# Service difficulty reports: N672FE

A list on [N672FE](https://openairdocs.org/aircraft/N672FE.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 6 · 287 reports

- [SDR FDEA202609081286](https://openairdocs.org/sdr/FDEA202609081286.md): Bottle · low pressure · Sep 8, 2026 · N672FE · Airbus A300F4605R · Passenger/Crew Doors
  > LEFT FWD CREW ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED LEFT FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRES.
- [SDR FDEA202602150210](https://openairdocs.org/sdr/FDEA202602150210.md): Safety Wire · wrong part · Feb 15, 2026 · N672FE · Airbus A300F4605R · Escape Slide
  > L1 SLIDE ASSY. REPLACE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 STAINLESS STEEL WIRE AND EJECTOR BAG RELEASE CABLE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. AMM: 25-61-21-04 AMM: 25-61-20-05-01 CMM: 25-60-40 FEA: 6-2560-F0386375 A EA:
- [SDR FDEA202512050001](https://openairdocs.org/sdr/FDEA202512050001.md): Skin · cracked · Jan 2, 2025 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FWD CARGO COMPT DOOR INNER SKIN CRACK AT FR22A, BEAM1 NEAR LEFT ACTUATOR I/B SIDE. CUT OUT AND INSTALLED REPAIR DOUBLER AT FWD CARGO DOOR INNER SKIN FR22A BEAM1~2 I.A.W FEDEX EA NO: T6-5230-T0381602 P1, SEQ NO:1140, TITLE:DOORS-CARGO DOOR/HYD SYS- FWD CARG
- [SDR FDEA202412111817](https://openairdocs.org/sdr/FDEA202412111817.md): Bracket · cracked · Dec 11, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FEDEX QA SURVEILLANCE FINDING MDC DOOR CUT OUT AFT SIDE FRAME FOUND 2EA BRACKETS WITH CRACKED AND MISSING PART. REPLACED THE CRACK BRACKETS WITH NEW PART LOCATE AT MAIN DECK SIDE CARGO DOOR CUT OUT AFTER SIDE FRAME I.A.W A300-600F SRM 51-72-10-001 PAGE 2 A
- [SDR FDEA202412081840](https://openairdocs.org/sdr/FDEA202412081840.md): Fork · cracked · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR PNL BOTTOM FOUND A LINK FORK CRACK AT FR47, -Y2462 FABRICATED THE NEW LINK FORK AND INSTALLED WITH FASTENER AT M/D FLOOR PNL BOTTOM FR47,-Y2462 I.A.W A300-600F SRM 53-15-15 CONFIG2 FIG 10 PAGE65 ITEM45 & 51-72-10-001 PAGE2 & 51-40-21-001 PARA7 PA
- [SDR FDEA202412081827](https://openairdocs.org/sdr/FDEA202412081827.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR54.2 PLUS 1", Y0. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR54.2~55, Y0, I.A.W A300-600F SRM 53-10-16-201, PARA.4, PAGE 203~208, FIG.201, THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.
- [SDR FDEA202412081826](https://openairdocs.org/sdr/FDEA202412081826.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR62 PLUS 1", Y1959. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR62~65, Y1959, I.A.W A300-600F SRM 53-10-16-201, PARA.4, PAGE 203~208, FIG.201. THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.
- [SDR FDEA202412081820](https://openairdocs.org/sdr/FDEA202412081820.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR28-1", Y0 POSITION. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR26~30, Y0, I.A.W A300-600F SRM 53-10-16-201,PARA, 4,PAGE 203~208, FIG.201, THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.
- [SDR FDEA202412081808](https://openairdocs.org/sdr/FDEA202412081808.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR54.2 PLUS 1", Y0 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR54.2~55,Y0,I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100
- [SDR FDEA202412081807](https://openairdocs.org/sdr/FDEA202412081807.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR62 PLUS 1",Y1959 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR62~65,Y1959, I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100
- [SDR FDEA202412081806](https://openairdocs.org/sdr/FDEA202412081806.md): Seat Track · worn · Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK WORN AT FR28-1",Y0 POSITION ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR26~30,Y0,I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100
- [SDR FDEA202412071833](https://openairdocs.org/sdr/FDEA202412071833.md): Rib · corroded · Dec 7, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE OUTBD JACK RIB CORRODED ADJACENT TO UPPER BORE AT L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT L5 SPOILER OUTBD JACK RIB ABX 184.625 UPPER BORE. I.A.W FEDEX EA NO: T6-5740-T0381590 P1, SEQ NO: 1134, TITLE: WING-ATTACH FITTINGS-LH WING #5 SPOILER J
- [SDR FDEA202412071832](https://openairdocs.org/sdr/FDEA202412071832.md): Rib · corroded · Dec 7, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE OUTBD JACK RIB CORROSION ADJACENT TO LOWER BORE AT L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT L5 SPOILER OUTBD JACK RIB ABX 184.625 LOWER BORE. I.A.W FEDEX EA NO: T6-5740-T0381590 P1, SEQ NO: 1134, TITLE: WING-ATTACH FITTINGS-LH WING #5 SPOILER
- [SDR FDEA202412071825](https://openairdocs.org/sdr/FDEA202412071825.md): Fitting · not reported · Dec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO: E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 LONGN 1~3 PER FEDEX E.O NO:E6-5230-E0378588 A P5, SEQ NO:1115, TITLE:DOORS-CARGO DOO
- [SDR FDEA202412071824](https://openairdocs.org/sdr/FDEA202412071824.md): Fitting · not reported · Dec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO: E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 LONGN 1~3 PER FEDEX E.O NO:E6-5230-E0378588 A P5, SEQ NO:1115, TITLE:DOORS-CARGO DOO
- [SDR FDEA202412071799](https://openairdocs.org/sdr/FDEA202412071799.md): Fitting · not reported · Dec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME23 PER EO NO:E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME23 LONGN 1~3 PER FEDEX EO NO:E6-5230-E0378588 A P5, SEQ NO:1242, TITLE:DOORS-CARGO DOOR/HYD
- [SDR FDEA202412071798](https://openairdocs.org/sdr/FDEA202412071798.md): Fitting · not reported · Dec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME24 PER EO NO:E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 LONGN 1~3 PER FEDEX EO NO:E6-5230-E0378588 A P5, SEQ NO:1242, TITLE:DOORS-CARGO DOOR/HY
- [SDR FDEA202412051842](https://openairdocs.org/sdr/FDEA202412051842.md): Fitting · cracked · Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER LH FRAME 45 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR45. I.A.W FEDEX EO NO: E6-5310-E0330747 D P23, SEQ NO:1120, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41
- [SDR FDEA202412051841](https://openairdocs.org/sdr/FDEA202412051841.md): Fitting · cracked · Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER RH FRAME 45 BASE FITTING FOUND AREA 1 CRACK. ACCOMPLISHED THE FRAME FOOT REPAIR AT RH LOWER FRAME FITTING FR45. I.A.W FEDEX EO NO: E6-5310-E0330747 D P24, SEQ NO:1121, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41
- [SDR FDEA202412051839](https://openairdocs.org/sdr/FDEA202412051839.md): Fitting · cracked · Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER RH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT RH LOWER FRAME FITTING FR46. I.A.W FEDEX EO NO: E6-5310-E0330747 D P26, SEQ NO:1123, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41
- [SDR FDEA202412051838](https://openairdocs.org/sdr/FDEA202412051838.md): Fitting · cracked · Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER LH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR46. I.A.W FEDEX EO NO: E6-5310-E0330747 D P25, SEQ NO:1122, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41
- [SDR FDEA202412051837](https://openairdocs.org/sdr/FDEA202412051837.md): Fitting · cracked · Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > LOWER LH FRAME 44 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR44. I.A.W FEDEX EO NO: E6-5310-E0330747 D P21, SEQ NO:1119, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41
- [SDR FDEA202412041853](https://openairdocs.org/sdr/FDEA202412041853.md): Door · bent · Dec 4, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR WAS FOUND BULGE ON THE INNER SKIN AND CONNECTION CLIP AT BEARING FITTING FWD OF FR24 BETWEEN LONGERON PT7-PT8. ACCOMPLISHED THE DOUBLER REINFORCEMENT REPAIR AT MAIN CARGO DOOR INNER SKIN AND CONNECTING CLIP FR24 BETWEEN LONGERON PT7~8,
- [SDR FDEA202412041834](https://openairdocs.org/sdr/FDEA202412041834.md): Rib · corroded · Dec 4, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > FOUND RH #4 SPOILER OUTBOARD UP JACK RIB HOLE CORROSION. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R4 SPOILER OUTBD JACK RIB ABX112.525 UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0381568 P1, SEQ NO:1133, TITLE:WING-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT
- [SDR FDEA202412041818](https://openairdocs.org/sdr/FDEA202412041818.md): Strap · cracked · Dec 4, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FUSELAGE STRUCTURAL FOUND S-33R STRAP CRACK AT FR-85 14" AREA. CRACKED STRAP REPLACED NEW PART INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT FR85 14"
- [SDR FDEA202412031809](https://openairdocs.org/sdr/FDEA202412031809.md): Floor Support · corroded · Dec 3, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR SUPPORT FOUND CORROSION AT FR14~FR17, -Y1959 REPLACED CORROSION SUPPORT WITH NEW ONE AT M/D FLOOR SUPPORT FR14~FR17,-Y1959, I.W.A A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001,PARA.6,PAGE 7B~23,THE REPAIR IS CLASSIFIED AS MINOR CAT.A PER GMM 6
- [SDR FDEA202412031794](https://openairdocs.org/sdr/FDEA202412031794.md): Floor Support · corroded · Dec 3, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR SUPPORT FOUND CORROSION AT FR14-9"~FR14, Y730. REPLACED CORROSION FLOOR SUPPORT WITH NEW ONE AT M/D FR14-9"~ FR14, Y730 I.A.W A300- 600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE 7B~23. THE REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100
- [SDR FDEA202411301835](https://openairdocs.org/sdr/FDEA202411301835.md): Plate · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CGO COMPT UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L, FR21 POSITION. REPLACED FWD CGO COMPT UNDER FLOOR AREA LH SIDE PLATE AT S-43L~S-44L, FR21 POSITION I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-PAGE.23. THIS R
- [SDR FDEA202411301816](https://openairdocs.org/sdr/FDEA202411301816.md): Floor Support · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK AT FR80/82, Y300. REPLACED THE 1EA PROFILE-Z WITH NEW ONE AT M/D FLOOR SRTUCTURE FR80/82, Y300. I.A.W A300-600F SRM 51-72-10-001, PAGE.2& 51-40-21-001, PARA.6, PAGE.7B~23. REPIAR CLASSIFIED AS MINOR PER GMM 6-
- [SDR FDEA202411301802](https://openairdocs.org/sdr/FDEA202411301802.md): Floor Support · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK AT FR80/82, Y300. REINSTALLED THE 1EA PROFILE-Z WITH NEW ONE AT M/D FLOOR SRTUCTURE FR80/82, Y300 I.A.W A300-600F SRM 51-72-10-001, PAGE.2. REPIAR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202411301801](https://openairdocs.org/sdr/FDEA202411301801.md): Support · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D OVHD COMPT FOUND A HARNESS SUPPORT CRACK AT FR80/82 POSITION. REPLACED THE DAMAGE HARNESS SUPPORT WITH NEW AT M/D OVHD COMPT FR80/82 POSITION. I.A.W A300-600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.
- [SDR FDEA202411301796](https://openairdocs.org/sdr/FDEA202411301796.md): Support Bracket · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CGO COMPT BILGE AREA 1EA ELECTRICAL WIRE SUPPORT BRACKET CRACK AT FR59 CENTER LINE POSITION. REPLACED THE DAMGE 1EA ELECTRICAL WIRE SUPPORT BRACKET WITH NEW ONE AT AFT CGO COMPT BILGE AREA FR59 CENTER LINE POSITION I.A.W A300-600F SRM 51-72-10-001, PAG
- [SDR FDEA202411301795](https://openairdocs.org/sdr/FDEA202411301795.md): Support Bracket · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CGO COMPT BILGE AREA 1EA ELECTRICAL WIRE SUPPORT BRACKET CRACK AT FR63, S-44R POSITION. REPLACED THE DAMAGE WIRE SUPPORT BRACKET WITH NEW ONE AT BULK CGO COMPT BILGE AREA FR63 S-44R POSITION I.A.W A300-600F SRM 51-72-10-001, PAGE 2 REPAIR CLASSIFIED A
- [SDR FDEA202411301782](https://openairdocs.org/sdr/FDEA202411301782.md): Floor Support · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR STRUCTURE FOUND 1EA SHEAR PLATE CRACK AT FR79 5", Y1600 REPLACED THE DAMAGE SHEAR PLATE WITH NEW ONE AT M/D FLOOR STRUCTURE FR79 5",Y1600 I.A.W A300-600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100
- [SDR FDEA202411301781](https://openairdocs.org/sdr/FDEA202411301781.md): Floor Support · cracked · Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR STRUCTURE FOUND 1EA SHEAR PLATE CRACK AT FR79 5", -Y1600 REPLACED THE DAMAGE SHEAR PLATE AT M/D FLOOR STRUCTURE FR79 5", -Y1600 I.A.W A300- 600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100
- [SDR FDEA202411261836](https://openairdocs.org/sdr/FDEA202411261836.md): Plate · cracked · Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CGO COMPT SHEAR PLATE CRACK AT FR68~FR69, S-48L POSITION. INSTALLED THE FABRICATION NEW PART AT BULK CARGO COMPARTMENT AT FR68~69, S-48L I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE.7B~23& AIRBUS DRAWING NO: A53974299 REV.D & FEDEX GMM 7-0-1001. THE
- [SDR FDEA202411261780](https://openairdocs.org/sdr/FDEA202411261780.md): Crossbeam · corroded · Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Structure
  > BULK CGO COMPT CROSSBEAM EXTERNAL SURFACE CORRODED AT FR66,Y0-2" POSITION CUT OUT DAMAGED CROSSBEAM AREA AND INSTALLED REPAIR PARTS ON REPAIR AREA WITH FASTENERS FOR REPAIR. I.A.W A300-600F SRM 51-40-21-001 PARA6 PAGE7B-23 AND 53-10-15-201 PARA13 P373-P38
- [SDR FDEA202411261765](https://openairdocs.org/sdr/FDEA202411261765.md): Bracket · cracked · Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CGO COMPT FWD BULKHEAD LH BRACKET CRACK AT FR54, Y1959 POSITION. REPLACED THE CRACKED LH FWD BULKHEAD BRACKET, AT AFT CARGO COMPT FR54, Y1959 POSITION. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE 7B- PAGE 23 AND 51-72-10-001, PAGE 2. THIS REPAIR IS
- [SDR FDEA202411261764](https://openairdocs.org/sdr/FDEA202411261764.md): Bracket · cracked · Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CGO COMPT FWD BULKHEAD RH BRACKET CRACK AT FR54, -Y1959 POSITION. REPLACED THE CRACKED AFT CARGO COMPT FWD BULKHEAD RH BRACKET, AT FR54, -Y1959 POSITION. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE 7B - PAGE 23 AND 51-72-10-001, PAGE 2. THIS REPAIR
- [SDR FDEA202411261763](https://openairdocs.org/sdr/FDEA202411261763.md): Angle · cracked · Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Floor Panel
  > AVIONICS COMPT FLOOR CROSSBEAM PICK UP ANGLE CRACK AT FR10, Y403 POSITION. REPLACED AVIONICS COMPT FLOOR BEAM PICK UP ANGLE WITH NEW ONE AT FR10, Y403 POSITION. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS REPAIR IS C
- [SDR FDEA202411211783](https://openairdocs.org/sdr/FDEA202411211783.md): Skin · damaged · Nov 21, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR31~32, S-49R~52R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1
- [SDR FDEA202409231336](https://openairdocs.org/sdr/FDEA202409231336.md): Fitting · failed · Sep 23, 2024 · N672FE · Airbus A300F4605R · AC Generator-Alternator
  > RTO AT 75 KNOTS FOR GENERATOR 1 FAILURE ON ROLL AT KGTF. TAXI BACK TO RAMP FOR MAINTENANCE. RELEASED FOR SERVICE PER MEL 24-11-01-A CATEGORY B. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. MEL: 24-11-01-A DEFERRED PER MEL 24-11-01-A,
- [SDR FDEA202409231335](https://openairdocs.org/sdr/FDEA202409231335.md): Idg · leaking · Sep 23, 2024 · N672FE · Airbus A300F4605R · AC Generator-Alternator
  > RTO AT 75 KNOTS FOR GENERATOR 1 FAILURE ON ROLL AT KGTF. TAXI BACK TO RAMP FOR MAINTENANCE. #1 IDG FOUND LEAKING FROM SERVICING PORT. REMOVED AND REPLACED #1 ENG IDG SERVICE FITTING AND PACKING. SERVICED AND OPS CKED IDG IAW ABOVE LISTED REF. OPS AND LEAK
- [SDR FDEA202406270871](https://openairdocs.org/sdr/FDEA202406270871.md): Pitot Tube · obstructed · Jun 27, 2024 · N672FE · Airbus A300F4605R · Pitot/Static System
  > ON TAKEOFF WHEN SPEED WAS CHECKED AT 80 KNOTS, CAPTAIN AIRSPEED INDICATED 80 AND FO AIRSPEED INDICATED BETWEEN 40 AND 50. REJECTED TAKEOFF AND RETURNED TO RAMP. INSPECTED PITOT DRAIN IN NOSE WHEELWELL. NO WATER FOUND. INSPECTED LINES AT ADC 1 AND ADC
- [SDR FDEA202406180815](https://openairdocs.org/sdr/FDEA202406180815.md): Pitot Tube · obstructed · Jun 18, 2024 · N672FE · Airbus A300F4605R · Pitot/Static System
  > ON TAKEOFF ROLL, FO CALLED 80 KNOTS AND CAPT HAD 60 KNOTS. TAKEOFF REJECTED AT 80 KNOTS ON CAPTAIN SIDE. INSPECTED FO & CAPT PITOT TUBES & FLUSHED LINES FROM ADC 1, ADC2. FO SYS CHECKED GOOD. FOUND CHARRED DEBRIS IN CAPT PITOT PROBE. MM 34-11-15-04, INS
- [SDR FDEA202403260379](https://openairdocs.org/sdr/FDEA202403260379.md): Lamp · inoperative · Mar 26, 2024 · N672FE · Airbus A300F4605R · Emergency Lighting
  > LAMP INOP AT 31WL2 (R1 EMERGENCY EXIT SIGN) REMOVED AND REPLACED 1 LAMP AT 31WL2 (R1 EMERGENCY EXIT SIGN) AS REQUIRED, OPS CHECK GOOD.
- [SDR FDEA202307081184](https://openairdocs.org/sdr/FDEA202307081184.md): Computer · failed · Jul 8, 2023 · N672FE · Airbus A300* · Cabin Pressure Control System
  > CABIN 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. A
- [SDR FDEA202303080395](https://openairdocs.org/sdr/FDEA202303080395.md): Strut · damaged · Mar 8, 2023 · N672FE · Airbus A300* · Main Landing Gear
  > NOSE LANDING GEAR DRAG STRUT FAILED REMOVED AND REPLACED TELESCOPING STRUT. IAW AMM 32-31-24-04. OPS CHECK SATISFACTORY
- [SDR FDEA202207161738](https://openairdocs.org/sdr/FDEA202207161738.md): None · cracked · Jul 16, 2022 · N672FE · Airbus A300* · Passenger/Crew Doors
  > RH FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK PERFORMED THE REPAIR ON RH FWD PAX DOOR FRAME SEGMENT AT FR14C AS PER FEDEX EA#: 6-5210-T0369438 P1, TITLE: DOORS - PASSENGER / CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR
- [SDR FDEA202207131713](https://openairdocs.org/sdr/FDEA202207131713.md): None · delaminated · Jul 13, 2022 · N672FE · Airbus A300* · Wing, Control Surfaces
  > LH WING 5# SPOILER O/B HINGE ARM O/B END FOUND DELAMINATION SIZE:80MM X 25MM X 1.45MM PERFORMED THE REPAIR ON LH WING 5# SPOILER O/B HINGE ARM O/B END AS PER FEDEX EA #: 6-5750-T0315012 A P2 TITLE: WING - FLIGHT SURFACES - LH WING 5# SPOILER LOWER SURF

Next page: https://openairdocs.org/aircraft/N672FE/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 = 'N672FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N672FE/reports

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