# Service difficulty reports: N691FE A list on [N691FE](https://openairdocs.org/aircraft/N691FE.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 · 71 reports - [SDR FDEA202602190235](https://openairdocs.org/sdr/FDEA202602190235.md): Valve · faulted · Feb 19, 2026 · N691FE · Airbus A300F4605R · Escape Slide > THE L1 DOOR SLIDE EJECTOR BAG INFLATOR VALVE ACTUATING ARM HAS THE INCORRECT BREAKAWAY SAFETY WIRE INSTALLED. FOUND WHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 REV A. SHGN 18FEB26 21:50 MEM FEA: 6-2560-F0386375 REV A CMM: 25-60-40 INSTALLED THE CORRE - [SDR FDEA202504210627](https://openairdocs.org/sdr/FDEA202504210627.md): Skin · delaminated · Apr 21, 2025 · N691FE · Airbus A300F4605R · Spoilers > LH WING #4 SPOILER CENTER I/B HINGE ARM OUTBD SKIN FOUND DELAMINATION. SIZE: 40MM*30MM, DEPTH: 0.93MM COMPLIED WITH EA:6-5750-T0382761 P1, EA TITLE: WING - FLIGHT SURFACES - LH #4 SPOILER CENTER HINGE ARM OUTSIDE SURFACES DELAMINATION. REPAIRED LH WING #4 S - [SDR FDEA202504030560](https://openairdocs.org/sdr/FDEA202504030560.md): Fitting · not reported · Apr 3, 2025 · N691FE · Airbus A300F4605R · Cargo/Baggage Doors > COMPLY WITH EO 6-5230-E0378588 B P5 FOR MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS REPLACEMENT. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FI - [SDR FDEA202504010590](https://openairdocs.org/sdr/FDEA202504010590.md): Floor Support · cracked · Apr 1, 2025 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK FLOOR STRUCTURE - LH FLOOR SUPPORT CRACKED, BETWEEN FR38.1 AND FR38.2, AT Y2462 REPLACED THE CRACKED SUPPORT IN MAIN DECK FLOOR STRUCTURE - LH BETWEEN FR38.1 AND FR38.2, AT Y2462 PER A300-600F SRM51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR - [SDR FDEA202503310564](https://openairdocs.org/sdr/FDEA202503310564.md): Floor Support · misrepaired · Mar 31, 2025 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > EXISTING REPAIR ON MDCC RH FLOOR SUPPORT AT FR38.1 - FR38.2, -Y2462 REQUIRES EVALUATION FOR CONFORMITY EXISTING REPAIR ON MDCC RH FLOOR SUPPORT AT FR38.1 - FR38.2, -Y2462 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH DWG: A53781038 (ISSUE.G). REPLACED THE - [SDR FDEA202503310565](https://openairdocs.org/sdr/FDEA202503310565.md): Repair · cracked · Mar 31, 2025 · N691FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MDCC CROSSBEAM AT FR50, BETWEEN Y0 AND -Y450 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON MDCC CROSSBEAM AT FR50, BETWEEN Y0 AND -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53813946 (ISSUE.A00) AND FOUND CRACK. REPLA - [SDR FDEA202503280551](https://openairdocs.org/sdr/FDEA202503280551.md): Seat Track · misrepaired · Mar 28, 2025 · N691FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > EXISTING REPAIR ON MDCC SEAT TRACK AT FR31 - FR34, Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC SEAT TRACK AT FR31 - FR34, Y1959 AND FOUND NOT CONFORMITY WITH A300-600F SRM53-10-16-201. FIG.201A. DUE TO FASTENERS NOT MEET. REPAIRE - [SDR FDEA202503260555](https://openairdocs.org/sdr/FDEA202503260555.md): Skin · corroded · Mar 26, 2025 · N691FE · Airbus A300F4605R · Fuselage Main, Plate/Skin > LH FWD FUSELAGE TOILET SERVICE PANEL CUTOUT SKIN STIFFENER CORRODED. REPLACED THE HEAVY CORRODED STIFFENER (SKIN) ON LH FWD FUSELAGE TOILET SERVICE PANEL CUTOUT PER A300-600F SRM 51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100. - [SDR FDEA202503250567](https://openairdocs.org/sdr/FDEA202503250567.md): Seat Track · unknown · Mar 25, 2025 · N691FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > EXISTING REPAIR ON MDCC SEAT TRACK AT FR58-FR62, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT FR58 - FR62, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201. EO 6 - [SDR FDEA202503250566](https://openairdocs.org/sdr/FDEA202503250566.md): Seat Track · unknown · Mar 25, 2025 · N691FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > EXISTING REPAIR ON MDCC SEAT TRACK AT FR58-FR62, Y0 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT FR58 - FR62, Y0 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201. EO 6- 510 - [SDR FDEA202501220121](https://openairdocs.org/sdr/FDEA202501220121.md): Valve · underserviced · Jan 22, 2025 · N691FE · Airbus A300F4605R · Hydraulic Reservoir, Main > IN CRUISE FLIGHT GOT GREEN HYDRAULIC RSV LO LEVEL. BOTH ECAM AND OVERHEAD GAUGE SHOWED QUANTITY NEAR ZERO. RAN QRH, ALTERNATE EXTENDED GEAR AND GOT TOWED IN AFTER LANDING. EMERGENCY DECLARED AMM: 29-14-00-03 SERVICED GREEN RESERVOIR HEAD PRESSURE. WIT - [SDR FDEA202305110852](https://openairdocs.org/sdr/FDEA202305110852.md): Windshield · cracked · May 11, 2023 · N691FE · Airbus A300F4605R · Flight Compartment Windows > AT FL360, CAPTAIN S WINDSHIELD BEGAN ARCING AT BOTTOM LEFT BASE. SHORTLY AFTER IT BEGAN ARCING, WINDSHIELD SHATTERED ACROSS ENTIRE SCREEN. FOLLOWED QRH AND TURNED OFF WINDOW HEATER. NO CRACKING OBSERVED ON INSIDE OF COCKPIT. DECLARED AN EMERGENCY AND LAND - [SDR FDEA202303100398](https://openairdocs.org/sdr/FDEA202303100398.md): Unknown · unknown · Mar 10, 2023 · N691FE · Airbus A300F4605R · Fire Detection > DOWNWIND AT 3000 FT WENT TO SLATS EXTEND AND IMMEDIATELY GOT A MASTER WARNING FOR AVIONICS SMOKE, FO STATED HE THOUGHT HE SAW SMOKE. DECLARED EMERGENCY AND LANDED. AFTER LANDING WE COULD NOT SMELL SMOKE OR SEE VISIBLE SIGNS OF SMOKE. AFTER FIRE DEPARTME - [SDR FDEA202301280171](https://openairdocs.org/sdr/FDEA202301280171.md): Window · cracked · Jan 28, 2023 · N691FE · Airbus A300F4605R · Flight Compartment Windows > FO FRONT WINDOW ARCED IN FLIGHT AND CRACKED. NO CRACK ON INTERIOR SURFACE. QRH PROCEDURE ACCOMPLISHED. REMOVED F/O FIXED WINDSHIELD PANEL IAW AMM 56-11-11-04. INSTALLED FIRST OFFICER WINDSHIELD PANELS IAW AMM 56-11-11-04 UP TO AND INCLUDING STEP 2. E. - [SDR FDEA202105251397](https://openairdocs.org/sdr/FDEA202105251397.md): Indication Sys · malfunctioned · May 25, 2021 · N691FE · Airbus A300F4605R · Fuel Indicating System > RIGHT INNER TANK QUANTITY INDICATION MEL D INOP. ON CLIMB OUT RT INNER TANK PUMP FAULTED. COMPLIED WITH ECAM AND QRH AND TURNED PUMP OFF. NOTICED RIGHT OUTER TANK WAS BURNING DOWN AND NOT THE RIGHT INNER TANK. TURNED ON CROSSFEED VALVE TO FEED FROM LEFT I - [SDR FDEA2019122073257](https://openairdocs.org/sdr/FDEA2019122073257.md): Position Switch · inoperative · Dec 17, 2019 · N691FE · Airbus A300F4605R · Leading Edge Slat Position Indicating System > KRUGER FAULT WHEN SLATS WERE EXTENDED. T/S IN REF TO TSM 27-80-00, REMOVED AND REPLACED LT EXTEND KRUEGER FLAP POSITION SWITCH IN REF TO AMM 27-89-13-04, CYCLED SEVERAL TIMES WITH NO KRUEGER FLAP LIGHT OR SFCC FAULTS, A/C REMOVED FROM MEL CONFIG. A/C OK FOR - [SDR FDEA2018081402028](https://openairdocs.org/sdr/FDEA2018081402028.md): Smoke Warning · false activation · Jun 20, 2018 · N691FE · Airbus A300F4605R · Smoke Detection > DURING DESCENT, AS POWER WAS RETARDED AT 7000 - 8000 FT, ECAM POPULATED WITH MIN EQUIPMENT BAY SMOKE. BEGAN TO CONFIRM, ECAM WARNING WENT AWAY. NO SMOKE NOTICED. CREW VERIFIED NO SMOKE PRESENT. PERFOMED AVIONICS SMOKE RTS IAW AMM 26-15-00-05. OPS CHECK - [SDR FDEA2018062201546](https://openairdocs.org/sdr/FDEA2018062201546.md): Smoke Detector · failed · Jun 20, 2018 · N691FE · Airbus A300F4605R · Smoke Detection > ON SHORT FINAL, AMBER WARNING, ECAM-MIN EQPT. BAY SMOKE, NO-SMOKE FROM SNIFFER FAN. WARING WENT AWAY, BUT CME BACK TWICE. ONCE LANDED, THE WARING STOPPED. NO SMOKE DETECTED. REPLACED EQPT BAY DUCT SMOKE DETECTOR 12WA IAW AMM 26-15-12. - [SDR FDEA201803070616](https://openairdocs.org/sdr/FDEA201803070616.md): Floor Panel · damaged · Mar 7, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL B5327115400200 DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. FLOOR PANEL INSTALLED. MAJOR REPAIR - [SDR FDEA201803070615](https://openairdocs.org/sdr/FDEA201803070615.md): Seat Track · cracked · Mar 7, 2018 · N691FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK BL Y1959, FRAME 60 CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21, AND DWG A53274786. MAJOR REPAIR - [SDR FDEA201803010544](https://openairdocs.org/sdr/FDEA201803010544.md): Floor Panel · cracked · Mar 1, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241RH CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. - [SDR FDEA201803010543](https://openairdocs.org/sdr/FDEA201803010543.md): Floor Panel · cracked · Mar 1, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252KG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. - [SDR FDEA201803010542](https://openairdocs.org/sdr/FDEA201803010542.md): Floor Panel · cracked · Mar 1, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241DF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. - [SDR FDEA201803010541](https://openairdocs.org/sdr/FDEA201803010541.md): Floor Support · broken · Mar 1, 2018 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN CABIN RT SIDEWALL FLOOR SUPPORT BROKEN BETWEEN FRAMES 38.1 AND 38.2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR. - [SDR FDEA201802280520](https://openairdocs.org/sdr/FDEA201802280520.md): Floor Panel · cracked · Feb 28, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 251WH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A MAJOR REPAIR. - [SDR FDEA201802280519](https://openairdocs.org/sdr/FDEA201802280519.md): Floor Panel · cracked · Feb 28, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252VF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A MAJOR REPAIR. - [SDR FDEA201802280518](https://openairdocs.org/sdr/FDEA201802280518.md): Floor Panel · cracked · Feb 28, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252VH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A MAJOR REPAIR. - [SDR FDEA201802280517](https://openairdocs.org/sdr/FDEA201802280517.md): Floor Panel · cracked · Feb 28, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241LK DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A MAJOR REPAIR. - [SDR FDEA201802280516](https://openairdocs.org/sdr/FDEA201802280516.md): Floor Panel · cracked · Feb 28, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 241TH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 CLASSIFIED AS A CATAGORY A MAJOR REPAIR. - [SDR FDEA201802270511](https://openairdocs.org/sdr/FDEA201802270511.md): Floor Panel · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 242TH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. MAJOR REPAIR. - [SDR FDEA201802270510](https://openairdocs.org/sdr/FDEA201802270510.md): Floor Panel · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 261UF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATATORY A REPAIR. MAJOR REPAIR. - [SDR FDEA201802270509](https://openairdocs.org/sdr/FDEA201802270509.md): Floor Panel · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252GH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATAGORY A REPAIR. MAJOR REPAIR - [SDR FDEA201802270508](https://openairdocs.org/sdr/FDEA201802270508.md): Floor Panel · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252WG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATATORY A REPAIR. MAJOR REPAIR. - [SDR FDEA201802270507](https://openairdocs.org/sdr/FDEA201802270507.md): Floor Panel · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252NG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CATATORY A REPAIR. MAJOR REPAIR - [SDR FDEA201802270506](https://openairdocs.org/sdr/FDEA201802270506.md): Floor Panel · damaged · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 252DF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS CATATORY A REPAIR. MAJOR REPAIR - [SDR FDEA201802270502](https://openairdocs.org/sdr/FDEA201802270502.md): Web · cracked · Feb 27, 2018 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK CARGO, FRAMES 79 - 82 FLOOR WEB CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-21. - [SDR FDEA201609303395](https://openairdocs.org/sdr/FDEA201609303395.md): Cdu · failed · Sep 30, 2016 · N691FE · Airbus A300F4605R · Engine Thrust Reverser > RECIEVED ECAM INDICATION "REV ENG 1 PRESSURIZED" SHORTLY AFTER T/O. COMPLIED WITH ECAM. THROTTLE 1 AT IDLE POWER. RTB. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REPLACED THE NR 1 CDU, FEEDBACK ACTUATOR IAW AMM 78-31-01-04. FUNCTIONAL C - [SDR FDEA201509182899](https://openairdocs.org/sdr/FDEA201509182899.md): Skin · cracked · Sep 18, 2015 · N691FE · Airbus A300F4605R · Cargo/Baggage Doors > AFT CARGO DOOR INNER SKIN, FOUND CRACK AT FWD LWR SECTION. REPAIRED IAW EA 6-5230-T0320224 PT 1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201509152880](https://openairdocs.org/sdr/FDEA201509152880.md): Support Beam · corroded · Sep 15, 2015 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > BULK CARGO BAY Y805, LONGITUDINAL SUPPORT BEAM CORRODED, BETWEEN FRAMES 66 - 67. REPAIRED IAW SRM51-40-21. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201509152879](https://openairdocs.org/sdr/FDEA201509152879.md): Door Frame · dented · Sep 15, 2015 · N691FE · Airbus A300F4605R · Fuselage Main, Structure > FORWARD CARGO BAY CUT OUT FWD FRAME FOUND ONE DENT, FRAME 20A, STRINGER 40R - 41R. REPAIRED IAW EA 6-5310-T0320128 PT 1. MINOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201509082816](https://openairdocs.org/sdr/FDEA201509082816.md): Crossbeam · cracked · Sep 8, 2015 · N691FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK CARGO COMPARTMENT, FLOOR STRUCTURE AREA CROSSBEAM CRACKED FRAME 48, BETWEEN Y0 & Y-450. REPLACED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AREA CROSSBEAM IAW SRM 51-40-21. THIS REPAIR CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201509082814](https://openairdocs.org/sdr/FDEA201509082814.md): Skin Panel · punctured · Sep 8, 2015 · N691FE · Airbus A300F4605R · Wing, Plate/Skin > LEFT WING INBD TRAILING FLAP BOTTOM SKIN, ONE EACH POINT PUNCTURE. REPAIRED THE PUNCTURE IAW SRM 57-50-00 PARA 4E. THIS REPAIR CATEGORY A. MINOR REPAIR IAW GMM6-2-100. - [SDR FDEA201507142223](https://openairdocs.org/sdr/FDEA201507142223.md): Unknown · malfunctioned · Jul 14, 2015 · N691FE · Airbus A300F4605R · Engine Controls > ATTEMPTED TAKEOFF RW 15. AFT TOGA NR 2 THROTTLE CAME UP IMMEDIATELY, BUT NR 1 DID NOT. DISCONNECTED TAKEOFF AT APPROX 5 KTS. RAN ALL CHECKLISTS & TAXIED BACK TO RAMP, BEFORE ENTERING RAMP TALKED TO MX. DECIDED TO TRY TOGA AGAIN & BOTH THROTTLES BEGAN ADVAN - [SDR FDEA201505221621](https://openairdocs.org/sdr/FDEA201505221621.md): Rib · corroded · May 22, 2015 · N691FE · Airbus A300F4605R · Wing, Rib/Bulkhead > RIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE. COMPLIED WITH EA 6-5710-T0317624 WINGS, BASIC WING STRUCTURE. CORROSION REPAIR OF RIB 5 FWD LUG RT. - [SDR FDEA201505221620](https://openairdocs.org/sdr/FDEA201505221620.md): Rib · corroded · May 22, 2015 · N691FE · Airbus A300F4605R · Wing, Rib/Bulkhead > LEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & AFT FACE. COMPLIED WITH EA 6-5710-T0317626. TITLE WINGS-BASIC WING STRUCTURE, CORROSION REPAIR OF RIB 5 FWD LUG LT. - [SDR FDEA201310092471](https://openairdocs.org/sdr/FDEA201310092471.md): Line · leaking · Oct 9, 2013 · N691FE · Airbus A300F4605R · Pneumatic Distribution System > AFTER LEVELING AT FL320, NR 1 HP VALVE FAULT ILLUMINATED. FOUND NR 1 ENGINE HP VALVE PRESSURE SENSE LINE LEAKING. R & R SENSE LINE IAW MM 36-11-12-04-01. - [SDR FDEA201309062148](https://openairdocs.org/sdr/FDEA201309062148.md): Duct · cracked · Sep 6, 2013 · N691FE · Airbus A300F4605R · Pneumatic Distribution System > NR 1 ENGINE INTERSECT DUCT FOUND CRACKED, CONNECTS TO THE 8TH-STAGE CHECK VALVE AT ABOUT 3:00 POSITION. REPLACED PNEUMATIC AIR TUBE PER EM 71-00-02-004 PERFORM ENGINE PNEUMATIC LEAK CHECK IAW AMM 36-11-00-06-02 AND NO LEAKAGE FOUND. - [SDR FDEA201309062147](https://openairdocs.org/sdr/FDEA201309062147.md): Duct · cracked · Sep 6, 2013 · N691FE · Airbus A300F4605R · Engine Bleed Air System > NR 1 ENGINE TURBINE CLEARANCE CONTROL VALVE FWD MANIFOLD DUCT FOUND CRACKED AT ABOUT 3:00 POSITION. REPLACED PNEUMATIC AIR TUBE IAW EM 72-00-00-003 PERFORM ENGINE PNEUMATIC LEAK CHECKED IAW AMM36-11-00-06-02. - [SDR FDEA201309062146](https://openairdocs.org/sdr/FDEA201309062146.md): Duct · cracked · Sep 6, 2013 · N691FE · Airbus A300F4605R · Engine Thrust Reverser > NR 1 ENGINE PNEUMATIC Y-CHECK VALVE FOUND THRUST REVERSER VALVE BLEED AIR TUBE CRACKED AT ABOUT 2:00 POSITION. REPLACEED THE PNEUMATIC AIR TUBE PER EM71-00-02-005 2.PERFORM ENGINE PNEUMATIC LEAK CHECK PER AMM36-11-00-06-02 AND NO LEAKAGE FOUND. - [SDR FDEA201206222303](https://openairdocs.org/sdr/FDEA201206222303.md): Line · leaking · Jun 22, 2012 · N691FE · Airbus A300F4605R · Hydraulic System, Main > ON CLIMB OUT LOST YELLOW SYS HYD PUMP. R & R YELLOW ENG DRIVEN HYD IAW AMM 29-11-32-04-02. BLEED LINES TO PUMP. PREMATURE REMOVAL/INSTALLATION OFF DURING LEAK CHECK FOUND SUCTION HOSE SELF-SEALING ADAPTER ASSY CRACKED AND LEAKING. Next page: https://openairdocs.org/aircraft/N691FE/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 = 'N691FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N691FE/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.