# Service difficulty reports: N740FD

A list on [N740FD](https://openairdocs.org/aircraft/N740FD.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 · 156 reports

- [SDR FDEA202309221634](https://openairdocs.org/sdr/FDEA202309221634.md): Stringer Splice · cracked · Sep 22, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/Stringer
  > COMPLY WITH EO 6-5310-7-5023 A PT2. REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18RH - FR47. TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT2. TITLE: FUSELAGE
- [SDR FDEA202309051547](https://openairdocs.org/sdr/FDEA202309051547.md): Skin · damaged · Sep 5, 2023 · N740FD · Airbus A300* · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH WAS EVALUATED AND FOUND CONFORMITY WITH A300-600 SRM53-19-12 FIG.
- [SDR FDEA202309051546](https://openairdocs.org/sdr/FDEA202309051546.md): Skin · dented · Sep 5, 2023 · N740FD · Airbus A300* · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH WAS EVALUATED AND FOUND CONFORMITY WITH RAS/DATLS/0002239/2004 IS
- [SDR FDEA202309011535](https://openairdocs.org/sdr/FDEA202309011535.md): Stringer · unknown · Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202309011534](https://openairdocs.org/sdr/FDEA202309011534.md): Stringer · unknown · Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202309011533](https://openairdocs.org/sdr/FDEA202309011533.md): Stringer · unknown · Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308271511](https://openairdocs.org/sdr/FDEA202308271511.md): Skin Panel · cracked · Aug 27, 2023 · N740FD · Airbus A300* · Wing, Plate/Skin
  > LH WING - LEADING EDGE PANEL 523BB CUTOUT EDGE SKIN 1EA CRACK WAS FOUND COMPLIED WITH EA: 6-5710-T0375872 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS 8-9 - CRACK. REPAIRED THE LH WING LEADING EDGE PANE
- [SDR FDEA202308271510](https://openairdocs.org/sdr/FDEA202308271510.md): Angle · cracked · Aug 27, 2023 · N740FD · Airbus A300* · Wing Spar
  > RIB8 INSPECTION OF CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING, FASTENER HOLE 58 FOUND CRACK COMPLIED WITH EA: 6-5710-T0375850 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK ON RH WING RIB 8 SEAL ANGLE - REPAIR. REPAIRED T
- [SDR FDEA202308211471](https://openairdocs.org/sdr/FDEA202308211471.md): Spoiler · delaminated · Aug 21, 2023 · N740FD · Airbus A300* · Spoilers
  > LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM OUTSIDE SURFACE AND CENTER I/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)44MM*25MM, DEPTH: 1.3MM (2)80MM*25MM, DEPTH: 1.14MM (3)25MM*20MM, DEPTH: 2.65MM COMPLIED WITH EA: 6-5750-T0359414 A P2. TITLE: W
- [SDR FDEA202308211470](https://openairdocs.org/sdr/FDEA202308211470.md): Stringer · unknown · Aug 21, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/Stringer
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308211469](https://openairdocs.org/sdr/FDEA202308211469.md): Seat Track · unknown · Aug 21, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-510
- [SDR FDEA202308211468](https://openairdocs.org/sdr/FDEA202308211468.md): Seat Track · unknown · Aug 21, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5
- [SDR FDEA202308151438](https://openairdocs.org/sdr/FDEA202308151438.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6
- [SDR FDEA202308151437](https://openairdocs.org/sdr/FDEA202308151437.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6
- [SDR FDEA202308151436](https://openairdocs.org/sdr/FDEA202308151436.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5
- [SDR FDEA202308151435](https://openairdocs.org/sdr/FDEA202308151435.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5
- [SDR FDEA202308151434](https://openairdocs.org/sdr/FDEA202308151434.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-510
- [SDR FDEA202308151432](https://openairdocs.org/sdr/FDEA202308151432.md): Stringer · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308151431](https://openairdocs.org/sdr/FDEA202308151431.md): Stringer · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308151430](https://openairdocs.org/sdr/FDEA202308151430.md): Stringer · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308151429](https://openairdocs.org/sdr/FDEA202308151429.md): Stringer · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308151428](https://openairdocs.org/sdr/FDEA202308151428.md): Stringer · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201.
- [SDR FDEA202308151424](https://openairdocs.org/sdr/FDEA202308151424.md): Seat Track · unknown · Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5
- [SDR FDEA202207241792](https://openairdocs.org/sdr/FDEA202207241792.md): None · damaged · Aug 24, 2021 · N740FD · Airbus A300* · Fuselage Main, Structure
  > MDIS 740 25-50 5864 24AUG21 IND FACT U REF WRI 25-50/5863 SEAT TRACK DAMAGED AT LOCK POSITION M1654 SHGN 24AUG21 09:41 IND U FOUND ADAPTER SEAT TRACK LOBES MISSING OIL 24AUG21 09:56 IND U NO RESTRICTION REF: SR30-53-003 SEAT TR
- [SDR FDEA202103010519](https://openairdocs.org/sdr/FDEA202103010519.md): Pump · failed · Mar 1, 2021 · N740FD · Airbus A300B4622R · Hydraulic System, Main
  > PDIS 740 29-11 5444 01MAR21 ANC OPEN U LOGPAGES:3142187 UPON TAKEOFF YELLOW HYD PRESSURE DROPPED TO 0 PSI FOR APPROX 30 SEC WITH CORRESPONDING LOW HYD PRESS ECAM, PRESSURE THEN RETURNED TO 3050 PSI. THIS HAPPENED 3 SEPERATE TIMES WITHIN A 2 M
- [SDR FDEA202102110329](https://openairdocs.org/sdr/FDEA202102110329.md): Skin · damaged · Feb 11, 2021 · N740FD · Airbus A300B4622R · Elevator, Plate/Skin
  > LH ELEVATOR UPR SKIN PANEL RIB4-RIB5 FOUND IMPACT DAMAGE REPAIRED THE LH ELEVATOR UPR SKIN PANEL RIB4-RIB5 IMPACT DAMAGE PER A300-600 SRM55-21-12-201-2 PARA.5.J. THIS IS CAT B REPAIR. TRACKING EA: 6-5520-T0359677 P1 RAISED AND COMPLETED. TITLE: STABILIZE
- [SDR FDEA202102050293](https://openairdocs.org/sdr/FDEA202102050293.md): Hinge Arm · delaminated · Feb 5, 2021 · N740FD · Airbus A300B4622R · Spoilers
  > RH WING #3 SPOILER CENTER I/B HINGE ARM O/B SURFACE AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)20MM*10MM, DEPTH: 1.6MM (2)20MM*15MM, DEPTH: 2.1MM (3)20MM*15MM, DEPTH: 2.4MM COMPLIED WITH EA: 6-5750-T0359409 P1. TITLE: WING
- [SDR FDEA202102020263](https://openairdocs.org/sdr/FDEA202102020263.md): Stringer · corroded · Feb 2, 2021 · N740FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 46RH FOUND CORROSION BETWEEN FR61 AND FR62A COMPLIED WITH EA: 6-5310-150949 A P3. TITLE: FUSELAGE - MAINFRAME - CORROSION DAMAGE ON STRINGER 46R - REPAIR. REPAIRED THE AFT CARGO STRINGER 46RH CORROSION BETWEEN FR61 AND FR62A. THIS IS CAT
- [SDR FDEA202101290230](https://openairdocs.org/sdr/FDEA202101290230.md): Skin · cracked · Jan 29, 2021 · N740FD · Airbus A300B4622R · Wing, Plate/Skin
  > RH WING - RIB8~RIB9, SUSPECTED CRACK ACROSS FASTENER HOLE ON LWR SKIN FWD EDGE APPROX 1.0 INCH IN LENGTH COMPLIED WITH EA: 6-5710-T0359505 P1. TITLE: WINGS - BASIC WING STRUCTURE - RH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS8-9 - CRACK. REPAI
- [SDR FDEA2020081211857](https://openairdocs.org/sdr/FDEA2020081211857.md): Hydraulic System · low · Aug 11, 2020 · N740FD · Airbus A300B4622R · Hydraulic System, Main
  > DURIG CRUISE OBSERVED GREE HYDRAULICS ON OVERHEAD AT RED DOT, COMFIRMED BY ECAM. SHORTY THERE AFTER RECEIVED GRN LO LEVEL WARNIING. RAN QRH INCLUDING MANUAL GEAR EXTENETION CREW REQUESTED TOW TO GATE. ONCE PARKED, INSPECTED A/C FUSEAGE AND FLIGHT SURFACES
- [SDR FDEA202001170160](https://openairdocs.org/sdr/FDEA202001170160.md): Selector Valve · failed · Jan 17, 2020 · N740FD · Airbus A300B4622R · Landing Gear Selector
  > L/G RETRACTION FAILURE SYSTEM 1, DOORS OPENED BUT GEAR DIDNT MOVE. IF WIRING CHECKS ARE OK OK FROM 2GA TO 3GA, THE WIRING SHOULD ALSO BE MEGGED. COMPLETE IF MEG CHECKS ARE OK, R/R 2GA AND 3GA. COMPLETE IF REQUIRED R/R 2GAA AND 3GAA C/P'S. COMPLETE R&R LANDI
- [SDR FDEA2019040860769](https://openairdocs.org/sdr/FDEA2019040860769.md): Line · leaking · Apr 6, 2019 · N740FD · Airbus A300B4622R · Hydraulic System, Main
  > AFTER 30 MINUTES OF FLIGHT AT FL 290 GOT ECAM WARNING FOR GREEN HYSD PRESS LOW. VERIFIED ON OVERHEAD PANEL AND RT ECAM PAGE THAT GREEN HYDRAULIC WAS
- [SDR FDEA2018081412013](https://openairdocs.org/sdr/FDEA2018081412013.md): Switch · out of adjust · Aug 11, 2018 · N740FD · Airbus A300B4622R · Door Warning System
  > AT APPROXIMATELY 10,000 FT DURING DEPARTURE, RECIEVED AN ECAM CAUTION FOR THE MAIN DECK DOOR NOT CLOSED. COMPLIED WITH RED TABS AND RETURNED FOR LANDING. NO ABNORMAL CABIN RATE OBSERVED. FOUND THE SWITCH 48WS NOT MAKING CONTACT. ADJUSTED THE SWITCH IAW AM
- [SDR FDEA201807171770](https://openairdocs.org/sdr/FDEA201807171770.md): Seat Track · damaged · Jul 17, 2018 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SCALLOP BROKEN IN MAIN DECK CARGO BETWEEN FR66 AND FR67 Y1456 CUT OUT SEAT TRACK SECTION Y1456 FR66 TO FR67 IAW SRM 53-10-16 FIG 201. FABRICATED NEW SEAT TRACK SECTION, MATERIAL P/N A53274005-SFS-DAP. INSTALLED NEW SEAT TRACK SECTION FR66 TO FR67
- [SDR FDEA201807171766](https://openairdocs.org/sdr/FDEA201807171766.md): Seat Track · gouged · Jul 17, 2018 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON SEAT TRACK SCALLOP IN MAIN DECK CARGO AT FR60 Y1456. BLENDED AREA IAW SRM 51-73-10. CHECKED LIMITS, MINIMUM MATERIAL REMOVED IS.260 AFTER REWORK.190 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. FABRICATED NEW SEAT TRACK MATERIAL P/N# A53274005-
- [SDR FDEA201807161723](https://openairdocs.org/sdr/FDEA201807161723.md): Floor Panel · damaged · Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221LF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 221LF ON T18/1354016 IAW SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA201807161721](https://openairdocs.org/sdr/FDEA201807161721.md): Floor Panel · damaged · Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222F GOUGED. FABRICATED COURIER FLOOR PANEL 222F ON T18/1354014 IAW SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA201807161720](https://openairdocs.org/sdr/FDEA201807161720.md): Floor Panel · damaged · Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222QF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 222QF ON T18/1354018 IAW SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA2018071641714](https://openairdocs.org/sdr/FDEA2018071641714.md): Floor Panel · cracked · Jul 14, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 251WH IN MDC FABRICATED 251WH FLOOR PANEL ON T18/1354253IAW DWG SRZ 25-006 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201807131705](https://openairdocs.org/sdr/FDEA201807131705.md): Floor Panel · broken · Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 242EK FLOOR PANEL BROKEN. FABRICATED 242EK FLOOR PANEL ON T18/1353526 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA201807131704](https://openairdocs.org/sdr/FDEA201807131704.md): Floor Panel · broken · Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 242LK FLOOR PANEL BROKEN. FABRICATED 242LK FLOOR PANEL ON T18/1353615 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA201807131703](https://openairdocs.org/sdr/FDEA201807131703.md): Floor Panel · broken · Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 231TG FLOOR PANEL BROKEN. FABRICATED 231TG FLOOR PANEL ON T18/1353527 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA201807131702](https://openairdocs.org/sdr/FDEA201807131702.md): Floor Panel · broken · Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 232HG FLOOR PANEL BROKEN. FABRICATED 232HG FLOOR PANEL ON T18/1353529 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA201807131700](https://openairdocs.org/sdr/FDEA201807131700.md): Floor Panel · broken · Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 231HG FLOOR PANEL BROKEN. FABRICATE 231HG FLOOR PANEL ON T18/1353530 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA201806011373](https://openairdocs.org/sdr/FDEA201806011373.md): B-Nut · loose · Jun 1, 2018 · N740FD · Airbus A300B4622R · APU Oil System
  > DURING CRUISE AT 310 FT, THE APU AUTO SHUTDOWN. FOLLOWED QRH, TRIED TO RESTART, AND THE APU WOULD NOT RESTART. FOUND APU OIL LOW AT BLOCK IN. APU ECB SHOWED LOW OIL PRESSURE FAULT. CLEARED FAULT, SERVICED THE APU OIL SYSTEM. FOUND SCAVANGE LINE B-NUT L
- [SDR FDEA201609273373](https://openairdocs.org/sdr/FDEA201609273373.md): Indication Sys · faulty · Sep 27, 2016 · N740FD · Airbus A300B4622R · Fuel Indicating System
  > FUEL SYSTEM HAS MEL 28-42-02-02-A. AFTER T/O TRIM FUEL DASHES CAME AND WENT CAUSING FMMS ISSUES. FUEL LOW LEVEL LIGHTS THEN CAME ON AND OFF. REF MEL 28-42-02-02-A, STEP 5 DELETES FUEL QTY. INPUTS TO FMS, REF AMM 28-42-41-04, RT FUEL LOW LEVEL LIGHTS CHECK
- [SDR FDEA201603170939](https://openairdocs.org/sdr/FDEA201603170939.md): Seat Track · corroded · Mar 17, 2016 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDCC, FRAME 15A, Y953, SEAT TRACK WITH INNER - GRANULAR CORROSION. REPLACED THE SERIOUS CORRODED SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM6-6-100.
- [SDR FDEA201603140920](https://openairdocs.org/sdr/FDEA201603140920.md): Web · cracked · Mar 14, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MDCC FRAME 47, Y953~ 1456, FLOOR WEB, CRACKED APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM 53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM 53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM 53-15-1
- [SDR FDEA201603140919](https://openairdocs.org/sdr/FDEA201603140919.md): Web · cracked · Mar 14, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MDCC FRAME 47, -Y953~-Y1456, FLOOR WEB CRACKED, APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM53-15-15
- [SDR FDEA201603120909](https://openairdocs.org/sdr/FDEA201603120909.md): Web · cracked · Mar 12, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MDCC FRAME 47, Y0~ Y450, FLOOR WEB CRACKED, APPROX 1.0 INCH IN LENGTH. FABRICATE NEW WEB IAW DWG A53832100. INSTALL NEW WEB IAW SRM 51-40-21. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N740FD/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 = 'N740FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N740FD/reports

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