# Service difficulty reports: N671FE

A list on [N671FE](https://openairdocs.org/aircraft/N671FE.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 4 · 189 reports

- [SDR FDEA202410091666](https://openairdocs.org/sdr/FDEA202410091666.md): Fitting · cracked · Oct 9, 2024 · N671FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REMOVE MAIN CARGO DOOR ACTUATOR YOKE FOUND FR23 FRAME FITTING CRACK. I.A.W A300-600 AMM 52-36-27-04 REPLACED MAIN CARGO DOOR ACTUATOR YOKE AT FR23, LONGN 1~3 & FEDEX EO NO: E6-5230-E0378588 A P5, SEQ NO:1229, TITLE: DOORS- CARGO DOOR/HYD SYS- DETAILED VISU
- [SDR FDEA202410091633](https://openairdocs.org/sdr/FDEA202410091633.md): Seat Track · unknown · Oct 9, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING SPLICE REPAIR FOUND ON MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 52~53, -Y956, EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA. DUE TO NO LEGACY DOCUMENTATION SUPPORTING THIS EXISTING REPAIR
- [SDR FDEA202410041586](https://openairdocs.org/sdr/FDEA202410041586.md): Seat Track · corroded · Oct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE FOUND SEAT TRACK CORROSION AT FR15A 2" AND Y953 AREA REPLACED THE DAMAGE SEAT TRACK WITH NEW ONE AT MAIN DECK FLOOR STRUCTURE FR15A PLUS 2" AND Y953 AREA I.A.W A300-600F SRM 51-72-10-00, PAGE 2 & 51-40-21-001, PARA.6 PAGE 7B- PAG
- [SDR FDEA202410041585](https://openairdocs.org/sdr/FDEA202410041585.md): Plate · bent · Oct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > TAIL FUSELAGE INTERNAL FOUND 2EA SUPPORT AND WEB GOT DEFORM AT FR86-87 S33R AND S39R REPLACED THE DEFORM STRAPS AND WEBPLATE WITH NEW PARTS ON TAIL FUSELAGE BETWEEN FR86 TO FR87, S-33R AND S-39R I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40- 21-001,
- [SDR FDEA202410041470](https://openairdocs.org/sdr/FDEA202410041470.md): Crossbeam · corroded · Oct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE FOUND CROSSBEAM CORROSION AT FR47 AND Y370 AREA. REMOVED CORROSION CROSSBEAM AND INSTALLED NEW CROSSBEAM I.A.W A300-600F SRM 51- 72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT
- [SDR FDEA202410021661](https://openairdocs.org/sdr/FDEA202410021661.md): Skin · gouged · Oct 2, 2024 · N671FE · Airbus A300F4605R · Spoilers
  > LH WING SPOILER #3 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #3 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381100 P1, SEQ NO:1248, TITLE:WINGS-FLIGHT SURFACES-LH #3 SPOILER-OUTER HINGE ARMS
- [SDR FDEA202410021659](https://openairdocs.org/sdr/FDEA202410021659.md): Skin · gouged · Oct 2, 2024 · N671FE · Airbus A300F4605R · Spoilers
  > RH WING SPOILER #4 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPR SURFACE FOUND 4EA NICKS ACCOMPLISHED THE EDGE BAND REPAIR AT RH #4 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381096 P1, SEQ NO:1247, TITLE:WINGS-FLIGHT SURFACES-RH #4 SPOILER-OUTER
- [SDR FDEA202410021658](https://openairdocs.org/sdr/FDEA202410021658.md): Skin · gouged · Oct 2, 2024 · N671FE · Airbus A300F4605R · Spoilers
  > LH WING SPOILER #7 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #7 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381092 P1, SEQ NO:1246, TITLE:WINGS-FLIGHT SURFACES-LH #7 SPOILER-OUTER HINGE ARMS
- [SDR FDEA202410021656](https://openairdocs.org/sdr/FDEA202410021656.md): Skin · gouged · Oct 2, 2024 · N671FE · Airbus A300F4605R · Spoilers
  > LH WING SPOILER #6 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #6 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO: T6-5750-T0381085 P1, SEQ NO:1245, TITLE: WINGS-FLIGHT SURFACES-LH #6 SPOILER-OUTER HINGE AR
- [SDR FDEA202409301494](https://openairdocs.org/sdr/FDEA202409301494.md): Crossbeam · broken · Sep 30, 2024 · N671FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE FOUND FR61 CROSS BEAM CROWN BROKEN BETWEEN Y1456 AND Y1959 AREA REPLACED THE CROSS BEAM ADAPTER OF THE MAIN DECK CARGO FLOOR STRUCTURE AT FR 61 BETWEEN Y1456 AND Y1959 AREA. I.A.W A300-600F SRM 51-72-10-001, PAGE 2. THIS REPAIR IS
- [SDR FDEA202409291662](https://openairdocs.org/sdr/FDEA202409291662.md): Shear Web · cracked · Sep 29, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH CHORD CRACK AT FR38 POSITION UNDER FLOOR PANEL (RBL59) REPLACED THE DAMAGED SHEAR WEB WITH NEW PART AT FWD CARGO COMPARTMENT BETWEEN FR38~38.1, S-44R. I.A.W A300-600F SRM 51-72-10-001, PAGE.2. THIS REPAIR IS CLASSIFIED AS CAT.A MINOR PER
- [SDR FDEA202409271469](https://openairdocs.org/sdr/FDEA202409271469.md): Support Bracket · damaged · Sep 27, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > LOWER BEACON LIGHT POWER SUPPLY UNIT 4LV WIRE BUNDLE 1EA SUPPORT BRACKET BROKEN AT AFTER CARGO UNDER FLOOR PANEL 162DF REPLACED BROKEN SUPPORT BRACKET WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE 2 & 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIF
- [SDR FDEA202409261468](https://openairdocs.org/sdr/FDEA202409261468.md): Profile · cracked · Sep 26, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE FOUND T-PROFILE CRACK AT FR80/82,-Y1580 AREA. REMOVED CRACK T-PROFILE AND INSTALLED NEW T-PROFILE I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DE
- [SDR FDEA202409251657](https://openairdocs.org/sdr/FDEA202409251657.md): Spar · worn · Sep 25, 2024 · N671FE · Airbus A300F4605R · Spoilers
  > RH WING NR 2 SPOILER O/B SIDE FWD SKIN WORN CUT OUT THE DAMAGE AREA AND INSTALLED REPAIR PARTS AT RH #2 SPOILER FWD OF RIB 18 IAW EA NO:T6-5750-T0381047 P1, SEQ NO:1251, TITLE:WING-FLIGHT SURFACES-RH NR 2 SPOILER-WEAR DAMAGE AT OUTBOARD FACE OF FRONT SPAR AT R
- [SDR FDEA202409251631](https://openairdocs.org/sdr/FDEA202409251631.md): Seat Track · damaged · Sep 25, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DACK FLOOR STRUCTURAL FOUND SEAT TRACK CROWN BROKEN AT FR63 AND -Y2400 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR62~FR64 PLUS 10.5" I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CL
- [SDR FDEA202409251592](https://openairdocs.org/sdr/FDEA202409251592.md): Seat Track · damaged · Sep 25, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DACK FLOOR STRUCTURAL FOUND SEAT TRACK CROWN BROKEN AT FR63 AND -Y2400 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR62~FR64 PLUS 10.5" I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203 ~ 208. THIS REPAIR
- [SDR FDEA202409231660](https://openairdocs.org/sdr/FDEA202409231660.md): Rib · gouged · Sep 23, 2024 · N671FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > LH WING LE CAVITY RIB GOUGE ABOVE ANTI-ICE DUCT AT WOFX -259.4 NEAR KRUEGER FLAP. TRIMMED OUT THE DAMAGE AREA AND INSTALLED THE REPAIR ANGLE AT LH WING LE CAVITY RIB WOFX259.4 I.A.W FEDEX EA NO:T6-5710-T0380996 P1, SEQ NO:1243, TITLE:WING-BASIC WING STRUCT
- [SDR FDEA202409231630](https://openairdocs.org/sdr/FDEA202409231630.md): Seat Track · cracked · Sep 23, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DACK FLOOR STRUCTURE FOUND Y1456 SEAT TRACK CRACK AT FR 57.2 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57.1 PLUS 10"~FR58 PLUS 10", Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPA
- [SDR FDEA202409231591](https://openairdocs.org/sdr/FDEA202409231591.md): Seat Track · cracked · Sep 23, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DACK FLOOR STRUCTURE FOUND Y1456 SEAT TRACK CRACK AT FR 57.2 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57.1 PLUS 10"~FR58 PLUS 10", Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS RE
- [SDR FDEA202409201353](https://openairdocs.org/sdr/FDEA202409201353.md): Skin · no discrepancy · Sep 20, 2024 · N671FE · Airbus A300F4605R · Elevator, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER5-12", T/E-22.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202409201665](https://openairdocs.org/sdr/FDEA202409201665.md): Repair · none · Sep 20, 2024 · N671FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING FLUSH DOUBLER REPAIR FOUND ON LH CTR FLAP NOSE SKIN BTW RIB 23~24 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202409201636](https://openairdocs.org/sdr/FDEA202409201636.md): Skin · no discrepancy · Sep 20, 2024 · N671FE · Airbus A300F4605R · Trailing Edge Flaps
  > 00089009N00135 AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 14~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING R
- [SDR FDEA202408061088](https://openairdocs.org/sdr/FDEA202408061088.md): Transmitter · failed · Aug 6, 2024 · N671FE · Airbus A300F4605R · Hydraulic System, Main
  > ENROUTE TO MEM GOT A GREEN HYDRAULIC SYSTEM LOW LEVEL. PER ECAM TURNED OFF GREEN HYDRAULIC PUMPS. DECLARED AN EMERGENCY AND RECOVERED TO MEMPHIS. LOWERED THE GEAR VIA EMERGENCY EXTENSION AND LANDED STRAIGHT AHEAD ON 36C. UPON LANDING, HYDRAULIC QUANTITY S
- [SDR FDEA202403010225](https://openairdocs.org/sdr/FDEA202403010225.md): Feel Unit · faulted · Mar 1, 2024 · N671FE · Airbus A300F4605R · Elevator Control System
  > ON LANDING AIRCRAFT ELEVATOR CONTROLS ARE VERY HEAVY TO PULL AFT. CONTROL WILL NOT RETURN TO NEUTRAL POSITION WITHOUT PUSHING IT INTO PLACE ON GROUND. INSTALLED PUSH-PULL TOOL ON PILOT'S YOKE AND CHECKED ELEVATOR OPS LOAD PER A300-600 AMM 27-33-00-05
- [SDR FDEA202312051925](https://openairdocs.org/sdr/FDEA202312051925.md): Switch · inoperative · Dec 5, 2023 · N671FE · Airbus A300* · Emergency Lighting
  > FOUND DOOR INTERIOR EMERGENCY EXIT LIGHTS ALWAYS ILLUMINATED. NOTICED RED EMERGENCY LIGHT SWITCH FWD OF L1 DOOR IS STUCK INSIDE. RELEASED FOR SERVICE PER MEL: 33-XX-XX-XX CAT: C EXP: 15DEC23 "MEL 33-XX-XX-XX: COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS
- [SDR FDEA202306211077](https://openairdocs.org/sdr/FDEA202306211077.md): Psu · failed · Jun 21, 2023 · N671FE · Airbus A300* · Emergency Equipment
  > ON PRE-DEPARTURE CHECK FOUND THAT COUIER COMPARTMENT INTERIOR EMERGENCY EXIT LIGHTS ARE INOP, WILL NOT TEST. RELEASED FOR SERVICE PER MEL: 33-XX. INSTALLED NEW BATTERY, NO HELP. REINSTALLED ORIGIONAL BATTERY. A300 AMM 33-XX. RELAMPED PER IPC. NO HELP. P
- [SDR FDEA202302040234](https://openairdocs.org/sdr/FDEA202302040234.md): Transformer · failed · Feb 4, 2023 · N671FE · Airbus A300* · APU Start/Ignition System
  > WHILE ATTEMPTING TO START APU, GOT AN APU FAULT, THEN ELECTRICAL FUMES AND SMOKE IN COCKPIT PULLED APU/ START C/B. OPEN FRONT PANEL OFF OF 120 VU, INSPECTED WIRING, AND APU START CONTACTOR 5KA, APPEARS TO BE IN GOOD SHAPE, NO DAMAGE, 50 AMP BREAKER 10XH PO
- [SDR FDEA202205171405](https://openairdocs.org/sdr/FDEA202205171405.md): None · damaged · May 17, 2022 · N671FE · Airbus A300* · Rudder Structure
  > STABILIZER - RUDDER RH PANEL FOUND WATER INGRESS AROUND FASTENER #36, #37, #38 AND #39 COMPLIED WITH FEDEX EA: 6-5540-T0332902 A PT3, EA TITLE: STABILIZERS - RUDDER - RH - WATER INGRESS - AIRBUS SERVICE BULLETIN A300-55-6050 INSPECTIONS/EO 6-5540- E031936
- [SDR FDEA202205161404](https://openairdocs.org/sdr/FDEA202205161404.md): None · cracked · May 16, 2022 · N671FE · Airbus A300* · Passenger/Crew Doors
  > RH FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK COMPLIED WITH FEDEX EA: 6-5210-T0368735 PT1, EA TITLE: DOORS - PASSENGER/CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR - RSC TRACKING. REPAIRED RH FWD PAX DOOR - FRAME SEGMENT
- [SDR FDEA202205161395](https://openairdocs.org/sdr/FDEA202205161395.md): Seat Track · cracked · May 16, 2022 · N671FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE - SEAT TRACK CRACKED, BETWEEN FR20 AND FR21, Y1959 COMPLIED WITH FEDEX EA: 6-5310-T0368594 PT1, EA TITLE: FUSELAGE - MAINFRAME - MCD Y1959 SEAT TRACK BENT AND CRACKED BETWEEN FR20 AND FR21 - REPAIR. REPA
- [SDR FDEA202107241856](https://openairdocs.org/sdr/FDEA202107241856.md): Power Supply · no test · Jul 24, 2021 · N671FE · Airbus A300F4605R · Emergency Lighting
  > EMERGENCY LIGHTS PUSH TO TEST SWITCH IN COURIER AREA DOES NOT ILLUMINATE DURING TEST. DURING LIGHTING TEST, ALSO NOTED RED LED ON FRONT FACE OF POWER SUPPLY UNIT (29WL1) WAS ILLUMINATED.REMOVED AND REPLACED POWER SUPPLY UNIT (29WL1) REF AMM 33-51-14-04. OP
- [SDR FDEA202104080854](https://openairdocs.org/sdr/FDEA202104080854.md): Pawl · out of alignment · Apr 8, 2021 · N671FE · Airbus A300F4605R · Passenger/Crew Doors
  > L1 DOOR ESCAPE SLIDE HANDLE DIFFICULT TO DISARM HANDLE STIFF AND WE COULDN'T MOVE IT FAR ENOUGH INTO THE DISARM POSITION TO PIN IT.. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CATEGORY: C EXP "MEL 52-XX-XX-XX: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLI
- [SDR FDEA202104060831](https://openairdocs.org/sdr/FDEA202104060831.md): Hose · worn · Apr 6, 2021 · N671FE · Airbus A300F4605R · Hydraulic System, Main
  > LOST GREEN HYDRAULIC SYSTEM PASSING THROUGH FL290. FLUID LEVEL DECREASED TO RED DOT ALMOST IMMEDIATELY. LEVELED A\C AT FL330, SLOWED TO GREEN DOT. COMPLIED WITH QRH. DESCENDED TO FL310 AND MAINTAINED.65 MACH. CONTINUED TO MEMPHIS, EMERGENCY DECLARED
- [SDR FDEA202012203192](https://openairdocs.org/sdr/FDEA202012203192.md): Mount · cracked · Dec 20, 2020 · N671FE · Airbus A300F4605R · Leading Edge Devices
  > ON SLAT EXTENSION ON APPROACH GOT ECAM "KREUGER NOT EXTENDED" REMAINED NOT EXTENDED THROUGH LANDING. ON POSTFLIGHT WALKAROUND FOUND LEFT KRUEGER FLAP VANE OUTBOARD BRACKET MOUNT CRACKED AND INBOARD BRACKET BROKEN. REMOVED KRUEGER FLAP MOVEABLE VANE, PER MM
- [SDR FDEA2020040370586](https://openairdocs.org/sdr/FDEA2020040370586.md): Indication Sys · malfunctioned · Mar 17, 2020 · N671FE · Airbus A300F4605R · Door Warning System
  > PDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR
- [SDR FDEA2020031970586](https://openairdocs.org/sdr/FDEA2020031970586.md): Indication Sys · inoperative · Mar 17, 2020 · N671FE · Airbus A300F4605R · Door Warning System
  > PDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR
- [SDR FDEA2019111532941](https://openairdocs.org/sdr/FDEA2019111532941.md): Skin · cracked · Nov 13, 2019 · N671FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE NDT HFEC INSPECTION FOUND CRACK SIGNAL. FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE CRACK. COMPLIED WITH FEDEX EA:6-5710-T0350731 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MI
- [SDR FDEA201911082907](https://openairdocs.org/sdr/FDEA201911082907.md): Crossbeam · cracked · Nov 8, 2019 · N671FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDC FLOOR - FR64 Y-1456 - Y-1959, CROSSBEAM CRACKED APPROX 0.5 INCH IN LENGTH. MDC FLOOR FR64 B/W Y-1456 AND Y-1959 CROSSBEAM CRACKED APPROX 0.5 INCH. REPAIRED THE CRACKED CROSSBEAM PER A300-600F SRM53-10-15 FIGURE211. THIS REPAIR CATEGORY IS A. MAJO
- [SDR FDEA201911082906](https://openairdocs.org/sdr/FDEA201911082906.md): Rib · cracked · Nov 8, 2019 · N671FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING - MID FLAP RIB21 AFT AREA FOUND CRACK ON X-RAY INSPECTION. RH WING - MID FLAP RIB21 UPPER FLANGE CRACK BETWEEN STGR2.7 AND STGR2.8. REPAIRED THE CRACKED RIB FLANGE PER A300-600F SRM57-50-00-201 FIG.201. TRACKING EA:6-5750-T0350993 HAS BEEN ISSUED
- [SDR FDEA201705101390](https://openairdocs.org/sdr/FDEA201705101390.md): Skin · gouged · May 10, 2017 · N671FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. ACCOMPLISHED EA 6-5750-T0333072, PART 1. MAJOR REPAIR.
- [SDR FDEA201705101388](https://openairdocs.org/sdr/FDEA201705101388.md): Skin · gouged · May 10, 2017 · N671FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. REPAIRED THE FLAP UPPER SURFACE IAW EA 6-5750-T0332914, PART 1. MAJOR REPAIR.
- [SDR FDEA201705061364](https://openairdocs.org/sdr/FDEA201705061364.md): Seat Track · corroded · May 6, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION AT Y0 BETWEEN FRAMES 33 AND 34. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16, 51-4-21, AND SRM 51-40-44. MAJOR REPAIR.
- [SDR FDEA201705061363](https://openairdocs.org/sdr/FDEA201705061363.md): Seat Track · worn · May 6, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS HEAVILY WORN IN MAIN CABIN JUST AFT OF FRAME 78, Y852. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-10-16. MAJOR REPAIR.
- [SDR FDEA201705041356](https://openairdocs.org/sdr/FDEA201705041356.md): Floor Panel · broken · May 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 251VF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.
- [SDR FDEA201705041355](https://openairdocs.org/sdr/FDEA201705041355.md): Floorboard · dented · May 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241TH HAS SEVERAL DENTS AND MISSING EDGE FILLER. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.
- [SDR FDEA201705041354](https://openairdocs.org/sdr/FDEA201705041354.md): Floor Panel · delaminated · May 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 161AF HAS DELAMINATION ON BOTTOM SIDE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005, REV M. MAJOR REPAIR
- [SDR FDEA201704301336](https://openairdocs.org/sdr/FDEA201704301336.md): Support · cracked · Apr 30, 2017 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN CABIN SUPPORT WEB IS CRACKED AT FRAME 45. REMOVED AND REPLACED THE SUPPORT WEB IAW SRM 51-40-21 AND SRM 51-40-44. MAJOR REPAIR
- [SDR FDEA201704291296](https://openairdocs.org/sdr/FDEA201704291296.md): Seat Track · corroded · Apr 29, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 54.1 -Y1959. REMOVED AND REPLACED MAIN CABIN SEAT TRACK BETWEEN FR 54.1 -Y1959 IAW SRM 51-40- 21. THIS IS A MAJOR REPAIR.
- [SDR FDEA201704271284](https://openairdocs.org/sdr/FDEA201704271284.md): Floor Panel · cracked · Apr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241DF HAS IMPACT DAMAGE. FABRICATED MAIN CABIN FLOOR PANEL 241DF REF 70013348480001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.
- [SDR FDEA201704271283](https://openairdocs.org/sdr/FDEA201704271283.md): Floor Panel · dented · Apr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242UJ HAS SEVERAL DENTS. FABRICATED MAIN CABIN FLOOR PANEL 242UJ REF 70013348500001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N671FE/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 = 'N671FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N671FE/reports

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