# Service difficulty reports: N944FD

A list on [N944FD](https://openairdocs.org/aircraft/N944FD.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 3 · 130 reports

- [SDR FDEA202409041238](https://openairdocs.org/sdr/FDEA202409041238.md): Light · inoperative · Sep 4, 2024 · N944FD · Boeing 7572G5 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT INOP. RELEASED FOR SERVICE PER MEL 33-51-01-01. ACFT OK FOR SERVICE.
- [SDR FDEA202407251050](https://openairdocs.org/sdr/FDEA202407251050.md): Tach Generator · failed · Jul 25, 2024 · N944FD · Boeing 7572G5 · Engine RPM Indicating System
  > AFTER TAKEOFF, RECEIVED L ENG BLEED OFF EICAS RAN QRH 2.1.14 LEVELED AT FL360. NOTICED CABIN ALT AT 8000 WHILE 5 MIN CABIN ALT AT 9500 DESCENDED DOWN TO LOWER ALT IN DESCENT RECEIVED CABIN ALT HIGH MASTER WARNING AND EICAS MSG. RAN QRC THEN QRH 2.1.1 CONTI
- [SDR FDEA202302220332](https://openairdocs.org/sdr/FDEA202302220332.md): Engine · failed · Feb 22, 2023 · N944FD · Boeing 757200 · Engine Oil System (Airframe Furnished)
  > PDIS 944 79-01 0275 22FEB23 RSW OPEN U IN FLIGHT AT FL390 NOTICED R ENG OIL PRESS DISCREET LIGHT FLICKERING. ON EICAS NOTICED OIL QUANTITY 0, ALL OTHER ENGINE INDICATIONS APPEARED NORMAL. FOLLOWED QRH WHICH DIRECTED US TO REDUCE THROTTLE AN
- [SDR FDEA202211042728](https://openairdocs.org/sdr/FDEA202211042728.md): Pan · gouged · Nov 4, 2022 · N944FD · Boeing 7572G5 · Passenger/Crew Doors
  > R1 DOOR EXTERIOR HANDLE PAN WORN REMOVED AND REPLACED R1 DOOR HANDLE PAN IAW DWG 141N6200 REV T AND AMM 52-11-13-02.
- [SDR FDEA202211032725](https://openairdocs.org/sdr/FDEA202211032725.md): Wedge · delaminated · Nov 3, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > #6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4
- [SDR FDEA202211032724](https://openairdocs.org/sdr/FDEA202211032724.md): Wedge · delaminated · Nov 3, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > #4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4
- [SDR FDEA202211032723](https://openairdocs.org/sdr/FDEA202211032723.md): Wedge · delaminated · Nov 3, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > #3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4
- [SDR FDEA202211032722](https://openairdocs.org/sdr/FDEA202211032722.md): Wedge · delaminated · Nov 3, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > #5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4
- [SDR FDEA202211022713](https://openairdocs.org/sdr/FDEA202211022713.md): Floorbeam · corroded · Nov 2, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM STA 1681 IS CORRODED ON THE AFT FACE AND LOWER SURFACE OF THE UPPER CAP AT APPROX RBL 48 ACCOMPLISHED FEDEX EA # F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL 5, RBL 48, CORRODED DAMAGE. ORIG SUBMISSION DATE
- [SDR FDEA202211022714](https://openairdocs.org/sdr/FDEA202211022714.md): Floorbeam · corroded · Nov 2, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM IS CORRODED AT FASTENER HOLE BS 310 LBL 20 ACCOMPLISHED FEDEX EA # F-5310-T0371036 FUSELAGE - MAINFRAME - FLOOR BEAM TEE CAP, STA 310, LBL 20, CORROSION REPAIR
- [SDR FDEA202211022712](https://openairdocs.org/sdr/FDEA202211022712.md): Panel · cracked · Nov 2, 2022 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3, 51-40-02,51-70-04,54-50-70-0IAND AMM 51-24-02-7, 51-21-00/701, B757NDTM PART 1 51-01-01.
- [SDR FDEA202210312701](https://openairdocs.org/sdr/FDEA202210312701.md): Fitting · corroded · Oct 31, 2022 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous Structure
  > MAIN CABIN - STA 324-345 RBL2 INTERCOSTAL IS CORRODED AT FLOOR PANEL HOLES REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW B757 DWG 141N5160 REV CD AND 141N5161 REV -
- [SDR FDEA202210282687](https://openairdocs.org/sdr/FDEA202210282687.md): Stringer · cracked · Oct 28, 2022 · N944FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STA 1680-1701 STR29R HAS CRACKED STINGER REMOVED CRACKED STINGER SECTION ON STA 1680 - 1701 STR29 R/H FABRICATED -1 HAT SECTION AND -2 FILLER INTALLED IAW B757 SRM 53-00-03-2R
- [SDR FDEA202210282685](https://openairdocs.org/sdr/FDEA202210282685.md): Floorbeam · corroded · Oct 28, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN - ZONE 250 - STA 1681 FLOOR BEAM IS CORRODED ON LOWER SURFACE - LBL5 ACCOMPLISHED FEDEX EA #: F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 1681, LBL 23, LBL5, RBL48, CORROSION DAMAGE
- [SDR FDEA202210252660](https://openairdocs.org/sdr/FDEA202210252660.md): Web · corroded · Oct 25, 2022 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT PLATE IS CORRODED AFT OF CABLES BS 340, LBL 27 REMOVED, FABRICATED AND INSTALLED NEW FLOOR WEB IAW B757 DWG 141N5170 REV C
- [SDR FDEA202210242651](https://openairdocs.org/sdr/FDEA202210242651.md): Intercostal · corroded · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Structure
  > MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 25 - RBL 39 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW BAC DWG 141N5160 REV C. ORIG SUBMISSION DATE: 10/24/2022
- [SDR FDEA202210242650](https://openairdocs.org/sdr/FDEA202210242650.md): Intercostal · corroded · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Structure
  > MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 4- RBL 23 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW B757-2 DWG 141N5160. ORIG SUBMISSION DATE: 10/24/2022
- [SDR FDEA202210242652](https://openairdocs.org/sdr/FDEA202210242652.md): Floorbeam · corroded · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT BEAM IS CORRODED UPPER SIDE AT NUTPLATE HOLE BS 344 LBL20 - LBL22 REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT BEAM ISW B757-2 DWG 141N5161 REV A AND 141N5170 REV C
- [SDR FDEA202210242649](https://openairdocs.org/sdr/FDEA202210242649.md): Floor Panel · damaged · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL AT STA 480-500 LBL 45 IS DAMAGED REPAIRED FLOOR PANEL IAW B757SRM 53-00-50-2R REPAIR 1
- [SDR FDEA202210242648](https://openairdocs.org/sdr/FDEA202210242648.md): Floorbeam · corroded · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES AND FWD EDGE IS GOUGED AND CORRODED BS 344 LBL0-LBL20 REPAIRED FLOOR BEAM IAW B757-2 SRM 53-00-51-2R REPAIR #10
- [SDR FDEA202210242647](https://openairdocs.org/sdr/FDEA202210242647.md): Floor Panel · delaminated · Oct 24, 2022 · N944FD · Boeing 7572G5 · Fuselage Floor Panel
  > MAIN CABIN ZONE 240 - FLOOR PANEL 242MCF IS DELAMINATED REPAIRED FLOOR PANEL 242 MCF IAW B757 SRM 53-00-50-2R, REMOVED AND INSTALLED INSERTS IAW B757 SRM 53-00-50-2R
- [SDR FDEA202210222642](https://openairdocs.org/sdr/FDEA202210222642.md): Skin · damaged · Oct 22, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER SURFACE HAS AREA OF BARE METAL REPAIRED #8 SLAT UPPER TRAILING EDGE LOWER SURFACE ARE OF BARE METAL IAW FEDEX EA# F-5750-T0370952
- [SDR FDEA202210222641](https://openairdocs.org/sdr/FDEA202210222641.md): Wedge · delaminated · Oct 22, 2022 · N944FD · Boeing 7572G5 · Leading Edge Devices
  > #8 SLAT T/E WEDGE IS DISBONDED REPAIRED #8 SLAT T/E WEDGE DISBOND ON 3EA. AREA IAW FEDEX EA# F-5750-T0370952.
- [SDR FDEA202210052470](https://openairdocs.org/sdr/FDEA202210052470.md): Panel · cracked · Oct 5, 2022 · N944FD · Boeing 7572G5 · Wing, Plate/Skin
  > RW LEADING EDGE PANEL BEHIND #7 SLAT IS CRACKED AT OB SPLICE AREA. REPAIRED RW LEADING EDGE PANEL BEHIND #7 SLAT IAW B757-200 SRM 57-41-02-2RFIG 201 SHEET 8 AND 51-70-07
- [SDR FDEA202210052469](https://openairdocs.org/sdr/FDEA202210052469.md): Panel · damaged · Oct 5, 2022 · N944FD · Boeing 7572G5 · Vertical Stabilizer, Plate/Skin
  > LH VERTICAL PANEL 322CL DAMAGED REPAIRED L/H VERTICAL STAB PANEL 322CL SKIN IAW B757-200 SRM 55-30-01-2R FIG 201 REPAIR 4 SHEET1 AND SRM 51-70-07-0G.
- [SDR FDEA202011202924](https://openairdocs.org/sdr/FDEA202011202924.md): Drag Fitting · cracked · Nov 20, 2020 · N944FD · Boeing 7572G5 · Wing, Attach Fittings
  > THE RT WING OUTBOARD DRAG FITTING HAS INDICATIONS OF DEFECTS ON THE NR 4 & NR 13 HOLE. THE NR 4 HOLE HAS INDICATION AT THE 3 O`CLOCK LOCKING AFT AND NR 13 HAS INDICATION ALSO AT THE 3 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPL
- [SDR FDEA202011202923](https://openairdocs.org/sdr/FDEA202011202923.md): Drag Fitting · corroded · Nov 20, 2020 · N944FD · Boeing 7572G5 · Wing, Attach Fittings
  > THE RT INBOARD DRAG FITTING UPPER SURFACE HAS CORROSION AT NR 3 AND NR 8 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED INBOARD FITTING.
- [SDR FDEA202011202922](https://openairdocs.org/sdr/FDEA202011202922.md): Drag Fitting · cracked · Nov 20, 2020 · N944FD · Boeing 7572G5 · Wing, Attach Fittings
  > THE RT WING INBOARD DRAG FITTING HAS INDICATIONS ON THE NR 3, NR 8 HOLE AND THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE SPAR. THE 2 HOLES THAT ATTACH TO THE SKIN HAVE MULTIPLE SIGNALS AND UNABLE TO CLOCK POSITION. THE 3RD HOLE FROM THE BOTTOM THAT ATTA
- [SDR FDEA202011202921](https://openairdocs.org/sdr/FDEA202011202921.md): Drag Fitting · cracked · Nov 20, 2020 · N944FD · Boeing 7572G5 · Wing, Attach Fittings
  > THE RT UPPER SKIN DRAG FITTING NR 3 AND NR 5 HOLES HAVE INDICATIONS OF DEFECTS NOTED. THE NR 3 HOLE HAS INDICATION AT THE 1 O`CLOCK LOOKING AFT. THE NR 5 HOLE HAS INDICATION AT THE 12 O`CLOCK LOOKING AFT. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WIN
- [SDR FDEA202011202918](https://openairdocs.org/sdr/FDEA202011202918.md): Drag Fitting · corroded · Nov 20, 2020 · N944FD · Boeing 7572G5 · Wing Main, Frame Structure
  > THE RT WING OUTBOARD DRAG FITTING UPPER SURFACE HAS CORROSION ON NR 4 AND NR 13 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR. REPLACED OUTBOARD FITTING.
- [SDR FDEA202011192911](https://openairdocs.org/sdr/FDEA202011192911.md): Skin · dented · Nov 19, 2020 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/Skin
  > LH ENGINE PYLON IB SIDE ABOUT MID SECTION ON LWR FACE HAS DENT. COMPLIED WITH FEDEX EA. F - 5430-T0358210 P1 NACELLS / PYLON - SKIN /PLATES/ PANELS - LH ENGINE PYLON INBOARD SIDE SKIN PANEL REPAIR NEAR PPS 136. PERFORMED SATIFACTORY LEAK CHECK IAW B757 AMM
- [SDR FDEA202011072791](https://openairdocs.org/sdr/FDEA202011072791.md): Frame · cracked · Nov 7, 2020 · N944FD · Boeing 7572G5 · Fuselage Main, Frame
  > THE RT 1640 FRAME BY STR 14R LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING OUTBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT ALL WORK ACCOMPLI
- [SDR FDEA202011072790](https://openairdocs.org/sdr/FDEA202011072790.md): Frame · cracked · Nov 7, 2020 · N944FD · Boeing 7572G5 · Fuselage Main, Frame
  > THE LT 1640 FRAME BY STR 14L LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING INBOARD). REPAIR AS REQUIRED, LAYERS NEED TO BE SEPARATED TO DETERMINE WHAT LAYER HAS DEFECT. ALL WORK ACCOMPL
- [SDR FDEA2020040620689](https://openairdocs.org/sdr/FDEA2020040620689.md): Reservoir · failed · Apr 2, 2020 · N944FD · Boeing 7572G5 · Passenger/Crew Doors
  > R1 DOOR EMERGENCY POWER RESERVOIR HAS NO PRESSURE. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR REF B757 AMM 52-11-30-4. OPS CHECK SATIS. A/C OK TO CONT SERVICE. RII BY
- [SDR FDEA2019122313275](https://openairdocs.org/sdr/FDEA2019122313275.md): Collar · inoperative · Dec 21, 2019 · N944FD · Boeing 7572G5 · Passenger/Crew Doors
  > GUST LOCK ON L FWD ENTRY DOOR WILL NOT MOVE TO ALLOW DOOR TO CLOSE. REF MM 52-11-08-08, INSTALLED NEW HOLD OPEN LOCK COLLAR ON L1 DOOR. L1 DOOR HOLD OPEN LOCK COLLAR OPERATES NORMALLY. PART INSTALLED PN 10-N6008-1 / SN 20-024.
- [SDR FDEA2019061741301](https://openairdocs.org/sdr/FDEA2019061741301.md): Bottle · empty · Jun 14, 2019 · N944FD · Boeing 7572G5 · Emergency Equipment
  > FOUND POWER ASSIST RESIVOUR FOR L1 DOOR BLOWN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-30-4-0 NOMENCLATURE-CYLINDER, EMERGENCY POWER RESERVOIR, /N 803300-35A, S/N 1394
- [SDR FDEA2019022860509](https://openairdocs.org/sdr/FDEA2019022860509.md): Hose · defective · Feb 26, 2019 · N944FD · Boeing 7572G5 · Hydraulic System, Main
  > L HYD SYS PRESS LIGHT ILLUMINATED ON FINAL AFTER LANDING GEAR DOWN AND LOCKED AND FLAPS AT FINAL CONFIGURATION. FOLLOWED BY L HYD SYS PRESS AND L YAW DAMPER. CLEARED RUNWAY AFTER LANDING- MAINT TOW TO GATE. REMOVED AND REPLACED DEFECTIVE FLEX HOSE O
- [SDR FDEA201811123187](https://openairdocs.org/sdr/FDEA201811123187.md): Shim · migrated · Nov 12, 2018 · N944FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous Structure
  > RT PYLON UPPER AFT DRAG LINK SPAR FITTING SHOWS SIGNS OF SHIM MIGRATION. COMPLIED WITH EA F-5740-T0343112 PART 1. RT WING DRAG FITTING TO WING UPPER SKIN SHIM MIGRATION REPAIR.
- [SDR FDEA201810303054](https://openairdocs.org/sdr/FDEA201810303054.md): Skin · cracked · Oct 30, 2018 · N944FD · Boeing 7572G5 · Fuselage Main, Plate/Skin
  > CRACK LIKE INDICATION WAS NOTED AROUND AND BELOW FASTENER DURING NDT INSPECTION OF REPAIR AREA AT BS 1360 APPROX 4 INCHES ABOVE STR 5L. STRIP/REMOVED PAINT AT MARKED AREA FOR FURTHER NDT INSPECTIONS OF THE AREA. COMPLIED WITH EA F-5330-T0343048 P1. FUSELAGE SK
- [SDR FDEA201810283036](https://openairdocs.org/sdr/FDEA201810283036.md): Floorbeam · cracked · Oct 28, 2018 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > SUB BEAM AT STA 580 IS CRACKED. TRIMMED ENTIRE UPPER FLANGE OF THE BS 580 FLOOR BEAM SPLICE. FABRICATED REPAIR ANGLE AND RADIUS STRAP AND INSTALLED IAW EA F-5310-T0343027 P-1.
- [SDR FDEA201810263017](https://openairdocs.org/sdr/FDEA201810263017.md): Skin · corroded · Oct 26, 2018 · N944FD · Boeing 757200 · Wing, Plate/Skin
  > CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSI
- [SDR FDEA20181113017](https://openairdocs.org/sdr/FDEA20181113017.md): Skin · corroded · Oct 26, 2018 · N944FD · Boeing 7572G5 · Wing, Plate/Skin
  > CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND SKINS - RH WING LOWER SKIN CORROSION AT TRAILING EDGE, WSTA 711.50 RH WING LOWER SKIN CORROSI
- [SDR FDEA201707282079](https://openairdocs.org/sdr/FDEA201707282079.md): Adc · malfunctioned · Jul 28, 2017 · N944FD · Boeing 7572G5 · Altimeter, Barometric/Encoder
  > AFTER TAKEOFF, LOST MULTIPLE AVIONICS, PILOTS ALTITUDE, AIRSPEED, RADIO ALTIMETER, AUTOTHROTTLES. FIRST OFFICER`S FLT DISPLAY WAS SIMILAR BUT REGAINED AIRSPEED, ALTITUDE, BUT NO AUTOTHROTTLES. LAST FLIGHT FAULTED ADC SYS L WITH FAULT CODES 110401, AND 13040
- [SDR FDEA201707282078](https://openairdocs.org/sdr/FDEA201707282078.md): Landing Gear · malfunctioned · Jul 28, 2017 · N944FD · Boeing 7572G5 · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF, PUT GEAR UP. GEAR RETRACTED. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR CAME DOWN. PUT GEAR DOWN FOR LANDING AND RECEIVED GOOD DOWN INDICATION. PERFORMED A BITE OF THE PSEU AND FOUND NO FAULTS ON THE BOX IAW AMM 32-09-06, STEP 4. E. JACKED AIR
- [SDR FDEA201610013404](https://openairdocs.org/sdr/FDEA201610013404.md): Floorbeam · cracked · Oct 1, 2016 · N944FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > STUB FRAME BS 580 LBL 44-46 CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION REINFORCEMENT STUB FRAME IAW DWG 657N4311 REV - AND SRM 51-40-05-0G, 51-40-02-0G. MAJOR REPAIR.
- [SDR FDEA201410173289](https://openairdocs.org/sdr/FDEA201410173289.md): Skin · delaminated · Oct 17, 2014 · N944FD · Boeing 7572G5 · Trailing Edge Flaps
  > LEFT OTBD AFT FLAP UPSIDE OTBD END DELAMINATED. REPAIRED IAW EA F-5750-T0312494.
- [SDR FDEA201409032431](https://openairdocs.org/sdr/FDEA201409032431.md): Windshield · cracked · Sep 3, 2014 · N944FD · Boeing 7572G5 · Flight Compartment Windows
  > ON CLIMB OUT FIRST OFFICERS R1 WINDOW BEGAN TO ARC. COMPLIED WITH QRH & WINDOW CRACKED AFTER COMPLETING CHECKLIST. LANDED AT NEAREST SUITABLE AIRPORT. R&R FIRST OFFICERS WINDSHIELD. COMPLIED WITH WINDOW HEATING SYS CHECK & WINDOW WIPER OPERATIONAL CHECK.
- [SDR FDEA201212214349](https://openairdocs.org/sdr/FDEA201212214349.md): Slide · dislodged · Dec 21, 2012 · N944FD · Boeing 7572G5 · Escape Slide
  > L1 DOOR ESCAPE SLIDE FELL OFF OF DOOR. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHECKED NORMAL. ACFT OK TO CONTINUE.
- [SDR FDEA201210293773](https://openairdocs.org/sdr/FDEA201210293773.md): Carriage · gouged · Oct 29, 2012 · N944FD · Boeing 7572G5 · Trailing Edge Flaps
  > NR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.
- [SDR FDEA201209233412](https://openairdocs.org/sdr/FDEA201209233412.md): Sensor · dirty · Sep 23, 2012 · N944FD · Boeing 7572G5 · Door Warning System
  > TAXIING INTO POSITION FOR TAKE OFF, RECEIVED LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON INTERMITTENTLY DURING TAXI BACK TO GATE. INSPECTED ENTRY DOOR, FOUND GREASE, DIRT AND DEBRIS ON PROXMITY SWITCH, CLEANED AREA, OPERATED DOOR IAW AMM 52-11-01-6 SYS CHECKE

Next page: https://openairdocs.org/aircraft/N944FD/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 = 'N944FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N944FD/reports

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