Douglas DC-9-32F

Service difficulty reports · 517

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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 = 'DC932F'
  ORDER BY difficulty_date DESC"

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SDR ABXA070261Frame · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPAIRED AREA IAW DC9 SRM 5303 FIG 34.Aug 15, 2007 · N909AX · Doug DC932F · Fuselage Main, FrameSDR ABXA070260Fitting · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED CLIP FOR INTERCOSTAL, REF AD 2002-21-09. FABRICATED AND INSTALLED NEW CLIP IAW DWG 9957899 AND DC9 SRM 51-30-05.Aug 15, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070259Fitting · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED INTERCOSTAL CLIP, REF AD 2002-21-09. FABRICATED AND INSTALLED IAW DWG 9957899 AND DC9 SRM 51-30-5.Aug 14, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070258Frame · crackedWHILE COMPLYING WITH EA 53300036, FOUND CENTER FRAME CRACKED AT BOTH ENDS, REF AD 2002-21-09. REPAIRED BOTH ENDS OF FRAME IAW DC9 SRM 53-03 FIG 34. TWO CRACKS: .75 INCH AND .86 INCH.Aug 14, 2007 · N909AX · Doug DC932F · Fuselage Main, FrameSDR ABXA070203Attach Bracket · corrodedFORWARD LOWER CARGO ATTACH BRACKETS CORRODED AT NUT PLATES - STA 389 AND 408, LEFT BUTT LINE 33. REMOVED CORROSION AT STA 389 AND 408, LEFT BUTT LINE 33 IAW DC9 SRM.Jun 12, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070202Seat Track · crackedFLOOR TRACK CRACKED AND CORRODED AT STA 389, LEFT BUTT LINE 44. REPAIRED TRACK IAW DC9 SRM.Jun 12, 2007 · N909AX · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA070201Attach Bracket · crackedFUSELAGE FRAME UPPER ATTACH BRACKET CRACKED AT LEFT BUTT LINE 54, APPROXIMATELY FS 412. REMOVED AND REPLACED FITTING IAW DC9 REA D953-55887-MR.May 27, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070199Intercostal · crackedINTERCOSTAL AT 28 RIGHT WAS CRACKED AROUND BOLT HOLE AT FS 596. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159.May 24, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070200Intercostal · crackedINTERCOSTAL CRACKED IN CEILING STRUCTURE AT FL 256, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159.May 24, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070198Cusp Web · crackedLEFT CUSP WEB AT STA 960 CRACKED AT LIGHTNING HOLE. REPAIRED AREA IAW DC9 SRM 53-01.May 23, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070197Cusp Web · crackedRIGHT CUSP WEB AT STA 943 - 965 CRACKED AT 4 PLACES. REPAIRED CUSP WEB IAW DC9 SRM 53-01.May 23, 2007 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070196Support Bracket · crackedLEFT WING AFT SPAR HAD CRACKED VERTICAL SUPPORT BRACKET NEAR INBOARD SPOILER ACTUATOR. REPLACED BRACKET IAW DC9 SRM.May 22, 2007 · N909AX · Doug DC932F · Wing SparSDR ABXA070194Mount · crackedUPPER STOP MOUNT ON AFT LOWER CARGO DOOR FORWARD FLANGE WAS CRACKED. REMOVED AFT LOWER CARGO DOOR. REPLACED HINGE. REINSTALLED DOOR AND TESTED DOOR WARNING IAW DC9 MM 51-31-00.May 21, 2007 · N909AX · Doug DC932F · Cargo/Baggage DoorsSDR ABXA070154Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN CRACKED AT 4:00 POSITION ADJACANT TO DOOR PIN ALIGNMENT RECEPTACLE. REPAIRED CRACK IN SKIN IAW DWG 5934886-502 AND REA D953-55733.Apr 23, 2007 · N905AX · Doug DC932F · Fuselage Main, BulkheadSDR ABXA070155Cusp Web · crackedCUSP WEB CRACKED AT STA 598 TO 617 AT BUTT LINE 58 LEFT. REPAIRED AREA OF WEB IAW DC9 SRM 53-01.Apr 23, 2007 · N905AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA070153Skin · crackedFUSELAGE SKIN CRACKED 2 PLACES FS 1087 LONGERON 3 - LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN AT STA 1095, LONGERON 3 - 4 RIGHT IAW DC9 SRM 53-04.Apr 20, 2007 · N905AX · Doug DC932F · Fuselage Main, Plate/SkinSDR ABXA070041Jackscrew · obstructedHORIZONTAL STABILIZER JACKSCREW FOUND TO BE HITTING MECHANICAL STOPS DURING OPERATION. REMOVED AND REPLACED JACKSCREW IAW DC9 MM, REF WORK ORDER 600265725.Feb 9, 2007 · N905AX · Doug DC932F · Stabilizer Control SystemSDR ABXA060306Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.Nov 27, 2006 · N909AX · Doug DC932F · Emergency LightingSDR ABXA060305Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.Nov 20, 2006 · N960AX · Doug DC932F · Emergency LightingSDR ABXA060272Battery · dischargedEMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.Sep 23, 2006 · N905AX · Doug DC932F · Emergency LightingSDR ABXA060245Battery · dischargedEMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.Aug 21, 2006 · N904AX · Doug DC932F · Emergency LightingSDR ABXA060226Engine · defectiveLEFT OIL PRESSURE LOW ANNUNCIATOR CAME ON AFTER TAKEOFF. PRESSURE AND OIL QUANTITY BOTH QUICKLY WENT TO -0-. ENGINE POWER REDUCED TO IDLE AND THEN SHUTDOWN. EMERGENCY DECLARED FOLLOWED BY NORMAL LANDING. ENGINE RAN ABOUT 2 MINUTES AFTER OIL SYSTEM FAILURE.Aug 4, 2006 · N904AX · Doug DC932F · Engine (Turbine/Turboprop)SDR ABXA060178Longeron · crackedLONGERON 30 CRACKED AT SPLICE FS 484-503. REMOVED DAMAGED LONGERON 30 AND REPLACED WITH NEW LONGERON FROM FS 417-590 IAW DC9 SRM 53-02.Apr 25, 2006 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA060179Frame · crackedLEFT FORWARD MAIN FRAME FS 699 AFT FLANGE CRACKED AT POINTS F - E AND POINTS H - I. REQUIRED 5935650 REPAIR INSTALLED. REPLACED LEFT FORWARD MAIN FRAME FS 699 IAW DC9 JOB CARD EA53400321-001-2.Apr 25, 2006 · N904AX · Doug DC932F · Fuselage Main, FrameSDR ABXA060177Repair · unknownPREVIOUS REPAIR FOUND AT BOTTOM AFT 2 DOOR STOPS OF FORWARD PASSENGER DOOR (REFER TO NEA53100033-001). REMOVED AND INSTALLED REPAIR IAW DWG SR09530252.Apr 24, 2006 · N904AX · Doug DC932F · Fuselage Main, StructureSDR ABXA060176Skin · crackedFUSELAGE SKIN WAS CRACKED AT MAIN ENTRY DOOR STOP ON AFT SIDE OF DOOR CUTOUT FORTH FROM TOP. REPAIRED FUSELAGE SKIN IAW DC9 SRM.Apr 24, 2006 · N904AX · Doug DC932F · Fuselage Main, Plate/SkinSDR ABXA050318Battery Pack · dischargedDURING PREDEPARTURE CHECK FOUND COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. DEFERRED NR 47327 REMOVED AND REPLACED BATTERIES IN PACK IAW AMM.OPS CHECKED GOOD. DEFERRED IAW GMM. ITEM 2 A12 FOR BATTERY PACK REPLACEMENT WITHIN 3 FLIGHT DAYS. PLACARD INSTALLED, Dec 6, 2005 · N909AX · Doug DC932F · Emergency LightingSDR ABXA050188Knob · looseCOCKPIT DOOR LATCH MECHANISM INOP FROM OUTSIDE COCKPIT AND DOOR WAS DIFFICULT TO OPEN AND CLOSE. RESECURED SCREWS IN DOOR HANDLE OPERATES PROPERLY AT THIS TIME.Aug 13, 2005 · N904AX · Doug DC932F · Fixed Inner DoorsSDR ABXA050228Support Angle · crackedCENTER TANK UPPER SUPPORT ANGLE WAS CRACKED AT STA 660, LEFT BUTT LINE 42. REMOVED AND REPLACED SUPPORT ANGLE IAW DC-9 SRM.May 17, 2005 · N909AX · Doug DC932F · Fuselage Main, Attach FittingsSDR ABXA050227Shear Tie · crackedRIGHT XCW 23 STRINGER 15 - 16, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP IAW DC-9 SRM.May 17, 2005 · N909AX · Doug DC932F · Wing, Center BoxSDR ABXA050226Shear Tie · crackedRIGHT XCW "0" STRINGER 17 - 18, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIPS IAW DC-9 SRM.May 17, 2005 · N909AX · Doug DC932F · Wing, Center BoxSDR ABXA050140Seat Track · brokenOUTBOARD SEAT TRACK AT FS 579 LEFT BLOWN AT SPLICE. REMOVED AND REPLACED LEFT OUTBOARD SEAT TRACK FS 579 - 560.May 17, 2005 · N909AX · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050139Intercostal · crackedINTERCOSTAL CRACKED BETWEEN STA 484 AND 503 AT LONGERON 30 FORWARD LOWER CARGO. REPAIRED AREA IAW DWG K05159 AND DC-9 SRM 51-30-5.May 16, 2005 · N909AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA050138Outflow Valve · corrodedCORROSION AROUND FASTENERS ON SUGAR SCOOP BETWEEN STA 945 - 965. REMOVED AND REPLACED OUTFLOW VALVE NOZZLE VALVE IAW DC-9 MM 21-32-05-4-0002.May 16, 2005 · N909AX · Doug DC932F · Pressure Regulator/Outflow ValveSDR ABXA050137Attach Bracket · crackedLEFT INBOARD FLAP HINGE ATTACH BRACKET CRACKED IN TWO PLACES INSIDE FLAP. MOVED AND REPLACED LEFT INBOARD FLAP HINGE ATTACH BRACKET IAW DC-9 DWG 5914872.May 16, 2005 · N909AX · Doug DC932F · Trailing Edge FlapsSDR ABXA050141Pan · crackedCRACK IN OUTER PAN AT FASTENER AFT EDGE STOP NR 3. REPAIRED CRACK IAW DC-9 SRM 52-03.May 16, 2005 · N909AX · Doug DC932F · Cargo/Baggage DoorsSDR ABXA050136Longeron · crackedLONGERON 20 LT AFT OF TRAP PANEL FITTING CRACKED. REMOVED AND REPLACED LONGERON 20 LT IAW DC-9 SRM 51-30-1 AND 51-30-5.May 13, 2005 · N909AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA050135Skin · corrodedSEVERAL AREAS OF CORROSION (BULGING SKIN) EVIDENT ON BOTTOM SKIN OF RIGHT AILERON. REPAIRED AREA IAW DC-9 SRM.May 13, 2005 · N909AX · Doug DC932F · AileronsSDR ABXA050104Skin · corrodedEVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04.Apr 18, 2005 · N905AX · Doug DC932F · Fuselage Main, Plate/SkinSDR ABXA050103Panel · crackedRIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5.Apr 15, 2005 · N905AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA050101Skin · corrodedSKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02.Apr 14, 2005 · N905AX · Doug DC932F · Fuselage Main, Plate/SkinSDR ABXA050102Longeron · corrodedSKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.Apr 14, 2005 · N905AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA040403Relay · failedDURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AND 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY'S 1 AND 2. FOUND UDec 26, 2004 · N905AX · Doug DC932F · Stabilizer Control SystemSDR ABXA040354Frame · crackedLEFT MAIN FRAME AT STA 718, CRACKED BEYOND LIMITS IN WHEEL WELL AREA AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME IAW DC-9 SRM.Oct 5, 2004 · N904AX · Doug DC932F · Fuselage Main, FrameSDR ABXA040327Wire · brokenIN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SHOWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 20-50-1. OPS CHECKEDSep 15, 2004 · N905AX · Doug DC932F · Ice/Rain Protection System WiringSDR ABXA040208Engine · stalledLEFT ENGINE COMP STALLED AND STARTED TO VIBRATE. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO BDL. REMOVED AND REPLACED NR 1 ENGINE IAW DC-9 AMM 72 AND ABX JOB CARDS. OPS CHECKED GOOD.Jun 10, 2004 · N909AX · Doug DC932F · Engine (Turbine/Turboprop)SDR ABXA040172Oil Tank · crackedAIR DIVERSION, EMERGENCY DECLARED, IN FLIGHT SHUT DOWN. AIRCRAFT DIVERTED TO SHV AFTER DEPARTURE FROM SAT WITH REPORT OF OIL PRESSURE LOSS ON NR 2 ENGINE. ENGINE OIL QUANTITY DROPPED TO ZERO, OIL TEMPERATURE BEGAN TO CLIMB. OIL PRESSURE DROPPED TO 35 PSI. NR 2May 7, 2004 · N904AX · Doug DC932F · Turbine Engine Oil SystemSDR ABXA040138Channel · damagedFOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DAMAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.Apr 3, 2004 · N905AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA040171Support · failedON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.Apr 2, 2004 · N905AX · Doug DC932F · Fuselage Miscellaneous StructureSDR Y2PA03025Relay · failedCREW WORKING ELECTRICAL PROBLEM ON LT BUSS USING COM W/APU STARTED & RUNNING. APU LOW OIL PRESSURE LIGHT & OIL TEMP HIGH LIGHT ILLUM. APU SHUTDOWN. A/C OPS ON NR 2 GEN & BATTERIES. AN EMERGENCY DECLARED, A/C GIVEN DIRECT TO SDF & VECTORED FOR APPROACH. AIDec 9, 2003 · N208US · Doug DC932F · Airborne Auxiliary Power Unit (APU) System
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