The following table lists exemptions that have been issued by the Aircraft Certification Standards in Headquarters or that affect aircraft certification activities in Headquarters.
This table does not identify exemptions issued by a regional Aircraft Certification Office or by another Civil Aviation Branch. For information on these exemptions refer to the Exemptions to the Canadian Aviation Regulations.
For further information, please contact the Manager, Domestic Regulations, Aircraft Certification Standards at 613-941-8382 or email aartc-d@tc.gc.ca.
| Exemption No. | Issue Date (dd-mm-yyyy) | Exempted Provision | Issuing Office | Petitioner Company | Aircraft Model | TC/STC/LSTC No. | Purpose | Status | RDIMS # |
|---|---|---|---|---|---|---|---|---|---|
| 017-2024 | 17-06-2024 | CAR 521.158(1) and AWM 533.27(f)(6) | AARD | Pratt&Whitney Canada | Model Engine: PW127XT-S | E-19 |
The purpose of this exemption is to permit P&WC to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the P&WC engine PW127XT-S, where the amended type design to be approved contains design features that do not comply with the applicable standards of airworthiness for the High Pressure Turbine (HPT) shaft. The proposed major change would exclude the entire HP rotor shaft system from consideration in determining the highest overspeed that would result from a complete loss of load on a turbine rotor. The proposed major change would include a HP rotor shaft system that does not comply with paragraph 533.27(f)(6). In particular, this exemption is intended to provide relief from the provisions specified under this exemption to allow P&WC to field a HP rotor shaft system with safety-related improvements as compared to the presently approved design. |
Approved | 20246983 |
| 031-2023 | 12-12-2023 | CAR 521.158(1) and AWM 525.1301(a)(1) and (a)(4), 525.1309(a), 525.1309(a) and (b), and paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness 2013-03 | AARD | Airbus Canada Limited Partnership | BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300) | A-236 |
The purpose of this exemption is to permit ACLP to continue to deliver new ACLP model BD-500-1A11 (marketing designation “A220-300”) aeroplane, where the amended type design approval contains design features that do not comply with the applicable standards of airworthiness for software that performs required flight management functions. The type design includes Flight Management System (FMS) application software “Build 8A2”. The type design includes an FMS with embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM, as well as paragraphs 4. (a) and (c)(2) of SCA 2013-03. In particular, this exemption is intended to provide relief from the provisions specified under this exemption to allow ACLP to continue to field an FMS application software “Build 8A2”. |
Approved | 19806058 |
| 030-2023 | 12-12-2023 | CAR 521.158(1) and AWM 525.1301(a)(1) and (a)(4), 525.1309(a), 525.1309(a) and (b), and paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness 2013-03 | AARD | Airbus Canada Limited Partnership | BD-500-1A10 (Marketing designation “A220-100”, formerly the CS100) | A-236 |
The purpose of this exemption is to permit ACLP to continue to deliver new ACLP model BD-500-1A10 (marketing designation “A220-100”) aeroplane, where the amended type design approval contains design features that do not comply with the applicable standards of airworthiness for software that performs required flight management functions. The type design includes Flight Management System (FMS) application software “Build 8A2”. The type design includes embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM, as well as paragraphs 4. (a) and (c)(2) of SCA 2013-03. In particular, this exemption is intended to provide relief from the provisions specified under this exemption to allow ACLP to continue to field an FMS application software “Build 8A2”. |
Approved | 19906577 |
| 054-2021 | 11-12-2021 | CAR 521.158(1) and AWM 533.27(f)(6) | AARD |
Pratt&Whitney Canada |
PW12XT Engine Models: PW127XT-M, PW127XT-N and PW127XT-L |
E-19 |
The purpose of this exemption is to permit P&WC to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the P&WC engine models PW127XT-M, PW127XT-N and PW127XT-L (marketing designation “PW127XT”), where the amended type design to be approved contains design features that do not comply with the applicable standards of airworthiness for the High Pressure Turbine (HPT) shaft. The proposed major change would exclude the entire HP rotor shaft system from consideration in determining the highest overspeed that would result from a complete loss of load on a turbine rotor. The proposed major change would include a HP rotor shaft system whose demonstrated design does not permit a complete showing of compliance to H3paragraph 533.27(f)(6). |
Approved |
17572323 |
| 110-2020 | 05-11-2020 | CAR 605.26(1) | AAR | N/A | N/A | N/A | The purpose of this exemption is to permit all passengers to use on Canadian aircraft Child Restraint System devices that are foreign-approved to design standards not included in paragraph 551.501(b)(1) of the AWM. | Approved | 16928170 |
| 053-2020 | 29-06-2020 | CAR 521.158(1) and AWM 525.1301(a)(1) and (a)(4), 525.1309(a), 525.1309(a) and (b), and paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness 2013-03 | AARD | Airbus Canada Limited Partnership | BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300) | A-236 | The purpose of this exemption is to permit ACLP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the ACLP model BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300). The purpose of the major design change is to introduce a new Flight Management System (FMS) Build 8A2 to replace Build 8A1. This exemption supersedes Exemption No. NCR-029-2018 in the TCDS and renders the type design eligible for a CAR 507.02 Certificate of Airworthiness or a CAR 509 Export Airworthiness Certificate after June 30, 2020. The approved change to the type design includes a Flight Management System (FMS) with embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM as well as paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness (SCA) 2013-03. | Approved | 16497767 |
| 040-2020 | 29-06-2020 | CAR 521.158(1) and AWM 525.1301(a)(1) and (a)(4), 525.1309(a), 525.1309(a) and (b), and paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness 2013-03 | AARD | Airbus Canada Limited Partnership | BD-500-1A10 (Marketing designation “A220-100”, formerly the CS100) | A-236 | The purpose of this exemption is to permit ACLP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the ACLP model BD-500-1A10 (Marketing designation “A220-100”, formerly the CS100). The purpose of the major design change is to introduce a new Flight Management System (FMS) Build 8A2 to replace Build 8A1. This exemption supersedes Exemption No. NCR-028-2018 in the TCDS and renders the type design eligible for a CAR 507.02 Certificate of Airworthiness or a CAR 509 Export Airworthiness Certificate after June 30, 2020. The approved change to the type design includes a Flight Management System (FMS) with embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM as well as paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness (SCA) 2013-03. | Approved | 16502074 |
| 019-2019 | 03-07-2019 | CAR 521.158(1) and PARAGRAPHS 5(b)(1) AND 19(b)(1) OF THE UNITED STATES (U.S.) SPECIAL FEDERAL AVIATION REGULATION (SFAR) No. 23, AS AMENDED BY SFAR 23-1 | AARD | Viking Air Limited | DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models | A-82 | The purpose of this exemption is to permit Viking to obtain a design change approval for the DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models incorporating type design changes recorded in Viking Report AEROC 6.1.G.11 DHC-6 Certified Airplane – Basic Definition, where the design change to be approved contains design features that do not comply with the applicable standards of airworthiness for “Takeoff speeds” and “Operating limitations – Takeoff weight limitations” in accordance with SFAR 23-1. In particular, this exemption is intended to provide relief from paragraphs 5(b)(1) and 19(b)(1) of SFAR 23-1, which require that the decision speed V1 be a ground speed (and not an airborne speed) and that the all-engines operating take-off distance at maximum take-off weight be determined accordingly. This exemption is intended to permit the approval of an aeroplane flight manual supplement (AFMS) containing Reduced Ground Roll – 20 Degree Flap Take-Off (RGRTO) procedures and performance data, where V1 is permitted to be an airborne speed. The use of the RGRTO AFMS procedures and performance data allows the aeroplane to become airborne with a minimum ground roll, in order to facilitate operations on short and/or unprepared (rough/soft) surfaces, such as may be encountered when conducting flight operations from remote and sparsely settled locations. |
Approved | 15076236 |
| 005-2019 | 25-02-2019 | CAR 521.158(1) and AWM 525.841(a)(2)(i) AND (3) | AARD | Airbus S.A.S. | A321-271N and A321-272N (A321neo), and models A321-271NX and A321-272NX (A321neo ACF) | A-166 | The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include new engine option (NEO) aeroplane models A321-271N and A321-272N (A321neo models) and Airbus “Cabin-Flex” option aeroplane models A321-271NX and A321-272NX (A321neo ACF models), which contain design features that do not fully comply with the applicable standards of airworthiness for “Pressurized Cabins” in accordance with paragraphs 525.841(a)(2)(i) and (3) of the AWM [Change 525-22]. In particular, these aeroplane models contain design features that allow the cabin pressure altitude to exceed 25,000 feet for more than 2 minutes, following a decompression that results from an uncontained engine failure condition, whereby the applicable standards of the AWM are not met. This exemption provides relief from the requirements of paragraphs AWM 525.841(a)(2)(i) and (3) [Change 525-22] for uncontained engine rotor failure (UERF) scenarios. | Approved | 14960745 |
| 002-2019 | 17-09-2019 | CAR 521.158(1) and AWM 525.807(g)(7) | AARD | Airbus S.A.S. | A321-271NX and A321-272NX (A321neo ACF) | A-166 | The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include Airbus “Cabin-Flex” option aeroplane models A321-271NX and A321-272NX (A321neo ACF models), which contain design features that do not comply with the applicable standards of airworthiness of the AWM [Change 525-23] specifying the maximum number of passenger seats permitted for all Type III exits. In particular, the proposed design exceeds the standard limit of 70 passenger seats permitted for all Type III exits, and therefore does not meet the standard. This exemption provides partial relief from 525.807(g)(7) of the AWM [Change 525-23] by targeting exclusively the provision limiting the maximum number of passenger seats permitted for all Type III exits. | Approved | 15103556 |
| 040-2018 | 13-09-2019 | CAR 521.158(1) and AWM 525.981(b)(2) | AARD | Cascade Aerospace Inc. | Bombardier DHC-8-402 | A-142 | Following our review, Transport Canada has determined that an exemption from AWM 525.981(b)(2) to allow approval of a change to the type design of the aeroplane model DHC-8-402 for the installation of an auxiliary fuel system, is not necessary. Based on our review of the design proposed and the Federal Aviation Administration Notice of Proposed Rulemaking and Final Rule justification for the adoption of the amendment 25-125 to 14 CFR part 25, which is the source code for AWM 525.981, the exception in subparagraph (b)(2) is not applicable. In consideration of the above, your request for an exemption from subsection 521.158(1) of the CARs with respect to paragraph 525.981(b)(2) of the AWM is therefore denied. |
Denied | 15088329 |
| 031-2018 | 08-01-2019 | CAR 521.158(1) and AWM 525.809(a) | AARD | Airbus S.A.S. | A321neo ACF aeroplane models (including any models designated as A321-2**NX) | A-166 | The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include new A321neo ACF aeroplane models (including any models designated as A321-2**NX), which have design features that do not fully comply with the applicable standards of airworthiness for “Emergency Exit Arrangement” in accordance with paragraph 525.809(a) of the AWM [Change 525-23]. In particular, this exemption is intended to provide relief from the requirement from paragraph 525.809(a) to provide a means of viewing the likely areas of evacuee ground contact prior to opening the over-wing emergency exits. This exemption does not provide relief from other aspects of 525.809(a). | Approved | 14689069 |
| 030-2018 | 17-01-2019 | CAR 521.158(1) and AWM 525.841(a)(2)(i) and (3) | AARD | Airbus S.A.S. | Airbus A321-271N and A321-272N (A321neo), and models A321-271NX and A321-272NX (A321neo ACF) | A-166 | The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include new engine option (NEO) aeroplane models A321-271N and A321-272N (A321neo models) and Airbus “Cabin-Flex” option aeroplane models A321-271NX and A321-272NX (A321neo ACF models), which contain design features that do not fully comply with the applicable standards of airworthiness for “Pressurized Cabins” in accordance with paragraphs 525.841(a)(2)(i) and (3) of the AWM [Change 525-22]. In particular, these aeroplane models contain design features that allow the cabin pressure altitude to exceed 40,000 feet, and to exceed 25,000 feet for more than 2 minutes, after decompression from any uncontained engine failure condition not shown to be extremely improbable, whereby the applicable standards of the AWM are not met. This exemption does not permit a non-compliance with AWM 525.841(a) for any other system and structural failure events not shown to be extremely improbable. | Approved | 14744000 |
| 029-2018 | 14-12-2018 | CAR 521.158(1) and AWM 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) | AARD | CSALP | BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300) | A-236 | The purpose of this exemption is to permit CSALP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the CSALP model BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300). The purpose of the major change is to replace the current TCDS limitation, resulting from the application of conditions contained in Exemption NCR-039-2016, that renders the type design ineligible for a new CAR 507.02 Certificate of Airworthiness or a new CAR 509 Export Airworthiness Certificate after December 31, 2018. The approved type design includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to paragraphs 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. | Approved | 14670338 |
| 028-2018 | 14-12-2018 | CAR 521.158(1) and AWM 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) | AARD | CSALP | BD-500-1A10 (Marketing designation “A220-100”, formerly the CS100) | A-236 | The purpose of this exemption is to permit CSALP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the CSALP model BD-500-1A10 (Marketing designation “A220-100”, formerly the CS300). The purpose of the major change is to replace the current TCDS limitation, resulting from the application of conditions contained in Exemption NCR-008-2016, that renders the type design ineligible for a new CAR 507.02 Certificate of Airworthiness or a new CAR 509 Export Airworthiness Certificate after December 31, 2018. The approved type design includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to paragraphs 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. | Approved | 14670583 |
| 027-2018 | 07-01-2019 | CAR 521.158(1) and AWM 525.785(b) and 525.562 | AARD | Conair Group Inc. | Bombardier aeroplane model DHC-8-402 | The purpose of this exemption is to permit Conair Group Inc. to obtain a supplemental type certificate (STC) for the Bombardier aeroplane model DHC-8-402, where the change to the type design to be approved contains design features that do not comply with the applicable standards of airworthiness for the protection from serious injury during emergency landing conditions for occupants of berths intended for a non-ambulant persons. | Approved | 14566185 | |
| 024-2018 | 14-09-2018 | CAR 521.158(1) and AWM 525.1322(a)(2) | AARD | Bombardier Inc. | BD-700-2A12 (Global 7000) | A-177 | The purpose of this exemption is to permit Bombardier to obtain an amended type certificate to include the Bombardier aeroplane model BD-700-2A12 (marketing designation “Global 7000”), where the type design to be approved contains design features that do not comply with the applicable standards of airworthiness for flight crew alerting. In particular, this exemption is intended to provide relief until December 31, 2020 from the provisions of paragraph 525.1322(a)(2) of the AWM, to allow Bombardier additional time to incorporate a design improvement into the Engine Indicating and Crew Alerting System (EICAS). Paragraph 525.1322(a)(2) specifies that flight crew alerts must be readily and easily detectable and intelligible by the flight crew under all foreseeable operating conditions, including conditions where multiple alerts are provided. This exemption permits approval of a type design where the L (R) ENG FLAMEOUT (Caution) messages are inhibited during the take-off and landing phases of flight. | Approved | 14412022 |
| 020-2018 | 27-09-2018 | CAR 521.158(1) and AWM 525.1447(c)(1) | AARD | Bombardier Inc. | BD-700-2A12 (Global 7000) | A-177 | The purpose of this exemption is to permit Bombardier and any design approval applicant to obtain an amended type certificate or supplemental type certificate to include aeroplane model BD-700-2A12 (marketing designation “Global 7000”), which contains design features that do not comply with the applicable standards of airworthiness, where certification for operation above 30,000 feet is requested, for the automatic presentation of oxygen dispensing units to occupants of the cabin before the cabin pressure exceeds 15,000 feet, in accordance with paragraph 525.1447(c)(1) of the AWM [Change 525-22]. In particular, and in consideration of the possibility of this aeroplane model to conduct high-altitude airport operations into airports constructed at elevations greater than 13,800 feet above sea level, this exemption is intended to provide relief from the application of the subject provision in order to prevent nuisance presentation of the oxygen dispensing units when operating at high-altitude airports. This exemption would permit the dispensing units providing the required oxygen flow to be automatically presented to the occupants before the cabin pressure altitude exceeds 17,000 feet. | Approved | 14050635 |
| 023-2017 | 21-12-2017 | CAR 521.158(1) and FAR 25.783 | AARD | Field Aviation Company Inc. | Bombardier CL-600-2C10 (CRJ-700) aeroplane, serial number 10343 | The purpose of this exemption is to permit Field Aviation to obtain a supplemental type certificate for the Bombardier model CL600-2C10 (CRJ-700) aeroplane, serial number 10343, in respect of a modified cargo door installation, where a full showing of compliance to 14 CFR 25.783 has not fully been completed. | Approved | 13436383 | |
| 016-2017 | 21-12-2017 | CAR 521.158(1) and SFAR 23.5(b)(1) and 19(b)(1) | AARD | Viking Air Limited | DHC-6 "Twin Otter" Series 400 as well as series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models | A-82 | The purpose of this exemption is to permit Viking to obtain a design change approval in respect of an aeroplane flight manual supplement containing Reduced Ground Roll – 20 Degree Flap Take-Off procedures and performance data for the DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models incorporating type design changes recorded in Viking Report AEROC 6.1.G.11 DHC-6 Certified Airplane – Basic Definition to comply with SFAR 23-1, without fully complying with the applicable standards of airworthiness for “Takeoff speeds” and “Operating limitations – Takeoff weight limitations” in accordance with SFAR 23-1. | Approved | 13104405 |
| 013-2017 | 26-06-2018 | CAR 521.158(1) and AWM 525.809(a) | AARD | Bombardier Inc. | BD-700-2A12 (Global 7000) | A-177 |
The purpose of this exemption is to permit Bombardier to obtain an amended type certificate to include a new aeroplane model BD-700-2A12 (Global 7000), which contains design features that do not fully comply with the applicable standards of airworthiness for “Emergency Exit Arrangement” in accordance with paragraph 525.809(a) of the AWM [Change 525-22]. In particular, this exemption is intended to provide relief from paragraph 525.809(a) of the AWM requirements in the following three scenarios:
|
Approved | 13125032 |
| 003-2017 | 22-02-2017 | CAR 605.84(1)(b) | AAR | all users of Helicopter External Transport System (HETS) conducting or permitting a take-off in a helicopter that does not meet Part I, Paragraph (B) of Airworthiness Directive (AD) CF-2014-26 | N/A | N/A | The purpose of this exemption is to allow all users of Helicopter External Transport System (HETS) to conduct or permit a take-off in a helicopter that does not meet the requirements of Part I, Paragraph (B) of AD CF-2014-26. | Approved | 12675976 |
| 096-2016 | 08-11-2016 | CAR 521.158(1) and FAR section 25.783 | AARD | Field Aviation Company Inc. | Bombardier CL-600-2C10 (CRJ-700) aeroplane, serial number 10343 | The purpose of this exemption is to permit Field Aviation to obtain a supplemental type certificate for the Bombardier model CL600-2C10 (CRJ-700) aeroplane, serial number 10343, where the design change to be approved includes a modified cargo door installation for which a full showing of compliance to 14 CFR 25.783 has not fully been completed. | Approved | 12332306 | |
| 039-2016 | 07-07-2016 | CAR 521.57(2)(a) and AWM 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) | AARD | Bombardier Inc. | BD-500-1A11 (CS300) | A-236 | The purpose of this exemption is to permit Bombardier to obtain a type certificate for the Bombardier CSeries aeroplane model BD-500-1A11 (CS300), where the type design to be approved includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to paragraphs 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. | Approved | 11960942 |
| 008-2016 | 13-05-2016 | CAR 521.158(1) and AWM 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) | AARD | Bombardier Inc. | BD-500-1A10 (CS100) | A-236 | The purpose of this exemption is to permit Bombardier to obtain an amended type certificate for the Bombardier CSeries aeroplane model BD-500-1A10 (CS100), where the amended type design to be approved includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. | Approved | 11538406 |
| 085-2015 | 17-12-2015 | CAR 521.33 and AWM 525.177(d), 525.251(d), 525.671(c)(1), 525.735(b)(1), 525.735(c)(1), 525.783(h)(4), 525.810(a)(2), 525.810(c), 525.856(b), 525.903(e), 525.981(a), 525.1301(a)(1), 525.1302(c)(1), 525.1309(a), 525.1309(b), 525.1309(c) 525.1309(d), 525.1459(a)(2) and 525.1523; as well as SCA 2013-03 | AARD | Bombardier Inc. | BD-500-1A10 (CS100) | A-236 | The purpose of this exemption is to permit Bombardier to obtain a "baseline" type certificate for the Bombardier Cseries earoplane model BD-500-1A10 (CS100), where the type design to be approved under the type certificate has yet to be shown to meet all applicable standards of the basis of certification. | Approved | 11284465 |
| 080-2015 | 26-10-2015 | CAR 521.31(1)(d) and AWM 525.981(a)(3) | AARD | Bombardier Inc. | CL-600-2E25 (CRJ 1000) | A-131 | The purpose of this exemption is to allow Bombardier to continue to hold a valid type certificate (No. A-131) that includes the CL-600-2E25 (CRJ 1000) model aeroplane, without a complete showing of compliance to 525.981(a)(3) of the AWM, where the structural aspects of the fuel tank system have not yet been demonstrated to have two independent means of lightning protection. | Approved | 10938643 |
| 078-2015 | 30-11-2015 | CAR 605.26(1) | AAR | N/A | N/A | N/A | The purpose of this exemption is to permit all passengers using a Child Restraint System foreign-approved to design standards not included in paragraph 551.501(b)(1) of the AWM, all passengers responsible for an infant and all passengers responsible for a person using a Child Restraint System foreign-approved to design standards not included in paragraph 551.501(b)(1) of the AWM to satisfy their requirements under subsection CAR 605.26(1). | Approved | 11111826 |
| 036-2015 | 22-01-2016 | CAR 521.158 and FAR paragrah 25.561 (c) | AARD | B/E Aerospace | Bombardier CL-600-2B16 | The purpose of this exemption is to allow the installation of an incubator unit without demonstrating restraint of its plastic cover, where the applicable standards of airworthiness of 14 CFR 25.561(c) would not be met. | Denied | 11133461 | |
| 034-2015 | 10-07-2015 | CAR 521.158 and FAR paragraph 25.787(a) | AARD | DECA Aviation Engineering Limited | DHC-8-315 aeroplane, Serial Number 609 | STC No. Q-LSA 15-014/D | The purpose of this exemption is to allow DECA Aviation Engineering Limited to modify a Bombardier Inc. model DHC-8-315 aeroplane, Serial Number 609, to a Medivac configuration that uses a net to enclose the stowage area in the passenger cabin rather than a solid partition, such that the stowage area enclosure requirements of the applicable standards in 14 CFR part 25 for aeroplanes with passenger seating of 10 or more are not met. | Approved | 10241638 |
| 005-2015 | 02-03-2015 | CAR 602.63(7)(a) | AAR | N/A | N/A | N/A | The purpose of this exemption is to permit Canadian offshore aircraft operators the use of a new HPTSS that meets the minimum performance specification of CAN-TSO-3C503 in lieu of older helicopter passenger suit system that are currently acceptable in accordance with section 551.407 of the AWM. | Approved | 10306906 |
| 045-2013 | 15-10-2013 | CAR 521.158 and FAR25.783(g) | AARD | Northeast Engineering and Development Limited (NEDL) | CL600-2B16 | A-131 | The purpose of this exemption is to permit the issuance of the corresponding Supplemental Type Certificate (STC) to NEDL for the installation of a loading ramp, which facilitates the loading of medical stretchers on the Bombardier model CL600-2B16 aeroplane without fully complying with the original design requirements for emergency exits. | Approved | 8636530 |
| 063-2012 | 22-08-2013 | CAR 521.31(1)(d) and AWM 525.809(a) | AARD | Bombardier Inc. | BD-500-1A10 (CSeries CS100) and BD-500-1A11 (CSeries CS300) | A-236 | The purpose of this exemption is to permit the CSeries to contain design features that, in the case of non-overwing passenger emergency exits, do not allow viewing of the likely areas of evacuee ground contact in dark-of-night conditions with the landing gear in any state of collapse, and in the case of overwing passenger emergency exits and the overhead flight crew emergency exit, do not allow viewing of the likely areas of evacuee ground contact in any lighting conditions with the landing gear extended or in any state of collapse, whereby the applicable standards of the AWM are not met, and to issue the corresponding type certificate. | Approved | 7839275 |
| 061-2012 | 29-10-2012 | CAR 521.31(1)(d) and AWM 525.981(a)(3) | AARD | Bombardier Inc. | CL-600-2E25 (CRJ-1000) | A-276 | To allow additional time to complete the necessary certification program, including design, testing, analysis and documentation without a complete showing compliance. | Approved | 7804298 |
| 034-2012 | 08-02-2013 | Car 521.31(1)(d) and AWM 525.841(a)(2)(i) | AARD | Bombardier Inc. | BD-500-1A10 (CSeries CS100) and BD-500-1A11 (CSeries CS300) | A-236 | To allow the certification without a complete showing of compliance to the cabin pressure altitude exposure time limits stipulated in subparagraphs 525.841(a)(2)(i) and (ii) of the AWM at Change 525-8 and only for the Uncontained Engine Failure (UEF) case. | Approved | 7164079 |
| 107-2011 | 10-08-2011 | CAR 521.158 | AARD | Kenn Borek Air Ltd. (KBA) | Viking DHC-6 | STC No.SA09-62 | To permit the removal of the engine inlet deflector system on the Viking DHC-6 “Twin Otter” Models 100, 200 and 300 aeroplanes and reissue the corresponding supplemental type certificate (STC) to KBA. This exemption provides revised conditions as compared to exemption 072-2009: removal of the condition for the seaplane configuration, revising the OAT, etc. | Approved | 6827264 |
| 102-2011 | 28-12-2011 | CAR 521.158 and AWM 527.1(a) | AARD | Bell Helicopter Textron Canada Ltd. | 429 | H-107 | To permit an increase to the maximum mass (weight) of any Bell Helicopter Model 429 from 3175 kg (7,000 lbs) to 3402 kg (7,500 lbs) or less, while maintaining a normal category rotorcraft certification. | Approved | 6730403 |
| 098-2011 | 02-06-2011 | CAR 521.158(1) with respect to 525.1301 and 525.1309 of the AWM | AARD | Bombardier Inc. | BD-700-1A10 (Global Express) and BD-700-1A11 (Global 5000) | A-177 | To allow the changed Bombardier model BD-700-1A10 (Global Express) and BD-700-1A11 (Global 5000) aeroplanes with the Global Vision Flight Deck (GVFD) modification at the Version 3.2 (v.3.2) configuration to be certificated without a finding of compliance with AWM 525.1301 and AWM 525.1309 at the time of certification. | Approved | 6739053 |
| 080-2010 | 01-11-2010 | CAR 521.31(1)(d) with respect to AWM 525.981(a)(3) | AARD | Bombardier Inc. | CL-600-E25 | A-131 | To allow the Bombardier CL-600-2E25 to be certificated without a complete showing of compliance with AWM 525.981(a)(3) at the time of certification. | Approved | 6151541 |
| 079-2010 | 01-10-2010 | CAR 602.40 | AARD | N/A | N/A | N/A | To permit persons to land and takeoff in helicopters, for the purposes of NVG aircraft certification flight tests or NVG research flights conducted by the National Research Council, Flight Research Laboratory, in areas that do not meet the night lighting requirements for an aerodrome. | Approved | 6158144 |
| 056-2010 | 05-06-2010 | CAR 521.158 and FAR Sec. 25.813(e) | AARD | Innotech Aviation Ltd. | BD-700-1A11 (Global 5000) | A-177 | To permit the installation of a door in a partition between passenger compartments and issue the corresponding supplemental type certificate. | Approved | 5871747 |
| 055-2010 | 05-06-2010 | CAR 521.158 and FAR Sec. 25.785(b) | AARD | Innotech Aviation Ltd. | BD-700-1A11 (Global 5000) | A-177 | To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate. | Approved | 5872314 |
| 047-2010 | 07-05-2010 | CAR 521.158 and FAR Sec. 25.813(e) | AARD | ACS-NAI Ltd | BD-700-1A10 (Global Express) | Any STC applied for by ACS-NAI | To permit the installation of a door in a partition between passenger compartments and issue the corresponding supplemental type certificate. | Approved | 5846877 |
| 046-2010 | 07-05-2010 | CAR 521.158 & FAR Sec. 25.785(b) | AARD | ACS-NAI Ltd | BD-700-1A10 (Global Express) | Any STC applied for by ACS-NAI | To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate. | Approved | 5846867 |
| 043-2010 | 21-05-2010 | CAR 521.158 & FAR 25.813(e) | AARD | Flying Colours Corp. | CL-600-2B19 (CL-850) | A-131 | To permit the installation of a door in a partition between passenger compartments and issue the corresponding supplemental type certificate. | Approved | 5835195 |
| 042-2010 | 07-05-2010 | CAR 521.158 and FAR Sec. 25.785(b) | AARD | ACS-NAI Ltd | BD-700-1A11 (Global 5000) | Any STC applied for by ACS-NAI | To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate. | Approved | 5828944 |
| 041-2010 | 07-05-2010 | CAR 521.158 & FAR 25.813(e) | AARD | ACS-NAI Ltd | BD-700-1A11 (Global 5000) | Any STC applied for by ACS-NAI | To permit the installation of a door in a partition between passenger compartments and issue the corresponding supplemental type certificate. | Approved | 5828803 |
| 036-2010 | 18-11-2010 | CAR 521.158 and SCA 2010-02 part of Para 3.2(a)(1) | AARD | Gulfstream Aerospace Corp. | GIV-X | A-129 | To permit certification of the GIV-X aeroplane for maximum operating altitude above 41000 feet up to 45000 feet without meeting one of the requirements of SCA 2010-02 | Approved | 5923026 |
| 012-2010 | 17-08-2010 | CAR 521.46 | AARD | (Transport Canada) | Canadian air operators, Part V, Subpart 21 | N/A | To grant applicants for Type Certificates as defined in Part V Subpart 21, a phased in period of this new requirement, reducing unintended disruption of ongoing flight test activities. | Approved | 5689250 |
| 129-2009 | 24-01-2010 | CAR 521.31(1)(d) & 525.562 and 525.785(b) of the AWM | AARD | Bombardier Aerospace | DHC-8 Series 400 | A-142 | To allow any Bombardier Aerospace DHC-8 Series 400 aeroplane to be configured for the installation of a portable medical stretcher to be used for a non-ambulatory person or a person who cannot be seated in an aircraft passenger seat due to medical reasons such that the emergency landing dynamic test conditions for the qualification of occupant injury criteria, as well as to the structural retention criteria, are not met with respect to the occupancy of the portable medical stretcher, as approved by the portable medical stretcher installation and the corresponding type certificate. | Approved | 5481051 |
| 072-2009 | 25-08-2009 | CAR 513.07 and AWM 513.07(1)(b), U.S. CAR 3.606 | AARD | Kenn Borek Air Ltd. (KBA) | Viking DHC-6 | STC No.SA09-62 | To permit the removal of the engine inlet deflector system on the Viking DHC-6 “Twin Otter” Models 100, 200 and 300 aeroplanes and issue the corresponding supplemental type certificate (STC) to KBA. | Approved | 5125632 |
| 050-2009 | 03-07-2009 | CAR 605.03(1)(b) & 703.25 | AARD | (Transport Canada) | Canadian air operators, subpart VII | N/A | To allow Canadian air operators to carry external loads on their float equipped aeroplanes without an authorization in the type certificate or in a supplemental type certificate and without complying with the conditions of the aeroplane flight authority with respect to the approval of the carriage of external loads. | Approved | 5047844 |
| 047-2009 | 19-06-2009 | CAR 513.07 and AWM 513.07(1)(b) | AART | Northeast Engineering and Development Limited (NEDL) | CL600-2A12 S/N 3022 Reg. C-GCFG | LSTC held by NEDL | To permit the installation of a loading ramp which facilitates the loading of the medical stretchers on this a/c, operated by the Gouvernement du Québec, Service aérien gouvernemental. | Approved | 5034786 |
| 028-2009 | 12-06-2009 | CAR 605.03(1)(b) & 703.25 | AARD | (Transport Canada) | Canadian air operators, subpart VII | N/A | Exemption cancelled 2009-07-03 superseded by exemption NCR/RCN 050-2009. | Cancelled | 4910045 |
| 147-2008 | 21-11-2008 | CAR 513.07 and AWM 513.07(1)(b) & FAR Sec. 25.813(e) | AARD | Aero Consulting Services Ltd. | CL-600-2B19 (CL-850) | Any STC or LSTC applied for by ACS | To approve the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 4476335 |
| 138-2008 | 12-04-2010 | CAR 521.158 and FAR Sec. 25.785(b) | AARD | Innotech Aviation Ltd. | BD-700-1A10 | A-177 | To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate to Innotech Aviation. | Approved | 4312292 |
| 137-2008 | 12-04-2010 | CAR 521.158 & FAR Sec. 25.813(e) | AARD | Innotech Aviation Ltd. | BD-700-1A10 | A-177 | To permit the installation of a door in a partition between passenger compartments and issue the corresponding type certificate. | Approved | 4341840 |
| 127-2008 | 07-11-2008 | CAR 602.40 | AAR | Transport Canada Aircraft Certification; National Research Council Canada IAR-FRL | N/A | N/A | To permit persons to land and takeoff in helicopters, for the purposes of NVG aircraft certification flight test or NVG research flights conducted by the National Research Council, Flight Research Laboratory, in areas that do not meet the night lighting requirements for an aerodrome. | Approved | 4408780 |
| 100-2008 | 09-09-2008 | CAR 513.07 and AWM 513.07(1)(b) | AARD | DECA Aviation Engineering Ltd. | CL-600-2B19 | STC No. SA08-66 | To obtain a supplemental type certificate (STC) for a design that includes the installation of a door in a partition between passenger compartments, such that the minimum emergency exit access requirements are not met, for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 4198676 |
| 076-2008 | 09-09-2008 | AWM 513.07(1)(b), CAR 513.07 & FAR 25.813(e) | AARD | Aero Consulting Services Ltd. | CL-600-2B19 | LSTC No.C-LSA08-029/D | To approve the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 4032680 |
| 074-2008 | 18-08-2008 | AWM 513.07(1)(b), CAR 513.07 & FAR 25.815 | AARD | DECA Aviation Engineering Ltd | British Aerospace (BAe) Jetstream Series 3112 | LSTC No. O-LSA06-305/D | To obtain a design approval for a cabin design that does not comply with the minimum cabin aisle width requirements of the applicable standards of airworthiness. | Approved | 4168059 |
| 031-2008 | 26-03-2008 | AWM 513.07(1)(b), CAR 513.07 & FAR 25.813(e) | AARD | Aero Consulting Services Ltd. | CL-600-2B19 | To permit the installtion of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 3877091 | |
| 006-2008 | 30-01-2008 | AWM 513.07(1)(b), CAR 513.07 &FAR 25.813(e) | AARD | Dassault Falcon Jet Corp. | Falcon 900EX | A-136 | To permit the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand transport service pursuant to CAR 704. | Approved | 3766453 |
| 093-2007 | 27-09-2007 | CAR 513.07 and AWM 513.07(b), U.S. CAR 3.606 | AARD | Erwin Aero Intl. Ltd. (EAI) | de Havilland DHC-6 Twin Otter Models 100, 200 and 300 | To permit the removal of the engine inlet deflector system on the de Havilland Canada DHC-6 “Twin Otter” Models 100, 200 and 300 aeroplanes and issue the corresponding supplemental type certificate (STC) to EAI. | Approved | 2507976 | |
| 013-2007 | 15-02-2007 | CAR 525.01 and AWM 525.811(8), 525.812 (b)(1)(I) and (ii) | AARD | Bombardier Aerospace | DHC-8 Series 100, 200, 300 and 400 | A-142 | Permit the installation of emergency exit signs with non-English lettering and/or markings that do not comply for the purpose of facilitating delivery of the affected a/c to a foreign customer. | Approved | 2192252 |
| 008-2007 | 26-04-2007 | CAR 602.40 | AAR | National Research Council - NCR-FRL | N/A | N/A | To permit persons to land and takeoff in helicopters, for the purposes of NVG aircraft certification flight test or NVG research flights conducted by the National Research Council, Flight Research Laboratory, in areas that do not meet the night lighting requirements for an aerodrome. | Approved | 2179381 |
| 051-2006 | 11-05-2006 | CAR 605.03(1)(b) & 703.25 | AARD | Air operators Subpart 703 | N/A | N/A | To carry external loads on their float equipped a/c without an authorization in the TC or STC . | Approved | 1798324 |
| 135-2005 | 05-08-2005 | CAR 513.07(1)(a) & AWM 525.785(b) | AARD | Gulfstream Aerospace Corp. | Gulfstream 200 | A-215 | The installation of side-facing divan(s), permitting that divan(s) be occupied during taxi, take-off and landing. | Approved | 1268971 |
| 123-2005 | 20-07-2005 | CAR 523.01(2) & AWM 523-VLA.3 | AARD | Diamond Aircraft Industries Inc. | DA20-C1 VLA | A-191 | To grant approval only to permit certification of all a/c, DA20-C1 VLA, at a Maximum Approved Takeoff Mass (Weight) of not more than 800 kg (1764 lbs). | Approved | 1260578 |
| 034-2005 | 18-03-2005 | CAR 537.01 & AWM 537.205(c) & Standard CAN/CGSB-65.17-99 Para 8.1.3.2 | AARD | DSS Marine Inc. | HPTSS DSS Marine Incorporated Model DS-HPTS-VO1 | AP-59 | To obtain an Appliance Tye Certificate without complying with the donning time test as required by the HPTSS Standard. | Approved | 1105374 |
| 204-2004 | 15-12-2004 | CAR 513.07(1)(a) & AWM 525.813(e) | AARD | Bombardier Inc. | BD700-1A11 | A-177 | To permit Bombardier Inc. to install a door in a partition betweeen passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 804789 |
| 203-2004 | 15-12-2004 | CAR 513.07(1)(a) | AARD | Bombardier Inc. | BD700-1A11 | A-177 | Permit Bombardier Inc. to install side-facing divan(s). | Approved | 843251 |
| 180-2004 | 16-11-2004 | CAR 513.07(1)(a) & AWM 525.785(b) | AARD | Bombardier Inc. | BD100-1A10 | A-177 | To permit Bombardier Inc. to install side-facing divan(s) | Approved | 905593 |
| 170-2004 | 09-12-2004 | CAR 605.38(1) | AARD | N/A | Air operators, subpart VII | N/A | To provide additional time to install an ELT where the a/c is a multi-engined turbo-jet aeroplane of more that 5,700 kg MCTOW that is being operated in IFR flight within controlled airspace over land, and south of latitude 66o30o N. | Approved | 946150 |
| 169-2004 | 12-01-2005 | CAR 513.07(1)(a) & AWM 525.813 (e) | AARD | ELISEN Technologies Inc. | BD700-1A10 | Installation of mid-cabin door on any BD700-1A10 a/c. for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. | Approved | 891281 | |
| 168-2004 | 12-01-2005 | CAR 513.07(1)(a) & AWM 525.785(b) | AARD | ELISEN Technologies Inc. | BD700-1A10 | Installation of side facing divan(s) on any BD700-1A10 a/c. | Approved | 892664 | |
| 167-2004 | 18-11-2004 | CAR 513.07(1)(a) & AWM 525.785(b) | AARD | Bombardier Inc. | BD700-1A10 | A-177 | Allow the installation of a side-facing divan(s) on any BD700-1A10 a/c. | Approved | 882497 |
| 182-2003 | 31-10-2003 | CAR 513.07(1)(a) | AARD | Deca Aviation Engineering Ltd | BD700-1A10 | A-177 | Allow the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation with a maximum of 19 passengers. | Approved | 446803 |
| 181-2003 | 31-10-2003 | CAR 513.07(1)(a) & AWM 525.813(e) | AARD | Bombardier Completion Center | BD700-1A10 | A-177 | Allow the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation with a maximum of 19 passengers. | Approved | 426695 |
| 132-2003 | 09-05-2003 | AWM 525.785(b) | AARD | Bombardier Completion Center | BD700-1A10 Global Express | A-177 | Installation of side-facing divan(s) for 704 operations. (Expired 30 Nov 04) | Approved | 395014 |
| 05-2002 | 16-07-2002 | AWM 525.813(e) | AARD | Dassault Aviation | Falcon 900 / 900EX | A-136 | Mid-Cabin Door | Approved | 160403 |
| 04-2002 | 17-05-2002 | AWM 525.562 and 525.785(b) | AARD | Bombardier Aerospace | DHC-8-400 | A-142 | Installation of Stretcher | Approved | 150236 |
| 03-2002 | 05-04-2002 | CAR 571.06(1), 705.134, 705.135, 705.137, 705.138, 705.139 and AWM 561.305, .307 | AAR | SFAR 92-4 | Air Operators, subpart 705 | N/A | Flight Crew Compartment Doors (cancels 2002-02) | Approved | 608931 |
| 02-2002 | 17-01-2002 | CAR 571.06(1), 705.134, 705.135, 705.137, 705.138, 705.139and AWM 561.305, .307 | AAR | SFAR 92-3 | Air Operators, subpart 705 | N/A | Flight Crew Compartment Doors (cancels 2001-01) | Approved | 601661 |
| 01-2002 | 25-01-2002 | AWM 525.813(e) | AARD | Deca Aviation Engineering Ltd | BD700-1A10 | Mid-Cabin Door | Approved | 609000 | |
| 01-2001 | 09-10-2001 | AWM 571.06(1), 705.134, 705.135, 705.137, 705.138, 705.139and AWM 561.305, .307 | AAR | SFAR 92-3 | Air Operators, subpart 705 | N/A | Quickly modify the flight crew compartment doors to delay or deter unauthorized entry. | Approved | 601655 |
| 01-2000 | 20-04-2000 | AWM 525.785(b) | AAR | Bombardier Completion Center | BD700-1A10 Global Express | LSTC Quebec Region |
Side Facing Divans. Replaced by 01 Sep. 2000 revision. | Approved | 602025 |
| 01-1999 Rev A | 03-09-1999 | AWM 525.813(e) | AAR | Bombardier Completion Center | BD700-1A10 Global Express | LSTC Quebec Region |
Interior Doors Revised Dec. 00. *Replaced by Revision A - 17 May 2001 | Approved | 601957 |
| 01-1997 | 25-06-1997 | AWM 522.177(b)(3) | AARD | PZL-BIELSKO | SZD-51-1 “Junior” glider | Rudder control force reversal | Approved | 536582 | |
| 03-1995 Rev A | 05-09-1995 | E&I, Part II, Section 1.13 | AARD | Beech Aircraft Corporation | B300/B300C Super King Air | TC Issue Paper 1-2, Item 15 | Runway factors. Exemption cancelled 24 May 1996. | Cancelled | 601943 |
| 02-1995 | 12-06-1995 | AWM 522.723 | AARD | WSK PZL-KROSNO | PZL-KROSNNO KR-03A | G-155 | Loads shock adsorption | Approved | 601934 |
| 01-1995 | 13-06-1995 | AWM 523.53 (c)(1) | AARD | Beech Aircraft Corporation | B300 & B300C | A-149 | Not issued FAA exempt was accepted | Denied | 601634 |
| 01-1994 Rev A | 13-06-1995 | FAR 23.3(a) | AARD | Air Tractor | AT-802 & AT-802A | A-194 | Maximum certificated take-off weight restricted category. | Approved | 601928 |
| 02-1992 | 09-10-1992 | FAR 25.785(h) | AARD | Aerospatiale | ATR 72-102 / 202 | A-159 | Flight attendants seat location | Approved | 601614 |
| 01-1992 | 22-02-1993 | FAR 25.783(g) | AARD | Innotech Aviation Ltd. | Canadair CL600 2A12, Serial # 3063 | Medical stretcher installation. | Approved | 601607 | |
| 04-1991 | 26-09-1991 | FAR 23.903(b)(1) | AARD | Beech Aircraft Corporation | B300/B300C Super King Air | A-149 | Not issued FAA exempt was accepted | Denied | 601230 |
| 03-1991 | 18-07-1991 | US CAR 4b.362. | AARD | Northeast Engineering and Development Ltd | Boeing 727-100C C-FPXD | Cargo passenger configuration emergency exits | Approved | 601221 | |
| 02-1991 | 31-05-1991 | AWM 571.215(a) | AARD | Air Transat | Lockheed L-1011, CF-TNC, CF-TNB, CF-TNA, CG-TSZ & Boeing 727 CG-AAD, CG-AAL, CG-AAG | Calibration cards to be provided within 30 days | Approved | 601209 | |
| 01-1991 | 31-01-1991 | AWM 591.103(a)(1) | AARD | NWT Air | L382 Aircraft C-GHPW | SDR - 48 hours remote area operations | Approved | 601186 | |
| 03-1990 | 16-01-1991 | FAR 25.571(e)(2) | AARD | CASA | CN-235-100 | A-169 | Propeller blade impact | Approved | 601174 |
| 02-1990 | 06-04-1990 | FAR 25.785(h) | AARD | Fokker Aircraft B.V. | F28 MK 3000/4000 | A-108 | Flight attendants seat location | Approved | 601166 |
| 01-1990 | 31-01-1990 | US CAR 4b.362 | AARD | Northeast Engineering and Development Ltd | Boeing 727-100C C-FRST, C-GVFA and C-GFRB | Cargo passenger configuration emergency exits | Approved | 601148 | |
| 06-1989 | 09-11-1989 | FAR 25.832 | AARD | Airbus Industrie | A320 | A-166 | Cabin ozone concentration | Denied | 1168312 |
| 05-1989 | 10-07-1989 | AWM 549.203(b) | AARD | Mr. D. Sevold | Pitcairn Model PAA-1 amateur built gyrocopter | STC 507 | Maximum take-off mass (weight) | Approved | 601134 |
| 04-1989 | 10-02-1989 | AWM 523.807(d)(1)(ii) | AARD | British Aerospace | Jetstream Series 3200 Model 3212 HP 137, Mk. 1 | A-162 | Emergency exits | Approved | 601119 |
| 03-1989 | 10-02-1989 | AWM 523 Various Paragraphs | AARD | British Aerospace | Jetstream Series 3200 Model 3212 | A-162 | Ground loads and landing gear requirements | Approved | 601112 |
| 02-1989 | 03-02-1989 | FAR 25.785(h) | AARD | Boeing Canada/ de Havilland Division | DHC-8 Series 300 | A-142 | Flight attendants seat location | Approved | 601091 |
| 01-1989 | 15-02-1989 | FAR 25.785(h) | AARD | Aerospatiale | ATR 42 | A-159 | Flight attendants seat location | Approved | 601076 |
| 01-1988 | 23-11-1988 | FAR 25.785(h) | AARD | Fokker Aircraft B.V. | F28 MK0100 | A-108 | Flight attendants seat location | Approved | 601041 |
| 02-1986 | 14-05-1986 | SFAR 41C, Paragraph 214(3)(a) | AARD | Beechcraft | Beech Model 300 | A-149 | Minimum aisle width | Approved | 601008 |
| 01-1986 | 14-03-1986 | FAR 25.807(c)(1) | AARD | Boeing Canada/ de Havilland Division | DHC-8 serie 100 | A-142 | Maximum number of passenger seats | Approved | 600975 |