# Service difficulty reports: N960FD

A list on [N960FD](https://openairdocs.org/aircraft/N960FD.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 · 99 reports

- [SDR FDEA202610201632](https://openairdocs.org/sdr/FDEA202610201632.md): Switch · inoperative · Oct 20, 2026 · N960FD · Boeing 757236 · Emergency Lighting
  > WHEN EMERGENCY LIGHT SWITCH WAS TURNED OFF, AFTER SHUTDOWN, THE UNARMED LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED UNARMED LIGHT HOUSING ASSY IAW SWPM20-84-18. OPS CHECKED NORMAL, UNARMED ANNUNCIATOR LIGHT REMAINS ILLUMINATED WITH EMERGENCY EXIT SWITCH
- [SDR FDEA202610051480](https://openairdocs.org/sdr/FDEA202610051480.md): Battery · inoperative · Oct 5, 2026 · N960FD · Boeing 757236 · Emergency Lighting
  > DURING PRE-FLIGHT TEST OF EMERGENCY LIGHTS AND FOLLOW UP OPERATION, THE RIGHT SIDE LIGHTS DID NOT REMAIN ILLUMINATED FOR MORE THAN A FEW SECONDS. THE LEFT SIDE WAS NORMAL. AMM 33-51-07-2 REPLACED M730 BATTERY PACK: SOURCE MANUFACTURING, OPS NORMAL. OK
- [SDR FDEA202401180086](https://openairdocs.org/sdr/FDEA202401180086.md): Stringer Splice · corroded · Jan 18, 2024 · N960FD · Boeing 757200 · Fuselage Main, Longeron/Stringer
  > DOT NO. 94-094 AFT CARGO STA 1460 FOUND CORROSION ON STINGER SPLICE S29 IN TWO SPOTS. REMOVED AND REPLACED CORRODED STRINGER SPLICE AT STA. 1460 S29 IAW DWG.146N3820, FABRICATED SPLICE CHANNEL ON VTMAE TRAVELER T24/1726453, MAJOR REPAIR
- [SDR FDEA202302280349](https://openairdocs.org/sdr/FDEA202302280349.md): None · none · Feb 28, 2023 · N960FD · Boeing 757200 · Standard Practices/Structures
  > STRONG ORDER OF PAINT THINNER AT LEVEL OFF. COMPLIED WITH FUMES CHECKLIST IN QRH. USED 100% OXYGEN FOR REMAINDER OF FLIGHT. EMERGENCY DECLARED. CONFIRMED SPILL IN D.G. CONTAINER. (ENTERED FOR FLIGHT CREW MEMBER 5148579 OVER PHONE. GMM: 03-4-200 MET
- [SDR FDEA202209242367](https://openairdocs.org/sdr/FDEA202209242367.md): Lens · cracked · Sep 24, 2022 · N960FD · Boeing 757236 · Emergency Lighting
  > DURING SERVICE CHECK FOUND RIGHT EXTERIOR SLIDE LT INOP REF AMM 33-51-06-2-1. INSTALLED R/H OUTER EMERGENCY LIGHT GASKET AND NEW LENS COVER AND BATTERY PACK. OPS CHECK GOOD ON ALL EMERGENCY LIGHTS.
- [SDR FDEA202202070238](https://openairdocs.org/sdr/FDEA202202070238.md): None · none · Feb 7, 2022 · N960FD · Boeing 757200 · Leading Edge Slat Control System
  > #6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED,REPLACED, ADJUSTED AND OPS CHECK IAW B7578 AMM 27-81-01-4 AND FEDEX EA F- 5750-T0366777
- [SDR FDEA202202070239](https://openairdocs.org/sdr/FDEA202202070239.md): None · none · Feb 7, 2022 · N960FD · Boeing 757200 · Leading Edge Slat Control System
  > #1 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK IAW B757-2 AMM 27-81-01-4
- [SDR FDEA202202070237](https://openairdocs.org/sdr/FDEA202202070237.md): None · none · Feb 7, 2022 · N960FD · Boeing 757200 · Leading Edge Slat Control System
  > #5 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK #5 SLAT IAW B757 AMM 27-81-01-4
- [SDR FDEA202202030209](https://openairdocs.org/sdr/FDEA202202030209.md): Fairing · cracked · Feb 3, 2022 · N960FD · Boeing 757200 · Nacelle/Pylon Structure
  > #1 PYLON AFT LOWER HEAT SHIELD IS CRACKED REPAIRED PER FEDEX EA # F-5480-T0366361 P1.
- [SDR FDEA202202030207](https://openairdocs.org/sdr/FDEA202202030207.md): Angle · cracked · Feb 3, 2022 · N960FD · Boeing 757200 · Nacelle/Pylon Structure
  > #1 PYLON AFT O/B LOWER PAN ATTACH ANGLE IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N5042 REV F
- [SDR FDEA202202030206](https://openairdocs.org/sdr/FDEA202202030206.md): None · none · Feb 3, 2022 · N960FD · Boeing 757200 · Fuselage Main, Structure
  > STA 580 BL 45.5 SEAT TRACK CRACKED AT INBD FLANGE ACCOMPLISHED FEDEX EA: F-5310-T0366333-P1: FUSELAGE - MAINFRAME - SEAT TRACK, STRAP AND WEB, STA 580 LBL 45, CRACK AND OIL CANNING DAMAGE
- [SDR FDEA202202010175](https://openairdocs.org/sdr/FDEA202202010175.md): Support · cracked · Feb 1, 2022 · N960FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > #2 ENG PYLON UPPER PANEL 443KL LANDING IS CRACKED REMOVED AND REPLACED PER BOEING DWG 313N5004 REV D
- [SDR FDEA202202010174](https://openairdocs.org/sdr/FDEA202202010174.md): Brace · cracked · Feb 1, 2022 · N960FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > #2 ENG PYLON STRUT PANEL 433ER LANDING ATTACH ANGLE IS CRACKED REMOVED AND REPLACED ANGLE PER BOEING DWG # 313N5004 REV D
- [SDR FDEA202201240126](https://openairdocs.org/sdr/FDEA202201240126.md): Doubler · none · Jan 24, 2022 · N960FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > APU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR IS CHAFFED. AT APU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR, REMOVED, FABRICATED AND INSTALLED NEW DOUBLER REPAIR IAW FED EX B757 SRM 53-80-08-2R.
- [SDR FDEA202201240124](https://openairdocs.org/sdr/FDEA202201240124.md): Retainer · cracked · Jan 24, 2022 · N960FD · Boeing 757200 · Wing, Control Surfaces
  > L/W #3 SPOILER I/B SEAL RETAINER IS CRACKED REMOVED AND REPLACED PER BOEING DWG # 113N4605
- [SDR FDEA202201220118](https://openairdocs.org/sdr/FDEA202201220118.md): Panel · cracked · Jan 22, 2022 · N960FD · Boeing 757200 · Wing, Fuselage Attach Fittings
  > RIGHT WING UPPER FIXED LEADING EDGE PANEL BEHIND SLATS 7 AND 8 CRACKED AND DELAMINATED REPAIRED FIXED LEADING EDGE PANEL IAW B757 SRM 57-41-01-2R FIG. 201 AND 51-70-07-0G.
- [SDR FDEA202201200105](https://openairdocs.org/sdr/FDEA202201200105.md): Web · cracked · Jan 20, 2022 · N960FD · Boeing 757200 · Nacelle/Pylon Structure
  > #2 PYLON STRUT TO WING NACELLE STRUT WEB CRACKED PP STA 200 REPAIRED PER EA # F-5450-T0366482-P1
- [SDR FDEA202201190097](https://openairdocs.org/sdr/FDEA202201190097.md): None · cracked · Jan 19, 2022 · N960FD · Boeing 757200 · Wing, Control Surfaces
  > L/W #3 FLAP TRACK AFT PHENOLIC RUB BLOCKS CRACKED REMOVED AND REPLACED 2EA RUB PLATES PER BOEING DWG # 113N2156 REV A
- [SDR FDEA202006051135](https://openairdocs.org/sdr/FDEA202006051135.md): Actuator · malfunctioned · Jun 5, 2020 · N960FD · Boeing 757236 · Landing Gear Actuator
  > ON TAKEOFF GEAR WOULD NOT RETRACT. RAN QRH, PROBLEM RESOLVED. NOTED AUTOBRAKES "RTO" DID NOT MOVE TO THE "OFF" POSITION AFTER LIFTOFF. REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR REF AMM 32-32-15-4. LEAK AND OPS CHECKS GOOD. OK FOR SERV
- [SDR FDEA2020060541134](https://openairdocs.org/sdr/FDEA2020060541134.md): Actuator · cracked · Jun 4, 2020 · N960FD · Boeing 757236 · Landing Gear Actuator
  > ON TAKEOFF GEAR WOULD NOT RETRACT. RAN QRH, PROBLEM RESOLVED. NOTED AUTOBRAKES "RTO" DID NOT MOVE TO THE "OFF" POSITION AFTER LIFTOFF. AMM: 32-32-15-4 REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR REF AMM 32-32-15-4. LEAK AND OPS CHECKS GO
- [SDR FDEA202005040888](https://openairdocs.org/sdr/FDEA202005040888.md): Floorbeam · corroded · May 4, 2020 · N960FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO BL20R BS 1020. REMOVED CORR ON FLOOR SUPPORT STA 1020 BLO TO BL20R IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 53-00-51-1A FIG 101. REMOVED FL
- [SDR FDEA2020050430885](https://openairdocs.org/sdr/FDEA2020050430885.md): Shear Web · corroded · May 3, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN COMPT. SHEAR WEB HAS CORROSION, BETWEEN LBL.34", AND LBL.46", FROM BS. 1711, TO BS. 1715. REMOVED CORR ON SHEAR WEB 1711 TO 1715 LBL34 AND LBL46 IAW B757 SRM 51-10-02. LOWEST REMAINING.052 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-51-2R REP
- [SDR FDEA202004300817](https://openairdocs.org/sdr/FDEA202004300817.md): Web · cracked · Apr 28, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE WEB IS CRACKED, BS. 720 STR. 4R. REMOVED WEB STA 720 STR 4R, FABRICATED, LOCATED, DILLED AND INSTALLED NEW WEB IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 143N8323 REV M, REV C AND REV -
- [SDR FDEA202004260791](https://openairdocs.org/sdr/FDEA202004260791.md): Floorbeam · corroded · Apr 26, 2020 · N960FD · Boeing 757200 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO RBL20 BS 1060. REMOVED CORR ON FLOOR SUPPORT STA 1060 BL0 TO BL20R IAW B757 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B757 SRM 53-00-51 FIG 101. REMOVED SUPPORT IAW B757 SRM 51-04
- [SDR FDEA2020042760791](https://openairdocs.org/sdr/FDEA2020042760791.md): Floorbeam · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO RBL20 BS 1060. REMOVED CORR ON FLOOR SUPPORT STA 1060 BL0 TO BL20R IAW B757 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B757 SRM 53-00-51 FIG 101. REMOVED SUPPORT IAW B757 SRM
- [SDR FDEA2020042760794](https://openairdocs.org/sdr/FDEA2020042760794.md): Seat Track · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, CORROSION ON SEAT TRACK FLANGE BETWEEN STA. 365 AND 377 RBL-44. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5310-T0353677 P1 FUSELAGE - MAINFRAME - RBL 45.50 SEAT TRACK CORROSION REPAIR FROM STA 365 TO 377
- [SDR FDEA2020042760793](https://openairdocs.org/sdr/FDEA2020042760793.md): Stringer Clip · cracked · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage Main, Attach Fittings
  > MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP IS CRACKED\GOUGED BS. 720 STR. 3R REMOVED, FABRICATED AND INSTALLED MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP AT STA 720 STR. 3R IAW BOEING DWG # 140N2001, REV D AND REV. BN, B757 SRM
- [SDR FDEA2020042760790](https://openairdocs.org/sdr/FDEA2020042760790.md): Seat Track · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STA 1180 LBL44.5 HAS EXFOILATION CORROSION EVALUATED SEAT TRACK STA 1180 LBL 44.5 FOUND OUT OF LIMITS DUE TO 100% MATERIAL LOSS DUE TO EXFOILATION IAW B757 SRM 53-00-52. REMOVED, TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW B757
- [SDR FDEA2020042760789](https://openairdocs.org/sdr/FDEA2020042760789.md): Crease Beam · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage Main, Structure
  > MAIN CABIN BETWEEN STA 860-879 CREASE BEAM CORRODED. REMOVED CORR ON RH CREASE BEAM STA 860-879 IAW B757 SRM 51-10-02. ORIG MAT.071 LOWEST REM.054 LOSS.017 FOUND OUT OF LIMITS IAW B757 SRM 53-30-13-1A. REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R REP 1
- [SDR FDEA2020042760788](https://openairdocs.org/sdr/FDEA2020042760788.md): Seat Track · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 44.5 STA 1320 TO 1540 HAS CORROSION ENTIRE LENGHT REMOVED CORR ON SEAT TRACK RBL 44.5 STA 1320 TO 1540 IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILIATION OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101. REMOVED SEAT TRACK, FABRICATED,
- [SDR FDEA2020042760787](https://openairdocs.org/sdr/FDEA2020042760787.md): Support · cracked · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > R1 DOOR LOWER SILL UPPER SURFACE HAS CORROSION ON THE THRESHOLD SUPPORT STA. 338 REMOVED CORROSION FROM R1 DOOR LOWER SILL UPPER SURFACE SUPPORT STA 338, FOUND OUT OF LIMITS WITH THE ORIGINAL MAT..050 REMAINING MATERIAL.043, REMOVED, FABRICATED AND INS
- [SDR FDEA2020042760786](https://openairdocs.org/sdr/FDEA2020042760786.md): Support · corroded · Apr 26, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > R-1 DOOR LOWER SILL UPPER SURFACE CORROSION ON THE TOP SIDE OF THRESHOLD SUPPORT AT STA 354. REMOVED CORROSION FROM R-1 DOOR LOWER SILL UPPER SURFACE, FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL.050 REMAINING MATERIAL.040, REMOVED, FABRICATED AND INSTALLED NE
- [SDR FDEA2020042310768](https://openairdocs.org/sdr/FDEA2020042310768.md): Plate · corroded · Apr 21, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION AT BL20L TO BL40L BS 1020. REMOVED CORR ON FLOOR FRAME UPPER CAP (PLATE) IAW SRM 51-10-02. 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-02
- [SDR FDEA202004200762](https://openairdocs.org/sdr/FDEA202004200762.md): Intercostal · corroded · Apr 20, 2020 · N960FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION WEB SUPPORT AFT PIT STA. 1420 - 1440 STR 29R-30. DOT 88-010. REMOVED FABRICATED AND INSTALLED AFT CARGO INTERCOSTAL AT BS1400-1420 29R-30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N5398 REV A, REV P.
- [SDR FDEA202004200761](https://openairdocs.org/sdr/FDEA202004200761.md): Shear Tie · corroded · Apr 20, 2020 · N960FD · Boeing 757236 · Fuselage Internal Mounting Structure
  > CORROSION SHEAR TIE AFT PIT STA. 1440 STR 29R TO STR. 30. DOT 88-014. REMOVED FABRICATED AND INSTALLED AFT CARGO SHEAR TIE AT BS1440 STR 29R TO STR 30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N1101 REV -, REV B.
- [SDR FDEA2020041760753](https://openairdocs.org/sdr/FDEA2020041760753.md): Door Frame · cracked · Apr 16, 2020 · N960FD · Boeing 757236 · Passenger/Crew Doors
  > RH #2 DOOR UPPER HINGE CUTOUT IS CRACKED
- [SDR FDEA2020030530483](https://openairdocs.org/sdr/FDEA2020030530483.md): Fire Warning · false activation · Mar 3, 2020 · N960FD · Boeing 757236 · Fire Detection
  > L ENG FIRE WARNING L ENG OVHT RAN ENGINES TO POWER FOR APPROX 5 MIN. TAXIED A/C PER JRH NO WARNINGS COMPLIED WITH PNEUMATIC BLEED DUCT LEAK CHECK USING ALUMINUM FOIL WRAP DURING POWER RUNS NO L
- [SDR FDEA201910312831](https://openairdocs.org/sdr/FDEA201910312831.md): Gust Lock · broken · Oct 31, 2019 · N960FD · Boeing 757236 · Passenger/Crew Doors
  > DURING PREFLIGHT FOUND L1 DOOR HOLD-OPEN LOCK (GUST LOCK) BROKEN. PLACING L1 DOOR ON MEL. INTALLED 1 LEFT HAND PASSENGER DOOR HOLD OPEN LOCK, IN REFERENCE TO MAITENNACE MANUAL CHAPTER 52-11-08-8, OPS CHECK NORMAL. A/C OK TO VCONTINUE.
- [SDR FDEA201909122229](https://openairdocs.org/sdr/FDEA201909122229.md): Fastener · sheared · Sep 12, 2019 · N960FD · Boeing 757236 · Flight Compartment Windows
  > MDIS 960 56-11 6213 12SEP19 MEM FACT U FIRST OFFICER SLIDING WINDOW CRANK HANDLE HARDWARE SHEARED. FACT 12SEP19 06:08 MEM U REMOVED AND REPLACED FIRST OFFICERS #2 WINDOW CRANK HANDLE ATTACH SCREW PART NUMBER NAS1352C06-20. WORK ACCOMPLISHED REF M
- [SDR FDEA201905161080](https://openairdocs.org/sdr/FDEA201905161080.md): Attach Fitting · worn · May 16, 2019 · N960FD · Boeing 757236 · Passenger/Crew Doors
  > PDIS 960 52-10 5966 16MAY19 MEM OPEN U LOGPAGES:3132652 LF CREW ENTRY DOOR IS VERY DIFICULT TO CLOSE. HANDLE WOULD NOT GO OVER CENTER W/O EXCESSIVE FORCE REMOVED & REPLACED L1 UPPER DOOR ATTACH FITTING REF. AMM 52-11-37-4 OPS CHECK GOOD AT THIS TIME
- [SDR FDEA201901040019](https://openairdocs.org/sdr/FDEA201901040019.md): Slide · partial deploy · Jan 4, 2019 · N960FD · Boeing 757236 · Escape Slide
  > L1 ENTRY DOOR GIRT BAR STAYED ENGAGED. L1 DOOR ASSIST BOTTLE BLEW. SLIDE PARTIALLT DEPLOYED. AMM: 25-66-01-4. REMOVED AND REPLACED L1 DOOR SLIDE/RAFT, REF AMM 25-66-01-4. OK FOR SERVICE. REMOVED SAFETY PINS INSTALLED AT L-1 DOOR EMERGENCY POWER RESERVOIR. A/C
- [SDR FDEA201810192957](https://openairdocs.org/sdr/FDEA201810192957.md): Fitting · worn · Oct 19, 2018 · N960FD · Boeing 757236 · Passenger/Crew Doors
  > LEFT FWD ENTRY DOOR REQUIRES MULTIPLE CLOSING ATTEMPTS TO GET CLOSED, LATCHED AND LOCKED INDICATION. R&R L1 TOP AFT LATCH FITTING, REF AMM 52-11-37-04. R&R AFT TOP DOOR LATCH ROLLER AND CHECKED DOOR AND SWITCH ADJUSTMENT, REF 52-11-00-5. OPERATION IS NORMAL WI
- [SDR FDEA201809262711](https://openairdocs.org/sdr/FDEA201809262711.md): Switch · obstructed · Sep 26, 2018 · N960FD · Boeing 757236 · Emergency Equipment
  > ON ARRIVAL KMEM L1 DOOR SLIDE ARMED LIGHT INOP. CLEAND DEBRIS FROM L1 DOOR SLIDE GIRT BAR SWITCHES. OPS CHECKS NORMAL IAW AMM 25-66-00-0-0.
- [SDR FDEA201809112441](https://openairdocs.org/sdr/FDEA201809112441.md): O-Ring · damaged · Sep 11, 2018 · N960FD · Boeing 757236 · Hydraulic Pressure Indicator
  > LT HYD QTY EICAS MSG INFLT ON FINAL FOUND O-RING DAMAGED ON DIFFERENTIAL PRESSURE INDICATOR AT LEFT PYLON FILTER MODULE. REMOVED AND REPLACED BOTH O-RINGS AND SERVICED LEFT SYSTEM RESERVOIR REF AMM 29-11-17-4. A/C OK FOR SERVICE.
- [SDR FDEA201804301145](https://openairdocs.org/sdr/FDEA201804301145.md): Hinge Fitting · cracked · Apr 30, 2018 · N960FD · Boeing 757236 · Engine Thrust Reverser
  > NR 2 INBD THRUST REVERSER HINGE FITTING, AFT UPPER HOLE, SHOWING A CRACK INDICATION.
- [SDR FDEA2018042601119](https://openairdocs.org/sdr/FDEA2018042601119.md): Skin · delaminated · Apr 25, 2018 · N960FD · Boeing 757236 · Wing, Plate/Skin
  > LEFT OTBD FLAP UPPER SURFACE, DELAMINATED AT MIDDLE OF FLAP 3 INCHES FROM T\E. REPAIRED IAW EA F-5750-T0339704.
- [SDR FDEA201804231099](https://openairdocs.org/sdr/FDEA201804231099.md): Skin · chafed · Apr 23, 2018 · N960FD · Boeing 75723A · Trailing Edge Flaps
  > LEFT INBD FLAP LE, CHAFED AT THE OTBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339646 P1.
- [SDR FDEA201804231098](https://openairdocs.org/sdr/FDEA201804231098.md): Skin · chafed · Apr 23, 2018 · N960FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT OTBD FLAP LE, CHAFED AT THE INBD EDGE OF FLAP, APPROXIMATELY 18 INCHES OTBD OF THE INBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339592 P1.
- [SDR FDEA201804231097](https://openairdocs.org/sdr/FDEA201804231097.md): Skin · chafed · Apr 23, 2018 · N960FD · Boeing 757236 · Trailing Edge Flaps
  > LEFT OTBD FLAP LE, CHAFED AT THE INBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339609 P1.
- [SDR FDEA201804221091](https://openairdocs.org/sdr/FDEA201804221091.md): Shear Plate · corroded · Apr 22, 2018 · N960FD · Boeing 757236 · Fuselage Main, Structure
  > SHEAR PLATE AT BS 377, LBL 8 HAS SURFACE CORROSION. BLENDED IAW EA F-5310-T0339615, P1.

Next page: https://openairdocs.org/aircraft/N960FD/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 = 'N960FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N960FD/reports

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