Douglas DC-9-31

Service difficulty reports · 7,433

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 = 'DC931'
  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 TWAA0006106Structure · crackedDURING OP 16 MAINT CHECK, THE SUPPORT STRUCTURE IN SIDE OF RT WING FLAP OTBD IDLE HINGE WAS CRACKED AT INBD AND OTBD SIDE. INSTALLED INBD AND OTBD RIBS PER DRAWING 5910134, SHEET 2 ZONE 18. ---CLOSED---Mar 1, 2000 · N989Z · Doug DC931 · Wing Miscellaneous StructureSDR TWAA0003727Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND HEAVY SEALANT OVER CORRODED FLOOR WEB AT STA 218, LBL 0 TO 12 INCHES. REPLACED FLOOR MEMBRANE FROM BL 0 TO LBL 20 IN WITH RIVETS PER SRM 51-30-02.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003726Floorbeam · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR WEB STA 160 TO 200 AND LBL 22 IN TO LBL 43 INCHES HAD LIGHT CORROSION TOP OF WEB. REMOVED MEMBRANE CORRODED AREA FROM STA 160 TO 175, LBL 22 IN TO 45 IN PER SPM 6-80-1 AND SRM 51-10-3. REPLACED MEMBRANE STA 175 TO 200 WIMar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003725Floorbeam · corrodedDURING OP 16 MAINT CHECK, FLOOR SUPPORT WEB AT STA 160 TO 200 HAD LIGHT CORROSION, LB 0 TO LBL 24. REMOVED CORROSION FROM BL 0 TO LBL 24 PER SPM 6-80-1 AND SRM 51-10-3. REPLACED MEMBRANE FROM STA 180 TO 200 WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003724Floorbeam · corrodedDURING OP 16 MAINT CHECK AT STA 200 AND BL 0 TO LBL 24 INCHES, FOUND HEAVY CORROSION AND SEALANT INSTALLED ON FLOOR WEB. PARTIAL MEMBRANE REMOVED. REPLACED FLOOR MEMBRANE FROM STA 175 TO 200, BL 0 TO LBL 44 WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003723Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, STA 200 LBL 0 TO 20 INCHES. INSTALLED NEW FLOOR SUPPORT MADE FROM TWA PN S2652479-1200, WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003721Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 17L WAS CRACKED AT THE AFT SIDE OF STA 965 BULKHEAD. REPLACED LONGERON 17L FROM STA 955 TO 996 PER DRAWING 5911427. INSTALLED RIVETS PER SRM 51-30-2. PAINT PER SRM 51-10-3.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003720Hinge · crackedDURING OP 16 MAINT CHECK, THE RT WING SUPPORT STRUCTURE INSIDE OF THE FLAP OTBD IDLE HINGE WAS CRACKED INBD AND OTBD SIDE.. INSTALLED INBD AND OTBD RIBS PER DRAWING 5910134, SHEET 2 ZONE 18.Mar 1, 2000 · N989Z · Doug DC931 · Trailing Edge FlapsSDR TWAA0003711Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 16L WAS CRACKED AT STA 965 FASTENERS. INSTALLED NEW SECTION OF LONGERON FROM STA 937 TO 975 PER SPM 6-70-01 PAGE 3 AND DOUGLAS PRINT 5911427. INSTALLED SPLICE AT STA 975 PER SRM 53-02 FIG 18.Mar 1, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003710Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 17L WAS CRACKED AT STA 965 AT FASTENERS. INSTALLED NEW SECTION OF LONGERON FROM STA 955 TO 996 PER SPM 6-70-01 PAGE 3 AND DOUGLAS PRINT 5911427. INSTALLED SPLICE AT STA 955 PER SRM 53-02 FIG 18.Mar 1, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAAD00037Power Supply · failedIND - THE RIGHT NACELLE SCAN LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE RIGHT NACELLE SCAN LIGHT. (M)Mar 1, 2000 · N912VJ · Doug DC931 · Emergency LightingSDR TWAA0006105Splice · corrodedDURING OP 16 MAINT CHECK CUSP ANGLE SPLICE HAD CORROSION AT STA 210 RT. NEW SPLICE MADE PER CUSP ANGLE CORROSION REPAIR, SRM 53-05, PAGE 141. --CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006108Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND HEAVY CORROSION AT STA 200, LBL 24 AND LBL 43. INSTALLED NEW FLOOR SUPPORT WITH RIVETS PER SRM 51-30-2. PATTERN FROM OLD PART. ALODINED, PRIMED, AND PAINTED WHITE. ---CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0006107Floorbeam · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR SUPPORT AT LBL 46 TO LBL 56 HAD HEAVY CORROSION. REPLACED FLOOR SUPPORT AT STA 200 FROM LBL 46 TO 56 WITH RIVETS PER SRM 51-36-02. PATTERN FROM OLD PART. ALODINED, PRIMED, AND PAINTED WHITE. ---CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003925Angle · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR SUPPORT Z ANGLE WAS CORRODED AT STA 200, BETWEEN RBL 25 AND RBL 45. REMOVED CORRODED SUPPORT ANGLE AND FABRICATED NEW ONE FROM TWA PN 56-1360 EXTRUDED ANGLE. TREATED PER SRM 51-10-3 AND INSTALLED.Feb 29, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003729Web · corrodedDURING OP 16 MAINT CHECK, FOUND SEVERE CORROSION AT STA 220, RBL 58, THE RT SIDE CUSP ANGLE. REPAIRED PER SRM CUSP ANGLE CORROSION REPAIR 53-05, PAGE 141 AND DOUGLAS DRAWING 9923667 AND 9910078..Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003718Floorbeam · canningDURING OP 16 MAINT CHECK, THE CABIN FLOOR WEB AT STA 160 TO 200 WAS OIL CANNING AND STRETCHED EXCESSIVELY, BL 0 AND LBL 42 INCHES. INSTALLED NEW MEMBRANE FROM STA 175 TO 200, BL 0, TO LBL 44 IN, WITH RIVETS PER SRM 51-30-2.Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003709Floorbeam · crackedDURING OP 16 MAINT CHECK, THE FWD CABIN FLOOR MEMBRANE WAS CRACKED AT STA 200, RBL 24. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 4 SHEET 3.Feb 29, 2000 · N984Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003402Power Supply · inoperativeTHE EGRESS LIGHTS PAST CABIN ROW 17 STAYED ON. REPLACED THE POWER SUPPLY. CHECK-C 11-25-99 STL.Feb 29, 2000 · N992Z · Doug DC931 · Emergency LightingSDR TWAA0003728Floorbeam · corrodedDURING OP 16 MAINT CHECK, FLOOR WEB HAD CORROSION AT STA 20, LBL 48 INCHES, BELOW FWD END OF CHAIR TRACK. REMOVED CORROSION PER SPM 6-80-1. INSTALLED NEW MEMBRANE AT STA 200 FWD OF NUMBER 1 TRACK WITH PROPER FASTENERS PER SRM 51-30-2.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003717Floorbeam · crackedDURING OP 16 MAINT CHECK, THE FLOORBEAM DOUBLER WAS CRACKED AT STA 180, LBL 19 TO BL 0. REPAIRED PER SRM 53-05, PAGE 224, AND DOUGLAS PRINT 99223484.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003716Floorbeam · crackedDURING OP 16 MAINT CHECK, THE FLOORBEAM DOUBLER WAS CRACKED AT STA 180, LBL 19 TO 54. REPAIRED PER SRM 53-05, PAGE 224 AND DOUGLAS PRINT 9923484.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003712Skin · crackedDURING OP 16 MAINT CHECK AT THE AFT RIGHT LAVATORY, THE FUSELAGE SKIN WAS CRACKED AT FASTENER HOLES AT STA 965 FRAME BELOW LONGERON 16R. REPAIRED CRACKED SKIN PER SRM 53-04, PAGE 93 FIG 17.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Plate/SkinSDR GTIA000117Lens · missingROW 5 EMERGENCY AISLE BULB AND LENS MISSING. REPLACED BULB AND LENS ROW 5. (M)Feb 28, 2000 · N969ML · Doug DC931 · Emergency LightingSDR TWAA0003715Door Frame · crackedDURING OP 16 MAINT CHECK, THE LT AFT OVERWING EXIT FRAME IN THE FUSELAGE WAS CRACKED ON THE FWD AND AFT SIDE OF THE EXIT DOOR UPPER LATCH FITTING. STOP DRILLED CRACK PER SRM 53-05, FIG 32, PAGE 79. REPAIRED PER SRM 53-05 PAGE 79 FIG 32.Feb 25, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003714Door Frame · crackedDURING OP 16 MAINT CHECK, THE LT FWD OVERWING EMERGENCY EXIT FRAME IN THE FUSELAGE WAS CRACKED ON THE FWD AND AFT SIDE OF THE EXIT DOOR UPPER LATCH FITTING. STOP DRILLED PER SRM 53-05 FIG 32 PAGE 79. REPAIRED PER SRM 53-05, PAGE 19 FIG 32.Feb 25, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003707Hinge · damagedDURING OP 16 MAINT CHECK, THE LT WING TE FLAP, OTBD FLAP IDLER HINGE INBD AND OTBD, UPPER ATTACH ANGLES ON INTERIOR OF FLAP HAD FIELD REPAIR INSTALLED. REPLACED HINGE IDLER INBD AND OTBD ATTACH ANGLES PER SRM 51-30-2 FOR RIVET REMOVAL AND INSTALLATION.Feb 25, 2000 · N984Z · Doug DC931 · Trailing Edge FlapsSDR GTIA000173Light · looseACY - FLT 876 - LOOSE FLOOR PATH LIGHTING ROW 1 E/F. INSTALLED NEW SECTION OF SEAT TRACK COVER FOR SEAT ROW 1 E/F PER MM 25-00. (M)Feb 24, 2000 · N928ML · Doug DC931 · Emergency LightingSDR USAA000477Spar · crackedPIT - FOUND SPAR CAP 1.25 INCH CRACK, LEFT WING AFT SPAR STATION 164 LOWER INBOARD FLAP STUD. INSTALLED DOUBLER PER J9-15-93807 (EO 5788D220). (M)Feb 24, 2000 · N932VJ · Doug DC931 · Wing SparSDR GTIA000119Light · inoperativePBI - FLT 242 - FLOOR EMERGENCY WHITE LIGHTS INOPERABLE. REPLACED BULB; OPS CHECK OK. (X)Feb 24, 2000 · N969ML · Doug DC931 · Emergency LightingSDR TWAA0003713Stringer · crackedDURING OP 16 MAINT CHECK, AT THE AFT RT LAV, STRINGER 16R WAS CRACKED AT BOTTOM FASTENER AT AFT SIDE OF 965 BULKHEAD. REPLACED LONGERON 16R FROM STA 955 TO 980 PER SPM 6-70-01 PAGE 2 AND 3. INSTALLED LONGERON SPLICE AT STA 955R PER SRM 53-02 PAGE 48.Feb 24, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003708Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT CORRODED AT STA 237 BETWEEN BL O AND LBL 22 IN. FABRICATED NEW PART PER SAMPLE SPM 6-70-01 AND SRM 53-11-1 MATERIAL SPECS. APPLIED PROTECTIVE TREATMENT PER SRM 51-10-3. INSTALLED PART PER SRM 51-30 AND 51-10-04.Feb 24, 2000 · N984Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003206Longeron · crackedDURING OP 16 MAINT, LONGERON 16R WAS CRACKED AT STA 945 AND 965. REMOVED AND REPLACED LONGERON PER SRM 51-01 PAGE 1, SRM 51-30-2, 51-30-05. PAINTED PER 57-00-3, STA 940 TO 996.Feb 23, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003204Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 17R CRACKED AT STA 965. REMOVED AND REPLACED LONGERON PER SRM 51-01 PAGE 1, SRM 51-30-02, SRM 51-30-5. PAINTED PARTS PER 57-10-3, STA 940 TO 996.Feb 23, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003302Skin · crackedDURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN CRACKED AT FASTENER HOLE OF STA 965 FRAME AND BELOW STRINGER 16R. REPAIRED CRACKED SKIN PER SRM 53-04, PAGE 93 FIG 17.Feb 22, 2000 · N989Z · Doug DC931 · Fuselage Main, Plate/SkinSDR 0000479960Turbine · damagedDURING CLIMBOUT, THE FLIGHT CREW REPORTED A LOUD BANG FROM THE LEFT ENGINE WITH AN ASSOCIATED LOSS IN N1 AND EPR INDICATIONS. COM PROCEDURES WERE FOLLOWED AND THE LEFT ENGINE WAS RETARDED TO IDLE. THE EGT INDICATION STABILIZED TO 380 DEGREES CELSIUS WITH ALLFeb 22, 2000 · N920RW · Doug DC931 · Turbine SectionSDR TWAA0003019Bracket · crackedDURING OP 16 MAINT CHECK, THE BULKHEAD BRACKET WAS CRACKED AT STA 148 BELOW LONGERON 3L. FABRICATED AND INSTALLED NEW BRACKET PER SPM 6-70-01, PAGE 3 AND DAC DRAWING 9955780.Feb 19, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003016Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF FLOOR WEB, FWD SIDE OF FLOOR SUPPORT ON AFT SIDE, STA 200, BL-0, LBL 52. REMOVED CORROSION BY REMOVING WEB. INSTALLED WEB REPAIR PER SRM 53-01, PAGE 9 SHEET 3, FIG 2.Feb 17, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003018Frame · damagedDURING OP 16 MAINT CHECK, FOUND TEMPORARY FORMER REPAIR AT STA 980, STRINGER 16L TO 18L. REPLACED FORMER FRAME WITH NEW PER TWA SP. INSTALLED FRAME SPLICE REPAIR BETWEEN LONGERON 11L AND 10L PER SRM 53-03, PAGE 131. INSTALLED SEALER PER SRM 51-20.Feb 16, 2000 · N989Z · Doug DC931 · Fuselage Main, FrameSDR GTIA000106Light · looseTPA - FLT 431 - FLOOR TRACK LIGHTING COMING OUT FROM FLOOR TRACK ROW 16, 17. REPLACED LAMP AND REINSTALLED FLOOR TRACK LIGHTING ROW 16 AND 17. OPS CHECK GOOD IAW DC9 MM 33-00. (M)Feb 16, 2000 · N928ML · Doug DC931 · Emergency LightingSDR GTIA000097Wire · exposedDTW - RIGHT SIDE AFT INTERIOR COMPARTMENT FLOOR TRACK LIGHTING WIRES PULLED OUT. FOUND WIRES LYING ON TOP OF CARPET. NO DAMAGE. RE-STOWED WIRES BACK UNDERNEATH CARPET. OPS PER 33-50-0 GOOD. NO OTHER DEFECTS NOTED. (M)Feb 16, 2000 · N969ML · Doug DC931 · Light System WiringSDR ABXA000108Sensor · failedRIGHT MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT GO OUT. RECYCLED GEAR. LIGHT STILL WOULD NOT GO OUT. REPLACED RIGHT MAIN GEAR DOWNLOCK SENSOR. CYCLED GEAR SEVERAL TIMES, OPS CHECKED GOOD IAW DC9 SMM 32-60-01.Feb 16, 2000 · N944AX · Doug DC931 · Landing Gear Position and WarningSDR 0000419975Valve · malfunctionedDURING APPROACH TO MBS WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED SLIGHTLY TO THE LEFT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. SLATS AND FLAPS WERE RETRACTED, FOLLOWED COM PROCEDURES, AND RETURNED TO DTW ANDFeb 16, 2000 · N9339 · Doug DC931 · Leading Edge Slat Position Indicating SystemSDR TWAA0003017Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 2L WAS CRACKED AT STA 200. REPAIRED LONGERON PER SRM 53-02, FIG 18.Feb 15, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0002706Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE BETWEEN STA 870 AND 889. INSTALLED ALUMINUM ALOY REPAIR PER SRM 53-01, PAGE 9. TREATED, PRIMED, AND PAINTED REPAIRED PER 51-10-03. REINSTALLED REMOVED CASTING.Feb 13, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0002705Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE, LT SIDE BETWEEN STA 851 AND 870. TREATED, PRIMED AND PAINTED ALL AREAS WORKED PER 51-10-03. INSTALLED ALUMINUM ALLOY REPAIR PER SRM 53-01 PAGE 9.Feb 13, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR GTIA000098Light · inoperativeCLE - EMERGENCY PATHWAY LIGHT INOPERATIVE, ROW 4. RELAMPED EMERGENCY PATHWAY LIGHT, OPS CHECK GOOD. (M)Feb 12, 2000 · N969ML · Doug DC931 · Emergency LightingSDR USAAD00028Manifold · leakingCLT-DAY FLT 860 - AFTER TAKEOFF, THE RIGHT ENGINE FIRE INDICATION ACTIVATED. THE THROTTLE WAS REDUCED AND THE INDICATION STOPPED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE THE RIGHT ENGINE FUEL HEAT MANIFOLD. (M)Feb 11, 2000 · N927VJ · Doug DC931 · Fuel HeaterSDR TWAA0002704Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON TOP OF FLOOR WEB, LBL 44 IN TO 56 IN, STA 160 TO 200. REMOVED CORROSION AND PRIMED AREA PER SRM 51-10-3.Feb 11, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0002703Floorbeam · corrodedDURING OP 16 MAINT CHECK, THE AFT CARGO COMPT LT FLOOR SUPPORT STRAP AT LBL 17 WAS CORRODED BEYOND LIMITS FROM STA 756 TO 927. INSTALLED NEW STRAP PER SRM 51-30 AND SRM 51-10-4 FASTENER CODE.Feb 10, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor Beam
Back to Douglas DC-9-31