# Service difficulty reports: N690FE

A list on [N690FE](https://openairdocs.org/aircraft/N690FE.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 · 127 reports

- [SDR FDEA202607030830](https://openairdocs.org/sdr/FDEA202607030830.md): Pressure Switch · leaking · Jul 3, 2026 · N690FE · Airbus A300F4605R · Hydraulic System, Main
  > ON TAKEOFF ROLL AT ABOUT 60KTS ECAM ALERT OF GREEN HYDRAULIC SYSTEM LOW PRESSURE. WE GOT TWO ECAM WARNINGS, ONE RIGHT AFTER THE OTHER. RTO, AUTO BRAKES DID NOT ENGAGE BEC OF LOW SPEED. TSM 29-32-00 FIG 105 AMM 29-14-00-03 JRH CH5 WITH REF ABOVE RAN NR 1 A
- [SDR FDEA202601130027](https://openairdocs.org/sdr/FDEA202601130027.md): Skin · punctured · Jan 13, 2026 · N690FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > UPON ARRIVAL FOUND HOLE IN THE FUSELAGE 12 1/2 " AFT OF THE LOWER FWD CARGO DOOR, 1"L X 1/2 "W. INSTALLED REPAIR DOUBLER & FILLER IAW EA 6-5330-T 0386106 PT 2. NOTE: REPAIR STILL NEEDS FINAL PAINT FINISH. PREPPED AND PAINTED IAW SRM 51-71-10.
- [SDR FDEA202511052133](https://openairdocs.org/sdr/FDEA202511052133.md): Compensator · failed · Nov 5, 2025 · N690FE · Airbus A300F4605R · Fuel Indicating System
  > DURING CRUISE AT FL370 FUEL ADVISORY FLASHED WITH RT OUTER & RT INNER QUANTITIES FLASHING. THE LT INNER QTY WAS DECREASING THROUGH 7000 LBS OF FUEL WITH RT INNER QTY AT 13,300 LBS. SUSPECTED FUEL LEAK. RESET FQI CHAN SUPPLY 1 & 2 CB'S WITH NO CHANGES & QT
- [SDR FDEA202510292116](https://openairdocs.org/sdr/FDEA202510292116.md): Rib · cracked · Oct 29, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1 EA CRACK (20MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB 27 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 27, S-2.8 ~ REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26 ~27, REAR SPAR ~S-2.2. I.A.W FEDEX EA NO:T6-5750-T038
- [SDR FDEA202510061965](https://openairdocs.org/sdr/FDEA202510061965.md): Rib · cracked · Oct 6, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP INTERNAL STRUCTURE CRACK AT UPR RIB26 STGR-2.7 TO STGR-2.8. ACCOMPLISHED RIB FLANGE REPAIR AT RIB26, S-2.7~S-2.8 AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, SEQ NO:XXXX, TITLE:WINGS- FL
- [SDR FDEA202510061964](https://openairdocs.org/sdr/FDEA202510061964.md): Rib · cracked · Oct 6, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP INTERNAL STUCTURE CRACK AT UPPER RIB26 STGR-2.8 TO REAR SPAR. ACCOMPLISHED RIB FLANGE REPAIR AT RIB26, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, REPAIR CLASSIFIED AS CAT
- [SDR FDEA202509301962](https://openairdocs.org/sdr/FDEA202509301962.md): Rib · cracked · Sep 30, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > 2EA CRACKS (5MM & 20MM) INDICATION WERE FOUND AT RH WING CENTER FLAP RIB27 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB27, S-2.7~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26~27, REAR SPAR~S-2.2 I.A.W FEDEX EA NO:T6-5750-T0385
- [SDR FDEA202509301946](https://openairdocs.org/sdr/FDEA202509301946.md): Skin · cracked · Sep 30, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1 EA CRACK (40MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB17 AFTER RIB FLANGE AREA OF TOP SURFACE ACCOMPLISHED RIB FLANGE REPAIR AT RIB17, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16 ~18, REAR SPAR ~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072P1,
- [SDR FDEA202509301944](https://openairdocs.org/sdr/FDEA202509301944.md): Skin · cracked · Sep 30, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1 EA CRACK (30MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB18 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB18, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16 ~18, REAR SPAR ~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072P
- [SDR FDEA202509301940](https://openairdocs.org/sdr/FDEA202509301940.md): Skin · cracked · Sep 30, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1 EA CRACK (20MM) WAS FOUND AT LH WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 27, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 26~27, REAR SPAR~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385172 P1, SEQ NO: T
- [SDR FDEA202509271995](https://openairdocs.org/sdr/FDEA202509271995.md): Rib · worn · Sep 27, 2025 · N690FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > DAMAGE NOTED AROUND THE LWR BORE HOLE ON THE OUTBD SIDE OF THE OUTBD JACK RIB AT R3 SPLR ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #3 SPOILER O/B JACK RIB LOWER BORE ABX 40.425 I.A.W EA NO: T6-5740-T0385131 P1, SEQ10
- [SDR FDEA202509271994](https://openairdocs.org/sdr/FDEA202509271994.md): Rib · worn · Sep 27, 2025 · N690FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > DAMAGE NOTED AROUND THE UPPER BORE HOLE ON THE INBD SIDE OF THE INBD JACK RIB AT R3 SPLR ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #3 SPOILER I/B JACK RIB UPPER BORE ABX 31.675 I.A.W EA NO: T6-5740-T0385131 P1, SEQ10
- [SDR FDEA202509271993](https://openairdocs.org/sdr/FDEA202509271993.md): Rib · worn · Sep 27, 2025 · N690FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > DAMAGE NOTED AROUND THE LWR BORE HOLE ON THE OUTBD SIDE OF THE OUTBD JACK RIB AT R5 SPLR ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #5 SPOILER O/B JACK RIB LOWER BORE ABX 184.625 I.A.W EA NO: T6-5740-T0385129 P1, SEQ1
- [SDR FDEA202509271992](https://openairdocs.org/sdr/FDEA202509271992.md): Rib · worn · Sep 27, 2025 · N690FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > DAMAGE NOTED AROUND THE LWR BORE HOLE ON THE OUTBD SIDE OF THE OUTBD JACK RIB AT R6 SPLR ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #6 SPOILER O/B JACK RIB LOWER BORE SP1X 40.425 I.A.W EA NO: T6-5740-T0385130 P1, SEQ1
- [SDR FDEA202509231906](https://openairdocs.org/sdr/FDEA202509231906.md): Fitting · damaged · Sep 23, 2025 · N690FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME24 PER EO:6-5230- E0378588 B P5. ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN 1~3 I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:959, TITLE:DOORS-CARGO D
- [SDR FDEA202509231905](https://openairdocs.org/sdr/FDEA202509231905.md): Fitting · damaged · Sep 23, 2025 · N690FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO:6-5230- E0378588 B P5. ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN 1~3 I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:959, TITLE:DOORS-CARGO
- [SDR FDEA202509221967](https://openairdocs.org/sdr/FDEA202509221967.md): Rudder · delaminated · Sep 22, 2025 · N690FE · Airbus A300F4605R · Rudder, Plate/Skin
  > 1EA WATER TRAPPED AREA (140MMX10MM) WAS FOUND AT L/H RUDDER HOISTING POINT1. ACCOMPLISHED THE LWR AFT HOIST POINT REPAIR AT LH RUDDER SKIN I.A.W A300-600F SRM 55- 41-12-201, PARA.24, PAGE.318~332, FIG.224(SHEET-1~3) & SRI:55-41-12-201, IIR:55-41-12-2-007-00,
- [SDR FDEA202509221966](https://openairdocs.org/sdr/FDEA202509221966.md): Rudder · delaminated · Sep 22, 2025 · N690FE · Airbus A300F4605R · Rudder, Plate/Skin
  > 1EA WATER TRAPPED AREA (180MMX110MM) WAS FOUND AT L/H RUDDER HOISTING POINT2. ACCOMPLISHED THE LWR FWD HOIST POINT REPAIR AT LH RUDDER SKIN I.A.W A300-600F SRM 55- 41-12-201, PARA.25, PAGE.343~350, FIG.225A(SHEET-1~3) & SRI:55-41-12-201, IIR:55-41-12-2-008-00
- [SDR FDEA202509221898](https://openairdocs.org/sdr/FDEA202509221898.md): Seat Track · worn · Sep 22, 2025 · N690FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK CROWN AREA GOT 2EA ENLARGE WORN MARKS LOCATION FROM FR54.3 PLUS 19" TO FR55 PLUS 2" AT Y0 POSITION. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MDCC FR54.3 PLUS 19"~FR55 PLUS 2", Y0 I.A.W A300-600F SRM 53-10-16-201, PARA.4, PAGE.201
- [SDR FDEA202509211943](https://openairdocs.org/sdr/FDEA202509211943.md): Profile · corroded · Sep 21, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CGO COMPT FLOOR BEAM PROFILE UPPER SKIN CORRODED AT FR66 - FR67, Y-805 POSITION. INSTALLED THE FABRICATION PROFILE WITH FASTENERS AT BULK CARGO COMPARTMENT FR66 - FR67, Y-805 IAW SRM 53-17-15-001, CONFIG-3, PAGE.80 AND 90, FIG.8(SHEET-1) & 51-41-21-001,
- [SDR FDEA202509211942](https://openairdocs.org/sdr/FDEA202509211942.md): Profile · corroded · Sep 21, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CARGO COMPT FLOORBEAM PROFILE UPPER SKIN CORRODED AT FR67 - FR68, Y46.7 POSITION. INSTALLED FABRICATION PROFILE WITH FASTENERS AT BULK CARGO COMPARTMENT FR67 - FR68, Y46.7 IAW SRM 53-17-15-001, CONFIG-3, PAGE.80 & 90, FIG.8(SHEET-1) & 51-41-21-001, PARA
- [SDR FDEA202509211939](https://openairdocs.org/sdr/FDEA202509211939.md): Profile · corroded · Sep 21, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CARGO COMPT FLOORBEAM PROFILE UPPER SKIN CORRODED AT FR67 - 68, Y625 POSITION. INSTALLED THE FABRICATION PROFILE WITH FASTENERS AT BULK CARGO COMPARTMENT FR 67 - 68, Y625 IAW SRM 53-17-15-001, CONFIG-3, PAGE.82 AND 90, FIG.8 (SHEET-1), & 51-41-21-001, PAR
- [SDR FDEA202509201941](https://openairdocs.org/sdr/FDEA202509201941.md): Skin · cracked · Sep 20, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH CTR FLAP INTERNAL STRUCTURE CRACK AT UPPER RIB 18, STGR-2.8 TO REAR SPAR. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 18, S-2.8~REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB 16~18, REAR SPAR~S-2.1 I.A.W FEDEX EA NO:T6-5750-T0385072 P1, SEQ NO: 1031, REPAIR CLAS
- [SDR FDEA202509191842](https://openairdocs.org/sdr/FDEA202509191842.md): Shear Plate · cracked · Sep 19, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB CRACK APPROX 1" AT FR79 PLUS 5", Y1620. REPLACED CRACK SHEAR WEB WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51- 40-21-001, PARA.6, PAGE.7B-23. THIS REPAIR CLSSSIFIED AS MINOR PER GMM 6-2-100. AT MAIN DECK FLOOR FR79
- [SDR FDEA202509191841](https://openairdocs.org/sdr/FDEA202509191841.md): Shear Web · damaged · Sep 19, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SHEAR WEB BROKEN AT FR77 Y-1900 REPLACED BROKEN SHEAR WEB WITH NEW ONE 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 6-2-100. AT MAINDECK FLOOR FR77 Y-1900 POSITION.
- [SDR FDEA202509181854](https://openairdocs.org/sdr/FDEA202509181854.md): Skin · misrepaired · Sep 18, 2025 · N690FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR102~103,STGR 1~2L 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 DOUBLER
- [SDR FDEA202509181853](https://openairdocs.org/sdr/FDEA202509181853.md): Seat Track · misrepaired · Sep 18, 2025 · N690FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING SPLICE REPAIR FOUND ON MDCC SEAT TRACK BTW FR37~38.2,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 121.707,INSPECTION OF SPLICE REPA
- [SDR FDEA202509171833](https://openairdocs.org/sdr/FDEA202509171833.md): Flap · no discrepancy · Sep 17, 2025 · N690FE · Airbus A300F4605R · Trailing Edge Flaps
  > EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB17-18, STGR2.7 - 2.8 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 TP1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, EXISTI
- [SDR FDEA202509161835](https://openairdocs.org/sdr/FDEA202509161835.md): Sidewall Panel · no discrepancy · Sep 16, 2025 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > EXISTING DOUBLER REPAIR FOUND ON RH FUSELAGE SKIN BTW FR1~2, AT 4 O'CLOCK POSITION. 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, EX
- [SDR FDEA202507101170](https://openairdocs.org/sdr/FDEA202507101170.md): Accumulator · underserviced · Jul 10, 2025 · N690FE · Airbus A300F4605R · Hydraulic Reservoir, Main
  > ABORTED TAKEOFF FOR YELLOW HYD LOW PRESS. THEN WHILE DOING FLIGHT CONTROL CHECK, NOTICED THE YELLOW HYD FLUID LEVEL DECREASING. AMM: 12-14-29-00 FOUND THE YELLOW SYSTEM ACCUMULATOR TO BE UNDERSERVICED. SERVICED IT ACCORDING TO AMM. OPERATED THE FLIGHT
- [SDR FDEA202502280306](https://openairdocs.org/sdr/FDEA202502280306.md): Actuator · failed · Feb 28, 2025 · N690FE · Airbus A300F4605R · Rudder Control System
  > ON FINAL, WITH AUTOPILOT OFF, RUDDER WAS VERY DIFFICULT TO OPERATE ON THE RIGHT PEDAL BUT THEN FELT LIKE IT PUSHED THROUGH SOMETHING AND WAS LESS STIFF BUT STILL MORE THAN NORMAL. LEFT PEDAL FELT NORMAL. ON TAXI OUT RUDER CHECK FELT NORMAL, TAXI IN, TRIED
- [SDR FDEA202403280394](https://openairdocs.org/sdr/FDEA202403280394.md): Control Panel · inoperative · Mar 28, 2024 · N690FE · Airbus A300F4605R · HF Communications System
  > BOTH CA AND FO UNABLE TO TRANSMIT OR BE HEARD ON VHF 1 OR VHF 2. TRIED SWITCHING HEADSET AND HAND MIC. INTERCOM WORKED FINE. OTHER JETS REPORTED POSSIBLE STUCK MIC. OUR RECEPTION WORKED FINE THROUGHOUT. WE PLUGGED AND UNPLUGGED ALL HEADSETS AND HAND MICS.
- [SDR FDEA202301310180](https://openairdocs.org/sdr/FDEA202301310180.md): Power Unit · no test · Jan 31, 2023 · N690FE · Airbus A300F4605R · Emergency Equipment
  > RIGHT DOOR SLIDE WILL NOT INDICATE ARMED. FOUND AUTONOMOUS STANDBY POWER UNIT NOT TESTING, RESET AND UNIT TESTED NORMALLY IAW AMM REF ABOVE. NO 60 DAY HISTORY, A/C OK TO CONTINUE.
- [SDR FDEA202212293032](https://openairdocs.org/sdr/FDEA202212293032.md): Pump · unknown · Dec 29, 2022 · N690FE · Airbus A300F4605R · Hydraulic Power Accumulator, Main
  > LOSS OF BLUE HYDRAULIC SYSTEM IN CRUISE. FACT 29DEC22 16:24 MEM U AMM: 29-11-32-04-02 AMM: 29-11-36-04-02
- [SDR FDEA202205281321](https://openairdocs.org/sdr/FDEA202205281321.md): None · none · May 28, 2022 · N690FE · Airbus A300* · Hydraulic System, Main
  > PDIS 690 29-10 4895 28MAY22 SHV FACT U WHEN GEAR WAS EXTENDED ON APPROACH, RECEIVED GREEN SYSTEM LO PRESSURE #1 AND #2 PUMPS. GREEN SYSTEM QUANTITY INDICATED MAXIMUM LEVEL. WARNING LASTED APPROX 20 SECONDS AND WENT AWAY. GREEN SYSTEM PRESSURE
- [SDR FDEA202202080256](https://openairdocs.org/sdr/FDEA202202080256.md): Battery · inoperative · Feb 8, 2022 · N690FE · Airbus A300* · Passenger/Crew Doors
  > WHILE CLOSING UP FOR DEPARTURE R1 DOOR SLIDE WILL NOT ARM. RESET ASPSU, REF AMM 52-70-00-05-02, VERIFIED R1 & L1 DOOR BUZZER AND AURAL WARNING FUNCTION NORMALY, SLIDE INDICATION VERIFIED GOOD ON ECAM DOORS PAGE. NO HISTORY 90 DAYS. SUSPECT ASPSU ANOMOLY.
- [SDR FDEA202108112006](https://openairdocs.org/sdr/FDEA202108112006.md): Girt Bar · misinstalled · Aug 11, 2021 · N690FE · Airbus A300F4605R · Emergency Equipment
  > DURING ARRIVAL R1 DOOR DIFFICULT TO OPEN, DURING DEPARTURE UNABLE TO ARM. RELEASED FOR SERVICE. DOOR R1 INOP. FOUND GIRT BAR ASSEMBLY NOT INSTALLED CORRECTLY. REINSTALLED GIRT BAR IAW AMM 25-61-21, DEACTIVATED DOOR AND VERIFIED CORRECT OPERATION OF G
- [SDR FDEA202105051134](https://openairdocs.org/sdr/FDEA202105051134.md): Valve · malfunctioned · May 5, 2021 · N690FE · Airbus A300F4605R · Aircraft Fuel Distribution System
  > PDIS 690 28-21 3548 05MAY21 PDX OPEN U RIGHT INNER TANK VALVES INDICATED CLOSED CLIMBING THROUGH FL180. RT INNER TANK VALVE SELECTORS WERE IN THE OPEN POSITION. NO CIRCUIT BREAKERS WERE POPPED. FUEL IMBALANCE WAS GETTING WORSE. NO HELP WITHIN
- [SDR FDEA202011193002](https://openairdocs.org/sdr/FDEA202011193002.md): Web · cracked · Nov 19, 2020 · N690FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED MAIN CARGO COMPARTMENT DECK FLOOR STRUCTURE AT LEVEL FRAME 47 AND 9 INCH FROM FUSELAGE CENTER LINE AT RT SIDE ON LOWER FUSELAGE. REPLACED WEB LOCATED MAIN CARGO COMPARTMENT DECK FLOOR STRUCTURE AT LEVEL FRAME 47 AND 9 INCH FROM FUSELAGE CENT
- [SDR FDEA202002270395](https://openairdocs.org/sdr/FDEA202002270395.md): Detector · failed · Feb 27, 2020 · N690FE · Airbus A300* · Landing Gear Position and Warning
  > PDIS 690 32-60 1966 26FEB20 MEM OPEN U LOGPAGES:2297513 UPON GEAR RETRACTION AFTER T/O GOT 3 GEAR UNSAFE INDICATIONS FOLLOWED BY LDG GEAR RETRACTION FAULT FOLLOWED QRH PROCEDURESAND RETURNED TO MEMPHIS FACT 27FEB20 10:31 MEM
- [SDR FDEA2020022870395](https://openairdocs.org/sdr/FDEA2020022870395.md): Warning Light · illuminated · Feb 27, 2020 · N690FE · Airbus A300F4605R · Landing Gear Position and Warning
  > PDIS 690 32-60 1966 26FEB20 MEM OPEN U LOGPAGES:2297513 UPON GEAR RETRACTION AFTER T/O GOT 3 GEAR UNSAFE INDICATIONS FOLLOWED BY LDG GEAR RETRACTION FAULT FOLLOWED QRH PROCEDURESAND RETURNED TO MEMPHIS ENT BY: 110437 RPT BY:603223
- [SDR FDEA202002160345](https://openairdocs.org/sdr/FDEA202002160345.md): Unknown · unknown · Feb 16, 2020 · N690FE · Airbus A300* · Passenger/Crew Doors
  > PDIS 690 52-10 1941 16FEB20 ABQ OPEN U LOGPAGES:2297502 R1 CABIN DOOR SLIDE WOULD NOT SHOW ARMED "SLIDE" INDICATION ON ECAM. MEL 16FEB20 00:31 ABQ U RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 26FEB20 "MEL 52-30-04:
- [SDR FDEA2020021860345](https://openairdocs.org/sdr/FDEA2020021860345.md): Indicator · unknown · Feb 16, 2020 · N690FE · Airbus A300F4605R · Emergency Equipment
  > PDIS 690 52-10 1941 16FEB20 ABQ OPEN U LOGPAGES:2297502 R1 CABIN DOOR SLIDE WOULD NOT SHOW ARMED "SLIDE" INDICATION ON ECAM. MEL 16FEB20 00:31 ABQ U RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 26FEB20 "MEL 52-30-04:
- [SDR FDEA201902080289](https://openairdocs.org/sdr/FDEA201902080289.md): Uplock Actuator · malfunctioned · Feb 8, 2019 · N690FE · Airbus A300F4605R · Landing Gear Position and Warning
  > ON CONFIGURING TO LAND, WHEN HANDLE LOWERED, RECEIVED UNSAFE NLG INDICATION ON PANELS, & ECAM. POSITION DETECTOR SWITCHED FROM NR 2 - NR 1, SAME RESULTS. LOW APPROACH. COMPLIED WITH QRH. NLG GREEN INDICATION AFTER MANUAL EXTENSION. DECLARED EMERGENCY, UNEVENT
- [SDR FDEA201806191543](https://openairdocs.org/sdr/FDEA201806191543.md): Mount · damaged · Jun 19, 2018 · N690FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > NR 1 PYLON FWD MOUNT INBD AFT BOLT HOLE HAS CORROSION. REAMED HOLE ON NR 1 PYLON AFT INBD MOUNT BOLT TO.997 IAW SRM 54-51-81. INSTALLED BUSHING IAW SRM 54-51-81.
- [SDR FDEA201806171512](https://openairdocs.org/sdr/FDEA201806171512.md): Floor Panel · delaminated · Jun 17, 2018 · N690FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 252GF FWD CORNER DELAMINATED. LOCATED FRAME 57.1 FABRICATED NEW FLOOR BOARD ON T18/1348329 IAW SRZ-25-005 (252GF) MAJOR REPAIR.
- [SDR FDEA201806171511](https://openairdocs.org/sdr/FDEA201806171511.md): Floor Panel · delaminated · Jun 17, 2018 · N690FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 252RH INBD AFT CORNER IS DELAMINATED. FABRICATED NEW FLOOR PANEL 252RH ON T18/1348328 IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201806171510](https://openairdocs.org/sdr/FDEA201806171510.md): Floor Panel · damaged · Jun 17, 2018 · N690FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 242PF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 242PF ON T18/1348235 IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201806161507](https://openairdocs.org/sdr/FDEA201806161507.md): Floor Panel · delaminated · Jun 16, 2018 · N690FE · Airbus A300F4605R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221RF DELAMINATED FABRICATED FLOOR PANEL 221RF ON T18/1348323 IAW DWG SRZ-25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201806161506](https://openairdocs.org/sdr/FDEA201806161506.md): Floor Panel · broken · Jun 16, 2018 · N690FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241LK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241LK ON T18/1348234 IAW DWG SRZ-25-005. CLASSIFIED AS A CAT"A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N690FE/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 = 'N690FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N690FE/reports

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