Douglas DC-9-33F
Service difficulty reports · 1,681
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 = 'DC933F' 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 = 'DC933F' 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 FXGA20160128001Strut · low pressureAFTER TAKEOFF COULD NOT RETRACT GEAR, HANDLE WOULD NOT MOVE TO UP POSITION. THE CAUSE WAS THE NLG STRUT WAS LOW ON PRESS.SDR K11A2015121516001Stringer · corrodedCORROSION AT STRINGER 23, RT BS 225 FWD CARGO.SDR FXGA201509221537Seat Track · damagedDAMAGED SEAT TRACK LUG AT FS 400, LBL 54. TO REMOVE AN OUT OF LIMIT IAW SRM CHAPTER 53-05 FIGURE 4B SHEET 1, SEAT TRACK LUG TO PRECLUDE THE INSTALLATION OF ANCHORING DEVICES IN THE DAMAGED AREA. TRIM OUT DAMAGED & MATCHING LUGS IAW DWG 1537-01. TRIM FLUSH TSDR FXGA20150602001Skin · crackedSKIN CRACK AT STATION 466 AROUND LOWER VHF ANTENNA. A CRACK WAS FOUND IN THE VICINITY OF THE LOWER VHF ANTENNA WHILE PERFORMING A VISUAL INSPECTION REQUIRED BY AD 85-03-08R1. STOP DRILL CRACK & ACCOMPLISH REPAIR IAW ATTACHED MSGS. TNK-TNKK-15-0026-01C DATEDSDR FXGA201505061516Frame · crackedFRAME REPAIR, STATION 389, LONGERON 12R - 14R. MAJOR REPAIR. FUSELAGE FRAME INBD FLANGE CRACKED AT STATION 389 BETWEEN LONGERON 12R & 14R.SDR FXGA201505061515Frame · corrodedFRAME REPAIR STA 180, L-28L TO L-28R. MAJOR REPAIR. FUSELAGE FRAME LOWER FLANGE CORRODED AT STATION 180 BTWN LONGERON 28 LEFT AND LONGERON 28 RIGHT.SDR FXGA201505061517Skin · damagedLIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 101 - 110, LONGERON 17L & 18L. MAJOR REPAIR. TWO EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.SDR FXGA201505061518Skin · damagedLIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 83.550 - 89.050, LONGERON 16R & 17R. MAJOR REPAIR, 3 EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.SDR 7AHR2015043000420Frame · crackedFRAME AT BS 389 BETWEEN LONGERONS 12 - 14R IS CRACKED. REPAIRED SECTION OF FRAME IAW SRM 53-03, FIG 4.SDR 7AHR2015043000371Frame · corrodedE & E BAY BILGE AREA FLOOR FRAME HAS CORRISON FROM LONGERON 28L-28R STA 180. R & R SECTION OF FRAME, STA 180, LONGERON 28L-28R IAW SRM 53-03, FIG 5.SDR 7AHR2015043000346Seat Track · corrodedLIGHT SURFACE CORROSION ON SEAT TRACK, FLOOR ATTACHMENT AREAS IN VARIOUS LOCATIONS IN PASSENGER CABIN, STA 160-996, RBL5435 TO LBL 54.5. REMOVED LIGHT CORROSION AND TREATED AREAS. INSTALLED SEAT TRACK REPAIR STA 408-484, RBL 33 IAW SRM 53-05, FIG 4F AND 51-10SDR 7AHR2015043000203Mount · crackedRT INBD SPOILER CONTROL MOUNT BRACKET CRACKED ON REAR SPAR. INSTALLED A REPAIR TO MOUNT BRACKET IAW SRM 51-10-3A, 51-30-2,51-10-2, 51-10-4 AND 51-30-5.SDR 7AHR2015043000138Fitting · crackedWING TO FUSELAGE FITTING CRACKED LT SIDE BS 600, LONGERON 22L. R & R THE FITTING IAW SRM 51-30-1, 51-10-02, 51-10-4, 5110-2 AND 57-31-4.SDR 7AHR2015043000137Fitting · crackedRIGHT WING TO FUSELAGE FITTING IS CRACKED AT BS 600-LONGERON 22R. R & R THE FITTING IAW SRM 51-30-5, PGS 12-14, 51-30-01,51-10-4.51-10-2 AND 57-31-4.SDR 7AHR2015043000122Cargo Track · corrodedFORWARD LOWER CARGO COMPARTMENT CARGO TRACK SUPPORT HAS CORROSION FROM BS 427-513, RBL 14. REMOVED CORROSION FROM AREA. TRACK SUPPORT CHANNEL AND UPPER SUPPORT FLANGE OF INTERCOSTAL WERE REPAIRED/REINFORCED IAW SRM 51-70-5, FIG 1.SDR 7AHR2015043000110Attach Angle · crackedRIGHT PLYON LOWER ATTACH ANGLE CRACKED AT 996. INSTALLED NEW SECTION OF RT PYLON LOWER ATTACH ANGLE IAW SRM 54-04, FIG 10.SDR K11A2015041416001Skin · corrodedCORROSION ON FUSELAGE BELL JUST AFT OF NR 1 DME INTERROGATOR ANTENNA, FS 330.SDR 7AHR2015020482319Seat Track · corrodedMAIN DECK SEAT TRACK HYAS EXFOLIATION AND LUGS WORM AT BS 515.00, RBL 1.00. REMOVED CORROSION, REMOVED DAMAGED AREA OF SEAT TRACK AND INSTALLED REPAIR IAW FLIGHT VEHICLE CONSULTING DWG 53-15015-1 WITH FORM 8110-3 APPROVAL.SDR 7AHR2015020482282Seat Track · corrodedMAIN DECK SEAT TRACK CORRODED AT BS 186.00, LBL 1.00. REMOVED DAMAGED AREA AND INSTALLED A REPAIR IAW FLIGHT VEHICLE CONSULTING DWG 53-15015-2 WITH FAA FORM 8110-3 APPROVAL.SDR 7AHR2015020482245Seat Track · corrodedMAIN DECK SEAT TRACK HAS CORROSION & LUGS HAVE EXCESSIVE WEAR AT BS 998.00-1005.00 AT RBL 24.00. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW FLIGHT VEHICLE CONSULTING DWG 53-15009-3 WITH FAA FORM 8110-3 APPROVAL.SDR 7AHR2015020482349Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CHORD & REPAIR ANGLE HAS DOUBLE DRILLED HOLE COMMON TO SEAT TRACK FWD OTBD FLANGE AT BS 699, LBL 45.00. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW FLIGHT VEHICLE DWG 53-15009-1 AND 53-15009-2 WITH FAA FORM 8110-3SDR 7AHR2015020482447Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED AT STA 160 BL 0. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-01, 51-10-4, 51-10-3 & 51-30-2, FIG 1.SDR 7AHR201502042285Seat Track · crackedMAIN DECK SEAT TRACK CORRODED AND CRACKED AT BS 323, LBL 44. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, PAR 4, FIG 4F.SDR 7AHR201502042220Seat Track · corrodedMAIN DECK SEAT TRACK HAS CORROSION ON LUGS FROM BS 933 - 948, RBL 55. REMOVED DAMAGED SECTION OF SEAT TRACK AND REPLACED IAW SRM 53-05, FIG 4F, 51-30-2 & 51-30-1.SDR 7AHR201502032378Door Frame · corrodedFWD CARGO DOOR CUT OUT LOWER DOOR FRAME HAS CORROSION IN SEVERAL AREAS. REMOVED DAMAGED AREA OF DOOR FRAME IAW SRM 51-70-5. DOOR FRAME REPAIRED BETWEEN STA 370-427 IAW SRM 53-05, FIG 44.SDR 7AHR2015020382350Floorbeam · damagedMAIN DECK FLOORBEAM FWD CHANNEL HAS DOUBLE DRILLED HOLE COMMON TO SEAT TRACK OTBD FWD HOLE WITH DAMAGE TO SEAT TRACK AT BS 680.00, LBL 43.00-45.00. UPON REMOVAL OF SEAT TRACK FITTING ON AFT SIDE AT STA 680 ALSO HAS DOUBLE DRILLED HOLE. R & R FITTING, PN 3922SDR 7AHR548B7582361Cusp Web · corrodedCUSP WEB HAS CORROSION ON BOTTOM SIDE RBL 45.00 BETWEEN BS 691.00-695.00. CUSP WEB REPAIR WAS ACCOMPLISHED IAW SRM 53-05 REPAIR CONFIGURATION.SDR 7AHR548B7582357Cusp Web · puncturedCUSP WEB AT BS 775 HAS CORROSION ON BOTTOM & TOP FROM RBL 50-57 JUST AFT OF FLOORBEAM. TRIMMED OUT DAMAGED AREA OF CUSP WEB IAW SRM 53-05, FIG 131A-18 AND INSTALLED REPAIR IAW SRM 51-30-2, FIG 20 & 51-30-1.SDR 7AHR201502032356Cusp Web · puncturedCUSP WEB PUNCTURED AT BS 797, RBL 47.5. REMOVED DAMAGED AREA, LOCATED AND DRILLED DOUBLER AND INSTALLED REPAIR IAW SRM 53-05, FIG 131A-19,53-05.SDR 7AHR201502032348Cusp Web · crackedCUSP WEB HAS PREVIOUSLY STOP DRILLED CRACKS THAT HAVE EXTENDED PAST THE STOP DRILLED AREAS AT BS 756 - 775, LBL 45. REPAIRED THE CUSP WEB IAW SRM 53-11-3, FIG 11B, 51-30-2, 51-30-01 & 51-30-3.SDR 7AHR548B7582228Cusp Web · crackedCUSP WEB IS CRACKED IN MULTIPLE AREAS AND MISSING FASTENERS FROM BS 756 - 775 BL 60. R & R CUSP MEMBRANE IAW SRM 53-11-3, FIG 11B, 51-30-2 & 51-30-1.SDR FXGA20141224001Unknown · malfunctionedAT APPROX 2245Z & CLIMBING THROUGH FL280, R OIL STRAINER CLOGGING, ANNUNCIATOR ILLUMINATED. PERFORMED ABNORMAL CHECKLIST. REDUCED POWER TO IDLE ON RT ENG. DECLARED AN EMER & RETURNED.SDR FXGA201409241439Seat Track · corrodedCORROSION ON INBD LT SEAT TRACK IN FLIGHT DECK. AFTER CORROSION REMOVAL, FOUND SEAT TRACK TO BE OUT OF LIMITS. REMOVED & FABRICATED NEW SECTION OF TRACK & INSTALLED IAW DC9-SRM 51-40-4, 51-30-2 & 53-05 FIG 92.SDR 7AHR201409242160Finger Doubler · corrodedLONGERON 26 RIGHT BS 598 INTERNAL FINGER DOUBLER PILLOWING AND CRACKED AT SPLICE FITTING. AFTER CORROSION REMOVAL THE AREA WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-3, 53-04-1, 51-30-5 AND 51-04-03.SDR 7AHR201409242362Seat Track · corrodedCORROSION WAS NOTED IN THE COCKPIT LT INBD SEAT TRACK. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-10-3, 51-10-04, 51-30-2 AND 53-05, FIG 92.SDR FXGA201409231438Skin · gougedVERTICAL STABILIZER LT TIP PLATING REPAIR FROM ZV73 TO ZV147 BETWEEN YV157 & YV172. GOUGES FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER & LOWER BANANA FAIRING.SDR FXGA201409231437Web · dentedNOSE LANDING GEAR SUPPORT WEB RT SIDE REPAIR. REPAIRS WEB DENTED IN RT SIDE NOSE GEAR WW NEAR RT TRUNNION FITTING.SDR FXGA201409231436Finger Doubler · corrodedREPAIR AT LONGERON 26RT FS 598 INTERNAL FINGER DOUBLER. LONGERON 26RT FS 598 INTERNAL FINGER DOUBLER IS PILLOWING & CRACKED AT SLICE FITTING LOCATION. REPAIR THE DOUBLER IAW SRM.SDR 7AHR2014092300002Structure · gougedGOUGED AREAS WERE FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER AND LOWER BANANA FAIRING. GOUGED AREAS WERE FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO TIP PLATING IAW FLIGHT VEHICLE CONSULTING DWG NR 55-14233-1, REV-NEW, DATED SESDR 7AHR201409232049Web · dentedWEB DENTED IN RT SIDE NOSE GEAR WHEEL WELL NEAR RT TRUNION FITTING. REMOVED DAMAGE FROM WEB, FABRICATED REPAIR PARTS FOR DOUBLER AND INSTALLED IAW FLIGHT VEHICLE CONSULTING, DWG 53-14230-1, REV NEW, DATED SEPT 4, 2014. APPROVAL FOR REPAIR IAW FORM 8110-3.SDR FXGA20131121001Unknown · malfunctionedAT ALTITUDE 350 CABIN PRESS LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES, COULD NOT RESTORE PRESS. DECLARED AN EMERGENCY WITH CTR AT 0253Z. DESCENDED TO 10,000 CONTINUED TO FAI.SDR FXGA20131023001Skin · damagedAIRCRAFT WAS STRUCK BY LIGHTNING DURING CLIMB. NO ABNORMAL INDICATIONS AFTER STRIKE. COMPLIED WITH LIGHTNING STRIKE INSPECTION PROCEDURES, IAW EAC POLICIES AND PROCEDURES. TWO BURNED RIVETS WERE FOUND AT LOWER FUSELAGE BS 434 CENTERLINE, INCLUDING CIRCULAR BSDR Y2PA20130405016Skin · cracked.7500 INCH CRACK DISCOVERED ON THE WINDOW BELT DOUBLER AT STATION 238 BETWEEN LONGERONS 11L AND 12L. INSTALLED PERMANENT REPAIR IAW SERVICE REWORK DWG J060109 AND EA 96-51-02 R1.SDR EE4Y201303270045Frame · damagedAFT CARGO COMPARTMENT BS 889 BETWEEN L27 AND 28L FRAME WITH AN ELONGATE HOLE. REPAIRED IAW SRM 53-03 PARA 1C, FIG 2A.SDR EE4Y201303270042Shear Tie · crackedUPPER FUSELAGE, CARGO CABIN, AT BS 945 BETWEEN L15 TO 16R FRAME SHEAR TIE CRACKED. REPLACED SHEAR TIE IAW SRM 51-01, PARA 2D.SDR EE4Y201303270041Bulkhead · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 996 L23L AFT PRESSURE BULKHEAD WEB CORRODED. REPAIRED PRESSURE BULKHEAD WEB SECTION IAW SRM 53-03 PARA 17, FIG 23.SDR EE4Y201303270038Skin · dentedLOWER FUSELAGE BS 248.5 BETWEEN L19 AND 20L SKIN DENTED. REPAIRED SKIN IAW SRM 53-01, FIG 1.SDR EE4Y2013032700037Tee Fitting · crackedUPPER FUSELAGE AFT PRESSURE BULKHEAD TEE BETWEEN L15 AND 17L, AT Z=14 AND Z=24 TEE CRACKED. REPLACED PRESSURE BULKHEAD TEE SECTION IAW S/B A53-232 ACCOMPLISHMENT INSTRUCTIONS OPTION II CONDITION 2, FIG 4, REV 2, DATE APRIL 28,95.SDR EE4Y2013032700036Frame · crackedCARGO CABIN AT BS 813, L17R, FRAME WEB WITH CRACK. REPAIRED CARGO CABIN FRAME SECTION BS 813 BETWEEN L16 AND 18R DUE TO CRACK IAW SRM 53-03, FIG 32, PARA 26.SDR EE4Y2013032700035Fitting · crackedLOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 5, AFT BEAM END CRACKED. REPLACED NR 5 DOOR BEAM END FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRUCTIONS CONDITION 3, REV 3, DATE FEB 21,2008 AND DWG 5934142, REV H, DATED 12-21-06.
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