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 ABXA000081Fitting · crackedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATACH FITTING CRACKED AT STA 737. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR CA000209044Spacer · cracked(CAN) FRONT COMPRESSOR ROTOR THIRD TO FORTH STAGE SPACER WAS FOUND CRCKED, ONE CRACK EXTENDED FROM TIEROD SLEEVE HOLES TO INSIDE DIAMETER. REPORT TO FOLLOW. THE CRACK WAS VERY TIGHT WHICH HAD NOT TRAVELLED OUT OF THE TIE ROD HOLES WALL. THE ITEM WAS FOUND DURRSDR CA000209045Receptacle · failed(CAN) DURING TAXI BURNING SMELL NOTED AND TRACED TO GALLEY OVEN. A/C RETURNED. GALLEY OVEN RECEPTACLE AT FAULT REPLACED.SDR AT0000039Angle · corrodedFOUND ELECTRICAL EQUIPMENT COMPARTMENT SUPPORT BETWEEN BS 110-120 IS CORRODED FROM LONGERON 25R TO 26R. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORROSION FROM COMPARTMENT, TREATED WITH ALODINE. FABRICATED REPAIR ANGLE FOR BRACKETS, PRIMED SUPPORT BRACKSDR AT0000032Skin · crackedFOUND FUSELAGE UPPER NOSE SKIN HAS 1 EACH CRACK ON RIGHT SIDE ATBS 76.55 17.25 OUTBOARD OF CENTER LINE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SB 53-262, EO NR 12-5330-29-B1048 AND SRO 09530239..SDR AT0000031Skin · crackedFOUND FUSELAGE UPPER SKIN HAS 2 EACH CRACKS ON LEFT SIDE AT BS 76..55, 16.25 OUTBOARD, AND 18.25 OF CENTER LINE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SB 53-262, EO NR 12-5330-29-B1048 AND SRD-SR09530239.SDR MWEA00023Clip · crackedINTERCOSTAL CLIP IS CRACKED AT FUSELAGE STATION 180, 20 LEFT OF CENTERLINE. MTC FABRICATED AND INSTALLED NEW CLIP.SDR MWEA00013Battery Pack · inoperativeEMERGENCY LIGHTS IN TAIL COMPARTMENT IS INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK.SDR 0000079926Sensor · malfunctionedLANDING GEAR DOOR OPEN LIGHT ILLUMINATED ENROUTE BDL-DTW. FLIGHT WAS CONTINUED TO DESTINATION AND LIGHT REMAINED ON AFTER GEAR EXTENSION. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SDR MWEA00027Bulkhead · corrodedUPPER WEB OF VENTRAL STAIRWAY BULKHEAD AT STATION 996 HAS AN AREA OF MODERATE CORROSION. MTC FABRICATED AND INSTALLED DOUBLER.SDR MWEA00024Skin · gougedLEFT HAND VERTICAL STABILIZER SKIN IS GOUGED UNDER THE FORWARD UPPER HORIZONTAL STABILIZER FAIRING. MTC FABRICATED AND INSTALLED DOUBLER.SDR AT0000027Bracket · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND INTERCOSTAL BRACKET AT BS 433 L-28R CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET AT BS 433 L-28R IAW DC9 SRM 51-10-04, 51-10-03, AND 51-30-05.SDR MWEA00016Floorboard · crackedRIGHT SIDE CABIN FLOORBOARDS MARKED F4 AND E6 HAVE SEVERAL CRACKS NEAR THE ENDS. MTC FABRICATED AND INSTALLED DOUBLERS.SDR L1GA200000008Floor Support · crackedHEAVY CORROSION AND CRACKS FOUND ON FLOORBOARD SUPPORT EXTRUSION AND WEB AT RBL 44 STATION 160 TO 200.SDR AT0000014Glide Slope · inoperativeATTEMPTED 3 APPROACHES INTO ATLANTA (ATL), BOTH NAV'S FAILED ON ALL THREE APPROACHES, CONDITIONS WERE ILS. AIRCRAFT DIVERTED TO (AGS) AUGUSTA FOR A VFR APPROACH. REMOVED AND REPLACED BOTH NAV RECEIVERS IAW DC9 MM 34-00.SDR MWEA00028Angle · crackedAFT CARGO DOOR UPPER ANGLE INSIDE INNER PAN IS CRACKED. MTC FABRICATED AND INSTALLED NEW ANGLE.SDR AT0000016Frame · damagedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND TEMPORARY FRAME REPAIR AT BS 218 LONGERON 26-27L AND LONGERON 26-27R. INSTALLED NEW REPAIR AT BS 218 LONGERON 26-27L AND LONGERON 26-27R IAW RES 00-0026.SDR AT0000015Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND TEMPORARY REPAIR IN FUSELAGE BS 240 LONGERON 26-29R. INSTALLED REPAIR AT BS 240 LONGERON 26-29R IAW REO L00008.SDR 0000049926Connector · brokenNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW EXTENDED GEAR, DECLARED AN EMERGENCY, AND PERFORMED FLY-BY OF TOWER TO DETERMINE IF GEAR WAS DOWN AND LOCKED. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CANSDR TWAA0001009Floor Panel · damagedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 40B WITH FIELD REPAIR. MADE NEW FLOOR PANEL PER TWA SSRM 53-00-104, PAGE 201.SDR TWAA0000502Actuator · wornCREW WAS UNABLE TO EXTEND THE NOSE LANDING GEAR DURING APPROACH TO MLI WAS NECESSARY TO USE MANUAL NOSE GEAR EXTENSION. FOUND PROBLEM WAS THE NOSE LANDING GEAR BUNGEE CYLINDER. MAINTENANCE FERRIED THE AIRCRAFT TO STL FOR REPLACEMENT. CHECK-C 8-28-99 STL.SDR MWEA00008Cover · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER.SDR TWAA0001008Floor Panel · corrodedDURING OP 16 MAINT CHECK, PANEL NUMBER 44 HAD GOUGES AT END OF TOP HATS AND CORROSION AT OPPOSITE END. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201.SDR TWAA0001007Floor Panel · brokenDURING OP 16 MAINT CHECK, NUMBER 21 FLOOR PANEL CORNER WAS BROKEN. FABRICATED NEW PANEL PER SSRM 53-00-14, PAGE 201.SDR TWAA0001006Floor Panel · crackedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 19 SUPPORT RIBS WERE CRACKED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201..SDR TWAA0001005Floor Panel · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANELS 7, 8, 9, 10, 11, 29, AND 58. NEW FLOOR PANELS MADE PER TWA SSRM 53-00-104.SDR AT0100043Cargo Track · corrodedFOUND AFT PIT CARGO TRACK BS 937 - 966 CORRODED BEYOND LIMITS. REPAIRED CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, AND 53-21.SDR TWAA0000304Angle · crackedDURING CHECK-C MAINT, FOUND THE RT AFT VERTICAL STABILIZER ATTACH ANGLE CRACKED APPROX .75 INCH IN AT STA 1104. RT VERT STAB ANGLE AT STA 1104 REPAIRED PER SRM 53-05, FIG 23.SDR MWEA00010Seat Track · crackedSEVERAL DAMAGED FASTENER HOLES SUBFLOOR UNDER INBOARD PILOTS SEAT TRACK. MTC STOP DRILLED CRACK, THEN FABRICATED AND INSTALLED DOUBLER.SDR MWEA00006Light · damagedFOUND SECTION OF EMERGENCY FLOOR TRACK LIGHTING DAMAGED AND LOOSE. MAINTENANCE REPLACED DAMAGED SECTION OF EMERGENCY FLOOR TRACK LIGHTING.SDR MWEA00004Cover · looseFORWARD ENTRY DOOR EMERGENCY SLIDE COVER CAME LOOSE WHEN OPENING DOOR IN MKE. MTC REINSTALLED FORWARD EMERGENCY DOOR SLIDE COVER.SDR 20001130SH006Engine · surgesMKE - FLT 279 - DURING TAKEOFF AT 90 KNOTS, LEFT ENGINE HAD A BAD COMPRESSOR SURGE. DISCONTINUED TAKEOFF. MTC INSPECTED INLETS AND EXHAUST NO DEFECTS NOTED. MTC THEN RAN ENGINES. NO ABNORMAL INDICATIONS NOTED. (X)SDR 20001130SH005Engine · surgesMKE - FLT 279 - DURING TAKEOFF ROLL, RIGHT ENGINE HAD A COMPRESSOR SURGE. DISCONTINUED TAKEOFF. MTC INSPECTED INLETS AND EXHAUST, NO DEFECTS NOTED. MTC THEN RAN ENGINE. NO ABNORMAL INDICATIONS NOTED. (X)SDR TWAA0000109Longeron · crackedDURING CHECK-C MAINT, FOUND 0.125 IN LONG CRACK IN RT LONGERON 12, JUST AFT OF APU EXHAUST DUCT EXIT ON FUSELAGE, INSIDE THE FUSELAGE INTERIOR TAIL. REMOVED AND REPLACED THE SPLICE WITH NEW LONGERON SPLICE PER SRM 51-30-2 AND SRM 51-30-5.SDR AT0000008Engine · fodON CLIMB-OUT, NOISE AND VIBRATION WERE NOTED FROM NUMBER 2 ENGINE. NR 2 ENGINE SHUT DOWN, AIRCRAFT RETURNED FOR LANDING. REMOVED AND REPLACED NR 2 ENGINE AND CONFIRMED BIRD STRIKE.SDR ABXA000062Fitting · crackedDURING C-CHECK, FOUND FITTING AT STATION 965 RBL 36 JUST BELOW FORWARD RIGHT PYLON CRACKED. REPLACED FITTING IAW DC9 SRM.SDR ABXA000061Bulkhead · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED ON RIGHT SIDE. REPAIRED AFT PRESSURE BULKHEAD IAW DC9 SRM 53-05.SDR MWEA00003Engine · malfunctionedDURING TAKEOFF ROLL, RIGHT ENGINE HAD A COMPRESSOR SURGE. DISCONTINUED TAKEOFF. SUSPECTED SNOW/SLUSH WENT INTO ENGINE. MTC INSPECTED INLETS AND EXHAUST, NO DEFECT NOTED. MTC THEN RAN ENGINES, NO ABNORMAL INDICATIONS NOTED.SDR MWEA00005Engine · malfunctionedDURING TAKEOFF AT 90 KNOTS, LEFT ENGINE HAD A LOAD COMPRESSOR SURGE. DISCONTINUED TAKEOFF. SUSPECTED SNOW/SLUSH WENT INTO ENGINE. MTC INSPECTED INLETS AND EXHAUST, NO DEFECT NOTED. MTC RAN ENGINES, NO ABNORMAL INDICATIONS NOTED.SDR AT0100041Skin Panel · corrodedFOUND SKIN UNDER C2 LOWER THRESHHOLD AT BS 917 CORRODED. INSTALLED REPAIR IAW DC9 REO-L00364.SDR AT0000007Socket · inoperativeEMERGENCY PATH LIGHT WILL NOT ILLUMINATE. REPLACED SOCKET IAW DC9 MM 33-51-01.SDR MWEA00002Antenna · inoperativeON TAKEOFF ROLL, HAD HEAVY SMELL OF ELECTRICAL FUMES. MTC FOUND SMELL IN RADOME AND REMOVED AND REPLACED WEATHER RADAR ANTENNA.SDR MWEA00904Rib · damagedTHREE EACH, LEFT TRAILING EDGE FLAP RIBS ARE DAMAGED. MAINTENANCE FABRICATED AND INSTALLED RIBS.SDR AT0000006Pushrod · disconnectedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. FOUND CABLE SECTOR DISCONNECTED FROM PUSHROD. ATTACHED PUSHROD AND FASTENED/SECURED IAW DC9 MM 32-23-01.SDR AT0000005Wire · brokenEMERGENCY TRACK LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD EMERGENCY TRACK LIGHT IAW MM 33-53.SDR AT0000004Control Cable · disconnectedAFTER TAKEOFF LANDING, GEAR WOULD NOT RETRACT. FOUND CABLE SECTOR DISCONNECTED FROM PUSH ROD. ATTACHED PUSH ROD AND FASTENED WITH CASTLE NUT AND SECURED WITH COTTER PIN. WORK DONE IAW MM 32-23-1.SDR AT0000002Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT AT BS 437R LONGERON 24 TO BE OUT OF LIMITS. REMOVED AND REPLACED DENTED SKIN AT BS 437R LONGERON 24 AND INSTALLED DOUBLERS IAW EO 99-1433 AND DC9 MM 34-43-01.SDR AT0000001Skin · dentedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND SKIN AT BS 110 DENTED. CUT AND SPLICED NEW SECTION OF SKIN IAW EO 99-1436.SDR TWAA0000614Bracket · missingDURING OP 16 MAINT CHECK, RT WING TE NEED INSTALL RIB ASSEMBLY OTBD OF CENTER FLAP HINGE ASSEMBLY AFTER FLAP BRACKET INSTALLED. INSTALLED RIB ASSEMBLY USING HI-LOCKS PER SRM 51-30-5 AND RIVETS PER SRM 51-30-2.SDR TWAA0000110Longeron · crackedDURING CHECK-C MAINT, FOUND IN THE FUSELAGE INTERIOR, BOTH FLANGES OF LONGERON 5L AT STA 639 WERE CRACKED APPROX 1/2 INCH LONG. REMOVED THE DAMAGED SECTION OF LONGERON AND FABRICATED A SECTION OF NEW LONGERON. LONG SPLICED AND INSTALLED PER SRM 53-02, FIG 18
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