Douglas DC-9-32

Service difficulty reports · 12,755

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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 95ZZZX5348Fitting · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA FOUND INSIDE THE MAIN CABIN AT FS 718, LONGERON 19 FRAME (RT) FITTING IS CRACKED FWD AND AFT SIDES, ONE 1 INCH FWD AND ONE 1 INCH AFT. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, SRM 51-Jan 19, 1995 · N938VV · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500196Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP BETWEEN XRS 387 AND XRS 395. REPAIRED RIGHT WING REAR LOWER SPAR CAP IAW ABX REA D957-10715-MR.Jan 18, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500178Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING UPPER BONDED PANEL INBOARD OF THE GEAR TRUNNION. REPLACED UPPER BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.Jan 18, 1995 · N988AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9500167Retainer · crackedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; SB 56-11, REV 3 X-RAY INSPECTION OF LEFT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239.Jan 18, 1995 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500165Retainer · crackedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV 3 X-RAY INSPECTION OF THE RIGHT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239.Jan 18, 1995 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZX5351Skin · dentedUPON A SCHEDULED INSPECTION A AERO CORP IN LAKE CITY, FLORIDA, THE EXTERNAL SKIN WAS FOUND WITH NUMEROUS DENTS, FROM FS 237 TO FS 541, FROM LONGERON 17R TO LONGERON 25R. REMOVED DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DC9 SJan 18, 1995 · N938VV · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95008Beam · crackedDURING C-CHECK, FOUND AFT CARGO DOOR NR 4 BEAM FWD END CRACKED. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 52-01.Jan 17, 1995 · N602ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA95007Skin · gougedDURING C-CHECK, FOUND LT VERTICAL STAB SKIN GOUGED UNDER HORIZONTAL TO VERTICAL STAB FAIRING. FABRICATED AND INSTALLED NEW SKIN SECTION IAW SRM 51-10-2A AND 51-01 PG 1.Jan 17, 1995 · N602ME · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR 9501569984Rib · crackedDURING PERIODIC CHECK, FOUND APPROXIMATELY 70 WORKING RIVETS ON THE LEFT SIDE OF THE RUDDER. FURTHER X-RAY INVESTIGATION REVEALED CRACKS IN THE 2ND RIB BELOW THE SEAM. REPLACED RUDDER.Jan 17, 1995 · N984US · Doug DC932 · Rudder, Spar/RibSDR CAL950038Slide · low pressureFLT NR 1524 - MSY - THE R-1 GALLEY DOOR SLIDE WAS FOUND WITH LOW PRESSURE DURING A PREFLIGHT CHECK. THE R-1 GALLEY DOOR SLIDE WAS REMOVED AND REPLACED. (Z)Jan 16, 1995 · N12507 · Doug DC932 · Escape SlideSDR ABXA9500181Retainer · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE CAPTAIN'S CLEARVIEW WINDOW RETAINER. REPAIRED RETAINER IAW ABX REA D953-10757-MR.Jan 16, 1995 · N988AX · Doug DC932 · Flight Compartment WindowsSDR ABXA9500171Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FUSELAGE EXTERIOR SKIN FROM FS 588 SPLICE TO FS 669 SPLICE AT LONGERON 26 LEFT TO 26 RIGHT. REPLACED SKIN IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jan 16, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZX868Instrument Amp · failedATL/MIA - FLT 595 - RETURNED TO ATL DUE TO FIRST OFFICER'S GYRO WENT INOP ON CLIMB-OUT. REMOVE AND REPLACE NR 2 GYRO AND REMOVE AND REPLACE INSTRUMENT AMP PER MM 34-00, OPS CHECK NORMAL.Jan 16, 1995 · N523MD · Doug DC932 · Navigation SystemSDR 95ZZZX867Vertical Gyro · failedATL/MIA - FLT 595 - RETURNED TO ATL DUE TO FIRST OFFICER'S GYRO WENT INOP ON CLIMB-OUT. REMOVE AND REPLACE NR 2 GYRO AND REMOVE AND REPLACE INSTRUMENT AMP PER MM 34-00, OPS CHECK NORMAL.Jan 16, 1995 · N523MD · Doug DC932 · Attitude Gyro and Indicating SystemSDR 95ZZZW96Bus Proct Pnl · failedATL-MEM - FLT 520 - REPORTED NUMEROUS CIRCUIT BREAKERS WERE POPPING IN COCKPIT. CAPTAIN DECLARED AN EMERGENCY. FLIGHT RETURNED TO ATL. REMOVED AND REPLACED BUS CONT PANEL, OPS CHECK GOOD PER MM 24-52.Jan 16, 1995 · N908VJ · Doug DC932 · AC Power Distribution SystemSDR 9501099919Mlg Door · openLEFT MAIN GEAR DOOR WAS OPEN ON LANDING INTO TUS. REPLACED THE LEFT MAIN GEAR DOOR SEQUENCE VALVE AND ACTUATOR DUE TO DAMAGE INCURRED. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jan 16, 1995 · N941N · Doug DC932 · Landing Gear Door Retract SectionSDR 95ZZZX866Vertical Gyro · failedATL/BNA - FLT 558 - RETURNED TO ATL DUE TO FIRST OFFICER'S ADI FAILING DURING CLIMB-OUT. REMOVED AND REPLACED NR 2 VERTICAL GYRO. OPS CHECK GOOD PER MM 34.Jan 15, 1995 · N523MD · Doug DC932 · Attitude Gyro and Indicating SystemSDR 95ZZZX5323Rudder Pedal · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A CRACK WAS FOUND IN THE CAPTAIN'S LEFT RUDDER PEDAL AFT, INBD BOLT HOLE DURING INSP ON SB 27-209, AD 82-04-02. REMOVED AND REPLACED THE RUDDER PEDAL IAW SB 27-209 AND AD 82-04-02. N/R NR 027A1/Jan 15, 1995 · N935VV · Doug DC932 · Rudder Control SystemSDR 95ZZZM355Rib · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LOWER RIB AT FS 813 LONGERON 27L TO LONGERON 27R WAS FOUND CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-30-3. N/R NR 027N1/0381.Jan 15, 1995 · N937VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM354Frame · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CRACKS WERE FOUND PROGRESSED BEYOND THE STOP DRILL IN THE LOWER FRAME AT FS 870 ABOVE LONGERONS 29 LT AND RT AND 28R. FABRICATED AND INSTALLED NEW LOWER FRAME IAW DC9 SRM 51-10-3, 53-03 AND 51-10Jan 15, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM350Skin · dentedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .052 IN DEPTH DENT WAS FOUND IN THE FUSELAGE (PRESSURIZED) SKIN FS 275. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04 FIG 38. N/R NR 027N1/0281.Jan 14, 1995 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500199Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR FROM STATION XRS 488 TO XRS 520. REPAIRED LEFT WING LOWER REAR SPAR IAW ABX REA D957-10692-MR.Jan 13, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500040Jamb · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON THE AFT LOWER CARGO DOOR JAMB WEB. REPAIRED WEB IAW ABX REA D953-10732-MR.Jan 13, 1995 · N945AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500039Blkhd Tee · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON BULKHEAD TEE AT STA 1039 BETWEEN LONGERON 30 AND 26L. REPAIRED TEE IAW ABX REA D953-10761-MR.Jan 13, 1995 · N945AX · Doug DC932 · Fuselage Main, BulkheadSDR 95ZZZW95Press Sensor · failedON CLIMB-OUT, PRESSURIZATION UNCONTROLLABLE IN AUTO AND MANUAL. AUTO PILOT PREVIOUSLY ON MEL. FLIGHT RETURNED TO ATL. REPLACED CABIN PRESSURE DIFFERENTIAL SENSOR.Jan 13, 1995 · N1269L · Doug DC932 · Cabin Pressure SensorSDR 95ZZZM356Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FRAME BETWEEN LONGERONS 24R AND 26R AT FS 218. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-2A, 53-03, 53-01, 51-10-4 AND 51-10-3. N/R Jan 13, 1995 · N937VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM353Skin · damagedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A LIFE LIMITED REPAIR WAS FOUND BETWEEN LONGERON 27L AND 28R AT FUSELAGE STATION 867 TO FS 900.5. FABRICATED AD INSTALLED FUSELAGE (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 51-10-3 AND 53-04 AND AERJan 13, 1995 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZM352Skin · dentedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .023 INCH DEPTH DENT WAS FOUND AT FS 945 AND LONGERON 26L. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 53-04 AND 51-30-2. N/R NR 027N1/0127.Jan 13, 1995 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZM351Skin · dentedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .027 INCH DEPTH DENT WAS FOUND AT FS 332 BETWEEN LONGERONS 23L AND 24L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04, 51-30-2 AND 51-10-4. N/R NR 027N1/0131.Jan 13, 1995 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500176Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP BETWEEN XRS 385 AND XRS 390. REPAIRED LEFT WING LOWER REAR SPAR CAP IAW ABX REA D957-10773-MR.Jan 12, 1995 · N988AX · Doug DC932 · Wing SparSDR ABXA9500148Skin · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE SKIN GOUGED AT THE ENTRY DOOR FORWARD JAMB, SECOND PRESSURE STOP FROM BOTTOM. REPAIRED SKIN IAW ABX REA D953-10696-MR.Jan 12, 1995 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500038Gusset · damagedDURING C-CHECK INSPECTION, FOUND A GUSSET CHAFED AT STA 965, LONGERON 4R AND 4L. REPAIRED GUSSET IAW ABX REA D953-10730-MR.Jan 12, 1995 · N945AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500037Floor Beam · damagedDURING C-CHECK INSPECTION, A PRIOR REPAIR TO THE FLOOR BEAM AT STA 996, RBL35 WAS REMOVED TO REVEAL SEVERAL CUTOUTS IN THE UPPER FLANGE OF THE ANGLE. FLOOR BEAM WAS REPAIRED IAW ABX REA D953-10768-MR.Jan 12, 1995 · N945AX · Doug DC932 · Fuselage Main, Floor BeamSDR 95ZZZW99Pressurization · malfunctionedATL-PHL - FLT 534 - EN ROUTE, OXYGEN MASKS DEPLOYED AUTOMATICALLY DUE TO USE OF AUTO PRESSURIZATION SYSTEM PREVIOUSLY PLACED ON MEL AS INOP. RETURNED TO MANUAL PRESSURIZATION CONTROL AND REGAINED CONTROL. MASK PANELS AT SEAT 4 AB ROW 6 AND 7 AB AND 11 AB DIDJan 12, 1995 · N907VJ · Doug DC932 · Cabin Pressure Control SystemSDR 9500689950Altimeter · malfunctionedFIRST OFFICER'S ALTIMETER FAILED DURING CLIMB-OUT FROM GEG. FLIGHT DIVERTED TO RAP AND LANDED WITHOUT INCIDENT. REPLACED ALTIMETER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jan 12, 1995 · N9346 · Doug DC932 · Altimeter, Barometric/EncoderSDR 95ZZZW100Pressurization · malfunctionedATL-IAD - FLT 192 - DURING CLIMB-OUT, AUTO PRESSURIZATION WENT INOP AND ACFT DEPRESSURIZED AT APPROXIMATELY 10,000 FEET. OXYGEN MASKS IN CABIN DEPLOYED AND CREW PRESSURIZED ACFT MANUALLY. UPON ARRIVAL IN IAD, OXYGEN MASKS WERE STOWED AND AUTO PRESSURIZATION Jan 11, 1995 · N907VJ · Doug DC932 · Cabin Pressure Control SystemSDR MWEA95005Frame · chafedDURING SERVICE CHECK FOUND FWD SIDE WEB OF STA 1038.868 RIB CHAFED BY THE LEFT TEMP CONTROL VALVE. REPOSITIONED THE TEMP CONTROL VALVE. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-01, FIG. 4. AIRCRAFT RETURNED TO SERVICE.Jan 10, 1995 · N502ME · Doug DC932 · Fuselage Main, FrameSDR ABXA9500190Angle · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD END OF THE CANTED KEEL ATTACH ANGLE HAD CORROSION REMOVAL THROUGH TWO FASTENER HOLES. REPAIRED CANTED KEEL ATTACH ANGLE IAW ABX REA D953-10752-MR.Jan 10, 1995 · N988AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZX864Skin · damagedMEM/ATL - FLT 147 - AIRCRAFT RETURNED TO GATE TO GET MORE PASSENGERS. WITH ENGINES RUNNING TOW BAR BROKE AND TUG JACKKNIFED, CAUSING DAMAGE TO BELLY SKIN FROM STA 110 TO STA 150. REPAIR TO BE MADE BY DOUGLAS AIRCRAFT CORPORATION.Jan 10, 1995 · N922VV · Doug DC932 · Fuselage Main, Plate/SkinSDR 95ZZZM341Angle · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE UPPER CUSP AT THE R-1 DOOR ENTRY WAS FOUND TO BE EXTENSIVELY CORRODED AT FS 200. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-05, 51-10-3, 51-30-1, 51-20-0 AND MM20-30-1. N/R NR 027N1/065Jan 10, 1995 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM327Fitting · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE KEEL BEAM FITTING AT FS 756 WAS CRACKED IN THE LEFT WW. REMOVED AND REPLACED THE FITTING IAW DC9 SRM 51-30-2 AND 51-30-1. N/R NR 027N1/0668.Jan 10, 1995 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM342Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO COMPARTMENT FRAMES ARE CORRODED AT FS 332 THROUGH 503 BETWEEN LONGERONS 28R AND 28L. FABRICATED AND INSTALLED REPAIR MEMBERS AND DOUBLERS IAW DC9 SRM 53-03, 51-10-2A, AND 51-10-Jan 8, 1995 · N936VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM328Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME BETWEEN LONGERON 28L AND 28R WAS FOUND CORRODED AT FS 522 AND 541. FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-10-3. N/R NR 027N1/0447 AND 0448.Jan 8, 1995 · N936VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM338Splice · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO BAY LONGERON 30 WAS FOUND WITH 3 IMPROPER SPLICES WITH CORROSION AT FS 813, 889 AND 945. FABRICATED AND INSTALLED 3 NEW SPLICES IAW DC9 SRM 53-02, 52-00. N/R NR 027A1/-0169.Jan 6, 1995 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZM329Skin · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN AT FS 1025 AND LONGERON 23L IS CORRODED. FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 53-10-1, 53-01, 51-10-3 AND 51-30-2. N/R NR 027N1/0421.Jan 6, 1995 · N936VV · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500188Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION BLEND OUT THAT EXCEEDED THE SRM LIMITS. LEFT WING REAR SPAR AT APPROXIMATELY WING STATION XRS 515. REPAIRED LEFT WING REAR SPAR TEE CAP IAW ABX REA D957-10701-MR.Jan 5, 1995 · N988AX · Doug DC932 · Wing SparSDR 95ZZZM340Frame · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME UPPER CHORD AT FS 446 BETWEEN LONGERON 25R AND LONGERON 30 WAS FOUND CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED A REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-03-02A, 51-10Jan 4, 1995 · N936VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM339Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME AT FS 465 BETWEEN LONGERON 29R AND LONGERON 30 ON INTERCOSTALS AND GUSSET WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED REPAIR ANGLES AND DOUBLERS FOR THE FRAME, GUSSETS, Jan 4, 1995 · N936VV · Doug DC932 · Fuselage Main, FrameSDR 95ZZZM330Keel Beam · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE CENTER WING KEEL AREA HAS EXTENSIVE CORROSION DAMAGE ON THE RT SIDE. FABRICATED AND INSTALLED REPAIRS FOR THE CENTER WING KEEL PANEL AND LONGERONS 29 LT AND RT IAW DC9 SRM 51-10-3, 51-30-0, 5Jan 4, 1995 · N936VV · Doug DC932 · Fuselage Main, KeelSDR MWEA96002Battery Pack · dischargedDURING A CHECK FOUND FIRST FOUR ROWS OF OVERHEAD EMERGENCY LAMPS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK.Jan 3, 1995 · N202ME · Doug DC932 · Emergency Lighting
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