# Boeing 757-23A

- Type: Aircraft model (FAA registry)
- Registry code: 1384967
- Manufacturer (registry): BOEING
- Model: 757-23A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 178
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 13
- Page: https://openairdocs.org/model/boeing-757-23a

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 (13)

- [N107TV](https://openairdocs.org/aircraft/N107TV): [Firedancer Asset Holding II LLC](https://openairdocs.org/faa-owner/FIREDANCER%20ASSET%20HOLDING%20II%20LLC), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), S/N 24527
- [N226G](https://openairdocs.org/aircraft/N226G): [L-3 Capital LLC](https://openairdocs.org/faa-owner/L-3%20CAPITAL%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), built 1992, S/N 25491
- [N757CJ](https://openairdocs.org/aircraft/N757CJ): [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), built 1990, S/N 24923
- [N757CL](https://openairdocs.org/aircraft/N757CL): [Bischoff Aerospace Inc](https://openairdocs.org/faa-owner/BISCHOFF%20AEROSPACE%20INC), [Doral, FL](https://openairdocs.org/faa-place/FL/Doral), S/N 25487
- [N917FD](https://openairdocs.org/aircraft/N917FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24291
- [N918FD](https://openairdocs.org/aircraft/N918FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24290
- [N919FD](https://openairdocs.org/aircraft/N919FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1990, S/N 24636
- [N920FD](https://openairdocs.org/aircraft/N920FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24289
- [N921FD](https://openairdocs.org/aircraft/N921FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1991, S/N 24924
- [N922FD](https://openairdocs.org/aircraft/N922FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24293
- [N938FD](https://openairdocs.org/aircraft/N938FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24292
- [N939FD](https://openairdocs.org/aircraft/N939FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24528
- [N994FD](https://openairdocs.org/aircraft/N994FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 25490

## NTSB investigations (4)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA23WA363](https://openairdocs.org/ntsb/DCA23WA363), Jul 16, 2023: Boeing 757-23A (N918FD), Tel Aviv, Israel, substantial damage
- [NTSB DCA18WA088](https://openairdocs.org/ntsb/DCA18WA088), Jan 30, 2018: Boeing 757 23A (N919FD), Tel Aviv, Israel, incident, no damage
- [NTSB DCA97RA001](https://openairdocs.org/ntsb/DCA97RA001), Oct 2, 1996: Boeing B-757-23A (N52AW), Lima, Peru, 70 fatal
- [NTSB BFO93IA175](https://openairdocs.org/ntsb/BFO93IA175), Sep 13, 1993: Boeing 757-200ER (N757NA), Jamaica, NY, incident, no damage. Probable cause: THE FAILURE OF THE LEFT HYDRAULIC PRESSURE SWITCH, WHICH CAUSED THE LEFT YAW DAMPER MODULE TO BECOME INOPERATIVE RESULTING IN UNCOMMANDED RUDDER MOVEMENTS DURING FLIGHT.

## FAA accident and incident reports (4)

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 20000107002559I](https://openairdocs.org/incident/20000107002559I), Jan 7, 2000: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. Flight 351 enroute from dfw to las on decent to Las Vegas could not deploy leading edge slats. Pliot and first officer followed in their qrh declaredan…
- [Incident 19990826024829I](https://openairdocs.org/incident/19990826024829I), Aug 26, 1999: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. During rotation a fire bell sounded and fire warning light illuminated on right engine. Smoke and fire was reported to the crew by ATC. Two f/a's aboard…
- [Incident 19940403009589I](https://openairdocs.org/incident/19940403009589I), Apr 3, 1994: Boeing 75723A (N757NA), Des Moines, IA. Lost oil presure. Secured NR1 engine. Found P3 sealing air tube had failed.
- [Incident 19930913038109I](https://openairdocs.org/incident/19930913038109I), Sep 13, 1993: Boeing 75723A (N757NA), New York, NY. Rudder ratio eicas message came on at alitude. Returned. Landed safely. Replaced righ rudder contro module.

## Service difficulty reports (1,396, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR FDEA202608261232](https://openairdocs.org/sdr/FDEA202608261232), Aug 26, 2026: FRAME. CRACKED. RIGHT, BS 1640 FUSELAGE FRAME WEB AT STRINGER 14R UPPER INBD CRACK INDICATION AT 2:00 O'CLOCK, AROUND THE BOTTOM INBD HOLE WITH TWO CRACK INDICATIONS AT 2:00 O'
- [SDR FDEA202608251224](https://openairdocs.org/sdr/FDEA202608251224), Aug 25, 2026: SKIN PANEL. CRACKED. LH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS R
- [SDR FDEA202608211211](https://openairdocs.org/sdr/FDEA202608211211), Aug 21, 2026: POWER SUPPLY. FAULTED. R1 EMERGENCY EXIT LIGHT FAILS OPS TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2012-1. REPLACED BATTERY, NO HELP. REMOVED AND REPLACED POWER SUPPLY/TRAY ASSY A
- [SDR FDEA202608201198](https://openairdocs.org/sdr/FDEA202608201198), Aug 20, 2026: BATTERY PACK. FAILED. INTERIOR EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED FWD BATTERY POWER SUPPLY IAW ABOVE REF. AFTER REPLACMENT FOUND CTR EXIT LIGHT AND R1 EXIT LIGHT OPS CHK 
- [SDR FDEA202608131118](https://openairdocs.org/sdr/FDEA202608131118), Aug 13, 2026: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 1200 BETWEEN BL 0 TO LBL 24.75 WITH CORROSION FLOORBEAM SECTION OUT OF LIMITS AT MAIN CABIN B.S 1200 BETWEEN LBL 5 TO LBL 11 WAS REPA
- [SDR FDEA202608121116](https://openairdocs.org/sdr/FDEA202608121116), Aug 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BEWTEEN BS 1060 TO 1080 RBL 45.50 WITH CORROSION MAIN CABIN SEAT TRACK SUPPORT (UPPER CHORD) BETWEEN STA 1040-1080 WITH CORROSION OUT OF L
- [SDR FDEA202608121115](https://openairdocs.org/sdr/FDEA202608121115), Aug 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 1180 TO BS 1200 LBL 24.75 OUTB FLANGE WITH CORROSION REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT STA 1180 TO 1200 LBL 24.75 I
- [SDR FDEA202608081101](https://openairdocs.org/sdr/FDEA202608081101), Aug 8, 2026: SKIN. DAMAGED. EVALUATE EXISTING DOUBLER REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE, NEAR MF STA 147.00 FOR RSC TRACKING PURPOSE ONLY EXISTING REPAIR ON RH INBOARD MAIN FLAP
- [SDR FDEA202608081100](https://openairdocs.org/sdr/FDEA202608081100), Aug 8, 2026: SKIN. DAMAGED. EVALUATE EXISTING COMPOSITE REPAIR AT LT ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA. REPAIRED AT LH ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA WAS EVALUATED UNDER
- [SDR FDEA202607100886](https://openairdocs.org/sdr/FDEA202607100886), Jul 10, 2026: LANYARD. OUT OF POSITION. DURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM . DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARB
- [SDR FDEA202606240800](https://openairdocs.org/sdr/FDEA202606240800), Jun 24, 2026: UNKNOWN. ODOR. AFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR 
- [SDR FDEA202605280647](https://openairdocs.org/sdr/FDEA202605280647), May 28, 2026: ADC. FAULTED. ALTITUDE DISAGREE TWO TIMES DURING DESCENT. FO ALTIMETER MATCHED THE STANDBY AND WAS 400 FEET DIFFERENT THAN CAPTAINS AMM: 34-12-01-4 REMOVED AND REPLACED CAPTA
- [SDR FDEA202605080570](https://openairdocs.org/sdr/FDEA202605080570), May 8, 2026: SKIN. DAMAGED. LH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND 
- [SDR FDEA202604180469](https://openairdocs.org/sdr/FDEA202604180469), Apr 18, 2026: FSEU. FAILED. WHILE CONFIGURING FOR LANDING, AS WE SELECTED FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE ON EICAS. INDICATOR REMAINED AT FLAPS 20. COMPLIED WITH QRH. RETRACTED F
- [SDR FDEA202604030397](https://openairdocs.org/sdr/FDEA202604030397), Apr 3, 2026: SKIN. DENTED. R/WING O/B T/E MAIN FLAP LOWER SURFACE HAS A DENT PANEL ASSY SKIN OUTER PLY THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5750-T0386919.
- [SDR FDEA202604020393](https://openairdocs.org/sdr/FDEA202604020393), Apr 2, 2026: FRAME. CRACKED. DURING ACCOMPLISHMENT WC EF 530-E0329085 D P6 MAIN FRAME BODY STATION 1640 FUSELAGE FRAME INSPECTION FOUND MISSING INTERNAL STRAP IN FRAME AT BS 640 BETWEEN STR
- [SDR FDEA202603220365](https://openairdocs.org/sdr/FDEA202603220365), Mar 22, 2026: SKIN. CORRODED. #2 ENG. L/H FUSELAGE EXTERIOR COMPOSITE PANEL HAS CORROSION ON OUTER ALUMINUM SKIN AT FWD LWR CORNER NEAR APU PLENUM DRAIN. APPROX. STA. 1904 REF. BOEING DWG. 1
- [SDR FDEA202603190358](https://openairdocs.org/sdr/FDEA202603190358), Mar 19, 2026: FSEU. FAILED. UPON SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE EICAS. FLAP HANDLE WAS AT 25 BUT THE FLAPS WERE AT 20. RAN QRH, RETRACTED FLAPS TO UP USING ALT FLAPS AND DI
- [SDR FDEA202508291579](https://openairdocs.org/sdr/FDEA202508291579), Aug 29, 2025: FRAME. CRACKED. CRACK INDICATIONS FOUND IN STA 1640 AT S-14R BOTTOM I/B OPEN HOLE APROX AT 8 O' CLOCK LOOKING AFT AND TWO CRACK INDICATIONS IN UPPER O/B OPEN HOLE APROX AT 6 & 
- [SDR FDEA202508281562](https://openairdocs.org/sdr/FDEA202508281562), Aug 28, 2025: SKIN. DELAMINATED. LH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA ) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5
- [SDR FDEA202507301342](https://openairdocs.org/sdr/FDEA202507301342), Jul 30, 2025: SKIN. DENTED. RIGHT HORIZONTAL STAB. UPPER SKIN WITH DENT BETWEEN STAB STA 104.248 AND STA 152.248 AND BETWEEN FRONT . SPAR AND AUX SPAR. EVALUATED DENT ON RH HORIZONTAL STAB
- [SDR FDEA202507221293](https://openairdocs.org/sdr/FDEA202507221293), Jul 22, 2025: SOCKET. LOOSE. PARKING BRAKE DISCRETE LIGHT DOES NOT ILLUMINATE WHEN PARKING BRAKE SET FOUND PARKING BRAKE LIGHT BASE ASSY LOOSE, TIGHTEN BASE. LIGHT OPS CKED GOOD. A/C OK FOR
- [SDR FDEA202507191267](https://openairdocs.org/sdr/FDEA202507191267), Jul 19, 2025: SKIN. DAMAGED. WHILE PERFORMING INSPECTION ON THE #2 CARGO DOOR LWR CORNERS SKIN CUTOUT FWD AND AFT, FOUND A REPAIR ON THE AFT LOWER CORNER OF THE #2 CARGO DOOR AREA. AD2006-1
- [SDR FDEA202507141192](https://openairdocs.org/sdr/FDEA202507141192), Jul 14, 2025: FLOORBEAM. CORRODED. MCD STA 1640 SUPPORT BEAM BL 0.00 TO LBL 45.50 HAS CORROSION. REMOVED CORROSION AT STA 1640 SUPPORT BEAM BL 0.00 - LBL 45050 IAW SRM 51-10-02. FOUND OUT OF LIMI
- [SDR FDEA202507141191](https://openairdocs.org/sdr/FDEA202507141191), Jul 14, 2025: CREASE BEAM. CORRODED. CORROSION NOTED ON THE ATTACHMENT FRAME OF MAIN DECK FLOORBOARD # 252 MKF (RH MOST O/B) AT STA 1540 - 1620. REPAIRED FRAME ATTACHMENT (CREASE BEAM) AT MAIN CABI
- [SDR FDEA202507111182](https://openairdocs.org/sdr/FDEA202507111182), Jul 11, 2025: SEAT TRACK. CORRODED. CORROSION NOTED ON THE SEAT TRACK BASE AT LH STA 1200-1240 I/B OF FLOOR PNL 251 MCF. REMOVED AND REPLACED SEAT TRACK AT L/H STA 1180 TO 1240 LBL 45.50 IAW SRM 5
- [SDR FDEA202501270142](https://openairdocs.org/sdr/FDEA202501270142), Jan 27, 2025: LENS. DETACHED. L EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270140](https://openairdocs.org/sdr/FDEA202501270140), Jan 27, 2025: LENS. DETACHED. EXTERNAL LH EMER. LIGHT LENSE DETACHED. L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK ADD CLEARED
- [SDR FDEA202501150070](https://openairdocs.org/sdr/FDEA202501150070), Jan 15, 2025: BATTERY. FAILED. EMERGENCY LIGHTS FOR R1 DOOR AND CENTER COURIER AREA INOP. IAW AMM: 33-51-07-2 REMOVED AND REPLACED BATERYPACK ASSY FOR CHARGER ASSEMBLY M730. OPS CHECK GOOD.
- [SDR FDEA202412021762](https://openairdocs.org/sdr/FDEA202412021762), Dec 2, 2024: GUARD. DAMAGED. EMERGENCY EXIT LIGHTS ARE UNARMED WHEN EMERGENCY EXIT LIGHT SWITCH IS CLOSED. FOUND SWITCH GUARD SPRING LOAD OUTSIDE OF THE SWITCH, REPOSITIONED THE SPRING, PER
- [SDR FDEA202409211334](https://openairdocs.org/sdr/FDEA202409211334), Sep 21, 2024: SKIN. DENTED. INCOMING A/C DAMAGE JUST BELOW AND FWD OF THE MAIN CARGO DOOR. DENT MEASURING APPROX 2"X3" AND MAX DEPTH OF 0.0119. LOCATED 2" AFT OF FS460 JUST BELOW STR 18L. 
- [SDR FDEA202409111303](https://openairdocs.org/sdr/FDEA202409111303), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 252 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MWF ON VTMAE TRAVELER T24/1774253 IAW DRAWING SRZ-25
- [SDR FDEA202409111302](https://openairdocs.org/sdr/FDEA202409111302), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 251 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER T24/1774230 IAW DRAWING SRZ-25
- [SDR FDEA202409111301](https://openairdocs.org/sdr/FDEA202409111301), Sep 11, 2024: FLOORBOARD. DAMAGED. MAIN DECK FLOORGOARD PANEL 251MXF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MXF ON VTMAE TRAVELER #T24/1774251 IAW SRZ-25-005 REVISION R DRAW
- [SDR FDEA202408081109](https://openairdocs.org/sdr/FDEA202408081109), Aug 8, 2024: SKIN. CORRODED. FOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T038
- [SDR FDEA202407251057](https://openairdocs.org/sdr/FDEA202407251057), Jul 25, 2024: RELAY. FAILED. NOSE L/G COMPONENTS INSPECTION REQUIRED TO CONFIRM NO DAMAGES. NOSE GEAR COMPONENTS VISUAL INSPECTION PERFORMED. NO OBVIOUS DAMAGES OBSERVED. ALSO NOSE GEAR STE
- [SDR FDEA202407251056](https://openairdocs.org/sdr/FDEA202407251056), Jul 25, 2024: RELAY. FAILED. RUNWAY ENGINE START. INSTEAD OF STABILIZING AT IDLE, THE RPM AND THRUST INCREASED WITH NO THROTTLE INPUT AND THROTTLES AT IDLE AND CONTINUED TO INCREASE RAPIDLY
- [SDR FDEA202407211036](https://openairdocs.org/sdr/FDEA202407211036), Jul 21, 2024: BATTERY PACK. NO TEST. ON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT 
- [SDR FDEA202406230855](https://openairdocs.org/sdr/FDEA202406230855), Jun 23, 2024: BATTERY PACK. FAILED. DURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS
- [SDR FDEA202406010758](https://openairdocs.org/sdr/FDEA202406010758), Jun 1, 2024: SUPPORT. DAMAGED. L/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGE
- [SDR FDEA202405250726](https://openairdocs.org/sdr/FDEA202405250726), May 25, 2024: CONTROLLER. FAILED. AT FL400 CABIN ALT HIGH WARNING DONNED MASKS. RAN QRH. INITIATED EMERGENCY DESCENT. CABIN ALTITUDE RATE REACHED 2000 FT PER MIN DOWN AND HIGHEST ALTITUDE REACHE
- [SDR FDEA202404300520](https://openairdocs.org/sdr/FDEA202404300520), Apr 30, 2024: FAN. FAILED. OIL BURNING SMOKE BELOW 5000FEET WITH LOW POWER SETTING. R & R L/H RECIRCULATION FILTER AND FAN, REVERSED MEL 21-25-01-02 & MEL 21-58-07, RECONNECTED WIRE ON PL
- [SDR FDEA202404230272](https://openairdocs.org/sdr/FDEA202404230272), Apr 23, 2024: GIRT BAR. OUT OF ALIGNMENT. LIGHT ON LEFT CREW ENTRY DOOR INOP. FACT 23APR24 08:51 AMS AMM: 25-66-10-2 AMM: 25-66-11-2 RELAMP NO HELP. FOUND SLIDE VERY HARD TO ARM AND GIRTBAR FITTINGS NOT
- [SDR FDEA202404030435](https://openairdocs.org/sdr/FDEA202404030435), Apr 3, 2024: LAMP. BURNED OUT. L1 MAIN ENTRY DOOR SLIDE LIGHT IS BURNT OUT. REMOVED AND REPLACED BOTH BULBS AND PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00-2-0, TEST SATIS, A/C OK FOR SERVICE.
- [SDR FDEA202404010430](https://openairdocs.org/sdr/FDEA202404010430), Apr 1, 2024: SKIN. CORRODED. R / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN COR
- [SDR FDEA202403290410](https://openairdocs.org/sdr/FDEA202403290410), Mar 29, 2024: WEB. CORRODED. FWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT O
- [SDR FDEA202403290408](https://openairdocs.org/sdr/FDEA202403290408), Mar 29, 2024: FAIRING. GOUGED. SEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-0
- [SDR FDEA202403280399](https://openairdocs.org/sdr/FDEA202403280399), Mar 28, 2024: SEAT TRACK. CORRODED. MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO
- [SDR FDEA202403280391](https://openairdocs.org/sdr/FDEA202403280391), Mar 28, 2024: WINDOW. CRACKED. WHILE IN CRUISE FLIGHT FL360, CAPTAIN SIDE FRONT WINDSCREEN ARCED FOLLOWED BY SHATTERING WITH OUTER PAIN. RAN QRH, ARCING CONTINUED. POSSIBLE DEFORMED WINDOW WI
- [SDR FDEA202403270388](https://openairdocs.org/sdr/FDEA202403270388), Mar 27, 2024: SEAT TRACK. CORRODED. SEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1

All 1,396: https://openairdocs.org/model/boeing-757-23a/reports.md

## STCs that may be installed (OpenAirDocs) (5)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series
- [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series
- [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series

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