N75AA

Cancelled 2004

Deregistered aircraft · 1980 Lockheed L-1011-385-1-15 · Rolls-Royce RB-211 series

Cancelled
April 22, 2004
Exported to
Swaziland
Status when cancelled
Valid registration
Serial number
193U1201
Year built
1980
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
July 8, 1998
Certificate issued
January 9, 2002
Last registry action
January 9, 2002
Mode S code
AA17B1
Owner when cancelled
Morris Waldo I
Location
Marion, IA
Owner type
Individual

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 8

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 20010125SG002Frame · corrodedONE 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)Sep 25, 2000 · N75AA · Lkheed 1011385115 · Fuselage Main, FrameSDR 20010125SG001Skin · corrodedFOUND 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)Sep 25, 2000 · N75AA · Lkheed 1011385115 · Fuselage Main, Plate/SkinSDR 20010103AP002Skin · corrodedON 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. Aug 18, 2000 · N75AA · Lkheed 1011385115 · Fuselage Main, Plate/SkinSDR 20001215AP002Skin · corrodedON 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. AREAAug 18, 2000 · N75AA · Lkheed 1011385115 · Fuselage Main, Plate/SkinSDR 99ZZZM217Switch · serviceableRIGHT 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 3Feb 19, 1999 · N75AA · Lkheed 1011385115 · Landing Gear Position and WarningSDR 98ZZZM970Vibration Light · malfunctionedNR 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-Aug 28, 1998 · N75AA · Lkheed 1011385115 · Engine Vibration AnalyzerSDR 98ZZZM969Vibration Light · malfunctionedNR 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)Aug 27, 1998 · N75AA · Lkheed 1011385115 · Engine Vibration AnalyzerSDR 98ZZZX4102Wire · shortedAFTER 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. Aug 25, 1998 · N75AA · Lkheed 1011385115 · Electrical Power System Wiring