# Service difficulty reports: N946FD

A list on [N946FD](https://openairdocs.org/aircraft/N946FD.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 4 · 175 reports

- [SDR FDEA202610191605](https://openairdocs.org/sdr/FDEA202610191605.md): Attach Angle · damaged · Oct 19, 2026 · N946FD · Boeing 757236 · Trailing Edge Flaps
  > R/H WING INBD T/E FLAP, OUTBD TRACK FAIRING 672HB ATTACH ANGLE HAS ELONGATED HOLES. PERFORMED REPAIR IAW B757-200 SRM 57-53-02-2R FIG 202 REPAIR 3 SHEET 1 AND 2. REMOVED AND REPLACED FITTINGS P/N 113N2304-10 AND 113N2306-1 IAW SRM 51-40-02. THIS CATAGORY B
- [SDR FDEA202610151596](https://openairdocs.org/sdr/FDEA202610151596.md): Panel · dented · Oct 15, 2026 · N946FD · Boeing 757236 · Vertical Stabilizer, Plate/Skin
  > DENT AT VERTICAL STAB LH SIDE COMPOSITE PANEL FWD OF FRONT SPAR LWR AREA BETWEEN FSS 119 TO FSS 170. REPAIRED DENT AT VERTICAL LH SIDE TORQUE BOX COMPOSITE PANEL LWR AREA BETWEEN FSS 119 TO FSS 170 IAW B757-200 SRM 55-30-01-2R, REPAIR 5 FIG 201, SHEET 1 M
- [SDR FDEA202610061485](https://openairdocs.org/sdr/FDEA202610061485.md): Floorbeam · corroded · Oct 6, 2026 · N946FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR STRUCTURE CROSSBEAM HAS CORROSION AT THE UPPER FWD FLANGE AT BS 377 FROM LBL 26 TO LBL 56. REPAIRED CROSSBEAM PER EA F-5310-T0388790 P1, FUSELAGE - MAIN FRAME - CORROSION REPAIR, SECTION 41 MAIN DECK FLOOR BEAM, UPPER FORWARD FLANGE STA 377
- [SDR FDEA202609301456](https://openairdocs.org/sdr/FDEA202609301456.md): Strap · corroded · Sep 30, 2026 · N946FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > APU AIR INLET DOOR ASSY ATTACHMENT CUT OUT FWD FRAME CORRODED STA 1787. REMOVED AND REPLACED THE ANGLE. PERFORMED REPAIR ON INITIAL MIDDLE STRAP BS 1825 BETWEEN STR 3R - 6R IAW SRM 53-80-15. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-80-15-1A. MAJOR REPAI
- [SDR FDEA202609291452](https://openairdocs.org/sdr/FDEA202609291452.md): Seat Track · corroded · Sep 29, 2026 · N946FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL SPOTS OF CORROSION AT CABIN SEAT TRACK FLANGE BS 900 TO 1020, RBL 58. ACCOMPLISHED SEAT TRACK REPAIR OPTION 1 PER SRM 53-00-52-2R FIG 201. MAJOR REPAIR.
- [SDR FDEA202609231420](https://openairdocs.org/sdr/FDEA202609231420.md): Wedge · dented · Sep 23, 2026 · N946FD · Boeing 757236 · Leading Edge Devices
  > NUMBER 7 SLAT UPPER SURFACE T/E WEDGE HAD A DENT AT OSS 390 AND 6" FWD OF AFT END. REPAIRED NR 7 SLAT UPPER SURFACE TRAILING EDGE WEDGE DENT IAW SRM 51-70-10-2R, FIG 201, SHEET 3. MAJOR REPAIR.
- [SDR FDEA202609231418](https://openairdocs.org/sdr/FDEA202609231418.md): Crease Beam · corroded · Sep 23, 2026 · N946FD · Boeing 757236 · Fuselage Main, Structure
  > MAIN CABIN RT BS 610, RBL 62., FLOOR SUPPORT FOR PANEL 232MIF HAD SURFACE CORROSION AROUND SCREW HOLES. REPAIRED MAIN DECK FLOOR STRUCTURE CREASE BEAM INBD CHORD AT RBL 62. BETWEEN BS 540 TO BS 660 IAW SRM 53-00-13-2R, FIG 201, SHEET 1 - 3.
- [SDR FDEA202604300522](https://openairdocs.org/sdr/FDEA202604300522.md): Transition Panel · tripped · Apr 30, 2026 · N946FD · Boeing 757236 · Trailing Edge Flap Control System
  > GOT TE FLAP DISAGREE WHEN MOVING THE FLAP HANDLE FROM 20 TO 25. RAN QRH, AND LANDED WITH ALTERNATE FLAPS 20. EMERGENCY DECLARED RESET LH OUTBOARD TRANSMISSION IAW 27-51-808
- [SDR FDEA202505280813](https://openairdocs.org/sdr/FDEA202505280813.md): Warning Message · illuminated · May 28, 2025 · N946FD · Boeing 757236 · Landing Gear Position and Warning
  > ON DEPARTURE FROM KSYR, UPON RETRACTING THE GEAR WE RECEIVED A GEAR DISAGREE EICAS WITH AN AMBER GEAR LIGHT ON THE RIGHT QUADRANT OF THE GEAR INDICATION LIGHTS. WE TESTED THE LIGHTS AND THE RIGHT MAIN GEAR LIGHT DID NOT TEST. RETURNED TO KSYR. UPON LOWERI
- [SDR FDEA202306231097](https://openairdocs.org/sdr/FDEA202306231097.md): Unknown · unknown · Jun 23, 2023 · N946FD · Boeing 757200 · Landing Gear System Wiring
  > MDIS 946 32-97 2317 23JUN23 EWR FACT U WIRE W2648-4502G/W BURNED AND DAMAGED UNDER MAIN DECK AT APPROX. STA 1620. FACT 25JUN23 02:58 EWR U EA: F-3246-T0374998A WIRES WERE CAPPED AND STOWED AND SECURED AS PER ABOVE E.A. WIRES WE
- [SDR FDEA202306231096](https://openairdocs.org/sdr/FDEA202306231096.md): Unknown · unknown · Jun 23, 2023 · N946FD · Boeing 757200 · Landing Gear System Wiring
  > MDIS 946 32-97 2316 23JUN23 EWR FACT U WIRE W2648-4501G/W-20 BURNED AND DAMAGED UNDER MAIN DECK AT APPROX. STA 1620. FACT 25JUN23 03:00 EWR U EA: F-3246-T0374998A CAPPED AND STOWED AS PER ABOVE E.A. CAPPED AND STOWED AS PER ABOVE E.A.
- [SDR FDEA202306231095](https://openairdocs.org/sdr/FDEA202306231095.md): Unknown · unknown · Jun 23, 2023 · N946FD · Boeing 757200 · Landing Gear System Wiring
  > MDIS 946 32-97 2314 23JUN23 EWR FACT U WIRE W2648-2501R/B/Z-24 BURNED AND DAMAGED UNDER MAIN DECK AT APPROX. STA 1620. FACT 25JUN23 03:02 EWR U EA: F-3246-T0374998A CAPPED AND STOWED AS PER PART 1 OF ABOVE EA. TERMINATED ANTI SKID WIRES
- [SDR FDEA202306231094](https://openairdocs.org/sdr/FDEA202306231094.md): Unknown · unknown · Jun 23, 2023 · N946FD · Boeing 757200 · Landing Gear System Wiring
  > WIRE W2648-2502R/B/Z-24 BURNED AND DAMAGED UNDER MAIN DECK AT APPROX. STA 1620. FACT 25JUN23 03:04 EWR U EA: F-3246-T0374998A CAPPED AND STOWED AS PER ABOVE PART 1 OF ABOVE EA 53. TERMINATED ANTI SKID WIRES W2648-2501R, W2648-2501B, W2648-2502R, W264
- [SDR FDEA202306030986](https://openairdocs.org/sdr/FDEA202306030986.md): Lamp · inoperative · Jun 3, 2023 · N946FD · Boeing 757200 · Emergency Equipment
  > L1 DOOR "SLIDE" LIGHT INOP. AMM: 33-16-02-2 RELAMPED PER B757 AMM 33-16-02-2 WITH NO HELP MEL 03JUN23 00:45 FSD U RELEASED FOR SERVICE PER MEL: 25-66-05-A CATEGORY: C EXPIRATION: 13JUN23 "MEL 25-66-05-A: _L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT
- [SDR FDEA202212182946](https://openairdocs.org/sdr/FDEA202212182946.md): Light · faulted · Dec 18, 2022 · N946FD · Boeing 757236 · Landing Gear Position and Warning
  > ON INITIAL APPROACH WE SELECTED THE GEAR HANDLE TO THE DOWN POSITION TO CONFIGURE FOR LANDING. RECEIVED NOSE & RT MLG INDICATION WITH NO LT MLG LIGHT. THERE WAS NO ASSOCIATED EICAS MESSAGE WITH THE INDICATION. PRESSED LIGHT TEST BUTTON & TAPPED LIGHT, STILL
- [SDR FDEA202211212823](https://openairdocs.org/sdr/FDEA202211212823.md): Drag Fitting · corroded · Nov 21, 2022 · N946FD · Boeing 757236 · Wing, Attach Fittings
  > LH WING DRAG FITTING HOLE 9 HAS CORROSION AND A CRACK INDICATION IN THE FITTING LAYER AT 3 O'CLOCK WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS THIS EA DEVIATES FROM EO F-5730-E0340076. COMPLIED WITH EA F-5730-T037
- [SDR FDEA202211152794](https://openairdocs.org/sdr/FDEA202211152794.md): None · none · Nov 15, 2022 · N946FD · Boeing 757258 · Standard Practices/Structures
  > DURING ACCOMPLISHMENT OF EO F-5310-E0347443 AN EXISTING REPAIR WAS FOUND AT STA 1360 INBD OF S26L THAT REQUIRES FURTHER INSPECTION PER EO. COMPLIED WITH EA # F-5310-145326D P6, FUSELAGE-MAINFRAME-LOWER CARGO FRAME REPAIRS AT BS 1320, S26L, BS 1340, S-26L,
- [SDR FDEA202210192612](https://openairdocs.org/sdr/FDEA202210192612.md): Gust Lock · broken · Oct 19, 2022 · N946FD · Boeing 757200 · Passenger/Crew Doors
  > L1 GUST LOCK APPEARS TO BE BROKEN. DOOR STILL OPENS AND CLOSES. REMOVED L1 DOOR BROKEN GUST LOCK, REPLACED IAW AMM 52-11-08-8. OPS CHECKS GOOD.
- [SDR FDEA202205221270](https://openairdocs.org/sdr/FDEA202205221270.md): Warning Message · illuminated · May 22, 2022 · N946FD · Boeing 757200 · Trailing Edge Flap Control System
  > DURING FINAL APPROACH WHILE SELECTING GEAR DOWN FLAPS 20, GOT TE FLAP DISAGREE EICAS AND TRAILING EDGE LIGHT. RAN QRH, WAS DIRECTED TO TRAILING EDGE FLAP ASYMMETRY QRH. LANDED PER QRH PROCEDURES. PERFORMED FSEU BITE PROCEDURE ON ALL 3 FSEU'S REF FIM 27-
- [SDR FDEA202108172027](https://openairdocs.org/sdr/FDEA202108172027.md): Ball Screw · damaged · Aug 17, 2021 · N946FD · Boeing 757236 · Trailing Edge Flap Control System
  > CONFIGURING AT DESTINATION, MOVING FLAPS LEVER FROM 15 TO 20, GOT A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE, ALTITUDE 2,500FT, SPEED 170KTS. DISCONTINUED APPROACH, RAN QRH, AND LANDED FLAPS 20 UNEVENTFULLY. EMERGENCY DECLARED. R & R LT INBOARD TRAILING E
- [SDR FDEA202108132009](https://openairdocs.org/sdr/FDEA202108132009.md): Warning Message · false activation · Aug 13, 2021 · N946FD · Boeing 757236 · Trailing Edge Flap Control System
  > DURING CONFIGURATION, AFTER MOVING FLAP LEVER TO 25, GOT TE FLAP DISAGREE EICAS MESSAGE. DISCON APPROACH, RAN QRH, & LANDED UNEVENTFUL. EMERGENCY DECLARED. DRAINED & SERVICED LT- I/B FLAP I/B TE FLAP TRANSMISSION IAW MM 12-13-06-3. RAN FLAPS & GOT FLAP IS
- [SDR FDEA202106241587](https://openairdocs.org/sdr/FDEA202106241587.md): Gcu · failed · Jun 24, 2021 · N946FD · Boeing 757236 · AC Generator-Alternator
  > AFTER MEL APU ELECTRICAL, TAXI OUT AND TAKEOFF NORMAL. JUST AFTER LIFTOFF MULTIPLE ELECTRICAL AND AVIONICS FAILURES. CAPTAIN AIRSPEED INDICATED 400 KNOTS ALTIMETER WENT TO 40,000 FEET ALL CAPTAIN FLIGHT INSTRUMENTS STOPPED WORKING. F/O AIRSPEED ALSO INDI
- [SDR FDEA202012103100](https://openairdocs.org/sdr/FDEA202012103100.md): Skin · corroded · Dec 10, 2020 · N946FD · Boeing 757236 · Leading Edge Devices
  > LT WING NR 4 SLAT LEADING EDGE SKIN CORRODED AT OSS 404.8. REPAIRED THE LT WING NR 4 SLAT CORRODED LEADING EDGE SKIN AT OSS 404.8, PER B757 SRM 57-43-01-2R REPAIR 6. RSC TRACKING EA: F-5750-T0358504 WAS ISSUED AND COMPLETED. TITLE: WING-FLIGHT SURFACES-NR
- [SDR FDEA201909102198](https://openairdocs.org/sdr/FDEA201909102198.md): Control Panel · burned · Sep 10, 2019 · N946FD · Boeing 757236 · DME/TACAN System
  > IN CRUISE, FIRST OFFICER SMELLED AND SAW SMOKE COMING OUT OF REAR OF NUMBER 2 VOR/DME BOX. THE AUTO/MAN SWITCH HAD BEEN SELECTED A FEW MINUTES PRIOR. DIVERT TO RPLC. REMOVED AND REPLACED RT VOR/DME PANEL PER MM 34-51-02-2-0 AND OPS TEST PER MM 34-51-00-5-99, P
- [SDR FDEA201811193291](https://openairdocs.org/sdr/FDEA201811193291.md): Stringer · corroded · Nov 19, 2018 · N946FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > CHECK FOUND FUSELAGE STRINGER CORRODED AT STA 740-STA 760 S22L. MADE THE REPAIR PARTS PER SRM 53-00-03 REPAIR 2 FIG 201, WET INSTALLED THE REPAIR PARTS PER SRM51-40-02. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201811193290](https://openairdocs.org/sdr/FDEA201811193290.md): Stringer · corroded · Nov 19, 2018 · N946FD · Boeing 757236 · Fuselage Main, Longeron/Stringer
  > CHECK FOUND FUSELAGE STRINGER CORRODED AT STA 740-STA 760 S25L. MADE THE REPAIR PARTS PER SRM 53-00-03 REPAIR 2 FIG 201, WET INSTALLED THE REPAIR PARTS PER SRM51-40-02. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201804020825](https://openairdocs.org/sdr/FDEA201804020825.md): Battery Pack · inoperative · Apr 2, 2018 · N946FD · Boeing 757236 · Emergency Lighting
  > FOUND THE LT ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. R & R THE BATTERY PACK IN THE POWER SUPPLY UNIT IAW AMM 33-51-07-2, CHECKED NORMAL IAW AMM 33-51-00-5. ACFT OK OR SERVICE.
- [SDR FDEA201802130375](https://openairdocs.org/sdr/FDEA201802130375.md): Proximity Sensor · out of tolerance · Feb 13, 2018 · N946FD · Boeing 757236 · Landing Gear Position and Warning
  > DURING DEPARTURE, SPEED TAPE ZIPPER WOULD NOT RETRACT ABOVE 267 KNOTS. BOTH CAPTAIN`S AND FIRST OFFICER`S ZIPPERS WERE FROZEN. NO EICAS MESSAGES, NO FLIGHT CONTROL PROBLEMS. PERFORMED A PSEU BITE IAW FIM 32-09, FAULT TREE 805, FAULT CODE 003 DISPLAYED
- [SDR FDEA201802080329](https://openairdocs.org/sdr/FDEA201802080329.md): Pump · leaking · Feb 8, 2018 · N946FD · Boeing 757236 · Hydraulic System, Main
  > LEFT HYD QTY LOW EICAS MESSAGE, FOLLOWED BY LT HYD SYS PRESSURE LOW DURING CRUISE FLIGHT, APPROX ONE HOUR PRIOR TO LANDING. AP FOLLOWING QRH PROCEDURES TURNED OFF THE ENGINE HYD PUMP AND LT ELEC HYD PUMP.HYD QTY INDICATED 0.04 ON STATUS PAGE. FOUND HYD
- [SDR FDEA201711213289](https://openairdocs.org/sdr/FDEA201711213289.md): Battery · discharged · Nov 21, 2017 · N946FD · Boeing 757236 · Emergency Lighting
  > DURING SERVICE CHECK FOUND EMERGENCY LIGHT INOP. PER AMM 33-51-07-2, REMOVED AND REPLACED THE BATTERY AND EMERGENCY LIGHT. OPS TEST NORMAL. A/C OK FOR SVC.
- [SDR FDEA201704151201](https://openairdocs.org/sdr/FDEA201704151201.md): Latch · debonded · Apr 15, 2017 · N946FD · Boeing 757236 · Emergency Equipment
  > FOUND L1 DOOR SLIDE COVER AFT LATCH BROKEN. LATCH DEBOND FROM COVER ASSY, NEED COMPOUND TO REPAIR. CANNED COVER ASSY AND INSTALLED AS PER AMM 25-66-01-4, ALL CHECK NORMAL.
- [SDR FDEA201701240245](https://openairdocs.org/sdr/FDEA201701240245.md): Gcu · faulty · Jan 24, 2017 · N946FD · Boeing 757236 · AC Regulator
  > REPEAT WRITE-UP L GEN OFF EICAS ON APPROACH. RUN CHECK LIST AND RESET THE L GEN CONT SWITCH AND GENERATOR CAME BACK ON LINE. DECLARED EMERGENCY. ALL INSPECTIONS SATISFACTORY. RECONNECTED L IDG PER AMM 24-11-01-6. OPENED & CLOSED L ENGINE FAN COWLS PER AMM 71-1
- [SDR FDEA201611053850](https://openairdocs.org/sdr/FDEA201611053850.md): Deck Plate · corroded · Nov 5, 2016 · N946FD · Boeing 757236 · Fuselage Floor Panel
  > MAIN CABIN DECK PLATE CORRODED AT BS 1710, RBL 53. REPAIRED IAW EA F-5310-T0329486 P1.
- [SDR FDEA201611053849](https://openairdocs.org/sdr/FDEA201611053849.md): Deck Plate · corroded · Nov 5, 2016 · N946FD · Boeing 757236 · Fuselage Floor Panel
  > CABIN DECK PLATE IS CORRODED FROM BS 1681 - 1720 RBL 5.. REPAIRED IAW EA F-5310-T0329486 P1.
- [SDR FDEA201611053831](https://openairdocs.org/sdr/FDEA201611053831.md): Shear Web · corroded · Nov 5, 2016 · N946FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CABIN SHEAR WEB IS CORRODED FROM BS 1681 - 1720, RBL 28.5. REMOVED THE CORROSION IAW SRM 51-10-02-OG. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAIL IV. INSTALLED A REPAIR IAW SRM 53-60-51-2R, FIG 201, DETAIL I.
- [SDR FDEA201611053830](https://openairdocs.org/sdr/FDEA201611053830.md): Shear Web · corroded · Nov 5, 2016 · N946FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CABIN SHEAR WEB IS CORRODED FROM BS 1681 - 1720, RBL 14. REMOVED THE CORROSION IAW SRM 51-10-02-OG, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A,FIG 101,DETAIL IV. INSTALLED A REPAIR IAW SRM 53-60-51-2R, FIG 201, DETAIL I.
- [SDR FDEA201610283738](https://openairdocs.org/sdr/FDEA201610283738.md): Structure · cracked · Oct 28, 2016 · N946FD · Boeing 757236 · Passenger/Crew Doors
  > R-2 DOOR UPPER HINGE CUTOUT IS CRACKED. INSTALLED A REPAIR ANGLE IAW B 757 SRM 52-10-02-2R FIG 201. COMPLIED CABIN PRESSURE CHECK WITH NORMAL RESULT IAW AMM 05-51-24-2.
- [SDR FDEA201610263701](https://openairdocs.org/sdr/FDEA201610263701.md): Floorbeam · cracked · Oct 26, 2016 · N946FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CARGO BAY FLOORBEAM CRACKED AT BS 580 LBL 44 - 46.
- [SDR FDEA201608122884](https://openairdocs.org/sdr/FDEA201608122884.md): Spring · broken · Aug 12, 2016 · N946FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR EXTERIOR HANDLE LATCH HOOK SPRING IS BROKEN.
- [SDR FDEA201608042819](https://openairdocs.org/sdr/FDEA201608042819.md): Fire Loop · false activation · Aug 4, 2016 · N946FD · Boeing 757236 · Fire Detection
  > DURING TAKEOFF AND ACCELERATING THROTTLES, NR 2 ENGINE FIRE BELL AND MASTER WARNING. DURING THROTTLE REDUCTION, ALL FIRE INDICATIONS EXTINGUISHED. REJECTED TAKE OFF AT APPROX 40 KNOTS. R & R NR 3 LOOP IAW AMM 26-11-01-04.
- [SDR FDEA201510283394](https://openairdocs.org/sdr/FDEA201510283394.md): Engine · malfunctioned · Oct 28, 2015 · N946FD · Boeing 757236 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, AFTER 1000' AGL, CLIMB MODE, LT ENG EPR SURGED +/- 0.10% TOTAL OF 0.20 EPR, N1 BOUNCING +/- 10%. QRH ENG LIMIT OR SURGE OR STALL CHECKLIST. AT 50% N1 ENG STABILIZED. INSPECTED PITOT HEADS ON LT SIDE, FOUND TWO HEADS MISSING. INSPECTED RT S
- [SDR FDEA201410313441](https://openairdocs.org/sdr/FDEA201410313441.md): Frame · gouged · Oct 31, 2014 · N946FD · Boeing 757236 · Fuselage Main, Frame
  > FORWARD ACCESSORY BAY FRAME AT BS 231.25 STRINGER 30 HAS A GOUGE IN UPPER FLANGE OF FRAME. REPAIRED IAW EA F-5310-T0312860 REV PS P1.
- [SDR FDEA201408172192](https://openairdocs.org/sdr/FDEA201408172192.md): Liner · out of position · Aug 17, 2014 · N946FD · Boeing 757236 · Passenger/Crew Doors
  > R1 DOOR SLIDE PACK HITS AFT SIDE OF DOOR CUT OUT WHILE BEING CLOSED. REF SNRDS 00005 & 00012 OF HANGAR WORK ORDER 61879. R & R R1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. ORIGINAL DISCREPANCY STILL EXISTS. DOOR SLIDE HAS BEEN REPLACED & DOOR WILL BE CHECKED
- [SDR FDEA201305090955](https://openairdocs.org/sdr/FDEA201305090955.md): Switch · inoperative · May 9, 2013 · N946FD · Boeing 757236 · Door Warning System
  > EXCESSIVE NOISE DURING TAKEOFF. SUSPECTED AN OPEN DOOR BUT NO INDICATIONS ON EICAS OR OVERHEAD PANEL OF OPEN DOOR. CABIN ALTITUDE KEPT CLIMBING, RETURNED TO DEPARTURE. FORWARD ACCESS DOOR WAS OPEN. OPEN AND CLOSED FORWARD ACCESS DOOR AND DID NOT GET AN IN
- [SDR FDEA201211093929](https://openairdocs.org/sdr/FDEA201211093929.md): Bulb · inoperative · Nov 9, 2012 · N946FD · Boeing 757236 · Escape Slide
  > RIGHT SLIDE LIGHT BULB INOPERATIVE. LAMPED R1 SLIDE LIGHT IAW MM 33-51-06-2-1. OPS CHECKED NORMAL. AC OK TO CONTINUE.
- [SDR FDEA201209123304](https://openairdocs.org/sdr/FDEA201209123304.md): Wire · damaged · Sep 12, 2012 · N946FD · Boeing 757236 · Hydraulic Power System Wiring
  > DURING SERVICE CHECK, FOUND HYD PTU CONTROLLER CIRCUIT BREAKER TRIPPED. RESET, RAN HYD SYSTEM, CIRCUIT BREAKER TRIPPED AGAIN. AFTER VISUAL INSPECTION, FOUND WIRE W5100-0038-20 WITH DAMAGED INSULATION. SECURED CONNECTOR D42282J AND CHECKED FOR 28VDC AT PIN 6 O
- [SDR FDEA201207032450](https://openairdocs.org/sdr/FDEA201207032450.md): Battery · inoperative · Jul 3, 2012 · N946FD · Boeing 757236 · Emergency Lighting
  > LEFT EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERY, OPS CHECKED NORMAL REF AMM 33-51-07-2-2.
- [SDR FDEA201205241955](https://openairdocs.org/sdr/FDEA201205241955.md): Bolt · loose · May 24, 2012 · N946FD · Boeing 757236 · Flight Compartment Windows
  > F/O'S WINDOW MADE A HIGH-PITCHED SQUEALING NOISE ABOUT AN HOUR INTO FLIGHT. VERY LOUD NOISE APPEARS TO HAVE MOVED TO THE BOTTOM LT CORNER. VISUALLY CHECKED WINDOW SEALS AND PRESSURIZED ACFT AND LEAK CHECKED F/O'S NR 2 WINDOW, FOUND LEAKS AT FORWARD LOWER AND
- [SDR FDEA201203271153](https://openairdocs.org/sdr/FDEA201203271153.md): Connector · loose · Mar 27, 2012 · N946FD · Boeing 757236 · Flight Control System Wiring
  > ON INITIATION OF DESCENT, A YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH T/E FLAP ASYM AND T/E CAUTION LIGHTS ON THE EICAS AND FOWARD PANEL. THE FLAP HANDLE WAS UP AND FLAP INDICATION GAUGE SHOWED UP AS WELL. THERE WAS NO ROLL TENDENCY. TROUBLESHOOTING FOUND
- [SDR FDEA201110264659](https://openairdocs.org/sdr/FDEA201110264659.md): Switch · broken · Oct 26, 2011 · N946FD · Boeing 757236 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS SWITCH IS BROKEN. EMERGENCY LIGHT GUARD IS LOOSE. SWITCH AND LIGHTS OPERATES NORMALY. REPLACED GUARD IAW CMM 33-51-03 OK FRO SERVICE. TERMINATING ACTION ACCOMPLISHED FOR MM-33-51-08-0.

Next page: https://openairdocs.org/aircraft/N946FD/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 = 'N946FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N946FD/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.