N11003
Registered owner: IVM SOLUTIONS LLC, AL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| TRANS WORLD AIRLINES | Operator | on 1973-01-10 | Operator named in NTSB report |
Accident & incident history
Operated by TRANS WORLD AIRLINES INC (per NTSB report)
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.
13 reports on file, 1995-02-01 – 1997-05-15.
Part: DOOR — DEPARTED (LT MLG)
STL - DURING CRUISE, AT 28,000, LEFT MAIN GEAR FLYING DOOR SEPARATED FROM AIRCRAFT. (M)
Part: FAIRING — LOOSE (ENGINE)
MCO - FLT 451 - DURING TAKEOFF, COMPRESSOR GAS GENERATOR FAIRING CAME LOOSE. REPLACED FAIRING, MFG, P/N LK73722. OPERATIONAL CHECK NORMAL. (M)
Earlier reports · 1995–1996 · 11 reports
1996
Part: BLKHD WEB — CRACKED (BS 1363)
MCI - 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)
Part: BLKHD WEB — CRACKED (FS 1363)
MCI - 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)
1995
Part: LENS — INOPERATIVE (LT MLG)
STL - 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.
Part: ENGINE — FAILED (NR 2)
STL - 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 - JFK.
Part: INTERCOSTAL — BROKEN (FS 1363)
JFK - 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.
Part: BULKHEAD — CRACKED (FS 1363)
JFK - 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.
Part: SKIN — CRACKED (FS 1363)
JFK - 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. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.
Part: STRINGER — CRACKED (FS 1363)
JFK - 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. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.
Part: BLKHD SKIN — CRACKED (FS 1363)
JFK - 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. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.
Part: BLKHD ANGLE — CRACKED (FS 1363)
JFK - 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.
Part: BLKHD SKIN — CRACKED (FS 1363)
DURING 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 53-11-00, FIGURE 850. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.