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|
Attributes | |
ACN | 1161766 |
Time | |
Date | 201403 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZZ.Airport |
State Reference | FO |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Challenger CL604 |
Operating Under FAR Part | Part 91 |
Flight Phase | Landing |
Route In Use | Visual Approach |
Flight Plan | None |
Component | |
Aircraft Component | Flap Control (Trailing & Leading Edge) |
Person 1 | |
Function | Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Experience | Flight Crew Last 90 Days 100 Flight Crew Total 7695 Flight Crew Type 410 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Maintenance Deviation - Procedural Published Material / Policy |
Narrative:
As part of the 48 month check; aircraft was required to do an air driven generator (air driven generator) drop test; to simulate total loss of aircraft power in flight; and ascertain the serviceability of the back up air driven generator. The maintenance organization told us an engineer would go with us for the test. We were supposed to just takeoff; do one visual circuit at the airport; drop the air driven generator and return for landing. We departed from runway 03 and climbed to 2;400 ft. On the downwind leg; we asked the engineer how he wanted the test conducted and it was agreed that generators 1 and 2 should be taken off. The air driven generator deployed successfully. On base leg; however; we could not get more than flaps 20 (which was the flaps we took off with and had chosen not to retract). We did the approach at flaps 20 speed of 160 KTS and only slowed down just prior to touchdown. After landing; only the left reverser deployed; we did not have ground spoilers; nose wheel steering and the anti-skid. This necessitated the application of maximum braking on the landing rollout; which resulted in the blow out of the four main tires. Aircraft was stopped on the runway and did not sustain any damage apart from the blown tires. There was no injury to the three crew on board. Roles were not clearly spelt out between the pilots and the engineer on board before the commencement of the flight. The pilots assumed the engineer was on board to talk us through the flight test; since we did not know other things he needed to see that necessitated his coming on the flight test. The engineer later said he did not know the pilots were expecting any inputs from him; so there was a communication gap. Flight crew should have relied on the QRH; rather assume the engineer was on board to talk us through the flight test.
Original NASA ASRS Text
Title: When a regular line flight crew was utilized to perform a required simulated failure of the AC electric system for a regular periodic maintenance check; a Maintenance Engineer was assigned to accompany them. When there was no comprehensive briefing as to how to perform the check it was conducted using TLAR (That Looks About Right) methodology which resulted in the loss of multiple systems for landing. Four main gear tires blew out when max braking was applied after the spoilers failed to deploy; one reverser failed to operate and the landing had had to have been made with only 20 degrees of flaps extended.
Narrative: As part of the 48 month check; aircraft was required to do an ADG (Air Driven Generator) drop test; to simulate total loss of aircraft power in flight; and ascertain the serviceability of the back up ADG. The Maintenance Organization told us an Engineer would go with us for the test. We were supposed to just takeoff; do one visual circuit at the airport; drop the ADG and return for landing. We departed from Runway 03 and climbed to 2;400 FT. On the downwind leg; we asked the Engineer how he wanted the test conducted and it was agreed that generators 1 and 2 should be taken off. The ADG deployed successfully. On base leg; however; we could not get more than flaps 20 (which was the flaps we took off with and had chosen not to retract). We did the approach at flaps 20 speed of 160 KTS and only slowed down just prior to touchdown. After landing; only the left reverser deployed; we did not have ground spoilers; nose wheel steering and the anti-skid. This necessitated the application of maximum braking on the landing rollout; which resulted in the blow out of the four main tires. Aircraft was stopped on the runway and did not sustain any damage apart from the blown tires. There was no injury to the three crew on board. Roles were not clearly spelt out between the pilots and the Engineer on board before the commencement of the flight. The pilots assumed the Engineer was on board to talk us through the flight test; since we did not know other things he needed to see that necessitated his coming on the flight test. The Engineer later said he did not know the pilots were expecting any inputs from him; so there was a communication gap. Flight crew should have relied on the QRH; rather assume the Engineer was on board to talk us through the flight test.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.