FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N990Z and the event date: up to this one’s cancellation.
Incident 19860502024009ITo Init Climb(1st Pwr Reduct) · St Louis, MONose gear door would not close after takeoff. Returned and found preload too low. Adjusted doors.Incident 19780424011259IForced/Precautionary Landing · Dallas, TXEngine failed on takeoff. Engine reverse blocker doors deployed and remained open in flight. Returned to airport
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TWAA9917301Plate · crackedTHE LEFT WING FUEL TANK PLATE NUMBER 1305 DOUBLER WAS CRACKED 1.75 INCH LONG AT THE 8 O'CLOCK POSITION. REPAIRED CRACKED DOUBLER PER ARA 16436 AT LT WING FUEL TANK DOUBLER NUMBER 1305. CHECK-C 9-21-98 STL.SDR TWAA9908101Pump · failedTHE RT ENGINE SHUT ITSELF DOWN DURING TAKEOFF. THE FLIGHT RETURNED TO SDF. REPLACED THE ENGINE FUEL PUMP DUE TO SHEARED SHAFT. ALSO, REPLACED THE FUEL CONTROL PRECAUTIONARY, (P/N 743602-5). CHECK-C 9-21-98 STL.SDR TWAA9814904Longeron · crackedDURING CHECK-C MAINT, FOUND .125 INCH CRACK IN LONGERON 4L AT STA 200. SPLICED IN NEW SECTION OF LONGERON PER DC9 SRM 53-02, FIG 18.SDR TWAA9804901Power Supply · inoperativeFLT STL - FLT 314 - ONE SECTION OF OVERHEAD COACH EMERGENCY LIGHTS WERE REPORTED INOP. REPLACED CEILING POWER SUPPLY IN FORWARF CABIN. (M)SDR TWAA9810108Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND ON RT WING THE SUPPORT ANGLE FROM FRONT SPAR TO NR 35 SLAT OTBD DRIVE TRACK ROLLER SUPPORT CASTING, CRACKED AT OTBD ANGLE. REMOVED AND REPLACED PLATE ON FORWARD SPAR PER SRM 51-01, PAGE 1 ITEM C, AND DAC DWG 991933SDR TWAA9810010Skin · corrodedMCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION ON FUSELAGE INTER SKIN SURFACE BELOW LT FWD EMERGENCY EXIT DOOR CUT OUT BETWEEN LONGERONS 17 AND 18, BETWEEN FS 617 AND FS 639. REMOVED CORROSION PER SRM 51-10-03. REPAIRED AREAS NECESSARY PER SRM 53-04 32SDR TWAA9805906Stringer · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND CRACK INDICATION ON LEFT WING AT XR 93, STRINGER 18. FOUND PER WORK SHEET MC8-SI-40. REMOVED FASTENER AND REAMED WITH .263 REAMER. NO CRACK INDICATION WITH HIGH FREQ EDDY CURRENT. (M)SDR TWAA9809510Skin · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACK AT FS 134, S196. REMOVED CLASS II REPAIR AND INSTALLED FLUSH REPAIR PER SRM 53-04, FIG 12B AND TWA STD PRACTICES. ACFT TT: 70,671 HOURS. ACFT TC: 77,211. (X)SDR TWAA9805904Doubler · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CRACK INDICATIONS IN 10 FASTENER HOLES IN BEAVER TAIL, TOP OF LEFT WING. CRACKS WERE INDICATED WITH HIGH FREQ EDDY CURRENT. REMOVED BEAVER TAIL DOUBLER AND INSTALLED NEW BEAVER TAIL DOUBLER PER SRM 51-01, AND STANDSDR 96ZZZM1204Dnlock Switch · failedSTL - DURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. FLIGHT RETURNED TO STL. REMOVED AND REPLACED DOWNLOCK SWITCH, MFG P/N H14-6. OPERATIONAL CHECK NORMAL.SDR 96ZZZM975Bolt · crackedSTL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK AT FRAME ATTACH BOLT, LONGERON L5, STATION 737. REPAIRED PER SRM 53-02.SDR 96ZZZX2550Longeron · crackedDURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 6L, STA 639. REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2. AIRCRAFT TOTAL TIME: 68,821 HOURS. CYCLES, 8,390.SDR 95ZZZW638Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND CRACKS 1.75 INCHES LONG ON BOTH SIDES OF SPLICE, LONGERON 30, STATION 446. REPAIRED PER SRM 53-02, FIGURE 14, SHEETS 1 AND 2, AND STANDARD PRACTICES.SDR 95ZZZW595Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND CRACKS 1.75 INCHES LONG ON BOTH SIDES OF SPLICE, LONGERON 30, STATION 446. REPAIRED PER SRM 53-02, FIGURE 14, SHEETS 1 AND 2, AND STANDARD PRACTICES.