# Service difficulty reports: N653FE

A list on [N653FE](https://openairdocs.org/aircraft/N653FE.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 · 221 reports

- [SDR FDEA202402210193](https://openairdocs.org/sdr/FDEA202402210193.md): Skin · delaminated · Feb 21, 2024 · N653FE · Airbus A300F4605R · Elevator, Plate/Skin
  > RH ELEVATOR TOP SKIN BROKEN AT ER2 - ER5 INSTALLED THE REPAIR FLIES ON RH ELEVATOR TOP SKIN AT ER2 - ER5 PER A300-600F SRM55--21- 12-201 PARA.5.H & SRM51-77-12-201. MINOR REPAIR IAW FEDEX GMM 6-2-100 ENTERED BY ERROR. THIS REPAIR IS JUST A COSMETIC REPAIR PE
- [SDR FDEA202402180183](https://openairdocs.org/sdr/FDEA202402180183.md): Seat Track · worn · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK Y-2462 WORN AT FR63 REPAIRED THE WORN SEAT TRACK IN MAIN DECK Y-2462 AT FR63 PER A300-600F SRM53-10-16-201 PARA.4.THIS IS ACT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402180182](https://openairdocs.org/sdr/FDEA202402180182.md): Floorbeam · cracked · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MDCC FLOOR CROSSBEAM FR30 CRACKED BETWEEN Y1456 - Y1959 COMPLIED WITH EA 6-5310 -T REPAIRED THE MDCC FLOOR CROSSBEAM FR30 CRACKED. REPAIR WITH MINOR DEVIATIONS. THIS REPAIR IS CAT. A REPAIR, MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402180181](https://openairdocs.org/sdr/FDEA202402180181.md): Web · cracked · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402180180](https://openairdocs.org/sdr/FDEA202402180180.md): Web · cracked · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-953 - Y-1456 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402180179](https://openairdocs.org/sdr/FDEA202402180179.md): Web · cracked · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y-450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y-450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402180178](https://openairdocs.org/sdr/FDEA202402180178.md): Web · cracked · Feb 18, 2024 · N653FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WEB CRACKED AT FR47 Y450 - Y0 REPAIRED THE CRACKED WEB IN MAIN DECK FLOOR STRUCTURE AT FR47 Y450 - Y0 PER A300- 600F SRM53-15-15-201 FIG.201.THIS IS CAT B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202402170175](https://openairdocs.org/sdr/FDEA202402170175.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WNG CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES
- [SDR FDEA202402170174](https://openairdocs.org/sdr/FDEA202402170174.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR. TITLE: W
- [SDR FDEA202402170173](https://openairdocs.org/sdr/FDEA202402170173.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR. TITLE: W
- [SDR FDEA202402170172](https://openairdocs.org/sdr/FDEA202402170172.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. TITLE:
- [SDR FDEA202402170171](https://openairdocs.org/sdr/FDEA202402170171.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFA
- [SDR FDEA202402170170](https://openairdocs.org/sdr/FDEA202402170170.md): Skin · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 6EA CRACKED AT RIB25,RIB26,RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25,26,27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: W
- [SDR FDEA202402170169](https://openairdocs.org/sdr/FDEA202402170169.md): Rib · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACKED AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES -
- [SDR FDEA202402170168](https://openairdocs.org/sdr/FDEA202402170168.md): Rib · cracked · Feb 17, 2024 · N653FE · Airbus A300F4605R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB13 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH
- [SDR FDEA202402130154](https://openairdocs.org/sdr/FDEA202402130154.md): Floorbeam · cracked · Feb 13, 2024 · N653FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MDCC FLOOR CROSSBEAM FR59 CRACKED BETWEEN Y-953 ~ Y-1456 REPAIRED THE CRACK IN THE MDCC FLOOR CROSSBEAM FR59 BETWEEN Y-953 ~ Y-1456 PER A300-600F SRM51-40-21 & SRM53-10-15-201 PARA.14. THE REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202401130074](https://openairdocs.org/sdr/FDEA202401130074.md): Control Unit · failed · Jan 13, 2024 · N653FE · Airbus A300F4605R · Fuel Indicating System
  > ON INITIAL CLIMB OUT RECEIVED TRIM TANK AFT TRANSFER NOT AVAILABLE CAUTION. PASSING 8000 MSL, LEFT ECAM SHOWED AMBER XXX IN GW, CG, AND T. FUEL. RIGHT ECAM SHOWED AMBER XXX IN LEFT INNER AND LEFT OUTER FUEL TANKS, AS WELL AS TOTAL FUEL, GW, AND CG. THE OV
- [SDR FDEA202401020007](https://openairdocs.org/sdr/FDEA202401020007.md): Coalescer Bag · failed · Jan 2, 2024 · N653FE · Airbus A300* · Humidity Control System
  > DURING DESCENT WHEN THROTTLES REDUCED TO IDLE, STRONG BURST OF SMOKE SMELL AND SLIGHT HAZE IN THE COCKPIT. IMMEDIATELY CLEARED AND DID NOT REOCCUR. REMOVED AND REPLACED BOTH COALESCER BAGS IAW A300 AMM 21-51-16-03. ITEM CLOSED. GROUND RUN CARRIED OUT AS
- [SDR FDEA202312140107](https://openairdocs.org/sdr/FDEA202312140107.md): Transmitter · faulted · Dec 14, 2023 · N653FE · Airbus A300F4605R · Landing Gear Brake System
  > ON LANDING ROLLOUT BRAKING WAS NOT AVAILABLE ON THE RIGHT SIDE FROM EITHER SEAT WITH THE BRAKES IN NORM/ON. SWITCHED BRAKES TO ALTN /ON AND BRAKING WAS RESTORED. PUMPED BRAKES IN NORMAL POSITION ON BOTH CAPT AND FO SIDE. NOTICED BRAKES WERE SLOW AND SPO
- [SDR FDEA202310231880](https://openairdocs.org/sdr/FDEA202310231880.md): Bulb · failed · Oct 23, 2023 · N653FE · Airbus A300* · Emergency Lighting
  > MDIS 653 33-50 6974 23OCT23 GSO FACT U ON 'A' CHECK, EMERG TEST BUTTON ON PANEL 25WL NOT ILLUMINATED. T/S PE ABOVE AMM, FOUND RED FAILURE LIGHT ON POWER SUPPULY UNIT 29WL. INSTALLED NEW BATTERY PER ABOVE AMM, NO RED OR GREEN LIGHT ON POWER U
- [SDR FDEA202210282684](https://openairdocs.org/sdr/FDEA202210282684.md): Valve · faulted · Oct 28, 2022 · N653FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > ON DEPARTURE WHEN RAISING THE GEAR WE GOT A LANDING GEAR RETRACTION FAULT. WE COMPLIED WITH THE QRH AND RETURN TO SDF FOR LANDING. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE. REMOVED AND REPLACED LANDING GEAR ELECTROVALVE 3GA IAW AMM 32-
- [SDR FDEA202209132318](https://openairdocs.org/sdr/FDEA202209132318.md): Overheat Loop · failed · Sep 13, 2022 · N653FE · Airbus A300F4605R · Overheat Detection
  > DURING CLIMBOUT, GOT AN ECAM MESSAGE GREEN RSVR OVHT. COMPLETED THE ECAM AND QRH, OVHT LIGHT INTERMITTENT. CONTINUED FLIGHT. DURING DESCENT, OVHT LIGHT EXTINGUISHED, DECIDED TO RESTORE SYS USING EDP. DECLARED AN EMERGENCY & LANDED WITHOUT ISSUES. IAW MM
- [SDR FDEA202205131201](https://openairdocs.org/sdr/FDEA202205131201.md): Control Unit · failed · May 13, 2022 · N653FE · Airbus A300F4605R · Autopilot System
  > AT FL 310, THE AUTOPILOT AND AUTO THROTTLES KICKED OFF. LOST FMAS AND FCP FOR THE REMAINDER OF THE FLIGHT. THE FD WERE NOT WORKING EITHER. REMOVED AND REPLACED FLIGHT CONTROL UNIT (303CA) USING MM 22-15-12-04, PERFORMED AFS/LAND AND LIGHT DISPLAY ALL CHEC
- [SDR FDEA202112033045](https://openairdocs.org/sdr/FDEA202112033045.md): Switch · unknown · Dec 3, 2021 · N653FE · Airbus A300* · Passenger/Crew Doors
  > R1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL: 52-XX-XX CAT: C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SY
- [SDR FDEA202112033044](https://openairdocs.org/sdr/FDEA202112033044.md): Switch · unknown · Dec 3, 2021 · N653FE · Airbus A300* · Passenger/Crew Doors
  > R1 DOOR CLOSES AND GREEN LOCKED INDICATORS SHOW IT CLOSED BUT SLIDES DOESN'T APPEAR ON ECAM MEL 03DEC21 RELEASED FOR SERVICE PER MEL: 52-XX-XX CAT: C EXP: 13DEC21 MEL 52-XX-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SY
- [SDR FDEA202108272108](https://openairdocs.org/sdr/FDEA202108272108.md): Skin · damaged · Aug 27, 2021 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > SCRATCHES WERE FOUND AT FR57 10", S41L 0.2" AND FR57 13" TO FR57 18", S43L. ACCOMPLISHED EXTERNAL SKIN DOUBLER REPAIR I.A.W. A300-600F SRM 53-10-12-201 P.265~268 FIG207 SM4.THIS IS CAT B REPAIR I.A.W. A300-600F SRI 53-10-12-201 AND IIR 53-10-12- 2-001-00.
- [SDR FDEA202107272005](https://openairdocs.org/sdr/FDEA202107272005.md): Doubler · gouged · Jul 27, 2021 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > DURING PFM WORKCARD:E6-5100-7-5000 D7 PT1, FOUND GOUGE ON THE EXISTING REPAIR DOUBLER SURFACE AND SKIN CUTOUT EDGE AREA AT FR20A BETWEEN S-38R TO S-41R. GENERTAING FROM EO:E6-5100-7-5000 D7 PT1 & WO/NRC:00080535/N00132, ACCOMPLISHED THE WORK I.A.W. E.A:T6-
- [SDR FDEA202107261934](https://openairdocs.org/sdr/FDEA202107261934.md): Frame · damaged · Jul 26, 2021 · N653FE · Airbus A300F4605R · Fuselage Main, Frame
  > 1EA DAMAGE HOLE WAS FOUND AT FR47, S-24R, SPLICE FITTING, HOLE H AREA I.A.W. EO: 6-5310-7-50170 PART 6 FUSELAGE MAINFRAME - INSPECTION HOLE IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26 LH/RH, AIRBUS SB A300-53-6123( SEQ NO: 001066) PERFORM A
- [SDR FDEA202107261857](https://openairdocs.org/sdr/FDEA202107261857.md): Skin · delaminated · Jul 26, 2021 · N653FE · Airbus A300F4605R · Rudder, Plate/Skin
  > 1EA WATER TRAPPED AREA (50MMX50MM) WAS FOUND AT RH RUDDER T/E SCREW NEAR NO.37 FASTENER. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 22, FIG. 220, P. 286-294 AND SRI 55-71-12-201, IIR 55-41-12-2-005-00, 3E.
- [SDR FDEA202107251898](https://openairdocs.org/sdr/FDEA202107251898.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #131NG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251897](https://openairdocs.org/sdr/FDEA202107251897.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #131LG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251896](https://openairdocs.org/sdr/FDEA202107251896.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #131SG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251895](https://openairdocs.org/sdr/FDEA202107251895.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #131RG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251894](https://openairdocs.org/sdr/FDEA202107251894.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132QG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251893](https://openairdocs.org/sdr/FDEA202107251893.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO COMPT FLOOR PANEL #151QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202107251892](https://openairdocs.org/sdr/FDEA202107251892.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT FLOOR PANEL #251UH WAS FOUND EDGE DAMAGED.
- [SDR FDEA202107251891](https://openairdocs.org/sdr/FDEA202107251891.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT FLOOR PANEL #241PH WAS FOUND INSERT DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107251890](https://openairdocs.org/sdr/FDEA202107251890.md): Floor Panel · damaged · Jul 25, 2021 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT FLOOR PANEL #241RJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107181844](https://openairdocs.org/sdr/FDEA202107181844.md): Rudder · delaminated · Jul 18, 2021 · N653FE · Airbus A300F4605R · Rudder Structure
  > 1EA WATER TRAPPED AREA (90MMX100MM) WAS FOUND AT RH RUDDER HOISTING POINT 2. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 25, FIG. 225A, P. 343-362 AND SRI 55-41-12-201, IIR 55-41-12-2-008-00, 3H.
- [SDR FDEA202105131213](https://openairdocs.org/sdr/FDEA202105131213.md): Servo Valve · malfunctioned · May 13, 2021 · N653FE · Airbus A300F4605R · Landing Gear Brake System
  > NR 2 BRAKE DID NOT RELEASE AFTER LANDING ROLLOUT. #2 TEMP REACHED MAX OF 370 DEGREES. PER MOCC THE #2 (13GG) SERVOVALVE IS REQUIRED TO BE CHANGED. REMOVED THE #2 (13GG) SERVOVALVE IAW AMM 32-42-48-04. INSTALLED THE #2 (13GG) SERVO VALVE DOWN TO AMM 32-42-
- [SDR FDEA201912043171](https://openairdocs.org/sdr/FDEA201912043171.md): Indicator · failed · Dec 4, 2019 · N653FE · Airbus A300F4605R · Door Warning System
  > R1 DOOR WILL NOT ARM.. RELEASED FOR SERVICE PER MEL: 52-XX-XX CATEGORY: C EXPIRATION: MM-DD-YY "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR ( R1) _____ DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPA
- [SDR FDEA2019093082370](https://openairdocs.org/sdr/FDEA2019093082370.md): Tachometer · malfunctioned · Sep 28, 2019 · N653FE · Airbus A300F4605R · Landing Gear Brake System
  > NR 5 BRAKE INDICATED ON DURING TAXI DRIFTED LEFT. THEN OFF, ATTEMPTED T/O AND HAD SAME INDICATION @80 KTS. CONDUCTED RTO AND RETURNED TO RAMP. TSI 2779 COMPLETED AND PROBLEM CORRECTED IN ASSOCIATED TSI ACTION IAW AMM 32-42-57-00, MAIN TACHOMETER REPLACE
- [SDR FDEA201902286505](https://openairdocs.org/sdr/FDEA201902286505.md): Bracket · chafed · Feb 26, 2019 · N653FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > MCD FR24 CHAFFED BETWEEN S-12R AND S-13R REMOVED AND REPLACED 1EA BRACKET AND 1EA SPLICE AT FR24 RH SIDE ON MCD IAW SRM 51-40-21 MAJOR REPAIR
- [SDR FDEA201902250502](https://openairdocs.org/sdr/FDEA201902250502.md): Floor Panel · delaminated · Feb 25, 2019 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > PANEL 162DF WAS FOUND DELAMINATED AFTER REMOVAL FOR FOM FABRICATED NEW PANEL 162DF IAW SRZ-25-005 AND TRAVELER T19/1395153 MAJOR REPAIR
- [SDR FDEA201902250501](https://openairdocs.org/sdr/FDEA201902250501.md): Floor Panel · damaged · Feb 25, 2019 · N653FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 162CF WAS FOUND DAMAGED AFTER REMOVAL FOR FOM 162CF FABRICATED NEW PANEL IAW SRZ-25-005 AND TRAVELER T19/1395152 MAJOR REPAIR
- [SDR FDEA201902210475](https://openairdocs.org/sdr/FDEA201902210475.md): Seat Track · damaged · Feb 21, 2019 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FR63 RT OUTBD Y-2462 SEAT TRACK LOBE MISSING. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.
- [SDR FDEA201902210474](https://openairdocs.org/sdr/FDEA201902210474.md): Seat Track · cracked · Feb 21, 2019 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN SEAT TRACK LBL 1456 WORN AND GOUGED FR57.1 TO FR60. UPON FURTHER INVESTIGATION SEAT TRACK FOUND TO BE CRACKED. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201. MAJOR REPAIR.
- [SDR FDEA201902210469](https://openairdocs.org/sdr/FDEA201902210469.md): Adapter · damaged · Feb 21, 2019 · N653FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > MCD ADAPTER FR 57.3 LT HAS DAMAGED LOBE FABRICATED NEW ADAPTER ON T19/1396201. REMOVED AND REPLACED MDCC ADAPTER AT FR57.3 LT IAW SRM 51-40-21, Y1456 TO Y1959 CLASSIFIED AS A CAT"A" MAJOR REPAIR.
- [SDR FDEA201902170440](https://openairdocs.org/sdr/FDEA201902170440.md): Closeout Panel · damaged · Feb 17, 2019 · N653FE · Airbus A300F4605R · Engine Thrust Reverser
  > FOUND PANEL PULLED LOSE AND CRACKED ON LT ENGINE, I/B THRUST REVERSER AT APPROX THE 6 O'CLOCK POSITION. REMOVED DAMAGED PANEL ON NR 1 ENG THRUST REVERSER AT 6 O'CLOCK POS REF SRM 51-40-20. PART REPLACEMENT WAS ACCOMPLISHED ON EA 6-530-TO343829 PART 2 WRI 543
- [SDR FDEA201902160434](https://openairdocs.org/sdr/FDEA201902160434.md): Seat Track · corroded · Feb 16, 2019 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN FR69 AND FR72 Y-953 SEAT TRACK HAS CORROSION BLEND OUT AREA ON SEAT TRACK AT BETWEEN FR69 TO FR72 Y-953 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK BETWEEN FR69 TO FR72 Y- 953 IAW SRM 53-40-21 MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N653FE/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 = 'N653FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N653FE/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.