FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N920L and the event date: up to this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA9908801Switch Box · wornTHE NOSE LANDING GEAR UNSAFE LIGHT APPEARED AFTER GEAR WAS EXTENDED. MANUAL EXTENSION OF THE NOSE LANDING GEAR WAS NO HELP. REPLACED THE GEAR DOOR PROXIMITY SWITCH BOX . CHECK-C 6-12-98 MCI.SDR TWAA9809418Frame · misdrilledMCI - DURING OP 15 MAINTENANCE CHECK, FOUND .3125 INCH HOLE IN TOP OF FORMER 36Z AT STR 29R, RBL 6. HOLE DRILLED FOR RIVNUT NO LONGER NEEDED. DID NDT CHECK FOR CRACKS. PLUGGED AND REPAIRED PER ARA 15285. (X)SDR TWAA9809417Intercostal · chafedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND INTERCOSTAL FS 980 TO FS 996 BETWEEN S27R AND S28R WITH APPROXIMATELY .25 INCH HOLE WORN INTO LIP. REPLACED AND INSTALLED NEW INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM C. (X)SDR TWAA9809212Skin · damagedMCI - DURING OP 15 MAINTENANCE CEHCK, THE AFT CARGO DOOR CUTOUT FUSELAGE SKIN WAS DAMAGED AT AFT LOWER EDGE. REPAIRED DAMAGED SKIN PER SRM 54-05 FIG 80, AND TWA STD PRACTICES. (M)SDR TWAA9809202Skin · crackedDURING OP-15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN WITH .125 INCH CRACK ON CARGO DOOR CUTOUT EDGE, FS 937 AND L26R. TRIMMED DAMAGED AREA AND CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 8C AND TWA STD PRACTICES. (M)SDR TWAA9809117Rib · crackedMCI - DURING OP 15 MAINTENANCE CHECK, THE LEFT WING OUTBOARD FLAP HINGE CASTING ATTACH RIBS WERE CRACKED ON INBOARD AND OUTBOARD SIDES INSIDE FLAP STRUCTURE. RIBS REMOVED AND NEW RIBS INSTALLED PER SRM 51-01, AND FASTENERS INSTALLED PER STANDARD PRACTICES ANDSDR TWAA9808703Bulkhead · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LOWER ANGLE CRACKED ONE INCH AT 3 O'CLOCK POSITION ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPAIRED ANGLE WITH DOUBLER PER SRM 53-01, PAGE 10. (M)SDR TWAA9808702Bulkhead · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT PRESSURE BULKHEAD, UPPER ANGLE CRACKED ONE INCH AT 9 O'CLOCK POSITION, FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)SDR TWAA9808701Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO DOOR CUTOUT SKIN DAMAGED ON LOWER FORWARD SIDE. REPAIRED SKIN AND INSTALLED DOUBLER PER SRM 53-05, PAGE 261. (M)SDR TWAA9802603Lamp · failedJAX - FLT 494 - FORWARD GALLEY OVERHEAD FLOURSCENT WORK LIGHT, RT OUTBOARD, WAS SMOKING SHORTLY AFTER TAKEOFF. THE LIGHT WAS TURNED OFF. AT JAX THE LIGHT WAS DEACTIVATED BY PULLING THE CIRCUIT BREAKER. CORRECTION WAS DEFERRED. ON LAYOVER, THE WIRING AND SESDR TWAA9781003Power Supply · weakSTL - FLT 535 - DURING LANDING, EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED WEAK POWER SUPPLY, MFG PN 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPS CHECK NORMAL. CHECK C - 6-28-97 - STL. (X)SDR TWAA9777001Battery Pack · dischargedSTL - FLT 541 - DURING TAKEOFF, EMERGENCY EXIT LIGHT ILLUMINATED AT ROWS 1-7. REMOVED AND REPLACED BATTERY PACK, MFG PN 2013-1A. OP CHECKS NORMAL. CHECK C - 6-21-97 - STL. (X)SDR TWAA9711001Relief Valve · failedSTL - FLT 322 - DURING CLIMB, THE NR 2 ENGINE, S/N 3994 INDICATED HIGH OIL PRESSURE. REMOVED AND REPLACED OIL PRESSURE RELIEF VALVE, MFG P/N 811131, MANUFACTURED BY PWA. OPERATIONAL CHECK NORMAL. (M)
Other aircraft with N920L · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N920L is registered now to the first aircraft listed.