# Service difficulty reports: N950FD

A list on [N950FD](https://openairdocs.org/aircraft/N950FD.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 · 97 reports

- [SDR FDEA202604140446](https://openairdocs.org/sdr/FDEA202604140446.md): Bulb · failed · Apr 14, 2026 · N950FD · Boeing 757236 · Emergency Lighting
  > DURING MX PRE-FLIGHT EMERGENCY LIGHT TEST, FOUND L1 DOOR EXIT SIGN SEEMS DIM. REMOVED AND REPLACED 9 FAULTY BULBS AT THE L1 EXIT SIGN IAW AMM 33-51-01-2. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202505070724](https://openairdocs.org/sdr/FDEA202505070724.md): Lamp · failed · May 7, 2025 · N950FD · Boeing 757236 · Emergency Lighting
  > R SLIDE LIGHT INOP. AMM: 33-51-06-2-1 RELAMPED R/H SLIDE LIGHT I/A/W AMM REFERENCED ABOVE, GOOD FOE SERVICE.
- [SDR FDEA202411221716](https://openairdocs.org/sdr/FDEA202411221716.md): Handle · no discrepancy · Nov 22, 2024 · N950FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR EXTERNAL DOOR HANDLE NOT OPERATING PROPERLY. INSPECTED AND OPERATED DOOR MULTIPLE TIMES PER AMM 12-21-18-13. DOOR OPERATES AS IT SHOULD. NO FAULTS FOUND. AC OK TO CONTINUE
- [SDR FDEA202403180307](https://openairdocs.org/sdr/FDEA202403180307.md): Seal · failed · Mar 18, 2024 · N950FD · Boeing 757236 · Flight Compartment Windows
  > R FWD WINDOW SHATTERED AT 360 AFTER ST ELMO FIRE. DIDN T HEAR AIR LEAK. STARTED R/R OF F/O`S WINDSHIELD IAW AMM 56-11-01-4. NEW WINDOW INSTALLED AND FIRST TORQUE SEQUENCE IS COMPLETED. STILL REQUIRES CORD INSTALLATION, SEALANT, REMAINDER OF TORQUE SEQUENCE
- [SDR FDEA202312151941](https://openairdocs.org/sdr/FDEA202312151941.md): Gust Lock · cracked · Dec 15, 2023 · N950FD · Boeing 757200 · Passenger/Crew Doors
  > DURING POST FLIGHT, FOUND L1 DOOR GUST LOCK COLLAR BROKEN. REMOVED BROKEN COLLARS. PLACARD INSTALLED. A/C OK TO CONTINUE USING R1 DOOR. L1 DOOR INOP. REMOVED BROKEN COLLARS. PLACARD INSTALLED. A/C OK TO CONTINUE USING R1 DOOR. REPLACED HOLD-OPEN LOC
- [SDR FDEA202306211074](https://openairdocs.org/sdr/FDEA202306211074.md): Drag Fitting · unknown · Jun 21, 2023 · N950FD · Boeing 757200 · Wing Structure
  > LT PYLON HAS 2 CRACK INDICATIONS AT #6 HOLE, 2 O'CLOCK & 7 O'CLOCK POSITIONS IN THE FITTING. 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #6
- [SDR FDEA202306211073](https://openairdocs.org/sdr/FDEA202306211073.md): Drag Fitting · unknown · Jun 21, 2023 · N950FD · Boeing 757200 · Wing Structure
  > LT PYLON HAS 1 CRACK INDICATION AT #3 HOLE, 6 O'CLOCK POSITION IN THE SKIN, 0.250 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WNG UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #3.
- [SDR FDEA202306211072](https://openairdocs.org/sdr/FDEA202306211072.md): Drag Fitting · unknown · Jun 21, 2023 · N950FD · Boeing 757200 · Wing Structure
  > LT PYLON HAS 1 CRACK INDICATION AT #8 HOLE 3 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #8.
- [SDR FDEA202306211071](https://openairdocs.org/sdr/FDEA202306211071.md): Drag Fitting · unknown · Jun 21, 2023 · N950FD · Boeing 757200 · Wing Structure
  > LT PYLON HAS 2 CRACK INDICATIONS AT #7 HOLE, 12 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #7.
- [SDR FDEA202302030200](https://openairdocs.org/sdr/FDEA202302030200.md): Transmission · failed · Feb 3, 2023 · N950FD · Boeing 757* · Trailing Flap Position Indicating System
  > PDIS 950 27-51 9670 03FEB23 MEM OPEN U TE FLAP DISAGREE DURING APPROACH. RAN QRH. ALTERNATE FLAP EXTENSION WORKED AS ADVERTISED. DIVERTED TO MEM. LANDED FLAPS 20 PER QRH GUIDANCE. EMERGENCY DECLARED. ***EMERGENCY DECLARED*** REMOVED AND RE
- [SDR FDEA202209132339](https://openairdocs.org/sdr/FDEA202209132339.md): Bearing · failed · Sep 13, 2022 · N950FD · Boeing 757236 · Trailing Edge Flap Control System
  > TE FLAP ASYM EICAS MSG AFTER SELECTING FLAPS 20. SPEED WAS 170 KTS AT 2000 FT. FLAP INDICATORS ARE SPLIT AT FLAPS 15. RIGHT WING WANTED TO COME UP. EMERGENCY DECLARED. FOUND LH OUTBOARD FLAP INBOARD TRACK UPPER ROLLER BEARINGS BADLY DAMAGED. PARTS
- [SDR FDEA202112083047](https://openairdocs.org/sdr/FDEA202112083047.md): None · none · Dec 8, 2021 · N950FD · Boeing 757200 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF AND RAISING GEAR HANDLE WE RECEIVED EICAS: GEAR DISAGREE & GEAR DOORS ALONG WITH GEAR AND DOORS LIGHTS. RETURNED TO IND AND GEAR EXTENDED NORMALLY. NO EMERGENCY DECLARED. CREW REPORTED LOUD NOISE WITH THE ALERTS ON. THEY SUSPECTED TH
- [SDR FDEA202012223196](https://openairdocs.org/sdr/FDEA202012223196.md): Line · out of position · Dec 22, 2020 · N950FD · Boeing 757236 · Emergency Equipment
  > RT FWD ENTRY DOOR WILL NOT ARM, NO SLIDE LIGHT. FOUND STATIC LINE INTERFERE WITH GIRT BAR. REPOSITION STATIC LINE AS REQUIRED. OPERATIONS CHECK NORMAL, REF B757-200 MM 25-66-01-4.
- [SDR FDEA2020090311872](https://openairdocs.org/sdr/FDEA2020090311872.md): Light · malfunctioned · Aug 13, 2020 · N950FD · Boeing 757236 · Emergency Equipment
  > RT CABIN DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN DOOR ARMED. OPERATED DOOR PER AMM 25-66-00-5. OK FOR SERVICE.
- [SDR FDEA2020081431872](https://openairdocs.org/sdr/FDEA2020081431872.md): Unknown · unknown · Aug 13, 2020 · N950FD · Boeing 757236 · Escape Slide
  > R CABIN DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN DOOR ARMED. OPERATED DOOR PER AMM 25-66-00-5. OK FOR SERVICE
- [SDR FDEA2020041750748](https://openairdocs.org/sdr/FDEA2020041750748.md): Element · failed · Apr 15, 2020 · N950FD · Boeing 757236 · Fire Detection
  > APU WHEN PUT ON LINE FIRE BOTTLE BLEW, APU FIRE WARNING LIGHT HORN ON CONSTANT, SHUT OFF APU RESET THE HORN FIRE WARNING. LIGHT OUT BUT FIRE BOTTLE SQUIBS FIRED. [APU FIRE LP1 STATUS] APU BTL [ECAS MSG]. REMOVED AND REPLACED LWR APU FIRE DET ELEMENT REF MM 26
- [SDR FDEA2020032980612](https://openairdocs.org/sdr/FDEA2020032980612.md): Warning System · false activation · Mar 28, 2020 · N950FD · Boeing 757236 · Door Warning System
  > INTERMITTANT R EMER DOOR ADVISORY AT BLOCK - IN HAD NO "R EMER DOOR" ADVISORY. VISUALLY CHECKED DOOR AND VERIFED IT WAS CLOSED WITH HANDLE LOCK PLATED STILL INSTALLED REF B757 AMM 52-21-01-2. COMPLETED #3 R EMER EXIT DOOR SENSOR TARGET TEST OF PSEU WI
- [SDR FDEA201901160151](https://openairdocs.org/sdr/FDEA201901160151.md): Warning System · activated · Jan 16, 2019 · N950FD · Boeing 757236 · Leading Edge Slat Position Indicating System
  > PDIS 950 27-80 6538 16JAN19 LOGPAGES:3084577 WHEN CONFIGURING FOR APPROACH RECEIVED MASTER CAUTION AND EICAS MASSAGE LE SLAT DISAGREE. RAN QRH, DECLARED EMERGENCY AND LANDED FLAPS 20.
- [SDR FDEA201708182273](https://openairdocs.org/sdr/FDEA201708182273.md): Floorbeam · cracked · Aug 18, 2017 · N950FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CARGO BAY STUB FLOORBEAM AT BS 580, LBL 45.5 - 58.22, AFT FLANGE IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND DWG 657N4311, REV -.
- [SDR FDEA201708102173](https://openairdocs.org/sdr/FDEA201708102173.md): Shear Plate · cracked · Aug 10, 2017 · N950FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CARGO BAY SHEAR PLATE IS CRACKED AT BS 580, LBL 45.5. REPAIRED THE SHEAR PLATE IAW EA F-5310-T0334835 P1.
- [SDR FDEA201708082148](https://openairdocs.org/sdr/FDEA201708082148.md): Seat Track · corroded · Aug 8, 2017 · N950FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON COURIER SEAT TRACK R1 DOOR ENTRY BS 345 TO 377, LBL 5. REMOVED CORROSION, HAD 100% MATERIAL LOSS AND IS OUT OF LIMITS. FABRICATED A NEW SEAT TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, 51-10-02, 53-00-52-1A, 51-40-05 AND DWGS
- [SDR FDEA201708042116](https://openairdocs.org/sdr/FDEA201708042116.md): Seat Track · cracked · Aug 4, 2017 · N950FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT SEAT TRACK AT BS 580 LBL 45.5 IS CRACKED ON IB FLANGE AT FLOORBEAM. REMOVED THE SEAT TRACK. FABRICATED A REPLACEMENT SEAT TRACK AND INSTALLED IAW SRM 51-40-02 AND DWG 143N5090, REV-, AND 143N5080, REV A.
- [SDR FDEA201708022097](https://openairdocs.org/sdr/FDEA201708022097.md): Door Frame · punctured · Aug 2, 2017 · N950FD · Boeing 757236 · Fuselage Main, Structure
  > TOP OF LOWER FRAME PUNCTURED BS 231 AT THE FORWARD ACCESSORY DOOR CUTOUT. COMPLIED WITH FED EX EA F-5310-T0334685 P1. REPAIRED THE DOOR FRAME IAW SRM 53-00-00-07-1A. REMOVED DAMAGE TO.500 DIA, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW EA F-5310-T033
- [SDR FDEA201704111133](https://openairdocs.org/sdr/FDEA201704111133.md): Slide · malfunctioned · Apr 11, 2017 · N950FD · Boeing 757236 · Escape Slide
  > AFTER SHUTDOWN ON ACFT EXIT FAILED TO DRM LEFT DOOR STOPPED BEFORE BLOWING SLIDE. REMOVED AND REPLACED L1 DOOR ESAPE SLIDE, OP CHECKED GOOD IAW MM 25-66-01-4-0.
- [SDR FDEA201610273723](https://openairdocs.org/sdr/FDEA201610273723.md): Light · inoperative · Oct 27, 2016 · N950FD · Boeing 757236 · Emergency Lighting
  > L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. RELAMPED L1 DOOR SLIDE LIGHT IAW AMM 25-66-00-5. OPS CHECK GOOD. A/C OK TO CONTINUE.
- [SDR FDEA201607062295](https://openairdocs.org/sdr/FDEA201607062295.md): Unknown · malfunctioned · Jul 6, 2016 · N950FD · Boeing 757236 · AC Generation System
  > ON INITIAL TAKEOFF AT APPROXIMATELY 30 KTS, LT GENERATOR OFF, LT BUSS TIE IS LN. LEFT BUSS OFF, RETURNED TO GATE. RELEASED FOR SERVICE IAW MEL 24-00-01, CATEGORY B EXPIRATION, MEL 24-00-01, LT IDENTIFY LT OR RT, GENERATOR INOPERATIVE. ASSOCIATED IDG DISCONN
- [SDR FDEA201606252138](https://openairdocs.org/sdr/FDEA201606252138.md): Switch · inoperative · Jun 25, 2016 · N950FD · Boeing 757236 · DC Generating System
  > RIGHT IRS DC FAIL ILLUMINATED MOMENTARILY AND EXTINGUISHED IN CRUISE; NO OTHER LIGHTS BUT SOME NOISE LIKE A RELAY OPENING AND CLOSING OCCURED ON THE F/O SIDE NEAR EFB OUTLET. SOME PERIOD OF TIME LATER THE LT A/C BUS FAILED, EQUIPMENT OVERHEAT ILLUMINATED WITH
- [SDR FDEA201604291427](https://openairdocs.org/sdr/FDEA201604291427.md): Fan · out of balance · Apr 29, 2016 · N950FD · Boeing 757236 · Turbine Engine Compressor Section
  > EXCESSIVE N1 VIBRATION ON LT ENG DURING TAKEOFF & CLIMB. N1 STAYED IN AMBER BAND. RAN QRH PROCEDURE & UNABLE TO OBTAIN CLIMB POWER. RETARDED THROTTLE TO OPERATE BELOW AMBER BAND & RETURNED. PERFORMED FAN TRIM BALANCE OF LT ENG IAW AMM 71-00-00-5-3 TEST 7.
- [SDR FDEA201601260327](https://openairdocs.org/sdr/FDEA201601260327.md): Housing · broken · Jan 26, 2016 · N950FD · Boeing 757236 · Emergency Equipment
  > FIRST OFFICERS SIDE, ESCAPE ROPE COVER WILL NOT STAY IN UPPER LATCH, HOUSING BROKEN. R & R FIRST OFFICERS SIDE ESCAPE ROPE COVER IAW AMM 25-61-00-4. COMPLIED WITH EA F-2510-T0322978. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201510233331](https://openairdocs.org/sdr/FDEA201510233331.md): Light · inoperative · Oct 23, 2015 · N950FD · Boeing 757236 · Emergency Lighting
  > SERVICE CHECK, L1 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. RELAMPED L1 DOOR EMER ESCAPE SLIDE LIGHT IAW AMM 33-51-06-2-1, USING BULB PN 767 LAMP, 6VDC 2 AMP. OPERATIONS NORMAL, OK FOR SERVICE.
- [SDR FDEA201508102525](https://openairdocs.org/sdr/FDEA201508102525.md): Skin · gouged · Aug 10, 2015 · N950FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED WITH GOUGE IN THE CENTER AT STRINGER 19L, BS 460. COMPLIED WITH EA F-5330-T0319367 P1.
- [SDR FDEA201508102524](https://openairdocs.org/sdr/FDEA201508102524.md): Skin · cracked · Aug 10, 2015 · N950FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BS 558, BETWEEN STRINGERS 28 & 29L. CUT OUT DAMAGED AREA IAW SRM 53-00-01-2 R16. FABRICATED REPAIR DOUBLER IAW SRM 53-00-01-2R16. ALODINE & PRIMED IAW SRM 51-20-01. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01-2R.
- [SDR FDEA201501220260](https://openairdocs.org/sdr/FDEA201501220260.md): Light · inoperative · Jan 22, 2015 · N950FD · Boeing 757236 · Emergency Equipment
  > 1R SLIDE ARM LIGHT INOPERATIVE. RELAMPED R1 SLIDE ANNUNCIATOR IAW AMM P2F1 25-6 6-00. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201408052082](https://openairdocs.org/sdr/FDEA201408052082.md): Skin · damaged · Aug 5, 2014 · N950FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT OTBD AFT FLAP BOTTOM PUNCTURED & TOP CRACKED OTBD OF OTBD FAIRING. REPAIRED OTBD AFT FLAP TE IAW SRM 57-53-01 & SRM 51-70-04 PARA B & PARA G FIG 9. TOP SURFACE REPAIR DIMENSIONS ARE 11.75 X 6 INCHES & DIMENSION OF LOWER SURFACE REPAIR IS A 2 INCH CIRCL
- [SDR FDEA201406171477](https://openairdocs.org/sdr/FDEA201406171477.md): Seal · unsecure · Jun 17, 2014 · N950FD · Boeing 757236 · Fuselage Main, Structure
  > FIRST OFFICER`S WINDOW WILL NOT CLOSE. WINDOW CONTACTING UPPER AFT WINDOW SEAL. SECURED SEAL, WINDOW OPS NORMAL IAW AMM 56-11-04-4.
- [SDR FDEA201401150120](https://openairdocs.org/sdr/FDEA201401150120.md): Control Rod · bent · Jan 15, 2014 · N950FD · Boeing 757236 · Door Warning System
  > R1 ARMING INDICATOR RETRACTABLE DOOR STICKY & HAS A WEAK SPRING. RELEASED FOR SERVICE IAW MEL 52-11-01-B. IDENTIFY L1 & OR R1 DOOR SLIDES, INOPERABLE OR MISSING. NO JUMP SEATER OR ACM ARE TO OCCUPY COURIER AREA IN FLIGHT. ARM INDICATOR RETRACTABLE DOOR CON
- [SDR FDEA201311152792](https://openairdocs.org/sdr/FDEA201311152792.md): Bearing · broken · Nov 15, 2013 · N950FD · Boeing 757236 · Passenger/Crew Doors
  > FOUND L1 DOOR HARD TO CLOSE. DISCOVERED BROKEN BEARING ON CRANK ROLLER IN UPPER CORNER. INSTALLED BEARING, DOOR OPERATES NORMAL.
- [SDR FDEA201309272334](https://openairdocs.org/sdr/FDEA201309272334.md): Control Unit · failed · Sep 27, 2013 · N950FD · Boeing 757236 · Windshield/Door Rain/Ice Removal
  > FL 400, CAPTAIN`S LT FWD WINDOW CRACKED, EICAS MESSAGE LT FWD WINDOW. NO DEFORMATION OR AIR LEAKAGE NOTED. REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT MM 30-41-01-4 AND REMOVED AND REPLACED WINDOW IAW AMM 56-11-01-4.
- [SDR FDEA201307241645](https://openairdocs.org/sdr/FDEA201307241645.md): Skin · damaged · Jul 24, 2013 · N950FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BS 585 BETWEEN S29 - 30L. BLENDED OUT AREA AND FOUND AREA CRACKED. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FABRICATED FILLER. INSTALLED REPAIR IAW SRM 53-00-01, NDTM PT6 51-00-10, NDTM PT6 51-00-19, SRM 53-00-
- [SDR FDEA201206202276](https://openairdocs.org/sdr/FDEA201206202276.md): Terminal · loose · Jun 20, 2012 · N950FD · Boeing 757236 · Light System Wiring
  > RT INTERIOR EMERGENCY EXIT LIGHT DOES NOT TEST. FOUND GROUND GD498-DC LOOSE AT TERMINAL STUD. TIGHTENED TERMINAL AT GROUND STUD REF SMP. PERFORMED OPS TEST OF INTERIOR EMERGENCY LIGHTING WITH TEST SWITCHES REF AMM SUP 33-51-00 501. EMERG LIGHTING, OPS CH
- [SDR FDEA201206192270](https://openairdocs.org/sdr/FDEA201206192270.md): Terminal · loose · Jun 19, 2012 · N950FD · Boeing 757236 · Light System Wiring
  > RT INTERIOR EMERGENCY EXIT LIGHT DOES NOT TEST. FOUND GROUND GD498-DC LOOSE AT TERMINAL STUD. TIGHTENED TERMINAL AT GROUND STUD REF SMP. PERFORMED OPS TEST OF INTERIOR EMERGENCY LIGHTING WITH TEST SWITCHES REF AMM SUP 33-51-00 501. EMERGENCY LIGHTING, OPS
- [SDR FDEA201203201035](https://openairdocs.org/sdr/FDEA201203201035.md): Guard · damaged · Mar 20, 2012 · N950FD · Boeing 757236 · Emergency Lighting
  > EMERGENCY LIGHTS ARMING SWITCH MUST BE MANUALLY ARMED. DOES NOT ARM OR TURN OFF WHEN CLOSING OR OPENING SWITCH HANDLE. REMOVED AND REPLACED PILOTS EMERGENCY LIGHT SWITCH GUARD ON P-5 PANEL PER SMP. OPS CHECKEDS GOOD PER MM 33-51-00-5
- [SDR FDEA201108193375](https://openairdocs.org/sdr/FDEA201108193375.md): Structure · corroded · Aug 19, 2011 · N950FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT LWR CARGO BAY, AFTER REMOVAL OF SUPPORT FITTING AT LOWER SILL NR 2 DOOR CUTOUT AREA. CORROSION FOUND UNDER SUPPORT FITTING ON LOWER CHORD STA 1415 - 1425. REPAIRED AS PER E.A. F-5310-152512. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201108113202](https://openairdocs.org/sdr/FDEA201108113202.md): Frame · corroded · Aug 11, 2011 · N950FD · Boeing 757236 · Fuselage Main, Frame
  > AFT LOWER CARGO COMP WHILE CARRYING OUT REPAIR CORROSION WAS EXPOSED WHILE REMOVING SEALANT AT STA 1400, FRAME LWR STRAP, BETWEEN STRINGERS S26L -26R. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV. 103. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201108103180](https://openairdocs.org/sdr/FDEA201108103180.md): Fairing · gouged · Aug 10, 2011 · N950FD · Boeing 757236 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 260.0. PUNCTURED SKIN REPAIRED IAW EA F-5480-150719. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201108103179](https://openairdocs.org/sdr/FDEA201108103179.md): Fairing · gouged · Aug 10, 2011 · N950FD · Boeing 757236 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN OTBD SIDE FOUND WITH GOUGE MARK AT PP STA 260.0. REPAIR CARRIED OUT ON GOUGED SKIN IAW EA F-5480-150720. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201108103178](https://openairdocs.org/sdr/FDEA201108103178.md): Skin · gouged · Aug 10, 2011 · N950FD · Boeing 757236 · Nacelle/Pylon, Plate/Skin
  > NR 2 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 260.0. PUNCTURED SKIN REPAIRED IAW EA F-5480-150720. (RT PYLON AFT FAIRING PAN GOUGE REPAIR). REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201107112636](https://openairdocs.org/sdr/FDEA201107112636.md): Skin · corroded · Jul 11, 2011 · N950FD · Boeing 757236 · Nacelle/Pylon, Plate/Skin
  > NR1 PYLON UPPER WEB DOUBLER EXTERNAL SKIN AT PPSTA 196.2 FOUND WITH CORROSION. R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201107112635](https://openairdocs.org/sdr/FDEA201107112635.md): Beam · dented · Jul 11, 2011 · N950FD · Boeing 757236 · Cargo/Baggage Doors
  > FWD LWR CARGO NR1 DOOR CENTER EDGE BEAM LWR SURFACE SKIN HAS 2 EA DENTS. DENTS ARE APPROX 1 INCH IN DIAMETER. R & R BEAM IAW EA F-5230-152516. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201107092619](https://openairdocs.org/sdr/FDEA201107092619.md): Shim · unknown · Jul 9, 2011 · N950FD · Boeing 757236 · Nacelle/Pylon Miscellaneous Structure
  > WHILE COMPLYING SSIP MOD TO NR 1 STRUT ASSY STRUCTURE, CLEARANCE OF MORE THAN 0.040" SHIMS THICKNESS REQUIRED BETWEEN LOWER SPAR FITTING AND AFT BULKHEAD. ACCOMPLISHED E.A. F-5450-150743. REPAIR IS CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N950FD/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 = 'N950FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N950FD/reports

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