Cameron Balloons U S A-300
Service difficulty reports · 3,457
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 = 'A300' 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 = 'A300' 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 FDEA202308031380Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 9~10,REAR SPAR DATUM 12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRSDR FDEA202308031378Support · damagedAFT CGO CMPTR RH FR59A FOUND 1EA WIRE CONDUIT SUPPORT BROKEN REMOVED BROKEN WIRE CONDUIT SUPPORT, AND INSTALLED NEW ONE. I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND 51-40-21-001, PARA.13, PAGE.149-156SDR FDEA202308021855Trunnion · unknownRIB 5 FWD GEAR TRUNION PINTLE HAS HEAVY PITTINGIN BETWEEN BEARING HALFSAT 2:00 TO 3:00 OCLOCK POSITIONS. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425SDR FDEA202308021345Transmitter · failedAROUND 45 MIN INTO CRUISE FLIGHT WE NOTICED THE GREEN HYD REVISOR QUANTITY DECREASING. SHORTLY AFTER WE RECEIVED AN ECAM - GREEN RSVR LO LEVEL. COMPLIED WITH ECAM AND ASSOCIATED PROC S. LANDING GEAR WAS MANUALLY EXTENDED. UNEVENTFUL LANDING KMEM 36C. EMSDR FDEA202308011488Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR 19~20, STGR 52~54L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202308011379Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR 27, BTW STGR 32~34R COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.SDR FDEA202307301575Fitting · crackedTHE MDC DOOR ACTUATOR YOKE BOTH SUPPORT FRAME WERE FOUND CRACK & BROKEN FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO:T6- 5230-T0375508 P1, SEQ NO:857, TITLE:DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARING FITTINSDR FDEA202307301414Fitting · crackedAVIONICS COMP'T ACCESS DOOR STOP OMEGA FITTING CRACK. REPLACED FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-PAGE.23SDR FDEA202307301335Valve · failedAPPROACHING RWY23R KTYS FOR TAKEOFF, INDICATING SMOKE IN COURIER AREA. STOPPED ACFT. CONFIRMED SMOKE IN COURIER AREA. NO SMOKE IN COCKPIT. DECLARED EMERGENCY WITH KTYS TOWER. CONDUCTED EMERG EVAC, EXITING VIA L1 SLIDE. PERCEIVED SMOKE COMING FROM VENTS OVESDR FDEA202307271315Unknown · unknownLEFT HAND PYLON - FOUND EXISTING REPAIR AT LOWER SPAR BETWEEN RIB 9 AND RIB 10 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA. THE EXISTING REPAIR ON LT PYLON LOWER SPAR BETWEEN RIB 9 & RIB 10 WAS EVALUATED & FOUND IN CONFORMITY WITH DWG: 41R54600029 SDR FDEA202307261304Pressure Deck · corrodedBAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION AT Y2462 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, Y2462 PER A300-600 SRM51-40-21 AND EA:6-5310-T0375709 PSDR FDEA202307261303Pressure Deck · unknownBAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION BETWEEN -Y450 AND -Y953 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, -Y450~-Y953 PER A300-600 SRM51-40-21 ANDSDR FDEA202307261302Fitting · crackedINSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH FOUND CRACK SIGNAL IN THE UPR SECOND CRACK STOP HOLE REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH PER A300-600 SRM 51-40-21 & EA: 6-5710-161345 SDR FDEA202307261301Fitting · crackedINSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH FOUND CRACK SIGNAL REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH PER A300-600 SRM51-40-21 & EA:6-5710-T0375488 P1. REPAIR IS CAT A REPAIR.MAJOR RSDR FDEA202307261300Unknown · unknownFWD CARGO DOOR ACTUATOR ATTACH FITTING AT FR22A FOUND CRACKSDR FDEA202307261299Floorbeam · crackedAFT CARGO FLOOR CROSSBEAM FOUND CORROSION AT FR62, -Y140 ~ -Y805. REPAIRED THE AFT CARGO CORRODED FLOOR CROSSBEAM AT FR62 -Y140 ~ -Y805 PER A300-600 SRM 53-10-15 PARA.9. THIS IS CAT.A REPAIR . MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202307261298Door · crackedRH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPAIRED THE CRACKED FRAME SEGMENT OF RH FWD PAX DOOR AT FR14C PER A300-600 SRM51-40-21 AND AIRBUS DRAWING F52181297 ISSUE: K & F52181299 ISSUE: A. THIS IS CAT A REPAIR. TRACKING EA:6-5210-T0375409 SDR FDEA202307261297Frame · crackedRH AFT PAX DOOR FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH FOUND 1EA CRACK. REPAIRED RH AFT PAX DOOR CRACKED FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH PER SRM51-40-21 & EA 6-5310-T0375247 P1.TITLE:FUSELAGE - MAINFRAME - CRACK FOUND ON RH DOOR FRAME FSDR FDEA202307191287Spoiler · unknownAIRCRAFT REPAIR ASSESSMENT EXISTING REPAIR FOUND ON LH #3 SPOILER CENTER HINGE ARM COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OFSDR FDEA202307191286Spoiler · unknownAGING AIRCRAFT ASSESSMENT : EXISTING REPAIR FOUND ON LH #3 SPOILER CENTER HINGE ARM COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTIONSDR FDEA202307191278Seat Track · unknownTHE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR74 - FR75, -Y1137.1 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM SUPPLEMENT 53-10-16 FIG.202. EO 6-5100-7-5000 D7 PT1 WAS COMPLETED, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDSDR FDEA202307121743Fitting · failedCORROSION FOUND IN THE RIB 5 FITTING. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425SDR FDEA202307111275Profile · crackedMAIN DECK FLOOR STRUCTURE PROFILE-Z FOUND CRACK NEAR FR 79 PLUS 5",Y1650 REPLACED WITH NEW PROFILE-Z I.A.W A300-600F SRM 51-72-10-001, PAGE 2.SDR FDEA202307101279Seat Track · wornFR54/FR54.2 LH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM ACTUAL MEASUREMENT:1.143MM. IAW SRM 53-15-16 PARA 5A PAGE 201- PAGE210 FIG.201 PERFORM REPAIR ACCOMPLISHED. MAJOR REPAIRSDR FDEA202307081187Actuator · failedPDIS 687 52-30 5349 08JUL23 MEM OPEN U UPON ARRIVAL IN MEMPHIS. BLOCKED AT GATE.GROUND CREW ADVISED MAIN CARGO DOOR LOCKS WERE OPEN ALONG WITH MAIN HANDLE.NO INDICATIONS IN COCKPIT ECAM DOOR PAGE .UPON VISUAL INSPECTION FOUND LATCHES AND DOORSDR FDEA202307081184Computer · failedCABIN PRESSURE MANUAL CONTROL. BOTH REGULATORS FAULTED. OPERATED IN MANUAL CONTROL. FOUND BOX LIGHT ILLUMINATED WITH A CODE 70 WHILE TESTING BOX .REMOVED AND REPLACED PDPU 54GB AND TEST OK PER ABOVE REF. PRESSURE CONTROLLERS BOTH TEST OK REF TSM 21-30-00. ASDR FDEA202307071281Seat Track · corrodedMAIN DECK DUMMY SEAT TRACK WAS BULGING AT -Y1456 FR54.1 AREA. REPLACED THE DUMMY SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B-50SDR FDEA202307071176Unknown · unknownPDIS 661 29-01 5576 30JUN23 MEM FACT U GREEN RESERVOIR OVERHEAT WARNING DURING CLIMB OUT. FOLLOWED THE ECAM AND QRH PROCEDURES. GRAVITY EXTENDED GEAR AND NO NOSE WHEEL STEERING AS A RESULT. OVERSPEED THE KRUGER FLAP AS A RESULT OF BEING ABOSDR FDEA202307061280Seat Track · corrodedMAIN DECK FLOOR STRUCTURE DUMMY SEAT TRACK FOUND CORROSION AT FR 54.1 , Y-450 REPLACED DUMMY SEAT TRACK WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, P2.SDR FDEA202307061183Unknown · unknownAIRCRAFT STRIKE. FUSELAGE DAMAGE AFT OF RADOME. COMPLIED WITH EA # 6-5310-T0375157 PART 1 & 2 FUSELAGE MAINFRAME FRAME 0-FRAME 1/ LOWER FUSELAGE SKIN AT 6 O'CLOCK POSITION STRUCTURALE REPAIR FOR DENT/CREASE TO FRAME AND SKIN.SDR FDEA202307051147Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24L - S25L REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24L - S25L PER FEDEX EA: #: 6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH&RH DOOR FRASDR FDEA202307051146Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24R - S25R REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24R - S25R PER FEDEX EA:#:6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH &RH DOOR FRSDR FDEA202307041221Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB FOUND CRACK NEAR FR79 PLUS 5",Y1650 REPLACED THE CRACKED SHEAR WEB WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, PAGE2.SDR FDEA202307041220Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB FOUND CRACK NEAR FR79 PLUS 5", Y-1650 REPLACED THE CRACKED SHEAR WEB WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, PAGE2.SDR FDEA202307031142Spoiler · delaminatedRH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1): 50MM*20MM, DEPTH: 1.60MM (2): 10MM*15MM DEPTH:2.3MM PERFORMED THE REPAIR ON RH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARMSDR FDEA202307031141Spoiler · delaminatedRH WING #3 SPOILER INBD HINGE ARM INBD SURFACE FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.70MM PERFORMED THE REPAIR ON RH WING #3 SPOILER INBD HINGE ARM INBD SURFACE PER FEDEX EA # 6-5750-T0374955 TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HINSDR FDEA202306301224Web · crackedLH WING T/E CAVITY TOP SKIN PNL SUPPORT WEB CRACK AT SPOILER#5 HINGE ARM REPLACED THE CRACK SUPPORT WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE2SDR FDEA197706301134Unknown · unknownGREEN RESERVOIR OVERHEAT WARNING DURING CLIMB OUT. FOLLOWED ECAM & QRH PROCEDURES. GRAVITY EXTENDED GEAR & NO NOSE WHEEL STEERING AS A RESULT. OVERSPEED KRUGER FLAP AS A RESULT OF BEING ABOVE 300 & .65 MACH AT THE TIME OF FAILURE. KRUGER FLAP WAS OVERSPESDR FDEA202306291226Floor Panel · damagedCATWALK FLOOR PANEL SOFT AT FR87-FR88 FABRICATED THE NEW FLOOR PANEL I.A.W FEDEX STANDARD REPAIR DRAWING NO:SRZ-25-005 "MAJOR REPAIR"SDR FDEA202306271276Adapter · wornAFT MAIN DECK COMPT FOUND 1EA CLS ADAPTER-FLANGE AREA WORN LOCATION AT FR68, BETWEEN Y-1378 AND Y-1778 DAMAGED CLS ADAPTER REPLACED NEW PART, INSTALLED WITH HI-LOK I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND 51-40-21-001, PARA.7, PAGE.24 - PAGE.50SDR FDEA202306271273Support · crackedCENTER MAIN DECK COMPT - LH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR38.1 TO FR38.2 COMMON TO Y2462. REPLACED THE NEW SUPPORT I.A.W A300-600F SRM 51-72-10-001,P2 AND SRM 51-40-21-001 PARA,7,PAGE 24~PAGE 50SDR FDEA202306271225Profile · crackedAFT MAIN DECK UTILITY AREA FOUND 1EA Z-PROFILE CRACKED AT FR80 AND -Y1470 POSITION REPLACED THE NEW PROFILE-Z. I.A.W A300-600F SRM 51-72-10-001, P2SDR FDEA202306271223Support · crackedCENTER MAIN DECK COMPT - RH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR38.1 TO FR38.2 COMMON TO -Y2462 REPLACED THE NEW SUPPORT. I.A.W A300-600F SRM 51-72-10-001,P2SDR FDEA202306271222Support · crackedCENTER MAIN DECK COMPT - RH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR37 TO FR38 COMMON TO -Y2462 REPLACED THE NEW SUPPORT. I.A.W A300-600F SRM 51-72-10-001,P2SDR FDEA202306271215Aileron · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON UPR & LWR SKIN AT RIB 13,T/E COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202306271180Flap · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 19~21, REAR SPAR DATUM 7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRSDR FDEA202306261219Crossbeam · unknownEXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 66 BTW - Y953 ~ -Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPASDR FDEA202306261197Flap · dentedRH WING CENTER FLAP NOSE FOUND 1EA DENT AT RIB19 PLUS 3" AREA PFM NOSE SKIN FLUSH REPAIR BY SKIN INSERT AND BUTTSTRAP WITH RIVETS, THIS IS CAT B REPAIR. I.A.W A300-600F SRM 57-50-00-201 FIG.208, PAGE.231-236 AND SRI:57-50-00-201, IIR:57-50- 00-2-002-00, PARSDR FDEA202306261192Support · corrodedFWD MAIN DECK UTILITY AREA - FLOOR SUPPORT GOT CORROSION LOCATION FROM FR13A TO FR14 COMMON TO Y730 REPLACED THE CORRODED SUPPORT WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B-PAGE 23.SDR FDEA202306261165Seat Track · unknownAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 75~76, -Y1221.2 TO -Y1623.6 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 1
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