NTSB investigations · 2
Matched to this aircraft by N924L and the event date: up to this one’s cancellation.
NTSB BFO88IA012Incident · No injuriesIncident investigationFinal reportBaltimore, MDTwa flt 388 (DC-9, N924L) was in clouds climbing to 7000' when Baltimore (bwi) TRACON adzd that an acft (Piper PA-28R) was straight ahead at 3 mi dscndg fm 6700'. Flt 388 had passed 6000' & the capt requested a traffic avoidance vector. The TRACON ctlr…NTSB MKC81FA051Accident · No injuriesClosedSt.Louis, MO
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N924L and the event date: up to this one’s cancellation.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA0013902Wire · damagedTHE 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.SDR TWAA0010705Skin · corrodedIN 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.SDR TWAA0010408Frame · damagedDURING 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.SDR TWAA0010407Frame · corrodedDURING 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.SDR TWAA0010406Skin · corrodedDURING 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---SDR TWAA0010405Web · corrodedDURING 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---SDR TWAA0000304Angle · crackedDURING 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.SDR TWAA0000109Longeron · crackedDURING 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.SDR TWAA0000110Longeron · crackedDURING 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 18SDR TWAA9810602Battery Pack · dischargedSTL - 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)SDR TWA9803704Batteries · dischargedSTL - 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)SDR TWAA9809511Skin · gougedMCI - 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)SDR TWAA9805802Bulkhead · corrodedMCI - 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)SDR TWAA9805705Bulkhead · corrodedMCI - 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 ISDR 95ZZZM750Wire · brokenSHV - 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.
Other aircraft with N924L · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N924L is registered now to the first aircraft listed.