# Service difficulty reports: N920FD

A list on [N920FD](https://openairdocs.org/aircraft/N920FD.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 · 222 reports

- [SDR FDEA202605280647](https://openairdocs.org/sdr/FDEA202605280647.md): Adc · faulted · May 28, 2026 · N920FD · Boeing 75723A · Air Data Computer
  > ALTITUDE DISAGREE TWO TIMES DURING DESCENT. FO ALTIMETER MATCHED THE STANDBY AND WAS 400 FEET DIFFERENT THAN CAPTAINS AMM: 34-12-01-4 REMOVED AND REPLACED CAPTAINS ADC. GROUND TEST NORMAL. PARTS INPUT WRI 34-16/ 7188. AMM: 34-12-01-4 REMOVED AND R
- [SDR FDEA202501150070](https://openairdocs.org/sdr/FDEA202501150070.md): Battery · failed · Jan 15, 2025 · N920FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY LIGHTS FOR R1 DOOR AND CENTER COURIER AREA INOP. IAW AMM: 33-51-07-2 REMOVED AND REPLACED BATERYPACK ASSY FOR CHARGER ASSEMBLY M730. OPS CHECK GOOD.
- [SDR FDEA202311211876](https://openairdocs.org/sdr/FDEA202311211876.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-13 BTW RBL 46-50 AND STA 720- 780. REMOVED FLOOR PANEL P\N 11864182-13 FROM STA 720-780 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 2 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DET
- [SDR FDEA202311211875](https://openairdocs.org/sdr/FDEA202311211875.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-21 BTW RBL 46-50 AND STA 780- 880. REMOVED FLOOR PANEL #11862182-21 FROM STA 780 - 880 IAW (B 757) AMM 53-01-01-4, EVALUATED AND REPAIRED 3EZ DENTS ON FLOOR PANEL IAW B757 SRM 53-00-50-R2 REP 1 DETAIL
- [SDR FDEA202311211874](https://openairdocs.org/sdr/FDEA202311211874.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-10 BTW RBL 46-50 AND STA 1320- 1420. REMOVED FLOOR PANEL P\N 11862182-10 FROM STA 1320-1420 BTW RBL 46-50 IAW B-757 AMM 53- 01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-5
- [SDR FDEA202311211873](https://openairdocs.org/sdr/FDEA202311211873.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-2 BTW RBL 46-50 AND STA 900- 1020. REMOVED FLOOR PANEL P\N 11862182-2 FROM STA 900-1020 BTW IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1
- [SDR FDEA202311211872](https://openairdocs.org/sdr/FDEA202311211872.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND DENT AT MAIN CARGO FLOOR PANE; P\N: 11862182-28 BTW RBL 46-50 AND STA 880-900 REMOVED FLOOR PANEL P\N 11862182-28 FROM STA 880-900 BTW RBL 46- RBL 50 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 1EA DENT ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R R
- [SDR FDEA202311211871](https://openairdocs.org/sdr/FDEA202311211871.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 6EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-2 BTW RBL 46-50 AND STA 1200- 1320. REMOVED FLOOR PANEL P\N 11864182-2 FROM STA 1200-1320 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 6 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DE
- [SDR FDEA202311211870](https://openairdocs.org/sdr/FDEA202311211870.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 4EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-26 BTW RBL 46-50 AND STA 1100- 1200. REMOVED FLOOR PANEL P\N 11863182-26 FROM STA 1100-1200 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 4EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-R2 REP 1 DET
- [SDR FDEA202311211869](https://openairdocs.org/sdr/FDEA202311211869.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-38 BTW RBL 46-50 AND STA 1055- 1100. REMOVED FLOOR PANEL P\N 11862182-38 FROM STA 1055-1100 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 D
- [SDR FDEA202311211868](https://openairdocs.org/sdr/FDEA202311211868.md): Floor Panel · dented · Nov 21, 2023 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-34 BTW RBL 46-50 AND STA 1020- 1055. REMOVED FLOOR PANEL P\N 11862182-34 FROM STA 1020-1055 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1
- [SDR FDEA202311201865](https://openairdocs.org/sdr/FDEA202311201865.md): Floorbeam · corroded · Nov 20, 2023 · N920FD · Boeing 757200 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM AT STA 880 LBL 48 TO 62 LBL SURFCE CORROSION. DOT 101. ACCOMPLISHED EA F-5321-T0376857 P1 "FUSELAGE MAINFRAME SECTION 43, FLOOR BEAM ASSY CORROSION, STA879, UPPER CHORD, LBL 45-58, DEVIATION FROM TYPICAL SRM REPAIR, WITH NO DEVIATION.
- [SDR FDEA202311191864](https://openairdocs.org/sdr/FDEA202311191864.md): Frame · unknown · Nov 19, 2023 · N920FD · Boeing 757200 · Standard Practices/Structures
  > DURING FUSELAGE MAINFRAME - AFT CARGO COMPARTMENT FRAME INSPECTION PER EO NO. F- 5310-E0347443 B P1 EXISTING REPAIR WAS FOUND AT STA 1300 BTW STRG 26L-27L CONTACT SERVICE ENGINEERING FOR ALTERNATIVE INSPECTION. ACCOMPLISHED EA NO. T F-5310-T0376726 P1. FUS
- [SDR FDEA202311061834](https://openairdocs.org/sdr/FDEA202311061834.md): Slat · debonded · Nov 6, 2023 · N920FD · Boeing 757200 · Leading Edge Devices
  > #5 SLAT FOUND DISBONDED. INSTALLATION OF #5 SLAT TO BE ACCOMPLISHED ON NR00110. NR ATTACHED. REPAIRED DISBONDING ON #5 SLAT IAW B757 SRM 51-70-10-2R, B757 SRM 51-20-01-0G, AND B757 AMM 51-21-15-7.
- [SDR FDEA202311061833](https://openairdocs.org/sdr/FDEA202311061833.md): Slat · debonded · Nov 6, 2023 · N920FD · Boeing 757200 · Leading Edge Devices
  > #2 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #2 SLAT FOR DISBONDING REPAIR IAW B757 AMM 27-81-02-4, B757 SRM 51-70-10-2R, B757 SRM 51-20-01-0G, B757 AMM 51-21-15-7. OPS CHECK GOOD IAW B757 AMM 27-81-02-4. REPAIRED #2 SLAT IAW SRM (B757) 57-43-02-2R.
- [SDR FDEA202311061832](https://openairdocs.org/sdr/FDEA202311061832.md): Skin · debonded · Nov 6, 2023 · N920FD · Boeing 757200 · Leading Edge Devices
  > #8 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #8 SLAT FOR DISBONDING REPAIR IAW B757 SRM 51-70-10-2R, B757 AMM 27-81-02-4, B757 AMM 51-21-15-7, AND B757 SRM 51-20-01-0G. OPS CHECK GOOD IAW B757 AMM 27-81-02-4. REPAIRED #8 SLAT IAW SRM (B757) 57-43-02-2R
- [SDR FDEA202309261652](https://openairdocs.org/sdr/FDEA202309261652.md): Unknown · unknown · Sep 26, 2023 · N920FD · Boeing 757200 · Landing Gear Steering System
  > PDIS 920 32-51 5203 26SEP23 TLV FACT U AFTER LANDING NOSEWHEEL MADE A CLUNKING SOUND WHEN ENGAGING TILLER TO TURN. I.A.W FIM 32-51 FAULT TREE 813 BLOCK 1, STEERING MEETERING VLV COVER REMOVED, AREA INSPECTED FOUND OK. I.A.W BLOCK 2 FOUND MISSI
- [SDR FDEA202302220331](https://openairdocs.org/sdr/FDEA202302220331.md): None · none · Feb 22, 2023 · N920FD · Boeing 757200 · Emergency Equipment
  > PDIS 920 25-60 4604 22FEB23 CDG FACT U SLIDE LIGHT DOES NOT ILLUMINATE WHEN MAIN ENTRY DOOR CLOSED AND ARMED. FACT 22FEB23 02:16 CDG U AMM 25-66-01-6 PERFORMED OPS CHECK OF LEFT PASSENGER DOOR SLIDE SYSTEM AS PER AMM 25-66-01-6. OPS CHECK
- [SDR FDEA202301190139](https://openairdocs.org/sdr/FDEA202301190139.md): Bulb · failed · Jan 19, 2023 · N920FD · Boeing 757200 · Passenger/Crew Doors
  > PDIS 920 52-10 4503 19JAN23 CDG FACT U DOOR L1 SLIDE LIGHT BURNT OUT FACT 19JAN23 18:59 CDG U AMM: 52-11-25-5 REBULBED SLIDE LIGHT AS PER SWPM AND TESTED OK IAW AMM 52-11-25-5. A/C OK FOR SERVICE.
- [SDR FDEA202301110068](https://openairdocs.org/sdr/FDEA202301110068.md): Bulb · failed · Jan 11, 2023 · N920FD · Boeing 757200 · Emergency Lighting
  > PDIS 920 33-50 4480 11JAN23 BER FACT U SLIDE ARMED LIGHT ON L1 OUT FACT 11JAN23 11:26 BER U AMM: 33-51-06-2-1 REV.130.13 BULB,S REPLACED ON SLIDE LIGHT ARMED / DISARMED INDICATOR, SLIDE ARMED / DISARMED FUNCTION CHECKED, O.K., ACC.AMM 33
- [SDR FDEA202208302101](https://openairdocs.org/sdr/FDEA202208302101.md): Control Valve · faulted · Aug 30, 2022 · N920FD · Boeing 75723A · Cabin Cooling System
  > RIGHT PACK OVERTEMP AND FAILED INFLIGHT. LEFT WAS MEL ED,DESCENDED BELOW 10000 ON OXYGEN. EMERGENCY DECLARED. AMM21-51-00-5, FIM21-51 TREE 803, 805. PERFORMED OPS TEST OF RH PACK AND CONTROL SYSTEM, AND BITE CHECKS OF CONTROLLERS. NO FAILURES OR MALFUN
- [SDR FDEA202205121193](https://openairdocs.org/sdr/FDEA202205121193.md): Transmitter · faulted · May 12, 2022 · N920FD · Boeing 757200 · Trailing Edge Flap Control System
  > PDIS 920 27-50 3732 12MAY22 CDG OPEN U TE FLAP DISAGREE WHEN SELECTING FLAP 20. RAN QRH, USED ALTN FLAP CONTROLLER TO LAND FLAPS 20. ***EMERGENCY DECLARED*** SHGN 13MAY22 00:26 CDG U CHECKED FAULTS IN FSEU 1 FOUND FLAP DISAGREE AND LEV
- [SDR FDEA202203090595](https://openairdocs.org/sdr/FDEA202203090595.md): Adc · unknown · Mar 19, 2022 · N920FD · Boeing 757200 · Navigation System
  > PDIS 920 34-16 3550 19MAR22 CDG OPEN U ON CLIMB THRU APPROXIMATELY FL280, THE FIRST OFFICER S SPEED TAPE READ, NO SPD AND THE ALTIMETER JUMPED SEVERAL HUNDRED FEET FOR APPROXIMATELY 1 SECOND BEFORE RETURNING TO NORMAL. RH AND LH AIR DATA COM
- [SDR FDEA202201190099](https://openairdocs.org/sdr/FDEA202201190099.md): Floor Panel · worn · Jan 19, 2022 · N920FD · Boeing 757200 · Standard Practices/Structures
  > MAIN DECK FLOOR PANEL #223MDF STATION 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005 REF. ENGINEERING DISPOSITION OF RFTA NO:02841-0205. MAJOR REPAIR
- [SDR FDEA202201190098](https://openairdocs.org/sdr/FDEA202201190098.md): Floor Panel · worn · Jan 19, 2022 · N920FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN DECK FLOOR PANEL #221BF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRX-25-005 REF. ENGINEERING DESPOSITION OF RFTA NO:02841-0205. MAJOR REPAIR
- [SDR FDEA202201190096](https://openairdocs.org/sdr/FDEA202201190096.md): Floor Panel · worn · Jan 19, 2022 · N920FD · Boeing 757200 · Fuselage Structure (General)
  > MAIN DECK FLOOR PANEL #222 MAF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ 25-005 REF. ENGEENIRING DISPOSITION OF RFTA NO: 02841-0205. MAJOR REPAIR
- [SDR FDEA202201160075](https://openairdocs.org/sdr/FDEA202201160075.md): Floor Panel · worn · Jan 16, 2022 · N920FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL #221MBF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005. REF ENGINEERING DISPOSITION OF RFTA NO: 02841-0205. MAJOR REPAIR
- [SDR FDEA202201060169](https://openairdocs.org/sdr/FDEA202201060169.md): Seat Track · corroded · Jan 6, 2022 · N920FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > STA 480-620, LBL 45.50, FOUND CORROSION ON SEAT TRACK WORK ACCOMPLISHED IN ACCORDANCE WITH EO #F-5310-T0366384. MAJOR REPAIR.
- [SDR FDEA202112280178](https://openairdocs.org/sdr/FDEA202112280178.md): Seat Track · corroded · Dec 28, 2021 · N920FD · Boeing 757200 · Fuselage Structure (General)
  > FOUND CORROSION ON SEAT TRACK BL 0, STA 1330-1320. WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5310-T0366212
- [SDR FDEA202112280168](https://openairdocs.org/sdr/FDEA202112280168.md): None · corroded · Dec 28, 2021 · N920FD · Boeing 757200 · Fuselage Main, Structure
  > FOUND CORROSION ON FLOOR BEAM EXISTING REPAIR AT STA 1320 BETWEEN RBL24 TO RBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EO # F-5310-T0366466
- [SDR FDEA202112280167](https://openairdocs.org/sdr/FDEA202112280167.md): Seat Track · corroded · Dec 28, 2021 · N920FD · Boeing 757200 · Fuselage Main, Structure
  > FOUND CORROSION ON SEAT TRACK RBL 45 BETWEEN STA 1320 TO 1420 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED 2 EA SEAT TRACKS SECTION, 2 EA SPLICES, AND 1 EA STRAP PER SRM 53-00-52, REPAIR 1 FIG. 201, THIS REPAIR IS A PERMANENT CAT. A REPAIR, THE INSP.
- [SDR FDEA202112280166](https://openairdocs.org/sdr/FDEA202112280166.md): Seat Track · corroded · Dec 28, 2021 · N920FD · Boeing 757200 · Fuselage Main, Structure
  > FOUND CORROSION ON SEAT TRACK RBL 24 ON STA 1320 AND STA 1410 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED SEAT TRACK SECTION, 2 EA SPLICES, AND 1 EA STRAP PER SRM 53-00-52 REPAIR 1, FIG 201, THIS REPAIR IS A PERMANENT CAT "A" REPAIR, THE INSP. GI
- [SDR FDEA202112280122](https://openairdocs.org/sdr/FDEA202112280122.md): Frame · unknown · Dec 28, 2021 · N920FD · Boeing 757200 · Standard Practices/Structures
  > FOUND UNDOCUMENTED WEB REPAIR AT STA 1375 OUTBD CREASE BEAM ON R/H SIDE PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W BOEING SR:1-198375510 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR
- [SDR FDEA202112090121](https://openairdocs.org/sdr/FDEA202112090121.md): Frame Splice · unknown · Dec 9, 2021 · N920FD · Boeing 757200 · Standard Practices/Structures
  > EVALUATE SUPPORT AT STA 1020, STR 5L & 5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W EA F-5310-T0366310 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR.
- [SDR FDEA202112090120](https://openairdocs.org/sdr/FDEA202112090120.md): Frame Splice · unknown · Dec 9, 2021 · N920FD · Boeing 757200 · Standard Practices/Structures
  > EVALUATE SUPPORT AT STA 980, S-5L PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366306 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR
- [SDR FDEA202112090119](https://openairdocs.org/sdr/FDEA202112090119.md): Frame Splice · unknown · Dec 9, 2021 · N920FD · Boeing 757200 · Standard Practices/Structures
  > EVALUATE SUPPORT AT STA 1100, S5L TO S-5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366309 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR
- [SDR FDEA202111222930](https://openairdocs.org/sdr/FDEA202111222930.md): None · damaged · Nov 22, 2021 · N920FD · Boeing 757200 · Flight Compartment Equipment
  > PDIS 920 25-10 3302 22NOV21 CDG FACT U FO SHOULDER RESTRAINTS DO NOT RETRACT. FACT 23NOV21 11:54 CDG INSPECTED F/O SEAT SHOULDER HARNESS PER MM 25-11-00-17 OPS CHECK OK THE REASON WHY THE SHOULDER HARNESS DOESN'T RETRACT TO THE SAME
- [SDR FDEA202108262099](https://openairdocs.org/sdr/FDEA202108262099.md): Line · unsecure · Aug 26, 2021 · N920FD · Boeing 75728A · Emergency Equipment
  > L1 DOOR DIFFICULT TO CLOSE AND ARM FOUND EMERGENCY SLIDE STATIC LINE LOOSE AND BUCKLE DANGLING CAUSING INTERFERENCE. REPOSITIONED IAW AMM 25-66-01-4. OPS TEST OKAY.
- [SDR FDEA202106291620](https://openairdocs.org/sdr/FDEA202106291620.md): Sensor · dirty · Jun 29, 2021 · N920FD · Boeing 75723A · Emergency Equipment
  > L1 DOOR SLIDE LIGHT INOP UPON LANDING. DOOR 1L GIRT BAR FITTINGS, SLIDER AND PROXIMITY SENSOR CLEANED FROM DEBRIS. GIRT BAR CYCLED SEVERAL TIMES AND SLIDE ARMED INDICATION LIGHT CHECKED IAW AMM 25-66-00-0-4.
- [SDR FDEA202106111497](https://openairdocs.org/sdr/FDEA202106111497.md): Bulb · inoperative · Jun 11, 2021 · N920FD · Boeing 75723A · Emergency Equipment
  > DOOR 1L SLIDE ARM LIGHT INTERMITTENT, MOSTLY INOP LH SLIDE ARMED INDICATOR LIGHT BOTH BULBS REPLACED IAW SWPM 20-84-18 IAW AMM 52-11-00, LH SLIDE HAS BEEN ARMED AND DISARMED SEVERAL TIMES IN ORDER TO CHECK GOOD FUNCTIONING OF THE LH "SLIDE" ARMED INDIC
- [SDR FDEA202105261402](https://openairdocs.org/sdr/FDEA202105261402.md): Bulb · inoperative · May 26, 2021 · N920FD · Boeing 75723A · Emergency Equipment
  > PDIS 920 25-60 2709 26MAY21 CDG OPEN U LOGPAGES:3001081 1L SLIDE ARMED LIGHT DID NOT ILLUMINATE WHEN ARMED RELEASED FOR SERVICE PER MEL: 25-66-05-A CATEGORY: C EXPIRATION: 05JUN21 "MEL 25-66-05-A: L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIG
- [SDR FDEA202104210963](https://openairdocs.org/sdr/FDEA202104210963.md): Case · corroded · Apr 21, 2021 · N920FD · Boeing 75723A · Engine (Turbine/Turboprop)
  > ENGINE #1 LP COMPRESSOR FRONT CASE OUTER SURFACE FORWARD OF KEVLAR WRAPPING IS CORRODED FROM 4 O'CLOCK TO 12 O'CLOCK POSITION (AFT LOOKING FORWARD) SNRM RECTIFIED AS PART OF ESN 30690 REMOVAL AND INSTALLATION OF ESN 30775 AS PER WO 79687 SEQ: 000235
- [SDR FDEA202104010808](https://openairdocs.org/sdr/FDEA202104010808.md): Valve · failed · Apr 1, 2021 · N920FD · Boeing 75723A · Fuel Controlling System
  > LEFT ENGINE WOULD NOT SHUTDOWN WHEN FUEL CUTOFF MOVED TO CUTOFF. IT RAN FOR APPROXIMATELY 25 SECONDS BEFORE SHUTTING DOWN. REMOVED L/H ENGINE FUEL FLOW GOVERNOR AS PER AMM 73-21-01-4-4. INSTALLED LEFT ENG FFG IAW AMM 73-21-01-4-4. PERFORMED ENG LEAK CHEC
- [SDR FDEA202009142212](https://openairdocs.org/sdr/FDEA202009142212.md): Mechanism · broken · Sep 14, 2020 · N920FD · Boeing 75723A · Passenger/Crew Doors
  > DURING PRE-FLIGHT CHECK, FLIGHT CREW NOTE L1 DOOR MECHANISM IS BROKEN. REMOVED AND REPLACED COLLAR ASSY FROM THE L1 DOOR MECHANISM PER AMM 52-11-08-8. OPENED AND CLOSED THE L1 DOOR PER AMM 52-11-00-2,OPS TEST OK. A/C OK FOR SERVICE.
- [SDR FDEA2020061981284](https://openairdocs.org/sdr/FDEA2020061981284.md): Girt Bar · out of adjust · Jun 18, 2020 · N920FD · Boeing 75723A · Emergency Equipment
  > R1 DOOR IS VERY STICKY TO DISARM. PERFORMED RT DOOR GIRT BAR ADJUSTMENT PER AMM 52-11-25-5-0. PERFORMED OPERATIONAL CHECK ON RT DOOR AND FOUND OK PER THE SAME AMM 52-11-25-5-0.
- [SDR FDEA2020061091158](https://openairdocs.org/sdr/FDEA2020061091158.md): Unknown · malfunctioned · Jun 9, 2020 · N920FD · Boeing 75723A · Passenger/Crew Doors
  > UNABLE TO ARM RIGHT FWD ENTRY DOOR. OPS CHECK PER AMM 52-11-00-5, TEST SATIS, A/C OK FOR SERVICE.
- [SDR FDEA2020051390843](https://openairdocs.org/sdr/FDEA2020051390843.md): Slide · unserviceable · Apr 29, 2020 · N920FD · Boeing 75723A · Escape Slide
  > L1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBER D30654-122. SERNP M8047 MANUFACTER AIR CRUSERS SLIDE RAFT
- [SDR FDEA2020043090843](https://openairdocs.org/sdr/FDEA2020043090843.md): Slide · out of limits · Apr 29, 2020 · N920FD · Boeing 75723A · Escape Slide
  > L1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBER D30654-122. SERNP M8047 MANUFACTER AIR CRUSERS SLIDE RAFT
- [SDR FDEA2020021490329](https://openairdocs.org/sdr/FDEA2020021490329.md): Skin · damaged · Feb 9, 2020 · N920FD · Boeing 75728A · Cargo/Baggage Doors
  > MDIS 920 51-00 1440 09FEB20 LGG OPEN U AFT CARGODOOR AND SKIN BEHIND GOT HIT BY ULD ON THE DRIFT WITH HIGH WINDS, CARGO DOOR HAS A HOLE, SKIN BEHIND IS DEFORMED, DAMAGED TO BE ASSESSED, AIRCRAFT DOWN. COMPLIED WITH E A F-5330-T0352406 PT1
- [SDR FDEA201912133242](https://openairdocs.org/sdr/FDEA201912133242.md): Floor Panel · damaged · Dec 13, 2019 · N920FD · Boeing 75723A · Fuselage Floor Panel
  > AFT CARGO PANEL # 161AF DAMAGED REPLACED AFT CARGO PANEL 161AF IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING # 453N1805.

Next page: https://openairdocs.org/aircraft/N920FD/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 = 'N920FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N920FD/reports

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