# Service difficulty reports: N751FD

A list on [N751FD](https://openairdocs.org/aircraft/N751FD.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 7 · 308 reports

- [SDR FDEA202602100164](https://openairdocs.org/sdr/FDEA202602100164.md): Cable · incorrect · Feb 10, 2026 · N751FD · Airbus A300B4622R · Escape Slide
  > DURING INSPECTION OF THE L1 DOOR SLIDE (PN: D30546-509, SN: C1384) FOUND THE BREAKAWAY WIRE ON THE RELEASE CABLE INCORRECT. CMM: 25-61-39 REPLACED THE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 REFERENCE FEA: 6-2560-F0386261 REV A P1 AND CMM 25
- [SDR FDEA202512192262](https://openairdocs.org/sdr/FDEA202512192262.md): Battery Pack · inoperative · Dec 19, 2025 · N751FD · Airbus A300B4622R · Emergency Lighting
  > DURING POST FLIGHT NONE OF THE EMEGENCY LIGHTING WILL TEST. REMOVED AND REPLACED BATTERY FOR POWER SUPPLY 29WL, ALL EMERGENCY LIGHTING OPS CHECKED GOOD, REF AMM 33-51-14-04. OK TO CONTINUE SERVICE.
- [SDR FDEA202509041616](https://openairdocs.org/sdr/FDEA202509041616.md): Pitot Tube · clogged · Sep 4, 2025 · N751FD · Airbus A300B4622R · Pitot/Static System
  > ON TAKEOFF ROLL, CAPTAIN S AIRSPEED SHOWED 95 KTS WHILE FO SIDE SHOWED 60 KTS. TAKEOFF REJECTED. PERFORMED FLIGHT ENVIRONMENT DATA BITE TEST PER A300 AMM 34-10-00-05, TEST PASSED, NO FAULTS NOTED. PERFORMED VISUAL INSPECTION OF F/O PITOT TUBE PER A300 AMM
- [SDR FDEA202506261054](https://openairdocs.org/sdr/FDEA202506261054.md): Hydraulic Line · damaged · Jun 26, 2025 · N751FD · Airbus A300B4622R · Hydraulic System, Main
  > DURING CLIMB OUT OF KMEM GOT ECAM YELLOW HYD SYS LO PRESSURE. THE YELLOW RESERVOIR SHOWED ZERO QUANTITY. COMPLETED THE ECAM AND QRH PROCEDURES. CONSULTED GOC, AND THEY HAD US CONTINUE TO KMSN. COMPLETED THE FLIGHT. FOUND YELLOW SYS PRESSURE FLEX LINE TO LH AI
- [SDR FDEA202404050466](https://openairdocs.org/sdr/FDEA202404050466.md): Web · bent · Apr 5, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > THSA COMPARTMENT FOUND 1EA SUPPORT WEB GOT DEFORM AT FR85-86, S-33R REPLACED THE DAMAGED SUPPORT WEB WITH NEW ONE. I.A.W A300-600 SRM 51-72-01-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT FR85~86, S-33R.
- [SDR FDEA202404040291](https://openairdocs.org/sdr/FDEA202404040291.md): Rib · cracked · Apr 4, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > PFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB 19 BTWN REAR SPAR ~ STRG 2.8. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-57
- [SDR FDEA202404040479](https://openairdocs.org/sdr/FDEA202404040479.md): Skin · cracked · Apr 4, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > PFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB19 BTWN REAR SPAR ~ STRG2.8. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-
- [SDR FDEA202403190293](https://openairdocs.org/sdr/FDEA202403190293.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0
- [SDR FDEA202403190292](https://openairdocs.org/sdr/FDEA202403190292.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W
- [SDR FDEA202403190290](https://openairdocs.org/sdr/FDEA202403190290.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613
- [SDR FDEA202403190289](https://openairdocs.org/sdr/FDEA202403190289.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT S
- [SDR FDEA202403190288](https://openairdocs.org/sdr/FDEA202403190288.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W
- [SDR FDEA202403190287](https://openairdocs.org/sdr/FDEA202403190287.md): Rib · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE: WINGS-FLIGHT SURFACES-RH CENTER FLAP; C
- [SDR FDEA202403190481](https://openairdocs.org/sdr/FDEA202403190481.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS-FLIGHT SURFACES-RH CENTER FLAP;
- [SDR FDEA202403190480](https://openairdocs.org/sdr/FDEA202403190480.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT SU
- [SDR FDEA202403190478](https://openairdocs.org/sdr/FDEA202403190478.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0
- [SDR FDEA202403190477](https://openairdocs.org/sdr/FDEA202403190477.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W F
- [SDR FDEA202403190476](https://openairdocs.org/sdr/FDEA202403190476.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613
- [SDR FDEA202403190475](https://openairdocs.org/sdr/FDEA202403190475.md): Skin · cracked · Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W
- [SDR FDEA202403150438](https://openairdocs.org/sdr/FDEA202403150438.md): Rib · gouged · Mar 15, 2024 · N751FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > LH WING SPOILER #6 ACTUATOR INBD JACK RIB LOWER HOLE GOUGE ACCOMPLISHED THE CAT.A REINFORCEMENT REPAIR AT LH WING #6 SPOILER JACK RIB STA SP1X 31.675, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5740- T0378536 P1, SEQ NO:1164, TITLE
- [SDR FDEA202403140339](https://openairdocs.org/sdr/FDEA202403140339.md): None · none · Mar 14, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > 00087567N00574 AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON AFT CGO FLOOR PNL 152FF TOP SIDE BTW FR56~57.1, -Y805 TO -Y1470 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTI
- [SDR FDEA202403140324](https://openairdocs.org/sdr/FDEA202403140324.md): Floor Panel · none · Mar 14, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING COMPOSITE REPAIR FOUND ON AFT CGO FLOOR PNL 152EF TOP SIDE BTW FR56~57, -Y140 TO -Y805 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA: A300-600 SRM 53-10-20
- [SDR FDEA202403130420](https://openairdocs.org/sdr/FDEA202403130420.md): Adapter · gouged · Mar 13, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE FOUND 1EA CLS T-ADAPTER GOT SOME GOUGED MARKS LOCATION AT FR61, Y1456 THRU Y1959 REPLACED THE DAMAGED ADAPTER WITH NEW ONE.I.A.W A300-600 SRM 51-72-10-001, PAGE2 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 (AT FR61, Y1456 TO Y1959
- [SDR FDEA202403120422](https://openairdocs.org/sdr/FDEA202403120422.md): None · none · Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON STRINGER BTW FR57.2~57.3, S-35L 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,
- [SDR FDEA202403120418](https://openairdocs.org/sdr/FDEA202403120418.md): Adapter · gouged · Mar 12, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR ADAPTER GOUGE 2EA AT FR62 -Y700 AND -Y875 REPLACED THE GOUGE ADAPTER WITH NEW PART. AT MAIN DECK FLOOR FR62 -Y700 AND -Y875. I.A.W A300-600 SRM 51-72-10-001 PAGE2 & 51-40-21-001 PARA7 PAGE24~PAGE50. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-1
- [SDR FDEA202403120360](https://openairdocs.org/sdr/FDEA202403120360.md): None · none · Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR63-64, S-49L. 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,
- [SDR FDEA202403120344](https://openairdocs.org/sdr/FDEA202403120344.md): None · none · Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > 00087567N00360 AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON FWD CARGO COMPT FLOOR CROSSBEAM BTW Y805 TO -Y805, FR38.2 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION
- [SDR FDEA202403110278](https://openairdocs.org/sdr/FDEA202403110278.md): Support Frame · cracked · Mar 11, 2024 · N751FD · Airbus A300B4622R · Cargo/Baggage Doors
  > THE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK AT FR23 FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO: T6- 5230-T0378435 P1, SEQ NO:1175 TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ALTUATOR BEARING FITTING REPL
- [SDR FDEA202403110340](https://openairdocs.org/sdr/FDEA202403110340.md): None · none · Mar 11, 2024 · N751FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR62- 64, S-48L 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, I
- [SDR FDEA202403100421](https://openairdocs.org/sdr/FDEA202403100421.md): Support Angle · corroded · Mar 10, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD CGO COMP'T UNDER ROLLER TRACK SUPPORT ANGLE TOP SKIN CORRODED AT FR31-FR32, S-43L POSITION. REMOVED DAMAGE ANGLE AND INSTALLED NEW ONE. IAW A300-600 SRM 51-40-21-001, PARA.6 PAGE 7B-PAGE23 & 51-72-10-001, PAGE2. THIS REPAIR CLASSIFIED AS MINOR PER GMM
- [SDR FDEA202403090419](https://openairdocs.org/sdr/FDEA202403090419.md): Floor Support · corroded · Mar 9, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK COURIER AREA FOUND 1EA FLOOR SUPPORT CORRODED POSITION AROUND SEVERAL OF ATTACHMENT HOLES LOCATION FROM FR11 TO FR15A AND Y953 ACCOMPLISHED THE REPLACEMENT OF FLOOR SUPPORT AT FR11 TO FR15A AND Y953, REPAIR CLASSIFIFED AS MINOR PER GMM 6-2-100 I.
- [SDR FDEA202403080417](https://openairdocs.org/sdr/FDEA202403080417.md): Beam · corroded · Mar 8, 2024 · N751FD · Airbus A300B4622R · Fuselage Main, Structure
  > REAR FUSELAGE L/H HORIZONTAL STAB CUTOUT EDGE BEAM GOT A PROFILE CORRODED AT FR89 PLUS 8", S-27L REPLACED THE DAMAGED BEAM WITH NEW ONE. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND 51-40-21-001 PARA7 P24-P50 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 ( A
- [SDR FDEA202403060463](https://openairdocs.org/sdr/FDEA202403060463.md): Plate · cracked · Mar 6, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD CGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L AND FR21 POSITION. REPLACED THE SIDE PLATE WITH NEW PART AT FR21 AND S-43L~44L, REPAIR CLASSIFIED AS MINOR REPAIR IAW SRM 51-72-10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B~50
- [SDR FDEA202403060412](https://openairdocs.org/sdr/FDEA202403060412.md): Floor Support · corroded · Mar 6, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > BULK CGO COMP'T FLOOR BEAM TOP SKIN CORROSION BTW FR66-FR68,Y140 POSITION. REPLACED THE NEW PROFILE, LONGITUDINAL BTW FR66~FR68, Y140. I.A.W A300-600 SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100
- [SDR FDEA202403040411](https://openairdocs.org/sdr/FDEA202403040411.md): Header · bent · Mar 4, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > AFT CGO COMP'T CEILING PNL SUPPOPRT DEFORM AT ENTRY AREA BTWFR60-FR61 POSITION. REPLACED THE DEFORM CEILING PNL SUPPORT WITH NEW PART. AT AFT CGO COMPONENT CEILING PANEL. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. I.A.W A300-600 SRM 51-72-10-001 PAGE2
- [SDR FDEA202403030434](https://openairdocs.org/sdr/FDEA202403030434.md): Floor Support · cracked · Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR ONE SUPPORT CRACK NEAR FR38.1 PLUS 5" STGR26R. REPLACED THE NEW SUPPORT. I.A.W A300-600 SRM 51-72-10-001,P2 NEAR FR38.1 PLUS 5" STGR 26R. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.
- [SDR FDEA202403030414](https://openairdocs.org/sdr/FDEA202403030414.md): Adapter · gouged · Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR ADAPTER GOUGE AT FR64 -Y1456 TO -Y1959 REPLACED THE DAMAGED ADAPTER WITH NEW ONE.I.A.W A300-600 SRM 51-72-10-001, PAGE2 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 (AT FR64, Y1456 TO -Y1959)
- [SDR FDEA202403030413](https://openairdocs.org/sdr/FDEA202403030413.md): Shear Web · damaged · Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB BROKEN AT FR79 5" Y1630 REPLACED THE NEW PLATE, SHEAR. I.A.W A300-600 SRM 51-72-10-001,P2 NEAR FR79 5" Y1630. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.
- [SDR FDEA202403030252](https://openairdocs.org/sdr/FDEA202403030252.md): Profile · cracked · Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR Z-PROFILE CRACK AT FR80/82 -Y1480 REPLACED THE NEW PROFILE-Z AT FR80/82 -Y1480.I.A.W A300-600 SRM 51-72-10-001,P2, THIS REPAIR CLASSIFIED AS MINOR PER GMM06-2-100
- [SDR FDEA202403030251](https://openairdocs.org/sdr/FDEA202403030251.md): Profile · cracked · Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR Z-PROFILE CRACK AT FR80/82 Y1480 [TS3RJ00C7E0U] REPLACED THE NEW PROFILE-Z AT FR80/82 Y1480.I.A.W A300-600 SRM 51-72-10-001, P2, THIS REPAIR CLASSIFIED AS MINOR PER GMM06-2-100
- [SDR FDEA202402290277](https://openairdocs.org/sdr/FDEA202402290277.md): Support Frame · cracked · Feb 29, 2024 · N751FD · Airbus A300B4622R · Cargo/Baggage Doors
  > THE MDC DOOR ACTUATOR YOKE AFT SUPPORT FRAME WAS FOUND CRACK FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO: T6- 5230-T0378435 P1, SEQ NO:1175 TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ALTUATOR BEARING FITTING REPLACEMENT
- [SDR FDEA202305080824](https://openairdocs.org/sdr/FDEA202305080824.md): Structure · damaged · May 8, 2023 · N751FD · Airbus A300* · Standard Practices/Structures
  > DURING ULTRASONIC INSPECTION IAW A300 NTM 57-0-45 PT 4. PROCEDURE A R/H LOWER WING BOX HOLE #1 CRACKED ON THE FWD SIDE OF THE FASTENER APPROXIMATELY 1/8" LONG. MARKED FASTENER WITH A "X" FOR IDENTIFICATION REAMED HOLE TO.593" AND INSTALLED A EN 6114-9-Y29 H
- [SDR FDEA202206161443](https://openairdocs.org/sdr/FDEA202206161443.md): Sensor · failed · Jun 16, 2022 · N751FD · Airbus A300* · Landing Gear Retraction/Extension System
  > PDIS 751 32-30 3421 16JUN22 YMX OPEN U LANDING GEAR LEVER INTERLOCKED CAUTION ON SYS 1 RIGHT AFTER CAPT TAT AND PITOT PROBE HEAT FAULTS. NO ISSUES ON SYS 2.MEL 16JUN22 12:44 YMX U RELEASED FOR SERVICE PER MEL: 32-30-01-B CATEGORY: C EXPI
- [SDR FDEA202109062223](https://openairdocs.org/sdr/FDEA202109062223.md): Floor Support · corroded · Sep 6, 2021 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FR12A-FR14 -Y1959 FLOOR SUPPORT CORRODED REPAIRED THE MAIN DECK FR12A-FR14 -Y1959 CORRODED FLOOR SUPPORT PER A300-600 SRM53-12-15-201. PARA.G. FIG207. THIS IS CATEGORY B REPAIR. THE REPAIR MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600 SRI
- [SDR FDEA202105261403](https://openairdocs.org/sdr/FDEA202105261403.md): Transmitter · cracked · May 26, 2021 · N751FD · Airbus A300B4622R · Hydraulic Indicating System
  > PDIS 751 29-30 2383 26MAY21 MEM OPEN U PASSING FL330 ON DESCENT TO MEM GREEN SYS RESERVOIR LOW LEVEL ILLUMINATED. GREEN SYSTEM SHOWED AT THE RED DOT. COMPLIED WITH ALL ECAM AND QRH PROCEDURES INCLUDING GRAVITY GEAR EXTENSION. FACT 26MAY21
- [SDR FDEA202105201316](https://openairdocs.org/sdr/FDEA202105201316.md): Skin · dented · May 20, 2021 · N751FD · Airbus A300B4622R · Trailing Edge Flaps
  > R/H IINBOARD FLAP, OUTBOARD TRAILING EDGE, LOWER SURFACE, HAS DENT MWT REPAIR PER SRM 57-50-00 FIG. 205
- [SDR FDEA202105041100](https://openairdocs.org/sdr/FDEA202105041100.md): B-Nut · loose · May 4, 2021 · N751FD · Airbus A300B4622R · Hydraulic System, Main
  > AFTER TAKEOFF, GEAR RETRACTED AND FLAPS RETRACTED GOT ECAM GREEN PRESSURE LOW, FOLLOWED BY GREEN FLUID QUANTITY LOW. FOLLOWED ECAM, MANUALLY EXTENDED GEAR. STOPPED ON THE RUNWAY AND TOWED TO THE GATE FOUND HYD FLUID POURING FROM #1 ENG, OPENED ENG AND
- [SDR FDEA202105031081](https://openairdocs.org/sdr/FDEA202105031081.md): Actuator · leaking · May 3, 2021 · N751FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > MOMENTS AFTER GEAR RETRACTION WE HAD AN INDICATION OF A TOTAL LOSS OF GREEN HYDRAULIC FLUID. BOTH ECAM HYDRAULIC PAGE AND ANALOG GAUGE SHOWED ZERO. EMERGENCY DECLARED. MOCC AND GOC NOTIFIED. COMPLIED WITH ECAM AND QRH FOR MANUAL GEAR EXTENSION. AFTER GEAR
- [SDR FDEA202103250778](https://openairdocs.org/sdr/FDEA202103250778.md): Indication Sys · inoperative · Mar 25, 2021 · N751FD · Airbus A300B4622R · Door Warning System
  > WHEN ARMING SLICED FOR DEPARTURE, R1 DOES NOT INDICATE ARMED RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 04APR21 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS
- [SDR FDEA202010152513](https://openairdocs.org/sdr/FDEA202010152513.md): Power Supply · damaged · Oct 15, 2020 · N751FD · Airbus A300B4622R · Door Warning System
  > BOTH LT AND RT MAIN CABIN ENTRY DOORS ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHTS INOPERABLE. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CATEGORY: C "MEL 52-XX-XX-XX: L1 AND R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS INOPERABLE. FACT 15OCT20 18:37

Next page: https://openairdocs.org/aircraft/N751FD/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 = 'N751FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N751FD/reports

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