# Service difficulty reports: N656FE

A list on [N656FE](https://openairdocs.org/aircraft/N656FE.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 · 243 reports

- [SDR FDEA202607170941](https://openairdocs.org/sdr/FDEA202607170941.md): Fcu · failed · Jul 17, 2026 · N656FE · Airbus A300F4605R · Flight Control System
  > DURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04
- [SDR FDEA202505030731](https://openairdocs.org/sdr/FDEA202505030731.md): Crossbeam · cracked · May 3, 2025 · N656FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSSBEAM AT FR24, Y-450 - Y-953 CRACKED. COMPLIED WITH EA 6-5310-T0383330 P1 TO REPAIR MDCC CRACKED CROSSBEAM AT FR24, Y-450 - Y-953. EA TITLE: FUSELAGE - MAINFRAME - CRACK ON FR24 CROSSBEAM, BETWEEN -Y450 AND -Y953. THIS IS CATEGORY A REPAIR. MAJOR
- [SDR FDEA202504300692](https://openairdocs.org/sdr/FDEA202504300692.md): Hinge Arm · delaminated · Apr 30, 2025 · N656FE · Airbus A300F4605R · Spoilers
  > RH WING #4 SPOILER CENTER I/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: 20MM*13MM, DEPTH: 1.85MM COMPLIED WITH EA 6-5750-T0383238 P1 TO REPAIR RH WING #4 SPOILER CENTER I/B HINGE ARM LWR SURFACE DELAMINATION, EA TITLE: WING - FLIGHT SURFACES - RH #
- [SDR FDEA202504290733](https://openairdocs.org/sdr/FDEA202504290733.md): Floor Support · corroded · Apr 29, 2025 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC FLOOR SUPPORT AT FR14-16, -Y1959 CORRODED. FABRICATED THE REPAIR PART PER DWG: A53612213(ISSUE.G00) AND PART MARKED AS FXA5361221321200 PER GMM7-0-1001, REPLACED THE MDCC CORRODED FLOOR SUPPORT AT FR14-16, -Y1959 PER A300-600F SRM51-40-21. THIS IS CAT
- [SDR FDEA202504280691](https://openairdocs.org/sdr/FDEA202504280691.md): Hinge Arm · delaminated · Apr 28, 2025 · N656FE · Airbus A300F4605R · Spoilers
  > LH WING #5 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 100MM*15MM, DEPTH: 1.40MM, CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 100MM*20MM, DEPTH: 1.41MM COMPLIED WITH EA: 6-5750-T0383448 P1 TO REPAIR
- [SDR FDEA202504230763](https://openairdocs.org/sdr/FDEA202504230763.md): Rib · cracked · Apr 23, 2025 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.6 AND STGR2.7 REPAIRED THE LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB17 BETWEEN STGR2.6 AND STGR2.7 PER A300-600F SRM57-50-00-201 FIG.201 AND COMPLIED WITH EA 6-5750-T0340067 A P2.
- [SDR FDEA202504230656](https://openairdocs.org/sdr/FDEA202504230656.md): Rib · cracked · Apr 23, 2025 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA:6-5750-T0383190 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BET
- [SDR FDEA202504200764](https://openairdocs.org/sdr/FDEA202504200764.md): Fitting · not reported · Apr 20, 2025 · N656FE · Airbus A300F4605R · Cargo/Baggage Doors
  > 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 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION
- [SDR FDEA202503090340](https://openairdocs.org/sdr/FDEA202503090340.md): Wire · chafed · Mar 9, 2025 · N656FE · Airbus A300F4605R · Door System Wiring
  > FOUND CONNECTOR 70WNA TO ASPSU WIRING CAFFED ON SERVERAL WIRES, REF WRI 52-10 7708. AWM: 52-73-01 INSPECTED WIRING AND FOUND ONLY SMALL SPORADIC AREAS OF OUTER INSULATION FLAKING OFF OF THE KAPTON WIRING. NO WIRING DAMAGE NOTED.
- [SDR FDEA202502280307](https://openairdocs.org/sdr/FDEA202502280307.md): Battery · inoperative · Feb 28, 2025 · N656FE · Airbus A300F4605R · Passenger/Crew Doors
  > DOOR R1 DOES NOT SHOW SLIDE INDICATION ON ECAM WITH DOOR CLOSED AND ARMED. RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 09MAR25 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE
- [SDR FDEA202502150235](https://openairdocs.org/sdr/FDEA202502150235.md): Ground Wire · damaged · Feb 15, 2025 · N656FE · Airbus A300F4605R · Light System Wiring
  > DURING EMERGENCY LIGHTS TEST FOUND EXIT LIGHT OVER R 1 DOOR INOP. WHILE TROUBLESHOOTING FOUND GROUND WIRE RECEPTACLE ON BACK OF LIGHT UNIT BROKEN OFF. REMOVED AND REPLACED R1 DOOR EXIT SIGN MODULE. OPS CHECK GOOD. PER SDR REQUIREMENTS THE UNSERVICEABLE.
- [SDR FDEA202501310161](https://openairdocs.org/sdr/FDEA202501310161.md): Limit Switch · faulted · Jan 31, 2025 · N656FE · Airbus A300F4605R · Emergency Exits
  > RH (FO SIDE) MAIN ENTRY DOOR SLIDE DOESN T INDICATE SLIDE (ARMED) WITH DOOR SLIDE HANDLE IN ARM POSITION. DURING DEBRIEF WITH INBOUND CREW, THEY STATED THE SLIDE INDICATION WAS NORMAL DURING THEIR FLIGHT. PERFORMED BITE TEST OF AUTONOMOUS STANDBY POWER
- [SDR FDEA202407050946](https://openairdocs.org/sdr/FDEA202407050946.md): Evas Unit · no test · Jul 5, 2024 · N656FE · Airbus A300F4605R · Emergency Equipment
  > WHILE WORKING EO 6-2560-E0332400 D PT 2, BLOCK 3, DISCOVERED THAT RH EVAS BLOWER BATTERY LIGHTS DO NOT DISPLAY DURING TEST. BLOWER BLOWS BUT NO LIGHTS. RELEASED FOR SERVICE PER MEL: 25-65-04 CATEGORY: D. RT COCKPIT SMOKE VISION SYSTEM (EVAS) - INOP.
- [SDR FDEA202405220719](https://openairdocs.org/sdr/FDEA202405220719.md): Accumulator · failed · May 22, 2024 · N656FE · Airbus A300F4605R · Hydraulic System, Main
  > ON CLIMB OUT GREENS SYSTEM HYDRAULIC ECAM SHOWED LOW QUANTITY. FOLLOWED ECAM PROCEDURES AND QRH. MANUAL GEAR EXTENSION AND SAFELY LANDED AIRCRAFT. TOWED OFF RUNWAY TO PARKING. FOUND GREEN SYSTEM ACCUMULATOR READING APPROXIMATELY 200 PSI. ATTEMPTED TO SERV
- [SDR FDEA202403070250](https://openairdocs.org/sdr/FDEA202403070250.md): Uplock · failed · Mar 7, 2024 · N656FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > NOSE GEAR DOOR INDICATED UNSAFE UPON EXTENSION FOR APPROACH AND LANDING. SPEED WAS 180KIAS. ALTITUDE WAS 4000MSL. STATUS/FLAPS WERE 15/15. COMPLIED WITH ECAM AND QRH. ON FINAL THE SECOND TIME, SELECTED FLAPS 20 AND SLOWED TO 160. PASSING 3000 FT THE GEAR
- [SDR FDEA202304060568](https://openairdocs.org/sdr/FDEA202304060568.md): Smoke Detector · failed · Apr 6, 2023 · N656FE · Airbus A300* · Fire Detection
  > AVIONICS SMOKE MASTER WARNING ON SHORT FINAL. NO SMOKE DETECTED IN THE COCKPIT OR THROUGH SNIFFER FAN. SMOKE INDICATION AND WARNING WENT AWAY SHORTLY AFTER CLEARING THE RUNWAY. EMERGENCY DECLARED. R&R SMOKE DETECTORS 11WA MAIN BAY SMOKE DETECTOR, AND 13WA
- [SDR FDEA202301190340](https://openairdocs.org/sdr/FDEA202301190340.md): Fitting · none · Jan 19, 2023 · N656FE · Airbus A300* · Wing Main, Frame Structure
  > DURING PERFORM REPEAT INSPECTION FOR CRACK HOLE AT FR40 CENTER WING JOINT LHS,FOUND MIDDLE HOLE OF CENTER WING JOINT FR40 LHS BOLT HOLE DIAMTER DEVIATION. I.A.W WORK CARD T 6-5710-T0321988 CP3,EA WORK CARD TITLE:WING-BASIC WING STRUCTURE- 2019-21-01-CRACK H
- [SDR FDEA202301180236](https://openairdocs.org/sdr/FDEA202301180236.md): Web · damaged · Jan 18, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING WEB REPAIR FOUND ON M/D WEB AT FR47, BTW Y0~Y450 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
- [SDR FDEA202301140235](https://openairdocs.org/sdr/FDEA202301140235.md): Crossbeam · damaged · Jan 14, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 66, 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 121.70
- [SDR FDEA202301130121](https://openairdocs.org/sdr/FDEA202301130121.md): Dummy Rail · worn · Jan 13, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > I.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.4 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202301130120](https://openairdocs.org/sdr/FDEA202301130120.md): Dummy Rail · worn · Jan 13, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > I.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.3 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202301130119](https://openairdocs.org/sdr/FDEA202301130119.md): Dummy Rail · worn · Jan 13, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > I.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 LH NO.4 TRACK GAP WAS 1.06MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202301130118](https://openairdocs.org/sdr/FDEA202301130118.md): Dummy Rail · worn · Jan 13, 2023 · N656FE · Airbus A300* · Fuselage Main, Structure
  > I.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR38.2/FR40 LH NO.4 TRACK GAP WAS 1.09MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202301120304](https://openairdocs.org/sdr/FDEA202301120304.md): Spoiler · delaminated · Jan 12, 2023 · N656FE · Airbus A300F4605R · Wing, Control Surfaces
  > 1EA DISBOND AREA WAS FOUND AT RH #5 SPOILER TOP SKIN.(1"X 2.25") ACCOMPLISHED THE HOT BOND REPAIR ON RH #5 SPOILER I.A.W A300-600F SRM 57-72-11-201, PARA.12B&D, PAGE.211-213, FIG.205&206 MAJOR REPAIR
- [SDR FDEA202301120303](https://openairdocs.org/sdr/FDEA202301120303.md): Spoiler · delaminated · Jan 12, 2023 · N656FE · Airbus A300F4605R · Wing, Control Surfaces
  > 1EA DISBOND AREA WAS FOUND AT LH #3 SPOILER TOP SKIN.(1.25" X 1.5") ACCOMPLISHED THE HOT BOND REPAIR ON LH #3 SPOILER I.A.W A300-600F SRM 57-72-11-201, PARA.12B&D, PAGE.211-213, FIG.205&206 MAJOR REPAIR
- [SDR FDEA202204180989](https://openairdocs.org/sdr/FDEA202204180989.md): None · none · Apr 18, 2022 · N656FE · Airbus A300F4605R · Extinguishing System
  > MDIS 656 26-20 4661 18APR22 LBB OPEN U DURING PREFLIGHT, FOUND #2 ENGINE AGENT 1 DISCHARGE LIGHT ON. DURING TROUBLESHOOTING FOUND ONE OF THE PINS ON PRESSURE SWITCH CANNON PLUG NOT FULLY SEATED INTO
- [SDR FDEA202109172337](https://openairdocs.org/sdr/FDEA202109172337.md): Warning Light · false activation · Sep 17, 2021 · N656FE · Airbus A300F4605R · Door Warning System
  > CLIMBING THROUGH 17 000 FT JUMPSEATER CALLED TO NOTIFY R1 DOOR LIGHT AND ALARM ON. PASSING 18000 GOT ECAM NOTIFICATION OF R1 NOT CLOSED. RAN QRH. INITIATED RETURN TO MEM. ON DES. AT 14000 FT ECAM NOTIFICATION WENT AWAY. AND JS NOTIFIED R1 LIGHT AND AL
- [SDR FDEA202103180689](https://openairdocs.org/sdr/FDEA202103180689.md): Feeder Cable · damaged · Mar 18, 2021 · N656FE · Airbus A300F4605R · Ice/Rain Protection System Wiring
  > CLIMBING THROUGH 14,000 SMELLED SMOKE AND SAW SMOKE COMING FROM LOWER RIGHT HAND CORNER OF CAP S AFT AFT LATERAL WINDOW. AFT LATERAL WINDOW VERY HOT TO TOUCH. NO FAULT ON OVHD AND NO ECAM. NO APPLICABLE QRH PROCEDURE. TURNED LEFT LAT WINDOW HEAT OFF AND CON
- [SDR FDEA2020080761777](https://openairdocs.org/sdr/FDEA2020080761777.md): Support Beam · cracked · Aug 6, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR22-FR23 FOUND CRACKS AS MARKED. FWD CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR22-FR23 FOUND CRACKS AS MARKED. REPLACED THE CRACKED DOOR ACTUATOR SUPPORT BEAM ON FWD CARGO BETWEEN FR22-FR23 PER A300-600F SRM
- [SDR FDEA2020080761776](https://openairdocs.org/sdr/FDEA2020080761776.md): Support Beam · cracked · Aug 6, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Structure
  > AFT CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR61-FR62 FOUND CRACKED. REPLACED THE AFT CARGO DOOR ACTUATOR SUPPORT BEAM IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202007241638](https://openairdocs.org/sdr/FDEA202007241638.md): Frame · cracked · Jul 24, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Frame
  > FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RHS UPPER BOLT HOLE WITH CRACK SIGNAL. INSPECTION COMPLIED WITH IAW EA 6-5710-T0355356 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202007201585](https://openairdocs.org/sdr/FDEA202007201585.md): Crossbeam · cracked · Jul 20, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Structure
  > CROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. CROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACK. COMPLY WITH EA:6-5310-T0355184 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA2020080541507](https://openairdocs.org/sdr/FDEA2020080541507.md): Floorbeam · cracked · Jul 14, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y953 AND -Y1456 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM AT FR64, BETWEEN -Y953 AND -Y1456. PER A300-600F SRM51-10-15 FIG211.THIS REPAIR WAS CATEGORY CATEGO
- [SDR FDEA2020080514506](https://openairdocs.org/sdr/FDEA2020080514506.md): Floorbeam · cracked · Jul 14, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959. REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM IAW SRM 53-10-15 FIG211. THIS REPAIR WAS CATEGORY A REPAIR, MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA2020080314507](https://openairdocs.org/sdr/FDEA2020080314507.md): Floorbeam · cracked · Jul 14, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64, BETWEEN -Y953 AND -Y1456. THE FLOORBEAM WAS REPAIRED IAW SRM 51-40-21, & SRM 53-10-15, FIG 211. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA2020080314506](https://openairdocs.org/sdr/FDEA2020080314506.md): Floorbeam · cracked · Jul 14, 2020 · N656FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959
- [SDR FDEA201907031476](https://openairdocs.org/sdr/FDEA201907031476.md): Warning System · false activation · Jul 3, 2019 · N656FE · Airbus A300F4605R · Trailing Flap Position Indicating System
  > PDIS 656 27-50 1775 03JUL19 YOW OPEN U LOGPAGES:2691848 ON 6 MILE FINAL SELECTED FLAPS 20 FOR A FLAP 20 LANDING; GOT ECAM FLAP SYS 1 FAULT WITH SINGLE LITE ON OVHD PANEL (FLAP SYS 1 FAULT). FLAPS INDICATED AT FLAP 20, CYCLED FLAPS WITH NO CH
- [SDR FDEA201902076262](https://openairdocs.org/sdr/FDEA201902076262.md): Smoke Warning · false activation · Feb 6, 2019 · N656FE · Airbus A300F4605R · Smoke Detection
  > AFTER DEICE WENT TO START # 2 AND GOT A CARGO SMOKE INDICATION. CREW ELECTED TO CALL AIRPORT FIRE DEPARTMENT TO INSPECT FOR SMOKE. FIRE DEPARTMENT ARRIVED AND INSPECTED ALL CARGO COMPARTMENTS ON AIRCRAFT. NO EVIDENCE OF SMOKE OR FIRE PRESENT. WHEN MX ARRIV
- [SDR FDEA201805301342](https://openairdocs.org/sdr/FDEA201805301342.md): Rudder · none · May 30, 2018 · N656FE · Airbus A300* · Rudder Structure
  > REWORK OF N/R# N00817 REQUIRED DUE TO INCORRECT REPAIR BEING ACCOMPLISHED ON RUDDER. ACCOMPLISHED REPAIR ON RUDDER IAW SRM 55-41-12 PARA 22 FIG 221. RSC TRACKING EA 6- 5540-T0340242 PART 1. STABILIZER - RUDDER - DENT FOUND ON RUDDER LEFT SKIN - SRM COMPOSITE
- [SDR FDEA2018052191264](https://openairdocs.org/sdr/FDEA2018052191264.md): Rib · cracked · May 19, 2018 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB 19 HAD A CRACK AT THE 6TH FASTENER, FWD OF THE REAR SPAR. REMOVED THE CRACK ON THE RIB, FABRRICATED, AND INSTALLED A RIB REPAIR AND DOUBLER IAW SRM 57-50-00, PARA 4A,E. MAJOR REPAIR.
- [SDR FDEA201805191263](https://openairdocs.org/sdr/FDEA201805191263.md): Rib · cracked · May 19, 2018 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB 17 WAS CRACKED AT THE 6TH FASTENER, FWD OF THE REAR SPAR. REMOVED AND REPLACED THE RIB IAW SRM 57-50-00, PARA 4A. MAJOR REPAIR.
- [SDR FDEA2018052191262](https://openairdocs.org/sdr/FDEA2018052191262.md): Rib · cracked · May 19, 2018 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB 11 HAD A CRACK AT THE 6TH FASTENER FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 202. MAJOR REPAIR.
- [SDR FDEA2018052191261](https://openairdocs.org/sdr/FDEA2018052191261.md): Seat Track · worn · May 19, 2018 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > DURING DUMMY SEAT TRACK INSPECTION EO 6-5310-7-3322, FOUND THE SEAT TRACK AT FR 54.1, Y2462 WORN BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21, AND SRM 53-15-16. MAJOR REPAIR.
- [SDR FDEA2018052191260](https://openairdocs.org/sdr/FDEA2018052191260.md): Rib · cracked · May 19, 2018 · N656FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB 12 HAS A CRACK AT THE 6TH FASTNER FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201.
- [SDR FDEA2018051651240](https://openairdocs.org/sdr/FDEA2018051651240.md): Floor Panel · broken · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 321BH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA2018051651241](https://openairdocs.org/sdr/FDEA2018051651241.md): Floor Panel · broken · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 232YG FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201805151234](https://openairdocs.org/sdr/FDEA201805151234.md): Floor Panel · damaged · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > UPPER MAIN CARGO DECK FLOOR PANEL 242UJ WAS FOUND DAMAGED FROM CARGO LOCKS AT NUMEROUS PLACES. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201805151233](https://openairdocs.org/sdr/FDEA201805151233.md): Floor Panel · broken · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 252DH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201805151232](https://openairdocs.org/sdr/FDEA201805151232.md): Floor Panel · broken · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 252UH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201805151231](https://openairdocs.org/sdr/FDEA201805151231.md): Floor Panel · broken · May 15, 2018 · N656FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 231AH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N656FE/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 = 'N656FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N656FE/reports

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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.