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 ABXA020367Duct · looseDURING FINAL APPROACH, ODOR OF SYNTHETIC OIL IN THE COCKPIT. LT TEMP CONTROLLER IN MANUAL WITH LT DUCT TEMP PEAKED. TURNED IT OFF. ODOR WENT AWAY. ON THE GROUND, TURNED LT SUPPLY SWITCH BACK ON, WAS ABLE TO CONTROL TEMP MANUALLY. OPS CHECKED LT MANUAL TEMP CONDec 19, 2002 · N900AX · Doug DC932 · Air Distribution SystemSDR ABXA020368Sensor · out of toleranceCOCKPIT TEMP VALVE IN AUTO WENT TO 80 PERCENT FULL HOT. LT DUCT TEMP PEGGED OUT HOT. SLIGHT SMOKE IN COCKPIT. MANUALLY DROVE VALVE FULL COLD. AC SMOKE CHECKLIST RUN. LT BLEED VALVE OFF FOR REST OF FLT. FOUND AUTO TEMP CONTROL TO COCKPIT TEMP SENSOR OUT OF TOLDec 17, 2002 · N900AX · Doug DC932 · Cabin Temperature Control SystemSDR MWEA020741Bearing · not seatedWHEN GEAR RETRACTED ALL LIGHTS OUT, EXCEPT THE LEFT GEAR UNSAFE LIGHT. MAINTENANCE RESEATED LEFT UPLATCH HOOK CENTER BEARINGS.Dec 17, 2002 · N216ME · Doug DC932 · Landing Gear Retraction/Extension SystemSDR 0204129986Controller · failedDURING CLIMB, FLIGHT ATTENDANT REPORTED CABIN RAPIDLY BECAME HOT AND SMELLED HOT. F/O REPORTED RIGHT PACK TEMP HIGH. PACK TEMP REDUCE IN MANUAL OPERATION. FLIGHT RETURNED TO AND LANDED WITHOUT INCIDENT. REPLACED CABIN TEMP CONTROLLER AND RIGHT COALESCER BAGDec 14, 2002 · N986US · Doug DC932 · Cabin Temperature ControllerSDR MWEA020732Fire Detector · faultyCARGO FIRE DETECTOR LOOP LIGHT CAME ON. REMOVED AND REPLACED THE METERING VALVE, BOTTLE ASSEMBLY, SQUIB DIVERTER AND SQUIB.Dec 14, 2002 · N204ME · Doug DC932 · Fire DetectionSDR ABXA020355Control Cable · contaminatedTHROTTLES EXTREMELY DIFFICULT TO MOVE DURING FLIGHT. EXPECTED ICE CONTAMINATION. CLEANED AND LUBRICATED CABLES AND FAIRLEADS ABOVE FORWARD BAG BIN. ICE REMNENTS NOTED ON GILL LINER ABOVE BAG BIN. THROTTLE MOVEMENT NORMAL. REMOVED ICE. MOPPED CARGO COMPARTMEDec 11, 2002 · N980AX · Doug DC932 · Power LeverSDR MWEA020727Starter · inoperativeLEFT ENGINE STARTER INOPERATIVE -- REMOVED AND REPLACED ENGINE STARTER.Dec 6, 2002 · N209ME · Doug DC932 · Engine CrankingSDR ABXA020350Pump · failedEMERGENCY DECLARED & DIVERTED. A/C CROSSTIE LOCKOUT, LT AC BUS OFF LDC BUS OFF LT GEN. APU WOULD NOT PICK UP RT SIDE. INSP LT GEN LEADS, CHECKED RESISTANCE ON LT DP CURRENT TRANS (ALL THREE). CHKD 3 CURRENT TRANS FOR LT MAIN SYS. VISUALLY INSP 3 PHASE BUS WIRDec 5, 2002 · N984AX · Doug DC932 · Electrical Power SystemSDR ABXA020361Frame · crackedFRAME AT STA. 180, LONGERON 4 LEFT, CRACKED FROM INBOARD LONGERON FASTENER. REPAIRED IAW DC-9 SSRM AND DRAWING K05159.Dec 3, 2002 · N981AX · Doug DC932 · Fuselage Structure (General)SDR ABXA020360Longeron · crackedLONGERON 30 CRACKED AT STA. 408 - 427. REPAIRED CRACKED LONGERON 30 IAW DC-9 SRM 53-02.Dec 3, 2002 · N981AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA020345Downlock Switch · failedNOSE LANDING GEAR SAFE LIGHT TOOK SEVERAL MINUTES TO ILLUMINATE AFTER SELECTING GEAR DOWN. RESULTING IN A MISSED APPROACH. THE GEAR SAFE LIGHT THEN ILLUMINATED. REPLACED THE NOSE LANDING GEAR DOWN LOCK SWITCH IAW MM. OPS CHECKED GOOD.Dec 3, 2002 · N928AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA020359Panel · crackedAFT LOWER CARGO DOOR OUTER PANEL CRACKED AND HAD IMPROPER EDGE DISTANCE AT THE NR 2 BEAM FORWARD SIDE. (HOLD OPEN LATCH AREA) REPLACED AFT LOWER CARGO DOOR ASSEMBLY IAW SRM.Dec 2, 2002 · N981AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA020358Intercostal · crackedFORWARD LOWER CARGO DOOR LOWER AFT STOP FITTING INTERCOSTAL CRACKED IN TWO PLACES. REPLACED FORWARD LOWER CARGO DOOR IAW SRM.Dec 2, 2002 · N981AX · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020721Retainer · corrodedRIGHT AFT OVERWING EXIT DOOR HAS CORROSION AT LOWER FORWARD CORNER OF SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER.Nov 27, 2002 · N502ME · Doug DC932 · Emergency ExitsSDR MWEA020720Retainer · corrodedRIGHT FORWARD OVERWING EXIT DOOR HAS CORROSION AT LOWER CORNER OF SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER.Nov 27, 2002 · N502ME · Doug DC932 · Emergency ExitsSDR ABXA020344Contactor · damagedON DESCENT, NOSE GEAR UNSAFE LIGHT WAS INTERMITTENT WITH THROTTLES AT IDLE. CREW REPORTED CYCLED GEAR, CHECKED GOOD. FOUND NOSE GEAR LIGHT BULB POSITIVE CONTACT FLATTENED AND MUSHROOMED CAUSING INTERMITTENT INDICATION. REPAIRED CONTACT. OPS CHECKED GOOD IAW AMNov 26, 2002 · N928AX · Doug DC932 · Landing Gear Position and WarningSDR MWEA020722Skin · damagedSKIN AT STATION 1121 LONGERON LEFT 18 HAS A APPROXIMATE 1.5" HOLE. -- REMOVED AND REPLACED SKIN.Nov 26, 2002 · N301ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MEX2002349Bungee Cylinder · defectiveMEX-CUU - AIRCRAFT RETURNED AFTER TAKEOFF, DUE TO PROBLEMS WITH NOSE GEAR. THE NOSE LANDING GEAR REMAINED EXTENDED PROCEDURE WAS ACCOMPLISHED AND PHYSICALLY CHECKED, NOSE GEAR REMAINED DOWN AGAIN. IN APPROXIMATION, CAPTAIN INFORMED THE NOSE GEAR RETRACTED UPNov 25, 2002 · N1003P · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA020310Jackscrew · corrodedDURING HORIZONTAL STABILIZER JACKSCREW INSPECTION PER AD 2000-15-15, DC-9 SB DC-9-27A362, FOUND BRONZE METAL SHAVINGS INSIDE THE LUBRICATION GREASE AND THE JACKSCREW THREADS WERE PITTED AND CORRODED. REPLACED JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01-4-0001.Nov 25, 2002 · N985AX · Doug DC932 · Stabilizer Control SystemSDR ABXA020343Battery · dischargedCOCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND LIGHT BULBS. OPS CHECKED GOOD IAW AMM.Nov 23, 2002 · N989AX · Doug DC932 · Emergency LightingSDR MWEA020719Switch · defectiveAFTER LEFT ENGINE START LEFT AIRFOIL ICE PROTECTION TEMPERATURE LIGHT CAME ON. -- REMOVED AND REPLACED ELECTRONIC THERMAL SWITCH CONTROL.Nov 22, 2002 · N501ME · Doug DC932 · Airfoil Anti/De-ice SystemSDR MWEA020717Frame · damagedFUSELAGE FRAME STATION 897 HAS 1 EACH OVERSIZED HOLE IN THE INBOARD CAP LOCATED BETWEEN LONGERON 28 RIGHT AND LONGERON 29 RIGHT HOLE MEASURES .403 INCH DIAMETER. FABRICATED AND INSTALLED BUSHING.Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020716Frame · damagedTHE INBOARD CAP OF FUSELAGE FRAME STATION 937 HAS ADDITIONAL HOLES LOCATED BETWEEN LONGERON 26 RIGHT AND LONGERON 26 RIGHT, WHICH MEASURES .098 INCH IN DIAMETER. PLUGGED ADDITIONAL HOLES WITH AD MATERIAL MWX-ORD-02-00349 H.Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020715Angle · dentedAFT BAGGAGE PIT FRAME HAS A DENT IN IT BETWEEN THE DOOR JAMB AND THE DOOR BEAM. -- FABRICATED AND INSTALLED REPAIR ANGLE.Nov 20, 2002 · N202ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020714Track · corrodedAFT PIT, AFT LEFT CARGO TIE-DOWN TRACK IS CORRODED OUT OF LIMITS. -- FABRICATED AND INSTALLED REPLACEMENT TRACK.Nov 20, 2002 · N202ME · DC932 · Fuselage Main, StructureSDR MWEA020713Splice · corrodedFORWARD CARGO BAY AFT SIDE AND BOTTOM SIDE OF FRAME HEAVILY CORRODED STATION 503 LONGERON 28 RIGHT TO 28 LEFT. -- CUT AND REMOVED CORRODED SECTION OF FRAME AND INSTALLED Z FRAME REPAIR SPLICE.Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020712Pan · corrodedAFT PIT DOOR JAMB PAN HAS AREAS OF CORROSION. -- REMOVED AND REPLACED PAN AND SPLICE PLATE.Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020708Door Frame · damagedAFT CARGO DOOR LOWER JAMB HAS NR 40 SIZE HOLES AROUND MULTIPLE BLIND NUTS FASTENER HOLES. REMOVED AND INSTALLED NEW JAMB.Nov 19, 2002 · N202ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020698Web · corrodedAFT DOOR JAMB PAM WEB HAS AREAS OF CORROSION. -- REMOVED AND INSTALLED NEW WEB.Nov 18, 2002 · N202ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020699Csd · malfunctionedCREW NOTICED RIGHT CSD LOW OIL PRESSURE LIGHT CAME ON. REMOVED AND REPLACED RIGHT CONSTANT SPEED DRIVE UNIT.Nov 15, 2002 · N212ME · Doug DC932 · Alternator-Generator DriveSDR MWEA020693Doubler · crackedFORWARD CARGO BAY SUBFLOOR CRACKED NEXT TO CARGO DOOR FORWARD HINGE ATTACH POINT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020692Intercostal · corrodedINTERCOSTAL IN FORWARD BAG PIT HAS CORROSION ON FLANGE AT STATION 484-503 LONGERON 27-28 LEFT. -- FORMED AND INSTALLED NEW INTERCOSTAL.Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020691Longeron · corrodedFORWARD CARGO BAY CORRODED AROUND FASTENERS IN LONGERON 30 STATION 520-524. -- REMOVED AND REPLACED LONGERON SECTION AND INSTALLED FORWARD AND AFT LONGERON SPLICE.Nov 14, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR 0203949940Door Frame · crackedDURING AN OVERNIGHT CHECK, A CRACK WAS FOUND IN THE AFT PRESSURE BULKHEAD DOORJAMB. THE AIRCRAFT WAS FERRIED TO ACCOMPLISH REPAIRS. THE CRACK WAS 2 INCHES LONG AT STATION X=59.8. REPAIRED IAW EA.Nov 13, 2002 · N3322L · Doug DC932 · Fuselage Main, StructureSDR 0203739921Switch · out of rigAT APPROXIMENTLY 118 KNOTS THE FLAP/RUDDER STOP LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE LIGHT EXTINGUISHED. ALLOWED BRAKES TO COOL AND RETURNED AIRCRAFT TO GATE AT YYZ. MAINTENANCE REPLACED THE FLAP/RUDDER POSITION SWITCH AND RE-RIGGED THE AUXILIARY Nov 6, 2002 · N943N · Doug DC932 · Rudder Control SystemSDR MWEA020669Longeron · tool damageSTATION 598 T ANGLE AT LONGERON 17 LEFT HAS TWO DRILL STARTS JX6. -- REMOVED T ANGLE, BLENDED OUT TOOLING DAMAGE, FABRICATED AND INSTALLED NEW T ANGLE.Nov 6, 2002 · N202ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR 0203719986Door · crackedDuring Hck in DHN, a .6" crack was found in the fwd galley service door pan at the #2 door stop. The crack extended from the upper corner of the upper hinge cutout. Repaired per EA 99-191372.Nov 1, 2002 · N986US · Doug DC932 · Service DoorsSDR AT0200087AcmTAKE OFF FRO 28L-CLIMBING THROUGH 3,000' LEAD FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY, RETURNED TO PIT, COMPLETED EMERGENCY CHECK LIST. CORRECTIVE ACTION: INSPECTED, BOTH A/C PACKS DURING FULL POWER TAKE OFF RUNNov 1, 2002 · N837AT · Doug DC932 · Cabin Cooling SystemSDR ABXA020304Structure · wornTRAILING EDGE, WING STA. 161, UPPER SURFACE HAD EXCESSIVE WEAR. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 30, 2002 · N984AX · Doug DC932 · Wing Main, Frame StructureSDR MWEA020667Slat · chafedLEFT SLAT #4 DRIVE ARM ATTACH BOLT CHAFING INBOARD RIB. -- REMOVED SLAT TRACK DOOR, BLENDED OUT DAMAGE AREA AND INSTALLED SLAT DRIVE DOOR.Oct 30, 2002 · N602ME · Doug DC932 · Leading Edge DevicesSDR ABXA020274Coalescer Bag · contaminatedVERY STRONG ODOR (MUSTY) WAS PRESENT FROM TAKE-OFF THROUGH FIRST 20 TO 30 MINUTES OF FLIGHT. CLOSING A/C VENTS WOULD DECREASE THE INTENSITY OF THE ODOR BUT WOULDN'T ELIMINATE IT. REPLACED BOTH WATER SEPARATOR COALESER BAGS IAW DC-9 MM 21-20-02-2-0001.Oct 30, 2002 · N901AX · Doug DC932 · Humidity Control SystemSDR 0203729984Slat · crackedDuring Shop Visit in ATL, a crack and elongated hole were found on the lower skin of the subject slat at the aft otbd corner. Repaired per EA 99-190789.Oct 25, 2002 · N984US · Doug DC932 · Wing, Attach FittingsSDR MWEA020643Control Cable · out of adjustCREW UNABLE TO RAISE LANDING GEAR. FOUND CABLE TENSION LOW AND ADJUSTED CABLE AND CONFIRMED PROPER RIG.Oct 25, 2002 · N502ME · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA020303Window Frame · crackedHFEC CRACK INDICATION AT WINDOW 21 RIGHT, 1/8 INCH FROM UPPER AFT EDGE, 3/16 INCH LONG. REPAIRED AREA IAW REA D953-45696-MR.Oct 22, 2002 · N984AX · Doug DC932 · Fuselage Main, StructureSDR ABXA020302Window Frame · crackedHFEC CRACK INDICATION AT WINDOW CUTOUT 14 RIGHT, 1/2 INCHES FROM UPPER FORWARD CORNER EDGE 1/4" LONG. REPAIRED AREA IAW REA D953-45678-MR.Oct 22, 2002 · N984AX · Doug DC932 · Fuselage Structure (General)SDR 0203539602O-Ring · wornAT 200 FEET DURING APPROACH FOR LANDING, THE RIGHT HYDRAULIC SYSTEM PRESSURE WAS AT 500 PSI WITH THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. RIGHT HYDRAULIC QUANTITY WAS INDICATING ZERO. LANDING WAS UNEVENTFUL AT MSP. MAINTENANCE FOUND AND REPLACED Oct 22, 2002 · N602NW · Doug DC932 · Hydraulic System, MainSDR ABXA020256Flange · crackedRIGHT FLAP INBOARD FIXED VANE GOUGED ON UPPER SURFACE DUE TO CRACKED ATTACH ANGLE. REPLACED FIXED VANE AND CRACKED VANE ATTACH ANGLE IAW DC-9 SRM 51-30-05 AND DC-9 MM 27-51-03-2-0002.Oct 21, 2002 · N980AX · Doug DC932 · Flight Control SystemSDR ABXA020301Floorbeam · corrodedFLOORBEAM WAS SEVERLY EXFOLIATED AT LEFT PYLON BULKHEAD, BUTT LINE 40 LEFT. INSTALLED 'J' CHANNEL AND AIR GRILL AT STA. 870 - 965. INSTALLED SEAT TRACK, STA. 908 - 965, BUTT LINE 44, IAW DC-9 SRM 51-30-1.Oct 20, 2002 · N984AX · Doug DC932 · Fuselage Main, Floor BeamSDR AT0200085Engine#2 ENGINE LOST POWER ON CLIMB OUT-ROLLED BACK TO 70% N1 WITH SIGNIFICANT VIBRATION. ALL OTHER PARAMETERS WITHIN LIMITS WITH POWER AT IDLE VIBE CEASED. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE IAW P.P. TASK CARDS 99-LEAK AND OPOct 20, 2002 · N830AT · Doug DC932 · Engine Ignition Analyzer SystemSDR ABXA020300Doubler · crackedRIGHT MAIN FRAME IN WHEEL WELL WAS CRACKED, INBOARD FLANGE. REPAIRED FRAME IAW REA D953-45633-MR AND S.B. 53-100.Oct 18, 2002 · N984AX · Doug DC932 · Fuselage Structure (General)
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