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.
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
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 95ZZZW786Limit Switch · failedFLT 558 - ATL-BNA - RETURNED TO ATL DUE TO A LEFT MAIN GEAR GREEN LIGHT ON. DURING APPROACH TO ATL NO NOSE DOWN LOCK INDICATION. REMOVED AND REPLACED LEFT GEAR DOWN LIMIT SWITCH AND LIGHT BULBS FOR NOSE GEAR DOWN LOCK LIGHT. (W)SDR 9507809924Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 160 - 200, LONGERON 22L. REPAIRED PER EA 99-097481. MFG PART NUMBER: 5911401-3.SDR ABXA9500450Skin · crackedDURING C-CHECK INSPECTION, FOUND SCREWS IN BARREL NUTS NOT SEATED PROPERLY AROUND REPAIR AT FORWARD UPPER CORNER OF ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-11476-MR.SDR 9507259604Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FRAME "T" FITTING FS 935 AT FLOOR LEVEL, LEFT SIDE. REPLACED FITTING PER SRM 51-42.SDR 9507249604Intercostal · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN INTERCOSTAL FITTING FS 579 BETWEEN LONGERONS 27L - 28L. REPLACED FITTING PER SRM 51-00.SDR 9507239604Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FRAME "T" FITTING FS 975, LONGERON 18R. REPLACED FITTING PER SRM 51-30-5.SDR MWEA95193Rib · crackedDURING ROUTINE MAINTENANCE, 2 CRACKS WERE FOUND ON LT WING LEADING EDGE RIB STA.XIS 137.0. ONE CRACK AT AFT UPPER END 3 FEET IN LENGTH, THE OTHER CRACK AT FWD UPPER END 1.50 INCHES IN LENGTH. BOTH CRACKS TEMPORARILY REPAIRED PER DOUGLAS TELEX 5-57-20-6 AND WSDR MWEA95192Spar · corrodedDURING ROUTINE MAINTENANCE, THE LEFT WING FWD UPPER SPAR CAP INBD OF SLAT DRIVE MECHANISM AT STA XIS 136.42 WAS FOUND TO BE CORRODED.SDR MWEA95191Rib · crackedDURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA XIS 129.710 WAS FOUND CRACKED AT LOWER LEG 2.75 INCHES IN LENGTH.SDR MWEA95190Rib · crackedDURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA.XIS 134.921 WAS FOUND CRACKED AT LOWER AFT END 1.3750 INCHES IN LENGTH.SDR ABXA9500449Frame · crackedDURING C-CHECK INSPECTION, FOUND FRAME 1079 CRACKED AT LONGERON 19L. REPAIRED IAW ABX REA D953-11507-MR.`SDR 9507829924Angle · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1095. REPAIRED PER EA 99-097075. MFG PART NUMBER: 5912141-59.SDR 9507209604Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE MAIN CABIN DOOR HINGE SUPPORT FITTING. REPLACED FITTING PER SRM 52-11-0 AND MM 20-50-01.SDR 9507179984Air Dist · smokeFLIGHT ATTENDANT REPORTED SMOKE IN FORWARD PORTION OF CABIN AFTER TAKEOFF. SHUT OFF GALLEY POWER, BUT SMOKE DID NOT DISSIPATE. FLIGHT RETURNED TO CID AND LANDED WITHOUT INCIDENT. CHECKED GALLEY WITH POWER ON AND CHECKED WIRING AND CANNON PLUGS TO OVENS. NOSDR MWEA95187Door · not securedPILOT REPORTS, AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO GATE. MAINTENANCE FOUND E AND E COMPARTMENT DOOR NOT PROPERLY SECURED. SECURED DOOR, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR 95ZZZM114Fuel · siphoningFLT NR 513 - ATL-MCO - AFTER AIRCRAFT WAS ON CLIMB-OUT FROM ATL, ANOTHER AIR CARRIER REPORTED FUEL COMING FROM THE RIGHT WING TIP. AIRCRAFT IMMEDIATELY RETURNED FOR LANDING. TRANSFERRED FUEL FROM LEFT TANK TO RIGHT TANK WHICH STOPPED SIPHONING OF FUEL. TRIESDR 9507819924Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FUSEALGE SKIN FS 160, LONGERON 30. REPAIRED PER EA 99-097479. MFG PART NUMBER: 5911401-5.SDR CAL950338S/O Valve · leakFLT NR 1581 - IAH - UPON LANDING FOUND HYDRAULIC FLUID LEAKING AT RUDDER. FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED SHUTOFF VALVE NO FURTHER ACTION. (W)SDR ABXA9500376Eyebolt · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD EYEBOLT HAD EXCESSIVE PLAY. REPLACED EYEBOLT, ADJUSTED AND FAIRED DOOR IAW DC-9 MM 32-12-1.SDR MWEA95189Skin · crackedDURING ROUTINE MAINTENANCE, A TEMPORARY REPAIR AT LONGERON 22L STA 160 WAS REPLACED WITH PERMANENT REPAIR IAW SRO9530219. TEMP REPAIR WAS ORIGINALLY INSTALLED DUE TO SKIN CRACK AT DESCRIBED LOCATION. RETURNED A/C TO SERVICE.SDR ABXA9500448T Cap · corrodedDURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT LOWER T-CAP BETWEEN STRINGERS 11 TO 12, 12 TO 13, 13 TO 14 AND 14 TO 15. REPAIRED IAW DC-9 SRM 51-22-1 AND DC-9 SB 57-98.SDR ABXA9500446Stringer · corrodedDURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING STRINGER NR 17 AT XCW 58. REPAIRED IAW DC-9 SB 57-98.SDR ABXA9500352Web · misdrilledDURING C-CHECK INSPECTION, FOUND HOLES DRILLED IN WEB AROUND LIGHTENING HOLE AT APPROXIMATELY STA 427, LONGERON 25R JUST ABOVE DOOR LOCKING CAM. REPAIRED IAW ABX REA D953-11484-MR.SDR 9513149607Tab · delaminatedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND APPROXIMATELY FOUR SQUARE INCHES OF DELAMINATION ON THE RIGHT AILERON CONTROL TAB LOWER SKIN. REMOVED AND REINSTALLED TAB IAW MM 27-10-1. MFG. PART NUMBER 5910047-2.SDR 9506909604Fittings · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 26R, 27R, 28R, AND 29R END FITTINGS FS 604. REPLACED FITTINGS.SDR MWEA95180Flashlight · inopCREW REPORTS, FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT. RETURNED A/C TO SERVICE.SDR ABXA9500451Frame · crackedDURING C-CHECK INSPECTION, FOUND FRAME STA 639, CRACKED AT AFT OUTBOARD FLANGE BETWEEN LONGERON 15L AND 16L. REPAIRED IAW ABX REA D953-11469-MR.SDR ABXA9500353Frame · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND FRAME AT STA 639 CRACKED AT AFT OUTBOARD FLANGE BETWEEN LONGERONS 15L AND 16L. REPAIRED IAW ABX REA D953-11469-MR.SDR ABXA9500447Stringer · corrodedDURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING STRINGER NR 12 AT XCW 58. REPAIRED IAW DC-9 SB 57-98.SDR MWEA95177Thermostat · failedCREW REPORTS, ON GROUND WITH APU RUNNING AND RIGHT PACK ON, CABIN FILLED WITH SMOKE. MAINTENANCE REPLACED LOAD THERMOSTAT. ALSO, INSTALLED LOAD CONTROL VALVE. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR ABXA9500526Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 22. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3.SDR ABXA9500525Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 22 NEAR T-CAP. REMOVED CORROSION ON AFT SIDE STRINGER 22, ALODINED AND PRIMED AREA IAW DC-9 SRM 57-03.SDR ABXA9500524Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 18, NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 51-10-3.SDR ABXA9500523Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 16. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3.SDR ABXA9500522Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 15 NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 57-03.SDR ABXA9500521Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 12 NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 57-03.SDR ABXA9500368Bulb · defectiveLEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE, RECYCLED GEAR AND FAILED AGAIN. WHILE TRYING TO GET BULBS OUT, ONE LIGHT ILLUMINATED. PUT GEAR DOWN, GOT NORMAL INDICATION BACKED UP WITH GROUND PROXIMITY SWITCH. FOUND BOTH LEFT MAIN LANDING GEAR SAFE BULBS HAD DESDR ABXA9500348Nut · brokenDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS AT STA 680 - 699, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2.SDR ABXA9500347Nut · brokenDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUT JUST AFT OF STA 756, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2.SDR ABXA9500346Nut · brokenDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS AT STA 718 - 737, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2.SDR ABXA9500345Nut · incorrectDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND INCORRECT FASTENER IN PLACE OF DOME NUT JUST AFT OF STA 658, LONGERON 18R. REPLACED FASTENER IAW DC-9 SRM 51-30-2.SDR ABXA9500344Nut · puncturedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND DOME NUTS JUST AFT OF STA 658, LONGERON 18L, PUNCTURED. REPLACED DOME NUTS IAW DC-9 SRM 51-30-2.SDR ABXA9500343Nut · brokenDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS JUST AFT OF STA 598, AT LONGERON 18L. REPLACED DOME NUTS IAW DC-9 SRM 51-30-2.SDR ABXA9500340Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE IN STRINGER NR 16. REMOVED CORROSION IAW DC-9 SRM 51-10-3.SDR ABXA9500339Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE IN STRINGER NR 22. REMOVED CORROSION IAW DC-9 SRM 51-10-3.SDR ABXA9500338Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 22 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03.SDR ABXA9500337Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORRROSION ON STRINGER NR 18 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 51-10-3.SDR ABXA9500336Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 15 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03.SDR 9506569951Vent Valve · malfunctionedFUEL BEGAN LEAKING FROM RIGHT WING TANK EN ROUTE PVD-DTW. LEAK WAS APPROXIMATELY 1600 LBS IN ONE HOUR. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLACED CLIMB VENT VALVE IN LEFT MAIN FUEL TANK. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CAL950306Skin · crackedIAH - A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 965R, THREE INCHES ABOVE L15. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B. (W)
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