Douglas DC-9-31
Service difficulty reports · 7,433
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 = 'DC931' 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 = 'DC931' 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 9702179933Switch · malfunctionedDURING APPROACH INTO DTW, ALL THREE RED UNSAFE LIGHTS REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR LEVER WARNING SWITCH S1-89. OPERATIONAL CHECK NSDR 9702169929Switch · malfunctionedFLAP/RUDDER STOP INOPERATIVE, LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP POSITION SWITCH S1-351. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR USAAD97047Power Supply · inoperativeCMH - LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. PLACED ON MEL. REPLACED POWER SUPPLY IN PIT ON 3-3-97. (M)SDR 9702339976Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LEFT SIDE OUTBOARD OF VERTICAL STIFFENER AT FS 110. REPAIRED PER EA 99-112044.SDR 9702329976Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LEFT SIDE INBOARD OF VERTICAL STIFFENER AT FS 110. REPAIRED PER EA 99-12044.SDR 9702299958Fitting · crackedDURING H-CHECK, FOUND CRACK IN RIB TO STRINGER ATTACH FITTING AT STR 23, RIB XRS 91.0, RIGHT WING. REPLACED PER SRM 51-30-5.SDR 9702089936Fuel Control · malfunctionedDURING TAKEOFF ROLL AT 75 KNOTS, THE LEFT ENGINE EPR, FUEL FLOW, AND N1 INDICAITONS BEGAN FLUCTUATING. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL. RAN ENGINE TO TAKEOFF POWER AND ALL PARAMETERS WERE NORMSDR 9702189935Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.SDR USAAD97030Wire · chafedLGA - FLOOR LEVEL LIGHTS INOPERATIVE AT ROWS 7-13. REPLACED CHAFED WIRE UNDER SEAT AT FORWARD EMERGENCY EXIT ROW ON RIGHT SIDE. (M)SDR USAA970044Skin · crackedPIT - DURING B-CHECK, FOUND 1.5 INCH CRACK IN VETICAL SKIN PANEL AT LEFT SIDE, VERTICAL STABILIZER SKIN, BENEATH DRAG ANGLE. REPAIRED DOUBLER .032 TITANIUM PER EA 46218. (M)SDR USAA970043Angle · crackedPIT - DURING B-CHECK, FOUND .75 INCH CRACK AT LEFT VERTICAL STABILIZER DRAG, DORSAL FIN, ANGLE JUST AFT OF STATION 1076. REPAIRED FOR MFG DRWG ANGLE AND DOUBLERS PE EA 46217. (M)SDR TWAA9716002Uplock Switch · dirtySTL - FLT 532 - DURING FINAL APPROACH, NOSE GEAR DOWN AND LOCKED LIGHT WENT OUT. DISCONNECTED, CLEANED AND RECONNECTED UPLOCK SWITCH. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9716001Coffeemaker · overheatedSTL - DURING DESCENT, EMERGENCY LANDING WAS DECLARED DUE TO ELECTRIAL ODOR. REMOVED AND REPLACED FIRST CLASS COFFEEMAKER, MFG P/N 50198A. OPERATIONAL CHECK NORMAL. (M)SDR ABXA9700813Bracket · corrodedDURING C-CHECK, THE RT AILERON PULLEY BRACKET IN THE WHEEL WELL WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM.SDR ABXA9700596Door · crackedDURING C-INSPECTION, FOUND THE LOWER CORNER OF THE LEFT MLG OUTBOARD ARTICULATING DOOR CRACKED. REPLACED THE DOOR IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9700592Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 3 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.SDR ABXA9700591Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 7 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.SDR ABXA9700590Rib · crackedDURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 8 CANTED RIB CRACKED LT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.SDR 9702319915Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 106, 23 INCHES RIGHT OF CENTER LINE. REPAIRED PER EA 99-112038.SDR 9702309915Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 106, 36 INCHES RIGHT OF CENTER LINE. REPAIRED PER EA 99-112038.SDR 9702159944Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK OK.SDR ABXA9700880Tab · damagedTHE RIGHT AILERON TAB WAS DAMAGED, HOLE IN UPPER OUTBOARD SKIN. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700838Cusp Web · corrodedDURING C-CHECK, THE CUSP WEB AT RBL 54, STA 275 WAS FOUND CORRODED. THE CUSP WEB WAS REPLACED IAW DC9 SRM.SDR ABXA9700837Cusp Web · crackedDURING C-CHECK, THE CUSP WEB AT RBL 46, STA 218 WAS FOUND CRACKED. THE CUSP WEB WAS REPLACED IAW DC9 SRM 51-30-1.SDR ABXA9700833Frame · damagedDURING C-CHECK, THE FUSELAGE FRAME AT STA 522 AT LONG 26 LT WAS FOUND DAMAGED. THE FRAME WAS REPAIRED IAW DC9 SRM 53-03, FIGURE 5.SDR ABXA9700832Frame · damagedDURING C-CHECK, THE FUSELAGE FRAME AT STA 579 AT LONG 25 RT WAS FOUND DAMAGED. THE FRAME WAS REPAIRED IAW DC9 SRM, AND DRAWING NR K05159.SDR ABXA9700827Frame · corrodedDURING C-CHECK, THE FUSELAGE FRAME AT STA 446 AT LONG 29 LT WAS FOUND CORRODED. THE FRAME WAS REPLACED IAW SRM 53-03, FIGURE 2A.SDR ABXA9700806Skin · corrodedDURING C-CHECK, THE FUSELAGE SKIN AT STA 588 AND 597 LONG 25 LT WAS FOUND CORRODED. THE SKIN WAS REPAIRED IAW REA D953-17985-MR.SDR ABXA9700805Skin · crackedDURING C-CHECK, THE FUSELAGE SKIN AT STA 996 LONG 14 LT, WAS FOUND CRACKED. THE SKIN WAS REPAIRED IAW REA D953-17705-MR.SDR ABXA9700801Fitting · crackedDURING COMPLIANCE OF AD 85-01-03 AMEND 39-4977: RT OUTBOARD SPOILER FITTING CRACKED. REPLACED FITTING IAW DC-9 M/M 27-61-1.SDR 9702199968Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR 9702029959Lock Mechanism · out of adjustDURING CLIMB, THE AIRSTAIR DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RIGGED INTERLOCK MECHANISM. OPERATIONAL CHECK OK.SDR 9701919914Downlock Switch · failedDURING APPROACH INTO DCA, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW CONFIRMED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS CALLED OUT OSDR ABXA9700834Frame · corrodedDURING C-CHECK, THE FRAME AT STA 237 AT LONG 20 RT TO 21 RT WAS FOUND CORRODED. THE FRAME WAS REPAIRED IAW DC9 SRM 53-03, FIGURE 5.SDR ABXA9700816Bulkhead Web · crackedDURING C-CHECK, THE LT ENGINE PYLON BULKHEAD WEB STA 965 WAS FOUND CRACKED. THE WEB WAS REPLACED IAW DC9 SRM 51-30-2.SDR ABXA9700815Slant Panel · corrodedDURING C-CHECK, THE LT SLANT PANEL WAS FOUND CORRODED. THE PANEL WAS REPLACED IAW DC9 SRM 51-30-1.SDR ABXA9700811Bracket · corrodedDURING C-CHECK, THE SLAT CONTROL SECTOR PULLEY BRACKET STA 637 WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM 27-80-2.SDR ABXA9700599Aileron · corrodedDURING C-INSPECTION, FOUND THE RIGHT AILERON LOWER SURFACE HAS CORROSION BULGES AT AILERON DAMPNERS. REPLACED RIGHT AILERON IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-10-1 AND 27-10-2.SDR ABXA9700507Spoiler · delaminatedBOTH UPPER AND LOWER SURFACES DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.SDR 9701899998Switch · failedRUDDER TRAVEL UNRESTRICTED LIGHT REMAINED ON AFTER TAKEOFF THROUGH 230 KNOTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RUDDER TRAVEL UNRESTRICTED SWITCH AND RUDDER CONTROL MANUAL SWITCH. ALSO, REPLACED LEAKING O-RING AT BELLOSDR 9701889988Escape Line · bindingDURING PERIODIC CHECK, FOUND LEFT AFT OVERWING EMERGENCY EXIT ESCAPE LINE WINDING IN HOUSING. MAINTENANCE LUBED REEL. OPERATIONAL CHECK NORMAL.SDR USAAD97028Battery Pack · dischargedROC - FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M)SDR GTIA9700144Intercostal · crackedMHV - FORWARD ACCESSORY COMPARTMENT AT STATION 180 ABOVE LONGERON L-29 AND INTERCOSTAL IS CRACKED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-10-3, 51-30-2. (M)SDR GTIA9700143Skin · mis repairedMHV - FS 996 - BELOW LONGERON 18R, REPAIR INSTALLED WITH BLIND FASTENERS, DOES NOT MEET REQUIREMENTS OF SRM 53-01 FIG 2, SHEET 3. REMOVED AND REPLACED REPAIR DOUBLER AND FILLER FABRICATED, TREATED, FINISHED, FASTENERS INSTALLED AND SEALED PER SRM 51-01, 51-10SDR ABXA9700824Intercostal · corrodedDURING C-CHECK, AN INTERCOSTAL FROM STA 578 TO 574 AT LONG 27 RT WAS FOUND CORRODED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM 51-30-2.SDR 9701779996Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT FORWARD AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9701749996T-Duct · failedDURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED BY SLIGHT ROLL TO THE RIGHT. CREW RETRACTED SLATS AND ACCOMPLISHED AN UNEVENTFUL LANDING USING FLAPS ONLY. MAINTENANCE REPLACED THE LEFT SLAT T-DUCT, OPERATIONAL CHECK NORMAL.SDR GTIA9700142Rear Spar · damagedMHV - PERFORM REPAIR AT WING STATION XRS 164 RT REAR SPAR PER DRAWING 5060165. REMOVED TEMP REPAIR, INSPECTED, STOPPED DRILLED CRACKS AND REINSTALLED TEMP REPAIR IAW SRM 51-10-3, 51-10-33, 51-30-5, 51-10-2, SB A47-146, AND DRAWING J06027. (M)SDR ABXA9700835Frame · crackedDURING C-CHECK, THE MAIN FRAME AT STA 718 RIGHT WAS FOUND CRACKED WHILE ACCOMPLISHING AD 78-07-05. THE FRAME WAS REPAIRED IAW REA DC53-17693-MR.SDR ABXA9700814Fitting · corrodedDURING C-CHECK, THE LONGERON END FITTING AT STA 756 LONG 30 WAS FOUND CORRODED. THE FITTING WAS REPLACED IAW DC9 SRM 53-02, PAGE 25.
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