# Service difficulty reports: Boeing 757-258

A list on [Boeing 757-258](https://openairdocs.org/model/boeing-757-258.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 96 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 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 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 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 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 FDEA202204291081](https://openairdocs.org/sdr/FDEA202204291081.md): Module · failed · Apr 29, 2022 · N965FD · Boeing 757258 · Rudder Tab Control System
  > RUDDER RATIO EICAS MESSAGE AFTER TAKEOFF. QRH CHECKLIST ACCOMPLISHED. NOTIFIED GOC. NO ADVERSE HANDLING CHARACTERISTICS NOTED IN FLIGHT OR ON LANDING. EMERGENCY DECLARED. SHGN 29APR22 17:31 OAK FOLLOWING 757 FIM 27-21 FAULT TREE 809. AT STEP 21 FOUND HYD
- [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 FDEA202104070840](https://openairdocs.org/sdr/FDEA202104070840.md): Floor Panel · damaged · Apr 7, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > AFT MAIN CABIN R/H FLOOR PANEL STA 1640 TO 1660 HAS BLUE WATER STAIN. PANEL 252MVF FABRICATED AFT MAIN CABIN R/H FLOOR PANEL 252MVF STA 1640 TO 1660 ON VT MAE TRAVELER # T21/1540623 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202104070839](https://openairdocs.org/sdr/FDEA202104070839.md): Floorboard · broken · Apr 7, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 251MWF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251MWF ON VT MAE TRAVELER # T21/1540891 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202104070838](https://openairdocs.org/sdr/FDEA202104070838.md): Floor Panel · sheared · Apr 7, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 251MVF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251MVF ON VT MAE TRAVELER # T21/1540720 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202104020813](https://openairdocs.org/sdr/FDEA202104020813.md): Floor Panel · delaminated · Apr 2, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > LAVATORY FLOOR PANEL 221BF DELAMINATED. FABRICATED LAVATORY FLOOR PANEL 221BF ON VTMAE TRAVELER # T21/1540096 IAW DWG SRZ-25-005 REV "R". CAT "A" MAJOR REPAIR
- [SDR FDEA202103270790](https://openairdocs.org/sdr/FDEA202103270790.md): Floor Panel · damaged · Mar 27, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > AFT MAIN CABIN FLOOR PANEL STA 1540 TO STA 1640 HAS A BLUE WATER STAIN. PANEL 252MNF. FABRICATED ZONE 250 FLOOR BOARD 252MNF ON VT MAE TRAVELER # T21/1541444 IAW DWG SRZ-25-005 REVISION R. MAJOR REPA
- [SDR FDEA202103270789](https://openairdocs.org/sdr/FDEA202103270789.md): Floorboard · damaged · Mar 27, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > ZONE 250 FLOOR BOARD 252MVF HAS BLUE STAIN. FABRICATED ZONE 250 FLOOR BOARD 252MVF ON VT/MAE TRAVELER # T21/1540717 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202103250772](https://openairdocs.org/sdr/FDEA202103250772.md): Floor Panel · delaminated · Mar 25, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222MF DELAMINATED. FABRICATED COURIER FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1540228 IAW FEDEX DWG SRZ-25-005. CAT 'A' MAJOR REPAIR.
- [SDR FDEA202103250768](https://openairdocs.org/sdr/FDEA202103250768.md): Frame · damaged · Mar 25, 2021 · N965FD · Boeing 757258 · Fuselage Main, Frame
  > MAIN CABIN AT STA. 1060 FR. REPAIR BTW STR 3R AND 9R REQUIRES OUTER AND INNER CHORDS TO BE FABRICATED. INNER CHORD FABRICATED ON VTMAE TRAVELER T21/1539829, OUTER CHORD FABRICATED ON VTMAE TRAVELER T21/1539836 IAW WORK CARD E.A. T F-5310-T0345523 B P2 STEP
- [SDR FDEA202103250771](https://openairdocs.org/sdr/FDEA202103250771.md): Floor Panel · delaminated · Mar 25, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > COURIR FLOOR PANEL 222AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 222F ON VTMAE TRAVELER # T21/1540217 IAW FEDEX DWG SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.
- [SDR FDEA202103250770](https://openairdocs.org/sdr/FDEA202103250770.md): Floor Panel · delaminated · Mar 25, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > COURIER 221AF FLOOR PANEL DELAMINATED. FABRICATED COURIER 221AF FLOOR PANEL ON VTMAE TRAVELER # T21/1540104 IAW FEDEX DWG SRZ-25-005 REV R. CAT A MAJOR REPAIR.
- [SDR FDEA202103250769](https://openairdocs.org/sdr/FDEA202103250769.md): Floor Panel · delaminated · Mar 25, 2021 · N965FD · Boeing 757258 · Fuselage Floor Panel
  > COURIER 221MBF FLOOR PANEL DELMINATED. FABRICATED COURIER 221MBF FLOOR PNEL ON VTMAE TRAVELEL # T21/1540114 IAW FEDEX DWG SRZ-25-005. CAT A MAJOR REPAIR
- [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 FDEA202010152516](https://openairdocs.org/sdr/FDEA202010152516.md): Sliding Window · out of adjust · Oct 15, 2020 · N965FD · Boeing 757258 · Flight Compartment Windows
  > CAPTAIN SIDE WINDOW VERY DIFFICULT TO CLOSE. FOUND LATCH HANDLE DIFFICULT TO ROTATE AFT TO OPEN WINDOW. PERFORMED ADJUSTMENT TO LOWER LINK ARM, REF 757 AMM SUBTASK 56-11-02-825-013. OPERATIONS CHECKS GOOD. A/C OK TO CONTINUE FOR SERVICE.
- [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 FDEA202007171567](https://openairdocs.org/sdr/FDEA202007171567.md): Link Assy · out of adjust · Jul 17, 2020 · N965FD · Boeing 757258 · Flight Compartment Windows
  > CAPTAIN`S EMERGENCY ESCAPE WINDOW DOES NOT FUNCTION CORRECTLY. MUST TURN WINDOW CRANK IN ORDER TO UNLOCK WINDOW HANDLE. ADJUSTED THE L2 WINDOW LINK ARM IAW AMM 56-11-02-5, UP TO STEPS (5)I(2). CONTINUE WITH L2 WINDOW LINING INSTALLATION PER (5)F. IN
- [SDR FDEA2020072361527](https://openairdocs.org/sdr/FDEA2020072361527.md): Sliding Window · malfunctioned · Jul 16, 2020 · N965FD · Boeing 757258 · Flight Compartment Windows
  > CAPTAIN`S EMERGENCY ESCAPE WINDOW DOES NOT FUNCTION CORRECTLY. MUST TURN WINDOW CRANK IN ORDER TO UNLOCK WINDOW HANDLE. ADJUSTED THE L2 WINDOW LINK ARM IAW AMM 56-11-02-5 UP TO STEPS (5) I (2). CONTINUE WITH L2 WINDOW LINING INSTALLATION PER (5) F. INSTAL
- [SDR FDEA2019121323227](https://openairdocs.org/sdr/FDEA2019121323227.md): Oxygen Mask · damaged · Dec 12, 2019 · N965FD · Boeing 757258 · Passenger Oxygen System
  > MDIS 965 35-20 5884 12DEC19 MEM FACT U FOUND #1 OXYGEN MASK STORAGE BOX IN THE PASSANGER COURIER AREA BUSTED. ALL OXYGEN LEAKED OUT OF THE TOP OF THE BOX. R/I 12DEC19 10:24 MEM U REASON CODE: FAILED OPS CK. & REPLACED WITH SERVICABLE UNI
- [SDR FDEA201903040543](https://openairdocs.org/sdr/FDEA201903040543.md): Floorbeam · cracked · Mar 4, 2019 · N965FD · Boeing 757258 · Fuselage Main, Floor Beam
  > MAIN CABIN STUB FLOORBEAM IS CRACKED AT STA 580 LBL 45. COMPLIED WITH EA F-5310-T0345550 P1 TITLE: FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45.
- [SDR FDEA201903040542](https://openairdocs.org/sdr/FDEA201903040542.md): Floorbeam · corroded · Mar 4, 2019 · N965FD · Boeing 757258 · Fuselage Main, Floor Beam
  > CABIN STA 365.25 BETWEEN RBL 45.50 - 64.20 FLOORBEAM T CHORD CORRODED. EVALUATED PREVIOUS REPAIR ON STA 365,RBL 45.5 TO RBL 64.20 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101, DET. III, REMOVED PREVIOUS REPAIR AND ADDITIONAL. CUT OUT UPPER FLOORBEAM,
- [SDR FDEA201903040541](https://openairdocs.org/sdr/FDEA201903040541.md): Deck Plate · corroded · Mar 4, 2019 · N965FD · Boeing 757258 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR WEB AFT AREA MAIN CABIN FLOOR STA 1703 RBL 45. REMOVED CORROSION ON MAIN DECK PLATE STA 1703, RBL 45 IAW SRM 51-10-02-OG, EVALUATED DAMAGE AREA, ORIG. MAT =.071", REM. MAT =.048", MAT LOSS =.023" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A,

Next page: https://openairdocs.org/model/boeing-757-258/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 aircraft_model_key = '757258'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-258/reports

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