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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA9700257Splice · crackedDURING C-CHECK, THE WING LEADING EDGE SKIN SPLICE WAS FOUND CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK, NR AF-796. THE CRACK WAS REPAIRED IAW DC-9 SRM.SDR ABXA9701012Beam · crackedFOUNR FWD SERVICE DOOR LOWER BEAM CRACKED AND SECOND BEAM FROM BOTTOM CRACKED. REPAIRED LOWER BEAM (P/N 9911582-3) AND SECOND BEAM (P/N 9911581-3) IAW DC9 SRM 52-05.SDR ABXA9600637Engine · bird strikeBIRD STRIKE LEFT ENGINE. REMOVED THE DAMAGED AREA TO THE LEFT ENGINE NR 1 BLADE, BORESCOPED THE LEFT ENGINE AND GROUND RAN TO TAKEOFF EPR, OPS CHECKED GOOD.SDR EIAA9633Wire · brokenSEA - WHEN LANDING GEAR RETRACTED DEPARTING SEA, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURE IAW OPS MANUAL WITH NO CHANGE OF INDICATION. LANDING GEAR EXTENDED NORMALLY WITH 3 GREEN AND UNSAFE LIGHTS OUT AT SEAT. ACCOMPLISHESDR ABXA9700467Floorbeam · damagedDURING C-CHECK, THE AFT FLANGE OF THE FLOORBEAM AT STA 917 WAS FOUND TO BE GOUGED AND WORN. REPAIRED IAW REA D953-16470-MR.SDR ABXA9700468Skin · damagedDURING C-CHECK, AN EXISTING CLASS TWO REPAIR WAS REMOVED FROM THE FUSELAGE SKIN AT STA 975 LONG 20 AND 21 RIGHT. REPAIRED IAW REA D953-16442-MR.SDR ABXA9700229Intercostal · crackedDURING C-CHECK, AN INTERCOSTAL WAS FOUND CRACKED BETWEEN STATION 897 TO 889 LONGERONS 30 AND 29 RIGHT. REPLACED IAW DC-9 SRM 53-30-2.SDR ABXA9700462Tab · delaminatedDURING C-CHECK, AN ELEVATOR CONTROL TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-30-3.SDR ABXA9700466Engine Mount · corrodedDURING C-CHECK, THE RIGHT HAND FORWARD ENGINE MOUNTS, BEAVERTAIL, WERE FOUND TO BE CORRODED. REPAIRED IAW REA D953-16454-MR.SDR ABXA9700465Frame · corrodedDURING C-CHECK, CORROSION WAS FOUND ON FUSELAGE FRAME 351 UPPER CAP AT LONGERON 24 LEFT. REPAIRED IAW REA D953-16412-MR.SDR ABXA9700464Fitting · corrodedDURING C-CHECK, AN END FITTING WAS FOUND TO BE ELONGATED AND CORRODED. REPAIRED IAW REA D953-16455-MR.SDR ABXA9700463Tab · delaminatedDURING C-CHECK, AN AILERON TRIM TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-10-5.SDR ABXA9700890Tab · delaminatedTHE LEFT ELEVATOR TAB WAS DELAMINATED ON THE INBOARD TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700886Tab · dentedTHE RUDDER TAB HAD 2 LARGE DENTS TO THE OUTER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9600621Oil Clog Light · illuminatedDURING FLIGHT, RIGHT OIL STRAINER CLOGGING ANNUNCIATOR CAUTION LIGHT ILLUMINATED. RIGHT THROTTLE WAS REDUCED TO IDLE, LIGHT REMAINED ILLUMINATED, PRECAUTIONARY SHUT-DOWN OF RIGHT ENGINE WAS ACCOMPLISHED. REPLACED THE RIGHT ENGINE OIL SCREEN, MEGGED THE WIRESSDR EIAA9627Throttle Linkage · looseDEN - LEFT ENGINE THROTTLE WOULD NOT RESPOND TO POWER REDUCTION ON DESCENT, PERFORMED ENGINE SECURING CHECKLIST. FOUND LEFT ENGINE FCU THROTTLE LINKAGE ATTACH BOLT BACKED OUT. INSPECTED BOLT, NUT AND LINKAGE ATTACH POINT. NO DEFECTS NOTED. REATTACHED LINKASDR ABXA9600608Power Supply · defectiveEMERGENCY LIGHTS WILL NOT SHUT OFF. REPLACED BATTERY POWER SUPPLY IAW DC-9 MM 33-50-0, OPS CHECK GOOD.SDR EIAA9623Connector · recessed pinSAN - NOSE GEAR WILL NOT SHOW DOWN AND LOCKED INDICATION (GREEN LIGHT) WITH VISUAL INDICATION SHOWING DOWN AND LOCKED. AT THE TOP OF DESCENT, WHEN POWER WAS IDLE, RED NOSE GEAR LIGHT WOULD NOT ILLUMINATE. RED GEAR LIGHT FOR NOSE GEAR DID CYCLE ON GEAR EXTENSISDR EIAA9621Flap Trans · failedDEN - AUTO PILOT PORPOISES VIOLENTLY IN PITCH WHILE COUPLED ON ILS, BEGINNING AT 500 FEET RADAR ALTITUDE. REPLACED RIGHT FLAP POSITION TRANSMITTER AND GAUGE IAW THE DC9 MM. OPERATIONS CHECK GOOD. (M)SDR 96ZZZM1230Indicator · failedDEN - AUTO PILOT PORPOISES VIOLENTLY IN PITCH WHILE COUPLED ON ILS, BEGINNING AT 500 FEET RADAR ALTITUDE. REPLACED RIGHT FLAP POSITION TRANSMITTER AND GAUGE IAW THE DC9 MM. OPERATIONS CHECK GOOD. REFERENCE EIAA9621.SDR ABXA9600520Batteries · dischargedCOCKPIT EMERGENCY LIGHTS ARE DIM. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES.SDR EIAA9620Rod End Nut · looseSEA - DURING DESCENT THROUGH 16,000 FEET, ELEVATOR CONTROL JAMMED UNTIL 15 LBS FORWARD FORCE APPLIED, THEN ABRUPTLY FREED. INSPECTED ELEVATOR SYSTEM IAW MM. NO FAULTS FOUND. UNABLE TO DUPLICATE. CLOSED ALL PANELS ASSOCIATED WITH INSPECTION. ALL CHECKS GOOSDR AU960923Angle · corroded(AUS) LEVEL 2 EXFOLIATION CORROSION AT BOTTOM OF `T' ANGLE (ATTACHMENT ANGLE) OF FUSELAGE TO CANTED PRESSURE PANEL IN RH WHEEL WELLSDR AU960922Floorbeam · corroded(AUS) LEVEL 2 CORROSION ON LOWER `T' OF FLOORBEAM AT FUSELAGE STN 937.SDR EIAA9618Battery Pack · dischargedOAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. (M)SDR 96ZZZX3743Light Panel · inoperativeOAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. REFERENCE OPERATOR CONTROL NR: EIAA9618.SDR 96ZZZM1231Light · inoperativeOAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. REFERENCE EIAA9618.SDR ABXA9600506Light Socket · defectiveON GEAR UPLATCH CHECK, RIGHT LANDING GEAR GREEN LIGHT CAME ON BRIGHT. GEAR RECYCLING WAS NORMAL EXCEPT LIGHT STAYED ON BRIGHT ALL THROUGH RECYCLING. REPLACED THE RIGHT MAIN LANDING GEAR DOWN LIGHT SOCKET.SDR ABXA9600586Bushing · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE HALF IAW DC-9 OVERHAUL MANUAL 32-10-16.SDR ABXA9600585Hinge · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE WORN. REPLACED HINGE IAW DC-9 SRM 51-30-2.SDR ABXA9600584Hinge · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600505Hyd Line · brokenRIGHT HYDRAULIC SYSTEM FLUID LOSS FAILURE ON CLIMBOUT. CREW PERFORMED ABNORMALS AND CAME TO A FULL STOP ON RUNWAY. MAINTENANCE SECURED THE GEAR AND STOWED MLG DOORS PRIOR TO TAXI. FOUND ALTERNATE PUMP HYDRAULIC LINE BROKEN IN THE RIGHT WHEEL WELL, REPLACED SDR ABXA9700615Flap Vane · gougedTHE LEFT OUTBOARD FLAP VANE HAS TWO GOUGES THROUGH THE SKIN ON THE INBOARD LEADING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700622Spoiler · crackedTHE LEFT OUTBOARD SPOILER WAS CRACKED AT THE CENTER HINGE CUP. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9600557Linkage · wornDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600544Linkage · wornDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PART IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600543Linkage · wornDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-220-7, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600542Linkage · wornDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600541Linkage · wornDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9600494Dnlock Switch · defectiveDURING APPROACH WHEN LANDING GEAR HANDLE WAS PLACED DOWN, NO GREEN NOSE GEAR DOWN LIGHT ILLUMINATED. RECYCLED GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. REPLACED NOSE GEAR DOWNLOCK AND UPLIMIT SWITCHES PER DC-9 M.M.SDR ABXA9600560Floor Panel · puncturedDURING C-CHECK INSPECTION, FOUND COCKPIT FLOOR PANEL PUNCTURED AFT OF THE PILOT'S CONTROL COLUMN. REPAIRED IAW DC-9 SRM 53-21-0, FIGURE 2B.SDR ABXA9600558Hinge · wornDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR HINGE WORN. REPLACED HINGE IAW DC-9 SRM 51-30-2.SDR ABXA9600491Uplatch · lack of lubeGEAR DOOR OPEN LIGHT STAYED ON AFTER LOWERING GEAR. WE RECYCLED GEAR AND LIGHT WENT OUT AFTER THE GEAR HAD BEEN DOWN FOR APPROXIMATELY 30 SECONDS. CLEANED AND LUBED MAIN LANDING GEAR DOOR UPLATCH HOOKS AND ROLLERS. OPERATIONAL CHECKED THE GEAR DOOR UNSAFE SSDR ABXA9600559Bulkhead Tee Cap · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD T-CAP CRACKED AT APPROXIMATELY LONGERON 27L. REPLACED T-CAP IAW DC-9 SRM 53-03, FIGURE 37A.SDR ABXA9600551Bulkhead Tee · trimmedDURING C-CHECK INSPECTION AND AFT PRESSURE BULKHEAD T-CAP CHANGE, LONGERON 25 LEFT TEE WAS TRIMMED FOR ACCESS. REPAIRED IAW ABX REA D953-15276-MR.SDR ABXA9600556Pan · crackedDURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, LBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.SDR ABXA9600555Subfloor · damagedDURING C-CHECK INSPECTION, FOUND SUBFLOOR DAMAGED AT STA 160 TO 200. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2, SHEET 3.SDR ABXA9600535Pan · crackedDURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 44. FABRICATED PAN IAW DOUGLAS DRAWING NR 9922405 AND INSTALLED IAW DC-9 SRM 51-30-2.SDR ABXA9600533Pan · crackedDURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.SDR ABXA9600532Pan · crackedDURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, BL 0. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.
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