# Service difficulty reports: N729FD

A list on [N729FD](https://openairdocs.org/aircraft/N729FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 225 reports

- [SDR FDEA202512162258](https://openairdocs.org/sdr/FDEA202512162258.md): Actuator · failed · Dec 16, 2025 · N729FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > LOUD 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 SEQ
- [SDR FDEA202508021355](https://openairdocs.org/sdr/FDEA202508021355.md): Thermocouple · failed · Aug 2, 2025 · N729FD · Airbus A300B4622R · Engine Temperature Indicating System
  > AFTER 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 TWO
- [SDR FDEA202505290819](https://openairdocs.org/sdr/FDEA202505290819.md): Mechanism · fod · May 29, 2025 · N729FD · Airbus A300B4622R · Passenger/Crew Doors
  > L1 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, CLE
- [SDR FDEA202501280145](https://openairdocs.org/sdr/FDEA202501280145.md): Bottle · low pressure · Jan 28, 2025 · N729FD · Airbus A300B4622R · Emergency Equipment
  > ON 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 FDEA202501140069](https://openairdocs.org/sdr/FDEA202501140069.md): Bottle · low pressure · Jan 14, 2025 · N729FD · Airbus A300B4622R · Emergency Equipment
  > R1 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 FDEA202407120992](https://openairdocs.org/sdr/FDEA202407120992.md): Fitting · unknown · Jul 12, 2024 · N729FD · Airbus A300B4622R · Cargo/Baggage Doors
  > PERFORM 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-M
- [SDR FDEA202406200978](https://openairdocs.org/sdr/FDEA202406200978.md): Floor Panel · delaminated · Jun 20, 2024 · N729FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #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 FDEA202406200977](https://openairdocs.org/sdr/FDEA202406200977.md): Floor Panel · delaminated · Jun 20, 2024 · N729FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #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 6-2-100
- [SDR FDEA202406130798](https://openairdocs.org/sdr/FDEA202406130798.md): Elevator · none · Jun 13, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 REQUIREMENT
- [SDR FDEA202406050914](https://openairdocs.org/sdr/FDEA202406050914.md): Skin · dented · Jun 5, 2024 · N729FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > NOSE 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 5
- [SDR FDEA202406040806](https://openairdocs.org/sdr/FDEA202406040806.md): Floor Support · corroded · Jun 4, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MDCC 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 P
- [SDR FDEA202406030867](https://openairdocs.org/sdr/FDEA202406030867.md): Angle · cracked · Jun 3, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD 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 RE
- [SDR FDEA202405300757](https://openairdocs.org/sdr/FDEA202405300757.md): None · none · May 30, 2024 · N729FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT 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 RE
- [SDR FDEA202405290957](https://openairdocs.org/sdr/FDEA202405290957.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > L3 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 FDEA202405290956](https://openairdocs.org/sdr/FDEA202405290956.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > L3 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 S
- [SDR FDEA202405290955](https://openairdocs.org/sdr/FDEA202405290955.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > L6 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 31
- [SDR FDEA202405290954](https://openairdocs.org/sdr/FDEA202405290954.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > L6 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 31
- [SDR FDEA202405290953](https://openairdocs.org/sdr/FDEA202405290953.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > L4 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 ABX
- [SDR FDEA202405290951](https://openairdocs.org/sdr/FDEA202405290951.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R6 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 3
- [SDR FDEA202405290918](https://openairdocs.org/sdr/FDEA202405290918.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R3 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 FDEA202405290917](https://openairdocs.org/sdr/FDEA202405290917.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R3 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 ABX31.6
- [SDR FDEA202405290916](https://openairdocs.org/sdr/FDEA202405290916.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > R5 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 FDEA202405290915](https://openairdocs.org/sdr/FDEA202405290915.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R5 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 FDEA202405290913](https://openairdocs.org/sdr/FDEA202405290913.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R5 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 ABX17
- [SDR FDEA202405290897](https://openairdocs.org/sdr/FDEA202405290897.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R4 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 STA
- [SDR FDEA202405290896](https://openairdocs.org/sdr/FDEA202405290896.md): Rib · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Spoilers
  > R4 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 STA
- [SDR FDEA202405290865](https://openairdocs.org/sdr/FDEA202405290865.md): Seat Track · gouged · May 29, 2024 · N729FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.A
- [SDR FDEA202405290783](https://openairdocs.org/sdr/FDEA202405290783.md): Floor Support · corroded · May 29, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN 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, PA
- [SDR FDEA202405280879](https://openairdocs.org/sdr/FDEA202405280879.md): Skin · cracked · May 28, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > 3EA 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, TITL
- [SDR FDEA202405280878](https://openairdocs.org/sdr/FDEA202405280878.md): Skin · cracked · May 28, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA 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:WIN
- [SDR FDEA202405270866](https://openairdocs.org/sdr/FDEA202405270866.md): Strap · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FUSELAGE 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, PARA
- [SDR FDEA202405270777](https://openairdocs.org/sdr/FDEA202405270777.md): Floorbeam · none · May 27, 2024 · N729FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT 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 C
- [SDR FDEA202405270824](https://openairdocs.org/sdr/FDEA202405270824.md): Rib · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Wing, Control Surfaces
  > ONE 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 FDEA202405270823](https://openairdocs.org/sdr/FDEA202405270823.md): Rib · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA 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 FDEA202405270822](https://openairdocs.org/sdr/FDEA202405270822.md): Rib · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > ONE 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, REPAI
- [SDR FDEA202405270821](https://openairdocs.org/sdr/FDEA202405270821.md): Rib · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > ONE 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, REPAIR
- [SDR FDEA202405270814](https://openairdocs.org/sdr/FDEA202405270814.md): Plate · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD 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 FDEA202405270813](https://openairdocs.org/sdr/FDEA202405270813.md): Plate · cracked · May 27, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD 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, THE
- [SDR FDEA202405270789](https://openairdocs.org/sdr/FDEA202405270789.md): Floorbeam · none · May 27, 2024 · N729FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT 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 CF
- [SDR FDEA202405250908](https://openairdocs.org/sdr/FDEA202405250908.md): Skin · gouged · May 25, 2024 · N729FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH 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 DAM
- [SDR FDEA202405240973](https://openairdocs.org/sdr/FDEA202405240973.md): None · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 REQUIREMEN
- [SDR FDEA202405240848](https://openairdocs.org/sdr/FDEA202405240848.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT 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 REQUIREMEN
- [SDR FDEA202405240802](https://openairdocs.org/sdr/FDEA202405240802.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 FDEA202405240801](https://openairdocs.org/sdr/FDEA202405240801.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 FDEA202405240800](https://openairdocs.org/sdr/FDEA202405240800.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 RE
- [SDR FDEA202405240799](https://openairdocs.org/sdr/FDEA202405240799.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 REQUIREMENT
- [SDR FDEA202405240797](https://openairdocs.org/sdr/FDEA202405240797.md): Elevator · unknown · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 REQUIREM
- [SDR FDEA202405240796](https://openairdocs.org/sdr/FDEA202405240796.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 REQUIREME
- [SDR FDEA202405240795](https://openairdocs.org/sdr/FDEA202405240795.md): Elevator · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator Structure
  > AIRCRAFT 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 FDEA202405240774](https://openairdocs.org/sdr/FDEA202405240774.md): Skin · none · May 24, 2024 · N729FD · Airbus A300B4622R · Elevator, Plate/Skin
  > AIRCRAFT 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

Next page: https://openairdocs.org/aircraft/N729FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N729FD/reports

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