# Service difficulty reports: N910FD

A list on [N910FD](https://openairdocs.org/aircraft/N910FD.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 · 98 reports

- [SDR FDEA202605180620](https://openairdocs.org/sdr/FDEA202605180620.md): Cover Panel · chafed · May 18, 2026 · N910FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > REMOVE AND REPLACE THE P/N 141N8315-53 COVER PANEL PER PRODUCTION DRAWING REQUIREMENTS. AS STATED ON EA.# F-5310-T0378954AP2. REMOVED AND REPLACED THE P/N 14N8315-53 COVER PANEL PER PRODUCTION DRAWING REQUIREMENTS AS STATED ON E.A# F-5310-T0378954 A P2. BO
- [SDR FDEA202601130025](https://openairdocs.org/sdr/FDEA202601130025.md): Window · cracked · Jan 13, 2026 · N910FD · Boeing 757236 · Flight Compartment Windows
  > PILOT LEFT FRONT WINDOW ARCING IN LOWER LEFT CORNER WITH SPARK THEN CRACK ON OUTER PANE. LT PILOT WINDOW EICAS ON. C/W QRH. DECLARED EMERGENCY AND DIVERTED TO EWR. REMOVED AND REPLACED L1 WINDOW.
- [SDR FDEA202509041635](https://openairdocs.org/sdr/FDEA202509041635.md): Actuator · failed · Sep 4, 2025 · N910FD · Boeing 757236 · Landing Gear Actuator
  > GEAR DISAGREE AFTER TAKEOFF AND HANDLE RAISED. LEFT MAIN REMAINED DOWN. RAN QRH TO GET ALL GEAR DOWN ***EMERGENCY DECLARED*** PERFORM SYSTEM BIT TEST OF PSEU DISPLAY 999 AND 000. PERFORMED SENSOR AND TARGET TEST ON SYS 1 AND 2 AND BOTH READS FAR. R
- [SDR FDEA202506100993](https://openairdocs.org/sdr/FDEA202506100993.md): Adc · inoperative · Jun 10, 2025 · N910FD · Boeing 757236 · Air Data Computer
  > ON DEPARTURE THE LEFT ADC FAILED GIVING ERRONEOUS AIRSPEED AND ALTITUDE INDICATIONS ALONG WITH MULTIPLE FLAGS. WE WERE IN CRITICAL PHASE OF FLIGHT SO IMMEDIATELY CHECKED THE RIGHT PFD AND STANDBY TO DETERMINE THEY WERE WORKING PROPERLY. SWITCHED THE LEFT A
- [SDR FDEA202405270731](https://openairdocs.org/sdr/FDEA202405270731.md): Floorbeam · corroded · May 27, 2024 · N910FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEAM UPPER CHORD AT MAIN CABIN STA 344-346 BETWEEN LBL 7 - LBL 21, AFTER EVALUATION FOUND OUT OF LI
- [SDR FDEA202405090632](https://openairdocs.org/sdr/FDEA202405090632.md): Panel · cracked · May 9, 2024 · N910FD · Boeing 757236 · Passenger/Crew Doors
  > AFTER REMOVAL OF BODY HINGE TORQUE TUBE FROM L1 DOOR WAS FOUND GOUGE ON SKIN CAVITIY. COMPPLIED WITH EA# F-5310-T0378954 P1 WITH NO DEVIAITON AT FUSELAGE-MAINFRAME- SECTION 41 SUB FRAME INSTALLATION, L/H FWD NO. 1 DOOR COVER PANEL 141N8315-53. THIS IS A
- [SDR FDEA202405090631](https://openairdocs.org/sdr/FDEA202405090631.md): Floorbeam · gouged · May 9, 2024 · N910FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM FWD WEB AND BTM SURFACE OF UPPER T-CHORD AT STA 580 RBL35 HAVE GOUGE. THIS IS MAJOR REPAIR. ACOMPLISHED EA T F-5310-T0378982 P1 FUSELAGE- MAINFRAME-FLOOR BEAM WEB, STA 580 RBL 35, GOUGE REPAIR.
- [SDR FDEA202405050583](https://openairdocs.org/sdr/FDEA202405050583.md): Seat Track · damaged · May 5, 2024 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK APPROX STA 579, LBL 45.5 HAS BROKEN SCALLOP. EVALUATED DAMAGE ON SCALLOP OF THE SEAT TRACK AT BS 579 LBL 45.5, NO DAMAGE PERMITTED IAW B 757 SRM 53-00-52-1A, SHEET 1 FIG 101, REMOVED, LOCATED, DRILLED AND INSTALLED. SEAT TRACK SECTION
- [SDR FDEA202405030569](https://openairdocs.org/sdr/FDEA202405030569.md): Support Fitting · cracked · May 3, 2024 · N910FD · Boeing 757236 · Wing Miscellaneous Structure
  > AFTER INSPECTION AT L/H WING SKIN, DRAG FITTING O/B FOUND #5 AND #13 HOLE WITH CRACK INDICATION. ACCOMPLISHED EA # F-5730-T0378855 P1 TITLE: WINGS - PLATES AND SKINS - LH WING UPPER SKIN AT DRAG FITTING, HOLE #5 AND #13, CRACK REPAIRED *THIS EA DEVIATES FR
- [SDR FDEA202405020551](https://openairdocs.org/sdr/FDEA202405020551.md): Seat Track · cracked · May 2, 2024 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 880 LBL 58.22 CORNER OF SEAT TRACK IS BROKEN THIS IS A MAJOR REPAIR. EVALUATED CRACK ON SEAT TRACK AT STA 880 LBL 58.22, FOUND OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG 101 SHEET I, REMOVED, LOCATED, DRILLED NEW SEAT TRACK SECTI
- [SDR FDEA202405010549](https://openairdocs.org/sdr/FDEA202405010549.md): Seat Track · corroded · May 1, 2024 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO COMPARTMENT F. STA FROM 560 TO 640 LBL 24.75 SEAT TRACK WITH EVIDENCE CORROSION 4 SPOT THIS IS A MAJOR REPAIR, REMOVED CORROSION AT SEAT TRACK 4 PLACES ON BS 560 - 640, LBL 24.75 IAW B757 SRM 51-10-02-OG. FOUN TO BE OUT OF LIMITS IAW B 757 SRM 53
- [SDR FDEA202404300530](https://openairdocs.org/sdr/FDEA202404300530.md): Crease Beam · corroded · Apr 30, 2024 · N910FD · Boeing 757236 · Fuselage Main, Structure
  > MAIN CABIN CREASE BEAM FROM STA 756 TO STA 780, LBL 64.5 CORRODED. THIS IS A MAJOR REPAIR, REMOVED CORROSION AT CREASE BEAM I.A.W B 757 S.R.M 51-10-02-0G, OUT OF LIMITS I.A.W. B 757 S.R.M 53-30-13-1A FIG 101 SHEET 5, DETAIL VIII, REMOVED, FABRICATED AND I
- [SDR FDEA202404300529](https://openairdocs.org/sdr/FDEA202404300529.md): Seat Track · gouged · Apr 30, 2024 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT STA 1520-1540 LBL 58.22 SEAT TRACK CROWN AREA HAS A GOUGE. THIS IS A MAJOR REPAIR. INSPECTED SEAT TRACK BS 1520-1540 LBL 58.22 IAW B 757 SRM 53-00- 52-1A FIG 101 SHEET I, NO ALLOWABLE DAMAGE, REMOVED, LOCATED AND INSTALLED NEW SEAT T
- [SDR FDEA202404300528](https://openairdocs.org/sdr/FDEA202404300528.md): Seat Track · corroded · Apr 30, 2024 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > AFT. CARGO COMPARTMENT STA. BETWEEN 1220-1240 RBL 45.50 SEAT TRACK EVIDENCE CORROSION. THIS IS A MAJOR REPAIR REMOVED CORROSION IAW B 757 51-10-02-OG, OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG 101 DETAIL VII, REMOVED, LOCATED AND INSTALLED NEW SEAT TRACK
- [SDR FDEA202401040037](https://openairdocs.org/sdr/FDEA202401040037.md): Unknown · unknown · Jan 4, 2024 · N910FD · Boeing 757200 · Door Warning System
  > DURING TAKEOFF ROLL AT 75KTS AND 160.0LBS THE MAIN CARGO DOOR WARNING LIGHTS, TONES AND EICAS ILLUMINATED. TAKEOFF WAS REJECTED AND ASSOCIATED QRH CHECKLISTS WERE ACCOMPLISHED.
- [SDR FDEA202304070603](https://openairdocs.org/sdr/FDEA202304070603.md): Slide · loose · Apr 7, 2023 · N910FD · Boeing 757200 · Passenger/Crew Doors
  > DURING SERVICE CHECK FOUND RIGHT PASSENGER ACCES DOOR LIFE RAFT LOOSE AND GIRT BAR OUT OF PLACE. UPDT 07APR23 06:51 BCN U AMM 25-66-01-4 NO DAMAGE OBSERVED, ONLY LIFE RAFT OUT OF PLACE. STOWED RAFT IN CARGO AREA INSIDE CARGO NET WITH SAFETY LOCKING PIN
- [SDR FDEA202211292854](https://openairdocs.org/sdr/FDEA202211292854.md): Duct · damaged · Nov 29, 2022 · N910FD · Boeing 757236 · Engine Thrust Reverser
  > UPON DEPLOYING THE REVERSERS ON LANDING, MANY EICAS INDICATIONS APPEARED FOR THE L HYD SYSTEM. SPOILERS, LT HYD QTY, RUDDER RATIO, & LT REVERSER CAUTION LIGHTS AND THE LT SYSTEM HYD QTY WAS.10. INSTALLED NEW C-DUCT PER WC7800000-02-02 AND AMM 78-31-20-4-4
- [SDR FDEA202106011427](https://openairdocs.org/sdr/FDEA202106011427.md): Control Cable · tangled · Jun 1, 2021 · N910FD · Boeing 757236 · Landing Gear Steering System
  > TILLER BINDING WHEN USED TO TURN. WHEN USING PEDALS, NOSE WHEEL DOES NOT RESPOND. STEERING RT, WHEN APPLYING LT RUDDER, TOOK NEARLY FULL DEFLECTION LT BEFORE NLG CAUGHT & STARTED A SEMI VIOLENT LT TURN. IAW AMM 32-51-00-5-3. CHECKED CABLE TENSION NGPPA, NGP
- [SDR FDEA202008272037](https://openairdocs.org/sdr/FDEA202008272037.md): Latch · damaged · Aug 27, 2020 · N910FD · Boeing 757236 · Auxiliary Power Unit (APU) Doors
  > R/H APU DOOR 316AR AFT 3 LATCHES HAVE DAMAGE ON LATCH CUT-OUTS REPAIRED R/H APU DOOR 316AR AFT 3 LATCHES CUTOUTS IAW FEDEX EA: F-5240-T0355591 P1 TITLE:DOORS- SERVICE- R/H APU DOOR LATCH CUTOUTS- CRACKED
- [SDR FDEA2020081401874](https://openairdocs.org/sdr/FDEA2020081401874.md): Strap · damaged · Aug 4, 2020 · N910FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > STABILIZER STRAP BSTA 365-377 RBL 24 FOUND DAMAGED REPAIRED DAMAGE ON STABILIZER STRAP AT BSTA 365-377 RBL 24 IAW SRM 53-10-51-2R REPAIR 1. STABILIZER STRAP RE-PROTECTED IAW SRM 51-21-00
- [SDR FDEA2020081891920](https://openairdocs.org/sdr/FDEA2020081891920.md): Floor Panel · delaminated · Jul 29, 2020 · N910FD · Boeing 757236 · Fuselage Floor Panel
  > FLOOR PANEL 221 MBF TOP COAT DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R.
- [SDR FDEA202007272006](https://openairdocs.org/sdr/FDEA202007272006.md): Seat Track · corroded · Jul 27, 2020 · N910FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > EVALUATE CORROISION ON SEAT TRACK LBL 45.50 STA 1180-1200 AS INDICATED EVALUATED CORROSION ON SEAT TRACK AT BS 1180-1200 LBL 45.50 IAW SRM 53-00-52-1A FIG 101 AND FOUND CORROSION OUTSIDE SRM LIMITS. FABRICATED AND REPLACED SEAT TRACK AT BS 1180-1200 LBL45.
- [SDR FDEA2020083171935](https://openairdocs.org/sdr/FDEA2020083171935.md): Floorbeam · corroded · Jul 27, 2020 · N910FD · Boeing 757236 · Fuselage Main, Floor Beam
  > CORROISION ON FLOOR BEAM AT STA 1200 LBL 2 TO LBL 68 EVALUATED UPPER SURFACE OF FLOOR BEAM AT BSTA 1200 LBL2 TO LBL68 AND FOUND CORROSION TO BE GREATER THAN 10% OF MATERIAL THICKNESS. REPAIRED UPPER SURFACE OF FLOOR BEAM AT STA 1200 LBL 2 TO LBL 68 IAW SR
- [SDR FDEA2020082071935](https://openairdocs.org/sdr/FDEA2020082071935.md): Floorbeam · corroded · Jul 27, 2020 · N910FD · Boeing 757236 · Fuselage Main, Floor Beam
  > CORROISION ON THE FLOORBEAM AT BS 1200, LBL 2 TO LBL 68. EVALUATED UPPER SURFACE OF THE FLOORBEAM AND FOUND TO BE GREATER THAN 10% OF MATERIAL THICKNESS. REPAIRED THE UPPER SURFACE OF THE FLOORBEAM IAW SRM 53-00-51-2R, REPAIR 8.
- [SDR FDEA202007242023](https://openairdocs.org/sdr/FDEA202007242023.md): Turbine Case · worn · Jul 24, 2020 · N910FD · Boeing 757236 · Turbine Section
  > ENGINE 2 TURBINE CASE WEAR 4.5 INCH BELOW OB SIDE TR HOLD OPEN BRACKET. REPAIRED NR 2 ENGINE TURBINE CASE, IAW FEDEX EA: F-7257-T0355605A P1 TITLE: ENGINE-TURBINE CASES/FRAMES-ENGINE NR 2 TURBINE CASE WEAR.
- [SDR FDEA202007242002](https://openairdocs.org/sdr/FDEA202007242002.md): Attach Bracket · cracked · Jul 24, 2020 · N910FD · Boeing 757236 · Nacelle/Pylon, Main Frame
  > LT SAILBOAT OUTBOARD ATTACHING BRACKET CRACKED. REMOVED LT SAILBOAT OUTBOARD ATTACHING BRACKET IAW SRM 51-40-02. FABRICATED LT SAILBOAT OUTBOARD ATTACHING BRACKET IAW BOEING DRAWING 313N5052 AND FEDEX GMM 7-0-1001. INSTALLED LT SAILBOAT OUTBOARD ATTACHING B
- [SDR FDEA2020083141932](https://openairdocs.org/sdr/FDEA2020083141932.md): Bulkhead · cracked · Jul 24, 2020 · N910FD · Boeing 757236 · Nacelle/Pylon, Main Frame
  > ENG 2 BULK HEAD AFT OF COMPRESSOR FAIRING LH SIDE 10 O CLOCK POSITION IS CRACKED REPAIRED #2 ENG BULKHEAD AFT OF COMPRESSOR FAIRING L/H SIDE 10 O CLOCK POSITION IAW AMM 72-03-01-8-4 REPAIR 9
- [SDR FDEA2020082041931](https://openairdocs.org/sdr/FDEA2020082041931.md): Bulkhead · cracked · Jul 24, 2020 · N910FD · Boeing 757236 · Engine (Turbine/Turboprop)
  > ENG 2 BULK HEAD AFT OF COMPRESSOR FAIRING LH SIDE 10 O CLOCK POSITION IS CRACKED REPAIRED #2 ENG BULKHEAD AFT OF COMPRESSOR FAIRING L/H SIDE 10 O CLOCK POSITION IAW AMM 72-03-01-8-4 REPAIR 9
- [SDR FDEA202007232005](https://openairdocs.org/sdr/FDEA202007232005.md): Fill Port · corroded · Jul 23, 2020 · N910FD · Boeing 757236 · Fuel Storage
  > RT OVERWING FILL PORT FAILED BONDING CHECK, EVALUATE STRUCUTRE UPON REMOVAL OF FILL PORT. EVALUATED RT OVERWING FILL PORT STRUCTURE IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3 AND FOUND CORROSION OUTSIDE SRM LIMITS. REPAIRED RT OVERWING FILL PORT IAW FEDEX EA: F-5
- [SDR FDEA202007232003](https://openairdocs.org/sdr/FDEA202007232003.md): Fill Port · corroded · Jul 23, 2020 · N910FD · Boeing 757236 · Fuel Storage
  > LT OVERWING FILL PORT FAILED BONDING CHECK, EVALUATE STRUCTURE UPON REMOVAL OF FILL PORT. EVALUATED LT OVERWING FILL PORT STRUCTURE IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, AND FOUND CORROSION OUTSIDE SRM LIMITS. REPAIRED LT OVERWING FILL PORT IAW FEDEX EA: F-
- [SDR FDEA2020083131937](https://openairdocs.org/sdr/FDEA2020083131937.md): Floor Support · corroded · Jul 23, 2020 · N910FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT FLOOR INTERCOSTAL SUPPORT CORRODED BSTA 1661 BSTA 1681 LBL 53.5 REMOVED AFT FLOOR INTERCOSTAL SUPPORT IAW SRM 51-40-02. FABRICATED NEW SUPPORT IAW ST MOBILE AREOSPACE DRAWING 11864179-9 AND FEDEX GMM 7-0-1001. SUPPORT INSTALLED IAW SRM 51-40-02.
- [SDR FDEA2020082031937](https://openairdocs.org/sdr/FDEA2020082031937.md): Floor Support · corroded · Jul 23, 2020 · N910FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT CORRODED BS 1661 - 1681, LBL 53.5. REMOVED THE AFT FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED A NEW FLOOR SUPPORT IAW DRAWING 11864179-9, AND GMM 7-0-1001. THE FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02.
- [SDR FDEA201906031209](https://openairdocs.org/sdr/FDEA201906031209.md): Battery · discharged · Jun 3, 2019 · N910FD · Boeing 757236 · Emergency Lighting
  > DURING SERVICE CHECK DOOR L1 EMERGENCY TEST FAIL BATTERY DOES NOT MAINTAIN THE CHARGE LOW CAPACITY. DOOR L1 EMERGENCY BATTERY ASSEMBLY REPLACED PER AMM 33-51-07-20 REV 123.18 SATIS.
- [SDR FDEA201905071014](https://openairdocs.org/sdr/FDEA201905071014.md): Line · damaged · May 7, 2019 · N910FD · Boeing 757236 · Fire Bottle, Portable
  > MDIS 910 26-22 9839 07MAY19 VIE OPEN U LOGPAGES:3025198 RAMP REPORTED BY INBOUND HAZCAN LINES IN MDC BENT AND RIPPED OFF. UPDT 07MAY19 19:08 VIE DG FIRE EXTINGUSHERS DEFERRED PER MEL 26-26-01-03 AND COMPLIED WITH EA F-2622-T0346866 PART 1 DAM
- [SDR FDEA2018090542345](https://openairdocs.org/sdr/FDEA2018090542345.md): Hinge Fitting · cracked · Sep 4, 2018 · N910FD · Boeing 757236 · Engine Thrust Reverser
  > NR 1 ENG O/B THRUST REVERSER AFT HINGE FITTING AFT UPR FASTENER HOLE CRACKED. COMPLIED WITH EA F-5450-T0341855, AFT UPPER BOLT HOLES CRACKED C/T SKIN. REPAIRED THE NR 1 ENG O/B THRUST REVERSER AFT HINGE FITTING AFT UPR FASTENER HOLE. MAJOR REPAIR IAW GMM 6-2-1
- [SDR FDEA2018090542344](https://openairdocs.org/sdr/FDEA2018090542344.md): Hinge Fitting · cracked · Sep 4, 2018 · N910FD · Boeing 757236 · Engine Thrust Reverser
  > NR 1 ENG I/B THRUST REVERSER AFT HINGE FITTING AFT UPR FASTENER HOLE CRACKED. COMPLIED WITH EA F-5450-T0341855, AFT UPPER BOLT HOLES CRACKED C/T SKIN. REPAIRED THE NR 1 ENG I/B THRUST REVERSER AFT HINGE FITTING AFT UPR FASTENER HOLE. MAJOR REPAIR IAW GMM 6-2-1
- [SDR FDEA201807161719](https://openairdocs.org/sdr/FDEA201807161719.md): Crank Assy · worn · Jul 16, 2018 · N910FD · Boeing 757236 · Passenger/Crew Doors
  > SLIDE ON DOOR 1R FAILS ARMING/ DISARMING TEST (AMM 52-11-00-216-025.) SLIDE ARMING HANDLE DOES NOT MOVE FREELY. R&R WORN CRANK ASSY.
- [SDR FDEA2018062971590](https://openairdocs.org/sdr/FDEA2018062971590.md): Girt Bar · out of adjust · Jun 27, 2018 · N910FD · Boeing 757236 · Emergency Equipment
  > NR 2 SLIDE ACTIVATION LEVER DIFFICULT TO SLIDE. ADJUSTED THE GIRT BAR MECHANISM IAW AMM 52-11-25-5.
- [SDR FDEA201801040024](https://openairdocs.org/sdr/FDEA201801040024.md): Cabin Pressure · malfunctioned · Jan 4, 2018 · N910FD · Boeing 757236 · Cabin Pressure Control System
  > CABIN ALTITUDE MASTER WARNING IN FLIGHT AT FL280, WITH ONLY RIGHT PACK OPERATING. CABIN ALTITUDE READ 10,000 FT. DECENDED TO FL 200 AND CABIN DECENDED TO 8,000 FT. MODE SELECT WAS ON AUTO 1. COMPLIED WITH FIM 21-30 FAULT TREE 802, AND PERFORMED A LEFT A
- [SDR FDEA201712013330](https://openairdocs.org/sdr/FDEA201712013330.md): Valve · inoperative · Dec 1, 2017 · N910FD · Boeing 757236 · Cabin Cooling System
  > NOTE: CAPTAIN REPORT TO GOC & MOCC = EMERGENCY LANDING TO STN DUE TO THE LOSS OF THE CABIN PRESSURIZATION PDIS 910 21-30 8396 01DEC17 STN CABIN ALTITUDE WARNING @ FL280 QRH COMPLIED WITH. CABIN @10000 FEET. ACCOMPLISHED FIM FAULT TREE 80
- [SDR FDEA201609013099](https://openairdocs.org/sdr/FDEA201609013099.md): Wire · shorted · Sep 1, 2016 · N910FD · Boeing 757236 · Landing Gear System Wiring
  > FLIGHT TEST, FTAM 4.73 ALT GEAR EXTENSION, ALT GEAR EXTEND SWITCH SELECTED DOWN THE ALT GEAR C/B POPPED, 5-5, C/B RESET AFTER 2 MINUTES. ALT GEAR EXTEND SWITCH RESELECTED FOR MORE THAN 2 SEC ALT GEAR DID NOT EXTEND. C/B, F-5, STAYED RESET. TROUBLESHOOTING A
- [SDR FDEA201609013100](https://openairdocs.org/sdr/FDEA201609013100.md): Unknown · malfunctioned · Sep 1, 2016 · N910FD · Boeing 757236 · Landing Gear Retraction/Extension System
  > FLIGHT TEST, FT AM 4.73 ALT GEAR EXTENSION, ALT GEAR EXTEND SWITCH SELECTED DOWN THE ALT GEAR C/B POPPED, 5-5. C/B RESET AFTER 2 MINUTES. ALT GEAR EXTEND SWITCH RESELECTED FOR MORE THAN 2 SECONDS, ALT GEAR DID NOT EXTEND. C/B, F-5, STAYED RESET.
- [SDR FDEA201608252975](https://openairdocs.org/sdr/FDEA201608252975.md): Wedge · delaminated · Aug 25, 2016 · N910FD · Boeing 757236 · Leading Edge Devices
  > DELAMINATION ON T/E WEDGE OF L/E SLAT NR 5. REPAIRED DAMAGE TO NR 5 L/E SLAT AT INBD END OF T/E WEDGE IAW SRM 51-70-10, REPAIR 4 AND EA F-5750-T0327454.
- [SDR FDEA201608102859](https://openairdocs.org/sdr/FDEA201608102859.md): Skin · corroded · Aug 10, 2016 · N910FD · Boeing 757236 · Leading Edge Devices
  > NR 4 SLAT LOWER SURFACE HAS CORROSION ON SKIN, ADJACENT TO OT/BD AUX TRACK WHERE LOWER COMPOSITE SEAL IS ATTACHED. SLAT NR 4 REPAIRED ON EA F-5750-T0327481, P1 WO 00067073, WRI 57507169 AND SNMR N00400.
- [SDR FDEA201608102858](https://openairdocs.org/sdr/FDEA201608102858.md): Skin · dented · Aug 10, 2016 · N910FD · Boeing 757236 · Leading Edge Devices
  > NR 6 SLAT DENTED ON LEADING EDGE NOSE SKIN EXTERIOR AT MID SPAN. SLAT REPAIRED IAW SRM 57-43-01 FIG 201 REPAIR 1 REV 118.
- [SDR FDEA201608102855](https://openairdocs.org/sdr/FDEA201608102855.md): Skin · delaminated · Aug 10, 2016 · N910FD · Boeing 757236 · Trailing Edge Flaps
  > SMALL AREA OF DELAMINATION ON LOWER SURFACE OF LT OTBD AFT FLAP. REPAIRED LOWER SURFACE AFT FLAP IAW SRM 57-53-01 IDENTIFICATION 1, FIGURE 1, SHEETS 1, 10, 11 & 13, SRM 57-53-01 REPAIR 1, FIG 201, SHEET 1, 3 & 5, SRM 51-70-04, GENERAL & PARA 5A, FIG 5.
- [SDR FDEA201608102853](https://openairdocs.org/sdr/FDEA201608102853.md): Skin · dented · Aug 10, 2016 · N910FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT INBD MAIN FLAP HAS A DENT ON UPPER SURFACE. DENT FOUND OUTSIDE LIMITS DUE TO DELAMINATION IAW SRM 57-53-01. DENT REPAIRED ON RT INBD MAIN FLAP UPPER SURFACE 108" FROM INBD EDGE & 20" FROM T/E IAW SRM 51-40-10, REPAIR 4 AND EA F-5750-T0327649.
- [SDR FDEA201608102852](https://openairdocs.org/sdr/FDEA201608102852.md): Skin · dented · Aug 10, 2016 · N910FD · Boeing 757236 · Trailing Edge Flaps
  > DENT ON RT INBD MAIN FLAP LOWER SURFACE ABOVE NR 6 FLAP TRACK FAIRING. DENT FOUND OUTSIDE LIMITS IAW SRM 57-53-01. REPAIRED RT INBD MAIN FLAP LOWER SURFACE, 63" FROM OTBD EDGE AND 20" FROM T/E IAW SRM 51-70-10. REPAIR 4 AND EA F-5750-T0327650.
- [SDR FDEA201608032823](https://openairdocs.org/sdr/FDEA201608032823.md): Pump · obstructed · Aug 3, 2016 · N910FD · Boeing 757236 · Fuel Boost Pump
  > DURING INSPECTION OF RT WING TANK A FOREIGN OBJECT WAS DETECTED. A PARTIALLY DISINTEGRATED CLOTH, RAG WAS IDENTIFIED COVERING, BLOCKING THE AFT FUEL PUMP AT POSITION WS 231.5. AN EVALUATION OF THE SYSTEM FOR CONTAMINATION TO BE PERFORMED IAW SNRM N00480, W/O
- [SDR FDEA201608022774](https://openairdocs.org/sdr/FDEA201608022774.md): Regulator · failed · Aug 2, 2016 · N910FD · Boeing 757236 · Extinguishing System
  > AFT CARGO FIRE EXTINGUISHING DISCHARGE SYSTEM FAILED FUNCTIONAL CHECK. REPLACED AFT CARGO FIRE EXTINGUISHER REGULATOR IAW AMM 26-23-03-4. PERFORMED SYS TEST OF AFT CARGO METERED DISCHARGE LINES IAW AMM 26-23-00-5.

Next page: https://openairdocs.org/aircraft/N910FD/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 = 'N910FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910FD/reports

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