Douglas DC-9-32

Service difficulty reports · 12,755

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC932'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MWEA98849Former · bentFOUND FORMER BENT AT STATION 965 FROM L26L TO L26R. MAINTENANCE REMOVED AND REPLACED FORMER.Aug 10, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98848Bulkhead Tee · dentedFOUND AFT PRESSURE BULKHEAD LOWER TEE DENTED BETWEEN LONGERON 29L-29R ON FORWARD LOWER LEG AND BETWEEN 29L-30 ON AFT LOWER LEG. MAINTENANCE REMOVED AND REPLACED TEE.Aug 10, 1998 · N209ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98847Support · bentFOUND JACK SUPPORT BRACKET BENT AT STATION 996 AT LONGERON 30. MAINTENANCE REMOVED AND REPLACED JACK SUPPORT BRACKET.Aug 10, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98846Frame · crackedFOUND THE MOST AFT CANTED FRAME AT STATION 1168 CRACKED AT THE 9 O'CLOCK POSITION. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.Aug 10, 1998 · N209ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98845Bulkhead Support · misinstalled4 BOT ORIG HOLES ON VERTICLE JACK PAD SUPPORT WILL CREATE BELOW MINIMUM EDGE DISTANCE IN VERTICLE LEG ON AFT PRESS BULK TEE. MAINTENANCE FABRICATED AND INSTALLED DOUBLER ANGLE REPAIR.Aug 10, 1998 · N209ME · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9800737Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED. REPLACED LONGERON 17R IAW DC9 SRM 51-30-2 AND 51-30-5.Aug 10, 1998 · N983AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9809899918Clamp · brokenTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO MSP. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CLAMP BROKEN AT LEFT AIR CYCLE MACHINE INLET DUCT. REPLACED CLAMP. OPERATIONAAug 8, 1998 · N940N · Doug DC932 · Pneumatic Distribution SystemSDR CALA9801415Cables · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING INTERIOR HANDLE WAS EXCESSIVE AT 45 POUNDS. THE FORCE REQUIRED USING EXTERIOR HANDLE WAS LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-3.Aug 7, 1998 · N14534 · Doug DC932 · Aerodynamic FairingsSDR MWEA98843Slide Cover · detachedTHE GALLEY SERVICE DOOR SLIDE COVER FELL OFF, MAINTENANCE RE-INSTALLED SLIDE COVER.Aug 6, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA98841Skin · misdrilledFOUND DOUBLE DRILLED HOLE AT FS 870 BETWEEN LONGERON 30 AND 29L ON SKIN. MTC FABRICATED AND INSTALLED DOUBLER.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98840Former · bentFOUND FORMER BENT AT STATION 937 IN BETWEEN L30 TO L29R TO L28R. MTC STRAIGHTENED OUT FORMER AND INSTALLED FASTENERS.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98839Seat Rail · wornFOUND THE CAPTAINS SEAT RAIL HOLES ARE WORN. MTC FOUND RAIL WEAR WITHIN LIMITS AND FABRICATED AND INSTALLED DOUBLER.Aug 5, 1998 · N209ME · Doug DC932 · Flight Compartment EquipmentSDR MWEA98838Frame · corrosionFOUND CORROSION ON AFT CARGO COMPARTMENT FUSELAGE FRAME FS 870 AT LONGERON 29L TO 29R. MTC FABRICATED AND INSTALLED REPAIR SPLICES.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98837Lockpin Socket · crackedFOUND BOTH LEFT AFT EMERGENCY EXIT LOCKPIN SOCKETS CRACKED. MTC REMOVED AND REPLACED LOCKPIN SOCKETS.Aug 5, 1998 · N209ME · Doug DC932 · Emergency ExitsSDR MWEA98836Clip · corrodedFOUND CORROSION ON END CLIP AT LEFT SIDE FUSELAGE AT STATION 996 BETWEEN LONGERON 18L AND 20L. MTC FABRICATED AND INSTALLED END CLIP.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98835Fitting · corrodedFOUND CORROSION ON END FITTING AT LONGERON 24L STATION 990. MTC FABRICATED AND INSTALLED NEW END FITTING.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98834Longeron · corrodedFOUND CORROSION ON AFT CARGO COMPARTMENT LONGERON 29R FROM FS 880 TO 895. MTC FABRICATED AND INSTALLED SPLICED PIECE OF LONGERON.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98833Skin · scratchedFOUND SCRATCHES ON FUSELAGE SKIN BETWEEN LONGERON 21 AND 22 RIGHT AT STATION 958 AND 964. MTC FABRICATED AND INSTALLED DOUBLERS.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98832Bulkhead Web · deformedFOUND LOWER AFT PRESSURE BULKHEAD DEFORMED AND WITH TOOLING MARKS FROM LONGERON 27L TO 27R. MTC FABRICATED AND INSTALLED REPAIR DOUBLER.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98831Splice · corrodedFOUND CORROSION BEYOND LIMITS ON SPLICE CAP AT FS 889 LONGERON 26L TO 29L. MTC FABRICATED AND INSTALLED NEW SPLICE CAP.Aug 5, 1998 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801390Skin · crackedINSPECTION FOUND AFT CARGO BARRIER DOOR SKIN CRACKED AND DELAMINATED ON INBOARD SIDE WITH A PUNCTURE ON OUTBOARD SIDE. THE DOOR WAS DISASSEMBLED. THE OUTER SKIN WAS REMOVED AND THE PUNCTURED AREA WAS TRIMMED OUT. NEW SKIN AND DOUBLERS WERE FABRICATED AND INSAug 5, 1998 · N15525 · Doug DC932 · Cargo CompartmentsSDR CALA9801388Skin · crackedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, 51-10-3, 51-30-2.Aug 5, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR CALA9801389Skin · corrodedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-0, 51-30-8, AND 51-30-2.Aug 4, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR VJ9800271Bolt · missingON TAKEOFF, RT EGT IN CAUTION RANGE AND RT THROTTLES DID NOT RESPOND TO THROTTLE MOVEMENT, ENGINE REMAINED AT TAKEOFF POWER. FLIGHT CREW SHUTDOWN ENGINE AND RETURNED TO ATL MAINTENANCE BASE. VISUAL INSPECTION OF NR 2 ENGINE REVEALED ENGINE THROTTLE ROD END Aug 3, 1998 · N930VV · Doug DC932 · Power LeverSDR VJ9800270Shutoff Valve · malfunctionedAFTER TAKEOFF, FLIGHT ATTENDANT REPORTED OVERHEAT SMELL AFTER FULL HOT HAD BEEN SELECTED TO COMPENSATE FOR AN OVER CHILL IN AIRCRAFT PASSENGER CABIN. SMOKE DETECTOR WARNING RECEIVED. FLIGHT CREW SHUTDOWN RT PACK AND SMELL ALONG WITH SMOKE DETECTION WARNING DAug 3, 1998 · N919VV · Doug DC932 · Cabin Cooling SystemSDR TWAA9812511Skin · damagedDURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 495 TO 505, LONG 19 TO 20R. REPAIRED PER DC9 SRM 53-04, FIG 12B SHEET 6.Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9812510Skin · damagedDURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 800, LONG 16R. INSTALLED CLASS I REPAIR DOUBLER PER SRM 53-04, FIG 12B.Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9812509Skin · dentedDURING OP 16 MAINT CHECK, FOUND DENT IN FUSELAGE AT FS 871, BETWEEN LONG 29 AND 30 RT, 4 IN BY 6 IN BY .125 IN. REPAIRED PER SRM 53-04, FIG 12B, PAGE 25.Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9812508Longeron · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF LONG 30 AT FS 950. REPLACED LONGERON FROM FS 931 TO 955, PER 51-01, PAGE 4. SEALED PER SRM 51-20-0.Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9812506Doubler · corrodedDURING OP 16 MAINT CHECK, FOUND REINFORCING DOUBLER ABOVE JACK PAD ABOVE SKIN WITH CORROSION, FS 996 LONGERON 28L TO L28R. REMOVED DOUBLER FOR REPLACEMENT PER SRM 51-01, PG 1 ITEM C. INSTALLED NEW 991561-73 DOUBLER PER DOUGLAS BLUEPRINT NR 9915561 AND SRM 53Aug 3, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9812505Doubler · crackedDURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 996, LONGERON 28 AND 29R. REPAIRED CRACK AS REQUIRED PER SRM 53-04, FIG 12B, AND ARA 15299.Aug 3, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9812504Bulkhead Angle · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON L-ANGLE AT PRESSURE BULKHEAD UNDER REPAIR 6 IN LBL TO 6 IN RBL. REMOVED L-ANGLE DOUBLER NR 9915661-33 FOR REPLACEMENT PER SRM 51-10-01, PG 1 ITEM C. INSTALLED NEW L-ANGLE DOUBLER 9915561-33 PER SRM 51-30-2.Aug 3, 1998 · N995Z · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801385Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 2L. REPAIRED IAW SRM 53-04, FIGURE 27.Aug 3, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800258Battery Charger · inoperativeROW 24 AND AFT EPL LIGHTING INOP. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK CHARGER IAW MM 25-60.Aug 1, 1998 · N919VV · Doug DC932 · Emergency LightingSDR VJ9800275Frame · crackedCABIN FRAME BETWEEN CABIN FLOOR AND CENTER TANK AT STA 617, RBL 58, CRACKED. HFEC INSPECTION VERIFIED CRACK IN RADIUS TO BE TWO INCHES FROM LOWER END OF PART. STOP DRILLED CRACK IAE EO 9-53-006. HFEC VERIFIED STOP DRILLED CRACKS, SHOT PEENED ENTIRE FRAME, TJul 31, 1998 · N902VJ · Doug DC932 · Fuselage Main, FrameSDR VJ9800274Longeron · corrodedFWD CARGO COMPARTMENT UPPER FLANGE OF LONGERON 27R, FS 346, CORRODED BEYOND LIMIT. CUT OUT CORRODED SECTION OF LONGERON AND SPLICED IN NEW SECTION IAW DC9 SRM 51-10-4, 51-10-3, 53-02, FIG 18.Jul 31, 1998 · N902VJ · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800257Slide · looseR1 DOOR EMERGENCY SLIDE APPEARS LOOSE. RESECURED R1 DOOR SLIDE PER MM 25-60.Jul 31, 1998 · N914VV · Doug DC932 · Emergency EquipmentSDR VJ9800256Slide · detachedR1 DOOR EMERGENCY SLIDE FELL OFF DOOR. SLIDE LANYARD DISCONNECTED. REINSTALLED R1 DOOR SLIDE IAW MM 25-60.Jul 31, 1998 · N966VV · Doug DC932 · Emergency EquipmentSDR VJ9800255Slide · detachedL1 DOOR EMERGENCY SLIDE PACK FELL OF DOOR. REINSTALLED SLIDE AND COVER PER MM.Jul 31, 1998 · N915VV · Doug DC932 · Emergency EquipmentSDR CALA9801382Strap · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-0.Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801381Bracket · gougedINSPECTION FOUND NR 1 THRUST REVERSER PANEL BRACKET GOUGED. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2A, AND 51-30-2.Jul 31, 1998 · N15525 · Doug DC932 · Engine Thrust ReverserSDR CALA9801380Angle · crackedINSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, AND 51-00.Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801375Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE ATTACH ANGLE AT STA 1059, LONGERON 15R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.Jul 31, 1998 · N14534 · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800684Retainer · crackedDURING AIRCRAFT C-CHECK, A CRACK WAS FOUND ON THE LOWER AFT CORNER OF THE WINDOW RETAINER LOCATED AT STATION 656R. CRACK MEASURES APPROXIMATELY .5. REPAIRED IAW ABX REA NR D 953-24234.Jul 31, 1998 · N983AX · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98828Slide Cover · detachedTHE GALLEY SLIDE COVER FELL OFF. MTC INSTALLED GALLEY DOOR SLIDE COVER.Jul 30, 1998 · N207ME · Doug DC932 · Emergency EquipmentSDR CALA9801374Skin · crackedINSPECTION FOUND TWO .5 INCH CRACKS AT FASTENERS IN LEFT FUSELAGE SKIN AT STA 1019 ABOVE PYLON. THE AREA WAS REPAIRED IAW SRM 53-04, FIGURE 27.Jul 30, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801373Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AT STA 1068. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 8.Jul 30, 1998 · N14534 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801372Skin · wornINSPECTION FOUND FUSELAGE SKIN HAD ELONGATED HOLES AT LT VERTICAL FIN ATTACH ANGLE AREA. ALL HOLES WERE REAMED, FILLER WAS FABRICATED AND INSTALLED, AND EDDY CURRENT WAS PERFORMED IAW ECRA 5330-02692.Jul 30, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801371Torsion Bar · corrodedINSPECTION FOUND RT WING INBOARD TORSION BAR CORRODED. THE TORSION BAR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 27-61-6.Jul 30, 1998 · N14534 · Doug DC932 · Drag Control SystemSDR CALA9801370Panel · corrodedINSPECTION FOUND CORROSION ON TOP SIDE LEFT WING PANEL NR 1122A. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, PAGE 8, 57-31-1, 51-10-3, AND 51-30-2.Jul 30, 1998 · N15525 · Doug DC932 · Wing, Plate/Skin
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