# Service difficulty reports: Boeing 757-236

A list on [Boeing 757-236](https://openairdocs.org/model/boeing-757-236.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 51 · 2,542 reports

- [SDR FDEA202610201632](https://openairdocs.org/sdr/FDEA202610201632.md): Switch · inoperative · Oct 20, 2026 · N960FD · Boeing 757236 · Emergency Lighting
  > WHEN EMERGENCY LIGHT SWITCH WAS TURNED OFF, AFTER SHUTDOWN, THE UNARMED LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED UNARMED LIGHT HOUSING ASSY IAW SWPM20-84-18. OPS CHECKED NORMAL, UNARMED ANNUNCIATOR LIGHT REMAINS ILLUMINATED WITH EMERGENCY EXIT SWITCH
- [SDR FDEA202610191605](https://openairdocs.org/sdr/FDEA202610191605.md): Attach Angle · damaged · Oct 19, 2026 · N946FD · Boeing 757236 · Trailing Edge Flaps
  > R/H WING INBD T/E FLAP, OUTBD TRACK FAIRING 672HB ATTACH ANGLE HAS ELONGATED HOLES. PERFORMED REPAIR IAW B757-200 SRM 57-53-02-2R FIG 202 REPAIR 3 SHEET 1 AND 2. REMOVED AND REPLACED FITTINGS P/N 113N2304-10 AND 113N2306-1 IAW SRM 51-40-02. THIS CATAGORY B
- [SDR FDEA202610151596](https://openairdocs.org/sdr/FDEA202610151596.md): Panel · dented · Oct 15, 2026 · N946FD · Boeing 757236 · Vertical Stabilizer, Plate/Skin
  > DENT AT VERTICAL STAB LH SIDE COMPOSITE PANEL FWD OF FRONT SPAR LWR AREA BETWEEN FSS 119 TO FSS 170. REPAIRED DENT AT VERTICAL LH SIDE TORQUE BOX COMPOSITE PANEL LWR AREA BETWEEN FSS 119 TO FSS 170 IAW B757-200 SRM 55-30-01-2R, REPAIR 5 FIG 201, SHEET 1 M
- [SDR FDEA202610061485](https://openairdocs.org/sdr/FDEA202610061485.md): Floorbeam · corroded · Oct 6, 2026 · N946FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR STRUCTURE CROSSBEAM HAS CORROSION AT THE UPPER FWD FLANGE AT BS 377 FROM LBL 26 TO LBL 56. REPAIRED CROSSBEAM PER EA F-5310-T0388790 P1, FUSELAGE - MAIN FRAME - CORROSION REPAIR, SECTION 41 MAIN DECK FLOOR BEAM, UPPER FORWARD FLANGE STA 377
- [SDR FDEA202610051480](https://openairdocs.org/sdr/FDEA202610051480.md): Battery · inoperative · Oct 5, 2026 · N960FD · Boeing 757236 · Emergency Lighting
  > DURING PRE-FLIGHT TEST OF EMERGENCY LIGHTS AND FOLLOW UP OPERATION, THE RIGHT SIDE LIGHTS DID NOT REMAIN ILLUMINATED FOR MORE THAN A FEW SECONDS. THE LEFT SIDE WAS NORMAL. AMM 33-51-07-2 REPLACED M730 BATTERY PACK: SOURCE MANUFACTURING, OPS NORMAL. OK
- [SDR FDEA202609301456](https://openairdocs.org/sdr/FDEA202609301456.md): Strap · corroded · Sep 30, 2026 · N946FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > APU AIR INLET DOOR ASSY ATTACHMENT CUT OUT FWD FRAME CORRODED STA 1787. REMOVED AND REPLACED THE ANGLE. PERFORMED REPAIR ON INITIAL MIDDLE STRAP BS 1825 BETWEEN STR 3R - 6R IAW SRM 53-80-15. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-80-15-1A. MAJOR REPAI
- [SDR FDEA202609291452](https://openairdocs.org/sdr/FDEA202609291452.md): Seat Track · corroded · Sep 29, 2026 · N946FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL SPOTS OF CORROSION AT CABIN SEAT TRACK FLANGE BS 900 TO 1020, RBL 58. ACCOMPLISHED SEAT TRACK REPAIR OPTION 1 PER SRM 53-00-52-2R FIG 201. MAJOR REPAIR.
- [SDR FDEA202609231420](https://openairdocs.org/sdr/FDEA202609231420.md): Wedge · dented · Sep 23, 2026 · N946FD · Boeing 757236 · Leading Edge Devices
  > NUMBER 7 SLAT UPPER SURFACE T/E WEDGE HAD A DENT AT OSS 390 AND 6" FWD OF AFT END. REPAIRED NR 7 SLAT UPPER SURFACE TRAILING EDGE WEDGE DENT IAW SRM 51-70-10-2R, FIG 201, SHEET 3. MAJOR REPAIR.
- [SDR FDEA202609231418](https://openairdocs.org/sdr/FDEA202609231418.md): Crease Beam · corroded · Sep 23, 2026 · N946FD · Boeing 757236 · Fuselage Main, Structure
  > MAIN CABIN RT BS 610, RBL 62., FLOOR SUPPORT FOR PANEL 232MIF HAD SURFACE CORROSION AROUND SCREW HOLES. REPAIRED MAIN DECK FLOOR STRUCTURE CREASE BEAM INBD CHORD AT RBL 62. BETWEEN BS 540 TO BS 660 IAW SRM 53-00-13-2R, FIG 201, SHEET 1 - 3.
- [SDR FDEA202608281249](https://openairdocs.org/sdr/FDEA202608281249.md): Lamp · inoperative · Aug 28, 2026 · N954FD · Boeing 757236 · Emergency Lighting
  > FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IN FLIGHT DECK EMERGENCY LIGHT IAW AMM 33-51-09-3. OPS CHKD SERVICEABLE.
- [SDR FDEA202608181146](https://openairdocs.org/sdr/FDEA202608181146.md): Adc · inoperative · Aug 18, 2026 · N978FD · Boeing 757236 · Airspeed/Mach Indicator
  > UPON ROTATION FOS AIRSPEED TAPE WENT AWAY. RECEIVED IAS DISAGREE EICAS. CAPTAIN FLIGHT DIRECTOR DROPPED PITCH INDICATOR. RECEIVED RUDDER RATIO AND MACH/SPD TRIM EICAS MESSAGES. ELEV ASYM STATUS MESSAGE. EMERGENCY DECLARED. AMM: 34-12-01-4 FIM: 27-09 TRE
- [SDR FDEA202607291055](https://openairdocs.org/sdr/FDEA202607291055.md): Electronic Unit · faulted · Jul 29, 2026 · N979FD · Boeing 757236 · Trailing Edge Flap Control System
  > AFTER SELECTING FLAPS 30, WE RECEIVED A TE FLAP DISAGREE MESSAGE. WE EXECUTED A GO AROUND AND DECLARED AN EMERGENCY. AFTER RUNNING THE QRH FOR FLAPS GREATER THAN 20 (INDICATING ROUGHLY 23 DEGREES WITH FLAPS STILL SELECTED AS 30) WE LANDED AND TAXIED TO TH
- [SDR FDEA202607150926](https://openairdocs.org/sdr/FDEA202607150926.md): Flap System · unknown · Jul 15, 2026 · N979FD · Boeing 757236 · Trailing Edge Flap Control System
  > WHILE ON APPROACH TO MEM, GOING FROM FLAPS 20 TO FLAPS 25 RECEIVED EICAS MSG FOR TE FLAP DISAGREE. RAN QRH DECLARED EMERGENCY LANDED WITH NO OTHER ISSUES. EMERGENCY DECLARED AMM: 27-51-00-5, AMM: 12-13-06-3, AMM: 12-21-09-3, FIM: 27-51-00. PERFOR
- [SDR FDEA202607070848](https://openairdocs.org/sdr/FDEA202607070848.md): Seat Track · cracked · Jul 7, 2026 · N979FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK LEFT O/B SEAT TRACK DAMAGED AT STATION 579. ACFT ARRIVED AT INDIANAPOLIS EAST HANGER FOR A DROP-IN MAINTENANCE VISIT DUE TO A CRACK ON THE SEAT TRACK FLANGE AT LBL 45 AND STA 580 (P/N 143N5110-1). THE DAMAGE CANNOT BE REPAIRED PER SRM 53-00-
- [SDR FDEA202607010826](https://openairdocs.org/sdr/FDEA202607010826.md): Seat Track · cracked · Jul 1, 2026 · N979FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CURRENT DROP-IN VISIT IN IND, THE FLOOR BEAM SEGMENT AT STA 580 AND LBL 45 WAS FOUND CRACKED UNDER THE LBL 45 SEAT TRACK. CREATED EA E.A.#: F-5310-T0387857 TITLE: FUSELAGE - MAINFRAME - STA 580 AND LBL 45 STUB FLOOR BEAM CRACKED REPAIR PER DRAWING
- [SDR FDEA202607010823](https://openairdocs.org/sdr/FDEA202607010823.md): Frame · cracked · Jul 1, 2026 · N979FD · Boeing 757236 · Fuselage Main, Frame
  > [MAIN DECK STUB FRAME IS CRACKED AT UPPER FLANGE AT 580 LBL 45.50 MAIN DECK STUB FRAME CRACKED AT UPPER FLANGE STA 580 LBL 45.50, 2026-07-01] ORG WRI 979 25-50 0563 MAIN CARGO DECK LEFT O/B SEAT TRACK DAMAGED AT STATION 579. LOCK ID B579. REPLACED SEGME
- [SDR FDEA202605180621](https://openairdocs.org/sdr/FDEA202605180621.md): Slide · faulted · May 18, 2026 · N954FD · Boeing 757236 · Escape Slide
  > DURING PREFLIGHT FOUND L1 DOOR SLIDE WILL NOT ENGAGE. ADJUSTED LT MAIN ENTRY DOOR GRIT BAR SLIDER IAW AMM 52-11-25-5. OPS CHECKED GOOD.
- [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 FDEA202605110582](https://openairdocs.org/sdr/FDEA202605110582.md): Reservoir · failed · May 11, 2026 · N949FD · Boeing 757236 · Passenger/Crew Doors
  > L1 PASSENGER DOOR ASSIST RESERVOIR DEPLETED TO ZERO. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER RESERVIOR CYLINDER IAW AMM 52-11-30-4. NO DDG PROCEDURES TO REVERSE, PLACARD PULLED MEL IS CLEARED.
- [SDR FDEA202604300522](https://openairdocs.org/sdr/FDEA202604300522.md): Transition Panel · tripped · Apr 30, 2026 · N946FD · Boeing 757236 · Trailing Edge Flap Control System
  > GOT TE FLAP DISAGREE WHEN MOVING THE FLAP HANDLE FROM 20 TO 25. RAN QRH, AND LANDED WITH ALTERNATE FLAPS 20. EMERGENCY DECLARED RESET LH OUTBOARD TRANSMISSION IAW 27-51-808
- [SDR FDEA202604140446](https://openairdocs.org/sdr/FDEA202604140446.md): Bulb · failed · Apr 14, 2026 · N950FD · Boeing 757236 · Emergency Lighting
  > DURING MX PRE-FLIGHT EMERGENCY LIGHT TEST, FOUND L1 DOOR EXIT SIGN SEEMS DIM. REMOVED AND REPLACED 9 FAULTY BULBS AT THE L1 EXIT SIGN IAW AMM 33-51-01-2. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202604070403](https://openairdocs.org/sdr/FDEA202604070403.md): Transmission · tripped · Apr 7, 2026 · N954FD · Boeing 757236 · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE ON APPROACH AFTER SELECTING FLAPS 1. COMPLIED WITH QRH. EMERGENCY DECLARED. FIM 27-51-00 FT 808 TROUBLESHOT IAW WITH FIM 27-51-00 FT 808. FOUND LEFT INBOARD DRIVE TRANSMISSION FOR INBOARD FLAPS OVERLOAD INDICATOR EXTENDED. RESET INDIC
- [SDR FDEA202603230367](https://openairdocs.org/sdr/FDEA202603230367.md): Flap System · malfunctioned · Mar 23, 2026 · N949FD · Boeing 757236 · Trailing Edge Flap Control System
  > WHEN MOVING FLAPS FROM 20 TO 25 POSITION AND APPROXIMATELY 155 KTS~WE RECEIVED TE FLAP DISAGREE. EXECUTED GO AROUND. FOLLOWED QRH AND LANDED FLAPS 20 USING ALT FLAP SYSTEM. AMM: 27-51-00-5 AMM: 05-51-08-2 NO CURRENT FOUND, C/W OVER SPEED INSPECTION
- [SDR FDEA202603170355](https://openairdocs.org/sdr/FDEA202603170355.md): Seat Track · damaged · Mar 17, 2026 · N979FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGE TO LOBES ONLY AND WITH IN DEFERAL LIMITS WITH NO EQUIPMENT INSTALLED WITHIN 3 INCHES IAW SRM 53-00-52-1A FIG 101 DETAIL XI SHEET 6. CREATED E.A.#: F-5310-T0387768P1 TITLE: FUSELAGE - MAINFRAME - MAIN CARGO COMPARTMENT SEAT TRACK SPLICE
- [SDR FDEA202603060319](https://openairdocs.org/sdr/FDEA202603060319.md): Door · binding · Mar 6, 2026 · N954FD · Boeing 757236 · Passenger/Crew Doors
  > LEFT ENTRY DOOR HARD TO ARM/DISARM. OPERATED L1 ENTRY DOOR SEVERAL TIMES IAW AMM REF 52-11-00-6, NO DEFECTS WERE NOTED. ACFT OK FOR RETURN TO SERVICE.
- [SDR FDEA202602270288](https://openairdocs.org/sdr/FDEA202602270288.md): Handle · malfunctioned · Feb 27, 2026 · N978FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR WOULD NOT DIS-ARM UPON BLOCK- IN KEWR. DOOR ARM/DE-ARM HANDLE WILL ONLY MOVE HALF WAY TO THE DE-ARM POSITION, SLIDE LIGHT IS OUT, BUT DE-ARM HANDLE ONLY MOVES HALF WAY AND THE KNUCKLE BUSTER IS NOT FULLY RETRACTED LIKE IT SHOULD BE. AMM 25-66-1
- [SDR FDEA202601290113](https://openairdocs.org/sdr/FDEA202601290113.md): Snubber · failed · Jan 29, 2026 · N979FD · Boeing 757236 · Passenger/Crew Doors
  > THE L1 DOOR WILL NOT OPEN COMPLETELY. R & R THE L1 DOOR ROTARY SNUBBER UP TO BUT NOT INCLUDING STEP 3.G.(12) IAW AMM 52-11-10-4. COMPLETED INSTALLATION OF L1 DOOR, PNEUMATIC LINE. RECONNECTED AND SAFETY PIN REMOVED. INSTALLATION OF L1 ROTARY SNUBBER PER
- [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 FDEA202601090015](https://openairdocs.org/sdr/FDEA202601090015.md): Bulb · failed · Jan 9, 2026 · N949FD · Boeing 757236 · Emergency Lighting
  > DURING MX PRE-FLIGHT FOUND L1 EMERGENCY EXIT SIGN BARELY LIT. FOUND L1 EMERGENCY EXIT SIGN HAS 11 BULBS INOP. REMOVED AND REPLACED 11 FAULTY BULBS IAW AMM 33-51-01-2. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202512172257](https://openairdocs.org/sdr/FDEA202512172257.md): Bolt · misinstalled · Dec 17, 2025 · N979FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR WILL ONLY OPEN HALF WAY. AMM: 52-11-08-4 PUT A/C BACK IN NORMAL CONFIG. OPENED AND CLOSED L1 DOOR MULTIPLE TIMES IAW AMM 52-11-00-2 AND FOUND HOLD OPEN LOCK LEVER CONTACTING TRIGGER CATCH BOLT. FOUND TRIGGER CATCH BOLT INSTALLED INCORRECTLY IAW AMM
- [SDR FDEA202510222074](https://openairdocs.org/sdr/FDEA202510222074.md): Skin · corroded · Oct 22, 2025 · N978FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE POSSIBLE CORROSION AT LAP JOINT BS 1664 BTW S25R-S26R CORROSION OUT OF LIMITS AT AFT FUSELAGE LAP JOINT STA 1664 BTW STR 25R-STR26R WAS REPAIRED IAW EA F-5330-T0385225 P1.
- [SDR FDEA202510222071](https://openairdocs.org/sdr/FDEA202510222071.md): Frame · corroded · Oct 22, 2025 · N978FD · Boeing 757236 · Fuselage Main, Frame
  > AFTER REMOVAL OF EXHAUST DUCT AND CORE ON APU FOUND SEVERE CORROSIONB ON FRAME (148N1606) AT STA 1992.8 APPOX 6 INCHES AT THE 6 OCLOCK POSITION (APPROX 4-7 O CLOCK) WAS FOUND FRAME, RING AND SPLICE WITH CORROSION OUT OF LIMITS EVALUATED IAW B757 SRM 53-
- [SDR FDEA202510212057](https://openairdocs.org/sdr/FDEA202510212057.md): Skin Panel · corroded · Oct 21, 2025 · N978FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > APU COMPARTMENT RT SIDE BS 1896.20, DOOR 316AR CUTOUT, INTERNAL SKIN, WITH CORROSION. CORROSION OUT OF LIMITS AT APU COMPT. RT SIDE B.S 1892 DOOR 316AR CUTOUT AREA ON INTERNAL SKIN WAS REPAIRED IAW SRM 53-80-01-2R AND SRM 51-70-10-2R.
- [SDR FDEA202510091936](https://openairdocs.org/sdr/FDEA202510091936.md): Seat Track · damaged · Oct 9, 2025 · N969FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FIRST OFFICER SEAT TRACK (AFT/LH) SHOWS GROOVE ON SURFACE AND ELONGATE REMOVED/REPLACED MAIN DECK FIRST OFFICER SEAT TRACK (AFT/LH) IAW B757 SRM 51-40-02- 0G AND B757 AMM 20-11-00-2
- [SDR FDEA202510091935](https://openairdocs.org/sdr/FDEA202510091935.md): Seat Track · damaged · Oct 9, 2025 · N969FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK PILOT AFT/RH SEAT TRACK SHOWS GOUGE ON SURFACE AND HOLES ELONGATE REMOVED & REPLACED MAIN DECK PILOT AFT/RH TRACK IAW B757 SRM 51-40-02-0G AND B757 AMM 20-11-00-2
- [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 FDEA202508281563](https://openairdocs.org/sdr/FDEA202508281563.md): Warning Message · illuminated · Aug 28, 2025 · N949FD · Boeing 757236 · Door Warning System
  > ON TAKEOFF AT 70 KTS MAIN CARGO DOOR WARNING WITH EICAS MSG. MASTER WARNING HORN SOUNDED. REJECTED TAKEOFF & MESSAGE CLEARED, SECOND ATTEMPT WAS GOOD WITH NO INDICATIONS PRESENT. ENTERED PER CA 219512 AMM: 52-32-00-5-0 AMM: 05-51-14-14-2 PERFORMED OPS CH
- [SDR FDEA202508281561](https://openairdocs.org/sdr/FDEA202508281561.md): Strut · corroded · Aug 28, 2025 · N979FD · Boeing 757236 · Nacelle/Pylon, Main Frame
  > ENGINE #1 I/B NACELLE STRUT INTERNAL STRUCTURE AT APROX PPSTA 140.0 HAS CORROSION ON SIDE SKIN DISCRIPANCY WAS ACCOMPLISHED ON NR N00271.
- [SDR FDEA202508151455](https://openairdocs.org/sdr/FDEA202508151455.md): Power Supply · inoperative · Aug 15, 2025 · N947FD · Boeing 757236 · Emergency Lighting
  > COURIER AREA CENTER EMERGENCY LIGHT WITH R1 DOOR EXTERIOR SLIDE LIGHT AND R1 EXIT LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. OPS CHK SERVICEABLE. OK TO CONTINUE.
- [SDR FDEA202508071390](https://openairdocs.org/sdr/FDEA202508071390.md): Strut · corroded · Aug 7, 2025 · N979FD · Boeing 757236 · Nacelle/Pylon, Main Frame
  > ENG #1 I/B NACELLE STRUT INTERNAL STRUCTURE THRU ACCESS PANEL # 433AL HAS CORROSION ON THE SKIN COMPLIED WITH EA # F-5450-T0384076 P1 TITLE: NACELLES/PYLON N0 1 PYLON, INBD PANEL, PP STA 163, INNER SKIN ASSY, CORROSION REPAIR
- [SDR FDEA202508071389](https://openairdocs.org/sdr/FDEA202508071389.md): Floorbeam · corroded · Aug 7, 2025 · N979FD · Boeing 757236 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM AT BS 1681.0 RBL 24.75 WITH EVIDENCE CORROSION COMPLIED WITH EA # F-5310-T0384192 TITLE: FUSELAGE - MAINFRAME - REPAIR OF STA 1681 FLOOR BEAM LOWER CHORD CORROSION AT RBL 26
- [SDR FDEA202507251320](https://openairdocs.org/sdr/FDEA202507251320.md): Skin · cracked · Jul 25, 2025 · N979FD · Boeing 757236 · Leading Edge Devices
  > L.E. SLAT NO 1 INB MAIN TRACK AREA, INTERNAL SKIN WITH CRACK. FABRICATED, LOCATED AND DRILLED REPAIR PARTS SLAT #1 INB MAIN TRACK AREA, REMOVED SLAT #1 IAW B 757 AMM 27-81-02-4, INSTALLED REPAIR PARTS IAW B 757 SRM 57-43-01-2R FIG 201 REP 4, RE-INSTALLED #
- [SDR FDEA202507201275](https://openairdocs.org/sdr/FDEA202507201275.md): Support Angle · corroded · Jul 20, 2025 · N979FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > STAB COMP BETWEEN STA 1787 TO 1825 STR 3R APU AIR INLET DOOR SURROUND ANGLE CORRODED.
- [SDR FDEA202507171249](https://openairdocs.org/sdr/FDEA202507171249.md): Window · cracked · Jul 17, 2025 · N948FD · Boeing 757236 · Flight Compartment Windows
  > L1 WINDOW CRACK DURING CRUISE AT FL400. WINDOW STARTED ARCING AND CRACKING, RAN WINDOW DAMAGE QRH. DESELECTED L FWD WINDOW HEAT, ARCING AND CRACKING STOPPED.
- [SDR FDEA202507101172](https://openairdocs.org/sdr/FDEA202507101172.md): Skin · delaminated · Jul 10, 2025 · N979FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING INB FLAP T/E BTW MF STA 223.86 TO MF 243.0 SUSPECT DELAMINATION. PERFORMED TAP TEST ON RT WING I/B FLAP T/E "MAIN FLAP DELAMINATION FOUND DIM = 3" LONG,12"WIDTH OUT OF LIMIT IAW B757 SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 5 NOTE "L" IAW B757
- [SDR FDEA202506191018](https://openairdocs.org/sdr/FDEA202506191018.md): Gust Lock · broken · Jun 19, 2025 · N979FD · Boeing 757236 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L1 DOOR GUST LOCK SPLIT COLLAR, OPS CHECK GOOD, OK FOR SERVICE.
- [SDR FDEA202506140942](https://openairdocs.org/sdr/FDEA202506140942.md): Gust Lock · damaged · Jun 14, 2025 · N949FD · Boeing 757236 · Passenger/Crew Doors
  > L-1 DOOR GUST LOCK BROKEN NOT ALLOWING DOOR TO SHUT PROPERLY. REMOVED BROKEN GUST LOCK COLLAR AND INSTALLED NEW COLLAR S/N 25-0009 PN 140N6008-1 REF INCLUDED MANUAL, NEWER COLLAR IS A FAULTY INSTALLED, SEVERE WEATHER INTERFERED WITH COMPLETION, ITEM NEEDS T
- [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 FDEA202505280813](https://openairdocs.org/sdr/FDEA202505280813.md): Warning Message · illuminated · May 28, 2025 · N946FD · Boeing 757236 · Landing Gear Position and Warning
  > ON DEPARTURE FROM KSYR, UPON RETRACTING THE GEAR WE RECEIVED A GEAR DISAGREE EICAS WITH AN AMBER GEAR LIGHT ON THE RIGHT QUADRANT OF THE GEAR INDICATION LIGHTS. WE TESTED THE LIGHTS AND THE RIGHT MAIN GEAR LIGHT DID NOT TEST. RETURNED TO KSYR. UPON LOWERI
- [SDR FDEA202505150757](https://openairdocs.org/sdr/FDEA202505150757.md): Flap System · malfunctioned · May 15, 2025 · N949FD · Boeing 757236 · Trailing Edge Flap Control System
  > WHEN CONFIGURING FOR APPROACH, SELECTED FLAPS 1. GOT TRAILING EDGE FLAPS DISAGREE EICAS AND ANNUNCIATOR. FLAPS DID NOT MOVE. FLAP LEVER WAS FIRMLY IN THE FLAPS 1 DETENT. REFERENCED THE QRH AND PUT THE FLAPS TO 20 USING THE ALT FLAPS SWITCH. LANDED WITH FL

Next page: https://openairdocs.org/model/boeing-757-236/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 = '757236'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-236/reports

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