# Service difficulty reports: N953FD A list on [N953FD](https://openairdocs.org/aircraft/N953FD.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 2 · 72 reports - [SDR FDEA202308241484](https://openairdocs.org/sdr/FDEA202308241484.md): Indicator · failed · Aug 24, 2023 · N953FD · Boeing 757200 · Hydraulic Power System > PDIS 953 29-02 8832 23AUG23 ROA OPEN U FIRST EICAS MESSAGE WAS L HYD QTY. RAN QRH 13.1.2. A FEW MOMENTS LATER EICAS MESSAGE L HYD SYS PRESS. RAN QRH 13.1.5. ***EMERGENCY DECLARED*** ENT BY:3692956 RPT BY:3692956 SHGN 23AUG23 15:32 ROA U - [SDR FDEA202302040202](https://openairdocs.org/sdr/FDEA202302040202.md): Gust Lock · failed · Feb 4, 2023 · N953FD · Boeing 757200 · Passenger/Crew Doors > GUST LOCK COLLAR BROKEN AT L1 DOOR. AMM: 52-11-08-8 COMPLETED INSTALLATION OF GUST LOCK COLLAR IAW B757 52-11-08-8. BROKEN C - [SDR FDEA202209132316](https://openairdocs.org/sdr/FDEA202209132316.md): Drag Fitting · corroded · Sep 13, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE 2 PYLON HOLE #14HAS REJECTABLE INDICATION DUE TO CORROSION IN SKIN AND A CRACK INDICATION AT 2 O'CLOCK IN THE DRAG FITTING. ACCOMPLISHED EA F-5730-T0370299 PT1 WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CRACKS/CORROSION REWORK, MAJO - [SDR FDEA202209122315](https://openairdocs.org/sdr/FDEA202209122315.md): Frame · cracked · Sep 12, 2022 · N953FD · Boeing 757236 · Fuselage Main, Frame > BODY STATION 1640 S-14R HAS A REJECTABLE CRACK INDICATION IN TOP I/B HOLE FWD LAYER FUSELAGE-MAINFRAME-INSPECTION OF BODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14R-BOEING ALERT SERVICE BULLETIN 757-53A0112-UPPER INBOARD HOLE-DAMAGE REPAIR. ACCOMPLI - [SDR FDEA202209112298](https://openairdocs.org/sdr/FDEA202209112298.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE #1 PYLON HOLE #17 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #17, MAJOR REPAIR - [SDR FDEA202209112297](https://openairdocs.org/sdr/FDEA202209112297.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE #1 PYLON HOLE #13 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #13, MAJOR REPAIR - [SDR FDEA202209112296](https://openairdocs.org/sdr/FDEA202209112296.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE #1 PYLON HOLE #9 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS- LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #9, MAJOR REPAIR - [SDR FDEA202209112295](https://openairdocs.org/sdr/FDEA202209112295.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE #1 PYLON HOLE #4 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #4, MAJOR REPAIR - [SDR FDEA202209112294](https://openairdocs.org/sdr/FDEA202209112294.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE #1 PYLON HOLE #3 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #3, MAJOR REPAIR - [SDR FDEA202209112293](https://openairdocs.org/sdr/FDEA202209112293.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Wing, Plate/Skin > LH WING #1 ENGINE DRAG FITTING HOLE #16 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #16, MAJOR REPAIR - [SDR FDEA202209112292](https://openairdocs.org/sdr/FDEA202209112292.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > LH WING #1 ENGINE DRAG FITTING HOLE #14 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #14, MAJOR REPAIR - [SDR FDEA202209112291](https://openairdocs.org/sdr/FDEA202209112291.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > LH WING #1 ENGINE DRAG FITTING HOLE #12 HAS REJECTABLE INDICATIONS DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT.1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #12, MAJOR REPAIR - [SDR FDEA202209112290](https://openairdocs.org/sdr/FDEA202209112290.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Wing, Plate/Skin > LH WING #1 ENGINE DRAG FITTING HOLE #11 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #11, MAJOR REPAIR - [SDR FDEA202209112288](https://openairdocs.org/sdr/FDEA202209112288.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > LH WING #1 ENGINE DRAG FITTING HOLE #7 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE COROSION INDICATIONS REPAIR ON HOLE #7, MAJOR REPAIR - [SDR FDEA202209112287](https://openairdocs.org/sdr/FDEA202209112287.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > LH WING #1 ENGINE DRAG FITTING HOLE #6 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1 WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #6, MAJOR REPAIR - [SDR FDEA202209112286](https://openairdocs.org/sdr/FDEA202209112286.md): Drag Fitting · corroded · Sep 11, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > LH WING #1 ENGINE DRAG FITTING HOLE #1 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1 WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #1, MAJOR REPAIR. - [SDR FDEA202209092268](https://openairdocs.org/sdr/FDEA202209092268.md): Drag Fitting · corroded · Sep 9, 2022 · N953FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings > ENGINE 2 PYLON HOLE #8 HAS REJECTABLE INDICATION DUE TO CORROSION IN SKIN AND DRAG FITTING. ACCOMPLISHED EA F-5730-T0370299 PT1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN AT DRAG FITTING, CRACKS / CORROSION REWORK. MAJOR REPAIR - [SDR FDEA202204060875](https://openairdocs.org/sdr/FDEA202204060875.md): None · none · Apr 6, 2022 · N953FD · Boeing 757 · Passenger/Crew Doors > MDIS 953 52-10 7823 06APR22 BWI OPEN U AFTER RAMP LOADED AIRCRAFT, FOUND L1 DOOR GUST LOCK BROKEN. REMOVED BROKEN GUST LOCK FRAGMENTS TO ALLOW DOOR TO BE OPENED AND CLOSED WITH NO HOLD OPEN LOCKING ACTION. FACT 08APR22 14:51 DTW - [SDR FDEA202201260140](https://openairdocs.org/sdr/FDEA202201260140.md): Hose · failed · Jan 26, 2022 · N953FD · Boeing 757200 · Hydraulic Power System > PDIS 953 29-02 7695 26JAN22 BHM FACT U UPON LOWERING LANDING GEAR FOR LANDING, LEFT HYDRAULIC QUANTITY WENT TO.14 AND THE PRESSURE TO 0 PSI. PART 26JAN22 04:44 MC1 U IDENTIFIED PARTS MLG DOWNLOCK ACTUATOR MPN: 271N6119-1 CPN: - [SDR FDEA202109252406](https://openairdocs.org/sdr/FDEA202109252406.md): Lock · sheared · Sep 25, 2021 · N953FD · Boeing 757236 · Emergency Equipment > AT A/C BLOCK-IN, WHEN L1 DOOR WAS OPENED FOUND L1 DOOR, PROXIMITY ACTUATOR FOR S10214, DETATCHED FROM GIRT BAR SLIDER (RIVETS SHEARED). COMPLIED WITH PART 2 OF E.A. F-2560-T0364440. REMOVED AND REPLACED L1 DOOR GIRT BAR - [SDR FDEA202108242078](https://openairdocs.org/sdr/FDEA202108242078.md): Engine · failed · Aug 24, 2021 · N953FD · Boeing 757236 · Engine (Turbine/Turboprop) > CLIMBING THROUGH 1000 AGL, VIOLENT SEIZURES FROM RIGHT ENGINE AND EGT REACHED 916. COMPLIED WITH QRC AND QRH. NO EMERGENCY DECLARED. INSTALLED A SERVICABLE #2 ENGINE IAW W/C 7180260-02-02. PERFORMED IDG DISCONNECT, OPS CHECKED PER W/C 2400400-02-01, AND C - [SDR FDEA202008121868](https://openairdocs.org/sdr/FDEA202008121868.md): Floorbeam · corroded · Aug 12, 2020 · N953FD · Boeing 757236 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM @ MAIN CABIN FWD WET AREA BS 365.25 BETWEEN RBL 24 AND RBL 57. REMOVED CORROSION ON FLOOR BEAM AT MAIN CABIN FWD WET AREA STA 365.25 BETWEEN RBL 24 TO RBL 57 IAW B757 SRM 51-10-02-0G. EVALUATED DAMAGED AREA AT STA 365, RBL 41 TO R - [SDR FDEA202008121867](https://openairdocs.org/sdr/FDEA202008121867.md): Floorbeam · corroded · Aug 12, 2020 · N953FD · Boeing 757236 · Fuselage Main, Floor Beam > MAIN DECK BS 1661 BL 0 FLOORBEAM TEE FITTING CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA ORIG. MAT.=.125", REM. MAT.=.106", MAT. LOSS=.019" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAIL VI. FABRICATED AND IN - [SDR FDEA2020081811864](https://openairdocs.org/sdr/FDEA2020081811864.md): Deck Plate · corroded · Aug 11, 2020 · N953FD · Boeing 757236 · Fuselage Miscellaneous Structure > MAIN DECK BETWEEN STA 1681 - 1720 BL 0 - LBL 58.22 WEB CORRODED FABRICATED AND INSTALLED 1EA REPAIR DOUBLER ON AFT MAIN DECK PLATE AT STA 1681 LBL 24.75 IAW B757 SRM 53-60-51-2R FIG 201 REPAIR 2 ALTERNATIVE I. REMOVED CORROSION ON DECK PLATE AT STA 1681-1 - [SDR FDEA2020081811863](https://openairdocs.org/sdr/FDEA2020081811863.md): Deck Plate · corroded · Aug 11, 2020 · N953FD · Boeing 757236 · Fuselage Miscellaneous Structure > MAIN DECK BETWEEN STA 1681 - 1720 BL 0 - RBL 58.22 WEB CORRODED FABRICATED AND INSTALLED 1EA REPAIR DOUBLER ON AFT MAIN DECK PLATE AT STA 1681, RBL 24.75 IAW B757 SRM 53-60-51-2R FIG 201 DETAIL I REPAIR 2 ALTERNATIVE I. REMOVED CORROSION ON DECK PLATE AT S - [SDR FDEA2020081211864](https://openairdocs.org/sdr/FDEA2020081211864.md): Web · corroded · Aug 11, 2020 · N953FD · Boeing 757236 · Fuselage Miscellaneous Structure > MAIN DECK BETWEEN STA 1681 - 1720 BLO - LBL 58.22 WEB CORRODED - [SDR FDEA2020081211863](https://openairdocs.org/sdr/FDEA2020081211863.md): Web · corroded · Aug 11, 2020 · N953FD · Boeing 757236 · Fuselage Miscellaneous Structure > MAIN DECK BETWEEN BS 1681 - 1720 BL 0 - RBL 58.22 WEB CORRODED. - [SDR FDEA201908151892](https://openairdocs.org/sdr/FDEA201908151892.md): Cargo Track · gouged · Aug 15, 2019 · N953FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings > MAIN CARGO TRACK GOUGED. PERFORMED A REPAIR TO THE CARGO TRACK IAW EA-T F-5321-348453 B P4. - [SDR FDEA201908151883](https://openairdocs.org/sdr/FDEA201908151883.md): Cargo Track · gouged · Aug 15, 2019 · N953FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings > MAIN CARGO TRACK BETWEEN BS 440-680 WAS FOUND GOUGED. REPLACED THE CARGO TRACK IAW EA - T F-5321-T0348233 A P4. - [SDR FDEA2019081541882](https://openairdocs.org/sdr/FDEA2019081541882.md): Cargo Track · gouged · Aug 14, 2019 · N953FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings > MAIN CARGO TRACK AT BS 440-680 FOUND GOUGED. REPAIRED IAW EA-T F-5321-T0348233, A P4. - [SDR FDEA2019081521850](https://openairdocs.org/sdr/FDEA2019081521850.md): Floorbeam · cracked · Aug 12, 2019 · N953FD · Boeing 757236 · Fuselage Main, Floor Beam > FLOORBEAM AT BS 580, LBL 45.5 WAS CRACKED. COMPLIED WITH EA F-5310-T0348746 P1. - [SDR FDEA201810182946](https://openairdocs.org/sdr/FDEA201810182946.md): Mechanism · obstructed · Oct 18, 2018 · N953FD · Boeing 757236 · Emergency Equipment > RIGHT CREW ENTRANCE DOOR DIFFICULT TO CLOSE AND ARM SLIDE. INSPECTED AREA OF DOOR MECHANISM AND FOUND DEBRIS IN THE TRACK OF THE FWD GIRT BAR LOCKING ATTACHMENT AREA. REMOVED AND CLEANED THE DEBRIS AND LUBRICATED. OPERATIONAL CHECKS NORMAL AND SLIDE ARMING NOR - [SDR FDEA201807221801](https://openairdocs.org/sdr/FDEA201807221801.md): Floorbeam · corroded · Jul 22, 2018 · N953FD · Boeing 757236 · Fuselage Main, Floor Beam > LT MAIN CABIN STA 377 FLOORBEAM UPPER CHORD HAS AREAS OF CORROSION ON FORWARD FLANGE UPPER AND LOWER SURFACES (EXFOLIATED LOWER AT NUTPLATES). COMPLIED WITH EA NR F-5310-T0341012 P1, FUSELAGE- MAINFRAME CORROSION ON STA 377.7 FLOORBEAM LBL 24.75 - LBL 58.22. - [SDR FDEA201807161718](https://openairdocs.org/sdr/FDEA201807161718.md): Seat Track · corroded · Jul 16, 2018 · N953FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK RT FLOORBEAM, RBL 14 SEAT TRACK STA 345 TO 9 G BULKHEAD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G, MEASURED 100% MATERIAL LOSS, OUT OF ALLOWABLE LIMITS IAW SRM 53-00-52-1A. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-08-0G, 51-40-02-0G & - [SDR FDEA201807161716](https://openairdocs.org/sdr/FDEA201807161716.md): Seat Track · corroded · Jul 16, 2018 · N953FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK LT FLOORBEAMS, LBL 7 SEAT TRACK HAS CORROSION FROM STA 345 TO STA 377. REMOVED CORROSION IAW SRM 53-00-52, 100% MATERIAL LOSS OUT OF ALLOWABLE LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-08-0G, 51-40-02-0G, 53-10-52-01 FIG 1 AND VA DWG 3470 - [SDR FDEA201703150919](https://openairdocs.org/sdr/FDEA201703150919.md): Control Rod · bent · Mar 15, 2017 · N953FD · Boeing 757236 · Passenger/Crew Doors > R1 DOOR SHOWS ARMED WHEN UNARMED. FOUND CONTROL ROD FOR THE SLIDE ARMING RETRACTABLE DOOR MECHANISM, BENT. REMOVED AND REPLACED THE CONTROL ROD. ADJUSTED THE CONTROL ROD AND PERFORMED A TEST OF THE SLIDE ARMING SYSTEM. COULD FIND NO OTHER DEFECTS. OK TO - [SDR FDEA201702070448](https://openairdocs.org/sdr/FDEA201702070448.md): Battery Pack · inoperative · Feb 7, 2017 · N953FD · Boeing 757236 · Emergency Lighting > DURING PRE FLIGHT CHECK, FOUND RT EMERGENCY EXIT LIGHT AND SLIDE LIGHT INOPERATIVE. WILL NOT TEST. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY BATTERY PACK. EMERGENCY LIGHTS TEST GOOD IAW AMM 33-51-07-2. ACFT OK FOR SERVICE. - [SDR FDEA201702010315](https://openairdocs.org/sdr/FDEA201702010315.md): Light · intermittent · Feb 1, 2017 · N953FD · Boeing 757236 · Emergency Equipment > JUMPSEATER REPORTED L1 SLIDE LIGHT FLICKERING DURING APPROACH AND LANDING. REMOVED AND REPLACED L-1 SLIDE LIGHT ASSY IAW WD 25-66-01. OPS CHECKS NORMAL IAW AMM 33-51-06-2-1. - [SDR FDEA201607202558](https://openairdocs.org/sdr/FDEA201607202558.md): Door · out of sequence · Jul 20, 2016 · N953FD · Boeing 757236 · Passenger/Crew Doors > LEFT FWD ENTRY DOOR SLIDE WOULD NOT ARM AFTER CLOSING. NO LIGHT ILLUMINATED WHEN POSITIONING HANDLE TO ARM. FOUND L1 DOOR OUT OF SEQUENCE, HAD TO REMOVE GIRT BAR AND SEQUENCE DOOR PROPERLY, AFTER DOOR WAS IN PROPER SEQUENCE REINSTALLED GIRT BAR AND PERFORM - [SDR FDEA201510073107](https://openairdocs.org/sdr/FDEA201510073107.md): Window · cracked · Oct 7, 2015 · N953FD · Boeing 757236 · Flight Compartment Windows > AT FL 370 THERE WAS A LOUD BANG FOLLOWED BY THE L1 WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION. DUE TO L1 WINDOW SHATTERED, R&R WINDOW TEMP CONTROLLER PRECAUTIONARY REF MM 30-41-01-4. GROUND OPS CK GOOD AT THIS TIME. A/C OK FOR SERVICE. REMOVED AND RE - [SDR FDEA201405020914](https://openairdocs.org/sdr/FDEA201405020914.md): Engine · failed · May 2, 2014 · N953FD · Boeing 757236 · Engine (Turbine/Turboprop) > AT FL 390, ACFT SHUDDERED WITH A ASSOCIATED POP. EGT WENT INTO RED, FOR RT ENGINE. IMMEDIATELY BROUGHT RT THROTTLE TO IDLE. EGT WAS IN THE RED APPROX 15 SECONDS AFTER THROTTLE WAS AT IDLE, MOTOR RAN NORMALLY AT IDLE. CAPTAIN STATED THAT HE OBSERVED THE - [SDR FDEA201310292644](https://openairdocs.org/sdr/FDEA201310292644.md): Girt Bar · loose · Oct 29, 2013 · N953FD · Boeing 757236 · Emergency Equipment > L1 DOOR SLIDE WILL NOT DISARM. GIRT BAR REMAINS ENGAGED IN FWD FLOOR LOCK. SLIDE STOWED. FOUND GIRT LOOSE FROM DOOR. ATTACHED IAW MM 25-66-10-2. OPS CHECKED NORMAL. - [SDR FDEA201310012353](https://openairdocs.org/sdr/FDEA201310012353.md): Battery Pack · failed · Oct 1, 2013 · N953FD · Boeing 757236 · Emergency Lighting > DURING PREFLIGHT, R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD. - [SDR FDEA201306291419](https://openairdocs.org/sdr/FDEA201306291419.md): Proximity Switch · dirty · Jun 29, 2013 · N953FD · Boeing 757236 · Entrance Stairs > WHEN CLOSING LT ENTRY DOOR AND ARMING FOR FLIGHT, SLIDE "ARMED" LIGHT DID NOT ILLUMINATE. TRIED A SECOND TIME AND IT ILLUMINATED. CLEANED BOTH GIRT BAR PROXIMITY SWITCHES ON L1 DOOR. ARMED L-1 DOOR SLIDE MULTIPLE TIMES WITH NORMAL INDICATION, IAW MM 25- - [SDR FDEA201303280677](https://openairdocs.org/sdr/FDEA201303280677.md): Lamp · unsecure · Mar 28, 2013 · N953FD · Boeing 757236 · Escape Slide > L1 DOOR SLIDE LIGHT DOESNT ILLUMINATE WHEN ARMED INTIL TAPPING LIGHT. SECURED LAMP IAW SMP. OPERATED ARM SYS NUMEROUS TIMES. OPS CHECKED GOOD. AC OK FOR CONTINUED SERVICE. - [SDR FDEA201210183682](https://openairdocs.org/sdr/FDEA201210183682.md): Transducer · failed · Oct 18, 2012 · N953FD · Boeing 757236 · Engine Vibration Analyzer > RT ENGINE SHUTDOWN AS A PRECAUTION FOR HIGH ENGINE VIBRATION (4.0) AMBER. RT ANTI-ICE VALVE FAILED TO OPEN IN ICING AND VIBRATION STARTED RT AFTER. SUSPECT COMPRESSOR BLADES WERE ICED. TROUBLE SHOT IAW FIM 71-05, PERFORMED AVM BITE IAW FIM 77-31 HAD A B8 - [SDR FDEA201207272712](https://openairdocs.org/sdr/FDEA201207272712.md): Skin · dented · Jul 27, 2012 · N953FD · Boeing 757236 · Fuselage Main, Plate/Skin > EXTERIOR SKIN DENTED AT BS 324 STR 24. REPAIR CARRIED OUT AS PER E.A F-5310-155921. REPAIR IS CLASSIFIED AS MAJOR. - [SDR FDEA201207132561](https://openairdocs.org/sdr/FDEA201207132561.md): Crease Beam · damaged · Jul 13, 2012 · N953FD · Boeing 757236 · Fuselage Main, Structure > LEFT CREASE BEAM AT BS 1584 HAS DAMAGED. CREASE BEAM REPAIRED IAW EA F-5310-161089, PART 1. REPAIR IS CLASSIFIED AS MAJOR. - [SDR FDEA201207102531](https://openairdocs.org/sdr/FDEA201207102531.md): Frame · corroded · Jul 10, 2012 · N953FD · Boeing 757236 · Cargo/Baggage Doors > FWD CARGO DOOR ASSY INNER CHORD AT FRAME BS 560 BELOW S25R AROUND FASTENER HOLE WITH CORROSION. REPAIR CARRIED OUT ON FWD CARGO DOOR IAW EA F-5230-161088, PART 1. REPAIR IS CLASSIFIED AS MAJOR. - [SDR FDEA201207062494](https://openairdocs.org/sdr/FDEA201207062494.md): Skin · corroded · Jul 6, 2012 · N953FD · Boeing 757236 · Fuselage Main, Plate/Skin > AFT LOWER CARGO COMPARTMENT DOOR CUTOUT EXT SKIN BETWEEN STA 1380 TO STA 1400 AND STR 26R TO STR 27R WITH CORROSION AROUND FASTENER HOLES. REPAIRED IAW EA F-5310-155912, PART 1. REPAIR IS CLASSIFIED AS MAJOR. Next page: https://openairdocs.org/aircraft/N953FD/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 = 'N953FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N953FD/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.