# Boeing 757-2B6 - Type: Aircraft model (FAA registry) - Registry code: 1384909 - Manufacturer (registry): BOEING - Model: 757-2B6 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 239 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-757-2b6 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 None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (30) As reported by operators and repair stations, by the model named in the report. - [SDR IXXA20191227029](https://openairdocs.org/sdr/IXXA20191227029), Dec 21, 2019: HINGE FITTING. CRACKED. MAINTENANCE REPORTS, DOOR HINGE ON THE L1 DOOR CRACKED. AIRCRAFT GROUNDED FOR FURTHER STRUCTURAL INSPECTION AND ENGINEERING REVIEW. AIRCRAFT GROUNDED +72 FOR UN - [SDR IXXA20161206194](https://openairdocs.org/sdr/IXXA20161206194), Dec 4, 2016: LIGHT. INOPERATIVE. LEFT EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE. RELAMPED LEFT EXTERIOR EMERGENCY ESCAPE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPL - [SDR IXXA20161110082](https://openairdocs.org/sdr/IXXA20161110082), Nov 5, 2016: SKIN. CRACKED. NR 1 ENGINE OUTBOARD COWL LOWER BIFURCATION SKIN IS CRACKED AND DELAMINATED. IAW 757 SRM 54-31-01 CRACK AND DELAMINATION ARE OUT OF LIMITS. #1 ENGINE OUTBOARD T - [SDR IXXA20160509021](https://openairdocs.org/sdr/IXXA20160509021), May 6, 2016: FLASHLIGHT. INOPERATIVE. LOWER FLASHLIGHT UNDER SUPERNUMERARY SEAT NOT RECEIVING POWER. DEFERRED IAW MEL 25-63-04-01. DEFERRED MX ITEM 47254 INITIATED. NO FLY DATE 05 17 2016. R & R EME - [SDR IXXA2016FA0000206](https://openairdocs.org/sdr/IXXA2016FA0000206), May 4, 2016: SKIN. DENTED. RIGHT FUSELAGE HAS A DENT FORWARD OF THE FORWARD CARGO DOOR BS 560, STR 24R GM014. MECHANCICALLY MEASURED DENTED AREA AT EXTERNAL FUSELAGE SKIN, FOUND TO BE WIT - [SDR IXXA20140612001](https://openairdocs.org/sdr/IXXA20140612001), Jun 12, 2014: SUPPORT ANGLE. CRACKED. NUMBER 2 NACELLE INSIDE PANEL 445AR-BR, OTBD OF DIAGONAL BRACE FWD ATTACH POINT. SUPPORT ANGLE AT FWD CHORD, CRACKED AT FASTENER HOLE TO EDGE. CRACK APPROX 1/4 - [SDR IXXA20140603002](https://openairdocs.org/sdr/IXXA20140603002), Jun 3, 2014: STRINGER. CRACKED. STATION 654 & 2 STRINGER 11L CRACKED 1/2 INCH. R & R CRACKED STRINGER SECTION IAW SERVICE BULLETIN 368-53-041 & SRM 53-00-03-B67. - [SDR FOTR3408712032012](https://openairdocs.org/sdr/FOTR3408712032012), Oct 29, 2012: SHEAR TIE. CORRODED. BS 1681, FRAME LOWER SHEAR TIE CORRODED ON AFT SIDE BETWEEN STRINGER 29R TO 29L. REPAIRED ON FAS WO 21197 NR 34087. - [SDR FOTR3456401042013](https://openairdocs.org/sdr/FOTR3456401042013), Oct 27, 2012: SKIN. DENTED. L3 DOOR SKIN HAS A DENT BETWEEN STR 15-16L. REPAIRED ON FAS WO 21197. - [SDR FOTR3456301042013](https://openairdocs.org/sdr/FOTR3456301042013), Oct 23, 2012: SKIN. DENTED. AT BS 405 BETWEEN STR 15 - 16L SKIN IS DENTED. REPAIRED FAS WO 21197. - [SDR FOTR3391612032012](https://openairdocs.org/sdr/FOTR3391612032012), Oct 4, 2012: SKIN. CORRODED. LT WING UPPER SURFACE HAS AREA OF CORROSION AT REAR SPAR 35" OTBD OF FUSELAGE BS 1060. REPAIRED ON FAS WO 21197, NR 33916. - [SDR FOTR3449012032012](https://openairdocs.org/sdr/FOTR3449012032012), Oct 3, 2012: FRAME. DAMAGED. BS 418, STR 8R, FRAME HAS EXISTING .1875 HOLE WITH NO ED. REPAIRED ON FAS WO 21197. - [SDR FOTR3431901042013](https://openairdocs.org/sdr/FOTR3431901042013), Oct 2, 2012: SKIN. DENTED. FUSELAGE SKIN DENTED, BS 600 STR 28 TO 29L. REPAIRED ON FAS WO 21197. - [SDR FOTR3398112032012](https://openairdocs.org/sdr/FOTR3398112032012), Sep 27, 2012: FRAME. CRACKED. FUSELAGE INTERIOR FRAME CRACKED AT BS 1640, STRINGER 14R. REPAIRED ON FAS WO 21197. - [SDR FOTR3387612032012](https://openairdocs.org/sdr/FOTR3387612032012), Sep 25, 2012: SKIN. DENTED. LT SIDE OF FUSELAGE SKIN HAS SEVERAL DENTS BS 1681 TO 1720, STRINGER 14L TO STRINGER 20L. REPAIRED ON FAS WO 21197 NR 33876. - [SDR FOTR3429912032012](https://openairdocs.org/sdr/FOTR3429912032012), Sep 20, 2012: INTERCOSTAL. CORRODED. AFT PIT BILGE AREA, INTERCOSTAL LOWER ANGLE HAS CORROSION AT BS 1475, RBL14. REPAIRED ON FAS WO 21197. - [SDR FOTR3410901042013](https://openairdocs.org/sdr/FOTR3410901042013), Sep 19, 2012: SKIN. CORRODED. LEFT WING UPPER SURFACE SKIN HAS AREA OF CORROSION AT BS 1003, 4 INCHES OTBD OF FUSELAGE. REPAIRED ON FAS WO 21197. - [SDR FOTR3430112032012](https://openairdocs.org/sdr/FOTR3430112032012), Sep 18, 2012: SHEAR TIE. CORRODED. AFT PIT BILGE AREA, SHEAR TIE AT BS 1440 RBL 3 HAS CORROSION ON FWD SIDE. REPAIRED ON FAS WO 21197. - [SDR FOTR3384612032012](https://openairdocs.org/sdr/FOTR3384612032012), Sep 16, 2012: SKIN. DENTED. LOWER FUSELAGE SKIN HAS A DENT AT BS 1654 BETWEEN STRINGER 27L AND 28L. REPAIRED ON FAS WO 21197, NR 33846. - [SDR FOTR3420412032012](https://openairdocs.org/sdr/FOTR3420412032012), Sep 15, 2012: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK AT LBL 45, BS 874 TO 900 HAS SEVERAL GOUGES ON UPPER SURFACE. REPAIRED ON FAS WO 21197 N34204. - [SDR FOTR3384912032012](https://openairdocs.org/sdr/FOTR3384912032012), Sep 12, 2012: SKIN. DENTED. LOWER FUSELAGE SKIN HAS A DENT AT BS 1780 JUST BELOW STR 26L. REPAIRED ON FAS WO 21197 NR 33849. - [SDR FOTR3386501042013](https://openairdocs.org/sdr/FOTR3386501042013), Sep 11, 2012: SKIN. DENTED. RIGHT SIDE OF FUSELAGE SKIN HAS A DENT AT BS 725 BETWEEN STRINGERS 20R AND 21R. REPAIRED ON FAS WO 21197, NR 33865. - [SDR FOTR3418312032012](https://openairdocs.org/sdr/FOTR3418312032012), Sep 8, 2012: TEAR STRAP. DAMAGED. SCRIBE LINE ON TEAR STRAP AT BS 660 BETWEEN STR 8L-10L. REPAIRED ON FAS WO 21197, NR34183. - [SDR FOTR3426012032012](https://openairdocs.org/sdr/FOTR3426012032012), Sep 6, 2012: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT BS 820 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197. - [SDR FOTR3426112032012](https://openairdocs.org/sdr/FOTR3426112032012), Sep 1, 2012: SHEAR TIE. CORRODED. FWD PIT-CORROSION ON SHEAR TIE AT BS 800 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197. - [SDR FOTR2012090134261](https://openairdocs.org/sdr/FOTR2012090134261), Sep 1, 2012: SHEAR TIE. CORRODED. FWD PIT-- CORROSION ON SHEAR TIE AT STA 800 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197 NR 24261. - [SDR FOTR3420012032012](https://openairdocs.org/sdr/FOTR3420012032012), Aug 8, 2012: FLOORBEAM. CORRODED. FLOORBEAM AT BS 395 RBL 51 HAS CORROSION ON UPPER FLANGE. REPAIRED ON FAS WO 21197. - [SDR FOTR3419412032012](https://openairdocs.org/sdr/FOTR3419412032012), Aug 7, 2012: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK HAS DAMAGED UPPER LUG AT BS 1190, RBL 24. REPAIRED ON FAS WO 21197 NR 34194. - [SDR FOTR3401512032012](https://openairdocs.org/sdr/FOTR3401512032012), Aug 3, 2012: STRINGER. CRACKED. STRINGER 2L CRACKED AT BS 336. REPAIRED ON FAS WO 21197. - [SDR FOTR3406321197](https://openairdocs.org/sdr/FOTR3406321197), Jul 3, 2012: SKIN. DENTED. LOWER FUSELAGE SKIN HAS A DENT AT BS 592 BETWEEN STRINGER 26 TO 27L. REPAIRED ON FAS WO 21197. --- 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.