Douglas DC-9-33F

Service difficulty reports · 1,681

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 = 'DC933F'
  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 ABXA060006Housing · crackedHOLD OPEN HOOK SUPPORT STRUCTURE INSIDE SERVICE DOOR WAS CRACKED AT LOWER SHAFT BEARING MOUNT. REPLACED FITTING IAW DC9 SRM.Dec 19, 2005 · N932AX · Doug DC933F · Cargo/Baggage DoorsSDR ABXA060005Fitting · crackedEND FITTING CRACKED LONGERON 29 RIGHT AT FS 604. REMOVED AND REPLACED END FITTING IAW DC9 SRM 51-30-5.Dec 18, 2005 · N932AX · Doug DC933F · Fuselage Main, Attach FittingsSDR ABXA060004Skin · corrodedCRACK IN FUSELAGE KEEL SKIN AT STA 600 BETWEEN LONGERON 30 - 29 LEFT. REPAIRED AREA IAW DC9 SRM 53-04 AND REA D953-52948MR.Dec 18, 2005 · N932AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA060002Floorbeam · corrodedCORROSION ON SUBFLOOR AT FLOORBEAM FS 135, LEFT BUTTLINE 14. REPAIRED CORRODED AREA IAW DC9 SRM 53-01.Dec 16, 2005 · N932AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA060003Structure · corrodedFOUND CORROSION ON SUBFLOOR AT FLOORBEAM FS 135, RIGHT BUTT LINE 28 TO 40. REPAIRED CORRODED AREA IAW DC9 SRM 53-01.Dec 16, 2005 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050356Switch · out of positionAFTER TAKEOFF WHEN THE GEAR WAS RAISED, GOT THE TAKEOFF WARNING HORN. LOWERED THE GEAR TO EXTINGUISH THE HORN. AFTER THE SLATS AND FLAPS WERE UP, GEAR WAS RAISED WITH NO FURTHER PROBLEMS. TAKEOFF WARNING TESTS OK. GEAR WARNING TEST FAILED AT 5 DEGREES FLADec 13, 2005 · N932AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA050239Intercostal · crackedINTERCOSTAL AT LONGERON 11 LEFT, FS 718 - 699 CRACKED ON ONE END. REPAIRED AREA IAW DC-9 SRM 53-01.Sep 12, 2005 · N930AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050238Skin · crackedFORWARD FUSELAGE SKIN AFT OF LEFT NOSE WHEEL WELL CRACKED IN SEVERAL PLACES. FABRICATED DOUBLER/INSTALLED IAW DC-9 SRM 51-30-2.Sep 9, 2005 · N930AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA050211Wire · brokenFIRST OFFICER'S BRIEFCASE LIGHT EMITTED ELECTRICAL SPARKS OUT OF THE LIGHT/LENSE AREA. MAINTENANCE REPAIRED BROKEN WIRE AT BRIEFCASE LIGHT. OPS CHECKED OK IAW ABX MAINTENANCE MANUAL 33-10.Sep 9, 2005 · N933AX · Doug DC933F · Light System WiringSDR ABXA050237Frame · crackedLEFT FORWARD MAIN FRAME CRACKED AT FORWARD AND AFT FLANGE POINTS G & J. MAIN FRAME REQUIRES REPLACEMENT PER NEA53400100-002-30 AND ES00914. REMOVED AND REPLACED LEFT FORWARD MAIN FRAME IAW EA 53400321-001-3.Sep 7, 2005 · N930AX · Doug DC933F · Fuselage Main, FrameSDR ABXA050236Channel · corrodedRIGHT FLOOR CHANNEL CORRODED ON UPPER AND LOWER SURFACE, FORWARD OF FRAME FS 313. CORRODED AREAS BEYOND LIMITS. REMOVED BAD SECTION FROM APPROXIMATELY STR 308 - 360. FABRICATED REPLACEMENT SECTION AS NEEDED AND RE-INSTALLED.Sep 7, 2005 · N930AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050182Panel · debondedLT WING OB UPPER TRAILING EDGE PANEL HAD SKIN DAMAGE AT STA. XRS 516. SKIN DEBONDED AND ROLLED BACK FROM THE LEADING EDGE PANEL. DAMAGED AREA MEASURED 6 INCHES LONG BY 18 INCHES WIDE. DEFERRED: NR 45199. TEMP REPAIRED IAW REA D957-52280. CLEARED: DI NR 45199.Aug 3, 2005 · N933AX · Doug DC933F · Wing, Plate/SkinSDR ABXA050098Bearing · wornDURING GEAR RETRACTION AFTER TAKEOFF, GEAR OPEN LIGHT ILLUMINATED. REMAINED ON FOR INFLIGHT PORTION, EXTINGUISHED DURING GEAR EXTENSION FOR LANDING. REMOVED AND REPLACED WORN BEARINGS AND HINGE PINS ON LEFT AND RIGHT MAIN LANDING GEAR INBOARD DOORS IAW DC-9 Apr 21, 2005 · N932AX · Doug DC933F · Landing Gear DoorsSDR ABXA050039Contact · wornUPON LOWERING THE LANDING GEAR, NO NOSE GEAR SAFE LIGHT. TESTED IN BRIGHT AND DIM. AFTER INITIATING A GO-AROUND, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED (APPROXIMATELY 30 SECONDS). FOUND BULB CONTACTS TO BE WORN. RELAMPED, OPS CHECKED GOOD.Mar 2, 2005 · N934AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA050035Battery · dischargedEMERGENCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-00. OPS CHECKED GOOD.Feb 22, 2005 · N932AX · Doug DC933F · Emergency LightingSDR ABXA050054Intercostal · crackedINTERCOSTAL AT STA 194 IN AIRSTAIR DOOR WAS CRACKED AND CORRODED. REPLACED INTERCOSTAL IAW DC-9 SRM 53-30-2.Feb 16, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050053Door Frame · crackedCRACK IN VENTRAL DOOR JAMB STRUCTURE AT UPPER RIGHT CORNER. REPAIRED DAMAGED VENTRAL DOOR JAMB IAW DC-9 SRM 53-05.Feb 15, 2005 · N933AX · Doug DC933F · Fuselage Main, StructureSDR ABXA050052Skin · crackedCRACK IN FUSELAGE SKIN AT SERVICE DOOR CUTOUT LOWER AFT CORNER. REPAIRED IAW REA D953-51475MR AND DC-9 SRM 53-05.Feb 9, 2005 · N933AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA050051Support Angle · crackedFLOOR STRAP SUPPORT ANGLE CRACKED AFT SIDE OF FRAME FS 503 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050047Channel · corrodedCORROSION AT FUSELAGE FRAME AND FLOOR SUPPORT AREA STA 200, LONGERON 18 RIGHT AREA. REMOVED FLOOR PANEL AND J-CHANNEL AND RE-INSTALLED. ALL CORROSION WORK COMPLETED ON NON ROUTINE 0259 IAW DC-9 SRM 51-30-1.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050046Pan · corrodedSERVICE DOOR THRESHOLD LOWER PAN HAD A BULGE AND 3 EACH POPPED RIVETS AT AFT CORNER. REPAIRED DOOR JAMB PAN IAW DC-9 SRM 53-05.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050050Support Angle · corrodedFLOOR STRAP SUPPORT ANGLE EXFOLIATED FS 364 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050049Pan · corrodedNUMEROUS SPOTS OF CORROSION ON FORWARD LOWER CARGO DOOR CUTOUT PAN WEB. CLEANED AND TREATED CORROSION IAW DC-9 SRM 51-10-3.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050048Seat Track · corrodedSEAT TRACK AT LEFT BUTTLINE 44 WAS CORRODED BETWEEN STA 214 AND 224. REPAIRED TRACK AND SPLICED IN NEW SECTION OF TRACK IAW DC-9 SRM 53-05.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050043Structure · crackedMAIN ENTRY DOOR CRACKED LOWER HINGE CUTOUT. REPLACED MAIN ENTRY DOOR ON NON ROUTINE 0311 IAW DC-9 SRM.Feb 8, 2005 · N933AX · Doug DC933F · Passenger/Crew DoorsSDR ABXA050045Frame · corrodedCORROSION ON FRAME FS 832 LONGERON 30. REPAIRED IAW DC-9 SRM 53-03.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Main, FrameSDR ABXA050044Attach Bracket · corrodedFORWARD AIRSTAIR COMPARTMENT FOUND CORROSION ON DOOR SWITCH AND ATTACH BRACKET. REPLACED ATTACH BRACKET AND WEB IAW DC-9 DWG 9922405 AND DC-9 SRM.Feb 8, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050041Fitting · crackedLONGERON END FITTING CRACKED, LONGERON 26 RIGHT AT APPROXIMATELY 612 - AFT OF P-DOME. INSTALLED NEW END FITTING P/N 3924028-501 IAW DC-9 SRM 51-30-5.Feb 7, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050042Fitting · crackedLONGERON END FITTING CRACKED, LONGERON 26 LEFT AT APPROXIMATELY 612, AFT OF P-DOME. REPLACED END FITTING IAW DC-9 SRM 51-30-5.Feb 7, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050040Attach Fitting · crackedRIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING FS 718 CRACKED. REPLACED FITTING IAW DC-9 SERVICE BULLETIN 53-80.Feb 7, 2005 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050032Angle · crackedCRACK INDICATION ON ANGLE, UPPER INTERIOR SURFACE OF PYLON, 3RD FROM FRONT SPAR. REMOVED ANGLE, FABRICATED NEW ANGLE, REINSTALLED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.Jan 21, 2005 · N935AX · Doug DC933F · Nacelle/Pylon, Main FrameSDR ABXA050033Floor Support · crackedCABIN FLOOR SUPPORT BRACE FITTING CRACKED FS 775, LONGERON 23 RIGHT. REMOVED AND REPLACED SUPPORT STRUT IAW DC-9 SRM 51-30-5 AND 51-30-2.Jan 21, 2005 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050031Bulkhead · crackedWEB WAS CRACKED BETWEEN LEFT UPPER RADOME GUIDE PIN AND RIVET. REPAIRED CRACKED WEB IAW DC-9 SRM 53-01.Jan 19, 2005 · N935AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA040387Window · stuckCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NORMAL.Dec 1, 2004 · N934AX · Doug DC933F · Flight Compartment WindowsSDR ABXA040399Bearing · crackedRIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM.Nov 16, 2004 · N934AX · Doug DC933F · Horizontal Stabilizer StructureSDR ABXA040398Frame · crackedRIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACED FRAME AT STA 699 IAW EA 53400322-001-3.Nov 12, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040393Skin · crackedLOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040392Skin · crackedMAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 53100126-001, SERVICE REPAIR DRAWING SR09530252-7001 AND DC-9 SRM 53-05.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040397Frame · crackedAFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040396Skin Panel · crackedTWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040395Frame · crackedFRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03.Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040394Longeron · crackedLONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415.Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA040350Door Frame · crackedCRACKED AT SHEAR PIN RECEPTICLE ON P-DOME, 11:00 POSITION. REPAIRED IAW REA D953-50852MR AND SRD 5934886-510.Oct 11, 2004 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA040356Floorbeam · corrodedCUT OUT AND REPAIR ANGLE ON FLOORBEAM AT FS 294, CORRODED RIGHT BUTT LINE 6. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5.Oct 6, 2004 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA040357Attach Angle · crackedNR 1 PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED ATTACH ANGLE IAW DC-9 SRM 54-04.Oct 6, 2004 · N931AX · Doug DC933F · Nacelle/Pylon Miscellaneous StructureSDR ABXA040303Rib · crackedP-DOME PLUG DOOR NR 9 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.Aug 28, 2004 · N935AX · Doug DC933F · DoorsSDR ABXA040304Rib · crackedPRESSURE DOME PLUG DOOR NR 4 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-02.Aug 28, 2004 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA040281Skin · dentedDENT IN FUSELAGE SKIN AT STA 837, LONGERON 22 RIGHT, 11 INCHES LONG X .75 INCH WIDTH X .020 INCH DEEP. INSTALLED PERMANENT REPAIR IAW COI 47242-001.Jul 24, 2004 · N935AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040213Connector · dirtyON INITIAL GEAR EXTENSION, RED NOSE LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION WITH NO GREEN LIGHT. RECYCLED GEAR WITH ONLY MOMENTARY FLICKER OF RED NOSE LIGHT. GREEN NOSE LIGHT EVENTUALLY ILLUMINATED AND WAS VERIFIED. ALL OTHER INDICATIONS NORMAL. INSPECTJun 23, 2004 · N930AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA040181Controller · defectiveON TAXI, LEFT PACK CYCLED ON AND OFF A FEW TIMES, BUT OPS NORMALLY BEFORE TAKE-OFF. AT 3500 FT LEFT PACK SHUTDOWN, AT 4000 FT RIGHT PACK SHUTDOWN. THEY BOTH CYCLED ON AND OFF. AT 10000 FT TURNED EACH PACK OFF PER ABNORMAL. ONE AT A TIME TO COOL DOWN. AFTEMay 19, 2004 · N931AX · Doug DC933F · Cabin Temperature Controller
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