# Service difficulty reports: N687FE

A list on [N687FE](https://openairdocs.org/aircraft/N687FE.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 3 · 126 reports

- [SDR FDEA202602260281](https://openairdocs.org/sdr/FDEA202602260281.md): Slide · faulted · Feb 26, 2026 · N687FE · Airbus A300F4605R · Escape Slide
  > WHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 FOUND RIVETS PULLED THROUGH AND METAL STRIP PULLED AWAY FROM SLIDE HOUSING. AMM: 25-61-21-04 FEA: 6-25-0-F0386375 REMOVED AND REPLACED L1 DUAL ESCAPE SLIDE - SAFETY PIN PULLED - ARMED AND DISARMED INDICATIONS
- [SDR FDEA202602180231](https://openairdocs.org/sdr/FDEA202602180231.md): Battery · inoperative · Feb 18, 2026 · N687FE · Airbus A300F4605R · Emergency Lighting
  > EMERGENCY LIGHTS DOOR TEST INOP AMM: 33-51-14-04 REMOVED/INSTALLED EMERGENCY POWER SUPPLY UNIT PER AMM REF. ABOVE, OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202508201511](https://openairdocs.org/sdr/FDEA202508201511.md): None · none · Aug 20, 2025 · N687FE · Airbus A300F4605R · Spoilers
  > EXISTING REPAIR FOUND ON RH WING NEW #5 SPOILER CENTER HINGE ARM 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, INSPECTION OF EXISTING
- [SDR FDEA202508201510](https://openairdocs.org/sdr/FDEA202508201510.md): None · none · Aug 20, 2025 · N687FE · Airbus A300F4605R · Spoilers
  > EXISTING REPAIR FOUND ON LH WING NEW #5 SPOILER OF TRAILING EDGE 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, INSPECTION OF EXISTIN
- [SDR FDEA202508181508](https://openairdocs.org/sdr/FDEA202508181508.md): None · no discrepancy · Aug 18, 2025 · N687FE · Airbus A300F4605R · Spoilers
  > EXISTING REPAIR FOUND ON LH WING NEW #5 SPOILER CENTER HINGE ARM 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, INSPECTION OF EXISTING
- [SDR FDEA202508111406](https://openairdocs.org/sdr/FDEA202508111406.md): Profile · cracked · Aug 11, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82, Y1448. REPLACED THE CRACK PROFILE-Z WITH NEW PART.LOCATE AT MAIN DECK FLOOR FR80/82 Y1448.I.A.W A300-600F SRM 51-72-10-001 PAGE 2 AND 51-40-21-001 PARA 6 PAGE 7B~PAGE 23.REPAIR CLASSIFIED AS
- [SDR FDEA202508071530](https://openairdocs.org/sdr/FDEA202508071530.md): Seat Track · worn · Aug 7, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND SEAT TRACK CROWN WORN AT FR28 PLUS 13"~FR28 PLUS 14", Y450. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR26~30,Y450 I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIR
- [SDR FDEA202508071529](https://openairdocs.org/sdr/FDEA202508071529.md): Seat Track · worn · Aug 7, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND SEAT TRACK CROWN WORN AT FR28 PLUS 14", -Y953 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR26~32,- Y953 I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIR IS CLASSIFIED
- [SDR FDEA202508051405](https://openairdocs.org/sdr/FDEA202508051405.md): Profile · cracked · Aug 5, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82,-Y1448. REPLACED THE CRACK PROFILE-Z WITH NEW PART.LOCATE AT MAIN DECK FLOOR FR80/82 - Y1448.I.A.W A300-600F SRM 51-72-10-001 PAGE 2 AND 51-40-21-001 PARA 6 PAGE 7B~PAGE 23.REPAIR CLASSIFIED AS
- [SDR FDEA202508041520](https://openairdocs.org/sdr/FDEA202508041520.md): Skin · contaminated · Aug 4, 2025 · N687FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA(80MM*100MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.22 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.22 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-
- [SDR FDEA202508041519](https://openairdocs.org/sdr/FDEA202508041519.md): Skin · contaminated · Aug 4, 2025 · N687FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA(110MM*100MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.30 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.30 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12
- [SDR FDEA202508041518](https://openairdocs.org/sdr/FDEA202508041518.md): Skin · contaminated · Aug 4, 2025 · N687FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA(95MM*70MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.20 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.20 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-2
- [SDR FDEA202508041517](https://openairdocs.org/sdr/FDEA202508041517.md): Skin · contaminated · Aug 4, 2025 · N687FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA(70MM*70MM) WERE FOUND AT L/H ELEVATOR TOP SKIN PANEL T/E NO.5 FASTENER. *COUNTING FASTENER FROM I/B TO O/B* ACCOMPLISHED THE COMPOSITE REPAIR AT L/H ELEVATOR TOP SKIN PANEL T/E NO.5 FASTENER POSITION. I.A.W A300-600F SRM 55-21-12-201
- [SDR FDEA202508041385](https://openairdocs.org/sdr/FDEA202508041385.md): Seat Track · no discrepancy · Aug 4, 2025 · N687FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR ANGLE FOUND ON MDCC SEAT TRACK BTW FR60~61,-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 121.7
- [SDR FDEA202508041384](https://openairdocs.org/sdr/FDEA202508041384.md): Doubler · no discrepancy · Aug 4, 2025 · N687FE · Airbus A300F4605R · Wing, Plate/Skin
  > EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN BTW RIB3~4,S-1.2 ~ FRONT SPAR 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, INSP
- [SDR FDEA202508041375](https://openairdocs.org/sdr/FDEA202508041375.md): Seat Track · no discrepancy · Aug 4, 2025 · N687FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK BTW FR31~34,-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 121.
- [SDR FDEA202508031488](https://openairdocs.org/sdr/FDEA202508031488.md): Floor Support · cracked · Aug 3, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR37~FR38,-Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR37~FR38, -Y2465 POS. 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
- [SDR FDEA202508031487](https://openairdocs.org/sdr/FDEA202508031487.md): Floor Support · cracked · Aug 3, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38.1~FR38.2,-Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, - Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED
- [SDR FDEA202508031486](https://openairdocs.org/sdr/FDEA202508031486.md): Floor Support · cracked · Aug 3, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, Y2465 POS. REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38.1~FR38.2, Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED
- [SDR FDEA202508031485](https://openairdocs.org/sdr/FDEA202508031485.md): Floor Support · cracked · Aug 3, 2025 · N687FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FOUND SUPPORT CRACK AT MDCC FLOOR STRUCTURE FR38~FR38.1, Y2465 POS REPLACED CRACK SUPPORT WITH NEW ONE. AT MDCC FLOOR STRUCTURE FR38~FR38.1, Y2465 POS. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED AS MI
- [SDR FDEA202508021537](https://openairdocs.org/sdr/FDEA202508021537.md): Skin · dented · Aug 2, 2025 · N687FE · Airbus A300F4605R · Leading Edge Devices
  > LH WING #1 SLAT O/B AFT SURFACE TOP AREA GOT A DENT ABOVE FOLDING NOSE. PERFORMED CUT OUT DAMAGED BOTTOM SKIN. AND INSTALLED 2EA REPAIR PARTS WITH ADHESIVE FOR CURE AT LH WING #1 SLAT O/B AFT SURFACE TOP AREA ABOVE FOLDING NOSE POSITION. I.A.W FEDEX EA NO:
- [SDR FDEA202507311605](https://openairdocs.org/sdr/FDEA202507311605.md): Fitting · damaged · Jul 31, 2025 · N687FE · 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:1101, TITLE:DOO
- [SDR FDEA202507301551](https://openairdocs.org/sdr/FDEA202507301551.md): Flap · no discrepancy · Jul 30, 2025 · N687FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON LH INBD FLAP LWR SKIN BTW RIB12A~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF DOUBLER REPAIR WITHOUT REPAIR RECORD AND DETERMINED IT NOT CONFORMITY ANY FAA
- [SDR FDEA202507301386](https://openairdocs.org/sdr/FDEA202507301386.md): Doubler · no discrepancy · Jul 30, 2025 · N687FE · Airbus A300F4605R · Leading Edge Devices
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING FLUSH DOUBLER REPAIR FOUND ON LH WING #1 SLAT NOSE SKIN BTW RIB 9~10 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202507301372](https://openairdocs.org/sdr/FDEA202507301372.md): Skin · no discrepancy · Jul 30, 2025 · N687FE · Airbus A300F4605R · Elevator, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16-12", T/E-22" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202507291604](https://openairdocs.org/sdr/FDEA202507291604.md): Fitting · cracked · Jul 29, 2025 · N687FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MDCD BEARING FITTING AT FR24 WAS FOUND CRACK ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN 1 ~ LONGN 3. I.A.W FEDEX EO NO:E6-5230-E0378588B P5, SEQ NO:1101, TITLE:DOORS - CARGO DOOR /HYD SYS -DETAILED VISUAL INSP
- [SDR FDEA202409051246](https://openairdocs.org/sdr/FDEA202409051246.md): Steering Sys · malfunctioned · Sep 5, 2024 · N687FE · Airbus A300F4605R · Landing Gear Steering System
  > LOW SPEED RTO AT APPROX 60 KNOS ON RW 31 AT YWG. FO REPORTED DIFFICULTY W/DIRECTIONAL CONTROL. FULL LEFT RUDR ALL THE WAY TO THE STOPS WAS NEEDED TO MAINTAIN CENTERLINE. AFTER THE REJECT THE WHEELS ON THE LEFT TRUCK HEATED TO OVER 300 DEGREES, WHILE THE T
- [SDR FDEA202408281180](https://openairdocs.org/sdr/FDEA202408281180.md): Support Fitting · corroded · Aug 28, 2024 · N687FE · Airbus A300F4605R · Wing Miscellaneous Structure
  > SMIS 687 57-10 6415 01JUL24 17:18 MEM FACT WS-C 00088832 MOD TYPE F MOD NO. 6-5710-F0377949 REV NO. PS P1 WINGS - MAIN LANDING GEAR SUPPORT WING RIB 5 - INSPECTION OF FWD PINTLE BUSHES COMPLY WITH FEA 6-5710-F0377949 REV NO. POS. P1 WINGS
- [SDR FDEA202408271178](https://openairdocs.org/sdr/FDEA202408271178.md): Support Rib · corroded · Aug 27, 2024 · N687FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH FWD LUG RIB 5 CORROSION FOUND IN BORE. REMOVED CORROSION FROM R/H MLG RIB 5 FWD LUG PER, E.A.6-5710-T0380346 PT 1
- [SDR FDEA202404300532](https://openairdocs.org/sdr/FDEA202404300532.md): Pitot Tube · clogged · Apr 30, 2024 · N687FE · Airbus A300F4605R · Pitot/Static System
  > IN CRUISE, BOTH CAPT AND FO STANDBY AIRSPEED INDICATORS WERE INACCURATE. STANDBY INDICATORS SEEMED TO INDICATE APPROXIMATELY HALF OF ACTUAL IAS AT ALL ALTITUDES. AT FL340,.787M, 280 IAS, CAPTAIN STANDBY AIRSPEED SHOWED 129 AND FOS SHOWED 130. AT 25K
- [SDR FDEA202307081187](https://openairdocs.org/sdr/FDEA202307081187.md): Actuator · failed · Jul 8, 2023 · N687FE · Airbus A300* · Cargo/Baggage Doors
  > PDIS 687 52-30 5349 08JUL23 MEM OPEN U UPON ARRIVAL IN MEMPHIS. BLOCKED AT GATE.GROUND CREW ADVISED MAIN CARGO DOOR LOCKS WERE OPEN ALONG WITH MAIN HANDLE.NO INDICATIONS IN COCKPIT ECAM DOOR PAGE.UPON VISUAL INSPECTION FOUND LATCHES AND DOOR
- [SDR FDEA202304140643](https://openairdocs.org/sdr/FDEA202304140643.md): Seat Track · damaged · Apr 14, 2023 · N687FE · Airbus A300* · Fuselage Main, Structure
  > HUB REPORTED BROKEN LOCK AT POSITION (3D) DURING LOAD, ID OF LOCK IS (J754) ITEM PLACED ON MEL 25-50-02-01-J WRI2550-5158. THIS ACTION TO OIL SEAT TRACK DAMAGE FOR REPAIR AT LATER DATE. REPAIRED THE DAMAGED SEAT TRACK AT FR28-FR30 -Y953 PER A300-600F SRM53
- [SDR FDEA202108011915](https://openairdocs.org/sdr/FDEA202108011915.md): Valve · failed · Aug 1, 2021 · N687FE · Airbus A300F4605R · Pneumatic Distribution System
  > MDIS 687 36-10 3306 31JUL21 MEM OPEN U FWD GROUND PNUMATIC SUPPLY PORT CHECK VALVE LEAKS AFTER ENGINE AIRSTART COMPLETED. SHGN 31JUL21 23:40 MEM U INSPECTED FWD GROUND PNUMATIC AIR SUPPLY CHECK VALVE. FOUND SPRING THAT NORMALLY CLOSES THE C
- [SDR FDEA202010302723](https://openairdocs.org/sdr/FDEA202010302723.md): Compressor · stalled · Oct 30, 2020 · N687FE · Airbus A300F4605R · Fuel Controlling System
  > AFTER DEPARTURE PASSING 10,000 RECEIVED ENG #2 MODE FAULT FOLLOWED ECAM AND REDUCED POWER AND RESELECT N1 MODE. FAULT CLEARED AFTER 10 SECOND HAD SEVERE BANK AND YAW ON RIGHT SIDE.SUSPECT COMPRESSOR STALL. ACCOMPLISHED BORESCOPE AND ENGINE STALL INSPECTI
- [SDR FDEA202010142485](https://openairdocs.org/sdr/FDEA202010142485.md): Skin · gouged · Oct 14, 2020 · N687FE · Airbus A300F4605R · Leading Edge Devices
  > RT NR 1 SLAT OUTBOARD INNER SURFACE GOUGED (3 LOCATION) RT NR 1 SLAT OUTBOARD INNER SURFACE GOUGED. COMPLIED WITH EA: 6-5750-T0357343 P1. THIS IS CAT A REPAIR. MAJOR REPAIR, IAW GMM 6-2-100.
- [SDR FDEA202010142487](https://openairdocs.org/sdr/FDEA202010142487.md): Beam · cracked · Oct 14, 2020 · N687FE · Airbus A300F4605R · Fuselage Main, Structure
  > NDT INSP LT CENTER WING JOINT AT FR 40 MID HOLE FOUND CRACKED SIGNAL. REAMED THE HOLE THROUGH ALL LAYERS STEP BY STEP 0.4OMM EACH TIME NOT EXCEED R2 DIMENSION, PER A300-600F SRM51-40-44. PERFORMED ROTO-TEST INSPECTION AND NO CRACK FOUND, PER A300-600F NTM51-
- [SDR FDEA202010132470](https://openairdocs.org/sdr/FDEA202010132470.md): Skin · delaminated · Oct 13, 2020 · N687FE · Airbus A300F4605R · Spoilers
  > RT WING NR 5 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED. 20MM X 25MM DEPTH: 1.10MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED. 15MM X 20MM DEPTH: 1.97MM. RT WING NR 5 SPOILER INBOARD HINGE ARM DELAMINATED. COMPLIED WITH EA: 6-5750-T0357149
- [SDR FDEA202010132469](https://openairdocs.org/sdr/FDEA202010132469.md): Skin · delaminated · Oct 13, 2020 · N687FE · Airbus A300F4605R · Spoilers
  > RT WING NR 4 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MMX30MM DEPTH: 1.20MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED, 15MM X 55MM DEPTH: 1.93MM. OUTBOARD HINGE ARM OUTBOARD SURFACE DELAMINTED, 20MM X 25MM DEPTH: 1.20MM. RT WING NR 4 SP
- [SDR FDEA202010132468](https://openairdocs.org/sdr/FDEA202010132468.md): Skin · delaminated · Oct 13, 2020 · N687FE · Airbus A300F4605R · Spoilers
  > LT WING NR 5 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 30MM X 35MM DEPTH: 1.35MM. OUTBOARD HINGE ARM LOWER SURFACE DELAMINATED, 20MM X 55MM DEPTH: 1.95MM. OUTBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MM X 40MM DEPTH: 1.30MM. LT WING NR 5
- [SDR FDEA202010132467](https://openairdocs.org/sdr/FDEA202010132467.md): Skin · delaminated · Oct 13, 2020 · N687FE · Airbus A300F4605R · Spoilers
  > LT WING NR 3 SPOILER INBOARD HINGE ARM OUTBD SURFACE DELAMINATED. 63MM X 23MM DEPTH: 1.50MM LT WING NR 3 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED. COMPLIED WITH EA: 6-5750-T0357145. THIS IS CAT A REPAIR. MAJOR REPAIR, IAW GMM 6-2-100.
- [SDR FDEA202010132466](https://openairdocs.org/sdr/FDEA202010132466.md): Skin · delaminated · Oct 13, 2020 · N687FE · Airbus A300F4605R · Wing, Control Surfaces
  > LT WING NR 4 SPOILER INBOARD HINGE ARM OUTBOARD SURFACE DELAMINATED, 20MM X 15MM DEPTH: 1.30MM. INBOARD HINGE ARM LOWER SURFACE DELAMINATED, 15MM X 20MM DEPTH: 1.90MM. OUTBOARD HINGE ARM OUTBD SURFACE DELAMINATED, 30MM X 20MM DEPTH: 1.27MM. LT WING NR 4 SPO
- [SDR FDEA202007311736](https://openairdocs.org/sdr/FDEA202007311736.md): Handle · unsecure · Jul 31, 2020 · N687FE · Airbus A300F4605R · Cargo/Baggage Doors
  > PASSING 180 CLIMBING, HEARD THUMP AND AIRCRAFT LURCHED. CONTROLS AND CONTROLABILITY FELT NORMAL. FOUND MAIN CARGO DOOR LATCH HANDLE DEPLOYED APPROX.3 INCHES UPON BLOCK IN. OPERATED DOOR SEVERAL TIMES AND OPERATION WAS NORMAL. WHILE UNLATCHING DOOR AT C
- [SDR FDEA202007301729](https://openairdocs.org/sdr/FDEA202007301729.md): Handle · unsecure · Jul 30, 2020 · N687FE · Airbus A300F4605R · Cargo/Baggage Doors
  > PASSING 180, HEARD A THUMP & ACFT LURCHED, CONTROLS & CONTROLABILITY NORMAL. FOUND MAIN CARGO DOOR LATCH HANDLE DEPLOYED APPROX 3 INCHES. OPERATED DOOR SEVERAL TIMES & OPERATION WAS NORMAL. WHILE UNLATCHING DOOR AT CONTROL PANEL, THERE WAS A 2 SEC DELA
- [SDR FDEA2020061631252](https://openairdocs.org/sdr/FDEA2020061631252.md): Smoke Detector · failed · Jun 13, 2020 · N687FE · Airbus A300F4605R · Smoke Detection
  > AFTER TAKE OFF, RECEIVED AN AVIONICS SMOKE ECAM. COMPLIED WIH QRH PROCEDURES AND RETURNED TO DEPARTURE. R & R THE SMOKE DETECTOR 13WA IAW MM 26-15-12-04, TESTED GOOD IAW MM 26-15-00-05. OK FOR SERVICE.
- [SDR FDEA2019081521853](https://openairdocs.org/sdr/FDEA2019081521853.md): Relay · failed · Aug 12, 2019 · N687FE · Airbus A300F4605R · Landing Gear Steering System
  > SHUTDOWN THE NR 1 ENGINE WHILE TAXING IN. AFTER THE HYDRAULIC PRESSURE FELL TO ZERO, THE NOSEWHEEL STEERING LOST HYD PRESSURE AND SLOWLY ROTATED TILLER TO FULL LEFT DEFLECTION. WAS UNABLE TO TURN THE TILLER. RESTARTED THE NR 1 ENGINE, ALL CONTROL OF NWS
- [SDR FDEA201810263022](https://openairdocs.org/sdr/FDEA201810263022.md): Switch · inoperative · Oct 26, 2018 · N687FE · Airbus A300F4605R · Elevator Control System
  > DURING PUSHBACK, AND DURING SECOND ENGINE START, RECEIVED A YELLOW SERVO CONTROL JAMB. REMOVE AND REPLACED RIGHT ELEVATOR YELLOW SYSTEM SERVO CONTROL CONTROL JAMB DETECTION SWITCH IAW MM 27-34-12-04, OPS TESTED GOOD IAW MM 27-34-12-04, OK FOR SERVICE.
- [SDR FDEA201809142526](https://openairdocs.org/sdr/FDEA201809142526.md): Switch · inoperative · Sep 14, 2018 · N687FE · Airbus A300F4605R · Door Warning System
  > ON CLIMB OUT GOT MAIN CARGO DOOR NOT LOCKED. COMPLETED QRH AND RTB CYYC. RELEASED FOR SERVICE. MAIN CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE INOP. REMOVED AND REPLACED WARNING SWITCH 49WS IAW AMM 52-71-00-04-02 AND PERFORMED ADJUSTMENT/TEST IAW
- [SDR FDEA201804130987](https://openairdocs.org/sdr/FDEA201804130987.md): Frame · cracked · Apr 13, 2018 · N687FE · Airbus A300F4605R · Fuselage Main, Frame
  > UNDER FLOOR PANEL 242YH AT -Y225, FRAME 47 WEB IS CRACKED. REMOVED AND REPLACED DAMAGED WEB IAW SRM 51-40-21. WEB FABRICATED ON T18/1334842 IAW SRM 53-15-15 CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201804130986](https://openairdocs.org/sdr/FDEA201804130986.md): Floor Panel · broken · Apr 13, 2018 · N687FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 231GG FLOOR PANEL BROKEN FABRICATED NEW PANEL 231GG ON T18/1334619 IAW DWG SRZ 25-005 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201804130985](https://openairdocs.org/sdr/FDEA201804130985.md): Floor Panel · damaged · Apr 13, 2018 · N687FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 232GG FLOOR PANEL BROKEN FABRICATED NEW PANEL 232GG ON T18/1334801 IAW DWG SRZ 25-005 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N687FE/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 = 'N687FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N687FE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.