# Service difficulty reports: N744FD

A list on [N744FD](https://openairdocs.org/aircraft/N744FD.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 6 · 271 reports

- [SDR FDEA202511142182](https://openairdocs.org/sdr/FDEA202511142182.md): Diaphragm · damaged · Nov 14, 2025 · N744FD · Airbus A300B4622R · Passenger/Crew Doors
  > L1 DOOR EMERGENCY ASSIST BOTTLE PRESSURE LOW. REPLACED DIAPHRAGM (PN# FE240-221-001, SN# N/A) IN THE PERCUSSION MECHANISM OF THE L1 DOOR ASSIST CYLINDER. NO PRESSURE DROP AFTER 4 HRS. LEAK CKS GOOD. REMOVED FROM MEL.
- [SDR FDEA202508121409](https://openairdocs.org/sdr/FDEA202508121409.md): Selector Valve · faulted · Aug 12, 2025 · N744FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. L/G RETRACTION FAULT ON ECAM. EMERGENCY DECLARED. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. AMM: 32-31-12-04, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE 3GA, OPS AND LEAK CHECK GOOD IAW ABOVE AM
- [SDR FDEA202506050846](https://openairdocs.org/sdr/FDEA202506050846.md): Slide Raft · not reported · Jun 5, 2025 · N744FD · Airbus A300B4622R · Escape Slide
  > LH #1 PASSENGER / CREW DOOR SLIDE / RAFT REPLACEMENT. PER AMM 25-61-22-04-01 REMOVED THE SLIDE / RAFT OF L1 PASSENGER / CREW DOOR (CPN: 2513882 MPN: D30546-509FX SN: A5687 POS: L1) PER AMM 25-61-22-04-01 INSTALLED THE SLIDE / RAFT OF L1 PASSENGER / CR
- [SDR FDEA202505290890](https://openairdocs.org/sdr/FDEA202505290890.md): Rib · cracked · May 29, 2025 · N744FD · Airbus A300B4622R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0383581 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP RIB 15 UPPER FLANGE AND BOTTOM SKIN REPAIR - RSC TRACKING. AND PER A300-600 SRM 57-50-
- [SDR FDEA202505290889](https://openairdocs.org/sdr/FDEA202505290889.md): Rib · cracked · May 29, 2025 · N744FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB13 BETWEEN STGR2.6 AND STGR2.7 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIR
- [SDR FDEA202505290888](https://openairdocs.org/sdr/FDEA202505290888.md): Rib · cracked · May 29, 2025 · N744FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB26 B/W STGR2.6 AND STGR2.8 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIRE
- [SDR FDEA202505290817](https://openairdocs.org/sdr/FDEA202505290817.md): Fitting · failed insp · May 29, 2025 · N744FD · Airbus A300B4622R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 4EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0383430. TITLE: DOORS - CARGO DOOR/HYD SYS - CRACKED HOLES ON MAIN DECK CARGO DOOR UPPER LONGERON. REPAIRED THE MAIN DECK CARGO
- [SDR FDEA202505290816](https://openairdocs.org/sdr/FDEA202505290816.md): Fitting · failed insp · May 29, 2025 · N744FD · Airbus A300B4622R · Cargo/Baggage Doors
  > COMPLY 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. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARG
- [SDR FDEA202505290815](https://openairdocs.org/sdr/FDEA202505290815.md): Door Frame · cracked · May 29, 2025 · N744FD · Airbus A300B4622R · Fuselage Main, Structure
  > LH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED LH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299(ISSUE: A). RSC TRACKING EA 6-5210-T0383529 RAISED AND ACC
- [SDR FDEA202505290814](https://openairdocs.org/sdr/FDEA202505290814.md): Door Frame · cracked · May 29, 2025 · N744FD · Airbus A300B4622R · Fuselage Main, Structure
  > RT FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299(ISSUE: A). RSC TRACKING EA 6-5210-T0383528 RAISED AND ACC
- [SDR FDEA202505260812](https://openairdocs.org/sdr/FDEA202505260812.md): Skin · delaminated · May 26, 2025 · N744FD · Airbus A300B4622R · Spoilers
  > LH WING #5 SPOILER CENTER O/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 63MM* 40MM, DEPTH: 1.56MM COMPLIED WITH EA: 6-5750-T0383369 P1, TITLE: WING - FLIGHT SURFACES - LH #5 SPOILER TOP SKIN UPPER SURFACE DELAMINATION ABOVE CENTER HINGE ARM. AND PER
- [SDR FDEA202505260811](https://openairdocs.org/sdr/FDEA202505260811.md): Skin · delaminated · May 26, 2025 · N744FD · Airbus A300B4622R · Spoilers
  > RH WING #5 SPOILER CENTER I/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 35MM* 13MM, DEPTH: 1.50MM; CENTER O/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 95MM*45MM, DEPTH: 1.45MM COMPLIED WITH EA: 6-5750-T0383370 P1, TITLE: WING - FLIGHT SURFACES
- [SDR FDEA202505200781](https://openairdocs.org/sdr/FDEA202505200781.md): Skin · damaged · May 20, 2025 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NDT INSP FOUND RH ELEVATOR INBD UPPER SURFACE TRAPPED WATER AS MARK COMPLIED WITH EA: 6-5520-T0383449 P1, EA TITLE: STABILIZERS - ELEVATORS - RH ELEVATOR UPPER SKIN WATER INGRESS REPAIR, AND A300-600 SRM55-21-12-201 PARA.5.J FIGURE 212 REPAIRED RH ELEVATOR
- [SDR FDEA202505200780](https://openairdocs.org/sdr/FDEA202505200780.md): Skin · damaged · May 20, 2025 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NDT INSP FOUND RH ELEVATOR MID UPPER SURFACE TRAPPED WATER AS MARK COMPLIED WITH EA: 6-5520-T0383449 P1, EA TITLE: STABILIZERS - ELEVATORS - RH ELEVATOR UPPER SKIN WATER INGRESS REPAIR, AND A300-600 SRM55-21-12-201 PARA.5.J FIGURE 212 REPAIRED RH ELEVATOR
- [SDR FDEA202501130062](https://openairdocs.org/sdr/FDEA202501130062.md): Bottle · low pressure · Jan 13, 2025 · N744FD · Airbus A300B4622R · Service Doors
  > R-1 DOOR DAMPER NEEDS TO BE SERVICE. SERVICED R1 DOOR DAMPER TO WITHIN LIMITS PER AMM 52-10-14-03-01 STEP 3.D.(12).
- [SDR FDEA202501100056](https://openairdocs.org/sdr/FDEA202501100056.md): Bottle · no test · Jan 10, 2025 · N744FD · Airbus A300B4622R · Emergency Equipment
  > WHILE OPENING R1 DOOR HEAR SIGNIFICANT POP SOUND. CLOSER INSPECTION FOUND BOLT THAT ATTACHES ASSIST CYLINDER TO FITTING FOR SNAPPED OFF( APPEARS TO HAVE AXIAL FATIGUE CRACK SEE PIC), ASSIST BOTTLE IS IN NORMAL OPPERATION RANGE, AND NO OTHER DEFECTS NOTED.
- [SDR FDEA202501070031](https://openairdocs.org/sdr/FDEA202501070031.md): Bottle · low pressure · Jan 7, 2025 · N744FD · Airbus A300B4622R · Emergency Exits
  > L1 EMERGENCY DAMPER CYLINDER BELOW MIN CHARGE. AMM 52-10-14-03-01 SERVICED L1 DAMPER CYLINDER PER PLACARD AND ABOVE AMM 52-10-14-03-01 STEP 3.D.(12)
- [SDR FDEA202412201821](https://openairdocs.org/sdr/FDEA202412201821.md): Battery · no test · Dec 20, 2024 · N744FD · Airbus A300B4622R · Emergency Lighting
  > COURIER AREA "EMERGENCY TEST" SW. 25WL DOESN'T ILLUMNIATE FOR 30 SEC. DURING OPS TEST OF EMERGENECY POWER SUPPLY UNITS. R & R EPSU AND BATTERY, REF AMM 33-51-14-04, OP'S CHECKS GOOD.
- [SDR FDEA202311210104](https://openairdocs.org/sdr/FDEA202311210104.md): Switch · inoperative · Nov 21, 2023 · N744FD · Airbus A300B4622R · Emergency Lighting
  > DURING PREFLIGHT CHECKS, EMERGENCY LIGHT TOGGLE SWITCH WAS STUCK IN OFF POSITION AND BROKE OFF WHEN MOVED TO ARM POSITION. NO REFERENCE REQUIRED PLACED EMERGENCY LIGHT SWITCH TO OFF/DISARM POSITION. LRD U IDENTIFIED PARTS TOGGLE SWITCH. COURIER COMPA
- [SDR FDEA202302080348](https://openairdocs.org/sdr/FDEA202302080348.md): Firewall · none · Feb 8, 2023 · N744FD · Airbus A300B4622R · Standard Practices/Structures
  > APU BULKHEAD FIRE WALL FOUND 4EA RIVETS LOOSEN. REPAIRED THE DAMAGE AREA WITH DOUBLER AND FILLER I.A.W EA NO:6-5310-T0372952 P1, SEQ NO:000818, TITLE:FUSELAGE-MAINFRAME-FR95 FIREWALL WEB ELONGATED FASTENER HOLES AND DOUBLER REPAIR.
- [SDR FDEA202301200343](https://openairdocs.org/sdr/FDEA202301200343.md): Flap · dented · Jan 20, 2023 · N744FD · Airbus A300B4622R · Wing, Control Surfaces
  > FOUND DENTS ON LOWER SKIN OF LH INNER FLAP O/B T/E. ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR (CAT.A) I.A.W EA NO:6-5750-T0372824 P1, SEQ NO:000815, TITLE:WING-FLIGHT SURFACES-LH INNER FLAP TRAILING EDGE LOWER SKIN REPAIR NEAR RIB28A. MAJOR REPAIR
- [SDR FDEA202301150208](https://openairdocs.org/sdr/FDEA202301150208.md): Floor Panel · damaged · Jan 15, 2023 · N744FD · Airbus A300* · Fuselage Floor Panel
  > THE #143DF KEEL BEAM FLOOR WAS FOUND SOFTEN AND CAUSE BY HYD FLUID CONTAMINATION FABRICATED NEW FLOOR PANEL I.A.W FEDEX STANDARD REPAIR DRAWING - FLOOR PANEL REPLACEMENT NO: SRZ-25-005 REV.R MAJOR REPAIR
- [SDR FDEA202206071392](https://openairdocs.org/sdr/FDEA202206071392.md): None · unknown · Jun 7, 2022 · N744FD · Airbus A300* · Landing Gear Brake System
  > PDIS 744 32-40 3862 07JUN22 MEM FACT U WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING AT KMEM, THE LEFT BRAKE INDICATED 600LBS AND THE RIGHT BRAKE INDICATED 250LBS. STILL SHOWS 600 LEFT, 250 RIGHT. ***EMERGENCY DECLARED*** IDENTIFIED PARTS
- [SDR FDEA202204130955](https://openairdocs.org/sdr/FDEA202204130955.md): Packing · damaged · Apr 13, 2022 · N744FD · Airbus A300B4622R · Hydraulic System, Main
  > AT FL 270 RECEIVED ECAM HYD GRN SYS LO PSI, THEN LO RESERVOIR. IMMEDIATELY TURNING OFF GRN SYS PUMPS TO PREVENT PUMP DAMAGE. CONFIRMED BOTH ECAM & OVERHEAD GRN SYS RES LOW. MANUAL GEAR EXTENSION QRH CHECKLIST. DURING DESCENT & DURING FINAL CONTINUED TO
- [SDR FDEA202204070886](https://openairdocs.org/sdr/FDEA202204070886.md): None · none · Apr 7, 2022 · N744FD · Airbus A300* · Landing Gear Retraction/Extension System
  > PDIS 744 32-30 3672 07APR22 MEM OPEN U LANDING GEAR WOULD NOT COME DOWN. REFERENCED QRH. L/G GRAVITY EXTENSION ACCOMPLISHED. GEAR CAME DOWN. FOUND PROXIMITY DETECTOR PROCESSING UNIT (PDPU, 54GB) WITH RED FAULT LIGHT ON. RECALLED MEMORY AND
- [SDR FDEA202008181922](https://openairdocs.org/sdr/FDEA202008181922.md): Skin · delaminated · Aug 18, 2020 · N744FD · Airbus A300B4622R · Vertical Stabilizer, Plate/Skin
  > VERTICAL LEADING EDGE DAMAGE REPAIR VERTICAL LEADING EDGE. MULTPLIE SPOTS OF COMPOSITE SEPARATED AND EXPOSED, 10 AREAS OF DAMAGE ON THE RT SIDE OF VERTICAL STAB, REPAIRED THE VERTICAL LEADING EDGE 10EA AREA IAW SRM 55-31-12-20-2, PARA 2.A, SRM 51-77-11, FIG
- [SDR FDEA2020081821888](https://openairdocs.org/sdr/FDEA2020081821888.md): Skin · cracked · Aug 12, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Structure
  > LEFT WING LE PANEL 513AB ACCESS LAND IS CRACKED AT AFT IB AREA ACCOMPLISHED REPAIR DOUBLER ON L/W L/E PANEL LAND IAW A300-600SRM 53-15-63, FIG.201
- [SDR FDEA2020081421869](https://openairdocs.org/sdr/FDEA2020081421869.md): Frame · damaged · Aug 12, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Frame
  > 10 EA FASTENER IS LEAKING FUEL AT FRAME 47 WING ROOT AREA FRAME 47 WING ROOT AREA 10EA FASTENERS REPAIRED PER EA # 6-5710-T0355031 P1.
- [SDR FDEA2020081211862](https://openairdocs.org/sdr/FDEA2020081211862.md): Skin · dented · Aug 11, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING REPAIR OF DENT AFT OF L-1 DOOR, FASTENER HOLES DRILLED INTO CHEM MIL. COMPLIED WITH EA 6-5330-T0355104-P1.
- [SDR FDEA202008081835](https://openairdocs.org/sdr/FDEA202008081835.md): Spoiler · gouged · Aug 8, 2020 · N744FD · Airbus A300* · Drag Control System
  > #2 SPOILER HAS GOUGE ON O/B FACE OF SPAR AROUND NUTPLATE HOLE REPAIRED RIGHT WING #2 SPOILER IAW FEDEX EA 6-5750-T0355493-P1, TITLE: WINGS - FLIGHT SURFACES - RH WING - NO. 2 SPOILER, SPAR OUTBD END, GOUGE
- [SDR FDEA2020081081835](https://openairdocs.org/sdr/FDEA2020081081835.md): Spar · gouged · Aug 8, 2020 · N744FD · Airbus A300B4622R · Spoilers
  > NR 2 SPOILER WAS GOUGED ON THE OTBD FACE OF THE SPAR AROUND NUTPLATE HOLES. REPAIRED IAW EA 6-5750-T0355493-P1.
- [SDR FDEA202008071798](https://openairdocs.org/sdr/FDEA202008071798.md): Seat Track · gouged · Aug 7, 2020 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK WAS GOUGED AT FRAME 60, RBL 78. REMOVED AND REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-10-16, FIG 208.
- [SDR FDEA202008071797](https://openairdocs.org/sdr/FDEA202008071797.md): Seat Track · gouged · Aug 7, 2020 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK WAS GOUGED AT FRAME 58, RBL 78. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-10-16, FIG 208.
- [SDR FDEA2020080751771](https://openairdocs.org/sdr/FDEA2020080751771.md): Bulkhead · cracked · Aug 5, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Bulkhead/Firewall
  > NO.1 ENG INLET, O/B SIDE, AFT BULKHEAD CRACKED AROUND SENSE LINE ELBOW. REPAIRED #1 ENG INLET, O/B SIDE, AFT BULKHEAD AT SENSE LINE PER P&W SRM 54-10-00 FIG. 201.
- [SDR FDEA202008031763](https://openairdocs.org/sdr/FDEA202008031763.md): Skin · corroded · Aug 3, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NR 4 LIGHTNING STRIP, OUTBOARD OF NR 3, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE NR 4 LIGHTNING STRIP IAW SRM:55-21-12 PARA 5.E.
- [SDR FDEA202008031762](https://openairdocs.org/sdr/FDEA202008031762.md): Skin · corroded · Aug 3, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NR 3 LIGHTNING STRIP, OUTBOARD OF NR 2, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED NR 3 LIGHTNING STRIP IAW SRM 55-21-12 PARA 5.E.
- [SDR FDEA202008031761](https://openairdocs.org/sdr/FDEA202008031761.md): Skin · corroded · Aug 3, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NR 2 LIGHTNING STRIP, OUTBOARD OF NR 1, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED NR 2 LIGHTNING STRIP IAW SRM: 55-21-12 PARA 5.E
- [SDR FDEA202008031760](https://openairdocs.org/sdr/FDEA202008031760.md): Skin · corroded · Aug 3, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > NR 1 LIGHTNING STRIP, MOST INBOARD. RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED THE NR 1 LIGHTNING STRIP INBD RT ELEVATOR IAW SRM: 55-21-12, PARA 5.E
- [SDR FDEA2020082001752](https://openairdocs.org/sdr/FDEA2020082001752.md): Skin · delaminated · Aug 2, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED. REPAIRED THE AREA AT RIB ER2 ADJACENT TO THE RT ELEVATOR UPPER SKIN IAW SRM: 55-20-00, & 55-21-12 PARA 5.E. REMOVED & REPLACED THE LIGHTNING CONDUCTOR STRIP IAW SRM: 55-21-12, PARA 5.E. MAJOR
- [SDR FDEA2020080321757](https://openairdocs.org/sdr/FDEA2020080321757.md): Panel · cracked · Aug 2, 2020 · N744FD · Airbus A300B4605R · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON PANEL 413BL FWD INSIDE IB CORNER CRACKED UNDER SEAL. REPAIRED NR 1 PYLON PANEL 413BL FWD INSIDE IB CORNER IAW SRM 54-52-51.
- [SDR FDEA202008021756](https://openairdocs.org/sdr/FDEA202008021756.md): Panel · cracked · Aug 2, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON PANEL 473BL FWD INSIDE OB CORNER CRACKED UNDER SEAL. REPLACED THE NR 1 PYLON PANEL 713AL FWD OB CORNER IAW SRM 54-52-51
- [SDR FDEA2020080321752](https://openairdocs.org/sdr/FDEA2020080321752.md): Skin · delaminated · Aug 2, 2020 · N744FD · Airbus A300B4622R · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED REPAIRED DELAMINATED AREA AT RIB ER2 ADJACENT TO RH ELEVATOR UPPER SKIN IAW A300- 600 SRM: 55-20-00 & 55-21-12 PARA 5.E. REMOVED & REPLACED LIGHTNING CONDUCTOR STRIP IAW A300-600 SRM: 55-21-12
- [SDR FDEA2020080311739](https://openairdocs.org/sdr/FDEA2020080311739.md): Panel · cracked · Aug 1, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON PANEL 423BL FOUND TO BE CRACKED ON THE OUTBOARD SIDE NR 2 PYLON PANEL 423BL. REPAIR IAW EA 6-5450-T0355366, P1.
- [SDR FDEA202007271679](https://openairdocs.org/sdr/FDEA202007271679.md): Floor Panel · delaminated · Jul 27, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 152FF HAS DISBONDED UPPER SKIN AND DAMAGED EDGE FILLER FABRICATED PANEL IAW SRZ-25-005 REV:R MAJOR REPAIR
- [SDR FDEA202007271678](https://openairdocs.org/sdr/FDEA202007271678.md): Floor Panel · delaminated · Jul 27, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > AVIONICS FLOOR PANEL 122JF HAS CORNER DAMAGE FABRICATED PANEL 122JF IAW FEDEX SRZ-25-005 REV: R MAJOR REPAIR
- [SDR FDEA202007271677](https://openairdocs.org/sdr/FDEA202007271677.md): Floor Panel · delaminated · Jul 27, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 152EF HAS DISBANDED UPPER SKIN AND CORNER DAMAGE FABRICATED PANEL 152EF IAW FEDEX SRZ-25-005 REV: R MAJOR REPAIR
- [SDR FDEA202007271676](https://openairdocs.org/sdr/FDEA202007271676.md): Floor Panel · delaminated · Jul 27, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > AVIONICS FLOOR PANEL 121JF HAD CORNER DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005, REV R. MAJOR REPAIR.
- [SDR FDEA2020072761671](https://openairdocs.org/sdr/FDEA2020072761671.md): Floor Panel · delaminated · Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231LG WAS CRACKED AT THE CORNER. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R. MAJOR REPAIR.
- [SDR FDEA2020072761670](https://openairdocs.org/sdr/FDEA2020072761670.md): Floor Panel · punctured · Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231UG HAS 2 EA. PUNCTURES ON BOTTOM SIDE. REPAIRED FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R, MAJOR REPAIR.
- [SDR FDEA2020072761669](https://openairdocs.org/sdr/FDEA2020072761669.md): Floor Panel · delaminated · Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231JG WAS CRACKED. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N744FD/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 = 'N744FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N744FD/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.