# Service difficulty reports: N964FD

A list on [N964FD](https://openairdocs.org/aircraft/N964FD.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 · 184 reports

- [SDR FDEA202212082893](https://openairdocs.org/sdr/FDEA202212082893.md): Flap · chafed · Dec 8, 2022 · N964FD · Boeing 757258 · Wing, Control Surfaces
  > R/H WING, OTBD MAIN FLAP L/E IS WORN NEAR THE INBD EDGE. REPAIRED RH WING, OTBD MAIN FLAP LE SKIN IAW EA F-5750-T0371953-P1.
- [SDR FDEA202212072885](https://openairdocs.org/sdr/FDEA202212072885.md): Beam · corroded · Dec 7, 2022 · N964FD · Boeing 757200 · Wing, Attach Fittings
  > RIGHT WING, AILERON BALANCE WEIGHT ATTACH BEAM IS CORRODED REMOVED AND REPLACED BEAM IAW BAC DWG 113N7100, SHEET 2, REVISION L AND B757 SRM 51- 40-02.
- [SDR FDEA202212072884](https://openairdocs.org/sdr/FDEA202212072884.md): Bracket · cracked · Dec 7, 2022 · N964FD · Boeing 757200 · Wing, Attach Fittings
  > LEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE L-BRACKET BROKEN/CRACKED REMOVED AND REPLACED CRACKED L-BRACKET ON LEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE, WITH NEW BRACKET P/N 313N5004Y15, P.O # 1044727.1 IAW BAC DWG 313N5004, REV C
- [SDR FDEA202212072882](https://openairdocs.org/sdr/FDEA202212072882.md): Skin · damaged · Dec 7, 2022 · N964FD · Boeing 757258 · Trailing Edge Flaps
  > RH O/B AFT FLAP O/B EDGE HAS COMPOSITE DAMAGE EVALUATED AND REPAIRED RH O/B AFT FLAP O/B EDGE IAW B757 SRM 57-53-01-2R, 51-70-04-0G.
- [SDR FDEA202212062880](https://openairdocs.org/sdr/FDEA202212062880.md): Scuff Plate · cracked · Dec 6, 2022 · N964FD · Boeing 757258 · Fuselage Miscellaneous Structure
  > R1 CABIN ENTRY DOOR CUTOUT AFT LOWER CORNER AND FWD SCUFF PLATE IS CRACKED ON THE TOP EDGE. REPAIRED THE R-1 DOOR FWD AND AFT LOWER CORNER SCUFF PLATES IAW DWG SR57- 53-003, REV. B. REMOVED AND REINSTALLED SCUFF PLATES IAW AMM 53-13-01-4.
- [SDR FDEA202212022867](https://openairdocs.org/sdr/FDEA202212022867.md): Seal Depressor · cracked · Dec 2, 2022 · N964FD · Boeing 757258 · Fuselage Miscellaneous Structure
  > MCD CUT OUT AFT EDGE LOWER SEAL DEPRESSOR IS CRACKED AND DEFORMED AT THE BOTTOM EDGE REMOVED, FABRICATED AND INSTALLED NEW SEAL DEPRESSOR P/N 143N8724-2 AT THE MCD CUTOUT AFT LOWER EDGE IAW BAC DWG 143N8724, REV. - AND 143N8720, REV. A.
- [SDR FDEA202211302862](https://openairdocs.org/sdr/FDEA202211302862.md): Skin · dented · Nov 30, 2022 · N964FD · Boeing 757258 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD AFT FLAP LOWER SURFACE IS DELAMINATED BETWEEN THE INBOARD AND OUTBOARD FLAP TRACKS REMOVED PAINT FINISH ON DENT AREA AND FOUND NO DELAMINATION OR BROKEN FIBERS. REPAIRED DENT IAW B757 SRM 57-53-01-2R FIG. 201 TABLE 2, SRM 51-70-04-0G PARA
- [SDR FDEA202211252843](https://openairdocs.org/sdr/FDEA202211252843.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS944-960, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK ORG MAT.230, REMOVED.012, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15
- [SDR FDEA202211252842](https://openairdocs.org/sdr/FDEA202211252842.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS900-BS928, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT.230, REMOVED.035, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15
- [SDR FDEA202211252841](https://openairdocs.org/sdr/FDEA202211252841.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS973-BS994, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT.230, REMOVED.016, FOUND TO BE IN LIMITS PER B757 SRM 53- 00=52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15
- [SDR FDEA202211252840](https://openairdocs.org/sdr/FDEA202211252840.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED BETWEEN BS917 - BS1037, RBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT IS.230, REMOVED.011, FOUND TO BE IN LIMITS PER B757 SRM 53-00-52-1A, ALODINED, PRIMED AND PAINTED PER B757SRM 51-20-01 AND B757 AMM 51-21
- [SDR FDEA202211252839](https://openairdocs.org/sdr/FDEA202211252839.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK IS GOUGED AND CORRODED BETWEEN BS914 - BS1037, LBL 45.5 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT.230, REMOVED.030, FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-21-15
- [SDR FDEA202211252838](https://openairdocs.org/sdr/FDEA202211252838.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK GOUGED AND CORRODED BETWEEN BS1018 - BS1039, LBL 24.75 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT.230, REMOVED.019, FOUND TO BE WITH IN LIMITS PER B757 SRM 53-00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01 AND B757 AMM 51-
- [SDR FDEA202211252837](https://openairdocs.org/sdr/FDEA202211252837.md): Seat Track · corroded · Nov 25, 2022 · N964FD · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK GOUGED AND CORRODED BETWEEN STA 915 TO 1037, RBL45.5 BLENDED DAMAGE FROM SEAT TRACK, ORG MAT.230, REMOVED.022 FOUND TO BE IN LIMITS PER B757 SRM 53- 00-52-1A, ALODINED, PRIMED AND PAINTED PER B757 SRM 51-20-01-0G AND B757 AMM 51-21-1
- [SDR FDEA202211232835](https://openairdocs.org/sdr/FDEA202211232835.md): Floor Panel · cracked · Nov 23, 2022 · N964FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL CRACKED @ BS879 - BS900 LBL 25 - LBL 44 FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005
- [SDR FDEA202211232833](https://openairdocs.org/sdr/FDEA202211232833.md): Flap · delaminated · Nov 23, 2022 · N964FD · Boeing 757200 · Trailing Edge Flaps
  > RH WING O/B MAIN FLAP UPPER SURFACE IS DELAMINATED APPROX 40" O/B FROMT THE I/B EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIR
- [SDR FDEA202211232832](https://openairdocs.org/sdr/FDEA202211232832.md): Flap · delaminated · Nov 23, 2022 · N964FD · Boeing 757200 · Trailing Edge Flaps
  > RH WING O/B MAIN FLAP UPPER SKIN IS DELAMINATED APROX 20" OB OF THE IB EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIR
- [SDR FDEA202211232831](https://openairdocs.org/sdr/FDEA202211232831.md): Flap · delaminated · Nov 23, 2022 · N964FD · Boeing 757200 · Trailing Edge Flaps
  > RH WING OB AFT FLAP UPPER SURFACE IS DELAMINATED BETWEEN THE I/B AND O/B TRACKS REPAIRED RH WING O/B AFT FLAP UPPER SURFACE IAW B757 SRM 57-53-01-2R AND 51-70-17-0G. MAJOR REPAIR
- [SDR FDEA202211152793](https://openairdocs.org/sdr/FDEA202211152793.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 242MBF IS DENTED/CRACKED FROM STA 900-1000, RBL 25-44. FABRICATED NEW FLOOR PANEL PER SRZ DWG SRZ -25-005.
- [SDR FDEA202211152792](https://openairdocs.org/sdr/FDEA202211152792.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 232MYF IS DENTED/CRACKED FROM STA 879-900, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.
- [SDR FDEA202211152791](https://openairdocs.org/sdr/FDEA202211152791.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 232MUF IS DENTED/CRACKED FROM STA 780-879, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.
- [SDR FDEA202211152790](https://openairdocs.org/sdr/FDEA202211152790.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 232MQF IS DENTED/CRACKED FROM STA 720-780, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005.
- [SDR FDEA202211152789](https://openairdocs.org/sdr/FDEA202211152789.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 232MLF IS DENTED/CRACKED FROM STA 680-720, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005
- [SDR FDEA202211152788](https://openairdocs.org/sdr/FDEA202211152788.md): Floor Panel · cracked · Nov 15, 2022 · N964FD · Boeing 757258 · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 232MGF IS DENTED/CRACKED FROM STA 625-680, RBL 25-44. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ DWG SRZ-25-005
- [SDR FDEA202210112544](https://openairdocs.org/sdr/FDEA202210112544.md): None · none · Oct 11, 2022 · N964FD · Boeing 757 · Passenger/Crew Doors
  > PDIS 964 52-10 8695 11OCT22 MEM OPEN U NO SLIDE LIGHT ON L1 RELAMPED SLIDE LIGHT. SYSTEM INDICATION OP CK'S NORMAL IN ACC B757 AMM 25-66-11-2-0
- [SDR FDEA202208282091](https://openairdocs.org/sdr/FDEA202208282091.md): Reservoir · discharged · Aug 28, 2022 · N964FD · Boeing 757258 · Service Doors
  > MDIS 964 52-10 8566 28AUG22 OAK FACT U EMERGENCY POWER RESERVOIR FOR R1 DOOR DISCHARGED. FACT 28AUG22 09:48 OAK U R&R EMERGENCY POWER RESERVOIR REF 757 AMM 52-11-30-4. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202204291087](https://openairdocs.org/sdr/FDEA202204291087.md): Gust Lock · cracked · Apr 29, 2022 · N964FD · Boeing 757258 · Passenger/Crew Doors
  > MDIS 964 52-10 8328 29APR22 RST OPEN U DURING DAILY CK FOUND THE L1 ENTRY DOOR GUST LOCK COLLAR BROKEN FACT 30APR22 17:07 TYS REMOVED AND REPLACED L1 PASSENGER DOOR HOLD OPEN LOCK. REFER
- [SDR FDEA202201100776](https://openairdocs.org/sdr/FDEA202201100776.md): None · none · Jan 10, 2022 · N964FD · Boeing 757200 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHTING LAMP INOP. RELAMPED L1 DOOR SLIDE EMERGENCY LIGHT ASSEMBLY PER AMM REF 33-51-06-2-1, PERFORMED SUCCESSFUL EMERGENCY LIGHT TEST, OK FOR SERVICE.
- [SDR FDEA202110082490](https://openairdocs.org/sdr/FDEA202110082490.md): Unknown · faulted · Oct 8, 2021 · N964FD · Boeing 757258 · Trailing Edge Flap Control System
  > ON APPROACH INTO OAK GOT TE FLAP DISAGREE WHILE EXPENDING FLAPS THROUGH 15. WENT AROUND. DISCOVERED HANDLE WAS STUCK BETWEEN FLAPS 15 AND 20. RAN QRH. DECLARED EMERGENCY. LANDED UNEVENTFUL IN OAK. FLAPS RETRACTED NORMALLY AFTER LANDING. REFERENCE WRI
- [SDR FDEA202101100034](https://openairdocs.org/sdr/FDEA202101100034.md): Skin · damaged · Jan 10, 2021 · N964FD · Boeing 757258 · Cargo/Baggage Doors
  > REPAIRED MAIN CARGO DOOR SKIN AT AFT ACTUATOR ON WRI 52-30/7347. THIS WRITEUP IS FOR TRACKING EA F-5230-T0359030, WRI IS FOR TRACKING EA F-5230-T0359030. COMPLIED WITH SKIN REPAIR, PER SRM 52-30-01-2R REPAIR 4. COMPLETED ON WRI 52-30/7347.
- [SDR FDEA202011032764](https://openairdocs.org/sdr/FDEA202011032764.md): Skin · punctured · Nov 3, 2020 · N964FD · Boeing 757258 · Leading Edge Devices
  > NR 6 SLAT HAS A PUNCTURE BLENDED NR 6 SLAT, IAW B757 SRM 51-10-02. ORIG MATERIAL.080, REMAINING.049, LOSS.031. FOUND OUT OF LIMITS, IAW B757 SRM 57-43-01-1A. REPAIRED SLAT, IAW B757 SRM 57-43-01-2R REP 9.
- [SDR FDEA202010292711](https://openairdocs.org/sdr/FDEA202010292711.md): Skin · chafed · Oct 29, 2020 · N964FD · Boeing 757258 · Trailing Edge Flaps
  > CHAFE MARK LEADING EDGE OF RIGHT OUTBOARD MAIN FLAP INBOARD SIDE. REMOVED DAMAGE ON LEADING EDGE OF RT OUTBOARD MAIN FLAP INBOARD SIDE, IAW B757 SRM 51-10-02. ORIG MAT.080 REM.030 LOSS.050 FOUND TO BE OUT OF LIMITS, IAW B757 SRM 57-53-01-1A FIG 101. REP
- [SDR FDEA202010282681](https://openairdocs.org/sdr/FDEA202010282681.md): Seat Track · corroded · Oct 28, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL 24 STA 1322. REMOVED CORROSION ON SEAT TRACK STA 1322 LBL 24, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL.090, REMAINING.034, LOSS.056 OUT OF LIMITS, IAW B757 SRM 53-00-52-1A. REMOVED, FABRICATED, AND INSTAL
- [SDR FDEA202010252648](https://openairdocs.org/sdr/FDEA202010252648.md): Seat Track · corroded · Oct 25, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 366. ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T0357429 P1. FUSELAGE-MAINFRAME-RBL 45.50 SEAT TRACK CORROSION REPAIR FROM STA 365 TO 377.
- [SDR FDEA202010232626](https://openairdocs.org/sdr/FDEA202010232626.md): Seat Track · corroded · Oct 23, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL 45 STA 1320. REMOVED CORROSION ON SEAT TRACK STA 1320 LBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-52 FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK, IAW B75
- [SDR FDEA202010212580](https://openairdocs.org/sdr/FDEA202010212580.md): Skin · damaged · Oct 21, 2020 · N964FD · Boeing 757258 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP TRAILING EDGE UPPER EXTERNAL SURFACE HAS MULTIPLE AREAS OF BARE COMPOSITE. EVALUATED LT WING OUTBOARD FLAP TRAILING EDGE UPPER EXTERNAL SURFACE AND FOUND TO BE OUT OF LIMITS, IAW B757 SRM 51-10-06-2R. REPAIRED AREA IAW B757 SRM 57-53
- [SDR FDEA202010152518](https://openairdocs.org/sdr/FDEA202010152518.md): Seat Track · corroded · Oct 15, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-24 STA 1540. REMOVED CORR ON SEAT TRACK STA 1540 RBL 24, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL.090, REMAINING.034, LOSS.056, OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED AND
- [SDR FDEA202010152517](https://openairdocs.org/sdr/FDEA202010152517.md): Seat Track · corroded · Oct 15, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-45 STA 1540. REMOVED CORR ON SEAT TRACK STA 1540 RBL 45, IAW B757 SRM 51-10-02. ORIGINAL MAT.090, REMAINING.040, LOSS.050, OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVED, FABRICATED, AND INSTA
- [SDR FDEA202010142493](https://openairdocs.org/sdr/FDEA202010142493.md): Seat Track · corroded · Oct 14, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT LBL-24 STA 1320 EVALUATED SEAT TRACK STA 1320 LBL 24. 100% MATERIAL LOSS, OUT OF LIMITS, IAW B757 SRM 53-00-5252-1A. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK, IAW B757 SRM 51-40-02, 53-6060-52-01 FIG 1 A
- [SDR FDEA202010142490](https://openairdocs.org/sdr/FDEA202010142490.md): Seat Track · corroded · Oct 14, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-45 STA 1320. REMOVED CORROSION FROM MAIN CABIN SEAT TRACK STA 1320 RBL 45, IAW B757 SRM 51-10-02-0G. ORIGINAL MATERIAL.090, 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-00-52-1A. REMOVED, F
- [SDR FDEA202010142489](https://openairdocs.org/sdr/FDEA202010142489.md): Seat Track · corroded · Oct 14, 2020 · N964FD · Boeing 757258 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL-24 STA 1320. REMOVED CORROSION ON SEAT TRACK STA 1320 RBL 24, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIG 101. REMOVE, FABRICATED AND INSTALLED NEW SEAT TRACK, IAW B
- [SDR FDEA202010142494](https://openairdocs.org/sdr/FDEA202010142494.md): Floorbeam · corroded · Oct 14, 2020 · N964FD · Boeing 757258 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN RBL 26 AND RBL 45 STA 1055. REMOVED CORROSION ON FLOOR SUPPORT PLATE STA 1055 RBL 26-RBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS FOUND OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED
- [SDR FDEA202010142491](https://openairdocs.org/sdr/FDEA202010142491.md): Floorbeam · corroded · Oct 14, 2020 · N964FD · Boeing 757258 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN LBL 24 AND LBL 45 STA 900. REMOVED CORROSION ON FLOOR SUPPORT PLATE STA 900 LBL 24-LBL 45, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED, AND I
- [SDR FDEA202010132481](https://openairdocs.org/sdr/FDEA202010132481.md): Floorbeam · corroded · Oct 13, 2020 · N964FD · Boeing 757258 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN RBL 1 AND RBL 24 STA 1020. REMOVED CORROSION ON FLOOR SUPPORT STA 1020 RBL 1-RBL 24, IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS, IAW B757 SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED
- [SDR FDEA2020081431879](https://openairdocs.org/sdr/FDEA2020081431879.md): Transmission · low · Aug 13, 2020 · N964FD · Boeing 757258 · Trailing Flap Position Indicating System
  > ON APPROACH WHEN WE SELECTED FLAPS 20 DEGREES WE RECEIVED A "TE FLAPS DISAGREE" MESSAGE. COMPLIED WITH QRH. VISUAL INSPECTION OF T/E FLAPS SHOWED NO MECHANICAL DAMAGE. RESTORED FLAP SYSTEM TO NORMAL AND OPERATED NORMALLY. FSEU #1 FAULT CODE 305, #2 FAULT
- [SDR FDEA2018122433599](https://openairdocs.org/sdr/FDEA2018122433599.md): Charger · inoperative · Dec 23, 2018 · N964FD · Boeing 757258 · Emergency Lighting
  > R1 EXTERIOR EMERGENCY SLIDE LIGHT WILL NOT TEST. RELAMPED BUT NO HELP.REF WDM 33-51-12, NO VOLTAGE AT LIGHT L30,HAS GOOD GROUND.REMOVED AND REPLACED POWER SUPPLY M730 REF MM 33-51-07-2.EMERGENCY LIGHT OPS CHECK NORMAL REF MM 33-51-00-5.A/C OK FOR
- [SDR FDEA201811283388](https://openairdocs.org/sdr/FDEA201811283388.md): Battery Pack · discharged · Nov 28, 2018 · N964FD · Boeing 757258 · Emergency Lighting
  > L1 DOOR SLIDE LIGHT INOP. R&R EMERGENCY BATTERY PACK M731 PER MM 33-51-07-2, PN 2013-1A S/N 54663.
- [SDR FDEA201811233359](https://openairdocs.org/sdr/FDEA201811233359.md): Light · inoperative · Nov 23, 2018 · N964FD · Boeing 757258 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGHT BULB (P/N GE767) REF AMM 33-51-01. OPERATIONAL CHECKS GOOD.
- [SDR FDEA201810232973](https://openairdocs.org/sdr/FDEA201810232973.md): Seal · leaking · Oct 23, 2018 · N964FD · Boeing 757258 · Flight Compartment Windows
  > A WHINE STARTED AT APPROXIMATELY 6K FT MSL. IT GOT LOUDER AS WE CLIMBED TO 15K FT MSL. WE SLOWED FROM 285 KTS IAS TO 210 KTS IAS AT 15K FT MSL, THE WHINE DECREASED SOME BUT NOT AS MUCH AS DESCENDING. WHINE STOPPED AT 7K FT MSL. BOTH INTERNAL AND EXTERNAL COMM
- [SDR FDEA201810082811](https://openairdocs.org/sdr/FDEA201810082811.md): Skin · cracked · Oct 8, 2018 · N964FD · Boeing 757258 · Trailing Edge Flaps
  > RT OTBD FLAP UNDERSIDE HAS SMALL CRACK ON THE INBD SIDE NEAR THE INBD FLAP TRACK FAIRING. REPAIRED RT OUTBD FLAP UNDERSIDE SMALL CRACK ON THE INBD SIDE NEAR THE INBD FLAP TRACK FAIRING IAW SRM 51-70-04-OG FIG 14 SHEET 2 AND EA WORK CARD TF-5750-T0342790 P1. RT

Next page: https://openairdocs.org/aircraft/N964FD/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 = 'N964FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N964FD/reports

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