# Service difficulty reports: N966FD

A list on [N966FD](https://openairdocs.org/aircraft/N966FD.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 · 109 reports

- [SDR FDEA202403230357](https://openairdocs.org/sdr/FDEA202403230357.md): Door · malfunctioned · Mar 23, 2024 · N966FD · Boeing 757204 · Passenger/Crew Doors
  > L1 DOOR NOT FUNCTIONING PROPERLY, UNABLE TO OPEN FROM OUTSIDE RELEASED FOR SERVICE PER MEL: 52-11-01-A: L1 DOOR INOP AMM: 52-11-01-A L1 DOOR INOP C/7391449. OPERATED L1 DOOR FROM BOTH INSIDE AND OUTSIDE USING ONE AMT, OPENED AND CLOSED WITH NO ISSU
- [SDR FDEA202307211264](https://openairdocs.org/sdr/FDEA202307211264.md): Windshield · arced · Jul 21, 2023 · N966FD · Boeing 757200 · Flight Compartment Windows
  > CAPTAINS NO. 1 WINDSHIELD HAS SMALL AREA OF ARCING. REPLACED CAPTAINS FWD WINDSHIELD REF AMM 56-11-01-4 UP THRU STEP 3.E.(21).(C).
- [SDR FDEA202307201262](https://openairdocs.org/sdr/FDEA202307201262.md): Window · burned · Jul 20, 2023 · N966FD · Boeing 757200 · Flight Compartment Windows
  > IN CRUISE, CAPTAIN FWD WINDSHIELD ARCING AND BURN MARKS. WINDOW HEAT EICAS MESSAGE. COMPLIED WITH QRH AND NO FURTHER ISSUES. ***EMERGENCY DECLARED*** DAMAGE TO OUTER PANE ONLY EA AND MEL APPLIED FOR FLIGHT TO IND FOR L1 WINDOW REPLACEMENT
- [SDR FDEA202210072519](https://openairdocs.org/sdr/FDEA202210072519.md): Skin · debonded · Oct 7, 2022 · N966FD · Boeing 757204 · Trailing Edge Flaps
  > RH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.
- [SDR FDEA202210072518](https://openairdocs.org/sdr/FDEA202210072518.md): Skin · debonded · Oct 7, 2022 · N966FD · Boeing 757204 · Trailing Edge Flaps
  > LH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.
- [SDR FDEA202209202348](https://openairdocs.org/sdr/FDEA202209202348.md): Line · leaking · Sep 20, 2022 · N966FD · Boeing 757204 · Hydraulic System, Main
  > TAXING IN AFTER LANDING, WHILE MAKING THE LEFT TURN FROM TAXIWAY C ONTO C8, THE TILLER LOST RESPONSIVENESS FOLLOWED BY A MASTER CAUTION ALERT AND L HYD SYS PRESS EICAS MESSAGE. VERIFIED ZERO HYD QUANTITY AND PRESSURE. COORDINATED A MX TOW IN WITH COMPAN
- [SDR FDEA202206091398](https://openairdocs.org/sdr/FDEA202206091398.md): Slide · out of alignment · Jun 9, 2022 · N966FD · Boeing 757200 · Escape Slide
  > MDIS 966 52-10 7355 09JUN22 PAE OPEN U R1 DOOR SLIDE WILL NOT ENGAGE MEL 09JUN22 02:32 PAE U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 12JUN22 "MEL 52-11-01-A: _R1____ (IDENTIFY L1 OR R1 DOOR OR SLIDE) - ___INOP_
- [SDR FDEA202206091397](https://openairdocs.org/sdr/FDEA202206091397.md): Girt Bar · faulted · Jun 9, 2022 · N966FD · Boeing 757200 · Emergency Equipment
  > ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE.
- [SDR FDEA202107131771](https://openairdocs.org/sdr/FDEA202107131771.md): Bottle · empty · Jul 13, 2021 · N966FD · Boeing 757230 · Escape Slide
  > DUE TO PARTCIAL DEPLOY OF R/H MAIN DOOR SLIDE FOUND EMERGENCY BOTTLE IN CEILING (L/H BOTTLE) FOR R/H MAIN DOOR, DEPLETED. REMOVED AND REPLACED R/H EMERGENCY POWER CYLINDER REF AMM: 52-11-30-4 OP'S CHECK GOOD. REF WRITE NUMBER: 52-10/ 6560 FOR
- [SDR FDEA202105311423](https://openairdocs.org/sdr/FDEA202105311423.md): Skin · damaged · May 31, 2021 · N966FD · Boeing 757204 · Trailing Edge Flaps
  > DOT(137-05) LH WING I/B MAIN FLAP UPPER SURFACE HAS SEVERAL HAIL DAMAGED. REPAIRED L/H WING I/B MAIN FLAP UPPER SURFACE IAW SRM 57-53-01-1A AND 51-70-07, MAJOR REPAIR.
- [SDR FDEA202105291421](https://openairdocs.org/sdr/FDEA202105291421.md): Floor Panel · delaminated · May 29, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL 231MGF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MGF ON VT MAE TRAVELER T21/1551858 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR
- [SDR FDEA202105291420](https://openairdocs.org/sdr/FDEA202105291420.md): Floor Panel · delaminated · May 29, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > LH MAIN CARGO COMPT FLOOR PANEL 231MCF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MCF ON VT MAE TRAVELER T21/1551856 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR
- [SDR FDEA202105271413](https://openairdocs.org/sdr/FDEA202105271413.md): Drag Fitting · cracked · May 27, 2021 · N966FD · Boeing 757204 · Nacelle/Pylon, Main Frame
  > #1 PYLON INBD DRAG FITTING HAS A CRACK INDICATION AT #3 HOLE. ACCOMPLISHED EA #F-5740-T0361812, TITLE: WINGS-ATTACH FITTINGS-DRAG FITTING #3 CRACKED HOLE-FEDEX EO F-5730-E0340076 PART 1 REV B- BOEING SB757-57A0073 STEPS 1 AND 2, MAJOR REPAIR.
- [SDR FDEA202105261406](https://openairdocs.org/sdr/FDEA202105261406.md): Floor Panel · delaminated · May 26, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1550764 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202105261405](https://openairdocs.org/sdr/FDEA202105261405.md): Floor Panel · delaminated · May 26, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1550761 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202105261404](https://openairdocs.org/sdr/FDEA202105261404.md): Floor Panel · delaminated · May 26, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > LAVATORY FLOOR PANEL 221BF DELAMINATED. FABRICATED FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1550763 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202105211336](https://openairdocs.org/sdr/FDEA202105211336.md): Floor Panel · damaged · May 21, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > MAIN CARGO COMPT FLOOR PANEL 231MSF HAS A DAMAGED AREA LOCATED AT FWD LH EDGE. FABRICATED FLOOR PANEL 231 MSF ON TRAVELER T21/1551857 IAW SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202105211337](https://openairdocs.org/sdr/FDEA202105211337.md): Floorboard · damaged · May 21, 2021 · N966FD · Boeing 757204 · Fuselage Floor Panel
  > MCD FLOORBOARD PNL 232 MTF HAS DAMAGE. FABRICATED MCD FLOORBOARD 232 MTF ON TRAVELER # T21/1551859 IAW DWG SRZ-25-005 REVESION R MAJOR REPAIR
- [SDR FDEA201905061008](https://openairdocs.org/sdr/FDEA201905061008.md): Floorbeam · cracked · May 6, 2019 · N966FD · Boeing 757204 · Fuselage Main, Floor Beam
  > STA 580 FLOORBEAM CRACKED - LBL45, UPPER CORD AFT FLANGE. COMPLIED WITH EA F- 5310 - T0346588 P1 TITLE: FUSELAGE MAINFRAME STA.580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.
- [SDR FDEA201904290967](https://openairdocs.org/sdr/FDEA201904290967.md): Floorbeam · corroded · Apr 29, 2019 · N966FD · Boeing 757204 · Fuselage Main, Floor Beam
  > CORROSION FOUND STA 1681 RBL 13 FLOORBEAM UNDER LIP OF THE TOP "T" CAP. COMPLIED WITH EA F-5310-T0346723 P1. TITLE: FUSELAGE-MAINFRAME - CORROSION ON STA 1681 FLOORBEAM UPPER CHORD, REINFORCING REPAIR, BL 0 TO RBL 45.7.
- [SDR FDEA201904290966](https://openairdocs.org/sdr/FDEA201904290966.md): Shear Web · corroded · Apr 29, 2019 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SHEAR WEB MAIN CARGO CABIN STA 1701 LBL 55.0. REMOVED CORROSION AT SHEAR WEB STA 1701 LBL 55.00 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071",MATERIAL REMAINING 0.038",MATERIAL LOSS 0.033",EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-5
- [SDR FDEA201904290965](https://openairdocs.org/sdr/FDEA201904290965.md): Shear Web · corroded · Apr 29, 2019 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SHEAR WEB MAIN CARGO CABIN STA 1688 LBL 57. REMOVED CORROSION AT FLOOR SHEAR WEB STA 1688 LBL 57 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071", MATERIAL REMAINING 0.058", MATERIAL LOSS 0.013", EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SR
- [SDR FDEA201904290964](https://openairdocs.org/sdr/FDEA201904290964.md): Seat Track · corroded · Apr 29, 2019 · N966FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE STA 1640 RBL 45.5 MAIN CARGO CABIN. REMOVED CORROSION AT SEAT TRACK FLANGE STA 1640 RBL 45.5, IAW SRM 51-10-02-OG EVALUATED AREA DAMAGE, ORIGINAL MAT. 0.070", REMAINING MAT. 0.035",MAT LOSS 0.035" FOUND TO BE OUT LIMITS IAW SRM
- [SDR FDEA201904260934](https://openairdocs.org/sdr/FDEA201904260934.md): Shear Web · corroded · Apr 26, 2019 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR WEB AFT WEB AREA STA 1681 RBL 32. REMOVED CORROSION ON SHEAR WEB IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA, FOUND TO BE OUT LIMITS IAW SRM 53-00 00-51-1A,FIG 101, DETAIL III. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, AND INS
- [SDR FDEA201904260933](https://openairdocs.org/sdr/FDEA201904260933.md): Floorbeam · corroded · Apr 26, 2019 · N966FD · Boeing 757204 · Fuselage Main, Floor Beam
  > CORROSION T CAP FLOOR BEAM MAIN CABIN STA 1681 RBL 32.0 COMPLIED WITH FEDEX EA # F-5310-T0346723 P1.
- [SDR FDEA201904260932](https://openairdocs.org/sdr/FDEA201904260932.md): Deck Plate · corroded · Apr 26, 2019 · N966FD · Boeing 757204 · Fuselage Main, Structure
  > CORROSION ON EXISTING REPAIR FLOOR WEB MAIN CABIN STA 1716 FROM RBL 45 TO BLO. COMPLIED WITH EA F-5310-T0346613 P1.
- [SDR FDEA201811223343](https://openairdocs.org/sdr/FDEA201811223343.md): Light · inoperative · Nov 21, 2018 · N966FD · Boeing 757204 · Emergency Lighting
  > COCKPIT CEILING EMERGENCY LIGHT WILL NOT TEST. RELAMPED AND OPS CHECK NORMAL REF MM 33-51-09-3. A/C OK FOR SERVICE.
- [SDR FDEA2018081492011](https://openairdocs.org/sdr/FDEA2018081492011.md): Bushing · bent · Aug 9, 2018 · N966FD · Boeing 757204 · Emergency Equipment
  > L1 DOOR DIFFICULT TO DISARM. L1 DOOR WILL NOT OPEN. APEARS THAT GIRT BAR HAS DROPPED FROM BOTTOM OF DOOR AND WAS JAMMED ALONG THE FLOOR. REPLACED THE L1 DOOR GIRT BAR FORWARD MECHANISM SPRING, BUSHINGS AND BOLT. OPS CHECKED GOOD IAW AMM 52-11-25-5.
- [SDR FDEA201707061861](https://openairdocs.org/sdr/FDEA201707061861.md): Sensor · out of adjust · Jul 6, 2017 · N966FD · Boeing 757204 · Door Warning System
  > LEFT FWD ENTRY DOOR WHEN OPEN, DOES NOT SHOW OPEN ON THE OVERHEAD PANEL OR EICAS SCREEN. CLEANED AND ADJUSTED THE L1 ENTRY DOOR SENSOR IAW AMM 52-71-00-5. OPS CHECKED GOOD.
- [SDR FDEA201702020388](https://openairdocs.org/sdr/FDEA201702020388.md): Liner · out of adjust · Feb 2, 2017 · N966FD · Boeing 757204 · Passenger/Crew Doors
  > L1 ENTRY DOOR ARMING LEVER INDICATOR DOES NOT FULLY RETRACT WHEN DOOR IS DISARMED. ADJUSTED L1 DOOR LINING IAW MM 52-11-02-4. OPS CHECKED GOOD.
- [SDR FDEA201611013779](https://openairdocs.org/sdr/FDEA201611013779.md): Lever · malfunctioned · Nov 1, 2016 · N966FD · Boeing 757204 · Passenger/Crew Doors
  > L1 DOOR ARMED INDICATOR HANDLE DOES NOT RECEDE FLUSH WITH DOOR PANEL IN THE DISARM POSITION. ACCOMPLISHED AN OPS CHECK OF THE L1 DOOR, DOOR ARMED INDICATOR WILL RETURN TO FLUSH. UNABLE TO DUPLICATE IAW AMM 52-11-00-0.
- [SDR FDEA201602060475](https://openairdocs.org/sdr/FDEA201602060475.md): Lanyard · tangled · Feb 6, 2016 · N966FD · Boeing 757204 · Emergency Equipment
  > ON BLOCK IN, FIRST OFFICER WAS UNABLE TO CONFIRM RT ENTRY DOOR DISARMED. WHEN HANDLE IN ARMED POSITION THE ARMED LIGHT DOES NOT COME ON. WHEN HANDLE MOVED TO DISARM POSITION, TAB MOVES IN BUT HANDLE DOES NOT MOVE ALL THE WAY TO DISARM. VISUALLY INSPECTED R1
- [SDR FDEA201504221278](https://openairdocs.org/sdr/FDEA201504221278.md): Shear Plate · corroded · Apr 22, 2015 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, LBL 24.75 TO BL 0 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317018 REV.
- [SDR FDEA201504221277](https://openairdocs.org/sdr/FDEA201504221277.md): Shear Plate · corroded · Apr 22, 2015 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, BL 0 TO RBL 24.75 FOUND CORROSION. COMPLIED WITH EA F-5310-T0316995 REV.
- [SDR FDEA201504221276](https://openairdocs.org/sdr/FDEA201504221276.md): Shear Plate · corroded · Apr 22, 2015 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, LBL 45.50 - 24.75 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317067 REV A.
- [SDR FDEA201504221275](https://openairdocs.org/sdr/FDEA201504221275.md): Shear Plate · corroded · Apr 22, 2015 · N966FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, RBL 24.75 - 45.50 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317046 REV.
- [SDR FDEA201408312377](https://openairdocs.org/sdr/FDEA201408312377.md): Light · damaged · Aug 31, 2014 · N966FD · Boeing 757204 · Emergency Lighting
  > EMERGENCY LIGHT, UNARMED LIGHT, INOPERATIVE. WHILE LAMPING THE LIGHT CAPSULE FELL APART. REQUIRES LIGHT ASSEMBLY. PANEL ASSEMBLY REQUIRED. R & R EMER LIGHTS, UNARMED, LIGHT ASSEMBLY IAW SMP. TESTED GOOD IAW MM 33-51-00-5.
- [SDR FDEA201405311236](https://openairdocs.org/sdr/FDEA201405311236.md): Skin · dented · May 31, 2014 · N966FD · Boeing 757204 · Trailing Edge Flaps
  > LEFT INBD AFT FLAP OTBD UPPER SURFACE HAS HAIL DAMAGE. SANDED, CLEANED & PREPPED AREA AT LT INBD AFT FLAP OTBD UPPER SURFACE. APPLIED REPAIR TO FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW MM 51-20-01 IAW EA F-57-50-T0308504.
- [SDR FDEA201405311235](https://openairdocs.org/sdr/FDEA201405311235.md): Skin · dented · May 31, 2014 · N966FD · Boeing 757204 · Trailing Edge Flaps
  > RIGHT OTBD AFT FLAP UPPER TE INBD SIDE HAS HAIL DAMAGE. SANDED, CLEANED & PREPARED AREA IAW SRM 57-53-01 FIG 201, 51-70-17 PARA 4 C. APPLIED REPAIR TO FLAP RT OTBD UPPER TE INBD SIDE OF AFT FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW AMM 51-00-01.
- [SDR FDEA201310092454](https://openairdocs.org/sdr/FDEA201310092454.md): Windshield · cracked · Oct 9, 2013 · N966FD · Boeing 757204 · Flight Compartment Windows
  > L1 WINDOW OUTER LAYER CRACKED AT FLT LV 400 -60C, AFTER 2.5 HRS OF FLIGHT. INSTALLED NEW L-1 WINDOW, FIRST TORQUE COMPLETED AT 2119Z. R & R L1 WINDSHIELD IAW AMM 56-11-01-4.
- [SDR FDEA201306111250](https://openairdocs.org/sdr/FDEA201306111250.md): Line · leaking · Jun 11, 2013 · N966FD · Boeing 757204 · Hydraulic System, Main
  > LOST LEFT HYD QTY AND LEFT HYD SYS PRESSURE AFTER POWER UP FOR TAKEOFF. RUDDER RATIO ON EICAS AND POWER TRANSFER UNIT ON STATUS CAME UP AS WELL. NO NOSE WHEEL STEERING AVAILABLE AFTER PTU AUTOMATICALLY CAME ON. APPEARS LOST ALL FLUID IN LEFT HYD. INSTALL
- [SDR FDEA201304300888](https://openairdocs.org/sdr/FDEA201304300888.md): Sensor · out of adjust · Apr 30, 2013 · N966FD · Boeing 757204 · Door Warning System
  > LT FWD ENTRY DOOR LIGHT & EICAS MESSAGE COMES ON INFLIGHT. LT FWD ENTRY DOOR WARNING SENSOR SYS ADJUSTMENT CARRIED OUT IAW AMM 52-71-00, REV 106 FOUND GOOD. TESTING OF DOOR WARNING SYS FOR NR 1 PASSENGER DOOR FOUND GOOD IAW AMM 52-71-00, REV 106.
- [SDR FDEA201304150783](https://openairdocs.org/sdr/FDEA201304150783.md): Spar · corroded · Apr 15, 2013 · N966FD · Boeing 757204 · Wing Spar
  > IAW EO F-2822-7-5009 PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE. REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. IAW EO F-2822-7-5009, PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE REMOV
- [SDR FDEA201304050726](https://openairdocs.org/sdr/FDEA201304050726.md): Skin · dented · Apr 5, 2013 · N966FD · Boeing 757204 · Cargo/Baggage Doors
  > CARGO DOOR OUTER SKIN AFT LOWER CORNER DENTED. REPAIRED IAW EA F-5230-166052 PART 1. MAJOR REPAIR.
- [SDR FDEA201304030718](https://openairdocs.org/sdr/FDEA201304030718.md): Skin · dented · Apr 3, 2013 · N966FD · Boeing 757204 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN DENTED BS 1698 AND 1 INCH BELOW S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.
- [SDR FDEA201304030717](https://openairdocs.org/sdr/FDEA201304030717.md): Skin · dented · Apr 3, 2013 · N966FD · Boeing 757204 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN DENTED AT BS 1717.5 AND 0.5 INCHES BELOW S14L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.
- [SDR FDEA201304030716](https://openairdocs.org/sdr/FDEA201304030716.md): Skin · dented · Apr 3, 2013 · N966FD · Boeing 757204 · Fuselage Main, Plate/Skin
  > AFTER PAINTING OBSERVED FUSELAGE EXTERIOR SKIN HAS A DENT AT BS 1695 AND 1 INCH ABOVE S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.
- [SDR FDEA201304030719](https://openairdocs.org/sdr/FDEA201304030719.md): Skin · dented · Apr 3, 2013 · N966FD · Boeing 757204 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS A PROTRUDING DENT AT BS 746 THREE INCHES ABOVE S25R. REPAIRED IAW SRM 53-00-01, FIG.201, REPAIR 16, REV.108. CAT B, MAJOR REPAIR.
- [SDR FDEA201304020702](https://openairdocs.org/sdr/FDEA201304020702.md): Stringer · corroded · Apr 2, 2013 · N966FD · Boeing 757204 · Fuselage Main, Longeron/Stringer
  > AREA AFT OF AFT CARGO BS 1681-1701, S22R HAS CORROSION ON UPPER FLANGE. REPAIR CARRIED OUT ON CORRODED PART OF STRINGER S-22R AT STA 1681-STA 1701, IAW SRM 53-00-03 FIG.201 DETAIL I REPAIR 2 REV.108. REPAIR IS MAJOR.
- [SDR FDEA201303290685](https://openairdocs.org/sdr/FDEA201303290685.md): Shear Tie · damaged · Mar 29, 2013 · N966FD · Boeing 757204 · Fuselage Internal Mounting Structure
  > FOUND 0.200 GAP IN BETWEEN SKIN AND SHEAR TIE AT BS 1701 BETWEEN STRINGER 15 - 16 LEFT, ONLY ALLOWED FOR UP TO 0.040 MAXIMUM GAP. REMOVED AND REPLACED WITH NEW SHEAR TIE FABRICATED AS PER DWG 140N2002 SHT.4 REV.B AND INSTALLED AS PER DWG 146N1026 SHT.2 REV

Next page: https://openairdocs.org/aircraft/N966FD/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 = 'N966FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N966FD/reports

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