N11003

Cancelled 2013

Deregistered aircraft · 1972 Lockheed L-1011-385-1 · Rolls-Royce RB-211-22 series

Cancelled
August 20, 2013
Status when cancelled
Sale reported, canceled
Serial number
193B-1015
Year built
1972
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 3, 1972
Last registry action
December 10, 2003
Mode S code
A02EA7
Owner when cancelled
Sale Reported
Owner type
Individual

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 2

Matched to this aircraft by N11003 and the event date: up to this one’s cancellation.

FAA incident reports · 7

FAA accident and incident reports matched to this aircraft by N11003 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 TWAA9760002Door · departedSTL - DURING CRUISE, AT 28,000, LEFT MAIN GEAR FLYING DOOR SEPARATED FROM AIRCRAFT. (M)May 15, 1997 · N11003 · Lkheed 10113851 · Landing Gear DoorsSDR TWAA9723002Fairing · looseMCO - FLT 451 - DURING TAKEOFF, COMPRESSOR GAS GENERATOR FAIRING CAME LOOSE. REPLACED FAIRING, MFG, P/N LK73722. OPERATIONAL CHECK NORMAL. (M)Feb 13, 1997 · N11003 · Lkheed 10113851 · Nacelle/Pylon StructureSDR 96ZZZM633Blkhd Web · crackedMCI - DURING SPECIAL CHECK, FOUND AFT BULKHEAD WEB CRACKED AT INBOARD SIDE OF WHEEL WELL STATION 1363, WL 102. REPAIRED PER SRM 53-11-00 AND 51-10-02. (M)Feb 27, 1996 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 96ZZZM632Blkhd Web · crackedMCI - DURING SPECIAL CHECK, FOUND MULTIPLE CRACKS IN BULKHEAD AND STIFFENER WEBS, FS 1363, RBL 42.5, WL 102 TO WL 143. REPAIRED PER SRM 51-10-02 AND 53-11-00. (M)Feb 27, 1996 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 96ZZZX216Lens · inoperativeSTL - FLT 86 - PRIOR TO LANDING, LT MLG GREEN LIGHT WAS INOPERATIVE RESULTING IN A FLY-BY. REPLACED LENS, MFG PN 10648 LD 2-359. CHECK C-10A - 11-24-95.Dec 27, 1995 · N11003 · Lkheed 10113851 · Landing Gear Position and WarningSDR 95ZZZX3182Engine · failedSTL - FLT 324 - AFTER TAKEOFF, SHUT DOWN NR 2 ENGINE, SN 4468, DUE TO HIGH AVM ON BOTH A AND B VIBRATION CHANNELS. CHECKED OIL SYSTEM CHIP DETECTORS, LUBRICATED FAN BLADES; PERFORMED FAN TRIM BALANCE. ENIGNE OPERATION CHECKED NORMAL. CHECK C-9B - 2-1-95 - JJun 9, 1995 · N11003 · Lkheed 10113851 · Engine (Turbine/Turboprop)SDR 95ZZZX892Stringer · crackedJFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFTFeb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, Longeron/StringerSDR 95ZZZX891Blkhd Skin · crackedJFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFTFeb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 95ZZZX890Skin · crackedJFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFTFeb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, Plate/SkinSDR 95ZZZX888Blkhd Angle · crackedJFK - DURING CHECK C-9B, FOUND A 3 INCH CRACK IN AFT BULKHEAD OUTBOARD CORD ANGLE, THROUGH BOTH LEGS AT WL 160, STA 1363, AND FOUND EXTERIOR CORD ANGLE CRACKED. REPAIRED PER SRM 53-11-00, FIGURE 842. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.Feb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 95ZZZX886Bulkhead · crackedJFK - DURING CHECK C-9B, FOUND A 28 INCH VERTICAL CRACK IN AFT BULKHEAD, STA 1363, THROUGH 8 STIFFENERS, WITH 7 STIFFENERS SHEARED. STOP DRILLED CRACKS AND REPAIR PER SRM 53-11-00, FIGURE 851. AIRCRAFT TOTAL TIME 60,716 HOURS; 22,699 CYCLES.Feb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 95ZZZX885Intercostal · brokenJFK - DURING CHECK C-9B, FOUND FORWARD END OF INTERCOSTAL, AFT BULKHEAD STA 1363, BROKEN AWAY FROM BULKHEAD BETWEEN STRINGERS 41L AND 42L, WHEELWELL. INSTALLED CLIP ANGLE PER SRM 53-12-00. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.Feb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, BulkheadSDR 95ZZZX884Blkhd Skin · crackedDURING CHECK C-9B, FOUND .25 INCH CRACK IN AFT BULKHEAD SKIN, STA 1363, ON OUTBOARD RIVET HOLE BETWEEN STIFFENER 15 AND 16; FOUND 4 INCH CRACK AT OUTBOARD FRAME, LT WHEELWELL, AT NR 16 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLERS PER SRM 53-11-00Feb 1, 1995 · N11003 · Lkheed 10113851 · Fuselage Main, Bulkhead

Other aircraft with N11003 · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N11003 is registered now to the first aircraft listed.