# Service difficulty reports: N959FD

A list on [N959FD](https://openairdocs.org/aircraft/N959FD.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 · 148 reports

- [SDR FDEA202305040803](https://openairdocs.org/sdr/FDEA202305040803.md): Unknown · unknown · May 4, 2023 · N959FD · Boeing 757200 · Cabin Pressure Control System
  > PDIS 959 21-30 9546 03MAY23 IND OPEN U AT FL 350 WE RECEIVED A CABIN ALT MASTER WARNING AND EICAS WARNING. CABIN ALT WAS AT 10,000 FT. COMPLIED WITH QRH. CABIN ALT CLIMBED TO 11,000 FT BEFORE WE WERE ABLE TO DESCEND. AROUND FL 180 CABIN AL
- [SDR FDEA202206231517](https://openairdocs.org/sdr/FDEA202206231517.md): Engine · leaking · Jun 23, 2022 · N959FD · Boeing 757200 · Fuel Controlling System
  > PDIS 959 73-20 8902 23JUN22 JAX OPEN U LOGPAGES:386108 ON TAKEOFF, CLIMB, RIGHT ENGINE DID NOT REACH TAKEOFF POWER SETTING. OM CLIMB OUT RIGHT ENGINESURGING WHEN SELECTED VNAV TMSP DID NOT GO INTO CLIMB MODE AND PROGRAMMED SPEEDS IN FMS DID
- [SDR FDEA202206171461](https://openairdocs.org/sdr/FDEA202206171461.md): Skin · gouged · Jun 17, 2022 · N959FD · Boeing 757200 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL GOUGED REPAIRED RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL IAW B757 SRM 57-53-01-2R-1 AND 51-70-10-2R REPAIR 4
- [SDR FDEA202206171460](https://openairdocs.org/sdr/FDEA202206171460.md): Wedge · delaminated · Jun 17, 2022 · N959FD · Boeing 757200 · Trailing Edge Flaps
  > R/W I/B FWD FLAP LOWER SURFACE T/E WEDGE IS DELAMINATED REMOVED AND REPLACED WEDGE PER BOEING DWG # 113N2603
- [SDR FDEA202206151433](https://openairdocs.org/sdr/FDEA202206151433.md): Doubler · cracked · Jun 15, 2022 · N959FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE PYLON INTERNAL SPLICE STRAP FOR PANELS 441AL AND 442AL RUBSTRIP IS CRACKED AND BROKEN IN SEVERAL SPOTS. REMOVE REPAIRED AND REINSTALLED PER BAC DWG 313N5003 REV Y AND FEDEX EA F-5450-T0368926 TITLE: NACELLES/PYLONS - WING PYLON/STRUT - NO 2 PYLO
- [SDR FDEA202206151432](https://openairdocs.org/sdr/FDEA202206151432.md): Skin · cracked · Jun 15, 2022 · N959FD · Boeing 757200 · Wing, Plate/Skin
  > L/W #3 SLAT I/B TRACK COVE PANEL IS CRACKED ON I/B SIDE REMOVED AND REPLACED PER BOEING DWG # 114N4077 REV F
- [SDR FDEA202206151431](https://openairdocs.org/sdr/FDEA202206151431.md): Fairing · cracked · Jun 15, 2022 · N959FD · Boeing 757200 · Nacelle/Pylon, Main Frame
  > #1 PYLON AFT NACELLE TRAILING EDGE IS CRACKED FWD OF THE SAIL BOAT FAIRING. REPAIRED FAIRING SKIN PER FEDEX EA # F-5480-T0368778 TITLE: NACELLES/PYLON - FILLETS/FAIRINGS - LH STRUT AFT FAIRING, TRAILING EDGE SKIN, CRACK REPAIR.
- [SDR FDEA202206141427](https://openairdocs.org/sdr/FDEA202206141427.md): Cover · cracked · Jun 14, 2022 · N959FD · Boeing 757200 · Engine (Turbine/Turboprop)
  > #1 ENGINE I/B FAN COWL UPPER AFT HINGE COVER IS CRACKED. REPAIRED HINGE COVER PER FEDEX EA F-7110-T0368874 TITLE: POWERPLANT - WING ENG COWL - NO 1 INBD FAN COWL, HINGE SHIELD, CRACK AND DENT DAMAGE.
- [SDR FDEA202206131424](https://openairdocs.org/sdr/FDEA202206131424.md): Strip · cracked · Jun 13, 2022 · N959FD · Boeing 757200 · Nacelle/Pylon, Main Frame
  > #1 PYLON FWD CHAFE STRIP UNDER PANEL 431AL IS WORN, CRACKED AND MISSING. REMOVED AND REPLACED CHAFE STRIP PER BAC DWG 313N5036 REV M, BAC 5000 AND B757 SRM 51-40- 02
- [SDR FDEA202206101412](https://openairdocs.org/sdr/FDEA202206101412.md): Support Angle · cracked · Jun 10, 2022 · N959FD · Boeing 757200 · Aerodynamic Fairings
  > RIGHT MAIN LANDING GEAR WHEEL WELL WING TO BODY SUPPORT ANGLE IS CRACKED APPROX. BS1088 REMOVED, FABRICATED NEW PART, AND INSTALLED PER BAC DWG 149N7552 REV F
- [SDR FDEA202206071391](https://openairdocs.org/sdr/FDEA202206071391.md): Web · damaged · Jun 7, 2022 · N959FD · Boeing 757200 · Cargo/Baggage Doors
  > MCD LOWER INTERNAL WEB IS DAMAGED IN 2EA LOCATIONS AT APPROX STA 580 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202206071390](https://openairdocs.org/sdr/FDEA202206071390.md): Web · damaged · Jun 7, 2022 · N959FD · Boeing 757200 · Cargo/Baggage Doors
  > MCD LOWER INTERNAL WEB IS DAMAGED IN 2EA LOCATIONS AT APPROX STA 500 AND STA 520 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202206061380](https://openairdocs.org/sdr/FDEA202206061380.md): Stop Fitting · gouged · Jun 6, 2022 · N959FD · Boeing 757200 · Passenger/Crew Doors
  > L1 DOOR UPPER FWD DOOR STOP IS GOUGED REMOVED, LOCATED, DRILLED AND INSTALLED NEW STOP FITTING IAW B757-2 DWG 141N8371 REV J AND 141N8341 REV D
- [SDR FDEA202204261057](https://openairdocs.org/sdr/FDEA202204261057.md): Gust Lock · broken · Apr 26, 2022 · N959FD · Boeing 757200 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BROKEN PERFORMED ADJUSTMENT/ TEST ON L1 DOOR REF AMM 52-11-00-5. NO DEFECTS NOTED. OKAY FOR SERVICE
- [SDR FDEA202109222357](https://openairdocs.org/sdr/FDEA202109222357.md): Transmission · low quantity · Sep 22, 2021 · N959FD · Boeing 757236 · Trailing Edge Flap Control System
  > WHEN SELECTING FLAPS TO 20, GOT TE FLAPS DISAGREE EICAS. COMPLIED WITH QRH, TRAILING EDGE LIGHT DISAPPEARED. LANDED WITHOUT ISSUE. FOUND LEFT WING OB FLAP TRANSMISSION FOR IB FLAP VERY LOW ON FLUID. SERVICED WITH BRACO 795 PER B757 AMM 12-13-06-3.
- [SDR FDEA202009302360](https://openairdocs.org/sdr/FDEA202009302360.md): Sensor · inoperative · Sep 30, 2020 · N959FD · Boeing 757236 · Door Warning System
  > PDIS 959 52-70 7383 30SEP20 MEM OPEN U. RT EMERGENCY DOOR EICAS MESSAGE DURING CRUISE. PRESSURIZATION APPEARED NORMAL. SHGN 30SEP20 09:25 MEM U SHGN 30SEP20 09:25 MEM U. FOUND GAP BETWEEN TARGET AND SENSOR AT NUMBER 3 RT EMERGENCY EXIT DOOR TO BE TOO SMAL
- [SDR FDEA202006251355](https://openairdocs.org/sdr/FDEA202006251355.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 740 - 720 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 720 TO STA 740 LBL 60 ORIGINAL MAT.050" 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40
- [SDR FDEA202006251353](https://openairdocs.org/sdr/FDEA202006251353.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 700 - 720 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 700 - 720 LBL 63. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-OG AND B DWG 143N5410 REV F. ORIG MAT 0.050", MAT REMOVED 0.010", MAT REMAI
- [SDR FDEA202006251352](https://openairdocs.org/sdr/FDEA202006251352.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 700 - 720 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 700 - 720 LBL 63. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-OG AND B DWG 143N5410 REV F. ORIG MAT 0.056", MAT REMOVED 0.0008", MAT REMA
- [SDR FDEA202006251350](https://openairdocs.org/sdr/FDEA202006251350.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 740-720 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 720 TO STA 740 LBL 63 ORIGINAL MAT.056" 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02
- [SDR FDEA202006251351](https://openairdocs.org/sdr/FDEA202006251351.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 680 - 700 LBL 63 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 680 TO STA 700 LBL 63 ORIGINAL MAT.056", MAT LOSS.017", REMAINING.039", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AND INS
- [SDR FDEA202006251354](https://openairdocs.org/sdr/FDEA202006251354.md): Floor Support · corroded · Jun 25, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STA 680 - 700 LBL 60 CORRODED. REMOVED CORROSION AT FLOOR SUPPORT STA 680 TO STA 700 LBL 60 ORIGINAL MAT.050", MATERIAL LOSS.010", MAT REMAINING.040" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED, FABRICATED AN
- [SDR FDEA202006231322](https://openairdocs.org/sdr/FDEA202006231322.md): Seat Track · corroded · Jun 23, 2020 · N959FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 1180-1200 RBL44.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT SEAT TRACK FLANGE STA 1180 - 1280 RBL 44.5, ORIG MAT 0.090", MAT REMOVED 0.060", MAT REMAINING 0.030", OUT OF LIMITS IAW SRM 53-00-02-1A. REMOVED, FABRICATED AND INSTALL
- [SDR FDEA202006231321](https://openairdocs.org/sdr/FDEA202006231321.md): Seat Track · corroded · Jun 23, 2020 · N959FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BS 1060, LBL 58 SEAT TRACK FLANGE CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. ORIG MAT.070 REM.046 LOSS.024, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW IAW SRM 53-40-52-01, 51
- [SDR FDEA2020061981272](https://openairdocs.org/sdr/FDEA2020061981272.md): Floorbeam · cracked · Jun 18, 2020 · N959FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN DECK BS 1018 BETWEEN RBL 24.75 - RBL 44.5 FLOOR SUPPORT DAMAGED. REMOVED COVER PLATE CRACKED AT BS 1018 BETWEEN RBL 24.75 - RBL 44.5. FABRICATED AND INSTALLED NEW COVER PLATE IAW DWG 144N5081 REV. A,C, AND SRM 51-40-02-OG.
- [SDR FDEA2020061981271](https://openairdocs.org/sdr/FDEA2020061981271.md): Floorbeam · cracked · Jun 18, 2020 · N959FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN DECK STA 1055 BETWEEN LBL 24.75 - LBL 44.5 FLOOR SUPPORT CRACKED. REMOVED COVER PLATE CRACKED AT STA 1055 BETWEEN LBL 24.75 - LBL 44.5. FABRICATED AND INSTALLED NEW COVER PLATE IAW DWG 144N5081 REV. A,C AND SRM 51-40-02-OG.
- [SDR FDEA2020061971262](https://openairdocs.org/sdr/FDEA2020061971262.md): Plate · corroded · Jun 17, 2020 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1017 BETWEEN LBL 24.75 FLOOR SUPPORT CORRODED. MAIN DECK STATION 1017 BETWEEN LBL 24.75 - 44.50 FLOOR SUPPORT PLATE 100% MATL. LOSS REMOVED PLATE,FABRICATED AND INSTALLED NEW PLATE IAW BOEING DWG 144N5081 REV C/A. AND B 757 SRM 51-40-02-OG.
- [SDR FDEA2020052621033](https://openairdocs.org/sdr/FDEA2020052621033.md): Charger · inoperative · May 22, 2020 · N959FD · Boeing 757236 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVER R1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSY (POWER SUPPLY) M730 REF AMM 33-51-07-2. REMOVED AND REPLACED R1 EMERGENCY EXIT SIGN REF AMM 33-51-01-2. EMERGENCY LIGHTS OPS CHECK
- [SDR FDEA202001200178](https://openairdocs.org/sdr/FDEA202001200178.md): Gust Lock · damaged · Jan 20, 2020 · N959FD · Boeing 757236 · Passenger/Crew Doors
  > DURING SERVICE FOUND LT ENTRY DOOR GUST DOOR LOCK BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN GUST LOCK REF AMM 52-11-08-8. MATERIAL 140N6008-1 COLLAR ASSY MATERIAL 140N6009-1 CATCH ASSY.
- [SDR FDEA2019121061807](https://openairdocs.org/sdr/FDEA2019121061807.md): Cover · dislodged · Nov 1, 2019 · N959FD · Boeing 757236 · Life Raft
  > GROUND PERSONNEL DISLODGED COVER FOR RAFT AT L1. CALLED MX TO RESEAT INSTALLED L1 DOOR SLIDE COVER REF. 757 AMM 52-11-02-4. A/C OK FOR SERVICE.
- [SDR FDEA201901120113](https://openairdocs.org/sdr/FDEA201901120113.md): Wire · broken · Jan 12, 2019 · N959FD · Boeing 757236 · Air Conditioning System Wiring
  > DURING CRUISE F/O TURNMED ON FOOT HEATER AND A SPARK AND A POP WAS FOLLOWED BY ELECTRICAL SMOKE. TURNED HEATER OFF AND SMOKE DISSIPATED. FOUND WIRES TO F/O LEFT FOOT HEATER BROKEN. REPAIRED BROKEN WIRES PER SWP CHAPTER 20-30 REFERENCING WIRING DIAGRAM 21-45-11
- [SDR FDEA201810222967](https://openairdocs.org/sdr/FDEA201810222967.md): Light · inoperative · Oct 22, 2018 · N959FD · Boeing 757236 · Emergency Lighting
  > RIGHT SIDE EMERGENCY SLIDE LIGHT INOP. RELAMPED RT EMERGENCY EVACUATION SLIDE LIGHT AS PER AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR FDEA201806051395](https://openairdocs.org/sdr/FDEA201806051395.md): Seat Track · corroded · Jun 5, 2018 · N959FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, COURIER SEAT TRACK, CORROSION ON UPPER SURFACE AT RBL 12 AND BETWEEN FS 345 AND FS 365. REMOVED CORROSION ON SEAT TRACK AT CABIN COURIER AREA FS 345 TO 365 RBL 12 AND EVALUATED DAMAGE ORIG. MAT:.070", MAT LOSS:.011", MAT. REM:.059" FOUND OUT OF
- [SDR FDEA201806051396](https://openairdocs.org/sdr/FDEA201806051396.md): Floorbeam · cracked · Jun 5, 2018 · N959FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM, CRACK IN UPPER SURFACE AT FS 324 AND APPROX RBL 55. REMOVED CORROSION IAW SRM 51-10-02-0G, EVALUATED AREA ORIGINAL MAT.120", MAT REMAINING.077", MAT LOSS.043", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG DETAIL VI, CUT OUT, FABRI
- [SDR FDEA201806041386](https://openairdocs.org/sdr/FDEA201806041386.md): Floor Support · corroded · Jun 4, 2018 · N959FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CORROSION ON UPPER SURFACE BETWEEN FS 345 AND FS 365 AT BL 0. REMOVED CORROSION ON FLOOR SUPPORT ORIGINAL MAT.063", MAT REMAINING.020". MAT LOSS.043", FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G AND 53-00-51-1A DETAIL III FIG 101,
- [SDR FDEA201803200741](https://openairdocs.org/sdr/FDEA201803200741.md): Unknown · malfunctioned · Mar 20, 2018 · N959FD · Boeing 757236 · Trailing Edge Flap Control System
  > DURING APPROACH TO LANDING TE FLAP DISAGREE APPEARED ON EICAS. FLAPS WOULD NOT MOVE, STUCK ABOUT 22. EXECUTED MISSED APPROACH AND FOLLOWED QRH. UNEVENTFUL LANDING AFTER DECLARING EMERGENCY. PERFORMED BITE TO FSEU NR 1, NR 2, & NR 3 AND CYCLED SEVERAL TIMES FL
- [SDR FDEA201708112187](https://openairdocs.org/sdr/FDEA201708112187.md): Lamp · inoperative · Aug 11, 2017 · N959FD · Boeing 757236 · Emergency Lighting
  > R1 DOOR EMERGENCY SLIDE LIGHT FOUND INOPERATIVE DURING TEST. REPLACED THE LAMP AND OPS CHECKED NORMAL IAW MM 33-51-06-2-1. ACFT OK FOR SERVICE.
- [SDR FDEA201611194123](https://openairdocs.org/sdr/FDEA201611194123.md): Light · inoperative · Nov 19, 2016 · N959FD · Boeing 757236 · Emergency Lighting
  > RT FWD EMERGENCY SLIDE EVACUATION LIGHT INOP. PERFORMED EMERGENCY LIGHTS OPS CHECK IAW AMM.
- [SDR FDEA201604161234](https://openairdocs.org/sdr/FDEA201604161234.md): Cable · out of rig · Apr 16, 2016 · N959FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR FAILED DISARM CABLE CHECK. DIMENSIONS REQUIRED 1.6 INCHES, ACTUAL MEASUREMENT IS 1.3 INCHES. UNABLE TO ADJUST CABLE TO LIMITS. PERFORMED RIG ON DISARM CABLE. ALL ADJUSTMENTS & MEASUREMENTS ARE WITHIN LIMITS. ALL DOOR FUNCTIONS OPERATE NORMAL.
- [SDR FDEA201507032140](https://openairdocs.org/sdr/FDEA201507032140.md): Roller · failed · Jul 3, 2015 · N959FD · Boeing 757236 · Passenger/Crew Doors
  > ON TAXI OUT, LT FWD ENTRY DOOR LIGHT ILLUMINATED. INSTALLED A NEW UPPER LATCH CAM ROLLER. PERFORMED ADJUSTMENT TEST IAW MM 52-11-00-5. DOOR OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201502040439](https://openairdocs.org/sdr/FDEA201502040439.md): Handle · detached · Feb 4, 2015 · N959FD · Boeing 757236 · Landing Gear Brake System
  > PARKING BRAKE HANDLE CAME OFF WHEN SETTING BRAKES AFTER PUSH BACK. R & R PARKING BRAKE LEVER IAW AMM 32-44-01-4. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
- [SDR FDEA201410203316](https://openairdocs.org/sdr/FDEA201410203316.md): Battery · discharged · Oct 20, 2014 · N959FD · Boeing 757236 · Emergency Lighting
  > RIGHT SIDE EMER EXIT SIGN STAYS ON 20 SECS & THEN GOES OUT DURING TEST, LT SIDE NORMAL. R & R RT EMER EXIT POWER SUPPLY BATTERY & PERFORM OPERATIONAL TEST IAW AMM 33-51-07-2 & 33-51-00-5. LIGHTS CHECKED NORMAL, OK FOR SERVICE.
- [SDR FDEA201408272336](https://openairdocs.org/sdr/FDEA201408272336.md): Light · inoperative · Aug 27, 2014 · N959FD · Boeing 757236 · Emergency Lighting
  > R1 OUTSIDE EMER EXIT LIGHT INOPERATIVE. RELAMPED IAW AMM. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201307111540](https://openairdocs.org/sdr/FDEA201307111540.md): Unknown · odor · Jul 11, 2013 · N959FD · Boeing 757236 · Air Distribution System
  > DURING CRUISE, CLIMBED FROM FL 370 TO FL 390 IN AREA OF HEAVY STATIC ELEC AND ST ELMO`S FIRE BOTH PILOTS SMELLED STRONG ODOR, LIKE BURNED RUBBER. ODOR DISSIPATED WITHIN FIVE MINUTES. ON DESCENT, PASSING 15000FT ODOR RETURNED. DONNED 02 MASKS, RAN "SMOKE FI
- [SDR FDEA201212104272](https://openairdocs.org/sdr/FDEA201212104272.md): Girt Bar · dirty · Dec 10, 2012 · N959FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR SLIDE ARMED KNOB IS NOT FUCTIONING CORRECTLY. REMOVED DEBRIS FROM FLOOR GIRT BAR ATTACHMENTS IAW MM RF 25-66-10-2. PERFORMED INSPECTION CHECK IAW MM REF. 52-11-00-6. OK FOR SERVICE. FINAL CLOSED.
- [SDR FDEA201211244151](https://openairdocs.org/sdr/FDEA201211244151.md): Bulb · inoperative · Nov 24, 2012 · N959FD · Boeing 757236 · Emergency Lighting
  > EXTERIOR EVACUATION SLIDE LIGHT FOR R1 DOOR INOP WHEN TESTED. R & R ESCAPE SLIDE EMERGENCY LIGHT BULB, OPS CHECK NORMAL, REF AMM 33-51-06-2-1 OK FOR SERVICE.
- [SDR FDEA201208153009](https://openairdocs.org/sdr/FDEA201208153009.md): Receptacle · dirty · Aug 15, 2012 · N959FD · Boeing 757200 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. CLEANED RECEPTACLE AND RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR FDEA201206122193](https://openairdocs.org/sdr/FDEA201206122193.md): Skin · dented · Jun 12, 2012 · N959FD · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN DENTED AT BS 680-700 BETWEEN S25-26 RT. REPAIRED IAW EA F-5330-161080, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201206082138](https://openairdocs.org/sdr/FDEA201206082138.md): Skin · damaged · Jun 8, 2012 · N959FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN DAMAGED AT BS 1440-1460 BETWEEN STR 19-20 RT. REPAIR CARRIED OUT ON BLENDED SKIN AT BS 1440-1460, STR 19R-20R, IAW EA F-5310-155896 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201206082140](https://openairdocs.org/sdr/FDEA201206082140.md): Skin · damaged · Jun 8, 2012 · N959FD · Boeing 757236 · Passenger/Crew Doors
  > CABIN, DURING REPLACEMENT OF DOOR R1 LOWER TORQUE TUBE BEARING, NOTICED TOOLING MARK IN DOOR SKIN AT AFT LOWER. REPAIRED IAW EA F-5210-155898, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N959FD/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 = 'N959FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N959FD/reports

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