# Service difficulty reports: N936FD A list on [N936FD](https://openairdocs.org/aircraft/N936FD.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 5 · 229 reports - [SDR FDEA202312141942](https://openairdocs.org/sdr/FDEA202312141942.md): Coupling · damaged · Dec 14, 2023 · N936FD · Boeing 757200 · Detection System > AT CRUIRE AT FL 340 HAD A LT ENGINE FIRE (L ENG FIRE) AND OVERHEAT (L ENG OVERHEAT) INDICTION ON EICAS, LT FIRE HANDLE AND LEFT CONTOL LEVER. NO UNUSUAL LT ENG INDICATIONS OR VIBRARATIONS OBSERVED., LT EGT REMAINED WITHIN LIMITS ENTIRE TIME. FOLLOWED QR - [SDR FDEA202311161857](https://openairdocs.org/sdr/FDEA202311161857.md): Flex Line · leaking · Nov 16, 2023 · N936FD · Boeing 757200 · Hydraulic System, Main > IN SHORT FINAL AFTER FULLY CONFIGURED, L HYD SYS PRESS EICAS CAME ON. LANDED WITH ROLL TO RIGHT, NO NOSE WHEEL STEERING. FACT 15NOV23 23:59 MEM U AMM: 20-10-10-4 AMM: 29-11-00-2 FIM: 29-11 F/T 808 AMM: 32-21-09-4 DURING INSPECTION AND CHECK FOUND - [SDR FDEA202309141597](https://openairdocs.org/sdr/FDEA202309141597.md): Skin · damaged · Sep 14, 2023 · N936FD · Boeing 757200 · Wing, Plate/Skin > DURING DVI INSPECTION OF L/E SKIN REPAIR ON #3 SLAT ON HECO CARD 9019, FOUND 2 BLIND FASTENERS THAT WERE LOOSE AND LOCKING PINS WERE NOT FLUSH WITH THE FASTENER HEAD. REMOVED AND REPLACED 2 EACH FASTENERS PER FEDEX EA# F-2780-T0350154 A P3 TITLE: FLIGHT CO - [SDR FDEA202309131593](https://openairdocs.org/sdr/FDEA202309131593.md): Skin · corroded · Sep 13, 2023 · N936FD · Boeing 757200 · Nacelle/Pylon, Plate/Skin > #1 PYLON PANEL 433HR HAS CORROSION ON AFT SURFACE OF THE PANEL FABRICATED NEW PANEL PER BAC DWG 311N5049 REV C AND FEDEX EA # F-5430-T0376029 TITLE: NACELLS/PYLONS - SKIN/PLATES/PANELS - #1 PYLON, STRUT ACCESS PANEL ASSY (443HR), FABRICATION - [SDR FDEA202309131592](https://openairdocs.org/sdr/FDEA202309131592.md): Compressor · loose · Sep 13, 2023 · N936FD · Boeing 757200 · Turbine Engine Compressor Section > #1 ENG FAN CASE AREA PROTECTIVE PLASTIC COVER FOR KEVLAR SEPERATING FROM COMPRESSOR CASING AT FWD EDGE SEVERAL PLACES REPAIRED #1 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WITH PATCH IAW B757 AMM: 72-34- 10-8-4 - [SDR FDEA202309131591](https://openairdocs.org/sdr/FDEA202309131591.md): Compressor · torn · Sep 13, 2023 · N936FD · Boeing 757200 · Engine (Turbine/Turboprop) > #2 ENGINE LP COMPRESSOR CASE KEVLAR WRAPPING FWD EDGE, PROTECTIVE PLASTIC COVER TORN AT 4 O'CLOCK POSITION. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WITH PATCH IAW B757 AMM 72-34- 10-8-4 - [SDR FDEA202309131590](https://openairdocs.org/sdr/FDEA202309131590.md): Compressor · loose · Sep 13, 2023 · N936FD · Boeing 757200 · Turbine Engine Compressor Section > #2 ENG LP COMPRESSOR CASE KEVLAR WRAPPING PROTECTIVE PLASTIC COVER, SEVERAL REPAIRS PATCHTAPE PEELING OFF. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WIHT PATCH IAW B757 AMM 72-34- 10-8-4 - [SDR FDEA202309111572](https://openairdocs.org/sdr/FDEA202309111572.md): Attach Angle · cracked · Sep 11, 2023 · N936FD · Boeing 757200 · Fuselage Main, Attach Fittings > LOWER FRAME ATTACH CLIP IS CRACKED IN LH MLG WHEEL WELL, ON AFT SIDE OF FRAME @ APPROX. STA 1064 LBL 30 REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP P/N 654N0243-13 PER BAC DWG 149N7550 REV H - [SDR FDEA202309101570](https://openairdocs.org/sdr/FDEA202309101570.md): Floor Support · cracked · Sep 10, 2023 · N936FD · Boeing 757200 · Fuselage Miscellaneous Structure > AFT PIT CARGO COMPARTMENT FLOOR STRINGER HAS A CRACK ON STA 1340 RBL 7.55 REPAIRED AFT PIT CARGO COMPARTMENT FLOOR STRINGER STA 1340 RBL 7.55 IAW B757 SRM 53-00-53-2R - [SDR FDEA202309031543](https://openairdocs.org/sdr/FDEA202309031543.md): Slat · delaminated · Sep 3, 2023 · N936FD · Boeing 757200 · Leading Edge Devices > DISBOND INDICATION FOUND 5" OUTBOARD ON TOP SIDE OF SLAT #2 T/E WEDGE. REPAIRED #2 SLAT T/E WEDGE BY REMOVING DAMAGED AREA OS UPPER SKIN LOCATED 5.5" FROM I/B END AND 6.2" FROM TE AND BONDING REPAIR FILLER AND DOUBLER IAW B757 SRM 57- 43-02-2R AND 51-70-10- - [SDR FDEA202309031542](https://openairdocs.org/sdr/FDEA202309031542.md): Slat · delaminated · Sep 3, 2023 · N936FD · Boeing 757200 · Leading Edge Devices > DISBOND INDICATION FOUND 93" OUTBOARD ON TOP SIDE OF SLAT #3 T/E WEDGE. REPAIRED #3 SALT T/E WEDGE UPPER SKIN DISBONDED AREA 93" FROM I/B END, 5375 FROM T/E IAW B757 SRM 57-43-02-2R FIG 201 REPAIR 1 AND 51-70-10-2R REPAIR 4 - [SDR FDEA202309031541](https://openairdocs.org/sdr/FDEA202309031541.md): Slat · delaminated · Sep 3, 2023 · N936FD · Boeing 757200 · Leading Edge Devices > DISBOND INDICATION FOUND 67" OUTBOARD ON TOP SIDE OF #3 TE WEDGE. REPAIRED #3 SLAT T/E UPPER SKIN DISBOND 67.5 FROM I/B END, 6.25" FROM T/E IAW B757 SRM 57- 43-02-2R FIG 201 REPAIR 1 AND 51-70-10-2R REPAIR 4. - [SDR FDEA202308291538](https://openairdocs.org/sdr/FDEA202308291538.md): Panel · cracked · Aug 29, 2023 · N936FD · Boeing 757200 · Wing, Plate/Skin > L.WING L/E PANEL 521AB HAS A CRACK AT THE EDGE OF THE PANEL EVALUATED, CLEANED, SANDED, REMOVED DAMAGE, ON L/E PANEL 521AB AND REPAIRED IAW B757 SRM 57-41-01-2R SRM 51-70-07, SRM 51-70-14 - [SDR FDEA202303010354](https://openairdocs.org/sdr/FDEA202303010354.md): Guide Arm · failed · Mar 1, 2023 · N936FD · Boeing 757200 · Passenger/Crew Doors > ENTRY DOOR WILL NOT CLOSE PROPERLY. APPEARS A HINGE IS NOT ALIGNED CORRECTLY. COMPLETED INSTALL OF L1 ENTRY DOOR GUIDE ARM. ALL ADJUSTMENTS AND OPS CHECKS GOOD. REF 757 AMM 52-11-04-2. RE - [SDR FDEA202302220333](https://openairdocs.org/sdr/FDEA202302220333.md): None · none · Feb 22, 2023 · N936FD · Boeing 757200 · Trailing Edge Flap Control System > PDIS 936 27-50 1303 22FEB23 MSP FACT U TE FLAP DISAGREE BETWEEN 5-15. RAN QRH AND LANDED MSP. ***EMERGENCY DECLARED*** FACT 22FEB23 13:11 MSP U FIM: 21-51-00-815-808 FIM: 21-51-00-815-815 UPON ENTERING FLIGHT DECK NOTED T/E AND L/E FLAP - [SDR FDEA202110252611](https://openairdocs.org/sdr/FDEA202110252611.md): Frame · unknown · Oct 25, 2021 · N936FD · Boeing 757200 · Fuselage Main, Structure > COMPLY WITH EA FOR FRAME REPAIR STA. 1640 RH COMPLIED WITH EA #T F-5310-138502E P9 EA TITLE FUSELAGE-MAINFRAME-EXISTING FRAME REPAIR OF BS 1640, WL 208.10 RIGHT HAND-FRAME SECTION REPLACEMENT, CATEGORY "B" REPAIR, MAJOR REPAIR. - [SDR FDEA202110212587](https://openairdocs.org/sdr/FDEA202110212587.md): None · cracked · Oct 21, 2021 · N936FD · Boeing 757200 · Fuselage Main, Structure > CRACKED FLOOR BEAM @ STA. 580,LBL 45. REPAIRED FLOOR BEAM AT STA 580 LBL 45 PER E.A. # F-5310-T0364468 P1 AND SR DRAWING # 57-53-004 E.A. TITLE FUSELAGE-MAINFRAME-FLOOR BEAM AT STA. 580 AND LBL 45 CRACKED REPAIR PER DRAWING SR 57-53-004 WITH MINOR DEVIATIO - [SDR FDEA202110152541](https://openairdocs.org/sdr/FDEA202110152541.md): Seat Track · cracked · Oct 15, 2021 · N936FD · Boeing 757200 · Fuselage Main, Structure > SEAT TRACK AT STA 580, LBL 45, FLANGE HAS A CRACK. REPAIRED SEAT TRACK LBL45 AT STA 530 - 680 IAW EA# F-5321-T0364473, FUSELAGE - CARGO FLOOR - SECTION 43 - MCD SEAT TRACK FLANGE CRACK AT STA 580 LBL45. MAJOR REPAIR - [SDR FDEA202110082498](https://openairdocs.org/sdr/FDEA202110082498.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER T21/1575353 IAW DWG SRZ 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082497](https://openairdocs.org/sdr/FDEA202110082497.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > EDGE DAMAGE NOTED ON FLOOR PANEL 242MEF BOTTOM SIDE. FABRICATED FLOOR BOARD 242MEF ON VT MAE TRAVELER T21/1577548 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082496](https://openairdocs.org/sdr/FDEA202110082496.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1575476 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082495](https://openairdocs.org/sdr/FDEA202110082495.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T21/1575357 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082494](https://openairdocs.org/sdr/FDEA202110082494.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 222MEF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MEF ON VT MAE TRAVELER T21/1575352 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082493](https://openairdocs.org/sdr/FDEA202110082493.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1575471 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR - [SDR FDEA202110082492](https://openairdocs.org/sdr/FDEA202110082492.md): None · damaged · Oct 8, 2021 · N936FD · Boeing 7572T7 · Standard Practices/Structures > ZONE 220 FLOOR BOARD 222BF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222BF ON VT MAE TRAVELER T21/1575359 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR - [SDR FDEA202101090028](https://openairdocs.org/sdr/FDEA202101090028.md): Indicator · no indication · Jan 9, 2021 · N936FD · Boeing 7572T7 · Passenger/Crew Doors > PRE-DEPARTURE UNABLE TO ARM L1 DOOR. NO SLIDE LIGHT. COMPLIED WITH INSPECTION & TEST OF GIRT BAR HANDING MECHANISM IAW MM 25-66-10-2. ALL CHECKED NORMAL. ARM LIGHT L1 DOOR TESTED NORMAL.. OK FOR SERVICE. - [SDR FDEA202011252964](https://openairdocs.org/sdr/FDEA202011252964.md): Transmission · tripped · Nov 25, 2020 · N936FD · Boeing 7572T7 · Trailing Edge Flap Actuator > TRAILING EDGE FLAP DISAGREE BETWEEN 20&25 W/FLAP HANDLE IN 25 DETENT. COMPLIED W/QRH EMERGENCY DECLARED. ACCOMPLISHED FIM 27-51-00-815-808 FIG 105. FOUND RT INBOARD FLAP TRANS OVERLOAD INDICATION POPPED. RESET AND ACCOMPLISHED LUBE OF TRANS, PER AMM 12-21- - [SDR FDEA201910112605](https://openairdocs.org/sdr/FDEA201910112605.md): Cusp Web · corroded · Oct 11, 2019 · N936FD · Boeing 7572T7 · Fuselage Miscellaneous Structure > MAIN CARGO AREA STA 1450 RH CUSP WEB CORRODED. REMOVED,FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 146N5590. - [SDR FDEA201910112604](https://openairdocs.org/sdr/FDEA201910112604.md): Skin · dented · Oct 11, 2019 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/Skin > EXTERIOR FUSELAGE SKIN DENTED AT STA 408 BETWEEN STRINGER 10L AND 11L REPAIRED PER EA# F-5310-T0349762-P1 - [SDR FDEA201910112592](https://openairdocs.org/sdr/FDEA201910112592.md): Skin · dented · Oct 11, 2019 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/Skin > LOWER AFT CARGO FUSELAGE AT BS 1635 BETWEEN STR27R AND 28R HAS PITTING CORROSION ON INTERNAL SURFACE ACOMPLISHED WORK IAW EA F-5310-T0349844 - [SDR FDEA2019101102590](https://openairdocs.org/sdr/FDEA2019101102590.md): Slat Track · corroded · Oct 10, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LEFT WING #3 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED #3 SLAT IB MAINTRACK REF B757 AMM 27-81-12-4. ADJUSTMENT OF #3 TRACK IS ACCOMPLISHED ON NR N00107. OPS CHECK OF #3 SLAT MAIN TRACK IS ACCOMPLISHED ON NR N00107. - [SDR FDEA2019101102584](https://openairdocs.org/sdr/FDEA2019101102584.md): Attach Angle · corroded · Oct 10, 2019 · N936FD · Boeing 7572T7 · Wing, Attach Fittings > L/W L/E PNL ATTACH STRUCTURE AT STA 532 HAS INTERGRANULAR CORROSION REMOVED AND REPLACED ANGLE PER B757 SRM 51-40-02 AND DWG #114N2151 - [SDR FDEA2019101102583](https://openairdocs.org/sdr/FDEA2019101102583.md): Attach Angle · corroded · Oct 10, 2019 · N936FD · Boeing 7572T7 · Wing, Attach Fittings > LEFT WING L/E PANEL ATTACH ANGLE AT WS 478 HAD INTERGRANULAR CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, AND DWG 114N2151. - [SDR FDEA201910092528](https://openairdocs.org/sdr/FDEA201910092528.md): Skin · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LT WING NR 3 SLAT LEADING EDGE IS CORRODED APPROXIMATELY 32 IN OUTBOARD OF THE INBOARD EDGE IN THE UNPAINTED SURFACE. REPAIRED PER B757 SRM 57-43-01-2R. - [SDR FDEA2019101092528](https://openairdocs.org/sdr/FDEA2019101092528.md): Skin · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LEFT WING NR 3 SLAT L/E WAS CORRODED APPROX 32 INCHES OTBD OF THE INBD EDGE IN THE UNPAINTED SURFACE. REPAIRED THE SLAT IAW SRM 57-43-01-2R. - [SDR FDEA2019101092536](https://openairdocs.org/sdr/FDEA2019101092536.md): Gear · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Slat Position Indicating System > LEFT WING NR 4 SLAT OTBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 4 SLAT OTBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4. - [SDR FDEA201910092538](https://openairdocs.org/sdr/FDEA201910092538.md): Sprocket · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Slat Control System > LEFT WING NR 4 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 57-81-18-4. OPS CHECKED GOOD IAW AMM 27-81-18-4. - [SDR FDEA2019101092537](https://openairdocs.org/sdr/FDEA2019101092537.md): Sprocket · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Slat Control System > LEFT WING NR 3 SLAT INBD TRACK DRIVE MOTOR SPROCKET TEETH PITTED. REMOVED AND REPLACED NR 3 SLAT INBD ROTARY ACTUATOR SPROCKET IAW AMM 27-81-18-4. OPS CHECK GOOD IAW AMM 27-81-18-4. - [SDR FDEA2019101092533](https://openairdocs.org/sdr/FDEA2019101092533.md): Slat Track · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LEFT WING NR 3 SLAT OTBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 3 SLAT OTBD TRACK IAW AMM 27-81-12-4. OPS CHECKED GOOD IAW AMM 57-81, 81-18-4. - [SDR FDEA2019101092542](https://openairdocs.org/sdr/FDEA2019101092542.md): Splice · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Wing, Plate/Skin > LEFT WING T/E OTBD PANEL SPLICE STRIP, JUST AFT OF THE AILERON WAS CORRODED. REMOVED AND REPLACED THE SPLICE STRIP IAW SRM 51-40-02, AND DWG 113N1640, REV B. - [SDR FDEA2019101092539](https://openairdocs.org/sdr/FDEA2019101092539.md): Striker · delaminated · Oct 9, 2019 · N936FD · Boeing 7572T7 · Main Landing Gear > LMLG DOOR AFT UPSTOP PAD IS WORN. REMOVED AND REPLACED STRIKER PLATE IAW SRM 51-10-02, DWG 149N6002, AND SRM 51-70-06-0G. REMOVED DAMAGED PLIES AND BONDED REPAIR IAW 5010, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51-20-05. RESTORED FINISH - [SDR FDEA2019101092535](https://openairdocs.org/sdr/FDEA2019101092535.md): Striker · delaminated · Oct 9, 2019 · N936FD · Boeing 75723A · Landing Gear Doors > RIGHT MLG DOOR LOWER UPSTOP PAD HAD COMPOSITE MATERIAL DELAMINATION. REMOVED DAMAGE AND STRIKER PLATE, BONDED NEW POTTING AND REPAIR PLIES AND STRIKER PLATE IAW DWG 149N6002, DWG 149N6003, REV C, SRM 51-70-06-0G, AND SRM 52-80-02-2R. SEALED PLATE IAW SRM 51- - [SDR FDEA2019101092532](https://openairdocs.org/sdr/FDEA2019101092532.md): Slat Track · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LEFT WING NR 4 SLAT INBD TRACK WORN AND PITTED. REMOVED AND REPLACED THE NR 4 SLAT INBOARD TRACK IAW AMM 27-81-12-4. ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON SNRM N00108. - [SDR FDEA2019101092529](https://openairdocs.org/sdr/FDEA2019101092529.md): Wedge · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > LEFT WING NR 5 SLAT LOWER T/E WEDGE WAS DELAMINATED AT THE INBD AFT CORNER. REPLACED THE SLAT. - [SDR FDEA2019101092527](https://openairdocs.org/sdr/FDEA2019101092527.md): Attach Angle · corroded · Oct 9, 2019 · N936FD · Boeing 7572T7 · Leading Edge Devices > RIGHT WING NR 9 SLAT LOWER T/E WEDGE ATTACH ANGLE IS CORRODED AND THE T/E WEDGE WAS BULGING WITH FASTENERS PULLING THROUGH AT THREE LOCATIONS. REPLACED THE SLAT. - [SDR FDEA2019101082502](https://openairdocs.org/sdr/FDEA2019101082502.md): Skin · dented · Oct 8, 2019 · N936FD · Boeing 7572T7 · Auxiliary Power Unit (APU) Doors > APU COMPARTMENT RT DOOR OUTER SURFACE IS CREASED. REPAIRED APU RT DOOR OUTER SKIN IAW EA F-5240-T0349703. - [SDR FDEA2019101082501](https://openairdocs.org/sdr/FDEA2019101082501.md): Skin · dented · Oct 8, 2019 · N936FD · Boeing 7572T7 · Auxiliary Power Unit (APU) Doors > APU COMPARTMENT LT DOOR OUTER SURFACE IS BULGED. REPAIRED APU DOOR OUTER SURFACE IAW EA F-5240-T0349685. - [SDR FDEA2019101082499](https://openairdocs.org/sdr/FDEA2019101082499.md): Skin · dented · Oct 8, 2019 · N936FD · Boeing 7572T7 · Fuselage Main, Plate/Skin > ETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED OPEN HOLES AND INSTALLED NEW FASTENERS IAW EA F-5330-T0349901. - [SDR FDEA201908091828](https://openairdocs.org/sdr/FDEA201908091828.md): Unknown · unknown · Aug 9, 2019 · N936FD · Boeing 757 · Wing, Plate/Skin > MOD TYPE T MOD NO. F-5730-T0348437 REV NO. PS P2 WINGS - PLATES AND SKINS - LH WING T.E. SKIN PANEL W BL 235 TO 300 - CRACKS AND COMPLY WITH E..A. F-5730-T0348437 REV NO. POS. - [SDR FDEA201907081509](https://openairdocs.org/sdr/FDEA201907081509.md): Battery · discharged · Jul 8, 2019 · N936FD · Boeing 7572T7 · Emergency Lighting > DURING PRE-DEPARTURE CHECK, FOUND NUMEROUS EMERGENCY EXIT SIGNS AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE EMERGENCY LIGHT BATTERIES USING SHIP'S POWER FOR 1 HOUR. NO HELP. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY ASSY IN REF TO AMM 33-51-07-2. Next page: https://openairdocs.org/aircraft/N936FD/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 = 'N936FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N936FD/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.