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 USAA990269Fitting · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION AT INERCOSTAL 'T' FITTINGS (1 INCH BY .5 INCH AREA) AT FORWARD CARGO DOOR LOWER AFT DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M)SDR USAA990268Fitting · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION AT INTERCOSTAL 'T' FITTINGS (1 INCH BY .5 INCH AREA) AT LOWER FORWARD CARGO DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M)SDR USAA990267Skin · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN SKIN COMING OUT FROM UNDER TOP AFT STOP AT AFT LEFT EMERGENCY EXIT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03. (M)SDR TWAA9904910Fitting · crackedDURING OP 16 MAINT CHECK, FOUND BELOW ELECTRIC POWER CABLE RACEWAY AT STA 718 APPROX LBL 54 IN, A CRACKED T FITTING. REPLACED FITTING PER SPM 6-70-01 AND INSTALLED HI-LOKS PER SRM 51-30-5.SDR EISA99061Power Supply · inoperativeFOUND LEFT NACELLE SCANNING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NACELLE SCANNING LIGHT POWR SUPPLY IAW MM CHAPTER 33-53-0. OPS CHECK GOOD. (M)SDR EISA99060Switch · shortedON FINAL, AFTER PUTTING GEAR DOWN DID NOT GET A GREEN NOSE GEAR DOWN INDICATION. FOLLOWED PROCEDURES AND CONFIRMED NOSE GEAR DOWN AND LOCKED THROUGH PEEPHOLE. REPLACED NOSE GEAR LOCK SWITCH PER M/LM 32-60-01. OPS CHECK GOOD. (M)SDR ABXA9900309Frame · crackedFUSELAGE FRAME CRACKED AT STATION 389 AND LONGERON 5 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03.SDR ABXA9900308Longeron · crackedLONGERON 13 LEFT CRACKED AT STATION 965 LOWER ATTACH BOLT. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR ABXA9900307Shear Tie · crackedFUSELAGE FRAME SHEAR TIE CRACKED BELOW LONGERON 15 LEFT AT STATION 945. REPLACED SHEAR TIE IAW DC9 SRM 51-10-4 AND 51-30-2.SDR ABXA9900306Longeron · crackedLONGERON 3 RIGHT CRACKED AT STATION 718. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR ABXA9900305Longeron · crackedLONGERON 17 RIGHT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 53-02.SDR USAAD99048Retract Mech · malfunctionedDAY-PHL - FLT 648 - AFTER TAKEOFF AND UPON RETRACTING, THE LANDING GEAR THERE WAS A VIBRATION COMING FROM THE NOSE GEAR AREA. THE CAPTAIN DECIDED TO RETURN TO THE FIELD. THE VIBRATION CONTINUED UNTIL THE NOSE GEAR WAS EXTENDED AT ABOUT 180 KTS WHEN THE VIBRASDR TWAA9904922Pressure Deck · crackedDURING OP 16 MAINT CHECK, FOUND IN LT WHEEL WELL APPROX .5 IN CRACK AFT SIDE OF 718 CASTING, IN PRESSURE DECK. REPLACED NEW PLATE AND FASTENERS PER SRM 51-30-0. MADE NEW PART PER SPM 6-70-01, ITEM 4A, DRAWING 991015.SDR EISA99069Fuel Pump · failedRIGHT ENGINE FAILED TO OR ABOUT 500 FT AGL AFTER TAKEOFF IN RDU. CREW HEARD LOUD POP OR BANG AT FAILURE. NORMAL SINGLE ENGINE LANDING AT RDU. EMERGENCY WAS DECLARED. REMOVED AND REPLACED ENGINE FUEL PUMP IAW MM 73-20-1. OPS GOOD PER MM CHAPTER 71-00. RIISDR CALA9900329Skin · debondedINSPECTION FOUND RT WING LOWER SKIN PANEL FORWARD OF RIGHT GEAR DEBONDED. THE PANEL WAS REMOVED, REPAIRED AND INSTALLED IAW SRM 51-30-2, PAGE 4.SDR CALA9900328Floorbeam · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT OVERHEAD FLOORBEAM AT STA 237, LBL 8. THE CRACKED AREA WAS CUT OUT IAW SRM 53-05, PAGE 216A. A DOUBLER AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-05, PAGE 216A.SDR CALA9900327Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LT ELEVATOR O/B TRAILING EDGE SKIN (JUST I/B OF STATIC WICK). THE CRACK WAS STOP DRILLED AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-70-1, PAGE 12. WEIGHT AND BALANCE WAS WITHIN LIMITS IAW SRM 55-20-1, FIGURE 4.SDR CALA9900326Strap · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT LONGERON 23L STRAP BETWEEN STA 937 AND 967 CORRODED. THE FASTENERS AND STRAP WERE REMOVED IAW SRM 51-30-2. THE SURFACE CORROSION WAS REMOVED IAW SRM 51-10-3. A NEW STRAP WAS INSTALLED IAW SRM 51-01-0, 51-10-3, AND 51-3SDR TWAA9904921Support · crackedDURING OP 16 MAINT CHECK, FOUND IN FWD CARGO COMPT A CRACK AT CARGO FLOOR SUPPORT CHANNEL, STA 218, ABOVE LONGERON 25L. EDDY CURRENT CHECK INDICATED CRACK IN FORMER RADIUS. REPAIRED CRACKED FORMER PER SRM 53-01, PAGE 10 FIG 2.SDR EISA99059Gasket · tornADDED 5 QUARTS OIL TO NR 2 ENGINE IN LAS, TOTAL 13 QUARTS. HALF WAY TO SAN, QUANTITY WAS DOWN TO 4 QUARTS. (KEPT SLOWLY DECREASING IN-FLIGHT). SHUT DOWN NR 2 ENGINE. TEMPERATURE NEVER EXCEEDED 110 DEGREES EVEN AFTER IDLING AND SHUT DOWN. DETERMINED OIL FISDR CALA9900318Skin · debondedINSPECTION FOUND LEFT AILERON TAB DEBONDED. THE LEFT AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-51, PAGE 203.SDR CALA9900317Fitting · crackedINSPECTION FOUND A 1.6 CRACK IN LEFT FLAP O/B ACTUATOR AFT HINGE FITTING. THE LEFT FLAP O/B ACTUATOR AFT HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-50-01, PAGE 505.SDR CALA9900315Angle · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN LEFT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604, APPROXIMATELY LEFT LOWER BELLY FORWARD ADF SENSE ANTENNA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-45.SDR 9901179980Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND ESCAPE PATH EMERGENCY LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED POWER SUPPLY AT RIGHT SERVICE DOOR, OPERATIONAL CHECK NORMAL.SDR TWAA9904904Casting · crackedDURING OP 16 MAINT CHECK, FOUND FORMER CASTING CRACKED AT STA 639, APPROX 58.2 IN RBL. REPLACED FORMER PER SPM 6-70-01, PAGE 3 ITEM B.SDR 9901169980Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS AND AT GALLEY DOOR INOPERATIVE. REPLACED BLOWN FUSE IN GALLEY DOOR POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR TWAA9904908Window · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FWD EDGE AND AFT EDGE OF WINDOW 31 ON RT SIDE. BLENDED PER SRM 53-05, FIG 111 AND INSTALLED DOUBLER PER ARA 16105.SDR 9901109964Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR GTIA9900046Wire · brokenFRONT WHITE EMERGENCY FLOOR LIGHT OUT. REPLACED SOCKET AND LENS AND LAMP TO FRONT EPL LIGHT AND REPAIRED BROKEN WIRES. OPERATION CHECK NORMAL. (M)SDR GTIA9900045Battery · dischargedACY - FLT 286 - OVERHEAD EMERGENCY LIGHT IN COCKPIT INOPERATIVE. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. REMOVED AND REPLACED 2 EACH BATTERIES ON EMERGENCY LIGHT PACK, OPERATIONS CHECK GOOD. (M)SDR 9901099964Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR TWAA9904303Angle · corrodedDURING OP 16 MAINT CHECK, FOUND GALLEY FLOOR DRAIN ATTACH ANGLE CORRODED AT BOTTOM OF ANGLE, LOCATED STA 150 TO 160. SANDED AND POLISHED CORRODED ATTACH ANGLE PER SPM 6-80-01, PAGE 1 AND REPLACED ATTACH ANGLE PER SPM 6-70-01.SDR EISA99055Bulb · failedOVERHEAD EMERGENCY LIGHT IN COCKPIT WILL NOT LIGHT. REPLACED LAMP IAW 33-00-00. (M)SDR TWAA9904302Casting · crackedDURING OP 16 MAINT CHECK, FOUND FORMER CASTING CRACKED AT STA 658, APPROXIMATELY 58 IN RBL. REPLACED FORMER PER SPM 6-70-01, PAGE 3, ITEM 13.SDR TWAA9904206Longeron · crackedFOUND LONGERON 7R CRACKED AT STA 617, .375 INCH OUT OF BOLT HOLE. REMOVED CRACKED LONGERON FROM STA 610R TO 644R. REPAIRED PER SRM 53-2 FIG 18 AND STANDARD PRACTICES. CHECK-C 8-25-98 STL.SDR EISA99058Batt Charger · failedEMERGENCY TRACK LIGHTING INOPERATIVE. SEAT ROWS 15 TO 18. FOUND DURING SERVICE. REMOVED AND REPLACED AFT BATTERY CHARGER FOR EMERGENCY LIGHT SYSTEM IAW MM 33-53-0. OPS CHECK GOOD. (M)SDR TWAA9904012Bolt · corrodedDURING OP 16 MAINT CHECK, FOUND RT MAIN LANDING GEAR PULLEY QUADRANT ON FWD O/B BULKHEAD CABLE GUIDE PIN HAD CORRODED BOLT AND NUT. REPLACED BOLTS AND BUSHINGS AND CLEANED LARGE GUIDE PINS, AND REPLACED SMALL GUIDE PINS PER SPM 6-30-7.SDR TWAA9904011Channel · crackedDURING OP 16 MAINT CHECK, FOUND FUSELAGE TO CENTER WING SECTION U ATTACH CHANNEL CRACKED AT STA 598, LONGERON 22R. REPLACED PART PER SPM 06-70-01, PAGE 2 AND PAGE 3.SDR TWAA9904205Casting · crackedDURING OP 16 MAINT CHECK, FOUND CASTING AT STA 756 LONGERON 20R TO 21R WAS CRACKED. REPLACED FRAME PER SERVICE BULLETIN 53-168.SDR TWAA9904204Casting · crackedDURING OP 16 MAINT CHECK, FOUND AT STA 737 BETWEEN WING CENTER SECTION AND FLOOR LINE CASTING WAS CRACKED, ALSO 3 INCHES I/B OF CASTING, ON RT SIDE. INSTALLED NEW FRAME PER SERVICE BULLETIN 53-131.SDR TWAA9903904Window · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOWS ON RT SIDE OF ACFT NUMBERS 6, 7, 13, 14, AND 15. BLENDED PER SRM 53-05 FIG 111. REPAIRED PER ARA 16117.SDR TWAA9904103Support · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT STA 224, LBL 0. REPAIRED PER SPM 6-70-01, PAGE 2 ITEM 4. INSTALLED SPLICE PER SRM 53-01, PAGE 10 FIG 2. REPLACED ANGLE FROM STA 218 TO 265.SDR EISA99056Battery Charger · failedEMERGENCY TRACK LIGHTING INOPERATIVE SEAT ROW 15 TO 18, FOUND SERVICE CHECK. REMOVED AND REPLACED AFT BATTERY CHARGER FOR EMERGENCY LIGHT SYSTEM IAW MM 33-53-0. OPS CHECK GOOD. (M)SDR EISA99054Seal · out of positionAFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE DUE TO FORWARD RIGHT OVERWING EMERGENCY DOOR NOT BEING SEATED. AIR TURN BACK. REMOVED AND REPOSITIONED DOOR SEAL PROPERLY. OPS CHECK OK IAW 77-52-20. (M)SDR TWAA9904203Support · corrodedDURING OP 16 MAINT CHECK, FOUND AT STA 980 LT AFT LAV AREA, CORROSION AROUND FASTENER HOLE ON TOP OF FLOOR SUPPORT, LBL 19 IN. REMOVED CORROSION AS NECESSARY PER TWA SPM 6-80-01 PAGE 1. REPAIRED FLOOR SUPPORT PER SRM 53-05 PAGE 31.SDR TWAA9903908Track · corrodedDURING OP 16 MAINT CHECK, FOUND EXFOIL CORROSION ON CARGO COMPT FLOOR TRACK IN THE AFT CARGO COMPT AT THE LT FWD TRACK, FWD OF DOOR CUTOUT ON RT SIDE FROM STA 760 TO 996. REPLACED WITH NEW TRACK PER TWA SPM 6-70-01, AND DOUGLAS PRINT 5956033.SDR TWAA9903907Window · damagedDURING OP1 6 MAINT CHECK, FOUND WINDOWS 3, 4, AND 5 ON LEFT SIDE OF AIRCRAFT WITH STATIC BURNS. BLENDED EACH PER SRM 53-05 FIG III, AND ARA 16105. INSTALLED EXTERNAL REPAIR ON EACH PER DRAWING SR0950053 AND ARA 16105.SDR USAAD99044Retract Mech · iced upBUF-LGA - FLT 1731 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE LEFT GEAR INDICATED UNSAFE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEARS COVERED WITH ICE SLUSH. ALL THREE LANDING GEAR WERE DEICED AND OSDR TWAA9904202Window · damagedDURING OP 16 MAINT CHECK, FOUND CABIN WINDOW NR 36 ON RT SIDE WITH STATIC BURN AT AFT EDGE AND FWD EDGE. BLENDED PER SRM 53-05 FIG 3 NUMBER 25 AND 26 CASE 2. INSTALLED DOUBLER PER DRAWING SRO9530053 AND ARA 16105.SDR TWAA9904104Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT TOP AND BOTTOM SIDES AT STA 160, RBL 1 TO 55. MADE NEW FLOOR SUPPORT OF 7075T6 ANGLE AND INSTALLED WITH HL - 40 HI-LOKS USING 870B2 SEALENT PER SRM 51-01, PAGE 1.
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