N924L
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 |
|---|---|---|---|
| TWA | Operator | on 1987-12-05 | Operator named in NTSB report |
| OZARK AIR LINES INC | Operator | on 1981-08-13 | Operator named in NTSB report |
Accident & incident history
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, 1995-11-11 – 2000-09-07.
Part: WIRE — DAMAGED (ROW 2) · airframe 78,491 hrs · 82,415 cycles
THE FIRST CLASS CABIN EGRESS LIGHTS DID NOT ILLUMINATE WHEN SWITCH PLACED IN THE TEST POSITION. SPLICED THE LIGHT CABLE AT THE SIDE WALL, ROW 2. CHECK-C 1-12-00 STL.
Part: SKIN — CORRODED (FUSELAGE) · airframe 78,004 hrs · 82,023 cycles
IN THE FORWARD CARGO COMPT, CORROSION WAS FOUND BETWEEN SKIN AND DOUBLER AT STA 598 TO 604, LONGERON 29L TO 29R, AND RIVETS POPPED ON THE SKIN. REMOVED CORRODED DOUBLER PER SRO-9530101. REPAIRED CORRODED SKIN PER DAC DRAWING SRO-9530101. CHECK-C 1-12-00 STL.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 78,004 hrs · 82,023 cycles
DURING CHECK-C MAINT AT STA 965 FOUND PREVIOUS FRAME REPAIR BETWEEN LONGERON 22 LT AND 25 LT, REQUIRED REPLACEMENT. REPAIRED FRAME AT STA 965 FROM LONGERON 26R TO 23L PER SRM 53-03 FIG 2A.
Part: FRAME — CORRODED (FUSELAGE) · airframe 78,004 hrs · 82,023 cycles
DURING CHECK-C MAINT THE FUSELAGE FROM STA 965 AFT SIDE BETWEEN LONGERON 29R TO 28L, WAS CORRODED IN THE AFT CARGO BIN. REPAIRED FRAME AT STA 965 PER SRM 53-03, FIG 2A, LONG 26R TO 23L.
Part: SKIN — CORRODED (FUSELAGE) · airframe 78,004 hrs · 82,023 cycles
DURING CHECK -C MAINT FOUND IN FWD CARGO COMPT AT STA 446, LONGERON 30, THE AFT SIDE OF FINGER DOUBLER HAD CORROSION. CUT OUT CORRODED SECTION OF SKIN AND INSTALLED DOUBLER REPAIR PER 53-04, FIG 44. ---CLOSED---
Part: WEB — CORRODED (E/E BAY FLOOR) · airframe 78,004 hrs · 82,023 cycles
DURING CHECK-C MAINT FOUND IN THE E/E BAY, FLOOR MEMBRANE WAS CORRODED AT STA 152, APPROX RBL 50 INCHES AT GALLEY DRAIN. REMOVED CORROSION PER SPM 6-80-1. INSTALLED DOUBLER PER SRM 53-01, FIG 2. TREATED AND PAINTED PER SRM 53-10-3. --CLOSED---
Part: ANGLE — CRACKED (BS 1104)
DURING CHECK-C MAINT, FOUND THE RT AFT VERTICAL STABILIZER ATTACH ANGLE CRACKED APPROX .75 INCH IN AT STA 1104. RT VERT STAB ANGLE AT STA 1104 REPAIRED PER SRM 53-05, FIG 23.
Part: LONGERON — CRACKED (APU BAY)
DURING CHECK-C MAINT, FOUND 0.125 IN LONG CRACK IN RT LONGERON 12, JUST AFT OF APU EXHAUST DUCT EXIT ON FUSELAGE, INSIDE THE FUSELAGE INTERIOR TAIL. REMOVED AND REPLACED THE SPLICE WITH NEW LONGERON SPLICE PER SRM 51-30-2 AND SRM 51-30-5.
Earlier reports · 1995–1999 · 7 reports
1999
Part: LONGERON — CRACKED (BS 639)
DURING CHECK-C MAINT, FOUND IN THE FUSELAGE INTERIOR, BOTH FLANGES OF LONGERON 5L AT STA 639 WERE CRACKED APPROX 1/2 INCH LONG. REMOVED THE DAMAGED SECTION OF LONGERON AND FABRICATED A SECTION OF NEW LONGERON. LONG SPLICED AND INSTALLED PER SRM 53-02, FIG 18.
1998
Part: BATTERY PACK — DISCHARGED (CABIN)
STL - DURING MAINTENANCE CHECK, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOP IN CABIN AISLE, AND RT AFT OVERWING EXIT LIGHT INOP. REPLACED CELL PACK B5-25. CHECK-C, 8-6-97 MCI. (M)
Part: BATTERIES — DISCHARGED (CABIN)
STL - FLT 218 - DURING PREFLIGHT, ONE SECTION OF OVERHEAD EMERGENCY LIGHTS IN COACH WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER PACK B-2. CHECK-C 8-6-97 MCI. (M)
1997
Part: SKIN — GOUGED (BS 964)
MCI - DURING OP 16 MAINTENANCE CHECK, FOUND GOUGE AT FS 964, STR 26R, BELOW LAP SEAM. SKIN GOUGE WAS .75 INCH BY 34 INCH BY .025 INCH. REPAIRED SKIN AT STR 26R, STA 964, PER SRM 53-04, FIG 12B SHEET 7 PAGE 45. ACFT TT: 70,977 HOURS. ACFT TC: 76.414. (X)
Part: BULKHEAD — CORRODED (AFT PRESS BLKHD)
MCI - DURING OP 16 MAINTENANCE CHECK, IN TAIL COMPARTMENT FOUND THE LOWER AFT SIDE OF PRESS BULKHEAD HAD BULGE AND CORROSION ON A Y-CHORD RBL, 4 INCHES. REMOVED CORROSION PER SRM 51-10-3, REPAIRED BULKHEAD PER SRM 53-03, FIG 9 SHT 2, AND SRM 51-00-0 PAGE 15 ITEM E. (M)
Part: BULKHEAD — CORRODED (BS 996)
MCI - DURING OP 16 MAINTENANCE, FOUND AFT PRESS BULKHEAD CORRODED AT STATION 996, AFT OF LONGERON 29R, FWDSIDE OF BULKHEAD. REMOVED CORROSION PER SRM 51-10-3 AND REPAIRED BULKHEAD PER SRM 53-03 FIG 9 SHT 2, AND SRM 51-60-0 PAGE 15 ITEM E. (M)
1995
Part: WIRE — BROKEN (GEAR INDICATION)
SHV - DURING LANDING, WHEN GEAR HANDLE WAS EXTENDED, RIGHT GEAR RED AND GREEN LIGHTS DID NOT ILLUMINATE. A FLY-BY WAS PERFORMED TO ENSURE GEAR WAS DOWN AND LOCKED. REPLACED BROKEN WIRE, REFERENCE WIRING DIAGRAM 32-61-00. OPERATIONAL CHECK NORMAL.