# Service difficulty reports: N741FD

A list on [N741FD](https://openairdocs.org/aircraft/N741FD.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 · 198 reports

- [SDR FDEA202506160965](https://openairdocs.org/sdr/FDEA202506160965.md): Support Rib · corroded · Jun 16, 2025 · N741FD · Airbus A300B4622R · Main Landing Gear Attach Section
  > L/H MLG SUPPORT WING RIB 5 FWD LUG CORROSION NOTED REPAIR PER E.A. 6-5710-T0383717 AND AIRBUS DRAWING R57240425.
- [SDR FDEA202506160964](https://openairdocs.org/sdr/FDEA202506160964.md): Support Rib · corroded · Jun 16, 2025 · N741FD · Airbus A300B4622R · Main Landing Gear Attach Section
  > R/H MLG SUPPORT WING RIB 5 FWD LUG CORROSION NOTED BETWEEN BUSH "D" AND BUSH "E". REPAIR IN ACCORDANCE WITH E.A. 6-5710-T0383720 AND AIRBUS REPAIR DRAWING R57240425.
- [SDR FDEA202503130409](https://openairdocs.org/sdr/FDEA202503130409.md): Data Unit · failed · Mar 13, 2025 · N741FD · Airbus A300B4622R · Indicating/Recording System
  > LIGHTNING STRIKE ON DEPARTURE. MULTIPLE ECAM DISPLAY ANOMALIES IN ENG, BLEED, PRESS, AND F/CTL. NO OTHER INDICATIONS OF DISCREPANCIES. AMM: 31-55-22-04 AMM: 31-51-00-05-01 PERFORMED ECAM BITE TEST PER AMM 31-51-00-05-01. FAILED SDAC. REPLACED SDAC IAW
- [SDR FDEA202502050225](https://openairdocs.org/sdr/FDEA202502050225.md): Structure · none · Feb 5, 2025 · N741FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON RH FWD DOOR LOWER FWD CORNER SKIN FR14-FR14A REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH FWD DOOR LOWER FWD CORNER SKIN FR14-FR14A WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM52-11-00-201-2 FIG.206. ONE MISS
- [SDR FDEA202502050206](https://openairdocs.org/sdr/FDEA202502050206.md): Rib · cracked · Feb 5, 2025 · N741FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > LH WING - CENTER SPAR RIB1 SPLICE TYPE 5 MIDDLE HOLE FOUND CRACK REPLACED THE CRACKED OUTER FITTING AT LH WING CENTER SPAR RIB1 PER A300-600 SRM 51- 40-21 & DWG: A57110911 ISSUE L.THIS IS A CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR FDEA202502020168](https://openairdocs.org/sdr/FDEA202502020168.md): None · none · Feb 2, 2025 · N741FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON LH WING I/B FLAP UPPER SKIN RIB1C - RIB3 S2.1 - S2.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISITING REPAIR ON LH WING I/B FLAP UPPER SKIN RIB1C-RIB3 S2.1-S2.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5752-114869. TITLE: STRUCTUR
- [SDR FDEA202502020167](https://openairdocs.org/sdr/FDEA202502020167.md): Stringer · damaged · Feb 2, 2025 · N741FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR ON FUSELAGE STRINGER S56L BETWEEN FR54 AND FR54.2 REQUIRES EVALUATION FOR CONFORMITY. REPAIRED FUSELAGE STRINGER S56L BETWEEN FR54-FR54.2 PER A300-600 SRM53-10-14 FIG.203. THIS IS A CATEGORY B REPAIR. THE FIRST INSPECTION THRESHOLD WAS 510
- [SDR FDEA202502010246](https://openairdocs.org/sdr/FDEA202502010246.md): Fitting · damaged · Feb 1, 2025 · N741FD · Airbus A300B4622R · Cargo/Baggage Doors
  > COMPLY WITH E.O.6-5230-E0378588 B PT5 PERFORM MDCD ACTUATOR BEARING FITTINGS REPLACEMENT 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 A
- [SDR FDEA202502010245](https://openairdocs.org/sdr/FDEA202502010245.md): Fitting · damaged · Feb 1, 2025 · N741FD · Airbus A300B4622R · Cargo/Baggage Doors
  > COMPLY WITH E.O.6-5230-E0378588 B PT5 PERFORM MDCD ACTUATOR BEARING FITTINGS REPLACEMENT COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME
- [SDR FDEA202501300152](https://openairdocs.org/sdr/FDEA202501300152.md): Rib · cracked · Jan 30, 2025 · N741FD · Airbus A300B4622R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0332530 A P2 REPAIRED RH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WINGS - FLIGHT SURFACES - C
- [SDR FDEA202501300151](https://openairdocs.org/sdr/FDEA202501300151.md): Rib · cracked · Jan 30, 2025 · N741FD · Airbus A300B4622R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB18, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0332530 A P2 REPAIRED RH WING CENTER FLAP RIB UPR FLANGE 2EA CRACKS AT RIB18,RIB20 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WINGS - FLIG
- [SDR FDEA202501190267](https://openairdocs.org/sdr/FDEA202501190267.md): Slide Raft · inoperative · Jan 19, 2025 · N741FD · Airbus A300B4622R · Life Raft
  > L1 REMOVE AND REPLACE L1/R1 DR SLIDE/ RAFT REPLACED THE SLIDE/RAFT OF L1 PASSENGER/CREW DOOR PER AMM 25-61-22-04-01. MINOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR FDEA202412101786](https://openairdocs.org/sdr/FDEA202412101786.md): Battery Pack · inoperative · Dec 10, 2024 · N741FD · Airbus A300B4622R · Emergency Lighting
  > CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW ABOVE REF, OPS CHECK GOOD.
- [SDR FDEA202207201775](https://openairdocs.org/sdr/FDEA202207201775.md): None · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Nacelle/Pylon Structure
  > LH PYLON O/B SIDE PANEL AT RIB8 FOUND 1EA CRACK REPAIRED THE CRACKED LH PYLON O/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 &
- [SDR FDEA202207201784](https://openairdocs.org/sdr/FDEA202207201784.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR50B CRACK WAS FOUND (LENGTH:14MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR50B PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAI
- [SDR FDEA202207201783](https://openairdocs.org/sdr/FDEA202207201783.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- L/H SIDE OF LH GANTRY 4 AT FR50.1 CRACK WAS FOUND (LENGTH:15MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR50.1 PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REP
- [SDR FDEA202207201782](https://openairdocs.org/sdr/FDEA202207201782.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- L/H SIDE OF LH GANTRY 4 AT FR49.1 CRACK WAS FOUND (LENGTH:56MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR49.1 PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REP
- [SDR FDEA202207201781](https://openairdocs.org/sdr/FDEA202207201781.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR51A CRACK WAS FOUND (LENGTH:25MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR51A PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAI
- [SDR FDEA202207201780](https://openairdocs.org/sdr/FDEA202207201780.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR52A CRACK WAS FOUND (LENGTH:35MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR52A PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAI
- [SDR FDEA202207201777](https://openairdocs.org/sdr/FDEA202207201777.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE - L/H SIDE OF LH GANTRY 2 AT FR49.1 CRACK WAS FOUND (LENGTH:30MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 2 LWR FLANGE AT FR49.1 PER EO: 6-5310-7-5021 F PT2 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR RE
- [SDR FDEA202207201776](https://openairdocs.org/sdr/FDEA202207201776.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE - L/H SIDE OF LH GANTRY 4 AT FR51A, FR52 & FR52A FOUND 3EA CRACKS. (LENGTH: 30MM, 11MM, 32MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR51A, FR52 & FR52A PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSU
- [SDR FDEA202207201779](https://openairdocs.org/sdr/FDEA202207201779.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE - R/H SIDE OF RH GANTRY 4 AT FR52A CRACK WAS FOUND (LENGTH:18MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF RH GANTRY 4 LWR FLANGE AT FR52A PER EO: 6-5310-7-5021 F PT7 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REPA
- [SDR FDEA202207201778](https://openairdocs.org/sdr/FDEA202207201778.md): Beam · cracked · Jul 20, 2022 · N741FD · Airbus A300* · Fuselage Main, Structure
  > FUSELAGE- R/H SIDE OF LH GANTRY 3 AT FR50.1 CRACK WAS FOUND (LENGTH:96MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 3 LWR FLANGE AT FR50.1 PER EO: 6-5310-7-5021 F PT4 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REP
- [SDR FDEA202207181753](https://openairdocs.org/sdr/FDEA202207181753.md): None · cracked · Jul 18, 2022 · N741FD · Airbus A300* · Passenger/Crew Doors
  > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS REPLACED RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (REV.K), F52181299(REV.G). TRACKING EA 6-5210-T0369499 P1 RAISED AND ACCOMPL
- [SDR FDEA202207011725](https://openairdocs.org/sdr/FDEA202207011725.md): Spoiler · delaminated · Jul 1, 2022 · N741FD · Airbus A300* · Wing, Control Surfaces
  > RH WING - #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 60MM*30MM, DEPTH: 1.59MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 40MM*30MM, DEPTH:1.54MM) REPAIRED THE RH WING #5 SPOILER CENTER I/B &O/B HINGE ARM O/B SIDE D
- [SDR FDEA202207011723](https://openairdocs.org/sdr/FDEA202207011723.md): Spoiler · delaminated · Jul 1, 2022 · N741FD · Airbus A300* · Wing, Control Surfaces
  > LH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 20MM*20MM, DEPTH: 2.1MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 80MM*90MM, DEPTH:1.64MM) REPAIRED THE LH WING #5 SPOILER CENTER O/B HINGE ARM LOWER SURFA
- [SDR FDEA202109242397](https://openairdocs.org/sdr/FDEA202109242397.md): Pump · leaking · Sep 24, 2021 · N741FD · Airbus A300B4622R · Hydraulic Pump (Electric/Engine), Main
  > BLUE SYSTEM HYDRAULIC PUMP LOW PRESSURE ON ROLL OUT WHEN SETTING SPOILERS. R & R #1 ENG BLUE SYS SUCTION LINE REF AMM 29-00-00-04. PERFORMED BLEEDING OF BLUE SYS REF AMM 29-00-00-04. NOTED WHEN DEPRESSURIZING RESERVOIR QTY INDICATION WAS OVERFULL. SUSPEC
- [SDR FDEA202101270198](https://openairdocs.org/sdr/FDEA202101270198.md): Switch · arced · Jan 27, 2021 · N741FD · Airbus A300B4622R · Exterior Lighting
  > DURING THE IN RANGE CHECK WHEN TURNED ON LT LANDING LIGHT THERE WAS A SPARK THAT CAME OUT FROM THE EXT LIGHT PANEL & THE UPPER BEACON CIRCUIT BREAKER POPPED. T AN ACRID SMELL IN THE COCKPIT FOR ABOUT 1 MINUTE. SPARKS COMING FROM BEHIND 426VU PANEL. INSPECTE
- [SDR FDEA2020011640129](https://openairdocs.org/sdr/FDEA2020011640129.md): Floor Panel · damaged · Jan 14, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO, 151HF FLOOR PANEL BROKEN. FABRCATED 151HF FLOOR PANEL ON T20/1467291 IAW DWG SRZ-25-005 REV R, MAJOR REPAIR CAT "A".
- [SDR FDEA2020011310114](https://openairdocs.org/sdr/FDEA2020011310114.md): Floor Panel · damaged · Jan 11, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC 242EK FLOOR PANEL BROKEN. FABRICATED 242EK FLOOR PANEL ON T20/1467275 IAW DWG SRZ-25-005 REV R, MAJOR REPAIR CAT "A".
- [SDR FDEA2020011310113](https://openairdocs.org/sdr/FDEA2020011310113.md): Floor Panel · damaged · Jan 11, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO, FLOOR PANEL 132RF BROKEN. FABRICATED 132RF FLOOR PANEL ON T20/1467278 IAW DWG SRZ-25-005 REV R, MAJOR REPAIR CAT "A".
- [SDR FDEA2020011310115](https://openairdocs.org/sdr/FDEA2020011310115.md): Floor Panel · damaged · Jan 11, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO 131QF FLOOR PANEL BROKEN. FABRICATED 131QF FLOOR PANEL ON T20/1467282 IAW DWG SRZ-25-005 REV R MAJOR REPAIR CAT "A".
- [SDR FDEA2020011310111](https://openairdocs.org/sdr/FDEA2020011310111.md): Floor Panel · damaged · Jan 11, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221PF BROKEN. FABRICATED COURIER FLOOR PANEL 221PF ON T19/1465916 IAW DWG SRZ- 25-005 REV R, CAT "A" MAJOR REPAIR.
- [SDR FDEA2020010980061](https://openairdocs.org/sdr/FDEA2020010980061.md): Floor Panel · broken · Jan 8, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 231WG BROKEN. FABRICATED 231WG FLOOR PANEL ON VTMAE TRAVELER # T19/1465938 IAW DWG SRZ-25-005 REV R, CAT "A' AND MAJOR REPAIR.
- [SDR FDEA2020010980060](https://openairdocs.org/sdr/FDEA2020010980060.md): Floor Panel · broken · Jan 8, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 252YG BROKEN. FABRICATED 252YG FLOOR PANEL ON VTMAE TRAVELER # T19/1465922 IAW DWG SRZ-25-005 REV R, CAT "A" AND MAJOR REPAIR.
- [SDR FDEA2020010980059](https://openairdocs.org/sdr/FDEA2020010980059.md): Floor Panel · broken · Jan 8, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 261VF BROKEN. FABRICATED 261VF FLOOR PANEL ON VTMAE TRAVELER # T19/1465945 IAW DWG SRZ-25-005 REV R, CAT "A" AND MAJOR REPAIR.
- [SDR FDEA2020010980058](https://openairdocs.org/sdr/FDEA2020010980058.md): Floor Panel · damaged · Jan 8, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 231EF BROKEN. FABRICATED 231EF FLOOR PANEL ON VTMAE TRAVELER # T19/1465948 IAW DWG SRZ-25-005 REV "R", CAT "A" AND MAJOR REPAIR.
- [SDR FDEA2020010980057](https://openairdocs.org/sdr/FDEA2020010980057.md): Floor Panel · broken · Jan 8, 2020 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 241KJ BROKEN. FABRICATED 241KJ FLOOR PANEL ON VTMAE TRAVELER # T19/1465934 IAW DWG SRZ-25-005 REV R, CAT "A" AND MAJOR REPAIR.
- [SDR FDEA201807201793](https://openairdocs.org/sdr/FDEA201807201793.md): Gcu · inoperative · Jul 20, 2018 · N741FD · Airbus A300B4622R · AC Generator-Alternator
  > GEN 1 FAULTED ON TAKEOFF ROLL, RESET WAS GOOD AFTER CLEARING RUNWAY. GEN NR 1 INOP. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. REMOVED AND REPLACED #1 GENERATOR CONTROL UNIT 1XU IAW AMM 24-22-12-04. OPS CHEC
- [SDR FDEA201806161508](https://openairdocs.org/sdr/FDEA201806161508.md): Battery · failed · Jun 16, 2018 · N741FD · Airbus A300B4622 · Door Warning System
  > RT SIDE SLIDE DID NOT ARM ON FIRST TRY. OPENED DOOR AND CLOSED IT AND THEN IT ARMED. R1 DOOR ESCAPE SLIDE ARMED NORMALLY ON ARRIVAL, BITE TEST OF ASPSU FAILS NR 1 BATTERY. R&R NR 1 BATTERY PER AMM 52-73-18-04-0. DOOR SLIDE OPS CHECK GOOD PER AMM 52-73-00-05-
- [SDR FDEA201706241760](https://openairdocs.org/sdr/FDEA201706241760.md): Gcu · failed · Jun 24, 2017 · N741FD · Airbus A300B4622R · AC Generator-Alternator
  > NR 2 GENERATOR FAULT. SWAPPED THE NR 2 GCU WITH APU GCU IAW AMM 24-22-12-04, PERFORMED OPERATIONAL TEST OF THE NR 2 GCU IAW AMM 24-41-00-05, TESTED NORMAL. PERFORMED HIGH POWER ENGINE RUN IAW JRH, TESTED NORMAL. PERFORMED WATER INSPECTION IN AVIONICS
- [SDR FDEA201706231752](https://openairdocs.org/sdr/FDEA201706231752.md): Gcu · failed · Jun 23, 2017 · N741FD · Airbus A300B4622R · AC Generator-Alternator
  > REJECTED TAKEOFF DUE TO BOTH GENERATORS 1 & 2 FAULTED. BITE CHECKED GPCU AND FOUND THE NR 1 AND 2 GCU FAILED. R & R THE GPCU IAW AMM 24-41-11-04, PERFORMED OPERATIONAL TEST IAW AMM 24-41-00-05, TESTED NORMAL. R & R THE NR 1 GCU IAW AMM 24-22-12-04, PERFORM
- [SDR FDEA201706121614](https://openairdocs.org/sdr/FDEA201706121614.md): Frame · cracked · Jun 12, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Frame
  > FUSELAGE FRAME 45 UPPER SECTION FOUND CRACKED AT STRINGER 35R REPAIRED IAW EO 6-5310-E0330747 P12. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201706121613](https://openairdocs.org/sdr/FDEA201706121613.md): Frame · cracked · Jun 12, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Frame
  > FRAME 46 FOUND CRACKED STRINGER 35R REPAIRED IAW EO 6-5310-E0330747 P14. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201706121612](https://openairdocs.org/sdr/FDEA201706121612.md): Frame · cracked · Jun 12, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Frame
  > FUSELAGE FR46 LH FRAME FOUND CRACK EXTENDED STOP HOLE AT ABOUT STR35LH LOCATION(EXTENDED CRACK LENGTH:1MM) THE WORK WAS COMPETED IN EO: 6-5310-E0330747 P13, TITLE: FUSELAGE - MAINFRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAME 41 AND 46, AIR
- [SDR FDEA201706071585](https://openairdocs.org/sdr/FDEA201706071585.md): Skin · punctured · Jun 7, 2017 · N741FD · Airbus A300B4622R · Ailerons
  > LEFT WING AILERON TOP SKIN CENTER SECTION PUNCTURED BETWEEN RIBS 4 & 5. REPAIRED. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201706061572](https://openairdocs.org/sdr/FDEA201706061572.md): Structure · cracked · Jun 6, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FUSE CTR WING BOX, INSP OF REAR SPAR & BOTTOM PANEL-NDT INSPECTION OF HOLE "G" WITH CRACK SIGNAL, LT SIDE. COMPLIED WITH EA6-5710-T0332723 P. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201706051567](https://openairdocs.org/sdr/FDEA201706051567.md): Fitting · cracked · Jun 5, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Structure
  > REAR SPAR & BOTTOM PANEL, NDT INSPECTION OF HOLE K HAD A CRACK SIGNAL. REPAIRED IAW EA6-5710-T0332723 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201706051564](https://openairdocs.org/sdr/FDEA201706051564.md): Fitting · cracked · Jun 5, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Structure
  > SPAR HAD A CRACK SIGNAL. REPAIRED IAW EA6-5710-T0332723 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201706051566](https://openairdocs.org/sdr/FDEA201706051566.md): Fitting · cracked · Jun 5, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Structure
  > REAR SPAR & BOTTOM PANEL, NDT INSPECTION OF HOLE B HAD A CRACK SIGNAL. REPAIRED IAW EA6-5710-T0332723 P1. MAJOR REPAIR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N741FD/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 = 'N741FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N741FD/reports

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