Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 219PA0014Proximity Switch · out of adjustAFT CARGO DOOR LIGHT CAME ON AT 75 KTS. RTO, NO BRAKES APPLIED, REVERSERS ONLY. ADJUSTED PROXIMITY SWITCH AND OPS CHECKED PER MM 52-10-00.SDR 219PA0013Lamp · inoperativeAFT CENTER AISLE EMERGENCY EXIT LIGHTS INOP. RELAMPED AND OPS CHECKS GOOD PER MM 33-51-02.SDR 219PA0012Battery Pack · inoperativeBOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED OVERWING BATTERY PACKS. OPS CHECKS GOOD PER MM 33-50-00.SDR 219PA0011Coupler · damagedYAW DAMPER LIGHT STAYS OFF WHEN SWITCHED FROM ON TO OFF. REPLACED YAW DAMPER COUPLER, OPS CHECKS NORMAL PER MM 22-12-01.SDR 219PA0010Computer · malfunctionedROLL CHANNEL WILL NOT ENGAGE ON AUTO PILOT AND HEADING SELECT WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED GOOD PER MM 22-11-0.SDR 219PA0009Computer · malfunctionedAUTO PILOT AILERON WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED NORMAL PER MM 22-11-0.SDR 219PA0008Limiter · inoperativeAUTOPILOT ROLL CHANNEL WILL NOT ENGAGE. REPLACED AILERON FORCE LIMITER IAW MM 22-12-10. OPS CHECKS OK.SDR 219PA0007Battery Pack · inoperativeFWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED FWD FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT BATTERY PACK PER MM 33-51-21.SDR 219PA0006Autopilot SysElevator channel of auto pilot will not stay engaged. Re-racked A/P pitch control channel unit. Ops chks good IAW MM 22-10-10.SDR 219PA0005LightEmergency light above aft service door inop. Removed and replaced emergency light above aft service door Ref. MM 33-50-09. Ops. chk. good per MM 33-50-01.SDR 219PA0004Brake Assy#3 Brake dragging. Log page entry, (found heat shield from #3 main wheel lodged in rotor of brake assy. R&R brake IAW MM32-41-41 and R&R #3 wheel IAW MM32-45-11). Upon further investigation, found brake pad separated from brake resulting in damage to wheel aSDR 219PA0001ABrake Assy · damagedNR 3 BRAKE DRAGGING. LOG PAGE ENTRY, (FOUND HEAT SHIELD FROM NR 3 MAIN WHEEL LODGED IN ROTOR OF BRAKE ASSY. R&R BRAKE IAW MM32-41-41 AND R&R NR 3 WHEEL IAW MM32-45-11). UPON FURTHER INVESTIGATION, FOUND BRAKE PAD SEPARATED FROM BRAKE RESULTING IN DAMAGE TO WSDR 219PA0003TransmitterLower than normal acceleration at T/O EPR 1.95 Engs do not seem to produce thrust per EPR setting. Inspected PT2 systems on #1 and #2 engines and found both EPR transmitters bad. R&R #1 eng & #2 eng EPR transmitter per MM77-11-07, Ops check of eng paramatersSDR 219PA0002Valve#2 engine would not produce calculated T/O thrust. T/O discontinued at approx. 60 kts.Verified. R&R'd #2 eng P&D valve IAW M/M73-12-1. Ops & Leak chks good. Also C/W work cardPAS-MF-25, JT8D eng. trim & data plate run. Ops chks good no defects notedSDR 219PA0001GeneratorRt Generator failed at begining of take-off roll. Reset CSD could not duplicate.
Other aircraft with N219PA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N219PA is registered now to the first aircraft listed.