# Service difficulty reports: N681FE

A list on [N681FE](https://openairdocs.org/aircraft/N681FE.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 · 339 reports

- [SDR FDEA202609031261](https://openairdocs.org/sdr/FDEA202609031261.md): Elec Connector · loose · Sep 3, 2026 · N681FE · Airbus A300F4605R · Door System Wiring
  > R1 DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL, ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. VERIFIED R1 DOOR ARMING HANDLE OPS AND THAT INDICATIO
- [SDR FDEA202607100915](https://openairdocs.org/sdr/FDEA202607100915.md): Warning System · malfunctioned · Jul 10, 2026 · N681FE · Airbus A300F4605R · Door Warning System
  > R1 DOOR WON T SHOW SLIDE WHEN DOOR IS ARMED. MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. AMM 52-73-13-04-02 AMM 31-55-22-04 SLAVED IN SWITCH 1
- [SDR FDEA202606060679](https://openairdocs.org/sdr/FDEA202606060679.md): Stowage Box · broken · Jun 6, 2026 · N681FE · Airbus A300F4605R · Crew Oxygen System
  > DURING REMOVAL OF FIRST OBSERVER SEAT FOUND O2 MASK WITH BROKEN MOUNTING SCREW. REMOVED AND REPLACED OBSERVER`S O2 BOX REF AMM 35-12-51-04
- [SDR FDEA202602120182](https://openairdocs.org/sdr/FDEA202602120182.md): Smoke Detector · no test · Feb 12, 2026 · N681FE · Airbus A300F4605R · Smoke Detection
  > AFT CARGO SMOKE LOOP A WILL NOT TEST. LIKELY FAILED COMPONENT IS THE 50WU3, ELECTRONIC SMOKE DETECTION UNIT. TROUBLESHOT IAW TSM 26-19-01 STANDARDS. AMM: 26-19-34-04 PERFORMED BITE TEST ON MAIN CARGO SMOKE DETECTOR CONTROL UNITS, 50WU1, 50WU2 AND 50WU3. FA
- [SDR FDEA202504010544](https://openairdocs.org/sdr/FDEA202504010544.md): Indication Sys · malfunctioned · Apr 1, 2025 · N681FE · Airbus A300F4605R · Passenger/Crew Doors
  > WHILE ARMING DOOR FOR DEPARTURE, R FWD SLIDE ARMED INDICATION WILL NOT ILLUMINATE ON ECAM. RELEASED FOR SERVICE PER MEL: 52-XX-XX CAT: C EXP: 11APR25 "MEL 52-XX-XX: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS T
- [SDR FDEA202412241831](https://openairdocs.org/sdr/FDEA202412241831.md): Rib · corroded · Dec 24, 2024 · N681FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > CORROSION NOTED ON LH RIB 5 FWD PINTLE LUG BETWEEN BUSHES "D" AND "E". LH RIB 5 REPAIRED IAW EA 6-5710-T0305976 B PT2: WINGS - BASIC WING STRUCTURE LH MLG RIB 5 FWD LUG - CORROSION. MAJOR REPAIR
- [SDR FDEA202412231828](https://openairdocs.org/sdr/FDEA202412231828.md): Rib · corroded · Dec 23, 2024 · N681FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH WING RIB 5 PINTLE FWD LUG HAS CORROSION BETWEEN BUSHES "D" AND "E". RH WING RIB 5 REPAIR ACCOMPLISHED PER EA 6-5710-T0305974 C PT2 WINGS - BASIC WING STRUCTURE - RH MLG RIB 5 FWD LUG CORROSION. MAJOR REPAIR
- [SDR FDEA202408311224](https://openairdocs.org/sdr/FDEA202408311224.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV LWR SKIN AT ER10 PLUS 22", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202408311223](https://openairdocs.org/sdr/FDEA202408311223.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV LWR SKIN AT ER5, T/E-6" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.70
- [SDR FDEA202408311222](https://openairdocs.org/sdr/FDEA202408311222.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13 PLUS 38", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202408311221](https://openairdocs.org/sdr/FDEA202408311221.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13 PLUS 31", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202408311220](https://openairdocs.org/sdr/FDEA202408311220.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13-3.5", T/E-10" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202408311219](https://openairdocs.org/sdr/FDEA202408311219.md): Elevator · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER10 PLUS 11", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREME
- [SDR FDEA202408311218](https://openairdocs.org/sdr/FDEA202408311218.md): Skin · no discrepancy · Aug 31, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER7 PLUS 16", T/E-14.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202408201154](https://openairdocs.org/sdr/FDEA202408201154.md): Skin · none · Aug 20, 2024 · N681FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON LH CENTER FLAP LOWER SKIN AT RIB20 ~ 21, TRAILING EDGE-14.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACK
- [SDR FDEA202408161253](https://openairdocs.org/sdr/FDEA202408161253.md): Skin · no discrepancy · Aug 16, 2024 · N681FE · Airbus A300F4605R · Cargo/Baggage Doors
  > EXISTING DOUBLER REPAIR FOUND ON AFTER CARGO DOOR LOWER FACE AT BEAM5 BETWEEN FR62A AND 63,EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF
- [SDR FDEA202408151264](https://openairdocs.org/sdr/FDEA202408151264.md): Profile · cracked · Aug 15, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT CRACK AT FR74 PLUS 22", -Y2020 REMOVED CRACK SUPPORT AND INSTALLED NEW SUPPORT. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE.7B-PAGE.23 AND 51-72-10-001, PAGE.2 & DRAWING A53981317. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
- [SDR FDEA202408151199](https://openairdocs.org/sdr/FDEA202408151199.md): Floorbeam · cracked · Aug 15, 2024 · N681FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR SUPPORT ANGLE CRACK AT FR77 Y1820 CRACKED ANGLE REPLACED NEW PART, INSTALLED WITH RIVETS AT MAIN DECK FLOOR FR77, Y1820. 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
- [SDR FDEA202408141216](https://openairdocs.org/sdr/FDEA202408141216.md): Rib · worn · Aug 14, 2024 · N681FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > THE BOLT BORE LOCATION #4 DAMAGE ON R5 SPOILER JACK RIB. ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH WING #5 SPOILER JACK RIB ABX175.875 I.A.W FEDEX EA NO:T6-5740-T0380389 P1, SEQ NO:977, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA175.87
- [SDR FDEA202408141215](https://openairdocs.org/sdr/FDEA202408141215.md): Seat Track · gouged · Aug 14, 2024 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR62 PLUS 2", Y1959 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR62~64, Y1959 I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A PER
- [SDR FDEA20240810125](https://openairdocs.org/sdr/FDEA20240810125.md): Skin · misrepaired · Aug 10, 2024 · N681FE · Airbus A300F4605R · Trailing Edge Flaps
  > EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN AT NOSE RIB5~10, FRONT SPAR~S-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-00 F
- [SDR FDEA202408101252](https://openairdocs.org/sdr/FDEA202408101252.md): Skin · damaged · Aug 10, 2024 · N681FE · Airbus A300F4605R · Trailing Edge Flaps
  > EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN AT NOSE RIB 5-10, FRONT SPAR-S-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-
- [SDR FDEA202408101251](https://openairdocs.org/sdr/FDEA202408101251.md): Skin · no discrepancy · Aug 10, 2024 · N681FE · Airbus A300F4605R · Trailing Edge Flaps
  > EXISTING DOUBLER REPAIR FOUND ON RT I/B FLAP UPPER SKIN AT NOSE RIB 10-16, S-1.1-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-00 FIG
- [SDR FDEA202408101201](https://openairdocs.org/sdr/FDEA202408101201.md): Shear Plate · cracked · Aug 10, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB CRACK AT FR79 PLUS 5" -Y1620 REPLACED THE CRACK SHEAR WEB BY NEW ONE WITH FASTENERS AT MAIN DECK FLOOR FR79 PLUS 5", -Y1620, I.A.W A300-600F S.R.M 51-72-10-001 AND 51-40-21-001 PARA.7, PAGE.24~50. THIS REPAIR CLASSIFIED AS MINOR P
- [SDR FDEA202408101200](https://openairdocs.org/sdr/FDEA202408101200.md): Shear Web · cracked · Aug 10, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB BROKEN AT FR77 -Y1920 REPLACED THE DAMAGE WEB WITH NEW ONE AT MAIN DECK FLOOR FR77 -Y1920. IAW A300-600F SRM 51-72-10-001, PAGE.2& 51-40-21-001, PARA.6, PAGE7B-PAGE23. THIS REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
- [SDR FDEA202408101197](https://openairdocs.org/sdr/FDEA202408101197.md): Profile · cracked · Aug 10, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR Z-PROFILE CRACK AT FR80/82, -Y1490 REPLACED THE DAMAGE Z-PROFILE BY NEW ONE WITH RIVETS AT MAIN DECK FR80/82, -Y1490 I.A.W A300-600F S.R.M 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS REPAIR CLASSIFIED AS MINOR PER G.M.M
- [SDR FDEA202408101175](https://openairdocs.org/sdr/FDEA202408101175.md): Elevator · no discrepancy · Aug 10, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LOWER SKIN AT ER5-8", TRAILING EDGE-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQ
- [SDR FDEA202408101174](https://openairdocs.org/sdr/FDEA202408101174.md): Elevator · no discrepancy · Aug 10, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LOWER SKIN AT ER2 16", TRAILING EDGE-17" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING RE
- [SDR FDEA202408101173](https://openairdocs.org/sdr/FDEA202408101173.md): Elevator · none · Aug 10, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LOWER SKIN AT ER5-8", TRAILING EDGE-21" * COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKIN
- [SDR FDEA202408091203](https://openairdocs.org/sdr/FDEA202408091203.md): Floorbeam · cracked · Aug 9, 2024 · N681FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > AVIONICS COMPARTMENT CABIN FLOOR STRUCTURE-CROSSBEAM OF ANGLE FITTING CRACK AT FR10 Y-953 POSITION. REPLACED THE CRACK ANGLE FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AT AVIONICS COMPARTMENT CABIN FLOOR STRUCTURE - CROSSBEAM Y-953 POSIT
- [SDR FDEA202408091195](https://openairdocs.org/sdr/FDEA202408091195.md): Floorbeam · cracked · Aug 9, 2024 · N681FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > AVIONICS COMPARTMENT CABIN FLOOR STRUCTURE-CROSSBEAM OF PICK-UP ANGLE CRACK AT FR10 Y403 POSITION. REPLACED THE PICK-UP CRACK ANGLE WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AT AVIONICS COMPARTMENT CABIN FLOOR STRUCTURE- CROSSBEAM Y403, FR10 PO
- [SDR FDEA202408081228](https://openairdocs.org/sdr/FDEA202408081228.md): Crossbeam · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR58, -Y450 TO -Y953 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,IN
- [SDR FDEA202408081213](https://openairdocs.org/sdr/FDEA202408081213.md): Crossbeam · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR77, Y1137.1 TO -Y1137.1 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12
- [SDR FDEA202408081191](https://openairdocs.org/sdr/FDEA202408081191.md): Seat Track · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK AT FR57~57.3, Y953 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 FDEA202408081190](https://openairdocs.org/sdr/FDEA202408081190.md): Seat Track · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK AT FR56~57.2, 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 12
- [SDR FDEA202408081189](https://openairdocs.org/sdr/FDEA202408081189.md): Seat Track · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK AT FR54.2~55, -Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12
- [SDR FDEA202408081179](https://openairdocs.org/sdr/FDEA202408081179.md): Seat Track · no discrepancy · Aug 8, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK AT FR36~38.2, Y953 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 FDEA202408071204](https://openairdocs.org/sdr/FDEA202408071204.md): Skin · delaminated · Aug 7, 2024 · N681FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 2EA WATER TRAPPED AREAS (170MM X 60MM &45MM X 85MM) WERE FOUND AT ER7 OF LH ELEVATOR TOP SKIN. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT LH ELEVATOR UPPER SKIN PANEL NEAR ER7 AND NO.10 SCREW. PER GMM 6-2-100. I.A.W A300-600F SRM 55-21-12-201, PARA.5
- [SDR FDEA202408071202](https://openairdocs.org/sdr/FDEA202408071202.md): Plate · cracked · Aug 7, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L, FR21 POSITION. REPLACED THE CRACK PLATE WITH NEW PART. LOCATE AT FORWARD CARGO COMPARTMENT UNDER FLOOR AREA S-43L~ S44L FR21. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 REPAIR CLASSI
- [SDR FDEA202408071194](https://openairdocs.org/sdr/FDEA202408071194.md): Skin · contaminated · Aug 7, 2024 · N681FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 2EA WATER TRAPPED AREAS (170MM X 60MM &45MM X 84MM) WERE FOUND ATER7 OF LHELEVATOR TOP SKIN. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT LH ELEVATOR UPPER SKIN PANEL NEAR ER7 AND NO.10 SCREW. PER GMM 6-2-100. I.A.W A300-600F SRM 55-21-12-201, PARA.5J.
- [SDR FDEA202408061226](https://openairdocs.org/sdr/FDEA202408061226.md): Door · misrepaired · Aug 6, 2024 · N681FE · Airbus A300F4605R · Cargo/Baggage Doors
  > EXISTING DOUBLER REPAIR FOUND ON FWD CARGO DR OUTER SKIN BTW FR25~25A, BEAM1~BEAM1 5.25" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT WITHOUT FAA APPROVED DATA, REPORTED TO
- [SDR FDEA202408061225](https://openairdocs.org/sdr/FDEA202408061225.md): Door · none · Aug 6, 2024 · N681FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING DOUBLER REPAIR FOUND ON FWD CARGO DOOR OUTER SKIN BTW FR20A~20B, BEAM1~BEAM1 5.25" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT WITHOUT FAA APPROVED DATA, REPORTED T
- [SDR FDEA202408061196](https://openairdocs.org/sdr/FDEA202408061196.md): Adapter · gouged · Aug 6, 2024 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR ADAPTER GOUGE AT FR60 -Y880 REPLACED GOUGE ADAPTER WITH NEW ONE AT MAIN DECK FLOOR ADAPTER FR60, -Y880 I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001 PARA.6, PAGE.7B~PAGE23 THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100
- [SDR FDEA202408051248](https://openairdocs.org/sdr/FDEA202408051248.md): Rib · chafed · Aug 5, 2024 · N681FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH WING LEADING EDGE RIB GOUGE WAS FOUND ON THE UPPER FLANGE OF THE ANTI-ICE DUCT CUT-OUT AT STA WOFX-259.4 TRIMMED OUT AND INSTALLED THE REPAIR ANGLE AT RH WING LEADING EDGE RIB WOFX-259.4 I.A.W FEDEX EA NO:T6-5710-T0380442 P1, SEQ NO:984, TITLE:WING-BASI
- [SDR FDEA202408021317](https://openairdocs.org/sdr/FDEA202408021317.md): Fitting · cracked · Aug 2, 2024 · N681FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 24. INSTALLED THE NEW BEARING FITTING WITH FASTENERS AT MAIN DECK CARGO DOOR FR24, LONGN 1~3 I.A.W FEDEX EA NO:T6-5230-T0380187 P1, SEQ NO:987, TITLE:SOORS-CARGO DOOR/HYD SYS-MAIN C
- [SDR FDEA202408021316](https://openairdocs.org/sdr/FDEA202408021316.md): Fitting · cracked · Aug 2, 2024 · N681FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 23 INSTALLED THE NEW BEARING FITTING WITH FASTENERS AT MAIN DECK CARGO DOOR FR23, LONGN 1~3 I.A.W FEDEX EA NO:T6-5230-T0380187 P1, SEQ NO:987, TITLE:SOORS-CARGO DOOR/HYD SYS-MAIN CA
- [SDR FDEA202404200483](https://openairdocs.org/sdr/FDEA202404200483.md): Evas Unit · no test · Apr 20, 2024 · N681FE · Airbus A300F4605R · Emergency Equipment
  > RIGHT EVAS UNIT FAILS TEST/INOP.REMOVED AND REPLACED RT EVAS IAW AMM 25-64-00-04. A/C OK FOR SERVICE.
- [SDR FDEA202305110857](https://openairdocs.org/sdr/FDEA202305110857.md): Relay · unknown · May 11, 2023 · N681FE · Airbus A300* · Standard Practices/Structures
  > ON TAXI OUT, WHILE PERFORMING FLIGHT CONTROL CHECKS, THE ELEVATORS WOULD NOT MOVE IN EITHER DIRECTION. RETURNED TO GATE. FOLLOWED TSM 27-33-01 FIG 103 AND REPLACED RELAY 308CY1 IN REF TO ESPM. VISUALLY INSPECTED PITCH ARTIFICAL FEEL UNIT AND BOTH #1 & #2 A
- [SDR FDEA202303140411](https://openairdocs.org/sdr/FDEA202303140411.md): Pressure Switch · failed · Mar 14, 2023 · N681FE · Airbus A300F4605R · Hydraulic Indicating System
  > ON TAKEOFF ROLL AT 75 KTS RECEIVED ECAM YELLOW HYDRAULIC SYSTEM LOW PRESSURE, ABORTED TAKEOFF. FACT 14MAR23 03:51 ATL U AMM 29-00-00-06 AMM 29-10-00-05 PER CREW DEBRIEF, YELLOW HYDRAULIC PRESSURE WAS NORMAL ON TAXI BACK TO RAMP. INSPECTED YELLOW SYST
- [SDR FDEA202203310789](https://openairdocs.org/sdr/FDEA202203310789.md): None · cracked · Mar 31, 2022 · N681FE · Airbus A300* · Passenger/Crew Doors
  > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS REPLACED RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (REV.K), F52181299(REV.G). TRACKING EA 6-5210-T0367713 P1 RAISED AND ACCOMPL

Next page: https://openairdocs.org/aircraft/N681FE/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 = 'N681FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N681FE/reports

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