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Displaying 161 to 170 of 267 items.
… Administration (FAA), alerting maintainers, operators and owners of this potential safety issue. The following are … The absence of damage to the hook end of the seat belts and the "D-ring" type seat belt attachment fittings suggests … aligned with the opening in the hook end of the seat belt, and the seat belt became detached from the "D-ring" type seat …
6.504
… pump interaction problems. Intermittent electrical signal snags, caused by faulty connectors, can be elusive and … Information Letter (SIL) PW100-095 “Engine Electrical Signal Interruptions”; PW100 Workscope Planning Guide – …
1.913
… a Service Difficulty Report (SDR) that stated both left and right supports had cracks near the aft (torque tube) end. … that the cracks started in the upper flange of the support and extended into the web area approximately one inch from … Both aircraft had accumulated approximately 3600 hours TSN and 4100 landings. Fatigue stress damage to the balance …
7.565
… an uncommanded full left steering input was experienced and the crew was unable to maintain directional control. The aircraft veered off the runway and settled in a grassy area, sustaining minor damage to the nose gear and slight damage to the wing tip when it had contact with …
9.893