Douglas DC-9-31

Service difficulty reports · 7,433

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR 95ZZZM70Switch · inoperativeCLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY. MAINTENANCE May 29, 1995 · N972VJ · Doug DC931 · Landing Gear Position and WarningSDR 9508809989Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30, FS 937 TO 945. REPAIRED LONGERON PER EA 99-094824.May 29, 1995 · N8944E · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA950628Beltframe · chafedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA AT STA 1059 LONGERON 20R ON BELTFRAME. BLENDED OUT AREA, TREATED AND PRIMED INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A. (W)May 28, 1995 · N981VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950534Filter · leakingCVG - FLIGHT 0404 - CREW RECEIVED AN ERRATIC 'RIGHT OIL STRAINER CLOGGING' ANNUNCIATOR LIGHT BUT DID NOT EXTINGUISH WITH THE THROTTLE TO IDLE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE FLIGHT DIVERTED TO CVG. SINGLE ENGINE TIME WAS APPROXIMMay 28, 1995 · N965VJ · Doug DC931 · Turbine Engine Oil SystemSDR 9509209915Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING NR 2 FLAP FORWARD HINGE BEARING BORE. REPLACED FITTING PER CITEXT 09-5740-1-9800.May 28, 1995 · N965N · Doug DC931 · Wing, Control Surface Attach FittingsSDR USAA950627Beltframe · chafedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA STR 1076 LONGERON 14R ON BELTFRAME. BLENDED OUT CHAFED AREA, TREATED/PRIME, INSTALLED DOUBLER REPAIR UNDER FLANGE PER SRM 53-03 FIG 2A. (W)May 27, 1995 · N981VJ · Doug DC931 · Fuselage Main, FrameSDR ABXA9500640Doubler · damagedDURING C-CHECK INSPECTION, FOUND THE JAMB DOUBLER AT THE AFT EDGE OF THE AFT LOWER CARGO DOOR AT LONGERON 24 DAMAGED. REPAIRED IAW ABX REA D953-11616-MR.May 27, 1995 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500621Skin · damagedDURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND DAMAGED AT THE AFT EDGE OF THE AFT LOWER CARGO DOOR AT LONGERON 24. REPAIRED IAW ABX REA D953-11616-MR.May 27, 1995 · N946AX · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950656Skin · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1875 INCH CRACK IN FUSELAGE SKIN AT STA 100 AFT OF RT NOSE GEAR DOOR AFT HINGE. INSTALLED MFG NEW SKIN AND INSTALLED REPAIR PER SRM 53-01, FIGURE 2, SHEET 3. (X)May 26, 1995 · N983VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950655Skin · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 2 EACH, .1250 INCH CRACKS IN FUSELAGE SKIN AT STA 89 NEAR RT NOSE GEAR DOOR. INSTALLED MFG NEW SKIN REPAIR PER SRM 53-01, FIGURE 2, SHEET 3. (X)May 26, 1995 · N983VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950640Angle · corrodedPIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT STA 160 TO 218 CENTER LINE OF A/C, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 53-11. (W)May 26, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950639Angle · corrodedPIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 2 INCH BY 14 INCH AREA STA 200 TO 235, LT OF CENTER LINE IN FLOOR SUPPORT ANGLE, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 5May 26, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950638Angle · corrodedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF LEVEL 1 CORROSION IN FLOOR SUPPORT STA 200, RUNNNG FROM CENTER LINE LT TO O/B SEAT TRACK, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE PER May 26, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950637Angle · corrodedPIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT GALLEY NR 2 FLOOR SUPPORT FROM CENTER LINE TO I/B SEAT TRACK RT AT STA 200, PREVIOUS REWORK. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE SECTION PER SRM 53-11. (W)May 26, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500620Jamb · corrodedDURING C-CHECK INSPECTION, THE FORWARD UPPER CORNER OF THE AFT LOWER CARGO DOOR JAMB PAN WAS FOUND TO HAVE CORROSION DAMAGE. REPAIRED IAW ABX REA D953-11692-MR.May 26, 1995 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500619Skin · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION HAD BEEN BLENDED OUT OF THE EXTERIOR SURFACE OF THE SKIN ALONG THE LOWER EDGE OF THE FORWARD LOWER CARGO DOOR. REPAIRED IAW ABX REA D953-11690-MR.May 26, 1995 · N946AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA9500615Frame · damagedDURING C-CHECK INSPECTION, FOUND A FRAME IMPROPERLY PLUGGED AND HOLES WITH SHORT EDGE DISTANCE AT STA. 897, LONGERONS 28 AND 29R. REPAIRED IAW ABX REA D953-11619-MR.May 26, 1995 · N946AX · Doug DC931 · Fuselage Main, FrameSDR 9508799915Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 3 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5.May 26, 1995 · N965N · Doug DC931 · Cargo/Baggage DoorsSDR USAA950634Skin · dentedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY 10 INCH DENT FWD CARGO DOOR EXTERIOR SKIN UNDER DOOR HANDLE. INSTALLED DOUBLER REPAIR PER SRM 52-05 FIG 30. (W)May 25, 1995 · N981VJ · Doug DC931 · Cargo/Baggage DoorsSDR USAA950633Frame · chafedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA OUT OF LIMITS ON BELTFRAME STA 1076 LONG 14L. CUT OUT DAMAGED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 2A. (W)May 25, 1995 · N981VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950629Beltframe · chafedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 2.5 INCH CHAFED AREA AT STA 1059 LONGERON 14R BELTFRAME. BLENDED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A. (W)May 25, 1995 · N981VJ · Doug DC931 · Fuselage Main, FrameSDR ABXA9500622Jamb · damagedDURING C-CHECK INSPECTION, A WEB IN THE FORWARD LOWER CARGO DOOR JAMB WAS FOUND DAMAGED. REPAIRED IAW ABX REA D953-11706-MR.May 25, 1995 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500538Skin · gougedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED AT STA 425 LONGERON 30. REPAIRED IAW ABX REA D953-11709-MR.May 25, 1995 · N949AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500537Jamb · puncturedDURING C-CHECK INSPECTION, FOUND FLC DOOR JAMB WEB PUNCTURED AT STA 383 AND LONGERON 29R. REPAIRED IAW ABX REA D953-11695-MR.May 25, 1995 · N949AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500616Jamb · puncturedDURING C-CHECK INSPECTION, FOUND THE FORWARD LOWER CARGO DOOR JAMB PUNCTURED AND CORRODED AT STA. 427. REPAIRED IAW ABX REA D953-11598-MR.May 24, 1995 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950641Angle · corrodedPIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 6 INCH AREA PANEL NR 20 IN SUPPORT ANGLE AT STA 255, CENTER LINE, AREA PREVIOUSLY REWORKED. CPCP TASK NR C58-53303. SPLICED IN NEW SECTION OF ANGLE PER USAIR TYPICAL REPAIR 53-10-21A. (W)May 23, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950632Beam · chafedPIT - DURING Q-4/CX-5 INSPECTION, FOUND 1.5 INCH BY .050 DEEP CHAFE AFT FACE OF BEAM OF RT WING SHELF INBED OF THE SERVICE INTERPHONE JACK IN RT MLG WW. ROUTED OUT DAMAGED AREA AND INSTALLED A DOUBLER REPAIR PER SRM 53-01. (W)May 23, 1995 · N981VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950631Skin · gougedPIT - DURING Q-4/CX-5 INSPECTION, FOUND GOUGED OUT OF LIMITS AT STA 208 FROM LONGERON 1L TO AND BETWEEN LONGERON 1R AND LONGERON 2R. BURNISHED AREA AND INSTALLED TWO DOUBLERS PER SRM 53-04 FIG 38 NR 4 EFG. (W)May 23, 1995 · N981VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500618Rod · wornDURING C- CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT LANDING GEAR FLYING DOOR LINKAGE WORN. REPLACED DRIVE ROD IAW DC-9 M.M. 32-12-1.May 23, 1995 · N946AX · Doug DC931 · Landing Gear DoorsSDR ABXA9500617Fitting · crackedDURING C-CHECK INSPECTION, A BEAM SUPPORT FITTING WAS FOUND CRACKED AT STA. 965L. FITTING WAS REPLACED IAW DC-9 SRM 53-10-5 AND 53-10-2.May 23, 1995 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950630Bulkhead · crackedPIT - DURING Q-4/CX-5 INSPECTION, FOUND .5 INCH CRACK AND BUCKLING AT 965 RT BULKHEAD BETWEEN LONGERON 17R AND 18R FLOOR LEVEL. SPLICED IN NEW WEB SECTION FROM LONGERON 18R TO 17R PER SRM 53-03 FIG 19 AND USAIR EA 30491. (W)May 22, 1995 · N981VJ · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9500550Bushing · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR DRIVE ROD OUTBOARD END HAD SIDE PLAY. REPLACED BUSHINGS IAW DC-9 MM 32-10-6.May 22, 1995 · N949AX · Doug DC931 · Landing Gear Door Retract SectionSDR ABXA9500543T-Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 17 TO 18, 18 TO 19 AND 19 TO 20 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3.May 22, 1995 · N949AX · Doug DC931 · Wing Miscellaneous StructureSDR ABXA9500542Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL 1 CORROSION INSIDE BARREL NUT HOLE IN STRINGER 16, RIGHT WING. REMOVED CORROSION IAW DC-9 SB 57-98, DC-9 SRM 51-10-3.May 22, 1995 · N949AX · Doug DC931 · Wing, Longeron/StringerSDR ABXA9500541Bracket · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION AND CRACKED BRACKET BETWEEN STRINGERS 15 AND 16 AT STA XCW 58 ON THE RIGHT WING. REPLACED BRACKET IAW DC-9 SRM 51-30-5. CLEANED CORROSION BELOW BRACKET IAW DC-9 SRMMay 22, 1995 · N949AX · Doug DC931 · Wing Miscellaneous StructureSDR 9508579912Window Seal · deterioratedDURING FLIGHT DFW-DTW, THE FIRST OFFICER'S SLIDING WINDOW DEVELOPED AN EXTREMELY LOUD AIR LEAK THAT INTERFERED WITH FLIGHT COMMUNICATIONS. DIVERTED TO MEM AND LANDED WITHOUT FURTHER INCIDENT. RESEALED WINDOW, CHECKED OK.May 22, 1995 · N962N · Doug DC931 · Flight Compartment WindowsSDR 9508559959Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE FROM THE CLIPS USING BOTH THE INTERIOR AND EXTERIOR HANDLES. ADJUSTED BOTH SETS OF CLIPS, CHECKED OK.May 22, 1995 · N919RW · Doug DC931 · Aerodynamic FairingsSDR 9508549993Connector · looseDURING APPROACH INTO BWI, SLAT BLUE EXTEND LIGHT DID NOT ILLUMINATE AFTER SLAT EXTENSION. PERFORMED GO-AROUND PROCEDURES AND RECYCLED SLATS, STILL NO BLUE LIGHT. FIRST OFFICER VISUALLY CONFIRMED SLATS TO BE EXTENDED. SUCCESSFUL LANDING WAS ACCOMPLISHED USINMay 22, 1995 · N8986E · Doug DC931 · Leading Edge Slat Position Indicating SystemSDR ABXA9500596Door · defectiveDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR TO HAVE THE FOLLOWING DISCREPANCIES, ACTUATING ROD, ARTICULATING DOOR HINGE, AND ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED DOOR IAW DC-9 M.M. 32-12-1.May 21, 1995 · N907AX · Doug DC931 · Landing Gear DoorsSDR ABXA9500544T-Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL 1 CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 11 TO 12 AND 16 TO 17 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3.May 21, 1995 · N949AX · Doug DC931 · Wing Miscellaneous StructureSDR ABXA9500536Jamb · damagedDURING C-CHECK INSPECTION, FOUND ENTRY DOOR CUTOUT SKIN AND REPAIR SEPARATED AT UPPER FORWARD CORNER. REPAIRED IAW DC-9 SRM 53-05 FIGURE 25A AND ABX REA D953-11613-MR.May 21, 1995 · N949AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950524Eel Batteries · dischargedPIT - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LIGHTS AND REPLACED THE BATTERIES IN THE BATTERY PACK NR 1. OPERATIONS CHECKED NORMAL. (M)May 20, 1995 · N973VJ · Doug DC931 · Emergency LightingSDR USAA950440Clip · crackedPIT - SCHEDULED PRODUCTION CONTROL ITEM. FOUND .75 INCH CRACK STATION 995 BETWEEN LONGERSON 15 AND 16 RIGHT SKIN CLIP. SPLICED NEW SECTION OF SKIN CLIP PER SRM 53-03 FIG 6. (M)May 20, 1995 · N956VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500595Frame · crackedDURING COMPLIANCE OF A.D. 78-07-05; S.B. 53-131, FOUND LEFT FUSELAGE FRAME STA. 699 CRACKED IN THE UPPER FORWARD FLANGE OUTBOARD POCKET AND SPLICE AREA. REPAIRED FRAME IAW DC-9 S.B. 53-131 AND SERVICE REWORK DRAWING 5935650.May 20, 1995 · N907AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9500594Link · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-12-1.May 20, 1995 · N907AX · Doug DC931 · Landing Gear DoorsSDR ABXA9500593Bearing · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR ROD BEARING WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-12-1.May 20, 1995 · N907AX · Doug DC931 · Landing Gear DoorsSDR ABXA9500549Arm · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR ARTICULATING DOOR DRIVE ROD END HAD SIDE PLAY. REPLACED ARM IAW DC-9 OVERHAUL MANUAL 32-10-6.May 20, 1995 · N949AX · Doug DC931 · Landing Gear Door Retract SectionSDR 95ZZZW750Door Latch · out of adjustSTL - AFTER TAKEOFF RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION, AND LANDING GEAR DOOR OPENED DURING UPLATCH CHECK. FOUND DOOR LATCH MECHANISM, MFG P/N 5915169-5506, WOULD NOT ALWAYS ENGAGE DOOR ROLLERS. RIGGED DOOMay 20, 1995 · N980Z · Doug DC931 · Landing Gear Door Retract SectionSDR 9508519976Outflow Actuator · malfunctionedAIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED OUTFLOW VALVE ACTUATOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.May 20, 1995 · N9340 · Doug DC931 · Pressure Regulator/Outflow ValveSDR 9508469910Control Panel · malfunctionedDURING FLIGHT AND ON APPROACH, AN UNUSUAL VIBRATION WAS ENCOUNTERED WHICH SEEMED TO BE COMING FROM BELOW OR FORWARD OF COCKPIT. AFTER LANDING AND PASSENGER DEPLANEMENT, BLACK SMOKE FILLED THE COCKPIT. EXTINGUISHED ALL POWER TO AIRCRAFT AND PULLED ALL CIRCUITMay 20, 1995 · N960N · Doug DC931 · AC Power Distribution System
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