# Boeing 757-28A - Type: Aircraft model (FAA registry) - Registry code: 1384976 - Manufacturer (registry): BOEING - Model: 757-28A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 249 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 14 - Page: https://openairdocs.org/model/boeing-757-28a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (14) - [N176CA](https://openairdocs.org/aircraft/N176CA): [Cascade Spares Inc](https://openairdocs.org/faa-owner/CASCADE%20SPARES%20INC), [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville), built 1990, S/N 24543 - [N235WD](https://openairdocs.org/aircraft/N235WD): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 24235 - [N835AS](https://openairdocs.org/aircraft/N835AS): [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables), S/N 28835 - [N912FD](https://openairdocs.org/aircraft/N912FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1988, S/N 24260 - [N913FD](https://openairdocs.org/aircraft/N913FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24017 - [N914FD](https://openairdocs.org/aircraft/N914FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24367 - [N928FD](https://openairdocs.org/aircraft/N928FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24369 - [N963FD](https://openairdocs.org/aircraft/N963FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24368 - [N967FD](https://openairdocs.org/aircraft/N967FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1994, S/N 26269 - [N968FD](https://openairdocs.org/aircraft/N968FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1995, S/N 26274 - [N969FD](https://openairdocs.org/aircraft/N969FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1997, S/N 28164 - [N970FD](https://openairdocs.org/aircraft/N970FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1997, S/N 28166 - [N971FD](https://openairdocs.org/aircraft/N971FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1995, S/N 26277 - [N972FD](https://openairdocs.org/aircraft/N972FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1998, S/N 28203 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20010603010589I](https://openairdocs.org/incident/20010603010589I), Jun 3, 2001: Dhav DHC6300 (N237SA), Las Vegas, NV. (-23)Scenic 37, DHC-6-300, executed a go around and subsequently encountered engine failure prior to landing north Las Vegas, NV (vgt) airport safely. After… - [Incident 20000504022369I](https://openairdocs.org/incident/20000504022369I), May 4, 2000: Dhav DHC6300 (N237SA), Monument Valley, UT, Minor damage. (-23)According to the crew while taking off on runway 34 at 60 knots the a ircraft was hit with a gust of wind and veered 20 degrees to the left exiting the… ## Service difficulty reports (1,998, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA202610061486](https://openairdocs.org/sdr/FDEA202610061486), Oct 6, 2026: BULB. FAILED. 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 - [SDR FDEA202608291251](https://openairdocs.org/sdr/FDEA202608291251), Aug 29, 2026: TRANSMISSION. TRIPPED. DURING APPROACH, RECEIVED A TE FLAP DISAGREE. RAN QRH & DECLARED AN EMERGENCY, LANDED UNEVENTFULLY. INSPECTED OVERLOAD INDS ON LT & RT, INBD & OTBD FLAPS & FOUN - [SDR FDEA202608281246](https://openairdocs.org/sdr/FDEA202608281246), Aug 28, 2026: WINDOW. ARCED. AFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. RE - [SDR FDEA202608211220](https://openairdocs.org/sdr/FDEA202608211220), Aug 21, 2026: OXYGEN MASK. NO TEST. 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 - [SDR FDEA202608211213](https://openairdocs.org/sdr/FDEA202608211213), Aug 21, 2026: OXYGEN MASK. NO TEST. 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 & LEA - [SDR FDEA202608141125](https://openairdocs.org/sdr/FDEA202608141125), Aug 14, 2026: SLAT SYSTEM. ASYMETRIC. 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. POSIT - [SDR FDEA202607090877](https://openairdocs.org/sdr/FDEA202607090877), Jul 9, 2026: LIGHT. DAMAGED. 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), Jun 19, 2026: COLLAR. DAMAGED. 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), Jun 10, 2026: HOLDER. INOPERATIVE. 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 - [SDR FDEA202606030667](https://openairdocs.org/sdr/FDEA202606030667), Jun 3, 2026: PRESSURE SWITCH. FAILED. 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 - [SDR FDEA202606010661](https://openairdocs.org/sdr/FDEA202606010661), Jun 1, 2026: SKIN. CRACKED. 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 - [SDR FDEA202605290653](https://openairdocs.org/sdr/FDEA202605290653), May 29, 2026: SKIN. DENTED. 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 - [SDR FDEA202605290652](https://openairdocs.org/sdr/FDEA202605290652), May 29, 2026: SKIN. DELAMINATED. 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 RE - [SDR FDEA202605290651](https://openairdocs.org/sdr/FDEA202605290651), May 29, 2026: SKIN. DENTED. 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 - [SDR FDEA202605270639](https://openairdocs.org/sdr/FDEA202605270639), May 27, 2026: SEAT TRACK. CORRODED. 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 F - [SDR FDEA202605230629](https://openairdocs.org/sdr/FDEA202605230629), May 23, 2026: SKIN. CORRODED. 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 - [SDR FDEA202605230628](https://openairdocs.org/sdr/FDEA202605230628), May 23, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 660 TO 885 RBL 58.22 WITH CORROSION. - [SDR FDEA202605210626](https://openairdocs.org/sdr/FDEA202605210626), May 21, 2026: SKIN. DELAMINATED. 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 - [SDR FDEA202605050561](https://openairdocs.org/sdr/FDEA202605050561), May 5, 2026: MODULE. FAULTED. 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 RE - [SDR FDEA202605050558](https://openairdocs.org/sdr/FDEA202605050558), May 5, 2026: LIGHT. NO DISCREPANCY. 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 - [SDR FDEA202604160456](https://openairdocs.org/sdr/FDEA202604160456), Apr 16, 2026: CONTROL CABLE. OUT OF ADJUST. EXPERIENCED EXTREME UNCOMMANDED PITCH OSCILLATIONS ON CLIMB OUT BETWEEN 3 AND 4 THOUSAND FEET. OSCILLATIONS LASTED 10 TO 15 SECONDS. AIR CRAFT CLEAN CONFIGURATI - [SDR FDEA202604090419](https://openairdocs.org/sdr/FDEA202604090419), Apr 9, 2026: LAMP. FAILED. 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), Apr 8, 2026: TRANSMISSION. FAILED. 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 160KT - [SDR FDEA202604020391](https://openairdocs.org/sdr/FDEA202604020391), Apr 2, 2026: BATTERY PACK. INOPERATIVE. 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- - [SDR FDEA202603060325](https://openairdocs.org/sdr/FDEA202603060325), Mar 6, 2026: BATTERY PACK. FAULTED. 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), Mar 4, 2026: GIRT BAR. DIRTY. 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 MAIN - [SDR FDEA202603030306](https://openairdocs.org/sdr/FDEA202603030306), Mar 3, 2026: LIGHT. INOPERATIVE. 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 I - [SDR FDEA202602110171](https://openairdocs.org/sdr/FDEA202602110171), Feb 11, 2026: FLEX LINE. LEAKING. 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 PRI - [SDR FDEA202601160063](https://openairdocs.org/sdr/FDEA202601160063), Jan 16, 2026: BATTERY PACK. FAILED. 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 - [SDR FDEA202601050005](https://openairdocs.org/sdr/FDEA202601050005), Jan 5, 2026: SKIN. CRACKED. 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 RUNN - [SDR FDEA202601030003](https://openairdocs.org/sdr/FDEA202601030003), Jan 3, 2026: REPAIR. NOT REPORTED. 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 EXISTI - [SDR FDEA202512292294](https://openairdocs.org/sdr/FDEA202512292294), Dec 29, 2025: STRINGER. CORRODED. AFT CARGO COMPARTMENT, DURING REMOVAL OF PRODUCTION STRINGER SPLICE TO GAIN ACCESS FOR STRINGER REPAIR FOUND STRINGER 21L, BS 1460 - 1465 EXFOLIATED. REPAIRED T - [SDR FDEA202512292293](https://openairdocs.org/sdr/FDEA202512292293), Dec 29, 2025: STRINGER. CRACKED. 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 - [SDR FDEA202512262290](https://openairdocs.org/sdr/FDEA202512262290), Dec 26, 2025: FITTING. LOOSE. 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 - [SDR FDEA202512232285](https://openairdocs.org/sdr/FDEA202512232285), Dec 22, 2025: FLOOR SUPPORT. DAMAGED. 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 IA - [SDR FDEA202512212275](https://openairdocs.org/sdr/FDEA202512212275), Dec 21, 2025: SHEAR PLATE. CORRODED. 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 V - [SDR FDEA202512202272](https://openairdocs.org/sdr/FDEA202512202272), Dec 20, 2025: STRINGER. CORRODED. 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), Dec 20, 2025: SHEAR TIE. CORRODED. 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), Dec 20, 2025: SHEAR TIE. CORRODED. 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), Dec 20, 2025: STRINGER SPLICE. CORRODED. 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), Dec 20, 2025: STRINGER. CORRODED. 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), Dec 20, 2025: STRINGER SPLICE. CORRODED. 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), Dec 20, 2025: STRINGER. CORRODED. 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), Dec 20, 2025: SKIN PANEL. CRACKED. 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 - [SDR FDEA202512182261](https://openairdocs.org/sdr/FDEA202512182261), Dec 18, 2025: STRINGER. CORRODED. 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), Dec 11, 2025: SEAT TRACK. CORRODED. 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 - [SDR FDEA202511122167](https://openairdocs.org/sdr/FDEA202511122167), Nov 12, 2025: CIRCUIT BREAKER. FAULTED. 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- - [SDR FDEA202511112157](https://openairdocs.org/sdr/FDEA202511112157), Nov 11, 2025: GIRT BAR. DAMAGED. 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- - [SDR FDEA202511112156](https://openairdocs.org/sdr/FDEA202511112156), Nov 11, 2025: LIGHT. NO TEST. 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- - [SDR FDEA202510292106](https://openairdocs.org/sdr/FDEA202510292106), Oct 29, 2025: TRANSMISSION. FAILED. 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 & FSE All 1,998: https://openairdocs.org/model/boeing-757-28a/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.