Boeing 757-231

Service difficulty reports · 1,658

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duckdb -csv -c "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 = '757231'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2015111807028Fastener · looseMISSING, LOOSE, CORRODED FASTENERS, SEEM JUST FORWARD OF LT & RT PAC BAYS. MARKED. REPLACED AND SECURED FASTENERS IAW SRM 51-10-02.Nov 18, 2015 · N722TW · Boeing 757231 · Fuselage Main, Plate/SkinSDR DALA2015111807029Skin · dentedNR 1 SLAT HAS NUMEROUS UNIDENTIFIED DENTS, SLAT UPPER T/E WEDGE. INSPECTED NR 1 SLAT FOUND NUMEROUS DENTS, ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON RC 56-0557-8-0072 . NR 1 SLAT NEEDS TO BE ADDED TO MONITOR INSP. INSTALLED I/D TAG ONov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807027Skin · dentedNR 10 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 10 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST CW ON R/C 56-0557-8- 0072. NR 10 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED I/DNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807026Skin · dentedNR 9 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 9 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 9 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED ID TAGNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807025Skin · dentedNR 8 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 8 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 8 SLAT NEEDS TO ADDED TO MONITOR INSPECTION, INSTALLED TAG ON SNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807024Skin · dentedNR 7 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER TE WEDGE. INSPECTED NR 7 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 7 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED ID TAG Nov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807023Skin · dentedNR 6 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 6 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 6 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION. INSTALLED ID TNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807022Skin · dentedNR 5 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 5 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 5 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION INSTALLED I/D TANov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807021Skin · dentedNR 4 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER TE WEDGE. INSPECTED NR 4 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072. NR 4 SLAT NEEDS TO BE ADDED TO MONTOR INSPECTION. INSTALLED ID TAGNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807020Skin · dentedNR 3 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 3 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON R/C 56-0557-8-0072 . NR 3 SLAT NEEDS TO BE ADDED TO MONITOR INSPECTION. INSTALLED ID TAGNov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015111807019Skin · damagedNR 2 SLAT HAS NUMEROUS UNIDENTIFIED DENTS SLAT UPPER T/E WEDGE. INSPECTED NR 2 SLAT FOUND NUMEROUS DENTS ALL ARE IN LIMITS OF SRM 57-43-02. TAP AND DELAMATION TEST C/W ON RC 56-0557-8-0072. NR 2 SLAT NEEDS TO BE ADDED TO MONTOR INSPECTION INSTALLED ID TAG ONov 17, 2015 · N722TW · Boeing 757231 · Leading Edge DevicesSDR DALA2015110906918Skin · dentedUPPER FUSELAGE SKIN HAS DENT AT BS 760- 800, S8R TO S9R. INSPECTED AND MEASURED DENT ON EXTERIOR FUSELAGE BS 760 TO 800, STR 8R-9R A/Y=100, FOUND WITH IN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III.Nov 10, 2015 · N727TW · Boeing 757231 · Fuselage Main, Plate/SkinSDR DALA2015110106687Line · failedCREW PERFORMED ATB DUE TO LT HYD SYS FAILURE. NR 5 AND NR 6 TIRES ALSO FOUND TO HAVE FAILED. DECLARED AN EMERGENCY WITH ATC, ARFF MET THE ACFT AFTER STOPPING ON THE RUNWAY, AND ACFT WAS TOWED OFF THE RUNWAY. REPLACED A HYDRAULIC LINE FROM THE TILT PRESSURE Nov 1, 2015 · N721TW · Boeing 757231 · Hydraulic System, MainSDR DALA2015102206749Floorbeam · corrodedMAIN CABIN FWD WET AREA, CORROSION ON FLOORBEAM AT BS 365 FRAME IN BL0 TO RBL28. CP53-222-01. REMOVED CORROSION AT MAIN CABIN FWD WET AREA ON FLOORBEAM AT BS 3C5 FROM BL0 TO RBL 28 IAW SRM 51-10-02. EVALUATED AREA WITH DIGITAL CALIPER FOUND TO BE OUT LIMIT Oct 31, 2015 · N711ZX · Boeing 757231 · Fuselage Main, Floor BeamSDR DALA2015102906610Strut · corrodedRUST EMANATING FROM NLG LOWER DRAG STRUT ATTACH PIN AT STRUT ATRH ATTACHMENT TO OUTER CYLINDER. REPLACED NLG LOWER DRAG STRUT ATTACH PIN IAW AMM 32-21-03. UNSERVICE AND SERVICE STRUT IAW AMM 12-15-02.Oct 28, 2015 · N717TW · Boeing 757231 · Nose/Tail Landing Gear Strut/AxleSDR DALA2016102110232Skin · damagedFUSELAGE SKIN REPAIR AT FS 293, BETWEEN S-18R AND S-19R. REF ERA 540714-14 FOR REPAIR.Oct 26, 2015 · N717TW · Boeing 757231 · Fuselage Main, Plate/SkinSDR DALA2015102306487Ball Screw · corrodedWHILE WORKING AN INSPECTION, RT INBD T/E FLAP BALLSCREW RT INBD T/E FLAP INBD BALLSCREW FOUND CORRODED. REMOVED RT INBD FLAP INBD BALLSCREW IAW AMM 27-51-11 . OFF PN, OFF SN 5467, OK TO INSTALL BALLSCREW ASSY IAW AMM 27- 51-11, PN 7821344, SN DL 15. REPLACED Oct 22, 2015 · N717TW · Boeing 757231 · Trailing Edge FlapsSDR DALA2015102206391Ball Screw · corrodedLT INBD T/E FLAP BALLSCREW CORROSION FOUND. SUMMARY, NR FOR ADDITIONAL INFORMATION 001-0067:2751-2539-LT/001 00195. REPLACED BALLSCREW ASSY IAW AMM 27-51-11. OPS TEST C/W ON R/C 2751-2538, STEP 18.Oct 21, 2015 · N717TW · Boeing 757231 · Trailing Edge Flap Control SystemSDR FDEA201510143201Door Seal · out of adjustR1 DOOR SLIDE DOES NOT ARM PROPERLY. FOUND INNER SEAL COMING LOOSE & CAUSING DOOR NOT TO ARM PROPERLY. ADJUSTED DOOR SEAL & REINSTALLED. DOOR OPERATES NORMAL IAW MM 52-71-00-5-0.Oct 14, 2015 · N989FD · Boeing 757231 · Passenger/Crew DoorsSDR DALA2015100205937Bottle · low pressureDURING SERVICE CHECK, FOUND 1L DOOR ASSIST BOTTLE PRESSURE IN RED BAND. R & R 1L DOOR ASSIST BOTTLE WITH A SERVICEABLE UNIT IAW AMM 52-11 AS REQUIRED.Oct 1, 2015 · N711ZX · Boeing 757231 · Passenger/Crew DoorsSDR DALA2015092805862Light · unsecureEMERGENCY AISLE LIGHT FIXTURE IS LOOSE/STICKING OUT AT SEAT 18D. RESECURED BRACKET. OPS NORMAL.Sep 26, 2015 · N722TW · Boeing 757231 · Emergency LightingSDR DALA2015090705487Floor Support · damagedSUPPORT BRACKET BELOW FLOOR PANEL IN E/E ADJACENT TO P37 PANEL DAMAGED. REPLACED FLOOR SUPPORT IN E/E PN 284N 1035-256, REF DWG 2841392, FLOOR PANELS AND COVERS INSTALLED.Sep 4, 2015 · N727TW · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015081805029Gcu · odorFUMES AFTER STARTING LT ENGINE START CREW NOTED EICAS RT AC BUS OFF WITH CIRCUIT BREAKER ON P6-1 PANEL ROW G5 POPPED. F/A ALSO SMELLED AN ELECTRICAL ODOR IN AFT CABIN. AFTER APU WAS RESTARTED THE RT AC BUS CAME BACK ON LINE. RETURNED TO THE GATE. REPLACED Aug 16, 2015 · N717TW · Boeing 757231 · AC Generation SystemSDR DALA2015080204785Floor Panel · puncturedA ONE INCH HOLE IN THE AFT CARGO FLOOR FIVE FEET FWD OF OF DOOR. INSTALLED TEMP REPAIR IAW ERA 489384-14MA.Jul 26, 2015 · N727TW · Boeing 757231 · Fuselage Floor PanelSDR FDEA201506151819Girt Bar · contaminatedRIGHT FWD ENTRY DOOR DID NOT SEEM TO ARM PROPERLY. FIRST OFFICER REPORTED ACTION OF ARMING HANDLE DID NOT FEEL RIGHT & SLIDE ARMED LIGHT DID NOT COME ON WITH ARMING HANDLE IN. CLEANED EXCESSIVE WHITE LITHIUM GREASE FROM GIRT BAR ASSEMBLY, CLEARED & STOWED UNJun 15, 2015 · N989FD · Boeing 757231 · Emergency EquipmentSDR DALA2015102906785Skin · damagedFWD OR R1 DOOR BS 293, RAMP REPORTS NICK ON SKIN. REPAIRED IAW ERA 540714-14, REV ORIGINAL.Jun 5, 2015 · N717TW · Boeing 757231 · Fuselage Main, Plate/SkinSDR DALA2015060303580Skin · gougedNR 3 LT FUSELAGE SKIN FOUND GOUGED AT APPROXIMATELY BS 395 BETWEEN STR 17-18LT. BLENDED OUT GOUGE ON LT FUSELAGE, STA 395, STR 17L-18L, ORIG MATERIAL .080, REMAINING MATERIAL .072, MATERIAL LOSS .008 AND IS WITHIN LIMITS SRM 53-00-01, FIG 101 AND DWG 141N3331May 30, 2015 · N711ZX · Boeing 757231 · Fuselage Main, Plate/SkinSDR DALA2015052903506Structure · corrodedMULTIPLES CORROSION AREAS FOUND AT MAIN CABIN AFT FLOOR DECK FROM BS 1720 TO BS 1680 AND BETWEEN BL0 TO LBL 50. REFER TO AMDS W/C 5100-01627-01. FOUND SPOTS OF CORROSION BETWEEN BS 1708 TO 1720, LBL 50 TO RBL 50 OUT OF LIMITS IAW SRM 53-60-51, FIG 101. WORKMay 28, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052903505Mount · corrodedCORROSION FOUND AT AFT GALLEY FLOOR MOUNT FITTING APPROXIMATELY AT BS 1717 AND RBL 40. REFER TO AMDS WC 5100-01627-01. R & R FITTING PN 146N5338-1, PO 711ZX-00301 IAW DWG 146N5300, REV A INSTALLED FITTING IAW DWG 146N5300, REV A. LP1968133.May 28, 2015 · N711ZX · Boeing 757231 · Fuselage Main, Attach FittingsSDR DALA2015052903504Deck Plate · corrodedCORROSION FOUND ON AFT DECK PLATE, BS 1701, RBL 24. OUT OF LIMITS IAW 53-60-51, FIG 101.May 28, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052203459Skin · crackedNR 2 CARGO DOOR EXTERIOR SKIN AT LWR AFT CORNER IS BENT, CRACKED AT PREVIOUS BLEND BS 1460. OPEN.May 21, 2015 · N711ZX · Boeing 757231 · Cargo/Baggage DoorsSDR DALA2015052103430Floor Support · corrodedCORROSION FOUND AT MAIN CABIN FLOOR SUPPORT BETWEEN BS 1660 - 1680, LBL 50. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW DWG.May 20, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052103429Floor Support · corrodedCORROSION AT MAIN CABIN FLOOR SUPPORT BETWEEN BS 1640 TO 1660 LBL 50. FOUND OUT OF LIMITS. R & R FLOOR SUPPORT IAW DWG.May 20, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052203434Skin · delaminatedNR 1 ENGINE, INBD FAN COWL, INNER SIDE HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND APPLIED REPAIR IAW SRM.May 19, 2015 · N711ZX · Boeing 757231 · Nacelle/Pylon, Plate/SkinSDR DALA2015052203432Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AT FASTENER LOCATIONS FROM BS 335-375 LBL 58. FOUND TO BE OUT OF LIMITS, IAW SRM. R & R FLOOR SUPPORT. 1May 19, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052203433Intercostal · crackedAFT CARGO, CEILING AREA, INTERCOSTAL IS CRACKED AT BS 1320, LBL 47. R & R AFT CARGO CEILNG AREA INTERCOSTAL IAW DWG 146N, 518, REV B.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052003372Intercostal · crackedAFT CARGO CEILING AREA, INTERCOSTAL IS CRACKED OTBD SIDE AT BS 1320, RBL 47. R & R INTERCOSTAL AT STA 1320 TO 1340, RBL 47 IAW DWG 146N5180, REV B.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052003371Stiffener · crackedAFT CARGO CEILING AREA, VERTICAL STIFFENER AT STA 1320, RBL 47, CRACKED. R & R STIFFENER IAW DWG 5007, REV A.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052003370Stiffener · crackedAFT CARGO CEILING AREA, FLOOR SUPPORT VERTICAL STIFFENER IS CRACKED AT FS 1320, RBL 26. R & R FLOOR SUPPORT VERTICAL STIFFENER AT FS 1320, RBL 26 IAW DWG 146N5002, REV C.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052003369Stiffener · crackedAFT CARGO CEILING AREA, VERTICAL STIFFENER IS CRACKED FWD SIDE OF FRAME STA 1320, LBL 47. R & R AFT CARGO CEILING AREA VERTICAL STIFFENER IAW DWG 146N5002, REV C.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015052003368Intercostal · crackedAFT CARGO CEILING AREA, INTERCOSTAL IS CRACKED FS 1320, RBL 26. R & R INTERCOSTAL IAW DWG 146N5180, REV B.May 18, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015051703363Floor Support · corrodedFOUND CORROSION ON FLOOR STRUCTURE SUPPORT INBD OF R4 DOOR OF THE AFT MAIN CABIN FROM FS 1640 TO FS 1681 AND RBL 52. R & R FLOOR SUPPORT BETWEEN FS 1660 TO 1681, RBL 52 IAW DWG 146N5230, REV B, PN 146N5246V6, PO 7112X-00266. INSTALLED SUPPORT IAW DWG 146N523May 16, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015051703319Floor Support · crackedAFT CARGO FLOOR SUPPORT IS CRACKED, FWD SIDE FS 1320, LBL 26, CEILING AREA. R & R THE FLOOR SUPPORT BETWEEN FS 1320 - 1340 IAW SRM AND DWG.May 16, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015071004275Frame · gougedMAIN CABIN FRAME , BS 1280, HAS TWO GOUGES AT THE WINDOW BELT, BETWEEN S11-13R. BLENDED OUT AREAS IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-07. REPAIR IAW ERA 532895-14AD, REV "0".May 14, 2015 · N711ZX · Boeing 757231 · Fuselage Main, FrameSDR DALA2015051503324Channel · corrodedMAIN CABIN AT L4 DOOR LOWER FRAME HAS TWO CHANNELS CORRODED BS 1665. R & R THE CHANNELS IAW SRM 51-40-02, PAR 4 & DWG 146N8722, REV B.May 14, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015051503323Support Channel · corrodedMAIN CABIN WET AREA, SUPPORT CHANNEL IS CORRODED BS 342, LBL 22. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-02, PAR 4, 51-40-02, PAR 7 AND DWG 141N5170, REV F.May 14, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015051403322Stiffener · corrodedLOWER FRAME AT L4 DOOR CUT OUT, BS 1661 HAS A CORRODED STIFFENER. R & R THE STIFFNER IAW SRM 51-40-02, PAR 7 & DWG 146N8722.May 13, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous StructureSDR DALA2015051403274Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM AT RT MAIN CABIN BS 1380 TO 1390. REMOVED CORROSION IAW SRM 51-10-2 AND FOUND OUT OF LIMITS IAW SRM 53-60-13. INSTALLED NEW CREASE BEAM IAW DWG 146N5590, REV B.May 13, 2015 · N711ZX · Boeing 757231 · Fuselage Main, StructureSDR DALA2015051203241Seat Track · brokenMAIN CABIN SEAT TRACK AT BS 720, RBL 45.5 HAS BROKEN OFF SECTION OF TRACK. REMOVED DAMAGE SECTION OF SEAT TRACK AND REPLACED NEW SECTION AT BS 700-780 IAW DWG 140N5080, REV C.May 11, 2015 · N711ZX · Boeing 757231 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015051203240Strap · crackedMAIN CABIN, STABILIZER STRAP UNDER FLOOR IS CRACKED, BS 375, LBL 45. INSTALLED REPAIRS PARTS IAW SRM 53-00-51, FIG 201.May 11, 2015 · N711ZX · Boeing 757231 · Fuselage Miscellaneous Structure
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