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|
Attributes | |
ACN | 523220 |
Time | |
Date | 200108 |
Day | Sat |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : iad.airport |
State Reference | VA |
Altitude | agl bound lower : 0 agl bound upper : 3000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : iad.tower |
Operator | common carrier : air carrier |
Make Model Name | Jetstream 41 |
Operating Under FAR Part | Part 121 |
Navigation In Use | other |
Flight Phase | climbout : initial climbout : takeoff |
Route In Use | departure : on vectors |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 270 flight time total : 2600 flight time type : 270 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : cfi pilot : atp |
Experience | flight time last 90 days : 40 flight time total : 1750 flight time type : 40 |
ASRS Report | 523220 |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper maintenance non adherence : company policies non adherence : published procedure other anomaly |
Independent Detector | other flight crewa other flight crewb |
Resolutory Action | flight crew : diverted to another airport flight crew : landed in emergency condition flight crew : declared emergency flight crew : regained aircraft control other |
Consequence | other other other |
Factors | |
Maintenance | contributing factor : engineering procedure contributing factor : work cards performance deficiency : scheduled maintenance performance deficiency : testing performance deficiency : inspection |
Supplementary | |
Problem Areas | Aircraft Maintenance Human Performance Company |
Primary Problem | Maintenance Human Performance |
Narrative:
At the time of the occurrence, I was handling pilot on the take off run. As I rotated, I immediately felt a tendency of the aircraft to roll to the right; to counteract this, it took my greater left aileron force and all left trim to keep the aircraft in a somewhat stabilized climb. I immediately informed the captain of these serious controllability problems and after completing the after take off checks we exchanged the controls so he could also feel what the problem was. Having established the seriousness of the problem we decided to declare an emergency and return to land in dulles runway 19L. I took the controls back and leveled off at 2000 ft. 160 KTS with flaps 9 degrees, in that configuration the aircraft was somewhat controllable. However, great force to the left on the yoke was necessary to keep the aircraft straight and level. While I kept flying, the captain called company maintenance and briefed the flight attendant. After that, the captain decided to take the controls for landing. We did our landing checks and safely landed the airplane, although it took both of us on the controls to keep the airplane aligned with the runway on final. Once at the gate, our maintenance team discovered that the push pull rods to the aileron trims had and been installed backwards and it would have been difficult for us (pilots) to notice it on our standard walk around.
Original NASA ASRS Text
Title: A BAE4100 FLC BATTLES THE CONTROLS TO MAINTAIN CTL OF THE ACFT AFTER TKOF WHEN THE ACFT ATTEMPTS A HARD RIGHT TURN. POST FLT INSPECTION FOUND AN IMPROPERLY INSTALLED AILERON TRIM PUSH-PULL ROD THAT HAD BEEN INSTALLED BACKWARDS AT IAD, VA.
Narrative: AT THE TIME OF THE OCCURRENCE, I WAS HANDLING PLT ON THE TAKE OFF RUN. AS I ROTATED, I IMMEDIATELY FELT A TENDENCY OF THE ACFT TO ROLL TO THE RIGHT; TO COUNTERACT THIS, IT TOOK MY GREATER LEFT AILERON FORCE AND ALL LEFT TRIM TO KEEP THE ACFT IN A SOMEWHAT STABILIZED CLIMB. I IMMEDIATELY INFORMED THE CAPT OF THESE SERIOUS CONTROLLABILITY PROBLEMS AND AFTER COMPLETING THE AFTER TAKE OFF CHECKS WE EXCHANGED THE CONTROLS SO HE COULD ALSO FEEL WHAT THE PROBLEM WAS. HAVING ESTABLISHED THE SERIOUSNESS OF THE PROBLEM WE DECIDED TO DECLARE AN EMER AND RETURN TO LAND IN DULLES RWY 19L. I TOOK THE CTLS BACK AND LEVELED OFF AT 2000 FT. 160 KTS WITH FLAPS 9 DEGS, IN THAT CONFIGURATION THE ACFT WAS SOMEWHAT CONTROLLABLE. HOWEVER, GREAT FORCE TO THE LEFT ON THE YOKE WAS NECESSARY TO KEEP THE ACFT STRAIGHT AND LEVEL. WHILE I KEPT FLYING, THE CAPT CALLED COMPANY MAINT AND BRIEFED THE FLT ATTENDANT. AFTER THAT, THE CAPT DECIDED TO TAKE THE CONTROLS FOR LANDING. WE DID OUR LANDING CHECKS AND SAFELY LANDED THE AIRPLANE, ALTHOUGH IT TOOK BOTH OF US ON THE CONTROLS TO KEEP THE AIRPLANE ALIGNED WITH THE RWY ON FINAL. ONCE AT THE GATE, OUR MAINT TEAM DISCOVERED THAT THE PUSH PULL RODS TO THE AILERON TRIMS HAD AND BEEN INSTALLED BACKWARDS AND IT WOULD HAVE BEEN DIFFICULT FOR US (PLTS) TO NOTICE IT ON OUR STD WALK AROUND.
Data retrieved from NASA's ASRS site as of July 2007 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.