# Service difficulty reports: N962FD

A list on [N962FD](https://openairdocs.org/aircraft/N962FD.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 · 130 reports

- [SDR FDEA202607220987](https://openairdocs.org/sdr/FDEA202607220987.md): Fitting · cracked · Jul 22, 2026 · N962FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous Structure
  > CRACK FOUND ON #2 ENGINE LOWER OUTBD MIDSPAR BULKHEAD FITTING. REPAIRED OUTBD MIDSPAR BULKHEAD FITTNG IAW EA F-5450-T0387823 PT1, NACELLS / PYLON - WING PYLON / STRUT - #2 PYLON - PP STA 174.30 MID BULKHEAD - RH FITTING CRACKED AT LOWER VERTICAL FLANGE. M
- [SDR FDEA202601060010](https://openairdocs.org/sdr/FDEA202601060010.md): Bulb · failed · Jan 6, 2026 · N962FD · Boeing 7572G5 · Emergency Lighting
  > DURING MX PRE-FLIGHT, FOUND R1 EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 FOUND R1 EMERGENCY EXIT SIGN HAS 9 BULBS OUT. REMOVED AND REPLACED 9 FAULTY BULBS AS PER ABOVE REF. PART NUMBER 0L3071BPEGPL. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202601060009](https://openairdocs.org/sdr/FDEA202601060009.md): Bulb · failed · Jan 6, 2026 · N962FD · Boeing 7572G5 · Emergency Lighting
  > DURING MX PRE-FLIGHT, FOUND L1 EMERGENCY EXIT SIGN DIM. AMM 33-51-01-2 FOUND L1 EMERGENCY EXIT SIGN HAS 7 BULBS OUT. REMOVED AND REPLACED 7 FAULTY BULBS AS PER ABOVE OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202406040767](https://openairdocs.org/sdr/FDEA202406040767.md): Floorbeam · corroded · Jun 4, 2024 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEAM UPPER CHORD AT MAIN CABIN STA 344-346 BETWEEN LBL 7 - LBL 21, AFTER EVALUATION FOUND OUT OF
- [SDR FDEA202311281899](https://openairdocs.org/sdr/FDEA202311281899.md): Slide · damaged · Nov 28, 2023 · N962FD · Boeing 757200 · Escape Slide
  > DOOR WAS ACCIDENTALLY ARMED, AND THEN OPENED FROM THE OUTSIDE AND THE SLIDE FELL OUT, BUT DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE. OPS CHECKS GOOD.
- [SDR FDEA202210112550](https://openairdocs.org/sdr/FDEA202210112550.md): Buss · failed · Oct 11, 2022 · N962FD · Boeing 757 · Electrical Power System Wiring
  > TURNING FINAL FOR THE RUNWAY, LOST LT GEN & LT AC BUSS, CONTINUED WITH A GO AROUND & RAN QRH & WERE ABLE ABLE TO GET A PARTIAL COCKPIT BACK. CONTINUED APPROACH AFTER DECLARING AN EMERGENCY. PERFORMED REMOVE AND REPLACE OF THE LT BUSS TIE BREAKER REF TSI 242
- [SDR FDEA202209282381](https://openairdocs.org/sdr/FDEA202209282381.md): Gcu · failed · Sep 28, 2022 · N962FD · Boeing 7572G5 · AC Generator-Alternator
  > ON FINAL TO KSBD LOST THE LEFT AC BUS. WE HAD L GEN OFF, L BUS OFF, AND L BUS TIE TO ISLN ON THE OVERHEAD PANEL. LOST ASSOCIATED EQUIPMENT ON CAPTAIN SIDE. FLAPS AT 20 DEGREES. WENT AROUND AND RAN THE AC BUS OFF CHECKLIST. WE WE ABLE TO GET THE LEFT
- [SDR FDEA202208262078](https://openairdocs.org/sdr/FDEA202208262078.md): Support Bracket · corroded · Aug 26, 2022 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous Structure
  > AUXILIARY POWER UNIT DOOR SURROUND STRUCTURE CORRODED. REMOVED & REPLACED ANGLE SUPPORT BRACKETS & APU FWD STRAP OF AUXILIARY POWER UNIT DOOR SURROUND STRUCTURE IAW BAC DWG 148N3152-1, 148N3152-2,148N3141-5 & 148N3138-20.
- [SDR FDEA202208222028](https://openairdocs.org/sdr/FDEA202208222028.md): Inlet · corroded · Aug 22, 2022 · N962FD · Boeing 7572G5 · Nacelle/Pylon, Main Frame
  > #1 ENGINE INLET COWL MOUNT FLANGE ON THE ENGINE SIDE IS CORRODED SPORADICALLY AROUND THE ENTIRE CIRCUMFERENCE OF THE ENGINE REMOVED AND REPLACED ENGINE PER FEDEX CARD # 7180260-01-02
- [SDR FDEA202208192007](https://openairdocs.org/sdr/FDEA202208192007.md): Panel · cracked · Aug 19, 2022 · N962FD · Boeing 757200 · Wing, Plate/Skin
  > R.WING #8 SLAT I/B AUX TRACK LOWER TRAILING EDGE CLOSE OUT PANEL IS CRACKED. REMOVE AND REPLACED CLOSE OUT PANEL WITH NEW PANEL PER BAC DWG 114N4147 REV A AND B757 AMM 27-81-02-4
- [SDR FDEA202208181997](https://openairdocs.org/sdr/FDEA202208181997.md): Filler · corroded · Aug 18, 2022 · N962FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > NOSE LANDING GEAR WHEEL WELL, UPPER AFT ACCESS PANEL 117CL, FORWARD SIDE OF STA 377.7 LBL 10 TO LBL 25, PLATE CORRODED. REMOVED, FABRICATED AND REPLACED NEW FILLER IAW VENTURA DWG 3471 REV B
- [SDR FDEA202208161983](https://openairdocs.org/sdr/FDEA202208161983.md): Skin · cracked · Aug 16, 2022 · N962FD · Boeing 757200 · Wing, Plate/Skin
  > R.WING O/B FIXED L/E SKIN UPPER SURFACE IS CRACKED @ #7 SLAT I/B MAIN TRACK LOCATION. APPROX. FSS 345 REPAIRED R.WING FIXED L/E SKIN PER B757 SRM 57-41-01 AND 51-70-07.
- [SDR FDEA202208151979](https://openairdocs.org/sdr/FDEA202208151979.md): Web · damaged · Aug 15, 2022 · N962FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR I/B SIDE HAS 1 EA GOUGE AT THE WEB APPROX BS 519.5 BETWEEN WL210 AND 220 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202208151978](https://openairdocs.org/sdr/FDEA202208151978.md): Web · gouged · Aug 15, 2022 · N962FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR I/B SIDE HAS 1 EACH GOUGE AT WEB APPROX BS 602 WL220 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202208111961](https://openairdocs.org/sdr/FDEA202208111961.md): Plate · cracked · Aug 11, 2022 · N962FD · Boeing 757200 · Wing Miscellaneous Structure
  > R. WING T/E WIGGLE PLATE IS CRACKED, O/B OF THE I/B FLAP, BELOW # 8 SPOILER REMOVE AND REPLACED WIGGLE PLATE PER BAD DWG 113N1630 REV C
- [SDR FDEA202011212942](https://openairdocs.org/sdr/FDEA202011212942.md): Girt Bar · failed · Nov 21, 2020 · N962FD · Boeing 7572G5 · Emergency Equipment
  > L1 GIRT BAR CENTERING BLOCK EXFOLIATED. REPLACED GIRT BAR AND GIRT BAR CENTERING BLOCK, REF B757 AMM 25-66-10-2. A/C OK FOR SERVICE.
- [SDR FDEA202009272333](https://openairdocs.org/sdr/FDEA202009272333.md): Idg · malfunctioned · Sep 27, 2020 · N962FD · Boeing 7572G5 · AC Generator-Alternator
  > RECEIVED A LT GEN OFF EICAS ON TAKEOFF ROLL AND REJECTED THE TAKEOFF. RAN THE REJECTED TAKEOFF CHECKLIST AND THE QRH, WHICH RESET THE FAULTS. TRIED THE TAKEOFF AGAIN AND REJECTED FOR THE SAME LT GEN OFF EICAS FAULT. REPLACED NR 1 ENGINE IDG. OPS AND LEAK
- [SDR FDEA2020072761662](https://openairdocs.org/sdr/FDEA2020072761662.md): Tee Fitting · corroded · Jul 26, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Attach Fittings
  > MAIN DECK BETWEEN STA 920-1040 RBL45.5 T CHORD CORRODED REMOVED CORR ON T CHORD STA 900-1040 RBL 45.5 IAW B757 SRM 51-10-02. ORIG MAT.090 REM O FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW T CHORD IAW B757 SR
- [SDR FDEA202007241642](https://openairdocs.org/sdr/FDEA202007241642.md): Tee Fitting · corroded · Jul 24, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN DECK STA 1200 BETWEEN LBL 24.75- LBL 45.5 T CHORD CORRODED REMOVED CORROSION FROM BS 1200 FLOOR BEAM (T CHORD) IAW B757 SRM 51-10-02. ORIG MAT.125 REMAING 0 FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DET III, REPAIRED FLOOR BEAM IAW B757 S
- [SDR FDEA202007201594](https://openairdocs.org/sdr/FDEA202007201594.md): Seat Track · corroded · Jul 20, 2020 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION IN MAIN CABIN @ RBL-45.5 BETWEEN STA. 1640 AND 1660 SEAT TRACK AT STA. 1640-1660 RBL45.5 OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-02 AND
- [SDR FDEA2020072301594](https://openairdocs.org/sdr/FDEA2020072301594.md): Seat Track · corroded · Jul 20, 2020 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION IN MAIN CABIN AT RBL 45.5 BETWEEN BS 1640 AND 1660. FOUND OUT OF LIMITS DUE TO EXFOILATION IAW SRM 53-00-52-1A, FIG 101. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW SRM 51-40-00-02, DWG 657N3318, REV B, AND 657N3311, REV B
- [SDR FDEA202007171564](https://openairdocs.org/sdr/FDEA202007171564.md): Seat Track · corroded · Jul 17, 2020 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN BS 1060 - 1180 LBL 58.22, THE SEAT TRACK WAS CORRODED. REPAIRED IAW EA F-5310-T0355139 P1.
- [SDR FDEA202007171563](https://openairdocs.org/sdr/FDEA202007171563.md): Frame · cracked · Jul 17, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Frame
  > DURING AN NDT OPEN HOLE INSPECTION, TWO CRACK NDICATIONS NOTED IN LOWER INBOARD HOLE AT APPROX. 8 AND 4 O'CLOCK POSTIONS LOOKING AFT. BS 1640 FRAME STRINGER 14L. ALL WORK ACCOMPLISHED IAW EA F-5310-T0355050 P1.
- [SDR FDEA202007171562](https://openairdocs.org/sdr/FDEA202007171562.md): Seat Track · corroded · Jul 17, 2020 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 1180-1200 LBL 44.5 SEAT TRACK CORRODED. REMOVED CORR ON SEAT TRACK STA 1180-1200 LBL 44.5 IAW B757 SRM 51-10-02. ORIG MAT.070 REM 0 OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW
- [SDR FDEA202007171561](https://openairdocs.org/sdr/FDEA202007171561.md): Crease Beam · corroded · Jul 17, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Structure
  > MAIN DECK BS 1600, LEFT SIDE INBD CREASE BEAM CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-60-13-1A, FIG 101. REPAIRED THE CREASE BEAM IAW SRM 53-00-13-2R, REP 1, ALT 1.
- [SDR FDEA2020072351517](https://openairdocs.org/sdr/FDEA2020072351517.md): Floorbeam · corroded · Jul 15, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN DECK STA 1015 BETWEEN LBL24.75-LBL45.5 FLOOR SUPPORT CORRODED REMOVED CORR ON FLOOR SUPPORT STRAP ONLY IAW B757 SRM 51-10-02. ORIG MAT.012 REM.005 LOSS.007 FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101. REMOVE, FABRICATED AND INSTALLED NEW
- [SDR FDEA2020071751517](https://openairdocs.org/sdr/FDEA2020071751517.md): Strap · corroded · Jul 15, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN DECK BS 1015 BETWEEN LBL 24.75 - LBL 45.5 FLOORBEAM CORRODED. REMOVED THE CORROSION ON THE STRAP ONLY IAW SRM 51-10-02. ORIG MAT.012 REM.005 LOSS.007, FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101. REMOVED, FABRICATED AND INSTALLED A NEW STRA
- [SDR FDEA202007091480](https://openairdocs.org/sdr/FDEA202007091480.md): Floorbeam · cracked · Jul 9, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR BEAM CRACKED, BS 580 BELOW SEAT TRACK LBL 44.5. TRIMMED UPPER FLANGE OF THE FLOORBEAM SPLICE, FABRICATD A REPAIR ANGLE, RADIUS STRAP, AND INSTALLED IAW EA TF-5310-T0355035 P1.
- [SDR FDEA2020071091480](https://openairdocs.org/sdr/FDEA2020071091480.md): Floorbeam · cracked · Jul 9, 2020 · N962FD · Boeing 7572G5 · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM CRACKED BS 580 BELOW SEAT TRACK LBL 44.5.
- [SDR FDEA2019110762899](https://openairdocs.org/sdr/FDEA2019110762899.md): Circuit Card · malfunctioned · Nov 6, 2019 · N962FD · Boeing 7572G5 · Detection System
  > DURING CLIMBOUT GOT STATUS MESSAGE L ENG OH LP2 PER CREW REPORT, STATUS MESSAGE WENT OUT ON LANDING. NO STATUS MESSAGE SHOWN. TROUBLESHOT PER 757 FIM 26-11/802 BLOCK 103. SYSTEM BITE SHOWED NO FAULTS. PER BLOCKK 103 REMOVED AND REINSTALLED AFOLTS CARD M
- [SDR FDEA201803010538](https://openairdocs.org/sdr/FDEA201803010538.md): Fseu · malfunctioned · Mar 1, 2018 · N962FD · Boeing 7572G5 · Trailing Flap Position Indicating System
  > DURING CRUISE, HAD A TE FLAP ASYMETERY EICAS MESSAGE. PERFORMED QRH PROCEDURE AND LANDED FLAPS UP. HAPPENED AFTER ABOUT 1.5 HOURS IN MODERATE TO LIGHT TURBULANCE. TROUBLESHOT IAW FIM 27-51, FAULT TREE 803. FOUND THE NR 1 FSEU FAULT, LEFT WING ASYMETER
- [SDR FDEA201801300276](https://openairdocs.org/sdr/FDEA201801300276.md): Sensor · malfunctioned · Jan 30, 2018 · N962FD · Boeing 7572G5 · Escape Slide
  > DURING CRUISE, NOTICED THE SLIDE LIGHT FOR THE L1 DOOR WAS EXTINGUISHED. REPLACED THE SENSOR IAW AMM 25-66-11-4. OPS CHECKED GOOD.
- [SDR FDEA201708112188](https://openairdocs.org/sdr/FDEA201708112188.md): Cover · dislodged · Aug 11, 2017 · N962FD · Boeing 7572G5 · Escape Slide
  > LEFT FWD ENTRY DOOR SLIDE COVER DISLODGED. IAW MM 25-66-01-4, REINSTALLED THE SLIDE COVER. OK FOR SERVICE.
- [SDR FDEA201607292656](https://openairdocs.org/sdr/FDEA201607292656.md): Hinge · dirty · Jul 29, 2016 · N962FD · Boeing 7572G5 · Fuselage, Door Hinge
  > LEFT CABIN DOOR HARD TO CLOSE. FOUND DEBRIS IN DOOR HINGE. CLEANED AND OPERATED THE DOOR SEVERAL TIMES IAW AMM 52-11-00-2, NO DEFECTS NOTED.
- [SDR FDEA201607012222](https://openairdocs.org/sdr/FDEA201607012222.md): Shear Plate · corroded · Jul 1, 2016 · N962FD · Boeing 7572G5 · Fuselage Miscellaneous Structure
  > MAIN CABIN SHEAR PLATE BS 380 - 440 BL 0 TO RBL 24.75 HAS LIGHT CORROSION. BLENDED SHEAR PLATE IAW SRM 51-10-02, ORIGINAL.125 REM.057 LOSS.068. FOUND OUT OF LIMITS IAW SRM 757, RCB 4.4.3. REPAIRED AREA IAW SRM, RCB 5.4.3, DOUBLER MADE FROM 7075, T6,.125
- [SDR FDEA201510223332](https://openairdocs.org/sdr/FDEA201510223332.md): Collar · broken · Oct 22, 2015 · N962FD · Boeing 7572G5 · Passenger/Crew Doors
  > L1 DOOR WOULD NOT OPEN FULL TRAVEL. REPLACED PREVIOUSLY REMOVED BROKEN HOLD & OPEN COLLAR IAW AMM 52-11-08-8. ACFT OK FOR SERVICE.
- [SDR FDEA201504231288](https://openairdocs.org/sdr/FDEA201504231288.md): Valve · malfunctioned · Apr 23, 2015 · N962FD · Boeing 7572G5 · Landing Gear Brake System
  > AT SLOW TAXI SPEEDS WITH PRESS ON BRAKES, THE BRAKES WILL SLOWLY RELEASE, RESULTING IN, PULSATING BRAKES DURING TAXI. IAW MM 12-15-05, CHECKED BRAKE CONTROL ACCUMULATOR, CHARGE WAS NORMAL. WITH ONLY RT ACMP ON, RT EICAS HYD PRESS IS 3000 PSI, BRAKE PRESS GAU
- [SDR FDEA201504041151](https://openairdocs.org/sdr/FDEA201504041151.md): Door · lack of lube · Apr 4, 2015 · N962FD · Boeing 7572G5 · Passenger/Crew Doors
  > L1 DOOR WILL NOT OPEN ALL THE WAY FWD TO LOCKED OPEN POSITION. LUBED DOOR HINGE TORQUE TUBE. DOOR OPENS & CLOSES NORMALLY.
- [SDR FDEA201502200556](https://openairdocs.org/sdr/FDEA201502200556.md): Door · unknown · Feb 20, 2015 · N962FD · Boeing 7572G5 · Passenger/Crew Doors
  > DOOR 1L WILL ONLY OPEN 1/2 WAY & IS TIGHT.
- [SDR FDEA201406301595](https://openairdocs.org/sdr/FDEA201406301595.md): Skin · dented · Jun 30, 2014 · N962FD · Boeing 7572G5 · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE HAS A DENT AT BS 502 JUST BELOW STRINGER 26L. COMPLIED WITH EA F-5330-T0309215 REV NR PS P1 FUSELAGE PLATES & SKINS STATION 502-5-266-SKIN DENT.
- [SDR FDEA201406301594](https://openairdocs.org/sdr/FDEA201406301594.md): Skin · dented · Jun 30, 2014 · N962FD · Boeing 7572G5 · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE HAS A DENT AT BS 1701 BETWEEN STRINGERS 19L & 20L. COMPLIED WITH F-5330-T0309246 REV NR PS P1 FUSELAGE PLATES & SKINS STATION 1701 SKIN DENT BETWEEN STRINGER 19L & 20L.
- [SDR FDEA201406251548](https://openairdocs.org/sdr/FDEA201406251548.md): Skin · dented · Jun 25, 2014 · N962FD · Boeing 7572G5 · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE HAS A DENT AT BS 763 JUST BELOW STRINGER 14L. COMPLIED WITH FX EA F-5330-TO309193 PT 1 FUSELAGE SKIN DENT BELOW STRINGER 14L AND AFT OF STATION 760.
- [SDR FDEA201406231533](https://openairdocs.org/sdr/FDEA201406231533.md): Seat Track · corroded · Jun 23, 2014 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > LT COURIER SEAT TRACK HAS CORROSION AT BS 345, LBL 4. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK AT BS 345 LBL 4 IAW B757 DWG 3504-NC-2, B757 SRM 51-40-05, & 51-40-02.
- [SDR FDEA201406231532](https://openairdocs.org/sdr/FDEA201406231532.md): Seat Track · corroded · Jun 23, 2014 · N962FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT COURIER SEAT TRACK HAS CORROSION AT BS 345. REMOVED, FABRICATED & INSTALLED NEW SEAT TRACK IN COURIER AREA AT BS 345 IAW SRM 51-40-02, 51-40-5, 51-20-61, & DWG 3504-NC-2.
- [SDR FDEA201403110478](https://openairdocs.org/sdr/FDEA201403110478.md): Light · inoperative · Mar 11, 2014 · N962FD · Boeing 7572G5 · Emergency Lighting
  > R1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RE LAMPED IAW AMM 33-51-06, OPERATIONS CHECKED GOOD.
- [SDR FDEA201303270674](https://openairdocs.org/sdr/FDEA201303270674.md): Handle · detached · Mar 27, 2013 · N962FD · Boeing 7572G5 · Flight Compartment Windows
  > CAPTAIN`S WINDOW CRANK HANDLE DETACHED. REPLACED WINDOW CRANK HARDWARE. OPS CHECKED GOOD IAW AMM 56-11-04-4.
- [SDR FDEA201212294398](https://openairdocs.org/sdr/FDEA201212294398.md): Connector · damaged · Dec 29, 2012 · N962FD · Boeing 7572G5 · Navigation System Wiring
  > WHILE INSTALLING PANEL ON LT SIDE OF PEDESTAL REF WRI 27-60/0753. FOUND CAPT'S STICK SHAKER WIRES ARCING. CONNECTOR MSN 1299126. REMOVED SPORTS TAPE AND FOUND WIRES WERE BROKEN INSIDE CLAMP FOR BACKSHELL. PINS DO NOT COME OUT OF THIS CONNECTOR AND WIRES HA
- [SDR FDEA201211023816](https://openairdocs.org/sdr/FDEA201211023816.md): Lamp · inoperative · Nov 2, 2012 · N962FD · Boeing 7572G5 · Emergency Lighting
  > RT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.
- [SDR FDEA201211013806](https://openairdocs.org/sdr/FDEA201211013806.md): Lamp · inoperative · Nov 1, 2012 · N962FD · Boeing 7572G5 · Emergency Lighting
  > RIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.
- [SDR FDEA201211013805](https://openairdocs.org/sdr/FDEA201211013805.md): Lamp · inoperative · Nov 1, 2012 · N962FD · Boeing 7572G5 · Emergency Lighting
  > RIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED PER MM 33-51-06-2-1 OPS CHECKED NORMAL

Next page: https://openairdocs.org/aircraft/N962FD/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 = 'N962FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N962FD/reports

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