# Service difficulty reports: Boeing 757-28A

A list on [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 40 · 1,998 reports

- [SDR FDEA202610061486](https://openairdocs.org/sdr/FDEA202610061486.md): Bulb · failed · Oct 6, 2026 · N968FD · Boeing 75728A · Emergency Lighting
  > FOUND L1 EMERGENCY EXIT SIGN DIM DURING MX PRE-FLIGHT AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. (P/N 0L3071BPEGPL). OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202608291251](https://openairdocs.org/sdr/FDEA202608291251.md): Transmission · tripped · Aug 29, 2026 · N969FD · Boeing 75728A · Trailing Edge Flap Actuator
  > DURING APPROACH, RECEIVED A TE FLAP DISAGREE. RAN QRH & DECLARED AN EMERGENCY, LANDED UNEVENTFULLY. INSPECTED OVERLOAD INDS ON LT & RT, INBD & OTBD FLAPS & FOUND RT INBD FLAP INBD TRANSMISSION OVERLOAD IND TRIPPED. UPON ENTERING FLIGHT DECK FOUND LE ALTERN
- [SDR FDEA202608281246](https://openairdocs.org/sdr/FDEA202608281246.md): Window · arced · Aug 28, 2026 · N963FD · Boeing 75728A · Flight Compartment Windows
  > AFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. REMOVED AND REPLACED L1 WINDSHIELD IAW AMM 56-11-01-4-0 SECTION E, STEP 13, FIRST TORQUE APPLIED SEC
- [SDR FDEA202608211220](https://openairdocs.org/sdr/FDEA202608211220.md): Oxygen Mask · no test · Aug 21, 2026 · N928FD · Boeing 75728A · Crew Oxygen System
  > DURING MX PREFLIGHT; CAPTAINS O2 MASK FAILS "PRESS TO TEST." REPLACED CAPT'S FULL FACE O2 MASK IAW B757 AMM CH. REF. LISTED ABOVE. OPS AND LEAK CKS GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202608211213](https://openairdocs.org/sdr/FDEA202608211213.md): Oxygen Mask · no test · Aug 21, 2026 · N928FD · Boeing 75728A · Crew Oxygen System
  > DURING MX PREFLIGHT, CAPTAINS O2 MASK FAILED A PRESS TO TEST. PREMATURE REMOVAL/INSTALLATION. REPLACED CAPT'S FULL FACE O2 MASK IAW AMM 35-11-51-4-99. OPS & LEAK CHKD GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202608141125](https://openairdocs.org/sdr/FDEA202608141125.md): Slat System · asymetric · Aug 14, 2026 · N912FD · Boeing 75728A · Leading Edge Slat Position Indicating System
  > LE SLAT ASYM. COMPLIED WITH THE QRH. EMERGENCY DECLARED. TROUBLSHOT THE LE SLAT SYSTEM AND FOUND A SINGLE TORQUE TUBE COUPLING DICONNECTED ON THE RT WING. POSITION IS OTBD OF THE RT ANGLE GEARBOX & FIRST ROTARTY ACTUATOR, ACCESS PANEL 611DB IAW MM 27-81-
- [SDR FDEA202607090877](https://openairdocs.org/sdr/FDEA202607090877.md): Light · damaged · Jul 9, 2026 · N790FD · Boeing 75728A · Emergency Lighting
  > L1 DOOR EMERGENCY SLIDE LIGHT WILL NOT TEST. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT, IAW AMMM 33-51-06-2-1. LIGHT TESTED GOOD.
- [SDR FDEA202606190785](https://openairdocs.org/sdr/FDEA202606190785.md): Collar · damaged · Jun 19, 2026 · N912FD · Boeing 75728A · Passenger/Crew Doors
  > DURING RAMP TRAINING L1 DOOR GUST LOCK WOULD NOT RELEASE. AMM 52-11-08-8 INSTALLED SERVICEABLE SPLIT COLLAR IN REF TO AMM. CLEARED MEL.
- [SDR FDEA202606100692](https://openairdocs.org/sdr/FDEA202606100692.md): Holder · inoperative · Jun 10, 2026 · N963FD · Boeing 75728A · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT AND SLIDE LIGHT WILL NOT TEST. A/C HAS BEEN POWERED FOR ALMOST 3 HOURS, NO HELP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT POWER SUPPLY M731. RADIANT POWER CORP, MPN 2013-1A, MSN 111794 POWER SUPPLY REMOVED. OPS CHECKS GO
- [SDR FDEA202606030667](https://openairdocs.org/sdr/FDEA202606030667.md): Pressure Switch · failed · Jun 3, 2026 · N968FD · Boeing 75728A · Hydraulic System, Main
  > JUST STARTING THE TAKEOFF ROLL GOT C HYD SYS PRESS CAUTION MESSAGE. ABORTED TAKEOFF AND RAN QRH PVD AMM: 29-11-19-4 REMOVED AND REPLACED CTR HYD SYSTEM PRESSURE SWITCH AT CANNON PLUG S10002. OP'S CHECK GOOD. NO LEAKS OR FAULTS NOTED. AC OK FOR SERVICE. AL
- [SDR FDEA202606010661](https://openairdocs.org/sdr/FDEA202606010661.md): Skin · cracked · Jun 1, 2026 · N912FD · Boeing 75728A · Leading Edge Devices
  > RH WING SLAT # 9 LOWER SURFACE O/N MAIN TRACK BRACKET AREA WITH CRACK APPLIED PERMANENT REPAIR AT RH WING SLAT # 9 LOWER FLEXIBLE SKIN PANEL BTW OSS 675 TO OSS 680 IAW B757 SRM 57-43-01-2R, FIG 201, RPR 10, SHEET 1 AND SRM 51-70-07-0G REPAIR DIM 2=5.100",
- [SDR FDEA202605290653](https://openairdocs.org/sdr/FDEA202605290653.md): Skin · dented · May 29, 2026 · N912FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > SEC 48 UPPER FUSELAGE BETWEEN BS 1941 AND BS 1963 WITH 03 DENTS APPLIED PERMANENT REPAIR AT SEC 48 UPPER FUSELAGE BTW STA 1941 TO 1963 IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06- 2R
- [SDR FDEA202605290652](https://openairdocs.org/sdr/FDEA202605290652.md): Skin · delaminated · May 29, 2026 · N912FD · Boeing 75728A · APU Cowling/Containment
  > APU COMPARTMENT INTERNAL SKIN AT BS 1900 DELAMINATED APPLIED PERMANENT AT APU COMPARTMENT INTERNAL SKIN IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06-2R
- [SDR FDEA202605290651](https://openairdocs.org/sdr/FDEA202605290651.md): Skin · dented · May 29, 2026 · N912FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > SEC 48 UPPER FUSELAGE BETWEEN BS 1896 AND BS 1918 HAS A CUSTER OF 04 DENTS (TWO ARE LOCATED AROUND THE AREA, AND TWO ARE LOCATED OVER A PREVIOUS REPAIR) APPLIED PERMANT REPAIR AT SEC 48 UPPER FUSELAGE LH BTW STA 1896 TO 1918 IAW B757 SRM 51-70-10-2R AND P
- [SDR FDEA202605270639](https://openairdocs.org/sdr/FDEA202605270639.md): Seat Track · corroded · May 27, 2026 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 660.0 TO 885.0 RBL 58.22 WITH CORROSION EVALUATED SEAT TRACK FOUND DATA NOT ALLOWED DAMAGE OUT OF LIMITS IAW SRM 53- 00-52-1A FIG 101 SHEET 1, REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN BS 660 TO 885, RBL 58.22 IAW B75
- [SDR FDEA202605230629](https://openairdocs.org/sdr/FDEA202605230629.md): Skin · corroded · May 23, 2026 · N912FD · Boeing 75728A · Nacelle/Pylon, Plate/Skin
  > PYLON NR 1 AROUND THE CUT OUT FOR ACCESS PANEL 433JR INTERNAL SKIN SHOWS CORROSION. REMOVED AND REPLACED INBD PYLON SKIN PANEL IAW B DWG 012N8774 REV A AND SRM 51-40-02-0G.
- [SDR FDEA202605230628](https://openairdocs.org/sdr/FDEA202605230628.md): Seat Track · corroded · May 23, 2026 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 660 TO 885 RBL 58.22 WITH CORROSION.
- [SDR FDEA202605210626](https://openairdocs.org/sdr/FDEA202605210626.md): Skin · delaminated · May 21, 2026 · N912FD · Boeing 75728A · Trailing Edge Flaps
  > L/H WING INB MAIN FLAP TRAILING EDGE PREVIOUS REPAIR IS DEBONDED REMOVED PREVIOUS REPAIR LOWER SKIN FOUND DEBONDED AND INSTALLED PERMANENT REPAIR AT LH WING I/B MAIN FLAP TRAILING EDGE IAW B757 SRM 57-53-01-2R, FIG 201, RPR 1, SHEET 2, DETAIL I, AND SRM 51
- [SDR FDEA202605050561](https://openairdocs.org/sdr/FDEA202605050561.md): Module · faulted · May 5, 2026 · N970FD · Boeing 75728A · Landing Gear Door Retract Section
  > AFTER TAKEOFF, GEAR DISAGREE AND GEAR DOORS EICAS MESSAGES APPEARED ACCOMPANIED BY AN AUDIBLE AND TACTILE INDICATION THAT THE GEAR AND/OR GEAR DOORS WERE NOT RETRACTED. APPROXIMATELY 3 MINUTES LATER ALL EICAS MESSAGES AND ACCOMPANYING INDICATORS CEASED. A
- [SDR FDEA202605050558](https://openairdocs.org/sdr/FDEA202605050558.md): Light · no discrepancy · May 5, 2026 · N963FD · Boeing 75728A · Door Warning System
  > FO SIDE SLIDE LIGHT INOP. PERFORMED OPERATIONAL TEST OF R1 GIRT BAR ENGAGED LIGHT, GIRT BAR ENGAGED WARNING LIGHT ILLUMINATES OVER SEVERAL CYCLES OF MODE SELECT LEVER.
- [SDR FDEA202604160456](https://openairdocs.org/sdr/FDEA202604160456.md): Control Cable · out of adjust · Apr 16, 2026 · N968FD · Boeing 75728A · Elevator Control System
  > EXPERIENCED EXTREME UNCOMMANDED PITCH OSCILLATIONS ON CLIMB OUT BETWEEN 3 AND 4 THOUSAND FEET. OSCILLATIONS LASTED 10 TO 15 SECONDS. AIR CRAFT CLEAN CONFIGURATION ACCELERATING TO 250 KNOTS. ENGAGED CENTER AUTOPILOT AND OSCILLATIONS CEASED. MULTIPLE HAND F
- [SDR FDEA202604090419](https://openairdocs.org/sdr/FDEA202604090419.md): Lamp · failed · Apr 9, 2026 · N912FD · Boeing 75728A · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. AMM: 33-51-06-2 RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE.
- [SDR FDEA202604080409](https://openairdocs.org/sdr/FDEA202604080409.md): Transmission · failed · Apr 8, 2026 · N969FD · Boeing 75728A · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE EICAS ALONG WITH TE FLAP FAILURE DESCENT TO MEMPHIS. RAN CHECKLIST, DROVE US FROM 9.1.17 TO 9.1.14, LANDED WITH FLAPS LESS THAN TOUCHDOWN 160KTS OR A LITTLE MORE. DECLARED EMERGENCY. EMERGENCY DECLARED. AMM 27-51-06-4 COMPLETED INSTALLATIO
- [SDR FDEA202604020391](https://openairdocs.org/sdr/FDEA202604020391.md): Battery Pack · inoperative · Apr 2, 2026 · N928FD · Boeing 75728A · Emergency Lighting
  > ON PREFLIGHT FOUND R1 DOOR SLIDE LIGHT INOPERATIVE. AMM 33-51-06-2-1, AMM 33-51-07-2, & AMM 33-51-07-862-036. REPLACED BULB IN R1 DOOR SLIDE LIGHT IAW MM 33-51-06-2-1. REPLACED R1 DOOR SLIDE LIGHT POWER SUPPLY IN FWD GALLEY AND BATTERY PACK IAW MM 33-51-07
- [SDR FDEA202603060325](https://openairdocs.org/sdr/FDEA202603060325.md): Battery Pack · faulted · Mar 6, 2026 · N912FD · Boeing 75728A · Emergency Equipment
  > RIGHT ENTRY SLIDE LIGHT REMAINS ON AFTER DISARMING. REPLACED BATTERY AT M730. REMOVED SOURCE MANUFACTURING BATTERY ASSEMBLY MPN 2013-1ASMI S/N 3341. TEST GOOD.
- [SDR FDEA202603040310](https://openairdocs.org/sdr/FDEA202603040310.md): Girt Bar · dirty · Mar 4, 2026 · N914FD · Boeing 75728A · Emergency Equipment
  > PDIS 914 52-10 5125 03MAR26 23:10 OGG FACT L1 ENTRY DOOR WOULD NOT SHOW DISARM. DISARM LEVER DID NOT COMPLETELY DISARM (LEVER AND KNUCKLE BLOCKER) REQUIRED MAINTENANCE TO DISARM THE DOOR. FACT 03MAR26 23:27 OGG AMM: 52-11-00-2 REMOVED U
- [SDR FDEA202603030306](https://openairdocs.org/sdr/FDEA202603030306.md): Light · inoperative · Mar 3, 2026 · N912FD · Boeing 75728A · Emergency Equipment
  > WHEN ARMING THE SLIDES FOR DEPARTURE, RT SLIDE LIGHT DID NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 25-66-04-B, CATEGORY C. VERIFIED SLIDE ARMED LT DOES NOT ILLUMINATE WHEN R1 DOOR SLIDE IS ARMED. PERFORMED GVI OF R1 DOOR ESCAPE SLIDE GIRT BAR, SKIRT & L
- [SDR FDEA202602110171](https://openairdocs.org/sdr/FDEA202602110171.md): Flex Line · leaking · Feb 11, 2026 · N917FD · Boeing 75728A · Hydraulic System, Main
  > ON APPROACH EXTENDING MLG & FLAPS TO 20, LT HYD QTY EICAS & COMPLETE LOSS OF LT SYS HYD FLUID. MAINTAINED CONFIGURATION & COMPLETED LT HYD QTY QRH PROCEDURE PRIOR TO LANDING. EMERGENCY DECLARED AMM 12-12-01, AMM 29-11-17-4, FOUND FLEX LINE CONNECTED TO SWI
- [SDR FDEA202601160063](https://openairdocs.org/sdr/FDEA202601160063.md): Battery Pack · failed · Jan 16, 2026 · N912FD · Boeing 75728A · Emergency Lighting
  > COURIER AREA CENTER OVERHEAD EMERGENCY EXIT LIGHT, R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT AND EXTERIOR R1 SLIDE LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. CTR & R1 OVERHEAD EXIT LIGHTS AND R1 EXTERIOR S
- [SDR FDEA202601050005](https://openairdocs.org/sdr/FDEA202601050005.md): Skin · cracked · Jan 5, 2026 · N963FD · Boeing 75728A · Fuselage Main, Plate/Skin
  > LEFT AFT FUSELAGE BS 1459-1461 (02EA) FASTENERS AFT OF BUTT SEAM BS 1459 ABOVE STR 20 AND DOUBLER THAT HAVE (02) POSSIBLE CRACKS INDICATION UNDER FASTENERS RUNNING PARALLEL OF THE DOUBLER DURING NDT HFEC INSPECTION COMPLIED WITH EA # F5330-T0385962 TITTLE
- [SDR FDEA202601030003](https://openairdocs.org/sdr/FDEA202601030003.md): Repair · not reported · Jan 3, 2026 · N963FD · Boeing 75728A · Standard Practices/Structures
  > EXISTING REPAIR FOUND AT # 2 CARGO DOOR AFT LOWER CORNER CUTOUT AREA COMPLIED WITH EA # F-5330-T0305556 B TITLE: FUSELAGE PLATES & SKINS - REPLACEMENT OF EXISTING STA 1440 FUSELAGE SKIN REPAIR AT 24R-25R (# 2 CARGO DOOR OPENING)
- [SDR FDEA202512292294](https://openairdocs.org/sdr/FDEA202512292294.md): Stringer · corroded · Dec 29, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, DURING REMOVAL OF PRODUCTION STRINGER SPLICE TO GAIN ACCESS FOR STRINGER REPAIR FOUND STRINGER 21L, BS 1460 - 1465 EXFOLIATED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REPAIR 2, FIG 201, DETAIL I, SHEET 6, AND SRM 51-40-02-OG.
- [SDR FDEA202512292293](https://openairdocs.org/sdr/FDEA202512292293.md): Stringer · cracked · Dec 29, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFTER DVI OF THE LAPPED AND OVERLAPPING SKIN UNDERNEATH OF THE EXISTING REPAIR DOUBLER BETWEEN BS 1430 TO BS 1475, STR 20L TO STR 21L FOUND STRINGER 21L CRACKED AT BS 1454. REPAIRED STRINGER 21L BETWEEN STA 1426 TO STA 1456 IAW B 757 SRM 53-00-03-2R REPAIR
- [SDR FDEA202512262290](https://openairdocs.org/sdr/FDEA202512262290.md): Fitting · loose · Dec 26, 2025 · N963FD · Boeing 75728A · Nacelle/Pylon, Attach Fittings
  > NR 1 ENGINE NACELLE STRUT R/H SIDE AFTER. HINGE FITTING BOLT HEAD BROKEN OFF. REMOVED AND REPLACED BOLT AT NO 1 ENGINE NACELLE STRUT R/H SIDE AFT. HINGE FITTING IAW SRM 51-40-02-0G AND E.A # F-5440-T0385898 P1.
- [SDR FDEA202512232285](https://openairdocs.org/sdr/FDEA202512232285.md): Floor Support · damaged · Dec 22, 2025 · N963FD · Boeing 75728A · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STRINGER AT B.S. 1260 LBL 10.45 WITH SEVERAL PERFORATIONS (MISDRILLED) AFT CARGO COMPARTMENT STRINGER AT BS.1260 LBL 10.45 WAS REPAIRED IAW B757 SRM 53-00- 53-2R. REPAIR1.
- [SDR FDEA202512212275](https://openairdocs.org/sdr/FDEA202512212275.md): Shear Plate · corroded · Dec 21, 2025 · N963FD · Boeing 75728A · Fuselage Main, Structure
  > GALLEY AREA BS 375 BTW LBL 20.00 TO LBL 26.00 SHOW PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE SEAT TRACK SUPPORT (U CHANNEL) AND (2EA) FLEXURE ANGLE IAW VENTURA AEROSPACE DWG 3471 REV # B DWG 3480 REV # B AND BOEING DWG PL 141N5131 REV # V.
- [SDR FDEA202512202272](https://openairdocs.org/sdr/FDEA202512202272.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, STRINGER 30 BTW BS 1440 TO 1460 FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, SRM 51-40-02-0G, & DWG 146N3110, REV B.
- [SDR FDEA202512202271](https://openairdocs.org/sdr/FDEA202512202271.md): Shear Tie · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 1460 SHEAR TIE BTW STR-29L TO STR-30, FOUND CORRODED. REPLACED SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202270](https://openairdocs.org/sdr/FDEA202512202270.md): Shear Tie · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Internal Mounting Structure
  > LOWER HALF OF FUSELAGE BS 1460 BETWEEN S28L AND S29L HAS POSSIBLE CORROSION. REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202269](https://openairdocs.org/sdr/FDEA202512202269.md): Stringer Splice · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BS 1460 SPLICE STRINGER 30 CORRODED. REPLACED SPLICE STRINGER LOCATED BS 1460 IAW SRM 51-40-02-0G, AND DWG 146N3820, REV C.
- [SDR FDEA202512202268](https://openairdocs.org/sdr/FDEA202512202268.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, STRINGER 30L BTW BS 1460 - 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-02-0G, & DWG 146N3110, REV C.
- [SDR FDEA202512202267](https://openairdocs.org/sdr/FDEA202512202267.md): Stringer Splice · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY, BS 1460 STRINGER SPLICE 29L CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-40-02-0G, DWG 146N3820, REV C.
- [SDR FDEA202512202266](https://openairdocs.org/sdr/FDEA202512202266.md): Stringer · corroded · Dec 20, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER 29L BTW BS 1460 TO 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-020-G, AND DWG 146N3110, REV B.
- [SDR FDEA202512202265](https://openairdocs.org/sdr/FDEA202512202265.md): Skin Panel · cracked · Dec 20, 2025 · N963FD · Boeing 75728A · Leading Edge Devices
  > RIGHT WING OTBD LEADING EDGE SLAT NR 10 INTERNAL LOWER MAIN TRACK SLAT HAS POSSIBLE CRACKED. REMOVED DAMAGED COVE SKIN AT RT WING OTBD LEADING EDGE SLAT 10 IAW SRM 51-40-02-0G, AND INSTALLED NEW FORMED COVE SKIN IAW B. DRAWING 114N4075 REV -, AND PL 114N40
- [SDR FDEA202512182261](https://openairdocs.org/sdr/FDEA202512182261.md): Stringer · corroded · Dec 18, 2025 · N963FD · Boeing 75728A · Fuselage Main, Longeron/Stringer
  > BULK AREA BETWEEN STA 1700 TO 1720 STR 23L CORRODED ACCOMPLISHED REPAIR ON STRINGER BTW STA 1685 TO STR 1720 IAW B757 SRM 53-00-03-2R, 51- 40-02-0G
- [SDR FDEA202512112236](https://openairdocs.org/sdr/FDEA202512112236.md): Seat Track · corroded · Dec 11, 2025 · N963FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 900 TO BS 1180.0 LBL 58.22 HAS MULTIPLE SPOTS WITH CORROSION. REMOVED AND EVALUATED MAIN CABIN SEAT TRACK BTW BS 900-1180, LBL 58.22 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A, DETAIL V, 51-40-02-0G. TRIMMED, LOCATED AND DR
- [SDR FDEA202511122167](https://openairdocs.org/sdr/FDEA202511122167.md): Circuit Breaker · faulted · Nov 12, 2025 · N912FD · Boeing 75728A · Light System Wiring
  > R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-60-01-2. RT EMERGENCY EXIT SIGN OPS CHECKED NORMAL IAW MM 33-51-01-2.
- [SDR FDEA202511112157](https://openairdocs.org/sdr/FDEA202511112157.md): Girt Bar · damaged · Nov 11, 2025 · N928FD · Boeing 75728A · Passenger/Crew Doors
  > L1 DOOR WILL NOT OPEN. TROUBLESHOT L1 DOOR AND DISCOVERED FWD END OF GIRT BAR JAMMED IN ARMING SLIDER. REMOVED AND REPLACED L1 DOOR GIRT BAR REMOVED IAW AMM 25-66-10-2 AND PERFORMED L1 DOOR ADJUSTMENT TESTS PER AMM 52-11-25-5. L1 DOOR OPS AND FUNCTIONS NORMA
- [SDR FDEA202511112156](https://openairdocs.org/sdr/FDEA202511112156.md): Light · no test · Nov 11, 2025 · N912FD · Boeing 75728A · Emergency Lighting
  > R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-60-01-2. R/H EMERGENCY EXIT SIGN OPS CHECKED NORMAL IAW M/M 33-51-01-2.
- [SDR FDEA202510292106](https://openairdocs.org/sdr/FDEA202510292106.md): Transmission · failed · Oct 29, 2025 · N967FD · Boeing 75728A · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE ON APPROACH. ALTERNATE FLAP CHKLST DID NOT WORK. DID QRH TE FLAP ASSEMETRY & LANDED LESS THAN 1 DEGREE FLAPS IAW QRH. PERFORMED FSEU BITE & FSEU #2 SHOWED CODE 327. WHICH IS DUE TO ONLY ONE ALT ARMING SWITCH BEING ARMED & FSEU NR 1 SHOWED

Next page: https://openairdocs.org/model/boeing-757-28a/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 = '75728A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-28a/reports

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