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 0104449922Intercostal · crackedDuring M ck in ATL, A crack was found in the outboard end of the 923484-9 intercostal at station 180 at x=-20. Material 7075-t6 AL. Repaired per EA 99-181321.Jul 9, 2001 · N945N · Doug DC932 · Fuselage Main, StructureSDR 0105009922Rib · crackedDuring Mck in ATL, the aft portion of the lower cap of the pylon closing rib was found cracked. The crack is .6" long and extends from a fasterner hole 3.7" forward from the aft end of the cap. Repaired per EA 99-181307.Jul 6, 2001 · N945N · Doug DC932 · Nacelle/Pylon, Main FrameSDR 0104409922Doubler · crackedDuring an Mck in ATL the production finger doubler along Longeron 18L was found with a cracked finger sta 850. Material .025" 2014-t6 AL. Repaired per EA 99-181280.Jul 5, 2001 · N945N · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011011Harness · defectiveNO NOSE LANDING GEAR SAFE (GREEN EXTENDED) OR OTHER LIGHT OR VISUAL INDICATION. REMOVED AND REPLACED UP LIMIT SWITCH WIRING HARNESS, CLEANED NOSE GEAR VIEWING COMPONENTS.Jul 2, 2001 · N301ME · Doug DC932 · Landing Gear Position and WarningSDR AT0100213Battery Pack · dischargedFOUND EMERGENCY LIGHTS OUT ON ROWS 23, 25, AND 28. REPLACED BATTERY PACK IAW DC9 MM 33.Jun 30, 2001 · N824AT · Doug DC932 · Emergency LightingSDR 0103189922Bulkhead · gougedDURING AN M-CHECK IN ATL, A GOUGE WAS FOUND IN THE STATION 604 BULKHEAD TEE AT LONGERON 27L. THE GOUGE WAS LOCATED IN THE AFT FACE OF THE WEB FLANGE AND WAS BLENDED OUT TO A MATERIAL THICKNESS OF 0.058 INCH.Jun 28, 2001 · N945N · Doug DC932 · Fuselage Main, BulkheadSDR MWEA011006Fitting · crackedFRAME ATTACH FITTING FORWARD SPAR CENTER TANK STATION XCW 40 LEFT IS CRACKED. -- LOCATED AND INSTALLED NEW FITTING.Jun 28, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011005Angle · crackedRIGHT WING TO FUSELAGE FITTING AT STATION 604 LONGERON 22 RIGHT IS CRACKED. -- REMOVED FITTING, LOCATED AND INSTALLED NEW FITTING.Jun 28, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR AT0100199Light · missingFOUND RED LENS AND BULB MISSING AT ROW 18. REPLACED RED LENS AND BULB AT ROW 18 IAW DC9 MM 33-21-27.Jun 26, 2001 · N845AT · Doug DC932 · Emergency LightingSDR MWEA011001Pressure Switch · failedON APPROACH TO MILWAUKEE, RIGHT ENGINE OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE WAS 42 PSI, OIL TEMP 110 DEGREES CELCIUS. SHUT OFF ENGINE, ENGINE WINDMILLED FOR TEN MINUTES WITH OIL PRESSURE AT 42-43 PSI. REMOVED AND REPLACED RIGHT ENGINE LOW OIL PRESSURE Jun 26, 2001 · N212ME · Doug DC932 · Engine Oil PressureSDR MWEA011000Fuel Control · faultyRIGHT ENGINE SURGE OF EPR & N1 1.80 TO 1.88, 4 PERCENT VARIABLE ON N1 AT ALL POWER SETTINGS. REMOVED AND REPLACED FUEL CONTROL UNIT ON RIGHT ENGINE.Jun 25, 2001 · N401ME · Doug DC932 · Fuel Control/Turbine EnginesSDR GTIA010565Gyro · defectiveFLT 304 - ACY - VERTICAL SPEED WHEEL DOES NOT AGREE WITH VERTICAL SPEED IN DESCENT AND CLIMB. AT 500 IN CLIMB ON VERT SPEED WHEEL, A/C CLIMBS 2000 FPM, 500 FPM DESCENDS AIRCRAFT AS MUCH AS 2500 FPM. REMOVED AND REPLACED NR 2 VG. OPS CHECK GOOD IAW DC-9 MM 3Jun 24, 2001 · N133NK · Doug DC932 · Attitude Gyro and Indicating SystemSDR ABXA010383Doubler · crackedAFT PRESSURE BULKHEAD CENTERLINE FINGER DOUBLER WAS CRACKED AND HAD A PIECE MISSING ON THE FORWARD SIDE OF BULKHEAD. REPAIRED AREA IAW REA D953-41525.Jun 24, 2001 · N928AX · Doug DC932 · Fuselage Main, BulkheadSDR GTIA010566Battery · dischargedFLT 8083 - ACY - FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE AT ROW 15 BOTH SIDES. REMOVED AND REPLACED TWO BATTERIES AT PACK B5-25. SYSTEM OPS CHECK GOOD PER DC-9 MM 33-53-00. (M)Jun 23, 2001 · N133NK · Doug DC932 · Emergency LightingSDR AT0100188Bulb · inoperativeFOUND AFT TAIL CONE OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. CORRECTIVE ACTION: RELAMPED LIGHTS. IAW DC9 MM 33-00Jun 22, 2001 · N828AT · Doug DC932 · Emergency LightingSDR ABXA010380Splice · damagedDURING C-CHECK, THE AFT PRESSURE BULKHEAD SPLICES WERE FOUND TO HAVE ELONGATED HOLES. REPAIRED AFT PRESSURE BULKHEAD TEE CAP SPLICES IAW REA D953-41487MR.Jun 20, 2001 · N928AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA010379Retainer · crackedCRACK AT LOWER AFT FASTENER OF WINDOW RETAINER, FS 658 AND LONGERON 15 RIGHT. REPAIRED AREA IAW DC-9 SSRM K07226.Jun 20, 2001 · N928AX · Doug DC932 · Passenger Compartment WindowsSDR ABXA010377Floorbeam · corrodedFLOORBEAM AT STA 965, LEFT BUTT LINE 45 WAS CORRODED ON AFT SIDE THROUGH LIGHTENING HOLE. REPAIRED FLOORBEAM IAW REA D953-41486MR.Jun 20, 2001 · N928AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA010378Floorbeam · corrodedFORWARD SIDE OF FLOORBEAM WEB EXFOLIATED AT FS 389, AT APPROXIMATELY LEFT BUTT LINE 48. REPAIRED FLOORBEAM AT FS 389, LEFT BUTT LINE 48 IAW REA D953-41479. MATERIAL REMOVED WAS APPROXIMATELY 1 - 2 INCHES.Jun 20, 2001 · N928AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA010375Frame · crackedFORWARD RIGHT MAINFRAME AT STA 699 WAS CRACKED IN THE FORWARD FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTION. INSTALLED REPAIR DOUBLER IAW DC-9 EA 53400120-1.Jun 19, 2001 · N928AX · Doug DC932 · Fuselage Main, FrameSDR ABXA010374Frame · corrodedUPPER AND LOWER SPLICE CHANNELS IN FRAME AT STA 937 WAS HEAVILY CORRODED AND BULGING ABOVE LONGERON 28 LEFT AND LONGERON 27 LEFT. REPLACED FRAME AT STA 937, LONGERON 28 TO LONGERON 25 LEFT IAW DC-9 SRM.Jun 19, 2001 · N928AX · Doug DC932 · Fuselage Main, FrameSDR ABXA010376Frame · crackedAFT LEFT MAINFRAME AT STA 737 WAS CRACKED IN THE AFT FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTION. REPAIRED MAINFRAME IAW DC-9 EA 53400310-001-1.Jun 19, 2001 · N928AX · Doug DC932 · Fuselage Main, FrameSDR ABXA010373Frame · corrodedUPPER CARGO FLOOR FRAME AT STA 965 WAS HEAVILY CORRODED FROM LONGERON 26 LEFT OUTBOARD TO LONGERON 22 LEFT. REPAIRED IAW REA D953-41486MR.Jun 19, 2001 · N928AX · Doug DC932 · Fuselage Main, FrameSDR MWEA010998Proximity Sensor · faultyLEFT MAIN RED UNSAFE LIGHT STAYED ON AFTER GEAR RETRACTED. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK PROX SENSOR.Jun 19, 2001 · N502ME · Doug DC932 · Landing Gear Position and WarningSDR ABXA010372Skin · damagedFUSELAGE SKIN CREASED AT STA 358 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR. CUTOUT WAS 2.1 INCH IN DIAMETER.Jun 18, 2001 · N928AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010371Skin · dentedFUSELAGE SKIN DENTED AT STA 353 BETWEEN LONGERON 21 AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR.Jun 18, 2001 · N928AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010370Skin · dentedREPAIR ON FUSELAGE SKIN DENTED AT STA 346, LONGERON 21 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR.Jun 18, 2001 · N928AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010369Floorbeam · corrodedFLOORBEAM LOWER FORWARD ANGLE CORRODED AT FS 965 LT, LBL 22-44. REPAIRED AREA IAW REA D953-41486MR.Jun 18, 2001 · N928AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA010368Retainer · crackedCRACK AT RADIUS OF FORWARD LOWER CORNER OF WINDOW RETAINER, FS 598 AND LONGERON 15 RIGHT. REPAIRED WINDOW RETAINER ON LOWER CORNER AT FS 598 AND LONGERON 15 RIGHT IAW DC-9 SRM DWG K07226.Jun 18, 2001 · N928AX · Doug DC932 · Passenger Compartment WindowsSDR ABXA010341Fire Warning · false activationLOWER CARGO FIRE LIGHT ILLUMINATED IN FLIGHT. ESTABLISHED EMERGENCY DESCENT TO SIOUX FALLS, SD. LIGHT WENT OUT WHILE DESCENDING. LANDED IN SIOUX FALLS WITH NO PROBLEMS. NO FIRE/SMOKE DETECTED BY SIOUX FALLS FIRE/RESCUE PERSONNEL. ABX ENGINEERING DOWNLOADEJun 18, 2001 · N983AX · Doug DC932 · Fire DetectionSDR MWEA010995Skin · damagedLEFT ELEVATOR UPGRADE REPAIR INSTALLED AT STATION XHS 70 TO SRM 55-03 FIGURE 14. -- REMOVED SKIN, FABRICATED NEW SKIN AND FINGER DOUBLER, INSTALLED SKIN.Jun 18, 2001 · N216ME · Doug DC932 · Elevator Control SystemSDR MWEA010994Skin · crackedFORWARD PAX DOOR SKIN HAS A SMALL CRACK AT THE LOWER SIDE OF THE HOLD OPEN HOOK CUT OUT. -- REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER.Jun 18, 2001 · N216ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA010993Frame · damagedEXTERIOR FUSELAGE HAS LIGHTENING STRIKES AT WINDOW 9L. -- BLENDED OUT DAMAGED AREAS, LOCATED AND DRILLED DOUBLER, INSTALLED REPAIR AT WINDOW.Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010992Seat Track · corroded#3 SEAT TRACK CORRODED AT FORWARD END APPROXIMATELY STATION 200. -- REMOVED CORROSION, REMOVED DAMAGED SECTION OF SEAT TRACK, LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK.Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010991Frame · gougedWINDOW 9L INNER WINDOW FRAME HAS SEVERAL MODERATE GOUGES/TOOL MARKS IN RADIUS OF FRAME BOTH FORWARD AND AFT SIDES. -- BLENDED TOOL MARKS, LOCATED AND DRILLED NEW INNER WINDOW FRAME, INSTALLED WINDOW RETAINER.Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010990Bracket · elongatedATTACH BRACKET HOLES ELONGATED FORWARD AND AFT, FORWARD CARGO DOOR HINGES ATTACH TO FUSELAGE. -- FABRICATED AND INSTALLED DOUBLERS.Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010989Skin · crackedEXTERIOR SKIN ABOVE FORWARD PAX DOOR HOLD OPEN HOOK CUT OUT HAS TWO SMALL CRACKS. -- TRIMMED, LOCATED AND DRILLED PLATE AND DOUBLERS, INTSTALLED DOUBLERS, PAN, PIN.Jun 18, 2001 · N216ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010988Tab · delaminatedRIGHT ELEVATOR GEARED TAB HAS TWO AREAS OF DELAMINATION ON PREVIOUS REPAIR. 1.5" BY 6.0" AREA ON TOP AND 4.0" BY 2.5" AREA ON BOTTOM. -- REMOVED DELAMINATED REPAIR, BONDED ON NEW REPAIR.Jun 18, 2001 · N216ME · Doug DC932 · Elevator Control SystemSDR GTIA010528ComputerDTW - FLT 9951 - AUTO PILOT VERTICAL SPPED WHEN COMMANDED UP OR DOWN THERE IS NO CONTROL UP TO 1500 FT PER MIN GOES DIRECTLY TO 1500 FT PER MINUTE. REMOVED AND REPLACED PITCH AXIS COMPUTER, OPS CHECKED GOOD PER DC9 MM 22-13-01. NO OTHER DISCREPANCIES NOTED. Jun 17, 2001 · N133NK · Doug DC932 · Auto Flight SystemSDR GTIA010527Charger · inoperativeFOUND WITH NO POWER ON A/C EMERGENCY LIGHTS (OVERHEAD) BETWEEN SEATS 17 AND 21 COME ON. REMOVED AND REPLACED BATTERY CHARGER FOR EMERGENCY OVERHEAD LIGHTS, SYSTEM OPS CHECK NORMAL IAW DC9 MM 33-50-00. NO OTHER DEFECTS NOTED. (M)Jun 15, 2001 · N133NK · Doug DC932 · Emergency LightingSDR AT0100182Light · inoperativeFOUND 2 RED EMERGENCY FLOOR TRACK LIGHTS AT FORWARD GALLEY INOPERATIVE. RELAMPED BULBS IAW DC9 MM 33-50.Jun 15, 2001 · N845AT · Doug DC932 · Emergency LightingSDR MWEA010985Skin · gougedGOUGE AT STATION 813 BETWEEN LONGERONS 25 AND 26 RIGHT. -- BLENDED GOUGE, CUT OUT SKIN, REMOVED LOWER FLANGE OF SHEAR TIES, FABRICATED REPAIR, INSTALLED REPAIR DOUBLER AND SKIN REPAIR, FABRICATED SHEAR TIE REPAIR ANGLES, INSTALLED SHEAR TIES.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010984Floorboard · damagedREMOVED CABIN FLOORBOARD B10 TO FACILITATE OTHER MAINTENANCE. -- FABRICATED NEW SKIN AND HAT SECTIONS, INSTALLED INSULATION AND SHIM MATERIAL.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010983Frame · damagedUPPER FUSELAGE FRAME STATION 737 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERONS 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED, LOCATED AND DRILLED REPAIR ANGLES, INSTALLED REPAIR.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010979Intercostal · damagedFORWARD ENTRY INTERCOSTAL HAS FIVE OPEN FASTENER HOLES AND INNER LEG HAS MATERIAL TRIMMED OUT STATION 228 ABOVE LONGERON 11 LEFT. -- FABRICATED AND INSTALLED REPAIR ANGLES.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010978Frame · damagedUPPER FUSELAGE FRAME STATION 889 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- FABRICATED, LOCATED AND DRILLED REPAIR ANGLE AND FILLER, INSTALLED REPAIR ANGLE DOUBLER.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010977Frame · damagedUPPER FUSELAGE FRAME 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 RIGHT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010976Frame · damagedUPPER FUSELAGE STATION 870 HAS TWO HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES, FABRICATED A REPAIR ANGLE, INSTALLED REPAIR ANGLE.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010975Frame · damagedUPPER FUSELAGE FRAME 813 HAS THREE HOLES THAT DO NOT HAVE (2D) SPACING BETWEEN LONGERON 5 AND 6 LEFT. -- PLUGGED HOLES IN FRAME, FABRICATED REPAIR PARTS, INSTALLED REPAIR.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010974Frame · misdrilledFRAME STATION 503 IN BETWEEN LONGERON 5 AND 6 RIGHT SIDE HAS ONE MISDRILLED HOLE AND THREE OPEN DRILLED HOLES, CHECK EDGE DISTANCE. -- FABRICATED, LOCATED AND DRILLED NEW ANGLE, INSTALLED REPAIR.Jun 15, 2001 · N301ME · Doug DC932 · Fuselage Main, Structure
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