N729FD
Service difficulty reports · 225
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N729FD' AND registry_match = 'registration' 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 n_number = 'N729FD' AND registry_match = 'registration' 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 FDEA202512162258Actuator · failedLOUD THUD UPON GEAR EXTENSION COMING FROM NOSE WHEEL AND IT TOOK A LONG TIME FOR THE NOSE GEAR TO EXTEND AND THEN IT TOOK AN EVEN LONGER TIME FOR THE MAIN GEAR TO EXTEND WITH A THUD SOUND THEN ALL 3 WERE EVENTUALLY GREEN. (ABNORMALLY LONG, AND NOT IN SEQSDR FDEA202508021355Thermocouple · failedAFTER TAKEOFF, HAD FLUXING VIBRATION ON CLIMB OUT. MONITORED INSTRUMENTS AND NOTHING WAS OUT OF LIMITS. UPON REACHING APPROXIMATELY 18000, NOTICED ATS LEVERS KICKED OFF. FOLLOWED ECAM AND RESET. INFORMED GOC AND MOCC INFLIGHT. NOTICED EGT ON NUMBER TWOSDR FDEA202505290819Mechanism · fodL1 DOOR UNABLE TO BE ARMED. RELEASED FOR SERVICE PER MEL : 52-11-01-01 CREW ENTRY DOOR ESCAPE SLIDE L1 INOP. SLIDE REMAINS INSTALLED ON DOOR. MEL: 52-11-01-01 VERIFIED DOOR CLOSED AND LOCKED. OK TO CONTINUE. FOUND DEBRIS IN GRIT BAR FLOOR LATCH, CLESDR FDEA202501280145Bottle · low pressureON WALK-AROUND FOUND R1 ASSIST BOTTLE LOW. IAW AMM 52 10-14-03-10 SERVICED R1 DOOR ASSIST BOTTLE IAW AMM PRESSURE CHART. A/C OK FOR SERVICE.SDR FDEA202501140069Bottle · low pressureR1 ASSIST BOTTLE REQUIRES SERVICE. SERVICED R1 ASSIST BOTTLE TO PROPER PRESSURE PER IAW TEMP CHART. NO FURTHER DEFECTS, WORKED IAW 52-10-14-03-10.SDR FDEA202407120992Fitting · unknownPERFORM FR24 BEARING FITTING REPLACEMENT AT MAIN DECK CARGO DOOR FR24, LONGN1~3 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0379211 P1, SEQ NO:1252, TITLE:DOORS-CARGO DOOR/HYD SYS-MSDR FDEA202406200978Floor Panel · delaminatedTHE #162HF FLOOR PANEL OF BULK CARGO COMPARTMENT WAS FOUND SOFTEN FABRICATED NEW FLOOR PANEL 162HF FR67~FR69, -Y46.7~-Y805 I.A.W FEDEX STANDARD REPAIR DRAWING SRZ-25-005 & SRZ-25-011. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202406200977Floor Panel · delaminatedTHE #161GF FLOOR PANEL OF BULK CARGO COMPARTMENT WAS FOUND SOFTEN FABRICATED NEW FLOOR PANEL 161GF FR69~FR70, -Y307~Y1304 I.A.W FEDEX STANDARD REPAIR DRAWING SRZ-25-005 & SRZ-25-011. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR FDEA202406130798Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 33", T/E-26.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202406050914Skin · dentedNOSE FUSELAGE LOWER SKIN PANEL GOT A DENT BETWEEN FR4~5, 7 O'CLOCK POSITION. ACCOMPLISHED THE DOUBLER REPAIR AT NOSE FUSELAGE LOWER SKIN PANEL BETWEEN FR4~5, 7 O'CLOCK I.A.W A300-600 SRM 53-11-12-201, PARA 5A , PAGE 203-210 FIG 201, SRI 53-11-12-201, IIR 5SDR FDEA202406040806Floor Support · corrodedMDCC FLOOR STRUCTURE SUPPORT LOWER SURFACE WAS FOUND CORROSION AT FR12A PLUS 5", Y953. INSTALLED THE NEW FLOOR SUPPORT AT MAIN DECK FR11~15A Y953 I.A.W A300-600 SRM 51-72-10- 001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~50, THE REPAIR CLASSIFIED AS MINOR PSDR FDEA202406030867Angle · crackedFWD CARGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L,FR26 POSITION. INSTALLED THE NEW PLATE ANGLE WITH FASTENERS AT UNDER FWD CARGO FLOOR AREA FR26 S-43L~44L I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B-23, THE RESDR FDEA202405300757None · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RUDDER RH PANEL SKIN AT FASTENER #20 COUNTED FROM BELOW COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PTI, TITLE: STRUCTURES- REPAIR CATALOG -A300/A310 REPAIR IDENTIFICATION & TRACKING RESDR FDEA202405290957Rib · gougedL3 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379359 P1, SEQ NO:001239, WRI: 57409742, TITLE: WINGS- ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT STA ABX 31.SDR FDEA202405290956Rib · gougedL3 SPOILER O/B JACK RIB UPPER & LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379359 P1, SEQ NO:001239, WRI: 57409742, TITLE: WINGS- ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT SSDR FDEA202405290955Rib · gougedL6 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #6 SPOILER O/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379363 P1, SEQ NO:001241, WRI: 57409744, TITLE: WINGS- ATTACH FITTINGS-LH WING #6 SPOILER JACK RIB AT STA SP1X 31SDR FDEA202405290954Rib · gougedL6 SPOILER I/B JACK RIB UPPER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #6 SPOILER I/B JACK RIB I.A.W FEDEX EA T6- 5740-T0379363 P1, SEQ NO:001241, WRI: 57409744, TITLE: WINGS- ATTACH FITTINGS-LH WING #6 SPOILER JACK RIB AT STA SP1X 31SDR FDEA202405290953Rib · gougedL4 SPOILER O/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT LH #4 SPOILER O/B JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379361 P1, SEQ NO:001240, WRI: 57409743, TITLE: WINGS- ATTACH FITTINGS-LH WING #4 SPOILER JACK RIB AT STA ABXSDR FDEA202405290951Rib · gougedR6 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #6 SPOILER JACK RIB I.A.W FEDEX EA NO: T6- 5740-T0379403 P1, SEQ NO:001245, WRI: 57409748, TITLE: WINGS- ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X 3SDR FDEA202405290918Rib · gougedR3 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0379398 P1, SEQ NO:001242, WRI:57409745, TITLE:WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX31.SDR FDEA202405290917Rib · gougedR3 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0379398 P1, SEQ NO:001242, WRI:57409745, TITLE:WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX31.6SDR FDEA202405290916Rib · gougedR5 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0379407 P1, SEQ NO:001244 WRI:57409747, TITLE: WINGS-ATTACH FITTINGS-RH WING#5 SPOILER JACK RIB AT STA ABX175.SDR FDEA202405290915Rib · gougedR5 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0379407 P1, SEQ NO:001244, WRI:57409747, TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIBS AT STA ABX SDR FDEA202405290913Rib · gougedR5 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0379407 P1, SEQ NO:001244, WRI:57409747, TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX17SDR FDEA202405290897Rib · gougedR4 SPOILER O/B JACK RIB UPPER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH WING #4 SPOILER JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379401 A P1, SEQ NO:001243, WRI: 57409746, TITLE: WINGS- ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STASDR FDEA202405290896Rib · gougedR4 SPOILER I/B JACK RIB LOWER BOLT HOLE FOUND GOUGE. ACCOMPLISHED THE REINFORCING REPAIR AT RH WING #4 SPOILER JACK RIB I.A.W FEDEX EA NO: T6-5740-T0379401 A P1, SEQ NO:001243, WRI: 57409746, TITLE: WINGS- ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STASDR FDEA202405290865Seat Track · gougedMAIN DECK FLOOR SEAT TRACK CROWN WAS FOUND GOUGE AT FR58 PLUS 1",-Y1950 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR FR57.3~FR59, -Y1950 I.A.W A300-600 SRM 53-10-16-201,PARA.10, PAGE.243~248, FIG.208(SHEET-1), THE REPAIR CLASSIFIED AS CAT.ASDR FDEA202405290783Floor Support · corrodedMAIN DECK FLOOR STRUCTURE SUPPORT UPPER SURFACE WAS FOUND CORROSION AT FR11 PLUS14"~FR11 PLUS 16", Y730 REPLACED THE DAMAGE SUPPORT WITH NEW AT MAIN DECK FLOOR STRUCTURE SUPPORT SURFACE FR11 PLUS 14" ~FR11 PLUS 16", Y730 I.A.W A300-600 SRM 51-72-10-001, PASDR FDEA202405280879Skin · cracked3EA CRACKS (5MM&8MM&12MM) WERE FOUND AT L/H WING CENTER FLAP RIB26 OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB26 S-2.6~R/S AND DOUBLER REPAIR AT RIB26~27 S- 2.3~R/S LH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379330 P1, SEQ NO:1249, TITLSDR FDEA202405280878Skin · cracked1EA CRACK (15MM) WAS FOUND AT L/H WING CENTER FLAP RIB17 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED FLANGE REPAIR AT RIB17 S-2.8~R/S AND DOUBLER REPAIR AT RIB17~18 S-2.1~R/S LH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379330 P1, SEQ NO:1249, TITLE:WINSDR FDEA202405270866Strap · crackedFUSELAGE STRUCTURAL S-33R WEB FOUND STRAP CRACK AT FR85 PLUS 10" AREA. REPLACED THE CRACK STRAP WITH NEW PART. LOCATE AT FUSELAGE FR85 PLUS 10" S-33R WEB. I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE,7B~PAGE,23 AND 51-40-21- 001, PARASDR FDEA202405270777Floorbeam · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON FWD CGO COMPT CROSSBEAM AT FR38.2, Y805 TO -Y805 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202405270824Rib · crackedONE CRACK (10MM) WAS FOUND AT R/H WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB20 S-2.7~2.8 AND DOUBLER REPAIR AT RIB19-20 S2.1R, RT CENTER FLAP IAW EA T6-5750-T0379321 P1, REPAIR CLASSIFIED AS MAJOR CAT.A PER SDR FDEA202405270823Rib · cracked1EA CRACK (10MM) WAS FOUND AT R/H WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB20 S-2.7~2.8 AND DOUBLER REPAIR AT RIB19~20 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, TITLE:SDR FDEA202405270822Rib · crackedONE CRACK (8MM) WAS FOUND AT R/H WING CENTER FLAP RIB17 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB17 S-2.8~R/S AND DOUBLER REPAIR AT RIB17~18 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, REPAISDR FDEA202405270821Rib · crackedONE CRACK (8MM) WAS FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB11 S-2.8~R/S AND DOUBLER REPAIR AT RIB11~12 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, REPAIRSDR FDEA202405270814Plate · crackedFWD CARGO COMP'T UNDER FLOOR AREA LH SIDE PLATE SHEAR CRACK AT S-43L~S-44L,FR38.1- FR38.2 POSITION INSTALLED THE NEW PLATE WITH FASTENERS AT FWD CARGO FLOOR AREA FR38.1~38.2 S- 43L~44L I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001,PARA.6-7, PAGE.7B-SDR FDEA202405270813Plate · crackedFWD CARGO COMP'T UNDER FLOOR AREA RH SIDE PLATE SHEAR CRACK AT S-43R~S-44R,FR36- FR37 POSITION INSTALLED THE NEW PLATE WITH FASTENERS AT FWD CARGO FLOOR AREA FR36~37 S-43R~44R I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6-7, PAGE.7B-50, THESDR FDEA202405270789Floorbeam · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON AFT CGO COMPT CROSSBEAM AT FR63, -Y140 TO -Y805 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFSDR FDEA202405250908Skin · gougedLH INNER FLAP UPPER FACE GOUGE AT FRONT SPAR PLUS 13.5", RIB8A-1" ACCOMPLISHED THE DOUBLER REPAIR AT LH I/B FLAP UPPER SURFACE RIB7~9, S-2.1~2.2 I.A.W FEDEX EA NO:T6-5750-T0379379 P1, SEQ NO:1250, TITLE:WING-FLIGHT SURFACES-LH INNER FLAP- DENT AND WEAR DAMSDR FDEA202405240973None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 PLUS 6", T/E-8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENSDR FDEA202405240848Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 PLUS 6", T/E-8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENSDR FDEA202405240802Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER10 10", L/E 2.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR FDEA202405240801Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13-19", T/E-25" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR FDEA202405240800Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER10 PLUS 25", L/E PLUS 2.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING RESDR FDEA202405240799Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER10-18.5", T/E-38" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202405240797Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 PLUS 27", T/E-22" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMSDR FDEA202405240796Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER10 PLUS 4", T/E-27" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMESDR FDEA202405240795Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 6", T/E-8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR FDEA202405240774Skin · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER6~7, T/E-39" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
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