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 ZIAA979001Longeron · corrodedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LEFT TO 29 RIGHT F/S 500 AND FUSE SKIN TO LONGERON ATTACH RIVETS LONG 29 RIGHT F/S 500. ALSO, LONGERON 30 RIGHT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION Jan 9, 1997 · N932VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970048Slide Cover · fell offL1 DOOR SLIDE PACK FELL OFF. REPLACED AND REINSTALLED L1 DOOR SLIDE IAW MM 25-62-0. (X)Jan 9, 1997 · N932VV · Doug DC932 · Emergency EquipmentSDR VJ970045Longeron · corrodedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LT TO 29 RT, FS 500 AND FUSELAGE SKIN TO LONGERON ATTACH RIVETS LONGERON 29 RT FS 500, ALSO LONGERON 30 RT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION AND TRJan 9, 1997 · N932VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9700794Shear Tie · corrodedDURING C-CHECK, FOUND CORROSION ON AFT SIDE OF FRAME AND SHEAR TIE STA 622. REPLACED SHEAR TIE IAW DC9 SRM 51-10-4, 51-30-5.Jan 9, 1997 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 97ZZZX883Longeron · crackedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LT TO 29 RT, FS 500 AND FUSELAGE SKIN TO LONGERON ATTACH RIVETS LONGERON 29 RT FS 500, ALSO LONGERON 30 RT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION AND TRJan 9, 1997 · N932VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM247Switch · malfunctionedFLT 423 - FLL - TAIL CONE UNSAFE LIGHT ON. DEFERRED TAIL CONE INDICATION IAW MEL 53-1, DMI NR 00088. TAIL CONE VISUALLY INSPECTED FOR SECURITY BY RSB. C-PLUG AT RELEASE HANDLE INSIDE IS COMING APART. REPLACED TAILCONE UNSAFE SWITCH. OPS CHECK GOOD ON GROUJan 9, 1997 · N12536 · Doug DC932 · Door Warning SystemSDR 97ZZZM235Longeron · crackedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LEFT TO 29 RIGHT F/S 500 AND FUSE SKIN TO LONGERON ATTACH RIVETS LONG 29 RIGHT F/S 500. ALSO, LONGERON 30 RIGHT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION Jan 9, 1997 · N932VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM226Pitch Computer · malfunctionedDTW - FLT 512 - PASSNG 2800 FOR 2900 FEET ON AUTOPILOT A/C PITCHED UP VIOLENTLY THEN KICKED OFF. RE-ENGAGED OK FOR REST OF FLT. TRANSFERRED TO DMI NR 00089 MEL 22-1. PLACARD INSTALLED, CATEGORY C, ON LOG PAGE 026218 1/10/97. 1/19/97, LOG PAGE 026386, REMOVJan 9, 1997 · N942ML · Doug DC932 · Autopilot ComputerSDR 9700439982Connector · brokenDURING PERIODIC CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS ALONG CATWALK INOPERATIVE. INSTALLED NEW CONNECTOR ON POWER SUPPLY, OPERATIONAL CHECK NORMAL.Jan 9, 1997 · N982US · Doug DC932 · Emergency LightingSDR VJ970035Skin · holeDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL A LIGHTNING STRIKE WAS FOUND IN THE FORWARD FUSELAGE AT FS 408 AT LBL 30. CUT OUT 2 INCH AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC-9 SRM 53-04 FIG 38 AND MM 20-40-1. (M)Jan 8, 1997 · N919VV · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9700800Fitting · crackedDURING C-CHECK, FOUND VERTICAL FITTING AT UPPER SURFACE OF CENTER TANK STA 680 CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.Jan 8, 1997 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9700429941Gen Contl Panel · malfunctionedRIGHT GENERATOR DROPPED OFF LINE ACCOMPANIED BY AC CROSSTIE LOCKOUT LIGHT ILLUMINATED. FLIGHT RETURNED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR CONTROL PANEL, OPERATIONAL CHECK NORMAL.Jan 8, 1997 · N3324L · Doug DC932 · AC Generation SystemSDR ABXA9700798Angle · crackedDURING C-CHECK, FOUND CRACKED FLOOR PANEL SUPPORT ANGLE STA 639. REPLACED ANGLE IAW DC-9 SRM 51-30-2.Jan 7, 1997 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700797Fitting · crackedDURING C-CHECK, FOUND VERTICAL FITTING CRACKED AT UPPER SURFACE OF CENTER TANK STA 680. REPLACED IAW DC-9 SRM 51-10-4, 51-30-2, 51-30-5.Jan 7, 1997 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700729Longeron · crackedDURING C-CHECK, FOUND LONGERON 17L CRACKED AT FRAME STA 980 REPAIR DOUBLER, (AD 92-22-08). REPLACED SECTION OF LONGERON 17 LEFT BETWEEN FS 955 AND FS 996 IAW DC-9 SRM CHAPTER 53-02, FIGURE 2.Jan 7, 1997 · N903AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM164Wire · brokenDTW - FLT 210 - CABIN EMERGENCY LIGHTS ARE OUT OF THE TRACK FLOOR BETWEEN ROWS 2 AND 7. FOUND BROKEN WIRE AT ROW 2 RE-CRIMPED, LIGHT TEST SHOWED NORMAL OPERATION IAW DC-9 MM 33-50. (M)Jan 7, 1997 · N12536 · Doug DC932 · Light System WiringSDR 9700339982Shear Clip · crackedDURING PERIODIC CHECK, FOUND TAIL INTERIOR SHEAR CLIP ON AFT SIDE OF FRAME AT FS 1087 CRACKED LEFT OF VERTICAL ATTACH FITTING. REPLACED SHEAR CLIP AND REPAIRED WEB PER EA 99-111969.Jan 7, 1997 · N982US · Doug DC932 · Fuselage Miscellaneous StructureSDR 9700269926Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECITON, FOUND EMERGENCY EXIT LIGHT SIGN ABOVE FORWARD OVERWING DOOR INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Jan 7, 1997 · N926NW · Doug DC932 · Emergency LightingSDR VJ970117Stringer · corrosionCORROSION WAS FOUND IN THE RIGHT WING INTERNAL, AROUND THE BARREL NUT HOLE AND UPPER CHORD ON THE STRINGER 16, STATION 58-63. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3. TREATED AND PRIMED AREAS IAW DC-9 SRM 51-22-1. ALL AREAS WITHIN LIMITS IAW EO Jan 6, 1997 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970041Longeron · crackedFORWARD PIT WAS CRACKED AT STATION 580 LONGERON 29L, ON THE LONGERON. REMOVED FASTENERS, REMOVED CRACK LONGERON, DRILLED NEW LONGERON AND SPLICE, TREATED AND INSTALLED IAW DC-9 SRM 53-02 FIG 14, 51-30-2, 51-30-5. (M)Jan 6, 1997 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970040Skin · corrodedCORROSION WAS FOUND ON THE FORWARD PIT BY 'Y' DUCT IN THE SKIN BLOWN OUT (LEVEL 2) AT STATION 580 L 30 RIGHT SIDE AND FORWARD OF STATION 580 L 30. REMOVED FASTENERS, REMOVED CORRODED AREA IN INTERNAL SKIN, FABRICATED FILLER AND REPAIR DOUBLER, DRILLED, TREATEJan 6, 1997 · N922VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ970039Flap Vane · corrodedCORROSION WAS FOUND ON THE LOWER SIDE OF INBOARD FLAP FIXED VANE IN PATCH AREA. REMOVED AND REPLACED LT INBOARD VANE USING TORQUE WRENCH A-042 IAW DC9 MM 27-31-3. (M)Jan 6, 1997 · N922VV · Doug DC932 · Trailing Edge FlapsSDR VJ970038Angle · corrodedTHE AFT CARGO HAS SEVERAL SPOTS OF CORROSION ON UPPER ANGLE OF STRINGER 29R, BETWEEN STATION 889 AND 937. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS, IAW DC-9 SRM 51-10-3, RECEIVED NEW INTERCOSTAL, DRILLED HOLES AND DEBURRED IAW DC-9 SRM 51-10-4, INSTJan 6, 1997 · N922VV · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700883Vane · delaminatedTHE LEFT WING CENTER FLAP VANE HAD AREAS OF CORROSION ON BOTH THE UPPER AND LOWER SURFACES. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.Jan 6, 1997 · N903AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9700504Tab · delaminatedLEFT ELEVATOR TAB DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.Jan 6, 1997 · N903AX · Doug DC932 · Elevator, Tab StructureSDR 97ZZZM155Longeron · crackedFORWARD PIT WAS CRACKED AT STATION 580 LONGERON 29L, ON THE LONGERON. REMOVED FASTENERS, REMOVED CRACK LONGERON, DRILLED NEW LONGERON AND SPLICE, TREATED AND INSTALLED IAW DC-9 SRM 53-02 FIG 14, 51-30-2, 51-30-5. (M)Jan 6, 1997 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM154'Y' Duct · corrodedFOUND CORROSION ON THE FORWARD PIT BY 'Y' DUCT IN THE SKIN BLOWN OUT (LEVEL 2) AT STATION 580L 30 RIGHT SIDE AND FOWARD OF STATION 580L 30. REMOVED FASTENERS, REMOVED CORRODED AREA IN INTERNAL SKIN, FABRICATED FILLER AND REPAIR DOUBLER, DRILLED, TREATED AND IJan 6, 1997 · N922VV · Doug DC932 · Pneumatic Distribution SystemSDR 97ZZZM153Vane · corrodedFOUND CORROSION ON THE LOWER SIDE OF INBOARD FLAP FIXED VANE IN PATCH AREA. REMOVED AND REPLACED LT INBOARD VANE USING TORQUE WRENCH A-042 IAW DC9 MM 27-31-3.Jan 6, 1997 · N922VV · Doug DC932 · Trailing Edge FlapsSDR 97ZZZM152Stringer · corrodedTHE AFT CARGO HAS SEVERAL SPOTS OF CORROSION ON UPPER ANGLE OF STRINGER 29R, BETWEEN STATION 889 AND 937. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS, IAW DC-9 SRM 51-10-3, RECEIVED NEW INTERCOSTAL, DRILLED HOLES AND DEBURRED IAW DC-9 SRM 51-10-4, INSTJan 6, 1997 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9700169605Uplock Switch · malfunctionedDURING CLIMBOUT, THE LEFT AND RIGHT MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR WITH SAME RESULTS. FLIGHT CONTINUED TO DESTINATION AT REDUCED SPEED AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES, DISCJan 6, 1997 · N605NW · Doug DC932 · Landing Gear Position and WarningSDR MWEA97076Splice · crackedDURING D-CHECK, FOUND LONG 30 SPLICE CRACKED BETWEEN STA 794 TO 813. MAINT INSTALL NEW SPLICE IAW SRM 53-01 PG 1.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97075Longeron · corrodedDURING D-CHECK, FOUND LONG 29R CORRODED IN AFT CARGO COMPT FS 965 TO 945. MAINT FAB LONG FROM AN EXTRUSION IAW SRM 53-11-3 AND INSTALLED IAW SRM 53-01 PG 1.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97074Splice · corrodedDURING D-CHECK, FOUND LONG 29L SPLICE AT STA 410 CORRODED. MAINT FAB AND INSTALLED SPLICE IAW DAC DRW 3913291 AND SRM 51-30.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97073Longeron · corrodedDURING D-CHECK, FOUND MODERATE CORROSION ON LONG 26L AT 756. MAINT FAB LONG IAW SRM 53-11-3 AND INSTALLED REPAIR IAW SRM 51-30.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97070Bulkhead T-Cap · corrodedDURING D-CHECK, FOUND BULK LWR T-CAP IN RT WHEEL WALL STA 756 CORRODED 3 INCHES OTBD OF KEEL. MAINT INSTALLED STRAP REPAIR IAW SRM 53-03 PG 57 FIG 17.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA97069Bulkhead Skin · corrodedDURING D-CHECK, FOUND CORROSION ON AFT BULKH ON LT WHEEL WELL ABOVE LONG 29L FITTING. MAINT REMOVED AND REPLACED SKIN SECTION IAW SRM 53-03 FIG 17, 51-30-2 AND 51-30-5.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA97068Intercostal · crackedDURING D-CHECK, FOUND INTERCOSTALS AT STA 229 TO 237 BETWEEN LONG 28L TO 27L AND 28 TO 27R MODERATE CORROSION AND SEVERAL SMALL CRACKS. MAINT REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-10-3.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97067Rib · chafedDURING D-CHECK, FOUND NR 5 SECTION LT FLAP T/E END RIB HEAVILY CHAFED. MAINT FAB A REPAIR IAW SRM 51-10-2A AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.Jan 5, 1997 · N202ME · Doug DC932 · Trailing Edge FlapsSDR MWEA97066Former · crackedDURING D-CHECK, FOUND LT KEEL OTBD END OF FORMER CRACKED AT FS 622 AND FS 659. MAINT FAB A REPAIR AND INSTALLED IAW 53-03 FIG 12.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97065Skin · corrodedDURING D-CHECK, FOUND AFT FUSE SKIN UNDER APU FLUID DEFLECT CORR BEYOND LIMITS AT FS 980 TO 996 LONG 28L TO 28R. MAINT REPAIRED AREAS IAW DAC TELEX SVC-MSP-0987/PDG.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA97064Clip · crackedDURING D-CHECK, FOUND A SHOVEL CLIP CRACKED IN LEFT KEEL FS 604 LONG 29L. MAINT FAB A NEW END FITTING IAW SRM 51-10-4 AND INSTALLED IAW SRM 51-30.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97063Seat Track · corrodedDURING D-CHECK, FOUND NR 2 SEAT TRACK FWD END HAD AREA OF LIGHT CORROSION ON BOTTOM CENTER. MAINT FAB AND INSTALLED A NEW SECTION OF SEAT TRACK IAW 53-05 FIG 4.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA97062Longeron · corrodedDURING D-CHECK, FOUND LEFT KEEL AREA LONG 29L HAS CORROSION FROM FS 604 TO 635. MAINT FAB AND INSTALLED A NEW LONG IAW SRM 53-01 FIG 1.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97061Doubler · dentedDURING D-CHECK, FOUND A DENT IN FUSE SKIN AT FS 256 LONG 17R AND 18R APPROX 1 INCH DIAMETER AND .025 DEEP. MAINT FAB A DOUBLER AND INSTALLED IAW SRM 53-04 FIG VIEW G.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97060Skin · corrodedDURING D-CHECK, FOUND LEFT WHEEL WELL KEEL SKIN CORRODED FROM STA 734 TO 756. MAINT FAB AND INSTALLED SKIN PANEL FROM STA 669 TO 756 IAW SRM 51-11-3 AND 51-10-5.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA97059Skin · corrodedDURING D-CHECK, FOUND MODERATE CORROSION ON INSIDE SURFACE OF FUSE SKIN, AFT INBD CORNER OF RT WHEEL WELL BETWEEN LONG 29R AND 30. MAINT FAB AND INSTALLED SKIN PANEL IAW SRM 51-30-5 AND DAC DRW 5911418.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA97058Longeron · crackedDURING D-CHECK, FOUND LONG SPLICE AT STA 313 TO 332 LONG CRACKED 29L. MAINT REMOVED AND REPLACED LONG SECTION FROM STA 227 TO 415 IAW SRM 51-30.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97057Longeron · corrodedDURING D-CHECK, FOUND EXFOLIATION CORR IN LONG 29L FWD CARGO COMPT FROM FRAME 503 TO STATION 509 APPROX. MAINT FAB A REPAIR IAW DOUGLAS DRW 592319 AND INSTALLED IAW SRM 51-30.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97056Strap · corrodedDURING D-CHECK, FOUND THE RT WING HAD A STRAP DOUBLER NEEDING PAINT OTBD OF NR 3 SLAT DRIVE TRACK BRACKET. MAINT FOUND CORR WHICH EXCEEDED LIMITS AND REPAIRED WITH DOUGLAS TELEX SVC-MSP-0997 KJL.Jan 5, 1997 · N202ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA97055Frame · corrodedDURING D-CHECK, FOUND STUB FRAME AT STA 658 LONGERON 27R CORRODED AND CRACKED AT OUTBD END. MAINT FAB AND INSTALLED REPAIR IAW SRM 53-03 FIG 12 PG 31.Jan 5, 1997 · N202ME · Doug DC932 · Fuselage Main, Frame
Back to Douglas DC-9-32