# Service difficulty reports: N651FE

A list on [N651FE](https://openairdocs.org/aircraft/N651FE.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 9 · 421 reports

- [SDR FDEA202412101647](https://openairdocs.org/sdr/FDEA202412101647.md): Control Unit · failed · Oct 13, 2024 · N651FE · Airbus A300F4605R · Door Warning System
  > DURING OPS CHECK OF 71WN FOUND THE AUTONOMOUS STANDBY UNIT FAILED OPS CHECK. REMOVED AND REPLACED AUTONOMOUS STANDBY UNIT. OPS CHECK GOOD.
- [SDR FDEA202408151129](https://openairdocs.org/sdr/FDEA202408151129.md): Connector · damaged · Aug 15, 2024 · N651FE · Airbus A300F4605R · Light System Wiring
  > R1 CEILING EMERGENCY LIGHT INOP. AMM: 33-51-00-05 WDM: 33-51-04 CLEANED AND RECECURED PLUG CONNETION 5824VC AND PERFORMED EMERGENCY LIGHT OPS TEST REF ABOVE REF, EMERGENCY LIGHTING NOW OPS CHECK NORMAL. PLACARD REMOVED. IDENTIFIED ITEM AS AN SDR, N
- [SDR FDEA202408151128](https://openairdocs.org/sdr/FDEA202408151128.md): Power Supply · failed · Aug 15, 2024 · N651FE · Airbus A300F4605R · Emergency Lighting
  > WHEN A/C WAS BOARDED, L1 AND R1 EMERGENCY EXIT SIGNS WERE ILLUMINATED WITH BOTH COCKPIT EMERGENCY SWITCH AND COURIER EMERGENCY SWITCH IN THE OFF POSITION. R/I 06JUL24 11:13 BWI REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 3214-41 POS: ONL
- [SDR FDEA202404300533](https://openairdocs.org/sdr/FDEA202404300533.md): Pitot Tube · blocked · Apr 30, 2024 · N651FE · Airbus A300F4605R · Pitot/Static System
  > IN CRUISE AT FL340,.80M (279 IAS) ABOUT 40 MINUTES INTO THE FLIGHT, RECEIVED FO IAS DISCREPANCY ECAM. HIS STANDBY AIRSPEED INDICATOR REMAINED AT 279-280 BUT HIS PFD SPEED TAPE WENT TO 220 KTS AND VERY SLOWLY CREEPED BACK UP TO 279-280. TOOK ABOUT TWO MIN
- [SDR FDEA202404260534](https://openairdocs.org/sdr/FDEA202404260534.md): Indicator · malfunctioned · Apr 26, 2024 · N651FE · Airbus A300F4605R · Airspeed/Mach Indicator
  > AFTER TURBULENCE AND ICING ENCOUNTER, FL360 ADC 2 AIRSPEED INDICATION DROPPED TO 60KTS. FO STANDBY, CAPT STANDBY AND ADC 1 SHOWED CORRECT INDICATION. FOLLOWED QRH PROCEDURE. AMM: 34-10-00-05, AMM: 22-40-00-05 PERFORMED BITE CHECK ON #2 ADC, TEST OK, AIRSPE
- [SDR FDEA202404230535](https://openairdocs.org/sdr/FDEA202404230535.md): Adc · failed · Apr 23, 2024 · N651FE · Airbus A300F4605R · Altimeter, Barometric/Encoder
  > AT FL350,.78 MACH, ABOUT 1 HOUR INTO FLIGHT, FO SPEED TAPE BEGAN ROLLING BACK FOLLOWED BY IAS DISCREPANCY ECAM ALERT. FOLLOWED ECAM AND QRH SWITCHING TO SYS 1 ADC ON FO SIDE. SUSPECT ADC2 FAILURE. R & R NO.2 ADC, PERFORMED SATISFACTORY ADS2 BITE TEST. COMP
- [SDR FDEA202403280390](https://openairdocs.org/sdr/FDEA202403280390.md): Seat Track · broken · Mar 28, 2024 · N651FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOBES BROKEN UNDER LOCK POSITION MG0828. NO FLOOR PANEL DAMAGE AND NO SEAT TRACK CRACKS. FABRICATED, LOCATED, AND MATCH-DRILLED NEW SEAT TRACK SECTION AND SPLICE FITTINGS IAW SRM FIG. 201. INSTALLED THE SEAT TRACK AND REPAIR IAW SRM 53-10-16.
- [SDR FDEA202312220068](https://openairdocs.org/sdr/FDEA202312220068.md): Fitting · corroded · Dec 22, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach Section
  > LH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON AFT SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425
- [SDR FDEA202312220067](https://openairdocs.org/sdr/FDEA202312220067.md): Fitting · corroded · Dec 22, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach Section
  > LH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON FWD SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425
- [SDR FDEA202312200066](https://openairdocs.org/sdr/FDEA202312200066.md): Fitting · corroded · Dec 20, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach Section
  > L/H MLG AFT PINTLE FWD LUG HAS SIGN OF CORROSION. REPAIRED PER AIRBUS INSTRUCTIONS R57240425
- [SDR FDEA202303210563](https://openairdocs.org/sdr/FDEA202303210563.md): Skin · unknown · Mar 21, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202303210562](https://openairdocs.org/sdr/FDEA202303210562.md): Skin · unknown · Mar 21, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202303210561](https://openairdocs.org/sdr/FDEA202303210561.md): Skin · unknown · Mar 21, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW RIB 1C~5,STGR 2.1~2.2. COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202303150622](https://openairdocs.org/sdr/FDEA202303150622.md): Skin · unknown · Mar 15, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > EXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-8.5" POSITION, BTW RIB 22~24, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED
- [SDR FDEA202303150621](https://openairdocs.org/sdr/FDEA202303150621.md): Skin · unknown · Mar 15, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > EXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-11.5" POSITION, BTW RIB 8~9, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED
- [SDR FDEA202303090400](https://openairdocs.org/sdr/FDEA202303090400.md): Seat Track · worn · Mar 9, 2023 · N651FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16 PARA 5A FIG.201 P201-P210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202303080646](https://openairdocs.org/sdr/FDEA202303080646.md): Spoiler · delaminated · Mar 8, 2023 · N651FE · Airbus A300* · Wing Structure
  > LH WING #6 SPOILER L/E CTR SECTION DELAMINATED. REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"
- [SDR FDEA202303080626](https://openairdocs.org/sdr/FDEA202303080626.md): Skin · delaminated · Mar 8, 2023 · N651FE · Airbus A300* · Wing Structure
  > LH WING #6 SPOILER L/E CTR SECTION DELAMINATED REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"
- [SDR FDEA202303070645](https://openairdocs.org/sdr/FDEA202303070645.md): Slat · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > AGING AIRCRAFT ASSESSMENT: EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITL
- [SDR FDEA202303070644](https://openairdocs.org/sdr/FDEA202303070644.md): Spoiler · delaminated · Mar 7, 2023 · N651FE · Airbus A300* · Wing Structure
  > 1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN. REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206.
- [SDR FDEA202303070631](https://openairdocs.org/sdr/FDEA202303070631.md): Skin · none · Mar 7, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-R
- [SDR FDEA202303070625](https://openairdocs.org/sdr/FDEA202303070625.md): Skin · delaminated · Mar 7, 2023 · N651FE · Airbus A300* · Wing Structure
  > 1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206.
- [SDR FDEA202303070544](https://openairdocs.org/sdr/FDEA202303070544.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00119 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~32, -Y1456 FOUND THE EXISTING SPLICE REPAIR UPPER FLANGE NOT COMPLIANCE WITH APPROVED DATA: A300-600F SRM 53-10-16-201, FIG.201, REMOVED HILOKS AND PERFORMED ROTOT
- [SDR FDEA202303070493](https://openairdocs.org/sdr/FDEA202303070493.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00125 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 69~70, Y450 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 FDEA202303070492](https://openairdocs.org/sdr/FDEA202303070492.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00124 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -Y450 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 FDEA202303070491](https://openairdocs.org/sdr/FDEA202303070491.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00123 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -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 1
- [SDR FDEA202303070490](https://openairdocs.org/sdr/FDEA202303070490.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00122 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 65~69, 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 121.7
- [SDR FDEA202303070489](https://openairdocs.org/sdr/FDEA202303070489.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00121 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~63, -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 12
- [SDR FDEA202303070488](https://openairdocs.org/sdr/FDEA202303070488.md): Seat Track · unknown · Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, Structure
  > N00120 AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 55~56, -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 12
- [SDR FDEA202303030483](https://openairdocs.org/sdr/FDEA202303030483.md): Aileron · damaged · Mar 3, 2023 · N651FE · Airbus A300* · Wing, Control Surfaces
  > LH WING AILERON UPPER SKIN DEFORMED AT RIB1 & REAR SPAR-17" ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-61-11-201, PARA.4D, PAGE.213-PAGE.216, FIG.204 MAJOR REPAIR
- [SDR FDEA202303020596](https://openairdocs.org/sdr/FDEA202303020596.md): Skin · damaged · Mar 2, 2023 · N651FE · Airbus A300* · Fuselage Main, Plate/Skin
  > EVALUATE PREVIOUS DENT AT LHS FUSELAGE LWR SKIN FR10 6", 8 O'CLOCK. ACCOMPLISHED THECAT B DOUBLER REPAIR IAW A300-600F SRM 53-12-12-201, CONFIG 2, PAR. 5A, PAGE 203-208, FIG.201 & SRI 53-12-12-201, IR 53-12-12-2-006-00, PARA. 3F, TABLE 207 "MAJOR REPAIR".
- [SDR FDEA202204180988](https://openairdocs.org/sdr/FDEA202204180988.md): Control Module · unknown · Apr 18, 2022 · N651FE · Airbus A300* · Detection System
  > MDIS 651 26-10 5623 18APR22 IND OPEN U #1 ENGINE AGENT #2 SQUIB INOP SHGN 18APR22 15:25 IND U WHEN TESTING #1 ENG SQUIB, AGENT 2 SQUIB LIGHT IS NOT ILLUMINATING. SQUIB LIGHT ILLUMINATES W/ ANNUN LT TEST. PER A300-600 TSM 26-21-00, FIG 11
- [SDR FDEA202203180745](https://openairdocs.org/sdr/FDEA202203180745.md): Light · inoperative · Mar 18, 2022 · N651FE · Airbus A300F4605R · Emergency Lighting
  > MDIS 651 33-50 5547 18MAR22 LRD FACT U LAVATORY AUXILIARY MIRROW EMERGENCY LIGHT OUT. FACT 18MAR22 14:45 LRD U RELAMPED LAV AUX MIRROW EMERGENCY, IAW AMM 33-51-21-04, OPS CKS NORMAL AT THIS TIME.
- [SDR FDEA202203150527](https://openairdocs.org/sdr/FDEA202203150527.md): Power Supply · unknown · Mar 15, 2022 · N651FE · Airbus A300* · Cargo/Baggage Doors
  > SLIDE DID NOT DISPLAY ON ECAM WHEN ARMING RIGHT CABIN DOOR. RELEASED FOR SERVICE PER MEL: 52- XX-XX CATEGORY: C EXP: 25MAR22 - (R1) DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." AUTONOMOUS STANDB
- [SDR FDEA202109232384](https://openairdocs.org/sdr/FDEA202109232384.md): Controller · inoperative · Sep 23, 2021 · N651FE · Airbus A300F4605R · Leading Edge Slat Control System
  > AFTER T/O ON SLAT RETRACTION HAD KRUEGER FAULT. RAN APPROPRIATE CHECKLISTS AND RTB. PERFORMED BITE DISPLAY OF BOTH SFCC'S AND FOUND ALL OF THE FAULT BALLS FOR THE NR 1 UNIT LIGHT. THAT FAULT CODE CORRESPONDS WITH BAD SFCC REF AMM 27-80-00. IND INSPECTED
- [SDR FDEA202010032403](https://openairdocs.org/sdr/FDEA202010032403.md): Actuator · failed · Oct 3, 2020 · N651FE · Airbus A300F4605R · Landing Gear Door Retract Section
  > CREW REPORT: DURING MANUAL GEAR EXTENSION GOT LOUD NOISE AND EXCESSIVE VIBRATION ABOVE NORMAL LEVELS. WOULD NOT RECYCLE, REMOVED AND REPLACED NLG DOOR ACTUATOR LT SIDE. REMOVED AND REPLACED NOSE GEAR SEQUENCE VALVE. REMOVED AND REPLACED NON RETURN VALVE.
- [SDR FDEA202008272047](https://openairdocs.org/sdr/FDEA202008272047.md): Pin · missing · Aug 27, 2020 · N651FE · Airbus A300F4605R · Escape Slide
  > MISSING PASSENGER CREW DOOR 831 INFLATE RESERVOIR SAFETY PIN ESCAPE SLIDE RAFT AT FWD GALLEY AREA (1EA). REPLACED PASSENGER CREW DOOR 831 ESCAPE SLIDE RAFT IAW AMM 25-61-21-04 AT FWD GALLEY AREA.
- [SDR FDEA202008171959](https://openairdocs.org/sdr/FDEA202008171959.md): Bolt · corroded · Aug 17, 2020 · N651FE · Airbus A300F4605R · Leading Edge Devices
  > CORROSION BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING (1 EA) REPLACED BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING IAW AMM 27-80-14- 04.
- [SDR FDEA2020081871927](https://openairdocs.org/sdr/FDEA2020081871927.md): Bolt · corroded · Aug 17, 2020 · N651FE · Airbus A300F4605R · Leading Edge Devices
  > ONE CORRODED BOLT ATTACHMENT ON SLAT TRACK NR 7 LOWER POSITION OF THE LT WING. REPLACED THE BOLT IAW AMM 27-80-14-04.
- [SDR FDEA2020009091896](https://openairdocs.org/sdr/FDEA2020009091896.md): Floor Panel · cracked · Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 232VH. THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA). MANUFACTURED FLOOR PANEL 232VH, AS PER DWG SRZ-25-005 REV. R AUG-22-2019. FLOOR PANEL MARKED WITH P/N FX B5327048401400 FDX AUG-11-2020, AS PER GMM 7-0-1
- [SDR FDEA2020082851896](https://openairdocs.org/sdr/FDEA2020082851896.md): Floor Panel · cracked · Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV.R AUG-22-2019 AND FLOOR PANEL MARKED WITH P/N: FX B5327048401400 FDX AUG-11-2020 AS PER GMM 7-0-1001,
- [SDR FDEA2020082051941](https://openairdocs.org/sdr/FDEA2020082051941.md): Floor Panel · delaminated · Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 242LK. REPAIRED THE FLOOR PANEL IAW DWG SRZ 25-005 REV. R.
- [SDR FDEA2020081851896](https://openairdocs.org/sdr/FDEA2020081851896.md): Floor Panel · cracked · Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. THIS NON ROUTINE CARD IS FOR PURPOSE RDR, SDR GENERATION. THIS JOB IS DOCUMENTED
- [SDR FDEA202008071957](https://openairdocs.org/sdr/FDEA202008071957.md): Floor Panel · delaminated · Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231UG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343,
- [SDR FDEA202008071960](https://openairdocs.org/sdr/FDEA202008071960.md): Floor Panel · delaminated · Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231ZG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343, THIS SNRM, (N00653) IS GENERATED RDR PURPOSE
- [SDR FDEA202008071958](https://openairdocs.org/sdr/FDEA202008071958.md): Floor Panel · delaminated · Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231NG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FPR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00543,
- [SDR FDEA2020082071956](https://openairdocs.org/sdr/FDEA2020082071956.md): Floor Panel · delaminated · Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED TOP LAYER FLOOR PANEL (MAIN DECK) 241EF IN PASSENGER CABIN (1 EA) REPAIRED FLOOR PANEL 241EF ON MAIN DECK ASPER A300 SRM 53-10-20 PAGEBLOCK 201 PARA B TOOL USED CALIPER PN 500-197-30 S/N A18135089 DUE DATE JUL-11-2021 SCALE PN CL5000 S/N AE-398
- [SDR FDEA2020082641977](https://openairdocs.org/sdr/FDEA2020082641977.md): Bolt · corroded · Aug 4, 2020 · N651FE · Airbus A300F4605R · Wing Miscellaneous Structure
  > CORROSION BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RT WING. REPLACED BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RY WING IAW AMM 27-80-14-04.
- [SDR FDEA2020082141961](https://openairdocs.org/sdr/FDEA2020082141961.md): Bolt · corroded · Aug 4, 2020 · N651FE · Airbus A300F4605R · Leading Edge Devices
  > CORROSION SLAT 2 SCREWJACK 4 BOLT ON LH WING REPLACED SLAT 2 SCREWJACK BOLT ON LH WING IAW AMM 27-84-22-04 STEP 2.D(5)(A)
- [SDR FDEA2020082041955](https://openairdocs.org/sdr/FDEA2020082041955.md): Bolt · corroded · Aug 4, 2020 · N651FE · Airbus A300F4605R · Leading Edge Devices
  > CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Next page: https://openairdocs.org/aircraft/N651FE/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 = 'N651FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N651FE/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.