# Service difficulty reports: N955FD

A list on [N955FD](https://openairdocs.org/aircraft/N955FD.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 2 · 62 reports

- [SDR FDEA202501090039](https://openairdocs.org/sdr/FDEA202501090039.md): Gust Lock · cracked · Jan 9, 2025 · N955FD · Boeing 757236 · Passenger/Crew Doors
  > R1 DOOR GUST LOCK - INOP. RELEASED FOR SERVICE PER MEL: 52-11-01-A. R1-GUST LOCK HOLD OPEN LOCK COLLAR CRACKED.
- [SDR FDEA202410051427](https://openairdocs.org/sdr/FDEA202410051427.md): Window · failed · Oct 5, 2024 · N955FD · Boeing 757236 · Flight Compartment Windows
  > LEFT FORWARD WINDSHIELD SHATTERED TWO HOURS INTO FLIGHT AT FL410. L FWD WINDOW EICAS MESSAGE. L FWD WINDOW HEAT INOP. QRC FOLLOWED. R&R'D L1 WINDOW PER M.M. 56-11-01-4. FIRST TORQUE ACCOMPLISHED AT 1230L. STILL REQUIRES CORD, SEALANT, AND 2ND AND 3RD TOR
- [SDR FDEA202405260730](https://openairdocs.org/sdr/FDEA202405260730.md): Bottle · blown · May 26, 2024 · N955FD · Boeing 757236 · Escape Slide
  > MDIS 955 52-20 8090 24MAY24 08:11 MEM FACT RAMP OPENED THE DOOR FROM THE INSIDE AND DOOR HAD BEEN ARMED,SLIDE FELL OUT AND BOTTLE BLOWN FACT 26MAY24 09:06 OAK AMM: 52-11-30-4 AMM: 25-66-01-4 AMM: 25-66-10-2 REPLACED LH (L1) DOOR SLIDE ASSY
- [SDR FDEA202405240727](https://openairdocs.org/sdr/FDEA202405240727.md): Reservoir · inoperative · May 24, 2024 · N955FD · Boeing 757236 · Emergency Equipment
  > RAMP OPENED THE DOOR FROM THE INSIDE AND DOOR HAD BEEN ARMED,SLIDE FELL OUT AND BOTTLE BLOWN. RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B. L1 SLIDE REMOVED? REMOVED SLIDE FROM L1 DOOR AND PLACED IN CARGO NET. DOOR FUNTIONS AS REQUIRED BOTTLE
- [SDR FDEA202307261316](https://openairdocs.org/sdr/FDEA202307261316.md): Flange · cracked · Jul 26, 2023 · N955FD · Boeing 757200 · Engine Thrust Reverser
  > NO. 1 R/H THRUST REVERSER OUTLET FLANGE FOR THE R/H HP3 BLEED VALVE, MISSING A SECTION OF THE FLANGE. M.W.T. REPAIRED OUTLET FLANGE REF. E.A. NO. F-7830-T0375434 REV NO. PS P1
- [SDR FDEA202209302419](https://openairdocs.org/sdr/FDEA202209302419.md): Tape · missing · Sep 30, 2022 · N955FD · Boeing 757236 · Standard Practices/Structures
  > LEFT ENGINE SURGED BRIEFLY DURING TO. DURING CLIMB AT 15,000 SURGING HAPPENED AGAIN 1.30 TO 1.48. FUEL FLOW, EGT FOLLOWED EPR. N1, N2 AND N3 SURGED ENOUGH TO YAW AIRCRAFT BUT DID NOT SURGE AS QUICKLY AT EPR, FUEL FLOW, AND EGT. SURGING HAPPENED IN CRUISE,
- [SDR FDEA202205061128](https://openairdocs.org/sdr/FDEA202205061128.md): Throttle · inoperative · May 6, 2022 · N955FD · Boeing 757236 · Power Lever
  > ON DESCENT INTO LAX LEFT THROTTLE WOULD NOT RETARD USING AUTO THROTTLES. DISCONNECTED AUTO THROTTLES AND TURNED OFF AT ARM SWITCH. STILL UNRESPONSIVE. AT FL 190 THROTTLE BECAME RESPONSIVE. CONTINUED ARRIVAL APPROACH AND LANDING USING MANUAL THROTTLES. CRU
- [SDR FDEA202201110212](https://openairdocs.org/sdr/FDEA202201110212.md): Splice · cracked · Jan 11, 2022 · N955FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR BEAM - UPPER CAP AFT FLANGE CRACKED, AT STA580, LBL45.5 COMPLIED WITH FEDEX EA: F-5310-T0366559 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR- REPAIR DOCUMENTATION
- [SDR FDEA202108122004](https://openairdocs.org/sdr/FDEA202108122004.md): Connector · loose · Aug 12, 2021 · N955FD · Boeing 757236 · Window System Wiring
  > FIRST OFFICER WINDOW CANNON PLUG LOOSE AND GETTING JAMMED IN TOP TRIM PIECE OF SLIDING WINDOW CANNON PLUG WAS SECURED OUT OF THE WAY. PERFORMED OPS CHCEK OF FO WINDOW REF B757 AMM 52-11-02-2. FO WINDOW OPEN ANS CLOSE NORMAL. OPS CHECK GOOD AIRCRA
- [SDR FDEA202107211831](https://openairdocs.org/sdr/FDEA202107211831.md): Gust Lock · failed · Jul 21, 2021 · N955FD · Boeing 757236 · Passenger/Crew Doors
  > FOUND L-1 DOOR GUST LOCK BROKEN., REPAIRED THE GUST LOCK.
- [SDR FDEA202012253207](https://openairdocs.org/sdr/FDEA202012253207.md): Actuator · twisted · Dec 25, 2020 · N955FD · Boeing 757236 · Cargo/Baggage Doors
  > WHILE RAMP WAS CLOSING MAIN CARGO DOOR, DOOR WOULD NOT CLOSE ALL THE WAY, TRIED TAKING THE DOOR TO FULL OPEN TO RESET DOOR. DOOR STILL WOULD GO CLOSED. ON LAST ATTEMPT TO OPEN DOOR WENT ABOUT 4 FOOT AND A LOUD POP. LOOKED AND AFT ACTUATOR WAS TWISTED. COMP
- [SDR FDEA2020062391294](https://openairdocs.org/sdr/FDEA2020062391294.md): Light · inoperative · Jun 19, 2020 · N955FD · Boeing 757236 · Emergency Lighting
  > RT EXTERNAL EMERGENCY LIGHT DOES NOT TEST. RELAMPED RT EMERGENCY SLIDE LIGHT REF AMM 33-51-06-2-1, OPS CHECKS GOOD.
- [SDR FDEA2020042310763](https://openairdocs.org/sdr/FDEA2020042310763.md): Skin · dented · Apr 21, 2020 · N955FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > OBSERVED SMALL DENT AND SCRATCH ON FUSELAGE. LEFT HAND SIDE BELOW CAPTS L2 WINDOW. REF WRI 56-10-5113, HFEC THE DENT ON NOSE SECTION OF AIRCRAFT, LEFT SIDE BELOW L3 WINDOW. MEASURED
- [SDR FDEA2020010980062](https://openairdocs.org/sdr/FDEA2020010980062.md): Seat Track · damaged · Jan 8, 2020 · N955FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGED SEAT TRACK AT STA 560 BL 0 REQUIRES REPAIR OR REPLACE REPAIRED SEAT TRACK AT STA 560 BL 0 IAW FEDEX EA#F-5320-T0351623
- [SDR FDEA2019123103332](https://openairdocs.org/sdr/FDEA2019123103332.md): Seat Track · corroded · Dec 30, 2019 · N955FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 578 RBL 45.50 SEAT TRACK HAS CORROSION. REMOVED DAMAGE AND RESTORED SURFACE PROTECTION IAW SRM 53-30-52-1A, 53-00 00-52-1A AND 51-20-01.
- [SDR FDEA2019123103331](https://openairdocs.org/sdr/FDEA2019123103331.md): Seat Track · corroded · Dec 30, 2019 · N955FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN BS 788 RBL 24.75 SEAT TRACK HAD CORROSION. REMOVED CORROSION FROM THE SEAT TRACK AT BS 788, RBL 24.75 IAW SRM 53-30-52-1A, AND SRM 51-20-01.
- [SDR FDEA201903060549](https://openairdocs.org/sdr/FDEA201903060549.md): Girt Bar · dirty · Mar 6, 2019 · N955FD · Boeing 757236 · Emergency Equipment
  > PDIS 955 25-60 4235 06MAR19 MSP FACT U LOGPAGES:2839823 COULDN'T ARM R1 DOOR ENTRY SLIDE. FACT 06MAR19 04:14 MSP U CLEANED GIRT BAR AND GIRT BAR FLOOR FITTINGS. DOOR ARMED NORMALLY SEVERAL TIMES. M/M REF 25-66-10.
- [SDR FDEA201805301332](https://openairdocs.org/sdr/FDEA201805301332.md): Axle · damaged · May 30, 2018 · N955FD · Boeing 757236 · Nose/Tail Landing Gear Strut/Axle
  > LEFT NOSE TIRE MISSING. PER ERS REQUEST ACCOMPLISHED NOSE LANDING GEAR SIDE LOAD INSPECTION REF AMM 05-51-01-2-99. NO DEFECTS NOTED. REMOVED AND REPLACED NLG AXLE. REMOVED P/N 162N1151-1 S/N 037AH91 CPN 3216237. INSTALLED P/N162N1151-3 S/N 81205 CPN 32161
- [SDR FDEA201805231305](https://openairdocs.org/sdr/FDEA201805231305.md): Sequence Valve · malfunctioned · May 23, 2018 · N955FD · Boeing 757236 · Landing Gear Position and Warning
  > AFTER TAKEOFF, THE MASTER CAUTION GEAR DISAGREE EICAS WITH GEAR LEVER IN THE UP POSITION. LANDING GEAR DISAGREE LIGHT WAS ILLUMINATED. ACFT DID NOT FEEL OR SOUND AS IF A GEAR WAS EXTENDED. FOLLOWED QRH AND RETURNED TO DEPARTURE. PERFORMED AN OPS CHECK OF T
- [SDR FDEA201803110651](https://openairdocs.org/sdr/FDEA201803110651.md): Girt Bar · out of adjust · Mar 11, 2018 · N955FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR WILL NOT ARM WHEN CLOSED. PERFORMED ADJ/TEST OF L1 DOOR GIRT BAR MECHANISM. OPS CHECKED GOOD IAW MM 52-11-25-5.
- [SDR FDEA201802060309](https://openairdocs.org/sdr/FDEA201802060309.md): Autothrottle Sys · malfunctioned · Feb 6, 2018 · N955FD · Boeing 757236 · Cabin Pressure Control System
  > LEFT ENGINE THRUST LEVER FROZE IN FLIGHT AT APROXIMTELY 1.5 EPR, WHILE PASSING 30,000 FT, TURNED AUTOTHROTTLES OFF AND MADE NO DIFFERENCE. ABLE TO BREAK LOOSE WITH A SUBSEQUENT BIND, BROKE FREE AGAIN AND WAS OK THE REMAINDER OF THE FLIGHT. PERFORMED AN IN
- [SDR FDEA201512023858](https://openairdocs.org/sdr/FDEA201512023858.md): Window · damaged · Dec 2, 2015 · N955FD · Boeing 757236 · Flight Compartment Windows
  > AT FLIGHT LEVEL 37000, LT OUTER WINDOW SHATTERED. R & R CAPTAINS FWD WINDOW L1 AMM 56-11-01-4. ALSO, R & R LT FWD RT SIDE WINDOW HEAT CONTROLLER IAW AMM 30-42-11-04. SYS OPERATIONS CHECKED GOOD IAW AMM 30-42-00-05 ADJUSTMENT TEST.
- [SDR FDEA201508112534](https://openairdocs.org/sdr/FDEA201508112534.md): Collar · broken · Aug 11, 2015 · N955FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. R & R L1 DOOR HOLD OPEN LOCK ASSEMBLY IAW MM 52-11-08-8. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201508102522](https://openairdocs.org/sdr/FDEA201508102522.md): Collar · broken · Aug 10, 2015 · N955FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. R & R L1 DOOR HOLD OPEN LOCK ASSEMBLY IAW MM 52-11-08-8. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201210053566](https://openairdocs.org/sdr/FDEA201210053566.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE AT FLAP STA 586.85. REPAIRED AS PER EA F-5730-162307. REPAIR IS MAJOR.
- [SDR FDEA201210053565](https://openairdocs.org/sdr/FDEA201210053565.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE AT FLAP STA 586.6. REPAIRED AS PER EA F-5730-162307. REPAIR IS MAJOR.
- [SDR FDEA201210053563](https://openairdocs.org/sdr/FDEA201210053563.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL SURFACE FOUND TOOL MARK ON SCREW HOLES AT FLAP STA 341.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201210053564](https://openairdocs.org/sdr/FDEA201210053564.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON HOLE AT FLAP STA 585.85. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201210053562](https://openairdocs.org/sdr/FDEA201210053562.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLES AT FLAP STA 338.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201210053561](https://openairdocs.org/sdr/FDEA201210053561.md): Skin · damaged · Oct 5, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE FLAP STA 585.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201210043550](https://openairdocs.org/sdr/FDEA201210043550.md): Floorbeam · corroded · Oct 4, 2012 · N955FD · Boeing 757236 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 720, RBL 61 HAS CORROSION ON UPPER TEE. REPAIR CARRIED OUT ON FLOORBEAM AT STA 720, RBL 61, IAW EA F-5310-162316, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201210043551](https://openairdocs.org/sdr/FDEA201210043551.md): Floorbeam · corroded · Oct 4, 2012 · N955FD · Boeing 757236 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 760 RBL 51 HAS CORROSION AT UPPER TEE. REPAIR CARRIED OUT IAW EA F-5310-162315, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201209273472](https://openairdocs.org/sdr/FDEA201209273472.md): Frame · corroded · Sep 27, 2012 · N955FD · Boeing 757236 · Fuselage Main, Frame
  > FOUND CORROSION ON TOP OF FRAME BS 1380, BETWEEN STRINGER 26R AND 28R. REPAIRED IAW EA F-5310-162305, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201209263451](https://openairdocs.org/sdr/FDEA201209263451.md): Skin · damaged · Sep 26, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL NR 3 FROM INBD, FIVE HOLES FOUND ELONGATED. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201209263449](https://openairdocs.org/sdr/FDEA201209263449.md): Skin · damaged · Sep 26, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL NR1 FROM INBD FIVE HOLES FOUND ELONGATED. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201209263448](https://openairdocs.org/sdr/FDEA201209263448.md): Skin · damaged · Sep 26, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE. REPAIRED AS PER E.A. F-5730-162307 PART 1.
- [SDR FDEA201209263447](https://openairdocs.org/sdr/FDEA201209263447.md): Skin · damaged · Sep 26, 2012 · N955FD · Boeing 757236 · Trailing Edge Flaps
  > RT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND DAMAGED ON SCREW HOLE AT 337.85. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.
- [SDR FDEA201209123300](https://openairdocs.org/sdr/FDEA201209123300.md): Frame · corroded · Sep 12, 2012 · N955FD · Boeing 757236 · Cargo/Baggage Doors
  > AFT CARGO DOOR HAS CORROSION AT BASE OF SNAP FASTENERS RETAINERS, FWD SIDE OF DOOR. AFT CARGO DOOR FRAME CORROSION REPAIR CARRIED OUT IAW EA F-5230-162301, PART 1.1. REPAIR IS MAJOR.
- [SDR FDEA201209043216](https://openairdocs.org/sdr/FDEA201209043216.md): Frame · chafed · Sep 4, 2012 · N955FD · Boeing 757236 · Fuselage Main, Frame
  > CABIN, FRAME AT BS 1289 HAS CHAFED AT STR 15L TO 16L. REPAIRED IAW EA F-5310-163116, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201208303199](https://openairdocs.org/sdr/FDEA201208303199.md): Floorbeam · corroded · Aug 30, 2012 · N955FD · Boeing 757236 · Fuselage Main, Floor Beam
  > CABIN, FLOORBEAM AT STA 1640, RBL 56 HAS CORROSION ON UPPER TEE. REPAIR CARRIED OUT IAW EA F-5310-161098, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201208283185](https://openairdocs.org/sdr/FDEA201208283185.md): Skin · scratched · Aug 28, 2012 · N955FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN AT STA 310-324, STR 17L -18L SCRATCHED. REPAIRED IAW SRM 53-00-01 FIG.201, REPAIR 16, REV.106. REPAIR IS MAJOR.
- [SDR FDEA201208273180](https://openairdocs.org/sdr/FDEA201208273180.md): Structure · corroded · Aug 27, 2012 · N955FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF RT SIDE CENTER TRANSITION PANEL, STA 1378 TO STA 1442, FOUND UPPER CHORD LOWER SURFACE HAS CORROSION AROUND ANCHOR NUT HOLES.
- [SDR FDEA201208273179](https://openairdocs.org/sdr/FDEA201208273179.md): Crease Beam · corroded · Aug 27, 2012 · N955FD · Boeing 757236 · Fuselage Main, Structure
  > CABIN, DOOR 3L STA 1320 TO 1340, CREASE BEAM WEB HAS CORROSION ON LOWER SURFACE. REMOVED AND REPLACED WITH CREASE BEAM FABRICATED AS PER DWG 146N8326 SHT.1 REV.C AND INSTALLED IAW DWG 146N8322 SHT.3 REV.- AND SRM 51-40-02 REV.106. REPAIR IS MAJOR.
- [SDR FDEA201208243146](https://openairdocs.org/sdr/FDEA201208243146.md): Strap · corroded · Aug 24, 2012 · N955FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > EMPENNAGE RT APU CUT-OUT AREA THE OUTER SPLICE STRAP AT BS 1825 STR 2-7 RT HAS INTERGRANULAR CORROSION. R & R WITH STRAP FABRICATED IAW DWG 148N3138, SHT 1, REV C AND INSTALLED IAW DWG 148N3105, SHT 5 REV -. REPAIR IS MAJOR;
- [SDR FDEA201208183069](https://openairdocs.org/sdr/FDEA201208183069.md): Angle · corroded · Aug 18, 2012 · N955FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > BS 1787 AT STR 6 CORRODED ON THE FWD LOWER NUTPLATE FOR APU INLET HOUSING MOUNT. R & R WITH ANGLE FABRICATED IAW DWG 148N3141, SHT 1, REV B AND INSTALLED IAW DWG 148N3105, SHT 5, REV. REPAIR IS MAJOR.
- [SDR FDEA201208183066](https://openairdocs.org/sdr/FDEA201208183066.md): Stringer · chafed · Aug 18, 2012 · N955FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > BS 880 TO 900, STRINGER 15L CHAFED. REPAIRED IAW EA F-5310-161099, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201208153006](https://openairdocs.org/sdr/FDEA201208153006.md): Floorbeam · damaged · Aug 15, 2012 · N955FD · Boeing 757236 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 377.7, LBL 19 - LBL 24, HAS DAMAGED HOLES. R & R FLOORBEAM, FABRICATED NEW FLOORBEAM IAW DWG 1415123, SHT 1, REV A AND INSTALLED IAW DWG 141N5113, SHT 1 REV F. MAJOR REPAIR.
- [SDR FDEA201208153010](https://openairdocs.org/sdr/FDEA201208153010.md): Frame · chafed · Aug 15, 2012 · N955FD · Boeing 757236 · Fuselage Main, Frame
  > FRAME AT BS 1280 CHAFED AT STR 13 L. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG. 201, REV.106. REPAIR IS MAJOR.
- [SDR FDEA201208153008](https://openairdocs.org/sdr/FDEA201208153008.md): Frame · chafed · Aug 15, 2012 · N955FD · Boeing 757236 · Fuselage Main, Frame
  > CABIN BS 1280 FRAME CHAFED AT STR 12 L. REPAIRED IAW SRM 53-00-07 REPAIR 3, FIG. 201, REV.106. REPAIR IS MAJOR.
- [SDR FDEA201208153011](https://openairdocs.org/sdr/FDEA201208153011.md): Deck Plate · corroded · Aug 15, 2012 · N955FD · Boeing 757236 · Fuselage Floor Panel
  > CABIN DECK PLATE AT STA 1712 LBL 20 (APPROX) HAS CORROSION. REPAIRED IAW EA F-5300-161100, PART 1, REPAIR IS MINOR.

Next page: https://openairdocs.org/aircraft/N955FD/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 = 'N955FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N955FD/reports

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