# Service difficulty reports: N667FE

A list on [N667FE](https://openairdocs.org/aircraft/N667FE.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 FDEA202609151338](https://openairdocs.org/sdr/FDEA202609151338.md): Pitot Tube · inoperative · Sep 15, 2026 · N667FE · Airbus A300F4605R · Pitot/Static System
  > DURING TAKEOFF CA AIRSPEED INDICATOR INDICATED 0. ABORTED TAKEOFF AND TAXIED BACK TO RAMP. REMOVED AND REPLACED CAPT'S PITOT TUBE EF AMM 34-11-15-04. LEAK CHECK GOOD. ACFT OK FOR CONTINUED SERVICE.
- [SDR FDEA202602170220](https://openairdocs.org/sdr/FDEA202602170220.md): Lever · inoperative · Feb 17, 2026 · N667FE · Airbus A300F4605R · Passenger/Crew Doors
  > L1 DOOR SLIDE LEVER WILL NOT MOVE TO ARM. AMM: 52-10-11-05-02 CHECKED FOR CORRECT OPERATION OF SLIDERS AND GIRT BAR. NO BINDING NOTED. ARMING HANDLE ARMS AND DISARMS SMOOTH. ARMED AND DISARMED SEVERAL TIMES. OKAY FOR SERVICE..
- [SDR FDEA202602150212](https://openairdocs.org/sdr/FDEA202602150212.md): Safety Wire · wrong part · Feb 15, 2026 · N667FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 A P1, FOUND SAFETY WIRE ON EJECTOR BAG RELEASE CABLE INCORRECT. REMOVED AND REPLACED EJECTOR BAG RELEASE CABLE SAFTEY WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. AC GOOD FOR SERVICE.
- [SDR FDEA202602030119](https://openairdocs.org/sdr/FDEA202602030119.md): Bottle · leaking · Feb 3, 2026 · N667FE · Airbus A300F4605R · Passenger/Crew Doors
  > LI DOOR ASSIST BOTTLE LEAKING. RELEASED FOR SERVICE PER MEL 52-11-01-05 CATEGORY: C. LEAK CHKD. SHOWS A LEAK ON ACCUMULATOR PARTING LINE. OK TO CONTINUE ON MEL. REMOVED AND REPLACED L1 DOOR DAMPER AND EMERGENCY OPS CYLINDER IAW AMM 52-10-14-04-02, OPS GOOD
- [SDR FDEA202510272093](https://openairdocs.org/sdr/FDEA202510272093.md): Door · unknown · Oct 27, 2025 · N667FE · 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 FDEA202510111960](https://openairdocs.org/sdr/FDEA202510111960.md): Door · cracked · Oct 11, 2025 · N667FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 2EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0385331 P1. REPAIR IS CONSIDERED AS CAT B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE(DT) APPROVAL. REQUIREMENT WILL BE TRACKE
- [SDR FDEA202510111959](https://openairdocs.org/sdr/FDEA202510111959.md): Skin · cracked · Oct 11, 2025 · N667FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN UPR EDGE FOUND 1EA CRACK AT BEAM 1 FWD OF FR22A COMPLIED WITH EA: 6-5230-T0385276 P1. REPAIRED THE FWD CARGO DOOR CRACKED INNER SKIN AT BEAM 1 FWD OF FR22A. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION PER EA: 6-5230-T038527
- [SDR FDEA202510111958](https://openairdocs.org/sdr/FDEA202510111958.md): Seat Track · cracked · Oct 11, 2025 · N667FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK SEAT TRACK CRACKED AT -Y953 BETWEEN FR18 AND FR19. REPLACED THE CRACKED SEAT TRACK AT -Y953 BETWEEN FR18 AND FR19 WITH FABRICATED PART IAW SRM 51-40-21 AND DWG A53612524(ISSUE: A00). THIS IS CATEGORY -A- REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202510041893](https://openairdocs.org/sdr/FDEA202510041893.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 2EA CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPAR，AND RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS
- [SDR FDEA202510041892](https://openairdocs.org/sdr/FDEA202510041892.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 4EA CRACKS AT RIB26 BETWEEN STGR2.7 AND REAR SPAR, AND RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 16
- [SDR FDEA202510041891](https://openairdocs.org/sdr/FDEA202510041891.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB16 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0385199 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 16, 17, 19, 26 AND 27 AT STR. 2.7/2.8. REPAIR
- [SDR FDEA202510041890](https://openairdocs.org/sdr/FDEA202510041890.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 11 BETWEEN S2.7 AND S2.8 COMPLIED WITH EA 6-5750-T0385199 P1. REPAIRED THE LT WING CENTER FLAP RIB UPPER FLANGE CRACK THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 57506818
- [SDR FDEA202510041889](https://openairdocs.org/sdr/FDEA202510041889.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIBS UPR FLANGE FOUND 8EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, AND RIB26 BETWEEN STGR2.6 AND REAR SPAR, AND RIB27 BETWEEN STGR2.6 AND REAR SPAR. REPAIRED THE RT WING CENTER FLAP RIBS UPR FLANGE 8EA CRACKS AT RIB25 BETWEEN STGR2
- [SDR FDEA202510041888](https://openairdocs.org/sdr/FDEA202510041888.md): Rib · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB12 BETWEEN STGR2.7 AND STGR2.8 REPAIRED THE RT WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB12 BETWEEN STGR2.7 AND STGR2.8. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 5750681
- [SDR FDEA202510041887](https://openairdocs.org/sdr/FDEA202510041887.md): Web · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK UNDERFLOOR WEB CRACKED AT FR47 BETWEEN -Y953 AND -Y1456 REPLACED THE CRACKED WEB ON MAIN DECK UNDERFLOOR AT FR47 BETWEEN -Y953 AND -Y1456 WITH FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: A53832103(ISSUE: E). THIS IS CATEGORY A REPAIR. MAJOR
- [SDR FDEA202510041886](https://openairdocs.org/sdr/FDEA202510041886.md): Web · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK UNDERFLOOR WEB CRACKED AT FR47 BETWEEN Y953 AND Y1456. REPAIRED THE CRACKED WEB ON MAIN DECK UNDERFLOOR AT FR47 BETWEEN Y953 AND Y1456 PER A300-600F SRM53-15-15-201-C2. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER SR
- [SDR FDEA202510041885](https://openairdocs.org/sdr/FDEA202510041885.md): Floorbeam · cracked · Oct 4, 2025 · N667FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS CATEGORY A REPA
- [SDR FDEA202502220272](https://openairdocs.org/sdr/FDEA202502220272.md): Fitting · leaking · Feb 22, 2025 · N667FE · Airbus A300F4605R · Passenger/Crew Doors
  > REF MTSI #52-10 6104. FOUND L1 DOOR PNEUMATIC ACCUMULATOR WITH SLOW LEAK. FIM: 52-10-00 FIG 101 AMM: 52-10-14 RATIER FIGEAC CMM: 52-11-02 AMM: 52-10-14-03-02 REF TSM 52-10-00 FIG 101 BLOCK 4, FOUND LEAK AT POINT 4. FOUND FITTING EXTREMELY LOOSE.TIGHT
- [SDR FDEA202502210263](https://openairdocs.org/sdr/FDEA202502210263.md): Bottle · low pressure · Feb 21, 2025 · N667FE · Airbus A300F4605R · Passenger/Crew Doors
  > L1 DOOR PNEUMATIC ACCUMULATOR PRESSURE LOW AMM: 52-10-14-03-02 SERVICED L1 DOOR PNEUMATIC ACCUMULATOR PER AMM
- [SDR FDEA202412261843](https://openairdocs.org/sdr/FDEA202412261843.md): Blower · no test · Dec 26, 2024 · N667FE · Airbus A300F4605R · Emergency Equipment
  > WHILE PERFORMING WORK CARD E.O.6-2560-E0332400 P2. FOUND CAPT (LH) EVAS BLOWER WILL NOT TEST.
- [SDR FDEA202409051244](https://openairdocs.org/sdr/FDEA202409051244.md): Actuator · failed · Sep 5, 2024 · N667FE · Airbus A300F4605R · Aileron Control System
  > AFTER STARTING #1 ENG, AILERONS DEFLECTED FULL LEFT AND WOULD NOT RETURN TO CENTER. AUTOPILOT WAS VERIFIED OFF.. WITH ALL HYD SYSTEMS PRESSURIZED AND THE GREEN AND YELLOW SERVOS OFF THE RIGHT AILERON IS DEFLECTING RIGHT WING UP. NOTED HYD LINES AT THE AU
- [SDR FDEA202409041237](https://openairdocs.org/sdr/FDEA202409041237.md): Hydraulic System · malfunctioned · Sep 4, 2024 · N667FE · Airbus A300F4605R · Hydraulic System, Main
  > AFTER STARTING #1 ENG, AILERONS DEFLECTED FULL LEFT AND WOULD NOT RETURN TO CENTER. AUTOPILOT WAS VERIFIED OFF. WITH ALL HYD SYSTEMS PRESSURIZED AND THE GREEN AND YELLOW SERVOS OFF THE RIGHT AILERON IS DEFLECTING RIGHT WING UP. NOTED HYD LINES AT THE A
- [SDR FDEA202406150807](https://openairdocs.org/sdr/FDEA202406150807.md): Pitot Tube · failed · Jun 15, 2024 · N667FE · Airbus A300F4605R · Pitot/Static System
  > TAKEOFF, MEM, NO AIRSPEED ON CAPT PFD. REJECTED THE TAKEOFF AT 80 KIAS. RAN RTO CHECKLIST. RTO ~85 KNOTS AT 246,000 LBS. R & R CAPT'S PITOT PROBE (41DA) IAW AIRBUS A300 AMM 34-11-15-04, ERFORMED LEAK AND FUNCTIONAL TEST OF CAPT'S PITOT PROBE IAW AMM 34-1
- [SDR FDEA202308171782](https://openairdocs.org/sdr/FDEA202308171782.md): Rib · cracked · Aug 17, 2023 · N667FE · Airbus A300* · Wing, Rib/Bulkhead
  > L3 SPOILER ACTUATOR I/B JACK RIB CRACK REPLACED THE NEW L3 SPLR ACTUATOR JACK RIB I.A.W A300-600F SRM 51-72-10-001, P.2
- [SDR FDEA202307191287](https://openairdocs.org/sdr/FDEA202307191287.md): Spoiler · unknown · Jul 19, 2023 · N667FE · Airbus A300* · Spoilers
  > AIRCRAFT REPAIR ASSESSMENT EXISTING REPAIR FOUND ON LH #3 SPOILER CENTER HINGE ARM 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
- [SDR FDEA202307191286](https://openairdocs.org/sdr/FDEA202307191286.md): Spoiler · unknown · Jul 19, 2023 · N667FE · Airbus A300* · Spoilers
  > AGING AIRCRAFT ASSESSMENT: EXISTING REPAIR FOUND ON LH #3 SPOILER CENTER HINGE ARM 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
- [SDR FDEA202307111275](https://openairdocs.org/sdr/FDEA202307111275.md): Profile · cracked · Jul 11, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE PROFILE-Z FOUND CRACK NEAR FR 79 PLUS 5",Y1650 REPLACED WITH NEW PROFILE-Z I.A.W A300-600F SRM 51-72-10-001, PAGE 2.
- [SDR FDEA202307101279](https://openairdocs.org/sdr/FDEA202307101279.md): Seat Track · worn · Jul 10, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM ACTUAL MEASUREMENT:1.143MM. IAW SRM 53-15-16 PARA 5A PAGE 201- PAGE210 FIG.201 PERFORM REPAIR ACCOMPLISHED. MAJOR REPAIR
- [SDR FDEA202307071281](https://openairdocs.org/sdr/FDEA202307071281.md): Seat Track · corroded · Jul 7, 2023 · N667FE · Airbus A300* · Fuselage Floor Panel
  > MAIN DECK DUMMY SEAT TRACK WAS BULGING AT -Y1456 FR54.1 AREA. REPLACED THE DUMMY SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B-50
- [SDR FDEA202307061280](https://openairdocs.org/sdr/FDEA202307061280.md): Seat Track · corroded · Jul 6, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE DUMMY SEAT TRACK FOUND CORROSION AT FR 54.1, Y-450 REPLACED DUMMY SEAT TRACK WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, P2.
- [SDR FDEA202307041221](https://openairdocs.org/sdr/FDEA202307041221.md): Web · cracked · Jul 4, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE SHEAR WEB FOUND CRACK NEAR FR79 PLUS 5",Y1650 REPLACED THE CRACKED SHEAR WEB WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, PAGE2.
- [SDR FDEA202307041220](https://openairdocs.org/sdr/FDEA202307041220.md): Web · cracked · Jul 4, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE SHEAR WEB FOUND CRACK NEAR FR79 PLUS 5", Y-1650 REPLACED THE CRACKED SHEAR WEB WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, PAGE2.
- [SDR FDEA202306301224](https://openairdocs.org/sdr/FDEA202306301224.md): Web · cracked · Jun 30, 2023 · N667FE · Airbus A300* · Wing Miscellaneous Structure
  > LH WING T/E CAVITY TOP SKIN PNL SUPPORT WEB CRACK AT SPOILER#5 HINGE ARM REPLACED THE CRACK SUPPORT WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE2
- [SDR FDEA202306291226](https://openairdocs.org/sdr/FDEA202306291226.md): Floor Panel · damaged · Jun 29, 2023 · N667FE · Airbus A300* · Fuselage Floor Panel
  > CATWALK FLOOR PANEL SOFT AT FR87-FR88 FABRICATED THE NEW FLOOR PANEL I.A.W FEDEX STANDARD REPAIR DRAWING NO:SRZ-25-005 "MAJOR REPAIR"
- [SDR FDEA202306271276](https://openairdocs.org/sdr/FDEA202306271276.md): Adapter · worn · Jun 27, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK COMPT FOUND 1EA CLS ADAPTER-FLANGE AREA WORN LOCATION AT FR68, BETWEEN Y-1378 AND Y-1778 DAMAGED CLS ADAPTER REPLACED NEW PART, INSTALLED WITH HI-LOK I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND 51-40-21-001, PARA.7, PAGE.24 - PAGE.50
- [SDR FDEA202306271273](https://openairdocs.org/sdr/FDEA202306271273.md): Support · cracked · Jun 27, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > CENTER MAIN DECK COMPT - LH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR38.1 TO FR38.2 COMMON TO Y2462. REPLACED THE NEW SUPPORT I.A.W A300-600F SRM 51-72-10-001,P2 AND SRM 51-40-21-001 PARA,7,PAGE 24~PAGE 50
- [SDR FDEA202306271225](https://openairdocs.org/sdr/FDEA202306271225.md): Profile · cracked · Jun 27, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK UTILITY AREA FOUND 1EA Z-PROFILE CRACKED AT FR80 AND -Y1470 POSITION REPLACED THE NEW PROFILE-Z. I.A.W A300-600F SRM 51-72-10-001, P2
- [SDR FDEA202306271223](https://openairdocs.org/sdr/FDEA202306271223.md): Support · cracked · Jun 27, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > CENTER MAIN DECK COMPT - RH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR38.1 TO FR38.2 COMMON TO -Y2462 REPLACED THE NEW SUPPORT. I.A.W A300-600F SRM 51-72-10-001,P2
- [SDR FDEA202306271222](https://openairdocs.org/sdr/FDEA202306271222.md): Support · cracked · Jun 27, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > CENTER MAIN DECK COMPT - RH SIDE END FLOOR SUPPORT GOT CRACKED LOCATION FROM FR37 TO FR38 COMMON TO -Y2462 REPLACED THE NEW SUPPORT. I.A.W A300-600F SRM 51-72-10-001,P2
- [SDR FDEA202306271215](https://openairdocs.org/sdr/FDEA202306271215.md): Aileron · unknown · Jun 27, 2023 · N667FE · Airbus A300* · Ailerons
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON UPR & LWR SKIN AT RIB 13,T/E COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202306271180](https://openairdocs.org/sdr/FDEA202306271180.md): Flap · unknown · Jun 27, 2023 · N667FE · Airbus A300* · Trailing Edge Flaps
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 19~21, REAR SPAR DATUM 7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIR
- [SDR FDEA202306261219](https://openairdocs.org/sdr/FDEA202306261219.md): Crossbeam · unknown · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage Main, Structure
  > 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 121.707, INSPECTION OF EXISTING REPA
- [SDR FDEA202306261197](https://openairdocs.org/sdr/FDEA202306261197.md): Flap · dented · Jun 26, 2023 · N667FE · Airbus A300* · Trailing Edge Flaps
  > RH WING CENTER FLAP NOSE FOUND 1EA DENT AT RIB19 PLUS 3" AREA PFM NOSE SKIN FLUSH REPAIR BY SKIN INSERT AND BUTTSTRAP WITH RIVETS, THIS IS CAT B REPAIR. I.A.W A300-600F SRM 57-50-00-201 FIG.208, PAGE.231-236 AND SRI:57-50-00-201, IIR:57-50- 00-2-002-00, PAR
- [SDR FDEA202306261192](https://openairdocs.org/sdr/FDEA202306261192.md): Support · corroded · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FWD MAIN DECK UTILITY AREA - FLOOR SUPPORT GOT CORROSION LOCATION FROM FR13A TO FR14 COMMON TO Y730 REPLACED THE CORRODED SUPPORT WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B-PAGE 23.
- [SDR FDEA202306261165](https://openairdocs.org/sdr/FDEA202306261165.md): Seat Track · unknown · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 75~76, -Y1221.2 TO -Y1623.6 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 1
- [SDR FDEA202306261162](https://openairdocs.org/sdr/FDEA202306261162.md): Seat Track · unknown · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 74~75, -Y852.4 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 FDEA202306261161](https://openairdocs.org/sdr/FDEA202306261161.md): Seat Track · none · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 63~66, Y0 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, I
- [SDR FDEA202306261145](https://openairdocs.org/sdr/FDEA202306261145.md): Seat Track · unknown · Jun 26, 2023 · N667FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 57.1~57.3, 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 FDEA202306261137](https://openairdocs.org/sdr/FDEA202306261137.md): Elevator · damaged · Jun 26, 2023 · N667FE · Airbus A300* · Elevator Structure
  > RH H/S ELEVATOR T/E SEVERAL FILLERS DETERIORATION. PFM ELEVATOR TRAILING EDGE FILLER REPAIR WITH RESIN I.A.W A300-600F SRM 55-21-12-201 PARA 5G, FIG 210, PAGE 257-262, THIS IS CAT B REPAIR I.A.W A300-600F SRI 55-21-12-201 IIR 55-21- 12-2-001-00 PARA 3A, PAG
- [SDR FDEA202306261136](https://openairdocs.org/sdr/FDEA202306261136.md): Elevator · damaged · Jun 26, 2023 · N667FE · Airbus A300* · Elevator Structure
  > LH H/S ELEVATOR T/E SEVERAL FILLERS DETERIORATION. PFM ELEVATOR TRAILING EDGE FILLER REPAIR WITH RESIN IAW SRM 55-21-12-201 PARA 5G, FIG 210, PAGE 257-262, THIS IS CAT B REPAIR I.A.W SRI 55-21-12-201 IIR 55-21- 12-2-001-00 PARA 3A, PAGE 201-205, TABLE 202

Next page: https://openairdocs.org/aircraft/N667FE/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 = 'N667FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N667FE/reports

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