# Service difficulty reports: Boeing 757-2B6 A list on [Boeing 757-2B6](https://openairdocs.org/model/boeing-757-2b6.md). Newest first. General aviation reporting is voluntary. - [SDR IXXA20191227029](https://openairdocs.org/sdr/IXXA20191227029.md): Hinge Fitting · cracked · Dec 21, 2019 · N557CM · Boeing 7572B6 · Fuselage, Door Hinge > MAINTENANCE REPORTS, DOOR HINGE ON THE L1 DOOR CRACKED. AIRCRAFT GROUNDED FOR FURTHER STRUCTURAL INSPECTION AND ENGINEERING REVIEW. AIRCRAFT GROUNDED +72 FOR UNSCHEDULED MAINTENANCE. ENGINEERING REVIEW COMPLIED WITH. REMOVED DOOR ASSEMBLY TO FACILITATE MAINTEN - [SDR IXXA20161206194](https://openairdocs.org/sdr/IXXA20161206194.md): Light · inoperative · Dec 4, 2016 · N557CM · Boeing 7572B6 · Emergency Lighting > LEFT EXTERIOR EMERGENCY ESCAPE LIGHT INOPERATIVE. RELAMPED LEFT EXTERIOR EMERGENCY ESCAPE LIGHT IAW AMM 33-51-06. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE. - [SDR IXXA20161110082](https://openairdocs.org/sdr/IXXA20161110082.md): Skin · cracked · Nov 5, 2016 · N557CM · Boeing 7572B6 · Engine Thrust Reverser > 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 THRUST REVERSER COWL WAS REMOVED AND REPLACED IAW 757 AMM 78-31-01. OPERATIONAL CHECK SATISFACTORY. A - [SDR IXXA20160509021](https://openairdocs.org/sdr/IXXA20160509021.md): Flashlight · inoperative · May 6, 2016 · N557CM · Boeing 7572B6 · Emergency Equipment > 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 EMER FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECKED SATISFACTORY. DMI CLEARED & ACFT RELEASED T - [SDR IXXA2016FA0000206](https://openairdocs.org/sdr/IXXA2016FA0000206.md): Skin · dented · May 4, 2016 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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 WITHIN 2" OF FORWARD LOWER CARGO DOOR CUTOUT AND OUT OF LIMITS IAW SRM 757-200, CHAPTER 53-00-01, FIGU - [SDR IXXA20140612001](https://openairdocs.org/sdr/IXXA20140612001.md): Support Angle · cracked · Jun 12, 2014 · N557CM · Boeing 7572B6 · Nacelle/Pylon Miscellaneous Structure > 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 INCH VERIFIED BY HFEC. CRACK LENGTH.6 INCHES, LOCATION NAC STATION 206.00 TO N/A. PART NAME BRAC - [SDR IXXA20140603002](https://openairdocs.org/sdr/IXXA20140603002.md): Stringer · cracked · Jun 3, 2014 · N557CM · Boeing 7572B6 · Fuselage Main, Longeron/Stringer > 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.md): Shear Tie · corroded · Oct 29, 2012 · N557CM · Boeing 7572B6 · Fuselage Internal Mounting Structure > 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.md): Skin · dented · Oct 27, 2012 · N557CM · Boeing 7572B6 · Passenger/Crew Doors > L3 DOOR SKIN HAS A DENT BETWEEN STR 15-16L. REPAIRED ON FAS WO 21197. - [SDR FOTR3456301042013](https://openairdocs.org/sdr/FOTR3456301042013.md): Skin · dented · Oct 23, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > AT BS 405 BETWEEN STR 15 - 16L SKIN IS DENTED. REPAIRED FAS WO 21197. - [SDR FOTR3391612032012](https://openairdocs.org/sdr/FOTR3391612032012.md): Skin · corroded · Oct 4, 2012 · N557CM · Boeing 7572B6 · Wing, Plate/Skin > 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.md): Frame · damaged · Oct 3, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Frame > BS 418, STR 8R, FRAME HAS EXISTING.1875 HOLE WITH NO ED. REPAIRED ON FAS WO 21197. - [SDR FOTR3431901042013](https://openairdocs.org/sdr/FOTR3431901042013.md): Skin · dented · Oct 2, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED, BS 600 STR 28 TO 29L. REPAIRED ON FAS WO 21197. - [SDR FOTR3398112032012](https://openairdocs.org/sdr/FOTR3398112032012.md): Frame · cracked · Sep 27, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Frame > FUSELAGE INTERIOR FRAME CRACKED AT BS 1640, STRINGER 14R. REPAIRED ON FAS WO 21197. - [SDR FOTR3387612032012](https://openairdocs.org/sdr/FOTR3387612032012.md): Skin · dented · Sep 25, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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.md): Intercostal · corroded · Sep 20, 2012 · N557CM · Boeing 7572B6 · Fuselage Miscellaneous Structure > 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.md): Skin · corroded · Sep 19, 2012 · N557CM · Boeing 7572B6 · Wing, Plate/Skin > 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.md): Shear Tie · corroded · Sep 18, 2012 · N557CM · Boeing 7572B6 · Fuselage Internal Mounting Structure > 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.md): Skin · dented · Sep 16, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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.md): Seat Track · gouged · Sep 15, 2012 · N557CM · Boeing 7572B6 · Fuselage, Seat/Cargo Attach Fittings > 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.md): Skin · dented · Sep 12, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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.md): Skin · dented · Sep 11, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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.md): Tear Strap · damaged · Sep 8, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > 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.md): Shear Tie · corroded · Sep 6, 2012 · N557CM · Boeing 7572B6 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT BS 820 BETWEEN STR 28L-28R. REPAIRED ON FAS WO 21197. - [SDR FOTR3426112032012](https://openairdocs.org/sdr/FOTR3426112032012.md): Shear Tie · corroded · Sep 1, 2012 · N557CM · Boeing 7572B6 · Fuselage Internal Mounting Structure > 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.md): Shear Tie · corroded · Sep 1, 2012 · N557CM · Boeing 7572B6 · Fuselage Internal Mounting Structure > 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.md): Floorbeam · corroded · Aug 8, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Floor Beam > FLOORBEAM AT BS 395 RBL 51 HAS CORROSION ON UPPER FLANGE. REPAIRED ON FAS WO 21197. - [SDR FOTR3419412032012](https://openairdocs.org/sdr/FOTR3419412032012.md): Seat Track · damaged · Aug 7, 2012 · N557CM · Boeing 7572B6 · Fuselage, Seat/Cargo Attach Fittings > 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.md): Stringer · cracked · Aug 3, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Longeron/Stringer > STRINGER 2L CRACKED AT BS 336. REPAIRED ON FAS WO 21197. - [SDR FOTR3406321197](https://openairdocs.org/sdr/FOTR3406321197.md): Skin · dented · Jul 3, 2012 · N557CM · Boeing 7572B6 · Fuselage Main, Plate/Skin > LOWER FUSELAGE SKIN HAS A DENT AT BS 592 BETWEEN STRINGER 26 TO 27L. REPAIRED ON FAS WO 21197. ## 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 = '7572B6' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-757-2b6/reports --- 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.