# Service difficulty reports: N963FD

A list on [N963FD](https://openairdocs.org/aircraft/N963FD.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 · 122 reports

- [SDR FDEA202608281246](https://openairdocs.org/sdr/FDEA202608281246.md): Window · arced · Aug 28, 2026 · N963FD · Boeing 75728A · Flight Compartment Windows
  > AFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. REMOVED AND REPLACED L1 WINDSHIELD IAW AMM 56-11-01-4-0 SECTION E, STEP 13, FIRST TORQUE APPLIED SEC
- [SDR FDEA202606100692](https://openairdocs.org/sdr/FDEA202606100692.md): Holder · inoperative · Jun 10, 2026 · N963FD · Boeing 75728A · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT AND SLIDE LIGHT WILL NOT TEST. A/C HAS BEEN POWERED FOR ALMOST 3 HOURS, NO HELP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT POWER SUPPLY M731. RADIANT POWER CORP, MPN 2013-1A, MSN 111794 POWER SUPPLY REMOVED. OPS CHECKS GO
- [SDR FDEA202605050558](https://openairdocs.org/sdr/FDEA202605050558.md): Light · no discrepancy · May 5, 2026 · N963FD · Boeing 75728A · Door Warning System
  > FO SIDE SLIDE LIGHT INOP. PERFORMED OPERATIONAL TEST OF R1 GIRT BAR ENGAGED LIGHT, GIRT BAR ENGAGED WARNING LIGHT ILLUMINATES OVER SEVERAL CYCLES OF MODE SELECT LEVER.
- [SDR FDEA202601050005](https://openairdocs.org/sdr/FDEA202601050005.md): Skin · cracked · Jan 5, 2026 · N963FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > LEFT AFT FUSELAGE BS 1459-1461 (02EA) FASTENERS AFT OF BUTT SEAM BS 1459 ABOVE STR 20 AND DOUBLER THAT HAVE (02) POSSIBLE CRACKS INDICATION UNDER FASTENERS RUNNING PARALLEL OF THE DOUBLER DURING NDT HFEC INSPECTION COMPLIED WITH EA # F5330-T0385962 TITTLE
- [SDR FDEA202601030003](https://openairdocs.org/sdr/FDEA202601030003.md): Repair · not reported · Jan 3, 2026 · N963FD · Boeing 75728A · Standard Practices/Structures
  > EXISTING REPAIR FOUND AT # 2 CARGO DOOR AFT LOWER CORNER CUTOUT AREA COMPLIED WITH EA # F-5330-T0305556 B TITLE: FUSELAGE PLATES & SKINS - REPLACEMENT OF EXISTING STA 1440 FUSELAGE SKIN REPAIR AT 24R-25R (# 2 CARGO DOOR OPENING)
- [SDR FDEA202512292294](https://openairdocs.org/sdr/FDEA202512292294.md): Stringer · corroded · Dec 29, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, DURING REMOVAL OF PRODUCTION STRINGER SPLICE TO GAIN ACCESS FOR STRINGER REPAIR FOUND STRINGER 21L, BS 1460 - 1465 EXFOLIATED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REPAIR 2, FIG 201, DETAIL I, SHEET 6, AND SRM 51-40-02-OG.
- [SDR FDEA202512292293](https://openairdocs.org/sdr/FDEA202512292293.md): Stringer · cracked · Dec 29, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFTER DVI OF THE LAPPED AND OVERLAPPING SKIN UNDERNEATH OF THE EXISTING REPAIR DOUBLER BETWEEN BS 1430 TO BS 1475, STR 20L TO STR 21L FOUND STRINGER 21L CRACKED AT BS 1454. REPAIRED STRINGER 21L BETWEEN STA 1426 TO STA 1456 IAW B 757 SRM 53-00-03-2R REPAIR
- [SDR FDEA202512262290](https://openairdocs.org/sdr/FDEA202512262290.md): Fitting · loose · Dec 26, 2025 · N963FD · Boeing 75728A · Nacelle/Pylon, Attach Fittings
  > NR 1 ENGINE NACELLE STRUT R/H SIDE AFTER. HINGE FITTING BOLT HEAD BROKEN OFF. REMOVED AND REPLACED BOLT AT NO 1 ENGINE NACELLE STRUT R/H SIDE AFT. HINGE FITTING IAW SRM 51-40-02-0G AND E.A # F-5440-T0385898 P1.
- [SDR FDEA202512232285](https://openairdocs.org/sdr/FDEA202512232285.md): Floor Support · damaged · Dec 22, 2025 · N963FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STRINGER AT B.S. 1260 LBL 10.45 WITH SEVERAL PERFORATIONS (MISDRILLED) AFT CARGO COMPARTMENT STRINGER AT BS.1260 LBL 10.45 WAS REPAIRED IAW B757 SRM 53-00- 53-2R. REPAIR1.
- [SDR FDEA202512212275](https://openairdocs.org/sdr/FDEA202512212275.md): Shear Plate · corroded · Dec 21, 2025 · N963FD · Boeing 75728A · Fuselage Main, Structure
  > GALLEY AREA BS 375 BTW LBL 20.00 TO LBL 26.00 SHOW PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE SEAT TRACK SUPPORT (U CHANNEL) AND (2EA) FLEXURE ANGLE IAW VENTURA AEROSPACE DWG 3471 REV # B DWG 3480 REV # B AND BOEING DWG PL 141N5131 REV # V.
- [SDR FDEA202512202272](https://openairdocs.org/sdr/FDEA202512202272.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, STRINGER 30 BTW BS 1440 TO 1460 FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, SRM 51-40-02-0G, & DWG 146N3110, REV B.
- [SDR FDEA202512202271](https://openairdocs.org/sdr/FDEA202512202271.md): Shear Tie · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 1460 SHEAR TIE BTW STR-29L TO STR-30, FOUND CORRODED. REPLACED SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202270](https://openairdocs.org/sdr/FDEA202512202270.md): Shear Tie · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Internal Mounting Structure
  > LOWER HALF OF FUSELAGE BS 1460 BETWEEN S28L AND S29L HAS POSSIBLE CORROSION. REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202269](https://openairdocs.org/sdr/FDEA202512202269.md): Stringer Splice · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BS 1460 SPLICE STRINGER 30 CORRODED. REPLACED SPLICE STRINGER LOCATED BS 1460 IAW SRM 51-40-02-0G, AND DWG 146N3820, REV C.
- [SDR FDEA202512202268](https://openairdocs.org/sdr/FDEA202512202268.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, STRINGER 30L BTW BS 1460 - 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-02-0G, & DWG 146N3110, REV C.
- [SDR FDEA202512202267](https://openairdocs.org/sdr/FDEA202512202267.md): Stringer Splice · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, BS 1460 STRINGER SPLICE 29L CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-40-02-0G, DWG 146N3820, REV C.
- [SDR FDEA202512202266](https://openairdocs.org/sdr/FDEA202512202266.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER 29L BTW BS 1460 TO 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-020-G, AND DWG 146N3110, REV B.
- [SDR FDEA202512202265](https://openairdocs.org/sdr/FDEA202512202265.md): Skin Panel · cracked · Dec 20, 2025 · N963FD · Boeing 75728A · Leading Edge Devices
  > RIGHT WING OTBD LEADING EDGE SLAT NR 10 INTERNAL LOWER MAIN TRACK SLAT HAS POSSIBLE CRACKED. REMOVED DAMAGED COVE SKIN AT RT WING OTBD LEADING EDGE SLAT 10 IAW SRM 51-40-02-0G, AND INSTALLED NEW FORMED COVE SKIN IAW B. DRAWING 114N4075 REV -, AND PL 114N40
- [SDR FDEA202512182261](https://openairdocs.org/sdr/FDEA202512182261.md): Stringer · corroded · Dec 18, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > BULK AREA BETWEEN STA 1700 TO 1720 STR 23L CORRODED ACCOMPLISHED REPAIR ON STRINGER BTW STA 1685 TO STR 1720 IAW B757 SRM 53-00-03-2R, 51- 40-02-0G
- [SDR FDEA202512112236](https://openairdocs.org/sdr/FDEA202512112236.md): Seat Track · corroded · Dec 11, 2025 · N963FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 900 TO BS 1180.0 LBL 58.22 HAS MULTIPLE SPOTS WITH CORROSION. REMOVED AND EVALUATED MAIN CABIN SEAT TRACK BTW BS 900-1180, LBL 58.22 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A, DETAIL V, 51-40-02-0G. TRIMMED, LOCATED AND DR
- [SDR FDEA202510172049](https://openairdocs.org/sdr/FDEA202510172049.md): Pitot Tube · failed · Oct 17, 2025 · N963FD · Boeing 75728A · Pitot/Static System
  > STARTED TAKEOFF. POWER WAS SET. SHORTLY THEREAFTER BETWEEN 30 AND 40 KNOTS, RECEIVED ABOUT 3 TO 5 CAS MESSAGES. AUTOTHROTTLE DISCONNECT, SOME PROBE WARNING AND A COUPLE OTHERS THAT WE CAN`T RECALL. REJECT WAS INITIATED AROUND 40 KNOTS AND THE MESSAGES DISAPP
- [SDR FDEA202505100745](https://openairdocs.org/sdr/FDEA202505100745.md): Slide · failed · May 10, 2025 · N963FD · Boeing 75728A · Escape Slide
  > RAMP PERSONNEL OPENED L1 AFTER DOORS WERE ARMED AND THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. L1 DOOR ASSIST BOTTLE BLOWN, SLIDE DID NOT DEPLOY. REPLACED THE L-1 EMERGENCY POWER RESERVOIR AND THE L1 SLIDE ASSY
- [SDR FDEA202503210469](https://openairdocs.org/sdr/FDEA202503210469.md): Computer · faulted · Mar 21, 2025 · N963FD · Boeing 75728A · Landing Gear System
  > MADE 2 TAKEOFF ATTEMPTS, MAX POWER FOR WIND SHEAR, EACH TIME REJECTED TAKEOFF DUE TO AIRCRAFT VEERING TO THE RIGHT OF CENTERLINE. NO EICAS MESSAGES OR WARNINGS RECEIVED. ENGINES APPEARED TO SPOOL UP NEARLY EVEN. RAN QRH REJECTED TAKEOFF AND AFTER LANDING
- [SDR FDEA202307071182](https://openairdocs.org/sdr/FDEA202307071182.md): Unknown · unknown · Jul 7, 2023 · N963FD · Boeing 757200 · Emergency Equipment
  > WITH OUR BEACON ON, A MECHANIC OPENED L FWD ENT DOOR FROM OUTSIDE THE AIRCRAFT WHEN THE SLIDE WAS ARMED. THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. OLD SLIDE FOUND IN MAIN CARGO IN NET. REMOVED DOOR LINERS FROM DOOR, VERIFIED CORRECT OPS OF DOOR D
- [SDR FDEA202206171458](https://openairdocs.org/sdr/FDEA202206171458.md): Hose · malfunctioned · Jun 17, 2022 · N963FD · Boeing 75728A · Fuel Controlling System
  > RIGHT ENGINE PROBLEM AT CRUISE. RIGHT EPR SHOWED MAX ON SCALE. FUEL FLOW APPRX 1/2 OF LEFT ENGINE. ALL RIGHT INSTRUMENTS WERE SIGNIFICANT THEN LEFT. HAD TO DESCEND FROM CRUISE F380 TO FL 320 TO HOLD AIRSPEED. HAD RIGHT SIGNIFICANT RIGHT THROTTLE VIBRATION
- [SDR FDEA202204120932](https://openairdocs.org/sdr/FDEA202204120932.md): Girt Bar · misaligned · Apr 12, 2022 · N963FD · Boeing 75728A · Passenger/Crew Doors
  > MDIS 963 52-10 7334 12APR22 PDX FACT U L-1 DOOR WILL NOT ARM FACT 12APR22 21:02 AFW U INSPECTED AND VERIFIED GIRT BAR ALLIGNMENT IN REF TO AMM 25-66-10-2. PERFORMED L1 DOOR GIRT BAR INSPECTION/CHECK IN REF TO AMM 25-66-10-2 SECTION 4. DO
- [SDR FDEA202202160422](https://openairdocs.org/sdr/FDEA202202160422.md): Floorbeam · cracked · Feb 16, 2022 · N963FD · 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-T0367280 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR- REPAIR DOCUMENTATION
- [SDR FDEA202201260143](https://openairdocs.org/sdr/FDEA202201260143.md): Life Raft · damaged · Jan 26, 2022 · N963FD · Boeing 757200 · Passenger/Crew Doors
  > R1 DOOR WAS OPENED FROM THE OUTSIDE WHILE STILL ARMED, SLIDE FELL OFF OF DOOR RAR R1 SLIDE/RAFT, REF B757 AMM 25-66-01-4. NO DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED.
- [SDR FDEA202110272644](https://openairdocs.org/sdr/FDEA202110272644.md): None · none · Oct 27, 2021 · N963FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FOUND LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" IB OF STR S29L WRITTEN ON WRI 53-00-6918 WORKED ON SEQ 5 UNDER W/O 81650 CARD WRITTEN FOR RDR/SDR. REPAIRED LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" I/B OF STR S29L REF 757 SRM 5
- [SDR FDEA202110272643](https://openairdocs.org/sdr/FDEA202110272643.md): None · none · Oct 27, 2021 · N963FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > FOUND LIGHTING STRIKE DAMAGE ON SECTION 43, ON STA 580, 4.5" IB OF STR 29R DAMAGE WRITTEN UP ON WRI 53-00-6925 REPAIR WORKED ON SEQ 6 W/O 81650. CARD WRITTEN FOR RDR/SRD REPAIRED LIGHTING STRIKE DAMAGE ON SECTION 43 ON STA 580 4.5" I/B OF STR 29R REF 757 SRM
- [SDR FDEA202107071697](https://openairdocs.org/sdr/FDEA202107071697.md): Battery Pack · inoperative · Jul 7, 2021 · N963FD · Boeing 75728A · Emergency Lighting
  > RIGHT SIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND TESTED OK IAW AMM: 33-51-07-2-2.
- [SDR FDEA202004300862](https://openairdocs.org/sdr/FDEA202004300862.md): Transition Panel · cracked · Apr 30, 2020 · N963FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > BULK PIT AT BS 1550 & L/H TRANSITION PANEL PUNCHED (CRACKED). TRANSITION PANEL REPAIR ACCOMPLISHED IAW B757-200 SRM 53-00-53-2R REPAIR 2.
- [SDR FDEA202004300860](https://openairdocs.org/sdr/FDEA202004300860.md): Access Panel · cracked · Apr 30, 2020 · N963FD · Boeing 75728A · Nacelle/Pylon, Plate/Skin
  > #2 PYLON, OUTBOARD, HINGED PANEL 443AR, INNER SURFACE CRACKED. REPAIRED INNER SURFACE OF #2 PYLON, OUTBOARD, HINGED PANEL 443AR IAW B757 SRM 51- 70-17-0G RESTORED FINISH IAW B757 AMM 51-21-14 B757 AMM 51-21-15. MINOR REPAIR
- [SDR FDEA2020043080815](https://openairdocs.org/sdr/FDEA2020043080815.md): Seat Track · corroded · Apr 28, 2020 · N963FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > R/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV G
- [SDR FDEA2020043080814](https://openairdocs.org/sdr/FDEA2020043080814.md): Seat Track · corroded · Apr 28, 2020 · N963FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > L/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV G
- [SDR FDEA202004260795](https://openairdocs.org/sdr/FDEA202004260795.md): Strap · gouged · Apr 26, 2020 · N963FD · Boeing 757* · Fuselage Main, Structure
  > FUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2
- [SDR FDEA2020042760795](https://openairdocs.org/sdr/FDEA2020042760795.md): Strap · gouged · Apr 26, 2020 · N963FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > FUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2
- [SDR FDEA2020042760792](https://openairdocs.org/sdr/FDEA2020042760792.md): Seal · cracked · Apr 26, 2020 · N963FD · Boeing 75728A · Engine Collector/Tailpipe/Nozzle
  > #2 EXHAUST NOZZLE 6 OCLOCK POSITION CASE DRAIN SUPPORT PLATE CRACKED REMOVED AND REPLACED SEAL PER B757 SRM 51-40-02-OG AND RR EIPC 78-11-04-03
- [SDR FDEA2020042750785](https://openairdocs.org/sdr/FDEA2020042750785.md): Filler · worn · Apr 25, 2020 · N963FD · Boeing 75728A · Trailing Edge Flaps
  > DURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR ON RIGHT WING OUTBOARD FLAP INBOARD LEADING EDGE SKIN FOUND FLUSH SKIN FILLER TO BE WORN REMOVED WORN FILLER IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR FILLER IAW B757 SRM 57-53-01-2R REPA
- [SDR FDEA2020042740782](https://openairdocs.org/sdr/FDEA2020042740782.md): Mount Bracket · cracked · Apr 24, 2020 · N963FD · Boeing 75728A · Fuselage Main, Attach Fittings
  > AILERON A2B CABLE PULLEY MOUNT BRACKET CRACKED AT STA 358 RBL25. STREAMER ATTACHED REMOVED, FABRICATED AND INSTALLED NEW STIFFENER, P/N 251N6133 IAW DWG 251N6133 REV B, EA # F-2710-T0353742-P1 FLIGHT CONTROLS-AILERON AND TABS-PULLEY BRACKET ASSY STA 345,
- [SDR FDEA2020042310767](https://openairdocs.org/sdr/FDEA2020042310767.md): Skin · dented · Apr 21, 2020 · N963FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERNAL SKIN,STA 1592.7 BETWEEN S22R-S23R DENTED REPAIRED PER B757 SRM 53-00-01-2R REPAIR 29
- [SDR FDEA2018081402006](https://openairdocs.org/sdr/FDEA2018081402006.md): Cover · damaged · Aug 10, 2018 · N963FD · Boeing 75728A · Escape Slide
  > L1 DOOR SLIDE COVER DAMAGED. REPAIRED L1 DOOR SLIDE COVER IAW AMM 25-00-00-8. ACFT OK FOR SERVICE.
- [SDR FDEA2018051871251](https://openairdocs.org/sdr/FDEA2018051871251.md): Heater · failed · May 17, 2018 · N963FD · Boeing 75728A · Heating System
  > APPOACHING THE BEGINNING OF THE HITHR 2 RNAV, ARRIVAL AT 340 LIGHT SMOKE AND AN ELECRICAL BURNING ODOR WAS IMMEDIATELY NOTICED IN THE COCKPIT. THE SOURCE SEEMED TO ORIGINATE ON THE CAPTAIN`S SIDE AROUND THE CONTROL COLUMN. THE SMOKE AND ODOR SEEMED TO DISSAP
- [SDR FDEA201804050858](https://openairdocs.org/sdr/FDEA201804050858.md): Stringer · damaged · Apr 5, 2018 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 16L AT BS 1710 DAMAGED. CUT-OUT THE DAMAGED SECTION OF THE STRINGER, DRILLED A NEW STRINGER AND SPLICE. A REPAIR WAS INSTALLED IAW SRM 53-00-03-2R, REPAIR 2, TYPE I, DETAIL I, FIG 201.
- [SDR FDEA201802220467](https://openairdocs.org/sdr/FDEA201802220467.md): Adc · failed · Feb 22, 2018 · N963FD · Boeing 75728A · Altimeter, Barometric/Encoder
  > AT APPROXIMATELY 7000 FT, LOST THE LT AIR DATA COMPUTER. SPEED TAPE, ALTITUDE, ALL INDICATIONS ON CAPTAIN`S SIDE, ROLLING ERRATICLY UP AND DOWN. DURING TROUBLESHOOTING FOUND THE LT AIR DATA COMPUTER FAULT BALL LATCHED. RETURNED CAPTAIN'S SOURCE SELECT S
- [SDR FDEA201706061571](https://openairdocs.org/sdr/FDEA201706061571.md): Connector · damaged · Jun 6, 2017 · N963FD · Boeing 75728A · Hydraulic Power System Wiring
  > DURING DESCENT, LT ENGINE HYD PUMP EICAS MESSAGE DISPLAYED. TURNED OFF PUMP IAW QRH. PINNED THE NR 2 WIRE ON THE CONNECTOR IAW SWPM. DRY MOTORED THE NR 1 ENGINE IAW JRH. NO FAULTS FOUND, HYDRAULIC PRESSURE NORMAL. COMPLIED WITH PART 1 OF EA F-2930- T03335
- [SDR FDEA201705021325](https://openairdocs.org/sdr/FDEA201705021325.md): Girt Bar · lack of lube · May 2, 2017 · N963FD · Boeing 75728A · Emergency Equipment
  > R1 DOOR WOULD NOT OPEN AT BLOCK IN. R1 DOOR GIRT BAR LOCK PLATES DIRTY AND DRY. LUBED GIRT BAR. OPS NORMAL.
- [SDR FDEA201702170580](https://openairdocs.org/sdr/FDEA201702170580.md): Liner · out of position · Feb 17, 2017 · N963FD · Boeing 75728A · Service Doors
  > WHILE ARMING THE RIGHT CREW ENTRY DOOR THE KNUCKLEBUSTER FAILED TO ARM IN THE CORRECT POSITION. REMAINED FLUSH WITH THE DOOR AND THE RED ARM WAS NOT VISIBLE. ADJUSTED LOWER DOOR LINING ON THE R1 DOOR IAW AMM 52-11-02-4. PERFORMED ADJUSTMENT TEST OF THE R
- [SDR FDEA201609103187](https://openairdocs.org/sdr/FDEA201609103187.md): Light · intermittent · Sep 10, 2016 · N963FD · Boeing 75728A · Passenger Compartment Lighting
  > BOTTOM ONE THIRD OF OVERHEAD PANEL LIGHTS WERE INTERMITTENT. REF WDM 23-71-11, 33-13-31 & CMM 23-70-43 CVR MPN 980-6116-002 DOES NOT CONTAIN CONTACTS FOR INTEGRAL PANEL LIGHTING.
- [SDR FDEA201604211334](https://openairdocs.org/sdr/FDEA201604211334.md): Lock Sensor · failed · Apr 21, 2016 · N963FD · Boeing 75728A · Landing Gear Position and Warning
  > AFTER TAKEOFF, RECEIVED GEAR DISAGREE EICAS ALERT. FOLLOWED CHECKLIST & PERFORMANCE TABLES & CONTINUED. DURING APPROACH WE EXTENDED GEAR EARLY AT APPROX 210 KTS. AT 170 KTS WE HEARD A CLUNK IN NOSE GEAR AREA. LANDING UNEVENTFUL, SWUNG GEAR & GOT LG MONITOR

Next page: https://openairdocs.org/aircraft/N963FD/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 = 'N963FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N963FD/reports

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