# Service difficulty reports: N722FD

A list on [N722FD](https://openairdocs.org/aircraft/N722FD.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 · 191 reports

- [SDR FDEA202608271240](https://openairdocs.org/sdr/FDEA202608271240.md): Adapter · damaged · Aug 27, 2026 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > RAMP ONLOAD CREW REPORTS A RESTRAINT SEPERATED FROM THE FLOOR ON THE FORWARD SIDE OF 13C IN MAIN CARGO. BESIDES THE BROKEN FLOOR TRACK LOBES-NO OTHER DAMAGE FOUND ON THE FLOOR TRACK OR ADJACENT FLOOR PANELS. OIL LBB NO RESTRICTION IAW DWG SR30-53-003.
- [SDR FDEA202604120430](https://openairdocs.org/sdr/FDEA202604120430.md): Bottle · leaking · Apr 12, 2026 · N722FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > ON TAKEOFF OUT OF SNA WHEN WE RETRACTED THE GEAR THERE WAS A LOUD GRINDING SOUND AND EXCESSIVE VIBRATIONS. IN MEM ON FINAL WHEN WE SELECTED GEAR DOWN THERE WERE VIBRATIONS AND THE GEAR DID NOT EXTEND. THE DOORS SHOWED OPEN. ON THE GO AROUND THE GEAR CAME
- [SDR FDEA202602140219](https://openairdocs.org/sdr/FDEA202602140219.md): Elec Connector · dirty · Feb 14, 2026 · N722FD · Airbus A300B4622R · Equipment/Furnishings Wiring
  > WHEN R1 SLIDE ARMED NO INDICATION ON ECAM OF SLIDE BEING ARMED. AMM: 52-73-13-05-01 CLEANED CONNECTOR AT ESCAPE SLIDE ARM SWITCH 14WN PER ESPM 20-55-50-0. PERFORMED ADJUSTMENT TEST OF ESCAPE SLIDE IAW AMM 52-73-13-05-01. OPS CHECKS GOOD OK FOR SERVIC
- [SDR FDEA202506170977](https://openairdocs.org/sdr/FDEA202506170977.md): Repair · no discrepancy · Jun 17, 2025 · N722FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. EO 6-5100-7-5000
- [SDR FDEA202506141065](https://openairdocs.org/sdr/FDEA202506141065.md): Skin · cracked · Jun 14, 2025 · N722FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > LWR FUSELAGE SKIN LAP JOINT AROUND FASTENER AT FR53-54, S44L FOUND CRACK. COMPLIED WITH EA:6-5330-T0383917 P1 REPAIRED LWR FUSELAGE THE CRACKED SKIN LAP JOINT AROUND FASTENER AT FR53-54,S44L. EA TITLE: FUSELAGE - PLATES & SKINS - CRACKED HOLES ON SKIN PANE
- [SDR FDEA202506140976](https://openairdocs.org/sdr/FDEA202506140976.md): Flap · misrepaired · Jun 14, 2025 · N722FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON LT O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. RE-REPAIRE
- [SDR FDEA202506130997](https://openairdocs.org/sdr/FDEA202506130997.md): Skin · delaminated · Jun 13, 2025 · N722FD · Airbus A300B4622R · Spoilers
  > RH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 30MM*10MM, DEPTH: 1.34MM COMPLIED WITH EA 6-5750-T0383788 P1 TO REPAIR RH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE: WING - FLIGHT
- [SDR FDEA202506130996](https://openairdocs.org/sdr/FDEA202506130996.md): Skin · delaminated · Jun 13, 2025 · N722FD · Airbus A300B4622R · Spoilers
  > RH WING #3 SPOILER CENTER I/B & O/B HINGE ARMS OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: (1)80MM*40MM, DEPTH: 1.3MM (2)80MM*40MM, DEPTH: 1.4MM COMPLIED WITH EA 6-5750-T0383786 P1 TO REPAIR RH WING #3 SPOILER CENTER I/B & O/B HINGE ARMS OUTSIDE SURFACE
- [SDR FDEA202506130995](https://openairdocs.org/sdr/FDEA202506130995.md): Skin · delaminated · Jun 13, 2025 · N722FD · Airbus A300B4622R · Spoilers
  > LH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.37MM COMPLIED WITH EA 6-5750-T0383770 P1 TO REPAIR LH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE: WING - FLIGHT
- [SDR FDEA202506130994](https://openairdocs.org/sdr/FDEA202506130994.md): Skin · delaminated · Jun 13, 2025 · N722FD · Airbus A300B4622R · Spoilers
  > LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 90MM*10MM, DEPTH: 1.56MM COMPLIED WITH EA 6-5750-T0373146 A P2 TO REPAIR LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE:WING - FLIGH
- [SDR FDEA202506130975](https://openairdocs.org/sdr/FDEA202506130975.md): Repair · no discrepancy · Jun 13, 2025 · N722FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000
- [SDR FDEA202506130974](https://openairdocs.org/sdr/FDEA202506130974.md): Repair · no discrepancy · Jun 13, 2025 · N722FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000
- [SDR FDEA202506130973](https://openairdocs.org/sdr/FDEA202506130973.md): Repair · no discrepancy · Jun 13, 2025 · N722FD · Airbus A300B4622R · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND FR68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-500
- [SDR FDEA202506061126](https://openairdocs.org/sdr/FDEA202506061126.md): Fitting · not reported · Jun 6, 2025 · N722FD · Airbus A300B4622R · Cargo/Baggage Doors
  > 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 B P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. TH
- [SDR FDEA202506061128](https://openairdocs.org/sdr/FDEA202506061128.md): Crossbeam · corroded · Jun 6, 2025 · N722FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO FLOOR BEAM CORRODED, AT FR56,Y805-Y1470. REPAIRED THE CORRODED FLOOR BEAM AT AFT CARGO FR56,Y805-Y1470 PER A300-600 SRM53- 10-15-201 FIGURE 207 & EA 6-5321-T0383821 P1. EA TITLE:FUSELAGE - CARGO COMP FLOOR - AFT CARGO FRAME 56 CROSSBEAM - SRM REPA
- [SDR FDEA202412101784](https://openairdocs.org/sdr/FDEA202412101784.md): Limit Switch · dirty · Dec 10, 2024 · N722FD · Airbus A300B4622R · Service Doors
  > R1 DOOR WILL NOT ARM. CLEANED THE 14WN LIMIT SWITCH ON THE RH DOOR IAW AMM 52-73-13-05-01. OPS CHECK GOOD AT THIS TIME. ACFT OK FOR SERVICE.
- [SDR FDEA202406030773](https://openairdocs.org/sdr/FDEA202406030773.md): Power Supply · inoperative · Jun 3, 2024 · N722FD · Airbus A300B4622R · Escape Slide
  > BOTH R1 AND L1 DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHT TEST FAILED - AUDIBLE BUZZERS WORK ON BOTH DOORS. CHECKING ASPSU TEST SWITCH RESULTED IN NO LIGHTS AT ALL - BOTH BATTERIES APPEAR DISCHARGED. - REMOVED AND REPLACED BOTH BATTERIES IAW AMM 52-
- [SDR FDEA202303080392](https://openairdocs.org/sdr/FDEA202303080392.md): Aileron · dented · Mar 8, 2023 · N722FD · Airbus A300* · Wing, Control Surfaces
  > LH WING AILERON TRAILING EDGE WEDGE UPPER SURFACE FOUND SMALL DENTS COMPLIED WITH EA: 6-5750-T0373267 P1. TITLE: WING - FLIGHT SURFACES - LH AILERON TRAILING EDGE WEDGE UPPER SURFACE REPAIR. AND REFER TO A300-600 SRM51-77-12-201 PARA.4.B FIGURE 218 & AMM57
- [SDR FDEA202303030370](https://openairdocs.org/sdr/FDEA202303030370.md): Spar · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · Nacelle/Pylon Structure
  > RH PYLON LWR SPAR FOUND CRACK BETWEEN RIB6 AND RIB7 AT STIFFENER END BY EDDY CURRENT INSPECTION COMPLID WITH EA: 6-5450-T0373394 P1. TITLE: NACELLES/PYLON - WING PYLON/STRUT - #2 ENGINE PYLON LOWER SPAR CRACK BETWEEN RIB 6&7 - REPAIR. REPAIRED THE RH PYLON
- [SDR FDEA202303030369](https://openairdocs.org/sdr/FDEA202303030369.md): Fitting · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · Wing Main, Frame Structure
  > RH WING CENTER SPAR TO RIB 1 SPLICE VERTICAL FLANGE 1EA FASTENER HOLE(TYPE 5) FOUND CRACK SIGNAL BY ULTRASONIC INSPECTION COMPLIED WITH EA: 6-5710-T0373257 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE ON FITTING RH WING CWT SPAR TO RIB1. REPAIRED T
- [SDR FDEA202303030368](https://openairdocs.org/sdr/FDEA202303030368.md): Panel · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · 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 FDEA202303030367](https://openairdocs.org/sdr/FDEA202303030367.md): Panel · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · Nacelle/Pylon Structure
  > LH PYLON I/B SIDE PANEL AT RIB8 FOUND 1EA CRACK. REPAIRED THE CRACKED LH PYLON I/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 FDEA202303030366](https://openairdocs.org/sdr/FDEA202303030366.md): Frame · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · Fuselage Main, Structure
  > FUSELAGE INTERNAL STRUCTURE - FRAME 14 FOUND CRACK SIGNAL AT JUNCTION AREA OF MAIN DECK FLOOR BEAM AND CRUCIFORM FITTING, RH SIDE, BY ULTRASONIC INSPECTION COMPLIED WITH EA: 6-5310-T0373313 P1. TITLE: FUSELAGE - MAINFRAME - CRACK HOLE FOUND ON FRAME 14 STR
- [SDR FDEA202303030365](https://openairdocs.org/sdr/FDEA202303030365.md): Spoiler · delaminated · Mar 3, 2023 · N722FD · Airbus A300B4622R · Wing, Control Surfaces
  > LH WING #3 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 40MM*10MM, DEPTH: 1.7MM COMPLIED WITH EA: 6-5750-T0373146 P1. TITLE: WING - FLIGHT SURFACES - LH 3# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WI
- [SDR FDEA202303030364](https://openairdocs.org/sdr/FDEA202303030364.md): Door · cracked · Mar 3, 2023 · N722FD · Airbus A300B4622R · Passenger/Crew Doors
  > RH FWD CREW/COURIER DOOR INTERNAL STRUCTURE FRAME SEGMENT AT FR14C FOUND 2EA CRACKS REPLACED RH FWD CREW/COURIER DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: A52111406 (ISSUE.C), A52111327(ISSUE.E). TRACKIN
- [SDR FDEA202303030363](https://openairdocs.org/sdr/FDEA202303030363.md): None · none · Mar 3, 2023 · N722FD · Airbus A300B4622R · Passenger/Crew Doors
  > LH FWD CREW/COURIER DOOR INTERNAL STRUCTURE FRAME SEGMENT AT FR14C FOUND 1EA CRACK
- [SDR FDEA202205121190](https://openairdocs.org/sdr/FDEA202205121190.md): Selector Valve · unknown · May 12, 2022 · N722FD · Airbus A300* · Tire
  > MDIS 722 32-44 2658 12MAY22 MEM OPEN U PER FLIGHT CREW: ON TAXI OUT, HOLDING SHORT OF RUNWAY, PARKING BRAKE WAS SET AND INDICATED PARKING BRAKE ON ON ECAM, HOWEVER WHEN BRAKE PEDALS WERE RELEASED A/C MOVED FORWARD. RECYCLED PARKING BRAKE 4
- [SDR FDEA202203300785](https://openairdocs.org/sdr/FDEA202203300785.md): None · none · Mar 30, 2022 · N722FD · Airbus A300B4622R · Emergency Exits
  > R1 CABIN DOOR DOES NOT INDICATE ARMED ON ECAM. ALL OTHER INDICATIONS ARE NORMAL. REMOVED POWER FROM ASPCU. AFTER PUTTING POWER BACK ON ASPCU, PERFORMED OPERATIONAL TEST OF R1 AND L1 DOORS ARM FUNCTION AND ALL INDICATIONS WORK PROPERLY AT THIS TIME. O
- [SDR FDEA202203080470](https://openairdocs.org/sdr/FDEA202203080470.md): None · leaking · Mar 8, 2022 · N722FD · Airbus A300* · Hydraulic Power System
  > ABOUT 5 TO 10 MINUTES IN CRUISE FLIGHT AT FL340 I NOTICED WITH MY OVERHEAD SCAN THAT THE GREEN HYD QUANTITY WAS MID WAY IN THE YELLOW. I THEN LOOKED AT THE GREEN HYDRAULICS ON THE ECAM AT IT SHOWED 440 PSI. FROM THERE IT WAS A FEW MINUTES AND WE GOT THE EC
- [SDR FDEA202012103112](https://openairdocs.org/sdr/FDEA202012103112.md): Battery Pack · dislodged · Dec 10, 2020 · N722FD · Airbus A300B4622R · Escape Slide
  > DOOR 1R SLIDE HAS BATTERY PACK FALLING OUT OF SLIDE INTERFERING WITH GIRT BAR ENGAGEMENT. REASON CODE: REMOVAL FROM A/C ONLY, NO INSTALLATION OFF MPN: D30546-509FX CPN: 2513882 POS: R1 SRL: A5756 TAG NBR: 00F514. REMOVED ESCAPE SLIDE FROM DOOR 1R, PER
- [SDR FDEA202012083067](https://openairdocs.org/sdr/FDEA202012083067.md): Battery · detached · Dec 8, 2020 · N722FD · Airbus A300B4622R · Escape Slide
  > CABIN DOOR R-1 NO SLIDE INDICATION ON ECAM WHEN ATTEMPTED TO ARM DOOR FOR PUSHBACK. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CAT: C EXP: 14DEC20 "MEL 52-XX-XX-XX: CREW ENTRY DOOR ESCAPE SLIDE R1-INOPERABLE. SLIDE REMAINS INSTALLED ON DOOR. THIS MEL ITEM W
- [SDR FDEA202012053068](https://openairdocs.org/sdr/FDEA202012053068.md): Unknown · unknown · Dec 5, 2020 · N722FD · Airbus A300B4622R · Cargo Compartments
  > DURING APPROACH WHILE DECELERATING HEARD AND FELT A THUD. SUSPECT POSSIBLE LOAD SHIFT. RAMP REPORTED CAN UNSECURED IN LOWER FORWARD BELLY, ALLOWING CAN TO SHIFT BETWEEN LOCKS, APPROXIMATELY 5 FEET FORWARD AND AFT. PERFORMED INSPECTION ON PALLET LOCKS, NO DE
- [SDR FDEA202011022750](https://openairdocs.org/sdr/FDEA202011022750.md): Floor Panel · cracked · Nov 2, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT METAL FLOOR PANEL 131LG IS CRACKED. FABRICATED FLOOR PANEL 131LG ON VTMAE TRAVELER T20/1516757, IAW DWG A53272573, PART MARKED PANEL PER GMM 07-0-1001. CLASSIFIED AS CAT "A" AND MAJOR REPAIR.
- [SDR FDEA202011022749](https://openairdocs.org/sdr/FDEA202011022749.md): Floor Panel · cracked · Nov 2, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT METAL FLOOR PANEL 131NG IS CRACKED. FABRICATED FLOOR PANEL 131NG ON VTMAE TRAVELER T20/1516758, IAW DWG A53272579, PART MARKED PANEL, IAW GMM 07-0-1001, CLASSIFIED AS CAT "A" AND MAJOR REPAIR.
- [SDR FDEA202011022748](https://openairdocs.org/sdr/FDEA202011022748.md): Floorboard · damaged · Nov 2, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 240 FLOOR BOARD 241XG IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241XG ON VTMAE TRAVELER T20/1518620, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202011022746](https://openairdocs.org/sdr/FDEA202011022746.md): Floorboard · broken · Nov 2, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 260 FLOOR BOARD 261NF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 261NF ON VTMAE TRAVELER T20/1518281, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202011022745](https://openairdocs.org/sdr/FDEA202011022745.md): Floorboard · damaged · Nov 2, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 230 FLOOR BOARD 232TG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232TG ON VTMAE TRAVELER T20/1518299, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202010312737](https://openairdocs.org/sdr/FDEA202010312737.md): Floorboard · broken · Oct 31, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 252BH IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252BH ON VTMAE TRAVELER T20/1518269, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202010312736](https://openairdocs.org/sdr/FDEA202010312736.md): Floorboard · broken · Oct 31, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 260 FLOOR BOARD 261RF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 261RF ON VTMAE TRAVELER T20/1518266, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202010312735](https://openairdocs.org/sdr/FDEA202010312735.md): Floorboard · broken · Oct 31, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 251RH IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251RH ON VTMAE TRAVELER T20/1518289, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202010312734](https://openairdocs.org/sdr/FDEA202010312734.md): Floorboard · broken · Oct 31, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 252VF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252VF ON VTMAE TRAVELER T20/1518802 IAW DWG SRZ- 25-005R, MAJOR REPAIR.
- [SDR FDEA202010272666](https://openairdocs.org/sdr/FDEA202010272666.md): Floorboard · damaged · Oct 27, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 230 FLOOR BOARD 231SG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 231SG ON TRAVELER T20/1518654, IAW DWG SRZ-25-005R MAJOR REPAIR.
- [SDR FDEA202010272665](https://openairdocs.org/sdr/FDEA202010272665.md): Floorboard · damaged · Oct 27, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 252GF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252GF ON TRAVELER T20/1518616, IAW DWG SRZ-25-005R, MAJOR REPAIR.
- [SDR FDEA202010232625](https://openairdocs.org/sdr/FDEA202010232625.md): Floor Panel · damaged · Oct 23, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO COMPT FLOOR PANEL 132RF IS BROKEN. FABRICATED FLOOR PANEL 132RF ON VTMAE TRAVELER T20/1517566, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT "A" REPAIR, MAJOR REPAIR.
- [SDR FDEA202010232624](https://openairdocs.org/sdr/FDEA202010232624.md): Floor Panel · damaged · Oct 23, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO COMPT FLOOR PANEL 131RF IS BROKEN. FABRICATED FLOOR PANEL 131RF ON VTMAE TRAVELER T20/1517567, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT "A" REPAIR, MAJOR REPAIR.
- [SDR FDEA202010232623](https://openairdocs.org/sdr/FDEA202010232623.md): Floor Panel · cracked · Oct 23, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152LF HAS CRACK AND EDGE DAMAGE. FABRICATED FLOOR PANEL 152LF ON VTMAE TRAVELER T20/1519074, IAW DWG SRZ-25-005R. CLASSIFIED AND CATAGORY "A" REPAIR, MAJOR REPAIR.
- [SDR FDEA202010232622](https://openairdocs.org/sdr/FDEA202010232622.md): Floor Panel · damaged · Oct 23, 2020 · N722FD · Airbus A300B4622R · Fuselage Floor Panel
  > PANEL 151KF HAS NUMEROUS AREAS OF DAMAGE TO EDGES AND MISSING CORE. FABRICATED FLOOR PANEL 151KF ON VTMAE TRAVELER T20/1519073 IAW DWG SRZ-25-005R. CLASSIFIED AS CATAGORY "A" REPAIR, MAJOR REPAIR.
- [SDR FDEA202010222600](https://openairdocs.org/sdr/FDEA202010222600.md): Seat Track · gouged · Oct 22, 2020 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > DOT 66-59 MAIN CABIN SEAT TRACK BETWEEN FR 63-64, Y1456 HAVE GOUGED AREAS. REMOVED DAMAGE AT SEAT TRACK Y 1456 ON SCALLOP HOLE UPPER, IAW SRM 51-73-10. MAXIMUM ALLOWABLE MATERIAL REMOVE IS 0.840" AFTER REWORK IS 0.870" FOUND OUT OF LIMITS, IAW SRM 53-10-16 F
- [SDR FDEA202010222599](https://openairdocs.org/sdr/FDEA202010222599.md): Floor Support · corroded · Oct 22, 2020 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > (DOT 38-79) MDC FLOOR SUPPORT Y730 BETWEEN FR 13-FR 14 CORRODED. NO ESTABLISHED LIMITS, FOUND TO BE OUT LIMITS. FABRICATED FLOOR SUPPORT ON VTMAE TRAVELER T20/1518605, P/N FX-A53612213202, IAW SRM 53-12-15, MAT. NSA 343036, BATCH 3272259. LOCATED AND DRILL
- [SDR FDEA202008059477](https://openairdocs.org/sdr/FDEA202008059477.md): Switch · worn · Jul 9, 2020 · N722FD · Airbus A300B4622R · Door Warning System
  > R1 MAIN CABIN ENTRY DOOR SLIDE WILL NOT ARM. IAW TSM 52-70-00, CHECKED FOR GROUND AT R1 DOOR LIMIT SWITCHES. FOUND EXCESSIVE RESISTANCE AT PIN "E" OF LIMIT SWITCH 1 (42WS), AND OPEN FOUND AT PIN "E" OF LIMIT SWITCH 2 (8WS). NO TIME TO FURTHER TROUBLESHOOT DUE

Next page: https://openairdocs.org/aircraft/N722FD/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 = 'N722FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N722FD/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.