# Service difficulty reports: N677FE

A list on [N677FE](https://openairdocs.org/aircraft/N677FE.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 · 275 reports

- [SDR FDEA202609171360](https://openairdocs.org/sdr/FDEA202609171360.md): Gfi · failed · Sep 17, 2026 · N677FE · Airbus A300F4605R · Fuel Boost Pump
  > AUTO FUEL FEED FAULTED. USED QRH PROCEDURES TO RESET SYS. NR 2 PUMP FAULTED & WOULD NOT RESET. NR 1 INNER TANK PUMP DEFERRED, LEAVING NO OPERATING PUMP IN RT TANK & APPROX 25,000 POUNDS IN RT TANK UNUSABLE. DECLARED EMERGENCY & TRIED TO ESTABLISH A WAY TO BURN
- [SDR FDEA202504180734](https://openairdocs.org/sdr/FDEA202504180734.md): Fork · worn · Apr 18, 2025 · N677FE · Airbus A300F4605R · Rudder Structure
  > RUDDER #2 HINGE ARM BEARING PLAY. REPLACED THE HINGE ARM FORK END ASSY WITH NEW. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~50. THE REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100. AT RUDDER #2 HINGE ARM.
- [SDR FDEA202504180699](https://openairdocs.org/sdr/FDEA202504180699.md): Web · bent · Apr 18, 2025 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > THE WEB DEFORM NEAR FR86 S-L33. REPLACED THE DAMAGE STRAP AND WEB WITH NEW PARTS ON FR86, S-33L. 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 CLISSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202504180695](https://openairdocs.org/sdr/FDEA202504180695.md): Web · bent · Apr 18, 2025 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > THE WEB DEFORM NEAR FR86 S-R33 REPLACED THE WEB AND STRAP WITH NEW PARTS AT FR86~87, STGR33R I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~50. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA202504180660](https://openairdocs.org/sdr/FDEA202504180660.md): Floorbeam · corroded · Apr 18, 2025 · N677FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR FOUND FLOOR BEAM CORROSION AT FR12A PLUS 16" Y740 REPLACED THE DAMAGE SUPPORT BY NEW ONE WITH RIVETS I.A.W. A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE,7B~PAGE,23.THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAI
- [SDR FDEA202504180639](https://openairdocs.org/sdr/FDEA202504180639.md): Skin · damaged · Apr 18, 2025 · N677FE · Airbus A300F4605R · Rudder, Plate/Skin
  > FOUND TWO BURN MARK NEAR RUDDER TOP SIDE TE AND PNL 326AT. PERFORM REPAIR OF APEX STRIP BY NEW STRIP SECTION AND CONNECTION PLATES WITH RIVETS AT NEAR RUDDER TOP SIDE TE AND PNL 326AT AREA I.A.W A300-600F SRM 55-41-12-201, PARA.13, PAGE.237~PAGE.239, FIG.2
- [SDR FDEA202504170722](https://openairdocs.org/sdr/FDEA202504170722.md): Fitting · damaged · Apr 17, 2025 · N677FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN1~LONGN3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:963, TITLE: DOOR
- [SDR FDEA202504160712](https://openairdocs.org/sdr/FDEA202504160712.md): Rib · worn · Apr 16, 2025 · N677FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH WING #5 SPOILER O/B JACK RIB UPPER BORE GOT ABRASION ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #5 SPOILER O/B JACK RIB UPPER BORE ABX184.625 I.A.W EA NO:T6-5740-T0383103 P1, SEQ NO:1060, TITLE:WING-ATTACH FITTINGS
- [SDR FDEA202504150667](https://openairdocs.org/sdr/FDEA202504150667.md): Seat Track · gouged · Apr 15, 2025 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR66 PLUS 11" Y1456 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR66~FR68, Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A P
- [SDR FDEA202504150662](https://openairdocs.org/sdr/FDEA202504150662.md): Seat Track · gouged · Apr 15, 2025 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR66 PLUS 11" Y-450 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR65~FR68, Y-450. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A P
- [SDR FDEA202504150625](https://openairdocs.org/sdr/FDEA202504150625.md): Seat Track · worn · Apr 15, 2025 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR57.3 PLUS 2" Y1456 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR56~FR59, Y1456, I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG 201,PAGE 203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A
- [SDR FDEA202504140661](https://openairdocs.org/sdr/FDEA202504140661.md): Seat Track · gouged · Apr 14, 2025 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR57.1 PLUS 3" Y-1959 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57~57.2, Y-1959. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.
- [SDR FDEA202504140626](https://openairdocs.org/sdr/FDEA202504140626.md): Seat Track · worn · Apr 14, 2025 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR60 PLUS 9" Y953 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR58~FR61, Y953, 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 FDEA202504130637](https://openairdocs.org/sdr/FDEA202504130637.md): Shear Web · damaged · Apr 13, 2025 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB BROKEN AT FR77 Y-1897 REMOVED DAMAGED SHEAR WEB AND INSTALLED NEW SHEAR WEB. I.A.W A300-600F SRM 51-72- 10-001, PAGE2 AND 51-40-21-001, PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DECK FLOOR FR77, Y-18
- [SDR FDEA202504120747](https://openairdocs.org/sdr/FDEA202504120747.md): Crossbeam · unknown · Apr 12, 2025 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR31, -Y450~-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,
- [SDR FDEA202504120746](https://openairdocs.org/sdr/FDEA202504120746.md): Crossbeam · none · Apr 12, 2025 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR29, -Y450~-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
- [SDR FDEA202504120742](https://openairdocs.org/sdr/FDEA202504120742.md): Crossbeam · none · Apr 12, 2025 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR30, - Y450~-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
- [SDR FDEA202504120658](https://openairdocs.org/sdr/FDEA202504120658.md): Floor Support · cracked · Apr 12, 2025 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT CRACK APPROX 3/4" AT FR38.1 PLUS 16" Y2602 REPLACED THE SUPPORT WITH NEW PART AND FASTENERS AT MAIN DECK FR38.1 PLUS 16", Y2602. I.A.W A300-600F SRM 51-40-21-001, PARA.7, PAGE.24~50 AND 51-72-10-001, PAGE.2. THE REPAIR CLASSIFIED AS
- [SDR FDEA202504120653](https://openairdocs.org/sdr/FDEA202504120653.md): Skin · corroded · Apr 12, 2025 · N677FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB27,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202504120643](https://openairdocs.org/sdr/FDEA202504120643.md): Skin · dented · Apr 12, 2025 · N677FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING FLUSH DOUBLER REPAIR FOUND ON LH O/B FLAP L/E NOSE BTW RIB14~RIB18 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 1
- [SDR FDEA202504110705](https://openairdocs.org/sdr/FDEA202504110705.md): Plate · cracked · Apr 11, 2025 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CGO COMP'T LH SIDE PLATE CRACK BETWEEN FR21~FR22 S-43L POSITION. REPLACED THE CRACK PLATE WITH NEW PART AT FWD CARGO COMP'T LH SIDE BETWEEN FR21 TO FR22, S-43L IAW A300-600F SRM 51-40-21-001, PARA.6, PAGE7B~PAGE23. THIS REPAIR IS CLASSIFIED AS MINOR
- [SDR FDEA202504110655](https://openairdocs.org/sdr/FDEA202504110655.md): Skin · damaged · Apr 11, 2025 · N677FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 2EA WATER TRAPPED AREA (65MMX35MM)(75MMX40MM) WERE FOUND AT LH ELEVATOR TOP SKIN PANEL T/E FASTENER NO.10 AND NO.37. *COUNTING FASTENER FROM I/B TO O/B*. ACCOMPLISHED THE COMPOSITE REPAIR AT LH ELEVATOR TOP SKIN PANEL T/E FASTENER NO.10 AND NO.37 I.A.W A30
- [SDR FDEA202504100618](https://openairdocs.org/sdr/FDEA202504100618.md): Skin · unknown · Apr 10, 2025 · N677FE · Airbus A300F4605R · Elevator, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER13 PLUS 29.5", T/E-24" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIR
- [SDR FDEA202504100617](https://openairdocs.org/sdr/FDEA202504100617.md): Skin · unknown · Apr 10, 2025 · N677FE · Airbus A300F4605R · Elevator, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER13 PLUS 28", T/E-18" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREM
- [SDR FDEA202504100614](https://openairdocs.org/sdr/FDEA202504100614.md): Skin · no discrepancy · Apr 10, 2025 · N677FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 14.5", T/E-12.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUI
- [SDR FDEA202504100613](https://openairdocs.org/sdr/FDEA202504100613.md): Skin · no discrepancy · Apr 10, 2025 · N677FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 9", T/E-11" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEN
- [SDR FDEA202504100612](https://openairdocs.org/sdr/FDEA202504100612.md): Skin · no discrepancy · Apr 10, 2025 · N677FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 26.5", T/E-29" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRE
- [SDR FDEA202504100611](https://openairdocs.org/sdr/FDEA202504100611.md): Skin · no discrepancy · Apr 10, 2025 · N677FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 12", T/E-47.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRE
- [SDR FDEA202504100610](https://openairdocs.org/sdr/FDEA202504100610.md): Skin · no discrepancy · Apr 10, 2025 · N677FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 15", T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREME
- [SDR FDEA202504090735](https://openairdocs.org/sdr/FDEA202504090735.md): Attach Fitting · cracked · Apr 9, 2025 · N677FE · Airbus A300F4605R · Cargo/Baggage Doors
  > 1EA CRACK WAS FOUND AT FWD CARGO DOOR ACTUATOR ATTACH FITTING. ACCOMPLISHED THE REPLACEMENT OF FRAME HEAD AND PERFORMED TRIM OUT ON INNER SKINS AND ANGLE PROFILE AT FWD CARGO DOOR FR22A, BEAM1~3. I.A.W FEDEX EA NO:T6-5230- T0383047 P1, SEQ NO:1070, TITLE:DO
- [SDR FDEA202504080723](https://openairdocs.org/sdr/FDEA202504080723.md): Fitting · cracked · Apr 8, 2025 · N677FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN1~LONGN3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:963, TITLE: DOORS - CARGO DOOR/HYD S
- [SDR FDEA202403190315](https://openairdocs.org/sdr/FDEA202403190315.md): Warning Light · false indication · Mar 19, 2024 · N677FE · Airbus A300F4605R · Doors
  > L1 AND R1 DOOR CABIN AND MAIN CARGO PRESSURE LIGHTS ARE ILLUMINATED ON THE GROUND WITH 0 PSID AND CABIN AT FIELD ELEVATION. RESET GROUND POWER, LIGHTS CLEARED, NO WARNINGS. CABIN PRESSURE CONTROL AND MONITORING ADJUSTMENT/TEST CARRIED OUT IAW 21-31-00-05 W
- [SDR FDEA202401190192](https://openairdocs.org/sdr/FDEA202401190192.md): Gcu · failed · Jan 19, 2024 · N677FE · Airbus A300F4605R · AC Generator-Alternator
  > DURING DECENT AC BUS 1 FAILURE. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. REMOVED AND REPLACED NR 1 GCU PER 24-22-12-04. OPS CHECK STILL REQUIRED.PERFORMED #1 IDG SERVICING PER 12-13-24 AMM: 24-22-12-04. PERFORMED ENGINE RUN PER A300 JRH AND OP
- [SDR FDEA202303070384](https://openairdocs.org/sdr/FDEA202303070384.md): Spoiler · delaminated · Mar 7, 2023 · N677FE · Airbus A300* · Wing, Control Surfaces
  > LH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE & CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATED (1) (S:10MM*15MM D:1.52MM) (2) (S:10MM*15MM D:1.52MM) REPAIRED LH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE DELAMINATION & CEN
- [SDR FDEA202303070383](https://openairdocs.org/sdr/FDEA202303070383.md): Spoiler · delaminated · Mar 7, 2023 · N677FE · Airbus A300* · Wing, Control Surfaces
  > RH WING #3 SPOILER I/B CENTER HINGE ARM O/B FOUND DELAMINATION. SIZE: 10MM*18MM, DEPTH: 1.59MM. REPAIRED THE RH WING #3 SPOILER I/B CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION PER FEDEX EA: 6-5750-T0373206 P1 & SB A300-57-6082 R03 FIGURE 2 SHEET 2 & 4
- [SDR FDEA202303050378](https://openairdocs.org/sdr/FDEA202303050378.md): Seat Track · corroded · Mar 5, 2023 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC SEAT TRACK -Y953 CORRODED AT FR54.2 - FR54.3. REPAIRED THE MDCC CORRODED SEAT TRACK -Y953 AT FR54.2 - FR54.3 PER A300-600F SRM53-10- 16-201 FIGURE 201. THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202303030362](https://openairdocs.org/sdr/FDEA202303030362.md): Crossbeam · cracked · Mar 3, 2023 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSS BEAM FOUND CRACKED AT FR64 Y1456 - Y1959 REPAIRED THE MDCC CRACKED CROSSBEAM AT FR64 Y1456~Y1959 PER A300-600F SRM51-40-21 & SRM53-10-15-201 PARA.14. THIS REPAIR IS CAT A REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202303030361](https://openairdocs.org/sdr/FDEA202303030361.md): Crossbeam · cracked · Mar 3, 2023 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSS BEAM FOUND CRACKED AT FR32 -Y450 ~ -Y953 REPAIRED THE MDCC CRACKED CROSS BEAM AT FR32 -Y450 ~ -Y953 PER A300-600F SRM53-10-15- 201 PARA.15 & FEDEX EA: 6-5310-T0373225 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK AT STIFFENER OF FR32 CROSSBEAM BETWE
- [SDR FDEA202303030360](https://openairdocs.org/sdr/FDEA202303030360.md): Crossbeam · cracked · Mar 3, 2023 · N677FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSS BEAM FOUND CRACKED AT FR38.2 Y1456 - Y1959 REPAIRED THE MDCC CRACKED CROSS BEAM AT FR38.2 Y1456 ~ Y1959 PER A300-600F SRM53-10- 15-201 PARA. 15 & FEDEX EA: 6-5310-T0373226 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK AT STIFFENER OF FR38.2 CROSSBEA
- [SDR FDEA202301070047](https://openairdocs.org/sdr/FDEA202301070047.md): Smoke Detector · false activation · Jan 7, 2023 · N677FE · Airbus A300F4605R · Fire Detection
  > AT FL370 GOT AFT BULK CARGO SMOKE INDICATION ON ECAM. COMPLIED WITH ECAM AND QRH. AFTER INITIAL INDICATION GOT ANOTHER MASTER WARNING AND ECAM INDICATION APPROXIMATELY 7-8 MINUTES LATER. REMOVED AND REPLACED (9WH, 10WH, 11WH, 44 WH) SMOKE DETECTORS IAW A
- [SDR FDEA202212162926](https://openairdocs.org/sdr/FDEA202212162926.md): Smoke Detector · false indication · Dec 16, 2022 · N677FE · Airbus A300F4605R · Fire Detection
  > AT CRUISE 33,000, RECEIVED A SMOKE INDICATION FOR THE AFT BULK BAY. FOLLOWED ECAM & QRH. DISCHARGED AGENT 1. INDICATION WENT AWAY AFTER. PERFORMED LOWER CARGO SMOKE DET ADJ/TEST IAW AMM. ALL INDICATIONS NORMAL. PERFORMED GVI OF LOWER AFT CARGO & BULK BAY FO
- [SDR FDEA202211142783](https://openairdocs.org/sdr/FDEA202211142783.md): Mount · corroded · Nov 14, 2022 · N677FE · Airbus A300F4605R · Engine Mount Section
  > #1 ENG PYLON SIDE OF FWD ENG MOUNT HAS PITTING ON LOWER SURFACE. ORIG SUB DATE: 11/14/2022
- [SDR FDEA202211142782](https://openairdocs.org/sdr/FDEA202211142782.md): Mount · damaged · Nov 14, 2022 · N677FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > #1 ENG, FWD MOUNT, AFT OUTBOARD HOLE HAS CORROSION ON THE TOP COUNTERBORE. COMPLIED WITH E.A.#: 6-5451-T0371499 (P1) PYLON STRUCTURE - TAIL PYLON/STRUT - #1 ENGINE FWD MOUNT AFT TENSION BOLT HOLES WITH CORROSION AND NICKS ON BOTTOM SURFACE OF MOUNT COMM
- [SDR FDEA202211142781](https://openairdocs.org/sdr/FDEA202211142781.md): Mount · corroded · Nov 14, 2022 · N677FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > #1 ENG, FWD MOUNT, AFT INBD HOLE HAS CORROSION ON TOP COUNTERBORE. 0003684179: CODY BACKUS CRB - 12-NOV-2022 20:49 COMPLIED WITH E.A.#: 6-5451-T0371499 (P1) PYLON STRUCTURE - TAIL PYLON/STRUT - #1 ENGINE FWD MOUNT AFT TENSION BOLT HOLES WITH CORROSION AN
- [SDR FDEA202211142780](https://openairdocs.org/sdr/FDEA202211142780.md): Mount · corroded · Nov 14, 2022 · N677FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > #1 ENGINE PYLON FWD MOUNT AFT OUTBOARD BOLT HOLE PITTED 0000265104: ARMSTRONG, BERNARD L - 03-NOV-2022 01:25 REPAIRED #1 ENGINE PYLON FWD MOUNT AFT OUTBOARD BOLT HOLE PER AIRBUS SRM 54-51-81. 0003655255: LEGGETT, JACOB A - 12-NOV-2022 21:37 COMPLIED WITH
- [SDR FDEA202211142779](https://openairdocs.org/sdr/FDEA202211142779.md): Mount · corroded · Nov 14, 2022 · N677FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > #1 ENGINE PYLON FWD MOUNT AFT INBOARD BOLT HOLE PITTED. REPAIRED #1 ENGINE PYLON FWD MOUNT AFT INBOARD BOLT HOLE PER AIRBUS SRM 54-51-81. COMPLIED WITH E.A. # 6-5451-T0371499 (P2) TITLE: PYLON STRUCTURE-TAIL PYLON/STRUT-#1 ENGINE FWD MOUNT AFT TENSION BOL
- [SDR FDEA202107281880](https://openairdocs.org/sdr/FDEA202107281880.md): Autothrottle Sys · malfunctioned · Jul 28, 2021 · N677FE · Airbus A300F4605R · Auto Throttle System
  > ON TAKEOFF (NON-PROFILE, AUTOTHROTTLES OFF PER MEL) THROTTLES SPLIT ONE KNOB LENGTH AFTER GEAR RETRACTION. TAKE OFF POWER WAS SET AT 101.5 N1 ON BOTH ENGINES. HOWEVER, SOMETIME AFTER ROTATION, THE NUMBER 2 ENGINE INCREASED TO 108.5 N1 DESPITE AUTOTHROTTLES
- [SDR FDEA202107271881](https://openairdocs.org/sdr/FDEA202107271881.md): Autothrottle Sys · malfunctioned · Jul 27, 2021 · N677FE · Airbus A300F4605R · Auto Throttle System
  > AFTER GEAR RETRACTION, AUTO THROTTLE SYSTEM COMMANDED #1 ENGINE TO REDUCE POWER BY 3-5% OF SELECTED FLX TRP VALUE. THE #1 THROTTLE WAS SPLIT BY A KNOB WIDTH FROM THE #2 THROTTLE. TRP FLX VALUE REMAIN UNCHANGED FROM BEING SET ON THE GROUND.ONCE THE THROTTLES
- [SDR FDEA202105051135](https://openairdocs.org/sdr/FDEA202105051135.md): Adc · failed · May 5, 2021 · N677FE · Airbus A300F4605R · Air Data Computer
  > IN CRUISE THE FO S ALTIMETER IS 300 FEET OFF CAPTAIN S ALTIMETER AND 200 FEET OFF THE STANDBY ALTIMETER. PERFORMED PITOT/STATIC ADJ/TEST PER A300 AMM 34-10-00-5. FOUND F/O ALT READING SPLIT FROM CAPTIANS AND STANDBY. R/R'D #2 ADC PER A300 AMM 34-11-34-04.
- [SDR FDEA202102040291](https://openairdocs.org/sdr/FDEA202102040291.md): Reservoir · failed · Feb 4, 2021 · N677FE · Airbus A300F4605R · Hydraulic Indicating System
  > ON APPROACH INTO KMEM RECEIVED ECAM ALERT GREEN HYD RSVR LO LEVEL ALERT. CONFIRMED LOW QUANTITY ON HYDRAULIC GAUGE AND ON ECAM SYSTEM DISPLAY. COMPLIED WITH ECAM AND QRH PROCEDURES, DECLARED EMERGENCY, LANDED SAFELY ON RUNWAY 36C. NO NOTICEABLE HYDRAULI

Next page: https://openairdocs.org/aircraft/N677FE/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 = 'N677FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N677FE/reports

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