N75AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
8 reports on file, 1998-08-25 – 2000-09-25.
Part: SKIN — CORRODED (FUSELAGE)
FOUND DURING C-CHECK, FUSELAGE SKIN PANEL CORRODED AND RIVETS LOOSE AT FS 943-983 STRINGER 31-36. SKIN PANEL REPAIR CARRIED OUT IAW SRM 51-50-01. (M)
Part: FRAME — CORRODED (FUSELAGE)
ONE SHEARED RIVET, ONE LOOSE RIVET AND AREA CORRODED UNDER PANEL STATION 789-809 STRINGER 29-38 FOUND DURING C-CHECK. LOWER FRAME REPAIR CARRIED OUT IAW SRM 51-50-02 FIG 2. (M)
Part: SKIN — CORRODED (FUSELAGE)
ON FUSELAGE SKIN FOUND RIVET HEAD POPPED AND AREA OF CORROSION DAMAGED FRAME STATION 780 AT STRINGER 39R. PARTIALLY CUT OUT DAMAGED AREA IAW L1011 SRM 53-31-00. FABRICATED PARTS IAW SRM 53-31-00, FIG 802. INSTALLED REPAIRED PARTS IAW SRM 53-31-00, FIG 802. AREA CLOSED, PRESSURE CHECK ACCOMPLISHED IAW MM 21-31-00. (M)
Part: SKIN — CORRODED (FUSELAGE)
ON FUSELAGE SKIN FOUND RIVET HEAD POPPED AND AREA OF CORROSION DAMAGE FRAME STATION 780 AT STRINGER 39R. PARTIALLY CUT OUT DAMAGED AREA IAW L1011 SRM 53-31-00. FABRICATED PARTS IAW SRM 53-31-00 FIG 802. INSTALLED REPAIR PARTS IAW SRM 53-31-00 FIG 802. AREA CLOSED. PRESSURE CHECK ACCOMPLISHED IAW MM 21-31-00. (M)
Part: SWITCH — SERVICEABLE (RT MLG DOOR)
RIGHT MAIN GEAR OR DOOR LIGHT ON FLIGHT ENGINEERS ANNUNCIATOR PANEL STAYED ON AFTER GEAR RETRACTED. A/C RETURNED TO GSO. NO FUEL WAS DUMPED AND THE LANDING WAS NORMAL. CHECK AND ADJUSTED RIGHT GEAR DOOR PROXIMITY SWITCH IAW 32-61-07. OPS CHECKED GOOD IAW 32-12-01. A/C RETURNED TO SERVICE. (M)
Part: VIBRATION LIGHT — MALFUNCTIONED (NR 2 ENGINE)
NR 2 ENGINE INCREASE IN VIBRATION .8 TO 3.0 IN CRUISE, BOTH CHANNELS. THRUST LEVER RETARDED TO IDLE, VIBRATION .4. LEVER ADVANCED, VIBRATION INCREASES TO 3.0 UNITS. REPLACED ENGINE VIBRATION CONDITIONING UNIT. SWAPPED NR 1 AND NR 2 INDICATORS IAW MM 77-31-00. (M)
Part: VIBRATION LIGHT — MALFUNCTIONED (LT/RT ENGINE)
NR 2 ENGINE INCREASE IN VIBRATION FROM .7 TO 3 UNITS ON BOTH CHANNELS. WARNING LIGHT ON. ENGINE SHUTDOWN. COMPLETE BOROSCOPE CARRIED OUT, NO NEW DAMAGE FOUND. VIBRATION SURVEY CARRIED OUT, AND FAN TRIM BALANCE PERFORMED IAW 72-00-00 TEST 11 AND 16. (M)
Part: WIRE — SHORTED (CABIN)
AFTER ABOUT AN HOUR ON THE GROUND IN HNL, FOUND FORWARD A/C GROUND SERVICE BUS BREAKER TRIPPED AND THE NR 1 TRANSFORMER RECTIFIER BREAKER TRIPPED. SMOKE AND ARCING WERE SEEN IN LOWER GALLEY AREA AT LEFT CIRCUIT BREAKER PANEL. FOUND TWO WIRE BUNDLES BURNED. ONE FROM THE NR 1 FLIGHT STATION BUS EXTENSION, AND THE OTHER FROM THE NR 3 FLIGHT STATION BUS EXTENSION.