the requirements of Part IV Subpart 5? See CAR 405.23 and STD 425.23
5.1.2 Is the aircraft equipped with either a turn and slip indicator or a turn coordinator? See STD 425.23
5.1.3 If a helicopter is to be used for dual flight instruction, is it equipped with an intercom system? See STD 425.23
5.1.4 If the aeroplane, helicopter or gyroplane is used for instrument flight training, is it equipped with an attitude indicator, vertical speed indicator and gyroscopic direction indicator? See STD 425.23
5.1.5 If the aeroplane or helicopter is used for radio navigation training, is it equipped with an ADF, VOR or GPS radio navigation aid receiver? See STD 425.23
5.1.6 If the aircraft is to be used for instrument training, is it equipped in accordance with requirements for IFR flight as outlined in CAR 605.18?
5.1.7 Is each front seat of an aeroplane or helicopter to be used by a trainee or flight instructor equipped with a safety belt that See CAR 406.33
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional requirements for Private Operator Passenger Transportation (Part VI Subpart 4)
Checklist 2, in conjunction with other applicable requirements, will apply in respect of the operation of a Canadian aircraft that is used for the transport of passengers, where the aircraft is a turbine powered pressurized aeroplane and is not required to be operated under Subpart 6 of Part IV (Flight Training Units) or under Part VII (Commercial Air Services)		Comment and initial (acceptable, accomplished, N/A .)
5.2.1 Does the private operator maintain his aircraft in accordance with the requirements of CAR 604 Division VI (Maintenance) and CAR 605 (Aircraft Requirements)? See CAR 604.07 (d)
5.2.2 Has the aeroplane been equipped with Life Preservers, Flotation Devices, Life Rafts and Survival Equipment pursuant to sections 602.61 and 602.63? See STD 624.38 and STD 625 Appendix C (10)
5.2.3 Is the aircraft equipped with the correct numbers of First Aid Kits and does each kit meet the Private Operator Passenger Transportation Standards required by CAR 604.39? See STD 624.39
5.2.4 Is the private operators aircraft pressurized and will it carry flight attendants? Has Protective Breathing Equipment been installed that will provide 15-minute of breathing gas at a pressure altitude of 8000 feet? See CAR 604.40
5.2.5 Is the aircraft equipped with the correct type and numbers of Hand Held Fire Extinguishers for use in the passenger compartment and where applicable, cargo compartment? See CAR 604.41
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional requirements for Aerial Work operations (Part VII Subpart 2)
Checklist 3, in conjunction with other applicable requirements, will apply in respect of the operation of an aeroplane or helicopter in aerial work involving the carriage on board of persons other than flight crew members, the carriage of helicopter Class B, C or D external loads, towing of objects other than a glider towing operation conducted by a flight training unit, and the dispersal of products. See CAR 702.01 (1)		Comment and initial (acceptable, accomplished, N/A .)
5.3.1 Is the air operator's aircraft pilot seat and any seat Harness? See CAR 702.44
5.3.2 Is the aircraft equipped with an External Load Equipment device authorized in a supplemental type certificate or in an airworthiness approval relating to the operational configuration of the aircraft? See CAR 702.45
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional requirements for Air Taxi Operations (Part VII Subpart 3)
Checklist 4, in conjunction with other applicable requirements, will apply in respect of the operation by a Canadian air operator, in an air transport service or in aerial work involving sightseeing operations, of a single engine aircraft or multi-engined aircraft, other than a turbo-jet-powered aeroplane, that has a MCTOW of 8618 kg (19000 lbs) pounds or less and a seating configuration, excluding pilot seats, of nine or less. See CAR 703.01		Comment and initial (acceptable, accomplished, N/A .)
5.4.1(a) Is the aircraft equipped with a power failure warning device or vacuum indicator to show the power available for gyroscopic instruments from each power source? See CAR 703.64 (a)
(b) Is the aircraft equipped with an alternate source of static pressure for the altimeter, airspeed and vertical speed indicators? See CAR 703.64 (b)
(c) Is the aircraft equipped with two generators, each of which is driven by a separate engine or by a rotor drive train? See CAR 703.64 (c)
(d) Is the aircraft equipped with two independent sources of energy, at least one of which is an engine driven pump? See CAR 703.64 (d)
(e) Is the aircraft equipped with at least one landing light? See CAR 703.64 (2)
5.4.2 Is the air operator's pressurized aircraft equipped with Protective Breathing Equipment that will provide 15-minute supply of breathing gas at a pressure altitude of 8000 feet at each flight crew member position? See CAR 703.67
5.4.3 If the air operator will carry passengers above FL 250, has First Aid Oxygen been provided in accordance with CAR 703.68?
5.4.4 Is the air operator's aircraft pilot seat and any seat Harness? See CAR 703.69
5.4.5 For Air Taxi Helicopter Operators, is the helicopter equipped with the emergency equipment pursuant to Division II of Part IV Subpart 2? Note: Refer to CAR 703.82 and STD 723.82(1) (2) for survival equipment and first aid kit content.
5.4.6 For Air Taxi Aeroplane Operators utilizing single engine aeroplanes in IFR and night VFR in accordance with CAR 723.22(1)(2); (a) Is the aeroplane turbine powered? Note: For the carriage of passengers in IFR and night VFR, aeroplanes must be turbine powered.
(b) Does the turbine engine have a proven Mean Time Between Failure (MTBF) of .01/1000 or less established over 100,000 hours in service?
(c) Does the aeroplane have two attitude indicators which are powered separately and independently from each other?
(d) Does the aeroplane have two power generation sources, either of which is capable of sustaining essential flight instruments and electrical equipment?
(e) Does the aeroplane have an auto ignition system?
(f) Does the aeroplane have a chip detector system capable of warning the pilot of excessive ferrous material in the engine lubrication system?
(g) Does the aeroplane have a radar altimeter?
(h) Does the aeroplane have a manual throttle which bypasses the governing section of the fuel control unit and permits unrestricted operation of the engine in the event of a fuel control unit failure?
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional requirements for Commuter Operations (Part VII Subpart 4)
Checklist 5, in conjunction with other applicable requirements, will apply in respect of the operation by a Canadian air operator, in an air transport service or in aerial work involving sightseeing operations, of a multi-engined aircraft that has a MCTOW of 8618 kg (19000 lbs) or less and a seating configuration, excluding pilot seats, of 10 to 19, or a turbo-jet-powered aeroplane that has a maximum zero fuel weight of 22680kg (50000 pounds) or less and for which a Canadian Type certificate has been issued authorizing the transport of not more than 19 passengers. See CAR 704.01		Comment and initial (acceptable, accomplished, N/A .)
5.5.1(a) Is the aircraft equipped with at least two generators, each of which is driven by a separate engine and at least half of which have a sufficient rating to supply the electrical loads of all instruments and equipment necessary for safe emergency operation of the aircraft? See CAR 704.62 (1)(a) Note: For multi engine helicopters, the generators may be driven by the main rotor drive train. See CAR 704.62 (2)
(b) Is the aircraft equipped with two independent sources of energy and a means of selecting either source, at least one source of energy being an engine-driven pump or generator, and each source being able to drive all gyroscopic instruments? See CAR 704.62 (1)(b)
(c) Is the aircraft equipped with at least one landing light? See CAR704.62 (3)
5.5.2 Is the air operator's pressurized aircraft equipped with Protective Breathing Equipment that will provide 15-minute supply of breathing gas at a pressure altitude of 8000 feet at each flight crew member position? See CAR 704.66
5.5.3 If the air operator will carry passengers above FL 250, has First Aid Oxygen been provided in accordance with CAR 704.67?
5.5.4 Is the air operator's aircraft pilot seat and any seat Harness? See CAR 704.68
5.5.5 Is there at least one Hand Held Fire Extinguisher accessible for immediate use and is it located in the passenger compartment? See CAR 704.83
5.5.6 Has the operator equipped the aeroplane with emergency equipment pursuant to Division II of Part VI Subpart 2? See CAR 704.84, STD 724.84(1)(2)(3), STD 624.38 and STD 625 Appendix C (9)
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements

Part 5: as applicable, this part may be completed by the APPLICANT prior to the aircraft being operated

Additional requirements for Airline Operations (Part VII Subpart 5)
Checklist 6 in conjunction with other applicable requirements, will apply in respect of the operation by a Canadian air operator, in an air transport service or in aerial work involving sightseeing operations of an aeroplane other than an aeroplane authorized to operate under Subpart 4, that has a MCTOW of more than 8618 kg (19000 lbs) for which a Canadian Type Certificate has been issued authorizing the transport of 20 or more passengers, or a helicopter that has 20 or more passenger seats. See CAR 705.01		Comment and initial (acceptable, accomplished, N/A .)
5.6.1(a) Is the aircraft equipped with two independent static pressure systems? See CAR 705.67 (a)
(b) Is the aircraft equipped with a windshield wiper or rain removal system for each pilot station? See CAR 705.67 (b)
(c) Is the aircraft equipped with heating or de-icing equipment for each carburator or an alternate air source for each pressure carburator or fuel injection system? See CAR 705.67 (c)
(d) Is the aircraft equipped with a placard on each door that provides passenger access to a passenger emergency exit, stating that the door must be secured or locked open during take-off and landing. See CAR 705.67 (d)
5.6.2 If the aircraft is to be operated at night, is the aircraft equipped with two Landing Lights? See CAR 705.68
5.6.3 If the aircraft is to be operated into known Icing Conditions at night, is the aeroplane equipped with a means to illuminate or detect the formation of ice? See CAR 705.69 (2)
5.6.4 If the aircraft is pressurized, has Protective Breathing Equipment been provided at each station that will provide 15 minutes of breathing gas at a pressure altitude of 8000 feet? See CAR 705.71
5.6.5 If the aircraft is pressurized and will carry passengers, has First Aid Oxygen been provided? See CAR 705.72
5.6.6 Is the aircraft equipped with an Interphone System that can be operated independently of the public address system? See CAR 705.73
5.6.7 Is the aircraft equipped with a Public Address System that can be operated independently of the interphone system? See CAR 705.74
5.6.8 Are all pilot seats and seats for each flight attendant upper torso straps with single point release? See CAR 705.75
5.6.9 Has the aircraft been equipped with Lavatory Fire Equipment in accordance with CAR 705.76?
5.6.10 If the aircraft was initially type certificated after January 1, 1958, do all passenger compartment seat cushions meet the standards respecting Flammability Requirements for Aeroplane Seat Cushions set out in Standard 525? See CAR 705.77
5.6.11 If the aircraft was initially type certificated after January 1, 1958, has the aeroplane been equipped with Floor Proximity Emergency Escape Path Markings that meet the standards set out in Standard 525? See CAR 705.78
5.6.12 Is the aircraft cargo and baggage compartment in compliance with Fire Protection requirements in accordance with CAR 705.81? See STD 725.81
5.6.13 If the aircraft is type certified to carry 60 or more passengers, have Portable Megaphones been installed in accordance with CAR 705.89?
5.6.14 Is the aircraft equipped with the correct numbers of First Aid Kits required by CAR 705.90? See STD 725.90
5.6.15 If the aircraft has a seating configuration of more than 100 passengers, has the aeroplane been equipped with an Emergency Medical Kit in accordance with CAR 705.91? See STD 725.91
5.6.16 Is the aircraft equipped with a Crash Axe? See CAR 705.92
5.6.17 Is the aircraft equipped with the correct type and numbers of Hand Held Fire Extinguishers required by CAR 705.93?
5.6.18 If the aircraft is pressurized and will operate above FL 250, has the aeroplane been equipped with 15 minute supply portable oxygen or sufficient portable oxygen units for each flight attendant? See CAR 705.94
5.6.19 Has the air operator equipped the aeroplane with survival equipment pursuant to CAR 602.61 and CAR 602.63? See CAR 705.95, STD 705.95 and STD 625 Appendix C (9)
5.6.20 Has the survival equipment been inspected regularly in accordance with the inspection schedule set out by the company operations manual? Note: See CAR 705.96 and STD 625 Appendix C (9)
Remarks:
Print name of applicant / importer who verified all the above requirements
Signature of applicant / importer who verified all the above requirements