# Service difficulty reports: N725FD

A list on [N725FD](https://openairdocs.org/aircraft/N725FD.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 · 220 reports

- [SDR FDEA202607080864](https://openairdocs.org/sdr/FDEA202607080864.md): Warning Buzzer · inoperative · Jul 8, 2026 · N725FD · Airbus A300B4622R · Door Warning System
  > DURING POST-FLIGHT, L1 DOOR SLIDE WARNING BUZZER INOP, WARNING LIGHT OPERATES NORMAL. RELEASED FOR SERVICE PER MEL: 52-73-01-02 CATEGORY C L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZERS INOP. MEL: 52-73-01-02. PERFORMED BITE OF ASPSU (70WN). TEST
- [SDR FDEA202605280641](https://openairdocs.org/sdr/FDEA202605280641.md): Hydraulic Line · leaking · May 28, 2026 · N725FD · Airbus A300B4622R · Hydraulic System, Main
  > CLIMBING THROUGH FL200 COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM. DECLARED AN EMERGENCY AND RETURNED TO MEMPHIS. FOLLOWED QRH PROCEDURES, LANDED UNEVENTFULLY, AND WAS TOWED TO GATE. FOUND FLEX LINE GOING TO LH MANIFOLD-DUAL CONNECTING BLOCK DAMAGED. REMOVED
- [SDR FDEA202602140198](https://openairdocs.org/sdr/FDEA202602140198.md): Safety Wire · wrong part · Feb 14, 2026 · N725FD · Airbus A300B4622R · Escape Slide
  > L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE ATTACHMENT HAS INCORRECT SAFETY WIRE. REQUIRES CAD PLATED COPPER SAFETY WIRE REF FEA 6-2560-F0386375 A P1 STEP 8. FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 RE SAFETIED EJECTOR BAG CABLE ATTACHMENT WITH CAD PLATED CO
- [SDR FDEA202506281072](https://openairdocs.org/sdr/FDEA202506281072.md): Spar · cracked · Jun 28, 2025 · N725FD · Airbus A300B4622R · Wing Spar
  > NDT INSP - RT WING FUEL TANK RIB9 REAR SPAR LOWER BOOM OUTBD HOLE W FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0383952 P1 TO REPAIR RH WING REAR SPAR BOTTOM FLANGE HOLE W/558 BETWEEN RIB9 AND 10 CRACKS. THIS EA DEVIATES FROM EO 6-5710-7-5001.THIS IS A CAT
- [SDR FDEA202506281071](https://openairdocs.org/sdr/FDEA202506281071.md): Fitting · damaged · Jun 28, 2025 · N725FD · Airbus A300B4622R · Cargo/Baggage Doors
  > COMPLY WITH EO 6-5230-E0378588 B P5. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: 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. REPLACED THE MAIN
- [SDR FDEA202506100863](https://openairdocs.org/sdr/FDEA202506100863.md): Stringer · corroded · Jun 10, 2025 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > FWD CARGO FR38.2 - FR39, S44R STRINGER CORRODED. REPAIRED THE CORRODED STRINGER AT FR38.2 - FR39, S44R PER A300-600 SRM53-10-14 & EA:6- 5310-T0383790 P1. TITLE: FUSELAGE - MAINFRAME - STRINGER REPAIR AT STGR44R, FR38.2 - FR39. THIS IS CAT B REPAIR AND MUST
- [SDR FDEA202403280389](https://openairdocs.org/sdr/FDEA202403280389.md): Control Handle · failed · Mar 28, 2024 · N725FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > ON TAKEOFF FROM MEM, WITH LDG GEAR POSDET ON SYS 1, WITH LNDGGEAR HANDLE UP, LANDING GEAR INDICATED 3 GREEN TRIANGLES, 3 RED UNLOCKED LIGHTS AND NO DOOR LIGHTS ILLUMINATED. AFTER SWITCHING TO POSDET 2 AND RAISING THE HANDLE, AFTER SHORT DELAY, THE GEAR RE
- [SDR FDEA202307061183](https://openairdocs.org/sdr/FDEA202307061183.md): Unknown · unknown · Jul 6, 2023 · N725FD · Airbus A300* · Fuselage Main, Plate/Skin
  > AIRCRAFT STRIKE. FUSELAGE DAMAGE AFT OF RADOME. COMPLIED WITH EA # 6-5310-T0375157 PART 1 & 2 FUSELAGE MAINFRAME FRAME 0-FRAME 1/ LOWER FUSELAGE SKIN AT 6 O'CLOCK POSITION STRUCTURALE REPAIR FOR DENT/CREASE TO FRAME AND SKIN.
- [SDR FDEA202303300668](https://openairdocs.org/sdr/FDEA202303300668.md): Crossbeam · corroded · Mar 30, 2023 · N725FD · Airbus A300* · Fuselage Main, Structure
  > IN FWD LOWER CGO COMPT EXFOLIATION CORROSION WAS FOUND AT CROSS BEAM AT FR32 JUNCTION TO ROLLER TRACK -Y1500 ABOVE STGR-43R CUT OUT THE CORROSION BEAM AND FABRICATED THE REPAIR PARTS, WET INSTALLED THE REPAIR PARTS WITH FASTENERS. I.A.W A300-600 SRM 53-10-
- [SDR FDEA202303280781](https://openairdocs.org/sdr/FDEA202303280781.md): Spoiler · worn · Mar 28, 2023 · N725FD · Airbus A300* · Spoilers
  > LH WING ONE ANCHOR NUT ATTACH SKIN ENLARGED AT O/B WEB AREA OF #2 SPOILER FRONT SPAR CAVITY ACCOMPLISHED THE REINFORCEMENT REPAIR, THIS IS CAT.A REPAIR I.A.W FEDEX EA NO:T6-5750- T0373843 P1, SEQ NO:816, TITLE:WING-FLIGHT SURFACES-LH #2 SPOILER-WEAR DAMAGE
- [SDR FDEA202303250707](https://openairdocs.org/sdr/FDEA202303250707.md): Coupling · cracked · Mar 25, 2023 · N725FD · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE FOUND STRINGER COUPLING CRACK AT FR73A STGR26L BELOW FLOOR AREA FABRICATED NEW SECTION AND INSTALLED WITH SEALANT & FASTENERS I.A.W AIRBUS DRAWING:A53980177(SHEET-1) & GMM 7-0-1001 & A300-600 SRM 51-40-21-001, PARA.7, PAGE.24-50
- [SDR FDEA202303240769](https://openairdocs.org/sdr/FDEA202303240769.md): Adapter · worn · Mar 24, 2023 · N725FD · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK - CROSSBEAM FITTED WITH CLS ADAPTER GOT 2EA WORN MARKS AT FR54.1 AND FROM -Y450 TO -Y953 FABRICATED THE ADAPTER PLATE AND WET INSTALLED WITH NEW FASTENERS. I.A.W EA#:T6- 5321-T0373945 P1, TITLE:FUSELAGE-CARGO COMP FLOORS-MAIN DECK CARGO COMPARTMEN
- [SDR FDEA202303240766](https://openairdocs.org/sdr/FDEA202303240766.md): Web · misaligned · Mar 24, 2023 · N725FD · Airbus A300* · Wing Miscellaneous Structure
  > AFTER REMOVED BUSH INSTALLED ON CWB(CENTER WING BOX) FR44 BEAM RH CUTOUT DOUBLER(Y-212), FOUND HOLE ECCENTRICITY DEVIATION REAMED AND INSTALLED THE BUSH TO THE DAMAGE HOLE, INSTALLED WITH NEW FASTENER I.A.W FEDEX EA NO:T6-5710-T0303307 A PART.3, SEQ NO:808
- [SDR FDEA202303200755](https://openairdocs.org/sdr/FDEA202303200755.md): Frame · cracked · Mar 20, 2023 · N725FD · Airbus A300* · Fuselage Main, Structure
  > 1EA CRACK (1'') WAS FOUND AROUND RIVET HEAD OF LH PAX DOOR FR73A. ACCOMPLISHED THE SPLICE REPAIR WITH NEW FRAME SECTION I.A.W FEDEX EA NO: T6-5310- T0373688 P1, SEQ NO:810, TITLE:FUSELAGE-MAINFRAME-EO 6-5310-E0327267(SB A300-53-6175) INSPECTION -CRACK FOUND
- [SDR FDEA202303200667](https://openairdocs.org/sdr/FDEA202303200667.md): Skin · delaminated · Mar 20, 2023 · N725FD · Airbus A300* · Spoilers
  > 1EA DISBOND AREA WAS FOUND AT RH #5 SPOILER TOP SKIN.(1.3"X1.4") ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 57-72-11-201, PARA.12, PAGE.211-217, FIG.207 "MAJOR REPAIR"
- [SDR FDEA202303190767](https://openairdocs.org/sdr/FDEA202303190767.md): Stiffener · corroded · Mar 19, 2023 · N725FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AVIONICS COMP'T BILGE AREA OF STIFFENER CORROSION BETWEEN FR18 AND FR19,S-51L POSITION. REPLACED THE DAMAGE STIFFENER WITH NEW PART I.A.W A300-600 SRM 51-72-10-001.PAGE 2
- [SDR FDEA202303190756](https://openairdocs.org/sdr/FDEA202303190756.md): Seat Track · corroded · Mar 19, 2023 · N725FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - SEAT TRACK CROWN AREA GOT CORROSION LOCATION FROM FR14 TO FR15A AND - Y450 REPLACED THE DAMAGE SEAT TRACK WITH NEW I.A.W A300-600 SRM 51-72-10-001.PAGE.2
- [SDR FDEA202303180657](https://openairdocs.org/sdr/FDEA202303180657.md): Rudder · corroded · Mar 18, 2023 · N725FD · Airbus A300* · Rudder Structure
  > RUDDER T/E ANGLE STRIP GOT MINOR CORROSION FROM RIB18-23 ( TOTAL 5 POINT) PFM REPAIR OF APEX STRIP BY NEW STRIP SECTIONS AND CONNECTION PLATES WITH RIVETS, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-41-12-201, PARA.16, PAGE.237-239, FIG.208C & SRI:55- 41-12
- [SDR FDEA202303170658](https://openairdocs.org/sdr/FDEA202303170658.md): Rudder · damaged · Mar 17, 2023 · N725FD · Airbus A300* · Rudder Structure
  > 1EA WATER TRAPPED AREA(50MMX150MM) WAS FOUND AT NO.13 SCREW OF LH RUDDER SIDE PANEL. ACCOMPLISHED THE COMPOSITE STRUCTURE CAT.B REPAIR AT SCREW LINE IN REPAIR ZONE P I.A.W A300-600 SRM 55-41-12-201, PARA.31, PAGE.313-324, FIG.221, & SRI:55-41-12-201, IIR:5
- [SDR FDEA202303150768](https://openairdocs.org/sdr/FDEA202303150768.md): Doubler · cracked · Mar 15, 2023 · N725FD · Airbus A300* · Fuselage Main, Structure
  > MAIN LANDING GEAR BAY CEILING L/H BONDED DIAPHRAGM U-SHAPE DOUBLER CENTER SECTION A POINT GOT CRACK AT FR49 PLUS 6" AND BEAM4 TO BEAM5 TRIMMED THE DAMAGED AREA AND REINFORCED WITH FILLER & DOUBLER I.A.W FEDEX EA NO:T6-5310-T0373853 P1, SEQ NO:812, TITLE:FU
- [SDR FDEA202303150710](https://openairdocs.org/sdr/FDEA202303150710.md): Skin · damaged · Mar 15, 2023 · N725FD · Airbus A300* · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA (40MMX60MM)WAS FOUND AT NO.28 FASTENER OF RH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3)
- [SDR FDEA202303150709](https://openairdocs.org/sdr/FDEA202303150709.md): Skin · damaged · Mar 15, 2023 · N725FD · Airbus A300* · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA (65MMX95MM)WAS FOUND AT NO.30 FASTENER OF LH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3) &
- [SDR FDEA202303150708](https://openairdocs.org/sdr/FDEA202303150708.md): Skin · damaged · Mar 15, 2023 · N725FD · Airbus A300* · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA (75MMX85MM)WAS FOUND AT NO.18 FASTENER OF LH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3)
- [SDR FDEA202303030656](https://openairdocs.org/sdr/FDEA202303030656.md): Floorbeam · corroded · Mar 3, 2023 · N725FD · Airbus A300* · Fuselage Main, Structure
  > BULK CARGO COMPARTMENT FLOOR BEAM EXTERNAL SURFACE GOT CORRODED BETWEEN Y140~-Y810 POSITION,FR66. REMOVED THE DAMAGED FLOOR BEAM AND FABRICATED THE REPAIR PARTS, WET INSTALLED THE REPAIR PARTS I.A.W A300-600 SRM 53-10-15-201, PARA.9, FIG.207, PAGE.237~242,
- [SDR FDEA202211302861](https://openairdocs.org/sdr/FDEA202211302861.md): Tire · failed · Nov 30, 2022 · N725FD · Airbus A300B4622R · Tire
  > NR 3 TIRE FAILED ON LANDING. REMOVED AND REPLACED THE NR 3 TIRE IAW AMM 32-41-11-04-02, PERFORMED GENERAL VISUAL INSPECTION OF ALL ADJACENT COMPONENTS, ADDITIONAL DAMAGE NOTED IN WRI 32-43-7691, PERFORMED BRAKE CHECK IAW
- [SDR FDEA202009282349](https://openairdocs.org/sdr/FDEA202009282349.md): Skin · dented · Sep 28, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED, BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R. REPAIRED THE FUSELAGE SKIN DENT (OIL CAN) BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R, PER A300-600 SRM53-10-12 FIG.223. THIS REPAIR CATEGORY B. THE FIRST INSPECTION THRESHOLD IS 51000
- [SDR FDEA202009252348](https://openairdocs.org/sdr/FDEA202009252348.md): Skin · cracked · Sep 25, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 R
- [SDR FDEA202009252347](https://openairdocs.org/sdr/FDEA202009252347.md): Skin · cracked · Sep 25, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 R
- [SDR FDEA202009182346](https://openairdocs.org/sdr/FDEA202009182346.md): Frame · cracked · Sep 18, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > LOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT MIDDLE HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER W
- [SDR FDEA202009182345](https://openairdocs.org/sdr/FDEA202009182345.md): Frame · cracked · Sep 18, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > LOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT MIDDLE HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER W
- [SDR FDEA202009182342](https://openairdocs.org/sdr/FDEA202009182342.md): Frame · cracked · Sep 18, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > LOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WI
- [SDR FDEA202009182341](https://openairdocs.org/sdr/FDEA202009182341.md): Frame · cracked · Sep 18, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > LOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WI
- [SDR FDEA202009182340](https://openairdocs.org/sdr/FDEA202009182340.md): Frame · cracked · Sep 18, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > LOWER FUSELAGE FR40, CENTER WING JOINT FOUND RT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WIN
- [SDR FDEA202009152324](https://openairdocs.org/sdr/FDEA202009152324.md): Beam · cracked · Sep 15, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > NDT INSPECTION FOUND FUSELAGE MAINFRAME RT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME RT NR 2 GANTRY OUTBOARD FLANGE AT FR 51.A, PER AIRBUS DWG R53810581 ISSUE C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX G
- [SDR FDEA202009152323](https://openairdocs.org/sdr/FDEA202009152323.md): Beam · cracked · Sep 15, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > NDT INSPECTION FOUND FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE AT FR 51.A, PER AIRBUS DWG R53810581 ISSUE: C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX
- [SDR FDEA202009152322](https://openairdocs.org/sdr/FDEA202009152322.md): Beam · cracked · Sep 15, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > NDT INSPECTION FOUND FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE AT FR51.A, PER AIRBUS DWG R53810581 ISSUE: C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX G
- [SDR FDEA202009102321](https://openairdocs.org/sdr/FDEA202009102321.md): Stringer Splice · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE FR 47 S 18L CRACK ON STRINGER CONNECTION SECTION. REPLACED THE CRACKED STRINGER SPLICE AT UPPER FUSELAGE FR 47 STGR 18L AND COMPLETED, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM6-2-100.
- [SDR FDEA202009102320](https://openairdocs.org/sdr/FDEA202009102320.md): Stringer Splice · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE FR 47 S18L CRACK ON STRINGER CONNECTION SECTION. REPLACED THE CRACKED STRINGER SPLICE AT UPPER FUSELAGE FR 47 STGR 18L AND COMPLETED, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM6-2-100.
- [SDR FDEA202009102310](https://openairdocs.org/sdr/FDEA202009102310.md): Panel · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-
- [SDR FDEA202009102309](https://openairdocs.org/sdr/FDEA202009102309.md): Panel · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2
- [SDR FDEA202009102308](https://openairdocs.org/sdr/FDEA202009102308.md): Panel · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.
- [SDR FDEA202009102307](https://openairdocs.org/sdr/FDEA202009102307.md): Panel · cracked · Sep 10, 2020 · N725FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.
- [SDR FDEA202006091165](https://openairdocs.org/sdr/FDEA202006091165.md): Hydraulic Line · leaking · Jun 9, 2020 · N725FD · Airbus A300B4622R · Hydraulic System, Main
  > AT FL340,.79 MACH, GRN HYD RSVR LO LEVEL INDICATION RECEIVED. COMPLIED W/ECAM. ZERO FLUID ON OVERHEAD PANEL & ON ECAM GREEN SYSTEM. RAN QRH: HYD RSVR LO LEVEL & HYD SYS LP PR. MANUALLY EXTENDED GR IAW QRH. NO NOSEWHEEL STEERING - TOWED BACK. EMERGENCY
- [SDR FDEA2019022630485](https://openairdocs.org/sdr/FDEA2019022630485.md): Floor Panel · damaged · Feb 23, 2019 · N725FD · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARMENT ZONE 230 FLOOR PANEL 231TG HAS BROKEN CORNER FABRICATED NEW FLOOR PANEL PER SRZ-25-005 REV. P
- [SDR FDEA2018092522662](https://openairdocs.org/sdr/FDEA2018092522662.md): Brake · cracked · Sep 22, 2018 · N725FD · Airbus A300B4622R · Landing Gear Brake System
  > MDIS 725 32-43 2981 22SEP18 DSM FACT U DURING #5 WHEEL CHANGE FOUND #5 BRAKE ASSY TO HAVE SEVERAL CRACKED, BROKEN, AND MISSING DRIVE KEY SEGMENTS AND REINFORCEMENTS. R/I 22SEP18 02:22 DSM U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF
- [SDR FDEA201809202630](https://openairdocs.org/sdr/FDEA201809202630.md): Warning System · false activation · Sep 20, 2018 · N725FD · Airbus A300B4622R · Fire Detection
  > NR 2 ENGINE LOOP "B" FAULT DURING CRUISE AT FL 300. EXTINGUISHED DURING DESCENT. CREW DEBRIEF INDICATED THAT B LOOP LIGHT NEVER ACTUALLY CAME ON JUST FLICKERED. HAS HISTORY, PERFORMED ENG FIRE TEST REF AMM 26-12-05, TEST GOOD, BITE TEST OF FDCU NO FAULTS. RAN
- [SDR FDEA201804261122](https://openairdocs.org/sdr/FDEA201804261122.md): Frame · cracked · Apr 26, 2018 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > MAIN FRAME, LT SIDE NT 3 GANTRY INBD SIDE LOWER FLANGE WITH CRACK SIGNAL BETWEEN FRAMES 50.A AND 50.B.
- [SDR FDEA201804261121](https://openairdocs.org/sdr/FDEA201804261121.md): Frame · cracked · Apr 26, 2018 · N725FD · Airbus A300B4622R · Fuselage Main, Frame
  > MAIN FRAME, RT SIDE NR 3 GANTRY INBD SIDE, LOWER FLANGE WITH CRACK SIGNAL BETWEEN FRAMES 50.A AND 50.B
- [SDR FDEA201804100956](https://openairdocs.org/sdr/FDEA201804100956.md): Door Frame · cracked · Apr 10, 2018 · N725FD · Airbus A300B4622R · Cargo/Baggage Doors
  > FWD CARGO COMPARTMENT DOOR ACTUATOR ATTACH FRAME FOUND CRACK AT FR22A.
- [SDR FDEA201804090953](https://openairdocs.org/sdr/FDEA201804090953.md): Bulkhead Web · cracked · Apr 9, 2018 · N725FD · Airbus A300B4622R · Fuselage Main, Bulkhead
  > MAIN DECK CARGO, HORIZONTAL PRESSURE VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y0 AND Y-450. REPLACED PRESSURE VERTICAL WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N725FD/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 = 'N725FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N725FD/reports

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