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 ABXA9900047Fairing · crackedDURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER OUTBOARD ACTUATOR FAIRING CRACKED. REPLACED OUTBOARD AFT FAIRING IAW DC9 SRM 51-30-2 AND 51-30-8.SDR CALA9900068Support · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT LT FORWARD ENTRY STA 160, LBL 54. THE FASTENERS WERE REMOVED FROM FLOOR SUPPORT ANGLE IAW SRM 51-30-2. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-3, AND 53-02-00.SDR AT9900143Floor Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND FLOOR TRACKS AT THE AFT PIT STA 756 TO 780 AND ON THE RIGHT LOWER SIDE AT STA 935 TO 996 WITH CORROSION. MECHANICALLY REMOVED CORROSION, FABRICATED NEW SECTION OF FLOOR TRACKS, DRILLED, DEBURRED, COUNTERSUNK, TREASDR AT9900111Blkhd Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND INTERCOSTAL TEE ANGLE AT STA 996 PRESSURE BULKHEAD Z-34 CORRODED. REMOVED AND REPLACED TEE ANGLE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, AND 53-01.SDR TWAA9901601Longeron · crackedDURING OP 15 MAINT CHECK, LONGERON 5R WAS CRACKED AT STA 737. CUT OUT DAMAGED SECTION OF LONGERON. INSTALLED NEW SECTION OF LONGERON AND SPLICES PER DRAWING SRO9530128 AND SRM 53-02, FIG 18.SDR AT9900127Structure · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FORWARD AND AFT CARGO COMPARTMENT. LOCATIONS ARE AS FOLLOW: CARGO DOOR FRAME LOWER EDGE AT STA 340 TO 427, FRAME STA 522 L-28L TO L-28R, AFT CARGO WEB STA 870 L-29R ON LEFT AND RIGHT SIDE, AFT CASDR AT9900038Retract Mech · lack of lubeNO NOSE GEAR DOWNLOCK INDICATION ON GEAR EXTENSION, UPON ARRIVAL INTO ORLANDO MCO. RECYCLED GEAR, NO HELP. USED MANUAL PROCEDURES AND GOT DOWNLOCK INDICATION ON NOSE GEAR. DECLARED NO EMERGENCY MADE NORMAL LANDING. JACKED AIRCRAFT, CYCLED GEAR TWICE IN NORSDR MWEA99050Skin · lightning strikeFOUND FOUR LIGHTNING STRIKE ARCS IN RIGHT WING LOWER PLATING SKIN. MTC REPAIRED WITH RIVET INSTALLATION.SDR CALA9900039Fitting · crackedFOUND INTERCOSTAL ANGLE FITTING UNDER UPPER FWD DOOR STOP CRACKED .5 INCH. REMOVED ANGLE, FABRICATED, TREATED, PRIMED AND INSTALLED PER SRM 51-10-2, 51-10-3 AND 51-30-2.SDR CALA9900037Rib · crackedRIB CRACKED THROUGH FASTENER HOLE INSIDE LEFT WING L/E XRS545 (.5) 12 INCES OUTSIDE OF NR 5 SLAT CENTER TRACK. REMOVED AND INSTALLED NEW RIB PER SRM 51-30-2.SDR CALA9900036Frame · crackedAIRSTAIR DOOR CUTOUT LEFT SUPPORT FRAME CRACKED .75 BELOW AIRSTAIR OPEN/CLOSE FORWARD BRACKET ATTACH LEG, APPROX FS 1090. CUT DAMAGED AREA, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-01.SDR AT9900135Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON UPPER NOSE SKIN RIGHT SIDE AT STA 69.5 AT SECOND FASTENER JUST TO THE RIGHT OF PREVIOUS REPAIR. REMOVED EXISTING FILLER, FASTENERS, ENLARGED EXISTING CUTOUT TO REMOVED CRACK, FABRICATED, TREATED, PRIMEDSDR AT9900081Intercostal · crackedSHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO PIT CEILING CENTER LINE AT STA 503 INTERCOASTAL CRACKED AT FOUR WAY TIE SUPPORT. FABRICATED REPAIR, HEAT TREATED, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 51-30-2, 53-11-2 FIG 4,SDR AT9900080Skin · damagedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CREASE AT STA 218 L-18-19L AND A DENT AT STA 220 L-18-19L BOTH OUT OF LIMITS. COLD WORKED DENTS, FABRICATED INTERNAL DOUBLER REPAIR, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLED INTERNAL REPAIR IASDR TWAA9901106Power Supply · inopTHE AFT MOST SECTION OF CABIN FLOOR EGRESS LIGHTS ILLUMINATED IN FLIGHT. CREW TRIED TO RESET BY DISARMING AND REARMING, BUT NO HELP. REPLACED THE POWER SUPPLY. CHECK-C 12-7-98 STL.SDR AT9900138Structure · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION, DELAMINATION AND ELONGATED HOLES. FIRST, AT THE FORWARD CARGO SIDE WALL STRAPS (4 EACH) AND THRESHOLD DOOR STRAP (AFT SIDE) CORRODED AND ENLONGATED HOLES. SECOND, AT THE E/E COMPSDR AT9900125Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT MAIN FRAME LOWER FORWARD POCKET AND LOWER FLANGE IN THE WHEEL WELL AT STA 718 CRACKED. REMOVED AND REPLACED MAIN FRAME IAW EO 12-5511-29-B1044, EO 12-5511-29-B1044, AND SB 53-131 R4. FRAME (P/N 9919619-50SDR AT0099104Trim Tab · out of positionSCHEDULED INSPECTION AT AERO CORP, FL. RUDDER TRIM TAB DOES NOT HAVE MINIMUM CLEARANCE AT TOP END PER DC9 MM 27-20-1 PG 602. TRIMMED TOP OF TRIM TAB TO 5/32 TO COMPLY WITH MM 27-20-0 PG 603, TREATED, AND PRIMED IAW DC9 SRM 51-10-3, 55-01 PG 1, AND RES NR 992SDR MWEA99049Shear Tie · crackedFUSELAGE FRAME AT STATION 896 SHEAR TIE CRACKED AT AFT FASTENER ROW ABOVE LONGERON 24 LEFT. MTC FABRICATED AND INSTALLED NEW SHEAR TIE.SDR MWEA99039Skin · dentedFUSELAGE SKIN DENTED AT STATION 890 TO 897 BETWEEN LONGERON 24 AND 25 LEFT. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR AT9900113Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND CABIN FLOORBOARD PANEL AT STA 680-756, STA 965-996, AND FLOOR BOARD NR 97 CORRODED, MISSING CHAFFED STRIP, ELONGATED HOLES, RIVET HEADS PULLING UP, AND MISSING INSULATION. FABRICATED NEW FLOORBOARD, HAT CHANNELS, ISDR VJ9900032Wire · brokenPATH LIGHTING DOES NOT ILLUMINATE FROM ROW 10 TO ROW 14. REPAIRED BROKEN WIRE AT ROW 14 PER DC-9 MM 33-50.SDR CALA9900062Tab · debondRIGHT AILERON INBOARD TAB HAS APPROXIMATELY 1 BY 10 DEBONDED LOWER SKIN. REMOVED AND REPLACED RIGHT AILERON PER MM 27-10-2.SDR ABXA9900155Frame · crackedDURING C-CHECK, FOUND PYLON BULKHEAD FRAME CRACKED, STATION 965 AT LONGERONS 15 TO 16 LEFT.SDR MWEA99038Fitting · crackedFOUND CRACK ON AFT CARGO DOOR BEAM END FITTING. MTC FABRICATED AND INSTALLED NEW END FITTING.SDR 9900149608Frame · crackedDURING PERIODIC CHECK, FOUND UPPER CORNER CRACKED AT FS 699, LONGERON 12L TO 26L. REPAIRED PER EA 99-163240.SDR CALA9900013Skin · bentAFT CARGO COMPARTMENT DOOR LOWER EXTERIOR SKIN EDGE BENT. CUT OUT BENT AREA AT AFT CARGO DOOR LOWER EDGE EXTERIOR SKIN AND INSTALLED DOUBLER REPAIR PER SRM 52-01.SDR CALA9900012Skin · corrodedFUSELAGE LOWER SKIN AT APPROX STA 332 AT RT LONGERON 29 AREA HAS ONE POPPED RIVET AND BULGED. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW FINGER DOUBLER PER SRM 51-00-00.SDR AT9900144Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION WITH CORROSION. FIRST, THE CABIN FLOOR PANEL NR 89 ON THE UNDER SIDE AT FORWARD END. SECONDLY, THE CUSP WEB AND FITTING AT STA 229 LEFT SIDE AROUND RIVETS AND DOUBLER. THIRD, THE PULLEY BRACKET SDR AT9900130Structure · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION. FIRST, AT STA 602 LONGERON L-29L. SECONDLY, THE AFT PIT FORWARD SIDE AT STA 382 BETWEEN L-29R TO L-27L. THIRD, THE LEFT LAVATORY BULKHEAD LOWER PORTION AT STA 965. LAST, CORROSSDR MWEA99031Rat Probe · failedRAT PROBE DRAWS ZERO AMPS. MAINTENANCE REMOVED AND REPLACED RAT PROBE.SDR CALA9900011Angle · crackedRIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51-10-3, AND 51-10-2.SDR AT9900259Fairing · delaminatedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND DELAMINATION ON INBOARD AND OUTBOARD SIDES OF LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING. REMOVED INNER SKIN AND HONEYCOMB CORE FROM LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING THAT WAS DELAMINATED. TRIM NEWSDR AT9900146Support · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS FLOOR FRAME AT DIFFERENT LOCATIONS CRACKED. FIRST, THE FORWARD CARGO FLOOR FRAME SCREW HOLE CRACKED/ELONGATED AT STA 237 BETWEEN L-29-30L. SECONDLY, STA 794 FRAME ON THE FORWARD SIDE BETWEEN L-29-30R. THSDR AT9900137Longeron · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT STA 361R L-28R. REMOVED FASTENERS, COLD WORKED DENT, HFCE INSPECTED DENT WITH NO CRACKS NOTED. FABRICATED DOUBLER, FINGER DOUBLERS, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSSDR AT9900019Battery Pack · dischargedWINDOW EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50.SDR ABXA9900022Control Valve · iced upON APPROACH, LANDING GEAR HANDLE WAS 'FROZEN' IN THE UP POSITION. ACCOMPLISHED DC9 ABNORMAL PROCEDURES. EMERGENCY GEAR EXTENSION, RESULTED IN UNEVENTFUL LANDING. REMOVED ICE FROM LANDING GEAR CONTROL VALVE CABLES, RESET EMERGENCY EXTENSION CONTROLS. CYCLEDSDR ABXA9900015Angle · crackedDURING C-CHECK, FOUND LEFT PYLON UPPER ATTACH ANGLE CRACKED. REPAIRED ATTACH ANGLE IAW DC9 SRM 54-04.SDR 9900129920Bulkhead · crackedDURING PERIODIC CHECK, FOUND STRUCTURE FATIGUE AT FS 83.5. REPAIRED PER EA 99-162798.SDR MWEA99030Actuator · lack of lubeAFTER TAKEOFF GEAR AND RETRACTION LOTS OF VIBRATION AND IT SEEMS ONE NOSE GEAR DOOR IS NOT CLOSED. FOUND RIGHT NOSE GEAR DOOR OPEN LUBED DOOR LINK ACTUATOR ASSEMBLY.SDR CALA9900014Switch · intermittentEMERGENCY FLOOR PATH LIGHTS INTERMITENT FROM COCKPIT SWITCH. REMOVED AND REPLACED COCKPIT SWITCH PER MM 33-00-00.SDR CA990203018Combustion Can · failed(CAN) ENGINE INDUCTED IN THE SHOP FOR 12 STAGE HP COMPRESSOR DISC BEING TX'D. DISASSEMBLY OF THE ENGINE FOUND TWO COMBUSTION CANS (IGNITER CANS) WERE SHOWING SIGNS OF EXTREME BRITTLENESS AND AN EXCESSIVE NUMBER OF INTERGRANULAR CRACKS. THE TWO CANS WERE SCRASDR AT9900145Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION CORRODED AND CRACKED. FIRST, THE AFT PIT LOWER SIDE WALL TIEDOWNS COVER ON THE LOWER SIDE. SECONDLY, THE AFT PIT CEILING SUPPORT CORRODED AND CRACKED AT STA 935 TO 996. ALSO, THE GLIDE SLOPE ANTSDR AT9900140Fairing · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 2 AFT INBOARD UPPER THRUST REVERSER ACTUATOR FAIRING IS CRACKED. REMOVED THE THRUST REVERSER FAIRING, WELDED AND REINSTALLED IAW DC9 MM 78-00 AND RES NR 99244.SDR AT9900020Skin · dentedSCHEDULED INSPECTION AT AERO CORP FL, FUSELAGE SKIN HAS NUMEROUS DENTS FROM FS 229 TO FS 589 RIGHT SIDE. REMOVED AND REPLACED FUSELAGE SKIN FS 229 TO 589 RIGHT SIDE IAW RES 982130 AND RES 982249. SKIN (P/N 5920-119-5).SDR ABXA9900030Bulkhead Web · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED. REPAIRED WEB CRACK IAW ABX REA D953-26127MR.SDR MWEA99023Angle · crackedFOUND CRACKED ANGLE BRACKET AT BUSS OF RIGHT VERTICAL STABILIZER AFT SPAR BOX. MTC FABRICATED AND INSTALLED NEW ANGLE CLIP.SDR MWEA99021Jamb · corrodedFOUND CORROSION ON AFT CARGO DOOR JAMB AFT WEB AREA. MTC FABRICATED AND INSTALLED WEB REPAIR WEB.SDR CALA9900010Terminal · failedAFT DOOR EMERGENGY EXIT LIGHT INOP. REPAIRED TERMINAL AT LIGHT AND OPS CHECK OK PER MM 33-53-01.SDR AT9900018Clamp · brokenCLIMBING THROUGH 14,000 FEET MASTER WARNING LIGHT ILLUMINATED WITH TAIL COMPARTMENT TEMPERATURE HI-LIGHT ON, NORMAL PROCEDURES FOLLOWED. REPLACED BROKEN CLAMP AT LEFT HAND HEAT EXCHANGER PRIMARY AIR DUCTING PER MM 36-10.
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