# Service difficulty reports: N688FE

A list on [N688FE](https://openairdocs.org/aircraft/N688FE.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 2 · 58 reports

- [SDR FDEA202606161352](https://openairdocs.org/sdr/FDEA202606161352.md): Adapter · cracked · Jun 16, 2026 · N688FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFTER REMOVING DAMAGED LOCK MC1550 AT POS 8L, FOUND SEAT TRACK LOBE DAMAGE AT SAME LOCATION. IAW WRI 25-50/8376. SEAT TRACK LOBE DAMAGE UNDER LOCK MC1550 AT POS 8L. REMOVED DAMAGED SEAT TRACK ADAPTER FITTING ON MAIN DECK CARGO AT POS 8L IAW SRM 51-40-20. DWG
- [SDR FDEA202603150376](https://openairdocs.org/sdr/FDEA202603150376.md): Web · cracked · Mar 15, 2026 · N688FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC UNDER FLOOR WEB AT FR47, BETWEEN Y0 AND -Y450 CRACKED. REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN Y0 AND -Y450 PER A300- 600F SRM53-15-15-201-C2. THIS REPAIR IS CATEGORY B PER A300-600F SRM53-15-15-201-C2, IT MUST BE INSPECTED AT DEFI
- [SDR FDEA202603150375](https://openairdocs.org/sdr/FDEA202603150375.md): Web · cracked · Mar 15, 2026 · N688FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC UNDER FLOOR WEB AT FR47, BETWEEN Y0 AND Y450 CRACKED. REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN Y0 AND Y450 PER A300- 600F SRM53-15-15-201-C2. THIS REPAIR IS CATEGORY B PER A300-600F SRM53-15-15-201-C2, IT MUST BE INSPECTED AT DEFINED
- [SDR FDEA202603130392](https://openairdocs.org/sdr/FDEA202603130392.md): Actuator · faulted · Mar 13, 2026 · N688FE · Airbus A300F4605R · Cargo/Baggage Doors
  > CARGO DOOR HYD SYS, DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24, AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN
- [SDR FDEA202603120364](https://openairdocs.org/sdr/FDEA202603120364.md): Floor Support · corroded · Mar 12, 2026 · N688FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC FLOOR SUPPORT AT FR11-FR14, Y730 CORRODED. FABRICATED THE REPAIR PART PER DWG: A53613824. REPLACED THE MDCC CORRODED FLOOR SUPPORT(EXTRUSION) AT FR11-FR14, Y730 PER SRM51-40-21.THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202603110351](https://openairdocs.org/sdr/FDEA202603110351.md): Rib · cracked · Mar 11, 2026 · N688FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386775 P1 TO REPAIR RT CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RI
- [SDR FDEA202603110350](https://openairdocs.org/sdr/FDEA202603110350.md): Rib · cracked · Mar 11, 2026 · N688FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0386774 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB26 BETWEEN STGR2.6 AND REAR SPAR, RIB
- [SDR FDEA202602180230](https://openairdocs.org/sdr/FDEA202602180230.md): Safety Wire · wrong part · Feb 18, 2026 · N688FE · Airbus A300F4605R · Escape Slide
  > WHILE ACCOMPLISHING EA 6-2560-F386375 REV A PART 1. FOUND THE EJECTOR BAG RELEASE CABLE SAFETY WIRE WAS IN CORRECT. L1 DOOR SLIDE - 3831690 EA: 6-2560-F0386375 REV A PART 1 INSTALLED CAD PLATED SAFETY WIRE TO THE EJECTOR BAG RELEASE CABLE.
- [SDR FDEA202602180228](https://openairdocs.org/sdr/FDEA202602180228.md): Safety Wire · wrong part · Feb 18, 2026 · N688FE · Airbus A300F4605R · Escape Slide
  > L1DOOR ESCAPE SLIDE NEEDS TO BE REMOVED TO ACCOMPLISH EA G-2560-F0386282 PART 1 REF WRI 25-60-8181. ESCAPE SLIDE DID NOT HAVE THE CAD PLATED SAFETY WIRE INSTALLED. EA: G-2560-F0386282 C PART 1 AMM: 25-61-21-04 REMOVED AND REINSTALLED L1 DOOR SLIDE AFTER C
- [SDR FDEA202512052221](https://openairdocs.org/sdr/FDEA202512052221.md): Smoke Detector · failed · Dec 5, 2025 · N688FE · Airbus A300F4605R · Smoke Detection
  > AVIONICS SMOKE WARNING ON TAKEOFF. WARNING CONTINUED UNTIL SHUTDOWN. EMERGENCY DECLARED. CONFIRMED NO OIL/HYDRAULIC ODOR IN FLIGHT DECK, AVIONICS COMPARTMENT. OPENED C/B 1WA (F25) AND NO ALERT MESSAGES OR FAULT LIGHT. SMOKE DETECTOR 13WA REQUIRES REPLACEME
- [SDR FDEA202411261737](https://openairdocs.org/sdr/FDEA202411261737.md): Trim System · malfunctioned · Nov 26, 2024 · N688FE · Airbus A300F4605R · Rudder Tab Control System
  > RUDDER TRIM REQUIRED 18 UNITS OF RIGHT TRIM TO FLY COORDINATED AT CRUISE. PER CREW DEBRIEFING AT LAX, THEY EXPLAINED THAT AFTER ENGINE START AT LBB THEY GOT PITCH FEEL SYS 2 FAULT AND RUDDER TRAVEL SYS FAULT. THEY RESET THE SWITCHES AND FAULT CLEARED, DUR
- [SDR FDEA202410281597](https://openairdocs.org/sdr/FDEA202410281597.md): Bushing · corroded · Oct 28, 2024 · N688FE · Airbus A300F4605R · Wing, Landing Gear Attach Fittings
  > CORROSION FOUND BETWEEN BUSHES D AND E LMLG C/W EA 6-5710-T0317860A P2 WINGS-BASIC WING STRUCTURE-CORROSION REPAIROF RIB 5 FWD LUG LH MAJOR REPAIR.( CAT. C REPAIR)
- [SDR FDEA202311021823](https://openairdocs.org/sdr/FDEA202311021823.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > LH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (17MM*12MM, DEPTH: 1.7MM) AND O/B SIDE (30MM*10MM, DEPTH: 1.1MM) FOUND DELAMINATION REPAIRED LH WING #5 SPOILER CENTER O/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5
- [SDR FDEA202311021822](https://openairdocs.org/sdr/FDEA202311021822.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > RH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (25MM*15MM, DEPTH: 2.1MM) & O/B SIDE (20MM*15MM, DEPTH: 1.4MM) AND CENTER I/B HINGE O/B SIDE (20MM*15MM, DEPTH: 1.07MM) FOUND DELAMINATION RH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE DELAMINATION WAS
- [SDR FDEA202311021821](https://openairdocs.org/sdr/FDEA202311021821.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > RH WING #3 SPOILER CENTER I/B HINGE O/B SIDE FOUND DELAMINATION (15MM*15MM, DEPTH: 1.22MM) REPAIRED RH WING #3 SPOILER CENTER I/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5 & EA 6-5750-T0376848 P1. MAJOR REPAIR I
- [SDR FDEA202310281808](https://openairdocs.org/sdr/FDEA202310281808.md): Slat · unknown · Oct 28, 2023 · N688FE · Airbus A300* · Leading Edge Devices
  > EXISTING REPAIR ON RH WING #1 SLAT END RIB 2A, FROM I/B EDGE ABOUT 7" REQUIRES EVALUATION FOR CONFORMITY COMPLIED WITH EA 6-5750-T0376898 A P1. REPAIRED THE RH WING #1 SLAT EXISTING REPAIR AT INBOARD EDGE CLOSE TO RIB 2A. THIS IS CAT A REPAIR AND THIS REP
- [SDR FDEA202310241793](https://openairdocs.org/sdr/FDEA202310241793.md): Seat Track · none · Oct 24, 2023 · N688FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR28-FR30, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR28 - FR30, Y450 WAS EVALUATED AND FOUND NOT CONFORMITY WITH A300-600F SRM53-10-16 FIG.201. REPORTED I
- [SDR FDEA202310231789](https://openairdocs.org/sdr/FDEA202310231789.md): Seat Track · none · Oct 23, 2023 · N688FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR56-FR57.2, Y0 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT FR56-FR57.2, Y0 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201. EO: 6-5100-7-5000 D
- [SDR FDEA202308311531](https://openairdocs.org/sdr/FDEA202308311531.md): Heat Shield · damaged · Aug 31, 2023 · N688FE · Airbus A300* · Brake
  > HEAT SHIELD BROKE OFF ON #4 MLG TIRE AND WHEEL ASSY. DURING WALKAROUND NOTED HEAT SHIELD PROTRUDING FROM THE WHEEL ASSY. REMOVED AND REPLACED TIRE AND WHEEL ASSY.
- [SDR FDEA202303030372](https://openairdocs.org/sdr/FDEA202303030372.md): Unknown · unknown · Mar 3, 2023 · N688FE · Airbus A300F4605R · Hydraulic Power System
  > AT CRUISE FL 290 GREEN SYSTEM LOW PRESSURE CAUTION WITH HYDRAULIC FLUID AT RED DOT. COMPLIED WITH ECAM AND QRH PROCEDURE. EMERGENCY DECLARED. PERFORMED FREE FALL RESORATION. CHECKS GOOD. FOUND HYDRAULIC LEAKING UNDER LEFT ENGINE. FOUND LEAKING O-RINGS AT H
- [SDR FDEA202303020359](https://openairdocs.org/sdr/FDEA202303020359.md): Pressure Switch · failed · Mar 2, 2023 · N688FE · Airbus A300* · Hydraulic Power System
  > AT CRUISE FL320 GREEN SYS LO PRESS CAUTION WITH HYD FLUID AT RED DOT ON OVERHEAD PANEL AND IN AMBER RANGE ON ECAM (50 PSI). COMPLIED WITH ECAM AND QRH PROCEDURE, MANUAL EXTENDED GEAR AND EMERGENCY DECLARED. ECAM MESSAGES KEPT CYCLING CONSTANTLY AS IF PRO
- [SDR FDEA202208022077](https://openairdocs.org/sdr/FDEA202208022077.md): Brake Sys · malfunctioned · Aug 2, 2022 · N688FE · Airbus A300F4605R · Landing Gear Brake System
  > PDIS 688 32-43 4514 02AUG22 MEM FACT U AFTER LANDING AND LEAVING RUNWAY, LOST BRAKING FOR A FEW SECONDS. AS BRAKE PEDALS WERE DEPRESSED, NO BRAKING WAS OCCURRING. BRAKE PEDAL FEEL WAS NORMAL, BUT NO BRAKES. JUST BEFORE RELEASING THE PEDDLES
- [SDR FDEA202104291067](https://openairdocs.org/sdr/FDEA202104291067.md): Fitting · cracked · Apr 29, 2021 · N688FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0361325 P1, TITLE: WINGS - BASIC WING STRUCTURE- CRACK HOLE C AT FR47 LHS DURING SB57-6121 EM
- [SDR FDEA202104271046](https://openairdocs.org/sdr/FDEA202104271046.md): Skin · corroded · Apr 27, 2021 · N688FE · Airbus A300F4605R · Wing, Control Surfaces
  > LH O/B FLAP UPPER SURFACE SKIN FOUND SEVERE CORROSION AT O/B STATIC DISCHARGER BASE COMPLIED WITH EA 6-5750-T0361302 P1, TITLE: WINGS - FLIGHT SURFACES - LH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION UNDERNEATH STATIC DISCHARGER - TRIMOUT/DOUBLER R
- [SDR FDEA202104090863](https://openairdocs.org/sdr/FDEA202104090863.md): Sensor · faulted · Apr 9, 2021 · N688FE · Airbus A300F4605R · Fuel Boost Pump
  > PDIS 688 00-00 3337 09APR21 MEM OPEN U CLIMBING THROUGH APPROXIMATELY FL280, 12 MINUTES INTO FLIGHT, BOTH CENTER TANK FUEL BOOST PUMPS FAULTED SIMULTANEOUSLY. FOLLOWED ECAM / QRH, PULLED AND RESET CB M55 ON 132 VU. PUMPS WERE INITIALLY RECOVE
- [SDR FDEA2020070211413](https://openairdocs.org/sdr/FDEA2020070211413.md): Windshield · cracked · Jul 1, 2020 · N688FE · Airbus A300F4605R · Flight Compartment Windows
  > CAPTAIN'S WINDSCREEN DEVELOPED CRACK THAT CONTINUED TO GROW AT FL 310. STOPPED GROWING ONCE WE SLOWED DOWN & DESCENDED. CORROBORATED A CRACK ON CAPT'S WINDSHIELD INNER PANE, APPROX. 22 INCHES LONG, FROM TOP LEFT CORNER DIAGONAL TOWARD RIGHT BOTTOM CORNER. L
- [SDR FDEA2018101602842](https://openairdocs.org/sdr/FDEA2018101602842.md): Floor Panel · damaged · Oct 10, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131HH DAMAGED AT EDGE COMMON TO FASTENER HOLES. FABRICATED 1EA PANEL 131HH ON T18/1370485 PER SRZ-25-005. MAJOR REPAIR CAT "A".
- [SDR FDEA2018101602841](https://openairdocs.org/sdr/FDEA2018101602841.md): Floor Panel · damaged · Oct 10, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131KH DAMAGED AT FASTENER HOLES. FABRICTED 1EA PANEL 131KH ON T18/1370484 PER SRZ-25-005. MAJOR REPAIR CAT "A".
- [SDR FDEA2018101602840](https://openairdocs.org/sdr/FDEA2018101602840.md): Seat Track · gouged · Oct 10, 2018 · N688FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK -Y1959 AT FRAME 57.2 TO 58 HAS 3EA GOUGES IN TRACK REMOVED DAMAGE AREAS IAW SRM 51-73-10. CHECKED LIMITS. MAX MATERIAL REMOVED IS.028 AFTER REWORK L=.2 W=.400 D=.035 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 201 TR 83340. FABRICATED NEW SEA
- [SDR FDEA2018101602839](https://openairdocs.org/sdr/FDEA2018101602839.md): Seat Track · worn · Oct 10, 2018 · N688FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > WORN OUT SEAT TRACK CROWN AREA Y450 BETWEEN STA 54.2 TO 54.3 BLENDED DAMAGE IAW SRM 51-73-10. CHECK LIMITS, MAX MATERIAL REMOVED IS.028 AFTER REWORK. L= 2.0 W=.400 D=.040 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 201 TR 83340. FABRICATED NEW SEAT TRACK
- [SDR FDEA201810052796](https://openairdocs.org/sdr/FDEA201810052796.md): Floor Panel · broken · Oct 5, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 251YG FLOOR PANEL BROKEN. FABRICATED 251YG FLOOR PANEL ON T18/1369457 IAW SRZ-25-005 CAT "A" MAJOR REPAIR. INSTALLED ON WORK CARD 250-FL-FIT SEQ#000062
- [SDR FDEA201810052795](https://openairdocs.org/sdr/FDEA201810052795.md): Floor Panel · broken · Oct 5, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 241RJ FLOOR PANEL BROKEN. FABRICATED 241RJ FLOOR PANEL ON T18/1869458 IAW SRZ-25-005. CAT "A" MAJOR REPAIR. INSTALLED ON WORK CARD 240-FL-FIT SEQ# 000060
- [SDR FDEA201810052793](https://openairdocs.org/sdr/FDEA201810052793.md): Floor Panel · damaged · Oct 5, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 241LK FLOOR PANEL BROKEN. FABRICATED 241LK FLOOR PANEL ON T18/1369459 IAW SRZ-25-005. CAT "A" MAJOR REPAIR. INSTALLED ON WORK CARD 240-FL-FIT SEQ# 000060
- [SDR FDEA2018100542778](https://openairdocs.org/sdr/FDEA2018100542778.md): Floor Panel · damaged · Oct 4, 2018 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 251DF FLOOR PANEL BROKEN. FABRICATED 251DF FLOOR PANEL ON T18/1369581 IAW SRZ 25-005, REPAIR IS CLASSIFIED AS CAT "A" AND MAJOR REPAIR.
- [SDR FDEA201708162225](https://openairdocs.org/sdr/FDEA201708162225.md): Fork · cracked · Aug 16, 2017 · N688FE · Airbus A300F4605R · Cargo/Baggage Doors
  > DURING EO E6-5230-EO0330595P2 FOR THE AFT DOOR LATCH INSPECTION, FOUND CRACK INDICATIONS ON BOTH FRONT AND AFT SIDES OF FRAMES C61 AND C61A. REMOVED AND REPLACED THE AFT CARGO DOOR WITH A SERVICEABLE UNIT. COMPLIED WITH E6-5230-E0330595P2.
- [SDR FDEA201506011672](https://openairdocs.org/sdr/FDEA201506011672.md): Rib · corroded · Jun 1, 2015 · N688FE · Airbus A300F4605R · Wing Spar
  > RIGHT MOVING MLG FWD LUG HAS CORROSION IN BORE & BOTH FACES. OMPLIED WITH EA 6-5710-T0317866. WINGS-BASIC STRUCTURE CORROSION REPAIR OF RIB 5.. FORWARD LUG RH.
- [SDR FDEA201506011671](https://openairdocs.org/sdr/FDEA201506011671.md): Rib · corroded · Jun 1, 2015 · N688FE · Airbus A300F4605R · Wing Spar
  > LT MLG FWD LUG HAS CORROSION IN BORE AND BOTH FACES COMPLIED WITH EA 6-5710-T0317860 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG LH
- [SDR FDEA201409072525](https://openairdocs.org/sdr/FDEA201409072525.md): Control Handle · failed · Sep 7, 2014 · N688FE · Airbus A300F4605R · Landing Gear Selector
  > AFTER TAKEOFF, RECEIVED A LANDING GEAR RETRACTION FAULT ON THE ECAM. FOLLOWED THE ECAM PROCEDURES & PLACED LANDING GEAR HANDLE IN THE DOWN POSITION. ALL GEAR DOWN INDICATIONS WERE NORMAL. LEAK CHECKED ELEC HYDRAULIC VALVE GOOD & STILL FAILED OPS CHECK. R &
- [SDR FDEA201405010917](https://openairdocs.org/sdr/FDEA201405010917.md): Indicator · faulty · May 1, 2014 · N688FE · Airbus A300F4605R · Fuel Quantity Indicator
  > ON ACFT POWER UP NOTICED AUTO LAND LIGHT, ANNUNCIATOR, FUEL TANK LOW LEVEL LIGHT, ENG & APU FIRE HANDLE LIGHT ALL REMAIN ON & FLICKER. R & R FUEL QTY IND IAW 28-42-41-04 FLICKERING STOP, AUTO LAND, FIRE HANDLE LIGHTS WENT OUT. CONNECTOR PLUGS WERE INSTALLED
- [SDR FDEA201402280423](https://openairdocs.org/sdr/FDEA201402280423.md): Filter · dirty · Feb 28, 2014 · N688FE · Airbus A300F4605R · Hydraulic System, Main
  > DURING CRUISE, ECAM WARNING FOR GREEN HYD LOW PRESSURE. PRESSURE INDICATED ZERO. GREEN HYD GAUGE ON OVERHEAD PANEL INDICATED LEVEL AT RED DOT. ECAM FLUID LEVEL INDICATED TOP OF RED BAND. CRANKED GEAR, NORMAL LANDING. AFTER ENGINE SHUTDOWN, GREEN LEVEL ON
- [SDR FDEA201402160327](https://openairdocs.org/sdr/FDEA201402160327.md): Connector · burned · Feb 16, 2014 · N688FE · Airbus A300F4605R · Equipment/Furnishings Wiring
  > WHILE WORKING LOWER FWD CARGO LOADING SYS IAW WRI 25-50 4866 & 25-504867. FOUND CONNECTOR DISCONNECTED & BAGGED IAW EA, BURNED & MELTED BAG PINS CONNECTOR & SURROUNDING WIRES. R & R COMPARTMENT CONTROL BOX & CONNECTOR. R &R CONNECTOR 230MY1B IAW WDM 25-52-0
- [SDR FDEA201402060272](https://openairdocs.org/sdr/FDEA201402060272.md): Transmitter · failed · Feb 6, 2014 · N688FE · Airbus A300F4605R · Hydraulic Quantity Sensor
  > ON DESCENT INTO AFW LOST GREEN SYS HYD QTY CONFIRMED BY ECAM HYD PAGE & GREEN SYS HYD QTY GAUGE. RAN QRH LOWERED GEAR MANUALLY. REMOVED & REPLACED GREEN SYSTEM HYD RES QTY TRANSMITTER IAW AMM 29-31-11-04, AND NO LEAKS NOTED ON OPS CHECK AND TRANSMITTER OPS C
- [SDR FDEA201401240191](https://openairdocs.org/sdr/FDEA201401240191.md): Skin · worn · Jan 24, 2014 · N688FE · Airbus A300F4605R · Wing, Plate/Skin
  > RIGHT WING RIBS 9 & 10 TE EDGE LOWER SKIN FASTENER HOLE FOR PYLON PIPE WORN OUT. REPAIRED IAW EA 6-5730-T0 305573 P.
- [SDR FDEA201401240190](https://openairdocs.org/sdr/FDEA201401240190.md): Skin · worn · Jan 24, 2014 · N688FE · Airbus A300F4605R · Wing, Plate/Skin
  > LEFT WING RIBS 9 & 10 TE LOWER SKIN FASTENER HOLE FOR PYLON PIPE WORN OUT. REPAIRED IAW EA 6-5730-T0305553 P1.
- [SDR FDEA201212014225](https://openairdocs.org/sdr/FDEA201212014225.md): Transmitter · leaking · Dec 1, 2012 · N688FE · Airbus A300F4605R · Hydraulic Indicating System
  > LOSS OF BLUE HYD SYS QTY AT ALTITUDE. FLUID LEVEL DOWN TO RED DOT ON GAUGE. FOLLOWED QRH, SHUT PUMPS DOWN IAW ECAM WARNINGS BEFORE AT RED LINE ON LEVEL INDICATION. SERVICED SYS IAW MM 12-12-29-0. R & R BLUE HYD QTY TRANSMITTER IN REF MM 29-31-11-04. RA
- [SDR FDEA201209063245](https://openairdocs.org/sdr/FDEA201209063245.md): Spring · broken · Sep 6, 2012 · N688FE · Airbus A300F4605R · Door Warning System
  > AVIONICS DOOR CAME OPEN IN FLIGHT (121BL). DOOR DID NOT OPEN BUT CREW GOT LIGHT IN COCKPIT. FOUND SPRING BROKEN. R & R THE DOOR HANDLE TENSION SPRINGS IAW MM 52-41-14-04. OPS TESTED GOOD. DOOR CLOSES SECURLY AND INDICATES ON ECAM.
- [SDR FDEA201109173928](https://openairdocs.org/sdr/FDEA201109173928.md): Bracket · cracked · Sep 17, 2011 · N688FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON REAR TOP END HYD LINE FITTING MOUNTING PLATE CRACKED AT 3 FASTENER HOLES AT WING ATTACHMENT 3" LONG 2" AND 1" LONG. DISCONNECTED LT AFT FAIRING HYD LINES IAW AMM 54-54-00-04 REPLACED WEB IAW SRM 51-72-00 REMOVED AND REINSTALLED AVIONICS WIRE BUND
- [SDR FDEA201109113827](https://openairdocs.org/sdr/FDEA201109113827.md): Seat Track · gouged · Sep 11, 2011 · N688FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FR 57.1 SEAT TRACK 2L HAS 2EA GOUGED SCALLOPS 9" APART. REMOVED IAW AMM 53-10-25-04-02. CUT AND FABRICATED NEW SEAT TRACK IAW SRM 53-10-16 P.205. APPLIED PROTECTIVE COATING IAW SRM 51-75-10. INSTALLED SEAT TRACK IAW SRM 53-10-16, P205.
- [SDR FDEA201109083780](https://openairdocs.org/sdr/FDEA201109083780.md): Floorbeam · bent · Sep 8, 2011 · N688FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > IN MAIN CABIN, CROSS SECTIONS BETWEEN SEAT TRACKS 1 AND 2R AT FRAMES 48, 49 AND 50 BENT REMOVED CROSS SECTIONS IAW SRM 51-40-21. CROSS SECTIONS CRACKED WHILE ATTEMPTING TO REFORM. FABRICATED NEW SECTIONS FROM 2024T-3 IAW AB DWG A53813978. INSTALLED NEW
- [SDR FDEA201109083762](https://openairdocs.org/sdr/FDEA201109083762.md): Floor Panel · delaminated · Sep 8, 2011 · N688FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL 131NH HAS A 3.25 " LONG DELAMINATION. FABRICATED A REPLACEMENT PANEL 131NH IAW DWG SRZ-25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N688FE/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 = 'N688FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N688FE/reports

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