N926L
Registered owner: LIFT AIRCRAFT LLC, IN (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 1992-04-08 | Operator named in NTSB report |
Accident & incident history
Operated by TRANS WORLD AIRLINES (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.
15 reports on file, 1996-01-14 – 2000-08-05.
Part: SOCKET — FAILED (ROW 15) · airframe 80,726 hrs · 84,474 cycles
BURNING ODOR REPORTED IN AREA OF OVERWING EXITS DURING CRUISE FLIGHT. DEACTIVATED EMERGENCY LIGHTS AND FERRIED AIRCRAFT TO STL FOR CORRECTIONS. FOUND AND REPLACED BURNED LOWER SIDEWALL LIGHT SOCKET AT ROW 15 LEFT SIDE OF CABIN. REPLACED LIGHT BALLAST AND EMERGENCY LIGHT POWER SUPPLY PRECAUTIONARY. CHECK-C 3-10-00 STL.
Part: FITTING — CRACKED (RT WING) · airframe 80,088 hrs · 83,966 cycles
DURING ROUTINE CHECK, FOUND RT WING SPAR TO TRAP FITTING WITH CRACK BETWEEN TRAP ATTACH BOLTS. REPLACED THE RT SPAR TO TRAP FITTING PER SRM 51-00, STANDARD PRACTICE AND EMLR 70740. CHECK-C 3-10-00 STL.
Part: LONGERON — CRACKED (BS 1076) · airframe 79,697 hrs · 83,656 cycles
DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT BELT RING 1076, .5 INCH LONG AND 1 RIVET WAS MISSING. REMOVED AND REPLACED LONGERON 2R AT STA 1076 PER ARA 16646.
Part: LONGERON — CRACKED (BS 1076) · airframe 79,697 hrs · 83,656 cycles
DURING CHECK-C MAINT, LONGERON 2L WAS CRACKED AT STA 1076. SPLICED IN NEW LONGERON SECTION PER SRM 53-02 FIG A, 53-02 FIG 7, 53-02 FIG 8, FROM STA 1040 TO 1076.
Earlier reports · 1996–1999 · 11 reports
1999
Part: CONNECTOR — LOOSE (RT MLG)
DURING LANDING, RIGHT GEAR SAFE LIGHT FLICKERED ON AND OFF. SECURED CONNECTOR ON THE RIGHT GEAR UPLOCK SWITCH.
Part: BATTERY PACK — DISCHARGED (CABIN)
THE RT ENGINE EMERGENCY NACELLE LIGHT, OVERWING EXIT LIGHTS, AND THE AFT CABIN EXIT LIGHTS WERE INOPERATIVE. REPLACED THE NACELLE LIGHT BATTERY PACK PN B030CF00101, THE OVERWING LIGHT BATTERY PACK PN 41B004AD07G3, AND BOTH AFT CABIN EXIT BULBS PN 1315. CHECK-C 1-31-99 STL.
1997
Part: BULKHEAD TEE — CRACKED (AFT PRESS BLKHD)
STL - REPLACED PRESSURE BULKHEAD TEE BETWEEN LONGERON 11R AND 12R DUE TO A CRACK. (M)
Part: FLOORBEAM — DAMAGED (BS 237)
STL - REPAIRED DAMAGED SECTION OF FLOORBEAM AT STATION 237. (M)
Part: LONGERON — CRACKED (BS 889)
STL - SPLICED IN NEW LONGERON PIECE CRACKED AT LONGERON 2 RIGHT AT STATION 889. (M)
Part: LONGERON — CRACKED (FUSELAGE)
STL - REMOVED AND REPLACED FORWARD SECTION OF LONGERON 24R JUST AFT OF THE FORWARD BAGGAGE BIN DOOR DUE TO A CRACK. (M)
Part: LONGERON — CRACKED (BS 775)
STL - INSTALLED SPLICE ON LONGERON 5 LEFT AT STATION 775 DUE TO A CRACK. (M)
1996
Part: LONGERON — CRACKED (BS 756)
STL - DURING SPECIAL INSPECTION, FOUND .5 INCH CRACK LONGERON 5R STATION 756, REPAIRED PER SRM 53-02 FIGURE 2.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.
Part: CYLINDER — MALFUNCTIONED (RT MLG)
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. CYCLED LANDING GEAR. FOUND RIGHT MAIN LANDING GEAR BUNGEE CYLINDER MALFUNCTION. REPLACED RIGHT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5505. LANDING GEAR OPERATION AND INDICATION THEN CHECKED NORMAL. (M)
Part: POWER WIRE — FAILED (CABIN)
STL - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 12A. REMOVED AND REPLACED POWER WIRE, MFG P/N 5853-1. OPERATIONAL CHECK NORMAL.