# Boeing 757-2B7 - Type: Aircraft model (FAA registry) - Registry code: 1384964 - Manufacturer (registry): BOEING - Model: 757-2B7 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 178 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 5 - Page: https://openairdocs.org/model/boeing-757-2b7 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 (5) - [N627NP](https://openairdocs.org/aircraft/N627NP): [Firedancer Asset Holding V LLC](https://openairdocs.org/faa-owner/FIREDANCER%20ASSET%20HOLDING%20V%20LLC), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), built 1995, S/N 27808 - [N628NP](https://openairdocs.org/aircraft/N628NP): [Jmac Inc](https://openairdocs.org/faa-owner/JMAC%20INC), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), built 1995, S/N 27809 - [N901FD](https://openairdocs.org/aircraft/N901FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1993, S/N 27122 - [N903FD](https://openairdocs.org/aircraft/N903FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1993, S/N 27124 - [N939UW](https://openairdocs.org/aircraft/N939UW): [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables), built 1994, S/N 27303 ## NTSB investigations (2) 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 DCA19CA066](https://openairdocs.org/ntsb/DCA19CA066), Dec 31, 2018: Boeing 757 (N938UW), Charlotte, NC, substantial damage. Probable cause: an inadvertent loss of airspeed and increased pitch attitude prior to touchdown. - [NTSB DCA12CA086](https://openairdocs.org/ntsb/DCA12CA086), Jun 7, 2012: Boeing 757 2B7 (N936UW), Philadelphia, PA, no damage. Probable cause: an inadvertent encounter with convective turbulence. ## 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 20140429005209I](https://openairdocs.org/incident/20140429005209I), Apr 29, 2014: Boeing 757-2B7 (N936UW), Richmond, VA, No damage. On April 29, 2014, at approximately 1939 UTC, usairways flight 815, a Boeing B-757, encountered severe clear air turbulence in the vicinity of flat rock VOR… - [Accident 20120607010549A](https://openairdocs.org/incident/20120607010549A), Jun 7, 2012: Boeing 757-2B7 (N936UW), Atlantic City, NJ, No damage. During descent into philadelphia international airport, the flight encountered moderate turbulence while descending through clouds between 10,000-12,000 feet.… ## Service difficulty reports (3,730, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA202607110913](https://openairdocs.org/sdr/FDEA202607110913), Jul 11, 2026: CONTROL VALVE. ODOR. FUME EVENT DESCEND THROUGH 20-25K. IT WAS A DIRTY OILY SOCK SMELL. PERFORMED INSPECTION OF HIGH PRESSURE DUCT & INTERMEDIATE PRESSURE DUCT ON BOTH ENGINES. REMO - [SDR FDEA202605300654](https://openairdocs.org/sdr/FDEA202605300654), May 30, 2026: STOWAGE BOX. DAMAGED. WHILE PRE FLIGHTING AC FOUND CAPTS O2 MASK BOX TEST BUTTON BROKEN. REMOVED AND REPLACED CAPTS 02 MASK STOWAGE BOX PER 757 AMM 35-11-51-4-99. OPS CHECK GOOD. MVP - [SDR FDEA202604250500](https://openairdocs.org/sdr/FDEA202604250500), Apr 25, 2026: CIRCUIT BREAKER. TRIPPED. LEFT AND RIGHT FUEL OVERRIDE CIRCUIT BREAKERS ARE TRIPPED ON PREFLIGHT. REINSTALLED THE P33 PANEL. AWAITING RETEST REQUIREMENTS FROM ENGINEERING IAW AMM: 20-11- - [SDR FDEA202602100158](https://openairdocs.org/sdr/FDEA202602100158), Feb 10, 2026: SKIN. CRACKED. ENG # 1 NACELLE STRUT UPPER WING SURFACE SPAR MID-SPAR ATTACH FITTING HAS A BOLT MIGRATED THIS ITEM HAS BEEN ACCOMPLISHED FOLLOWING WORK INSTRUCTIONS AS PER EA - [SDR FDEA202602070144](https://openairdocs.org/sdr/FDEA202602070144), Feb 7, 2026: WEDGE. DAMAGED. NUMBER 9 LEADING EDGE SLAT WEDGE DEBONDED, TWO PLACES. APPLIED A PERMANENT REPAIR TO NR 9 LE SLAT EDGE WEDGE IAW SRM 51-70-10-2R R ESTORED SURFACE IN REPAIRED A - [SDR FDEA202602070143](https://openairdocs.org/sdr/FDEA202602070143), Feb 7, 2026: WEDGE. DAMAGED. NUMBER 7 LEADING EDGE SLAT WEDGE DEBONDED. REPAIRED NR 7 LEADING EDGE SLAT IAW SRM 51-70-10-2R.TAP TEST RESULTED SATIFACTORY IAW SRM 51-10-06-2R. - [SDR FDEA202602040127](https://openairdocs.org/sdr/FDEA202602040127), Feb 4, 2026: STRINGER. DAMAGED. REMOVE EXISTING REPAIR AT STA 1656 ON STRINGER 26L REPAIRED STRINGER SECTION AT BS 1640 11" TO BS1660 10" STR 26L, IAW B757 SRM 53-00-03-2R, FIG 201, DETAIL I A - [SDR FDEA202601300106](https://openairdocs.org/sdr/FDEA202601300106), Jan 30, 2026: FLOOR SUPPORT. MECHANIC ERROR. AFT CARGO FLOOR SUPPORT, BS 1465 MISDRILLED HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT, IAW SRM 51-40-02-0G AND SRM 53-60-53-01, FIG 1, DET VII. - [SDR FDEA202601300105](https://openairdocs.org/sdr/FDEA202601300105), Jan 30, 2026: FLOOR SUPPORT. MECHANIC ERROR. AFT CARGO FLOOR SUPPORT, LBL 7.55 BTW BS 1480 TO 1500 MISDRILLED HOLES REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G AND SRM 53-60-53-0I FIG 1 DET - [SDR FDEA202601280095](https://openairdocs.org/sdr/FDEA202601280095), Jan 28, 2026: SKIN. DENTED. UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 TWO DENTS, APPLIED PERMANENT REPAIR AT UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 IAW SRM 53-80-01-1A, FIG 101, SHEET 2 - [SDR FDEA202601190068](https://openairdocs.org/sdr/FDEA202601190068), Jan 19, 2026: SKIN. CORRODED. NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 134.76 CORRODED. THIS ITEM HAS BEEN ACCOMPLISHED ON EA # F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- - [SDR FDEA202601190067](https://openairdocs.org/sdr/FDEA202601190067), Jan 19, 2026: SKIN. CORRODED. NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 200.50 SUSPECTED CORROSION. ACCOMPLISHED ON EA F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATE - [SDR FDEA202512162256](https://openairdocs.org/sdr/FDEA202512162256), Dec 16, 2025: BATTERY PACK. NO TEST. L1 EMERGENCY EXIT LIGHT FAILS TO TEST DURING PRE-FLT. REMOVED AND REPLACED THE BATTERY PACK FOR THE L 1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-07-2 EMERGENCY E - [SDR FDEA202511212196](https://openairdocs.org/sdr/FDEA202511212196), Nov 21, 2025: BULB. FAILED. R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2. OPS CHKD SERVICEABLE. - [SDR 7C7A2025101200043](https://openairdocs.org/sdr/7C7A2025101200043), Oct 12, 2025: BATTERY PACK. INOPERATIVE. FWD GALLEY EMERGENCY LIGHT INOP. - [SDR 7C7A2025100300042](https://openairdocs.org/sdr/7C7A2025100300042), Oct 3, 2025: STOP FITTING. GOUGED. L4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED. - [SDR 7C7A1900010000041](https://openairdocs.org/sdr/7C7A1900010000041), Oct 2, 2025: SLEEVE. DENTED. NR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE. - [SDR 7C7A2025100200040](https://openairdocs.org/sdr/7C7A2025100200040), Oct 2, 2025: HEAT SHIELD. CRACKED. LEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED. - [SDR FDEA202509261839](https://openairdocs.org/sdr/FDEA202509261839), Sep 26, 2025: ACTUATOR. FAILED. ON TAKE OFF OUT OF MEM, LANDING GEAR WOULD NOT RETRACT. RAN QRH, LANDING GEAR RETRACTED WITH LOCK OVERRIDE. LANDING GEAR EXTENDED NORMALLY ON APPROACH INTO FSD. - [SDR FDEA202509261838](https://openairdocs.org/sdr/FDEA202509261838), Sep 26, 2025: PACKING. FAILED. TAKEOFF ROTATION ON DEPARTURE IN MEM DID NOT FEEL NORMAL. IT FELT LIKE THE GEAR TRUCKS DID NOT TILT. AMM: 32-32-15-4 ON INSPECTION OF LEFT TRUCK TILT ACTUATOR, - [SDR 7C7A2025091800039](https://openairdocs.org/sdr/7C7A2025091800039), Sep 18, 2025: APU. OIL CONSUMPTION. HIGH OIL CONSUMPTION AUTO SHUTDOWN ACTIVATED - [SDR FDEA202508261543](https://openairdocs.org/sdr/FDEA202508261543), Aug 26, 2025: BATTERY. INOPERATIVE. DURING MX PRE-FLIGHT FOUND OVERHEAD EMERGENCY LIGHTS AT CENTER, AND R1 DOOR AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE BATTERY FOR OVER AN HOUR, NO FIX. RE - [SDR 7C7A2025081600038](https://openairdocs.org/sdr/7C7A2025081600038), Aug 16, 2025: ACCESS PANEL. DELAMINATED. RIGHT UPPER WING ACCESS PANEL 611KT FOUND DELAMINATED. - [SDR 7C7A2025081600037](https://openairdocs.org/sdr/7C7A2025081600037), Aug 16, 2025: HYDRAULIC LINE. GOUGED. LEFT NACELLE REVERSE FLOW CHECK CONTROL LINE FOUND GOUGED. - [SDR 7C7A2025081600036](https://openairdocs.org/sdr/7C7A2025081600036), Aug 16, 2025: SIGN. INOPERATIVE. AFT GALLLEY RIGHT SIDE EMERGENCY EXIT SIGN INOPERATIVE, WON'T TURN ON. - [SDR 7C7A2025081600035](https://openairdocs.org/sdr/7C7A2025081600035), Aug 16, 2025: SIGN. INOPERATIVE. L3 DOOR EXIT IND SIGN INOPERATIVE. - [SDR 7C7A1900010000034](https://openairdocs.org/sdr/7C7A1900010000034), Aug 16, 2025: SIGN. NO TEST. R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC, AND EXIT SIGN INOPERATIVE, NO TEST. - [SDR 7C7A2025081600033](https://openairdocs.org/sdr/7C7A2025081600033), Aug 16, 2025: SKIN. DENTED. RIGHT WING NR 6 SLAT TRAILING EDGE UPPER SKIN. - [SDR 7C7A2025081600032](https://openairdocs.org/sdr/7C7A2025081600032), Aug 16, 2025: SKIN. DEBONDED. RIGHT UPPER SURFACE SKIN PATCH DE-BONDED. - [SDR 7C7A2025081500031](https://openairdocs.org/sdr/7C7A2025081500031), Aug 15, 2025: FAIRING. DAMAGED. EVIDENCE OF DAMAGE AT EDGE OF CANOE PANEL 672HB. - [SDR 7C7A1900010000030](https://openairdocs.org/sdr/7C7A1900010000030), Aug 15, 2025: SKIN. DAMAGED. RIGHT WINGTIP HAS LIGHTING STRIKE. - [SDR 7C7A1900010000029](https://openairdocs.org/sdr/7C7A1900010000029), Aug 15, 2025: SKIN. DENTED. DENT ON FUSELAGE SKIN STA 846 BETWEEN S-4L AND S-5L. - [SDR 7C7A1900010000028](https://openairdocs.org/sdr/7C7A1900010000028), Aug 14, 2025: SKIN. DENTED. VERTICAL STABILIZER LH LOWER SIDE OF RUDDER HAS DENT - [SDR 7C7A1900010000027](https://openairdocs.org/sdr/7C7A1900010000027), Aug 14, 2025: SKIN. DENTED. DENT ON PREVIOUS BLEND ON FUSELAGE SKIN AT STA 481 BETWEEN STR 27L-28-L. - [SDR 7C7A2025081300026](https://openairdocs.org/sdr/7C7A2025081300026), Aug 13, 2025: SKIN. DENTED. DENT ON FUSELAGE SKIN STA 1697 BETWEEN S-18L AND S-19L. - [SDR 7C7A202508130001](https://openairdocs.org/sdr/7C7A202508130001), Aug 13, 2025: HINGE. DAMAGED. LH ENG OB LOWER BLOCKER FLAP #6 FROM 12 OCLOCK POSITION LOWER HINGE ATTACHEMENT PLATE HAS MISSING PIECE - [SDR 7C7A1900010000024](https://openairdocs.org/sdr/7C7A1900010000024), Aug 13, 2025: SKIN. DENTED. DENT ON FUSELAGE SKIN AT STA 531 BETWEEN STR 28L AND 28R - [SDR 7C7A1900010000023](https://openairdocs.org/sdr/7C7A1900010000023), Aug 9, 2025: BATTERY PACK. NO TEST. R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC INOP LIGHT ALONG WITH EXIT SIGN. - [SDR 7C7A2025080600022](https://openairdocs.org/sdr/7C7A2025080600022), Aug 6, 2025: SWITCH. BROKEN. DURING INSTALLATING AFT 3 LH DOOR LINNERS FJOUND SLIDE LIGHT INDICATIO SWITCH BROKEN - [SDR 7C7A1900010000021](https://openairdocs.org/sdr/7C7A1900010000021), Aug 2, 2025: LIGHT. BROKEN. DURING INSTALLING AFT 4 R/H DOOR LINERS FOUND SLIDE LIGHT INDICATOR SWITCH CONNECTOR BROKEN - [SDR 7C7A1900010000020](https://openairdocs.org/sdr/7C7A1900010000020), Aug 2, 2025: BATTERY. DISCHARGED. EMERGENCY MARKER AT R3 DOOR INOPERATIVE. - [SDR 7C7A1900010000019](https://openairdocs.org/sdr/7C7A1900010000019), Aug 2, 2025: FUSE. FAILED. AFT GALLEY R/H SIDE EMERGENCY EXIT MAKER INOP - [SDR FDEA202507201277](https://openairdocs.org/sdr/FDEA202507201277), Jul 20, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 440 TO BS 640 LBL 24.75 WITH MULTIPLE SPOTS CORRODED UPPER / LOWER FLANGE SURFACE. - [SDR FDEA202506281076](https://openairdocs.org/sdr/FDEA202506281076), Jun 28, 2025: SUPPORT BEAM. CORRODED. CARGO COMPARTMENT SUPPORT BEAM LOWER CHORD BS 1360 BETWEEN RBL 24.75 AND RBL 45.50 NUTS PLATE WITH CORROSION. - [SDR FDEA202506281075](https://openairdocs.org/sdr/FDEA202506281075), Jun 28, 2025: SHEAR TIE. CORRODED. AFT CARGO MCOMPARTMENT SHEAR TIE CORRODED AT BS 1480 BETWEEN STRINGER 28R - STR29R. - [SDR FDEA202506281074](https://openairdocs.org/sdr/FDEA202506281074), Jun 28, 2025: SHEAR TIE. CORRODED. AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 1500 BETWEEN STR 28R - STR 29R. - [SDR FDEA202506271067](https://openairdocs.org/sdr/FDEA202506271067), Jun 27, 2025: SUPPORT. CORRODED. AFT CARGO COMPARTMENT CEILING SUPPORT HAS CORROSION BETWEEN BS 1400.0 TO BS 1420.0 RBL 24.75. - [SDR FDEA202506271066](https://openairdocs.org/sdr/FDEA202506271066), Jun 27, 2025: SUPPORT. CORRODED. AFT CARGO COMPARTMENT CEILING PANEL SUPPORT HAS CORROSION BETWEEN BS 1400.0 TO BS 1420 RBL 45.50. - [SDR FDEA202506261063](https://openairdocs.org/sdr/FDEA202506261063), Jun 26, 2025: FLOORBEAM. CORRODED. MCC FLOOR BEAM SUPPORT UPPER HAS CORROSION RBL 8 -14 STA 560. PERFORMED FLOOR BEAM REPAIR AT MCC STA 560 FROM RBL 15.8 TO LBL 11.1 ON UPPER CHORD IAW B 757 SRM - [SDR FDEA202506261062](https://openairdocs.org/sdr/FDEA202506261062), Jun 26, 2025: BATTERY PACK. INOPERATIVE. CENTER AND RIGHT EMERGENCY EXIT SIGNS IN GALLEY FAIL TO LIGHT WHEN TESTED FOR SERVICE CHECK. AMM: 33-51-07-2 REMOVED AND REPLACED FOWARD GALLEY EMERGENCY LIGHTI All 3,730: https://openairdocs.org/model/boeing-757-2b7/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.