# Service difficulty reports: N654FE

A list on [N654FE](https://openairdocs.org/aircraft/N654FE.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 5 · 237 reports

- [SDR FDEA202607100898](https://openairdocs.org/sdr/FDEA202607100898.md): Glide Slope · malfunctioned · Jul 10, 2026 · N654FE · Airbus A300F4605R · Glide Slope System
  > ON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.
- [SDR FDEA202604290521](https://openairdocs.org/sdr/FDEA202604290521.md): Power Supply · failed · Apr 29, 2026 · N654FE · Airbus A300F4605R · Door Warning System
  > ON POST FLIGHT FOUND L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. DURING TEST, BOTH ASSOCIATED WARNING BUZZERS OPERATE NORMALLY. MEL 52-73-01-01: L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. REMOVED AND REPLACE
- [SDR FDEA202512022217](https://openairdocs.org/sdr/FDEA202512022217.md): Battery · failed · Dec 2, 2025 · N654FE · Airbus A300F4605R · Door Warning System
  > WITH R1 ENTRY DOOR ARMED NO ECAM INDICATION PRESENT. RELEASED FOR SERVICE PER MEL 52-30-04. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. R & R TWO BATTERIES
- [SDR FDEA202511192195](https://openairdocs.org/sdr/FDEA202511192195.md): Girt Bar · fod · Nov 19, 2025 · N654FE · Airbus A300F4605R · Emergency Equipment
  > R1 DOOR SLIDE WILL NOT ARM. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE.MSN DID A GVI OF GIRT BAR FOR DEBRIS & OPERATION IAW AMM 25-61-21-04, NO DEFECTS NOTED.
- [SDR FDEA202508291567](https://openairdocs.org/sdr/FDEA202508291567.md): Door · cracked · Aug 29, 2025 · N654FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 6EA FASTENER HOLES REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE PT1 BETWEEN FR22 AND FR25 6EA CRACKED FASTENER HOLES PER EA 6-5230-T0384742 P1, TITLE: DOORS - CARGO DOOR / HYD S
- [SDR FDEA202508131418](https://openairdocs.org/sdr/FDEA202508131418.md): Frame · cracked · Aug 13, 2025 · N654FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0384526 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR47 RH REAR SPAR HOLE C CRACK REPAIR - SB A
- [SDR FDEA202508131417](https://openairdocs.org/sdr/FDEA202508131417.md): Frame · cracked · Aug 13, 2025 · N654FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER 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-T0384530 P1. REPAIRED THE CENTER BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH S
- [SDR FDEA202508121408](https://openairdocs.org/sdr/FDEA202508121408.md): Skin · cracked · Aug 12, 2025 · N654FE · Airbus A300F4605R · Trailing Edge Flaps
  > NDT INSP FOUND RH WING CENTER FLAP TOP SKIN FLANGE RIB26 STGR2.7 AND STGR 2.8 CRACKED COMPLIED WITH EA: 6-5750-T0384484 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP - CRACK IN UPPER FLANGES OF RIB 26 REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING
- [SDR FDEA202508111404](https://openairdocs.org/sdr/FDEA202508111404.md): Actuator · faulted · Aug 11, 2025 · N654FE · Airbus A300F4605R · Cargo/Baggage Doors
  > CARGO DOOR, HYD SYS, DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MD
- [SDR FDEA202507231298](https://openairdocs.org/sdr/FDEA202507231298.md): Check Valve · leaking · Jul 23, 2025 · N654FE · Airbus A300F4605R · Hydraulic System, Main
  > CRUISING, FL340. ODOR IN FLT DECK. SMELLED LIKE A WET DOG, MUSTY TOWEL, OR DIRTY DIAPER. GOT STRONGER. OPENED C/P DOOR & SAW A CLOUD IN BACK. BURNING IN NOSTRILS. PUT ON OXY MASKS. DIDN`T RECEIVE FIRE - SMOKE WARNINGS. DIVERTED, COULDN`T DETERMINE SOURCE.
- [SDR FDEA202507221289](https://openairdocs.org/sdr/FDEA202507221289.md): Smoke Warning · activated · Jul 22, 2025 · N654FE · Airbus A300F4605R · Smoke Detection
  > MAIN DECK CARGO SMOKE ECAM PASSING 32K LEVELED OFF COMPLIED WITH ECAM. ATB DESCENDING THROUGH 20K RECALLED ECAM ALL RED ECAM CLEARED CONTINUED MEM NORMAL APP LANDING FIRE RESCUE CONFIRMED NO SMOKE. EMERGENCY DECLARED. REMOVED AND REPLACED SMOKE DETECTI
- [SDR FDEA202505230794](https://openairdocs.org/sdr/FDEA202505230794.md): Oxygen Mask · inoperative · May 23, 2025 · N654FE · Airbus A300F4605R · Passenger Oxygen System
  > ON PREFLIGHT FOUND CREW COCKPIT O2 WALK AROUND BOTTLE MASK UNSERVICEABLE. REMOVED AND REPLACED COCKPIT CREW 02 MASK PER REF ABOVE. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202505210771](https://openairdocs.org/sdr/FDEA202505210771.md): Flap System · stuck · May 21, 2025 · N654FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > ON DEPARTURE ON A SLATS/FLAPS 15/20 TAKEOFF AT COMMENCEMENT OF ATTEMPTED FLAP RETRACTION WE RECEIVED ECAM FOR FLAPS SYS 1 AND 2 FAULT/FLAPS STUCK. WE FOLLOWED THE ECAM AND SUBSEQUENT QRH PROCEDURE WITH NO SUCCESS WITH CYCLING. THE SLATS AND FLAPS REMAINE
- [SDR FDEA202502140230](https://openairdocs.org/sdr/FDEA202502140230.md): Battery · no test · Feb 14, 2025 · N654FE · Airbus A300F4605R · Emergency Lighting
  > DURING MX PREFLIGHT: JUMPSEAT AREA EMERGENCY LIGHTS INOP. AMM 33-51-14-04 REPLACED PSU EMERG. BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202502080253](https://openairdocs.org/sdr/FDEA202502080253.md): Power Supply · faulted · Feb 8, 2025 · N654FE · Airbus A300F4605R · Passenger/Crew Doors
  > RIGHT ENTRY DOOR WILL NOT ARM. FACT 08FEB25 13:52 OMA AMM: 52-73-18-04 RESET AUTOMONOMOUS POWER SUPPLY REF AMM 52-73-18-04, OP'S CHECK NORMAL. OK FOR SERVICE.
- [SDR FDEA202407211039](https://openairdocs.org/sdr/FDEA202407211039.md): Altimeter · failed · Jul 21, 2024 · N654FE · Airbus A300F4605R · Altimeter, Barometric/Encoder
  > AT CRUISE RECEIVED CAPT ALTI FAULT ECAM WITH COMMENSURATE INDICATIONS ON THE PRIMARY ALTIMETER INCLUDING OFF FLAG FOLLOWED BY ERRATIC ALTITUDE INDICATIONS VARYING BY UP TO APPROXIMATELY 1000 FEET FROM FO ALTIMETER. REFERENCE QRH FOR REQUIRED RVSM EQUIPMEN
- [SDR FDEA202405030570](https://openairdocs.org/sdr/FDEA202405030570.md): Bottle · overserviced · May 3, 2024 · N654FE · Airbus A300F4605R · Emergency Equipment
  > FOUND RH CREW ENTRY DOOR DAMPER CYLINDER SLIGHTLY OVERSERVICED. FACT 03MAY24 19:29 LRD AMM: 52-10-14-03-02 SERVICED RH CREW DOOR DAMPER CYLINDER AS REQUIRED IN REF WITH PLACARD AND AMM 52-10-14-03-02 STEP 3.D.(12).
- [SDR FDEA202404230271](https://openairdocs.org/sdr/FDEA202404230271.md): Warning Horn · false activation · Apr 23, 2024 · N654FE · Airbus A300F4605R · Passenger/Crew Doors
  > DURING CLIMBOUT, L1 DOOR INDICATED CONSTANT AUDIBLE ALARM AND FLASHING RED LIGHT. ATTEMPTED TO SEAT DOOR HANDLE WITH NO RESULT. REMAINED ON THROUGH CLIMB AND CRUISE. ADJ AND TEST IAW AMM STEP C. (1)-(6) NO FAULTS NOTED AT THIS TIME.
- [SDR FDEA202305270964](https://openairdocs.org/sdr/FDEA202305270964.md): Flap · dented · May 27, 2023 · N654FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CTR FLAP L/E GOT A DENT AT RIB11-2" PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIRED AREA. I.A.W A300-600F SRM 57-50-00-201, PARA.4H, P201-P236, FIG.208. THIS REPAIR IS CAT B REPAIR REFER CHAPTER TO SRI:57-50-00-201,IIR:57-50-0
- [SDR FDEA202305200962](https://openairdocs.org/sdr/FDEA202305200962.md): Skin · dented · May 20, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > 1EA DENT ON FUSELAGE SKIN, AT FR98~99, STGR2L~3L CUT OUT THE DAMAGED DENT, FABRICATED THE REPAIR DOUBLER AND INSTALLED WITH BLIND RIVETS, SEALANT I.A.W A300-600F SRM 53-19-12-201, PARA.6, FIG.202, PAGE.213~218, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY
- [SDR FDEA202305190993](https://openairdocs.org/sdr/FDEA202305190993.md): Unknown · unknown · May 19, 2023 · N654FE · Airbus A300F4605R · Wing Structure
  > LH WING TIP FWD NAV LIGHT CUTOUT UPPER & LOWER CORNER RIBS GOT ABRASION REPLACED THE UPPER AND LOWER CORNER RIBS WITH NEW PARTS IAW A300-600F SRM 51-72-10- 001, PAGE.2 & 51-40-21-001, PARA.6, PAGE7B~PAGE23
- [SDR FDEA202305180903](https://openairdocs.org/sdr/FDEA202305180903.md): Seat Track · unknown · May 18, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BETWEEN FR19~21, Y2462. EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A
- [SDR FDEA202305150972](https://openairdocs.org/sdr/FDEA202305150972.md): Frame · none · May 15, 2023 · N654FE · Airbus A300F4605R · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT: EXISTING FRAME REPAIR FOUND ON M/D AT FR 22, STGR 8R~9R 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 O
- [SDR FDEA202305131027](https://openairdocs.org/sdr/FDEA202305131027.md): Crossbeam · unknown · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 31 BTW Y1456 ~ Y1959 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 FDEA202305131026](https://openairdocs.org/sdr/FDEA202305131026.md): Crossbeam · unknown · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 32 BTW Y1456 ~ Y1959 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 FDEA202305130978](https://openairdocs.org/sdr/FDEA202305130978.md): Seat Track · corroded · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CGO COMP'T SEAT TRACK FOUND CORROSION AT FR15A, -Y953 AREA REPLACED THE NEW SEAT TRACK I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202305130971](https://openairdocs.org/sdr/FDEA202305130971.md): Skin · unknown · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 39~41L, FR 57.3~58 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12
- [SDR FDEA202305130970](https://openairdocs.org/sdr/FDEA202305130970.md): Skin · none · May 13, 2023 · N654FE · Airbus A300F4605R · Standard Practices/Structures
  > N00400 AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 51~54R, FR 60~61 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202305130963](https://openairdocs.org/sdr/FDEA202305130963.md): Flap · dented · May 13, 2023 · N654FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CTR FLAP L/E LWR SURFACE DENT AT O/B EDGE-11", D NOSE T/E -3.125". PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIR AREA I.A.W A300- 600F SRM 57-50-00-201, PARA.4H, P201-P236,FIG 208. THIS IS CAT B REPAIR REFER CHAPTER TO SRI: 5
- [SDR FDEA202305130936](https://openairdocs.org/sdr/FDEA202305130936.md): Skin · unknown · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 35~37R, FR26~27 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 FDEA202305130902](https://openairdocs.org/sdr/FDEA202305130902.md): Seat Track · none · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 57.1~57.2, Y1456 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 FDEA202305130901](https://openairdocs.org/sdr/FDEA202305130901.md): Floor Support · none · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D FLOOR SUPPORT BTW FR 14A~16A, -Y1456 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 FDEA202305130892](https://openairdocs.org/sdr/FDEA202305130892.md): Seat Track · unknown · May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~33, 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 FDEA202305120980](https://openairdocs.org/sdr/FDEA202305120980.md): Profile · cracked · May 12, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CGO COMP'T FLOOR FOUND Z-PROFILE CRACKED AT FR80/82, -Y1475 REPLACED WITH NEW Z-PROFILE I.A.W A300-600F SRM 51-72-10-001, PAGE 2
- [SDR FDEA202305100905](https://openairdocs.org/sdr/FDEA202305100905.md): Web · none · May 10, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON M/D WEB AT FR 47 BTW Y953 ~ Y1456 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 FDEA202305090883](https://openairdocs.org/sdr/FDEA202305090883.md): Dummy Rail · worn · May 9, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. REPAIRED THE RH NO2 FR54~FR54.2 DUMMY SEAT TRACK AND REINSTALLED O.K I.A.W A300-600 SRM:53-15-16 PARA 5A P201-P210 FIG.201 & AMM:20-21-12-00.
- [SDR FDEA202305090882](https://openairdocs.org/sdr/FDEA202305090882.md): Dummy Rail · worn · May 9, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/FR40 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. REPAIRED THE DUMMY SEAT TRACK WITH REINSTALLATION O.K I.A.W A300-600 SRM:53-15-16 PARA 5A P201~P210 FIG.201 & AMM:20-21-12-00.
- [SDR FDEA202305071020](https://openairdocs.org/sdr/FDEA202305071020.md): Shear Web · cracked · May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACK AT FR77 NEAR STGR26R AREA REPLACED THE CRACK WEB WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE2 & 51-40-21- 001, PARA.6, PAGE.7B-PAGE.23
- [SDR FDEA202305070982](https://openairdocs.org/sdr/FDEA202305070982.md): Shear Web · cracked · May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACK AT FR79 PLUS 3" NEAR STGR26R AREA REPLACED THE CRACKED SHEAR WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202305070981](https://openairdocs.org/sdr/FDEA202305070981.md): Shear Web · cracked · May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACKED AT FR79 PLUS 3" NEAR STGR26L AREA REPLACED THE CRACKED SHEAR WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE 2
- [SDR FDEA202305051021](https://openairdocs.org/sdr/FDEA202305051021.md): Fitting · cracked · May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Structure
  > AVIONICS COMP'T PICK UP FITTING CRACK AT FRAME 10 FWD SIDE -Y953 POSITION REMOVED CRACK FITTING,THEN INSTALLED NEW ONE WITH FASTENERS,I.A.W A300-600F SRM 51- 72-10-001,PAGE.2 & 51-40-21-001,PARA.6, PAGE.7B~23
- [SDR FDEA202305050992](https://openairdocs.org/sdr/FDEA202305050992.md): Unknown · unknown · May 5, 2023 · N654FE · Airbus A300F4605R · Ailerons
  > LH WING FIXED T/E ARROW EXTRUSION GOT CORROSION BETWEEN RIB26 & RIB28 REPLACED THE DAMAGED SECTION WITH NEW PART AND FASTENERS. I.A.W A300-600F SRM 51- 72-10-001, PAGE 2. AND 51-40-21-001, PARA 13, PAGE 149 - 156
- [SDR FDEA202305050984](https://openairdocs.org/sdr/FDEA202305050984.md): Fitting · cracked · May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AVIONICS COMP'T ANGLE FITTING CRACK AT FRAME10 FWD SIDE Y-953 POSITION CRACKED ANGLE FITTING REPLACED NEW PART, INSTALLED WITH RIVETS, I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.6, PAGE.7B-23
- [SDR FDEA202305050983](https://openairdocs.org/sdr/FDEA202305050983.md): Fitting · cracked · May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AVIONICS COMP'T PICK UP FITTING CRACK AT FRAME10 FWD SIDE Y403 POSITION CRACKED ANGLE FITTING REPLACED NEW PART, INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.6, PAGE.7B-23
- [SDR FDEA202305050977](https://openairdocs.org/sdr/FDEA202305050977.md): Stringer · corroded · May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > FWD CGO COMP'T BAY AFT AREA 1EA BONDING WIRE CONNECTION AREA GOT CORROSION AT S- 44R,FR38.2 POSITON. CUT OUT DAMAGED STRINGER, FABRICATED THE NEW REPAIR STRINGER AND COUPLING AND WET INSTALLED REPAIR PARTS WITH FASTENERS. I.A.W A300-600F SRM 53-10-14-201,
- [SDR FDEA202207081697](https://openairdocs.org/sdr/FDEA202207081697.md): Transmitter · unknown · Jul 8, 2022 · N654FE · Airbus A300F4605R · Hydraulic Indicating System
  > GREEN RSVR LO LEVEL ECAM COMPLIED WITH ECAM AND QRH. NO GREEN HYD SYSTEM, NO AUTO BRAKE, NO NOSE WHEEL STEERING. MANUAL GREER EXTENSION. LANDED KLBB VFR 17R. NO FURTHER EVENT. EMERGENCY DECLARED COMPLETED REQUIRED TSI 29-30/4488 AND REPLACED GREEN H
- [SDR FDEA202207031678](https://openairdocs.org/sdr/FDEA202207031678.md): None · unknown · Jul 3, 2022 · N654FE · Airbus A300* · Hydraulic Indicating System
  > PDIS 654 29-30 4470 02JUL22 MEM OPEN U DURING DESCENT, ECAM FOR GREEN RSVR LO LEVEL. LOW QUANTITY INDICATED ON ECAM AND OVERHEAD PANEL GAUGE. IN TERMINAL AREA AT KMEM, DECLARED AN EMERGENCY, RAN THE L/G GRAVITY EXTENSION CHECKLIST. LANDED ON
- [SDR FDEA202010312730](https://openairdocs.org/sdr/FDEA202010312730.md): Bulkhead · corroded · Oct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, Bulkhead
  > FWD CARGO FR 39, Y-450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSURE
- [SDR FDEA202010312729](https://openairdocs.org/sdr/FDEA202010312729.md): Bulkhead · corroded · Oct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, Bulkhead
  > FWD CARGO FR 39, Y450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSURE F
- [SDR FDEA202010312728](https://openairdocs.org/sdr/FDEA202010312728.md): Bulkhead · corroded · Oct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, Bulkhead
  > FWD CARGO FR 39, Y-1959-Y-2164 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-1959-Y-2164 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORR

Next page: https://openairdocs.org/aircraft/N654FE/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 = 'N654FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N654FE/reports

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