# Service difficulty reports: N746FD

A list on [N746FD](https://openairdocs.org/aircraft/N746FD.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 · 234 reports

- [SDR FDEA202603230366](https://openairdocs.org/sdr/FDEA202603230366.md): Skin · damaged · Mar 23, 2026 · N746FD · Airbus A300B4622R · Rudder, Plate/Skin
  > RUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE FOUND WATER INGRESS. DAMAGE AT RUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE PER A300-600 SRM55-41-12-201 PARA.30 FIGURE 219.
- [SDR FDEA202603010299](https://openairdocs.org/sdr/FDEA202603010299.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB25 AND 26 BETWEEN STGR2
- [SDR FDEA202603010298](https://openairdocs.org/sdr/FDEA202603010298.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB18 BETWEEN STGR2.7 AND REAR SPAR, RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB18 AND 19 BETWEEN STGR2.7
- [SDR FDEA202603010297](https://openairdocs.org/sdr/FDEA202603010297.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIBS UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN S2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 & REAR SPAR, RIB13 BETWEEN S2.6 AND S2.8 COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 7EA CRACKS OF RIB11
- [SDR FDEA202603010296](https://openairdocs.org/sdr/FDEA202603010296.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND FRONT SPAR COMPLIED WITH EA 6-5750-T0386614 INSPECTED THE LH WING CENTER FLAP RIB UPR FLANGE OF RIB15 BETWEEN STGR2.5 AND FRONT SPAR AND REPAIRED THE BOTTOM SKIN POCKET CUT OUT
- [SDR FDEA202603010295](https://openairdocs.org/sdr/FDEA202603010295.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 6EA CRACKS AT RIB16 BETWEEN STGR2.7 AND STGR2.8, RIB17 BETWEEN STGR2.8 AND REAR SPAR, RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6
- [SDR FDEA202603010294](https://openairdocs.org/sdr/FDEA202603010294.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 5EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.7 AND REAR SPAR, RIB27 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGES 5EA CR
- [SDR FDEA202603010293](https://openairdocs.org/sdr/FDEA202603010293.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK OF RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH
- [SDR FDEA202602250278](https://openairdocs.org/sdr/FDEA202602250278.md): Skin · chafed · Feb 25, 2026 · N746FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH WING INNER FLAP UPR SKIN FOUND CHAFE MARKS BETWEEN RIB16 AND RIB17. REPAIRED THE DAMAGED UPR SKIN IN RH WING INNER FLAP BETWEEN RIB16 AND RIB17 PER SRM57-50-00-201 PARA.4E. TRACKING EA 6-5750-T0386734 RAISED AND ACCOMPLISHED. REPAIR. MAJOR REPAIR IAW GMM
- [SDR FDEA202602210372](https://openairdocs.org/sdr/FDEA202602210372.md): Actuator · faulted · Feb 21, 2026 · N746FD · Airbus A300B4622R · Cargo/Baggage 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. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAI
- [SDR FDEA202511222198](https://openairdocs.org/sdr/FDEA202511222198.md): Warning Light · failed · Nov 22, 2025 · N746FD · Airbus A300B4622R · Door Warning System
  > INCOMING WALKAROUND INSPECTION FOUND LEFT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHTS INOP. ASSOCIATED WARNING BUZZER OPERATES NORMAL. AMM: 52-73-11-04-01 AMM: 52-22-13-04 REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT, WITH
- [SDR FDEA202511202193](https://openairdocs.org/sdr/FDEA202511202193.md): Light · failed · Nov 20, 2025 · N746FD · Airbus A300B4622R · Door Warning System
  > INCOMING WALKAROUND INSPECTION FOUND LT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM, LIGHTS INOPERATIVE. ASSOCIATED WARNING BUZZER OPERATES NORMALLY. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT WITH NEW UNIT FROM STOCK. OPS TESTED GOOD
- [SDR FDEA202407311070](https://openairdocs.org/sdr/FDEA202407311070.md): Pitot Head · obstructed · Jul 31, 2024 · N746FD · Airbus A300B4622R · Pitot/Static System
  > REPEAT DISCREPANCY, NO AIRSPEED INDICATION ON FO PFD DURING INITIAL TAKEOFF ROLL. REJECTED THE TAKEOFF. INSPECTED F/O'S PITOT PROBE IAW AMM 34-11-15-06, IT APPEARS TO BE METALLIC DEBRIS IN THE PROBE. PROBE NIS. F/O PITOT PROBE CLOGGED. REMOVED AND REP
- [SDR FDEA202308151427](https://openairdocs.org/sdr/FDEA202308151427.md): Splice · cracked · Aug 15, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > COMPLY WITH EO 6-5310-7-5023 A PT1 REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18L 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 PT1 REPLACED THE CRACKED
- [SDR FDEA202307271315](https://openairdocs.org/sdr/FDEA202307271315.md): Unknown · unknown · Jul 27, 2023 · N746FD · Airbus A300* · Nacelle/Pylon Structure
  > LEFT HAND PYLON - FOUND EXISTING REPAIR AT LOWER SPAR BETWEEN RIB 9 AND RIB 10 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA. THE EXISTING REPAIR ON LT PYLON LOWER SPAR BETWEEN RIB 9 & RIB 10 WAS EVALUATED & FOUND IN CONFORMITY WITH DWG: 41R54600029
- [SDR FDEA202307261304](https://openairdocs.org/sdr/FDEA202307261304.md): Pressure Deck · corroded · Jul 26, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > BAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION AT Y2462 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, Y2462 PER A300-600 SRM51-40-21 AND EA:6-5310-T0375709 P
- [SDR FDEA202307261303](https://openairdocs.org/sdr/FDEA202307261303.md): Pressure Deck · unknown · Jul 26, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > BAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION BETWEEN -Y450 AND -Y953 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, -Y450~-Y953 PER A300-600 SRM51-40-21 AND
- [SDR FDEA202307261302](https://openairdocs.org/sdr/FDEA202307261302.md): Fitting · cracked · Jul 26, 2023 · N746FD · Airbus A300* · Wing Main, Frame Structure
  > INSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH FOUND CRACK SIGNAL IN THE UPR SECOND CRACK STOP HOLE REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH PER A300-600 SRM 51-40-21 & EA: 6-5710-161345
- [SDR FDEA202307261301](https://openairdocs.org/sdr/FDEA202307261301.md): Fitting · cracked · Jul 26, 2023 · N746FD · Airbus A300* · Wing Main, Frame Structure
  > INSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH FOUND CRACK SIGNAL REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH PER A300-600 SRM51-40-21 & EA:6-5710-T0375488 P1. REPAIR IS CAT A REPAIR.MAJOR R
- [SDR FDEA202307261300](https://openairdocs.org/sdr/FDEA202307261300.md): Unknown · unknown · Jul 26, 2023 · N746FD · Airbus A300* · Cargo/Baggage Doors
  > FWD CARGO DOOR ACTUATOR ATTACH FITTING AT FR22A FOUND CRACK
- [SDR FDEA202307261299](https://openairdocs.org/sdr/FDEA202307261299.md): Floorbeam · cracked · Jul 26, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > AFT CARGO FLOOR CROSSBEAM FOUND CORROSION AT FR62, -Y140 ~ -Y805. REPAIRED THE AFT CARGO CORRODED FLOOR CROSSBEAM AT FR62 -Y140 ~ -Y805 PER A300-600 SRM 53-10-15 PARA.9. THIS IS CAT.A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202307261298](https://openairdocs.org/sdr/FDEA202307261298.md): Door · cracked · Jul 26, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPAIRED THE CRACKED FRAME SEGMENT OF RH FWD PAX DOOR AT FR14C PER A300-600 SRM51-40-21 AND AIRBUS DRAWING F52181297 ISSUE: K & F52181299 ISSUE: A. THIS IS CAT A REPAIR. TRACKING EA:6-5210-T0375409
- [SDR FDEA202307261297](https://openairdocs.org/sdr/FDEA202307261297.md): Frame · cracked · Jul 26, 2023 · N746FD · Airbus A300* · Fuselage Main, Structure
  > RH AFT PAX DOOR FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH FOUND 1EA CRACK. REPAIRED RH AFT PAX DOOR CRACKED FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH PER SRM51-40-21 & EA 6-5310-T0375247 P1.TITLE:FUSELAGE - MAINFRAME - CRACK FOUND ON RH DOOR FRAME F
- [SDR FDEA202307191278](https://openairdocs.org/sdr/FDEA202307191278.md): Seat Track · unknown · Jul 19, 2023 · N746FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR74 - FR75, -Y1137.1 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM SUPPLEMENT 53-10-16 FIG.202. EO 6-5100-7-5000 D7 PT1 WAS COMPLETED, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR ID
- [SDR FDEA202112233122](https://openairdocs.org/sdr/FDEA202112233122.md): Pump · failed · Dec 23, 2021 · N746FD · Airbus A300* · Hydraulic Accumulator, Auxiliary
  > PDIS 746 29-21 2913 23DEC21 IND OPEN U AFTER GEAR RETRACTION AROUND 2500 IN THE INITIAL CLIMB, WE GOT GREEN HYD PUMP #2 LO PR, COMPLIED WITH ECAM AND TURNED OFF. FOLLOWED QRH AND USED ELECTRIC PUMPS FOR APPROACH WITH MANUAL GEAR EXTENSION.
- [SDR FDEA202112223118](https://openairdocs.org/sdr/FDEA202112223118.md): None · none · Dec 22, 2021 · N746FD · Airbus A300* · Hydraulic Power System
  > PDIS 746 29-21 2911 22DEC21 MEM OPEN U DEPARTING KMEM27 AT APPROX 100 KNTS LOST GREEN SYSTEM HYDRAULIC PUMPS. NO APPARENT LOSS OF FLUID, JUST PSI. COMPLETE LOSS OF GREEN SYSTEM PRESSURE. ABLE TO RECOVER GREEN SYSTEM WITH PTU S. INFO 22DEC21 13:
- [SDR FDEA202103230743](https://openairdocs.org/sdr/FDEA202103230743.md): Floor Panel · damaged · Mar 23, 2021 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 251DL FOUND PUNCTURE REPAIRED THE MDCC 251DL PUNCTURED FLOOR PANEL AT FR57 - FR57.1 PER A300-600 SRM 53-10-20-201 PARA.9.A. AND INSTALLED THE MDCC FLOOR PANEL 251DL PER AMM 53-10-25-04- 02. THIS REPAIR CATEGORY AS "A". MAJOR REPAIR IAW FEDE
- [SDR FDEA202103200731](https://openairdocs.org/sdr/FDEA202103200731.md): Stringer · damaged · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > 3EA STRINGERS AT STGR50R, 51R, 52R BETWEEN FR67-68 FOUND DOUBLE HOLES AND DEFORMATION REPAIRED DOUBLE HOLES AND DEFORMATION OF 3EA STRINGERS AT STGR50R, 51R, 52R BETWEEN FR67-68 PER EA6-5310-T0360050 P1 & A300-600 SRM 51-40-21 & SRM 53-10-14 FIG.201. THI
- [SDR FDEA202103200730](https://openairdocs.org/sdr/FDEA202103200730.md): Skin · dented · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN FR67-FR68, STGR49R-STGR50R 1EA DENT REPAIRED THE DENT AT LOWER FUSELAGE SKIN FR67 - FR68, STGR49R - STGR50R PER EA 6- 5310-T0360050 P1 & A300-600 SRM 51-40-21 & SRM 51-40-30. THIS IS A CAT B REPAIR. THE FURTHER INSTPECTION REQUIREMENT PE
- [SDR FDEA202103200726](https://openairdocs.org/sdr/FDEA202103200726.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - LH #4 GANTRY OUTBD FLANGE FR49.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #4 GANTRY OUTBD FLANGE FR49.1 PER AIRBUS DWG: R53810581 ISSUE:C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-
- [SDR FDEA202103200724](https://openairdocs.org/sdr/FDEA202103200724.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - RH #4 GANTRY OUTBD FLANGE FR52.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #4 GANTRY OUTBD FLANGE FR52.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2
- [SDR FDEA202103200722](https://openairdocs.org/sdr/FDEA202103200722.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - LH #2 GANTRY OUTBD FLANGE FR52.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #2 GANTRY OUTBD FLANGE FR52.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2
- [SDR FDEA202103200721](https://openairdocs.org/sdr/FDEA202103200721.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - LH #2 GANTRY OUTBD FLANGE FR51.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #2 GANTRY OUTBD FLANGE FR51.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2
- [SDR FDEA202103200720](https://openairdocs.org/sdr/FDEA202103200720.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR50.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR50.1 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-1
- [SDR FDEA202103200719](https://openairdocs.org/sdr/FDEA202103200719.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR49.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR49.1 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-1
- [SDR FDEA202103200718](https://openairdocs.org/sdr/FDEA202103200718.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR49 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR49 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR FDEA202103200717](https://openairdocs.org/sdr/FDEA202103200717.md): Frame · cracked · Mar 20, 2021 · N746FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT FOUND FUSELAGE - MAINFRAME - RH #5 GANTRY INBD FLANGE FR51.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #5 GANTRY INBD FLANGE FR51A PER AIRBUS DWG: R53810583 ISSUE: D. THIS REPAIR IS CAT.A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202103150651](https://openairdocs.org/sdr/FDEA202103150651.md): Skin · delaminated · Mar 15, 2021 · N746FD · Airbus A300B4622R · Spoilers
  > LH WING 4# SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION, SIZE: 30MM * 30MM D:1.9MM PERFORMED THE REPAIR ON LH WING 4# SPOILER CENTER O/B HINGE ARM LOWER SURFACE PER EA #:6-5750-T0360096 P1, TITLE: WING - FLIGHT SURFACE - LH 4# SPOILER
- [SDR FDEA202101190156](https://openairdocs.org/sdr/FDEA202101190156.md): Proximity Sensor · failed · Jan 19, 2021 · N746FD · Airbus A300B4622R · Landing Gear Door Retract Section
  > ON GEAR RETRACTION, NLG DOOR INDICATOR ILLUMINATED ON BOTH GEAR INDICATOR PANELS. COMPLIED WITH QRH AND RETURNED TO AFW. PROXIMITY BOX SHOWING CODE 32 W/ BOX FAULT LIGHT ON. T/S PER A300 TSM 32-30-00. BITE TEST PROXIMITY DETECTOR PROCESSING UNIT (54GB), PE
- [SDR FDEA2019041640793](https://openairdocs.org/sdr/FDEA2019041640793.md): Aileron · stuck · Apr 14, 2019 · N746FD · Airbus A300B4622R · Aileron Control System
  > ON TAXI OUT DURING FLIGHT CONTROL CHECK, LEFT AILERON INDICATOR STUCK IN FULL UP POSITION. SEVERAL MORE MOVEMENTS OF THE AILERON AND THE INDICATOR SHOWS FULL DOWN POSITION WHILE AILERONS CONTROL ARE IN THE NEUTRAL POSITION.
- [SDR FDEA201812063443](https://openairdocs.org/sdr/FDEA201812063443.md): Adc · malfunctioned · Dec 6, 2018 · N746FD · Airbus A300B4622R · Air Data Computer
  > PASSING 9000FT SEVERAL FAILURES ADC 2 BOTH PITCH TRIMS BOTH YAW DAMPENERS ALL F/O INDICATIONS OF AIRSPEED ALTITUDE GPS1 ATS. UPDATE A/C BACK AT GATE ENTERED E& E COMPARTMENT STRONG SMELL OF ELECTRICAL ODOR SOMETHING BURNING OR OVERHEATING. CHECKED COMPONENTS O
- [SDR FDEA201811103178](https://openairdocs.org/sdr/FDEA201811103178.md): Warning System · false activation · Nov 10, 2018 · N746FD · Airbus A300B4622R · Door Warning System
  > L1 DOOR RED LIGHT FLASHED DURING FLIGHT, AS REPORTED BY JUMPSEATER. NO PRESSURIZATION O2 COCKPIT INDICATIONS NOTED. PERFORMED OPS CHECK OF DOOR WARNING SYSTEM IAW AMM 52-73-11-04-08. NO FAULTS NOTED. NO 90 HISTORY. ACFT OF FOR SERVICE.
- [SDR FDEA201809182581](https://openairdocs.org/sdr/FDEA201809182581.md): Floor Panel · delaminated · Sep 18, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221RF DELAMINATED. FLOOR PANEL 221RF FABRICATED ON T18/1362586 IAW SRZ 25-005, REPAIR IS CLASSIFED AS CAT "A" AND MAJOR REPAIR.
- [SDR FDEA2018091872561](https://openairdocs.org/sdr/FDEA2018091872561.md): Floor Panel · delaminated · Sep 17, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222NF DELAMINATED. FLOOR PANEL 222NF FABRICATED ON T18/1362587, CLASSIFIED AS CAT "A" AND MAJOR REPAIR IAW SRZ 25-005.
- [SDR FDEA2018091432520](https://openairdocs.org/sdr/FDEA2018091432520.md): Adapter · worn · Sep 13, 2018 · N746FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > WORN SEAT TRACK ADAPTER AT FR 62 BETWEEN -Y953 TO -Y1456. REMOVED WORN SEAT TRACK ADAPTER IAW SRM 51-40-21. LOCATED AND DRILLED NEW SEAT TRACK ADAPTER IAW SRM 51-40-00, INSTALLED NEW SEAT TRACK ADAPTER IAW SRM 51-40-21, REPAIR IS CLASSIFED AS CAT "A" AND MAJOR
- [SDR FDEA2018091432487](https://openairdocs.org/sdr/FDEA2018091432487.md): Floor Panel · broken · Sep 13, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > ROLLER TRAY PANEL 131HG FWD PIT IS BROKEN INTO PIECES. FABRICATED FLOOR PANEL 131 HG ON T18/1363243 PER SRZ 25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2018091432486](https://openairdocs.org/sdr/FDEA2018091432486.md): Floor Panel · delaminated · Sep 13, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > FLOOR PANEL 152KF AFT PIT IS DAMAGED. FABRICATED FLOOR PANEL 152KF ON T18/1363818 PER SRZ 25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2018091432485](https://openairdocs.org/sdr/FDEA2018091432485.md): Floor Panel · cracked · Sep 13, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > FLOOR PANEL 151EF AFT PIT IS BROKEN IN TWO. FABRICATED FLOOR PANEL 151 EF ON T18/1363152 PER SRZ 25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2018091422484](https://openairdocs.org/sdr/FDEA2018091422484.md): Floor Panel · damaged · Sep 12, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > PANEL 152CF AFT PIT IS DAMAGED. FABRICATED FLOOR PANEL 152CF ON T18/1363046 PER SRZ 25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA2018091422483](https://openairdocs.org/sdr/FDEA2018091422483.md): Floor Panel · delaminated · Sep 12, 2018 · N746FD · Airbus A300B4622R · Fuselage Floor Panel
  > PANEL 161HF BULK CARGO IS DAMAGED. FABRICATED FLOOR PANEL 161HF ON T18/1365001 PER SRZ 25-005 CAT "A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N746FD/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 = 'N746FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N746FD/reports

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