Boeing 757-222

Service difficulty reports · 15,539

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Query with SQL
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 = '757222'
  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 FDEA201411043504Skin · delaminatedNR 1 SLAT TE WEDGE UPPER SURFACE DELAMINATED AT INBD END. REPAIRED IAW SRM 51-70-10 REPAIR 4 .Nov 4, 2014 · N783FD · Boeing 757222 · Leading Edge DevicesSDR FDEA201411043505Power Supply · malfunctionedON SERVICE CHECK FOUND FLIGHT DECK EMER LIGHT NOT WORKING. DISCONNECTED THE FWD & AFT EMER LIGHTING POWER SUPPLIES & THEN RECONNECTED BOTH. ACFT WAS POWERED UP FOR APPROX 2 HRS, THEN RAN THE POWER SUPPLY TEST ON EACH IAW MM 33-51-07-02. BOTH POWER SUPPLIES Nov 4, 2014 · N797FD · Boeing 757222 · Emergency LightingSDR FDEA201411043492Frame · damagedPREVIOUS OPERATOR REPAIR. STATION 1680 FRAME RT SIDE HAS SMALL CUT IN FWD FACE OF FRAME JUST BELOW FLOORBEAM CHORD. COMPLY WITH F-5100-7-5001 PT 1 ATTACHMENT B COMPLIED WITH EA F-5310-T0312796 DATED 10/29/14 TITLE FUSELAGE MAINFRAME ACCOMPLISHMENT OF EA 757-Nov 4, 2014 · N784FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201411033464Skin · damagedEMPENNAGE SKIN HAD NICKS & SCRATCHES AT BS 1844 - 1862 STRINGER 5 - 6L. REMOVED AND TREATED IAW SRM 51-10-02 AND 51-20-01 REV 113, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET II ALLOWABLE DAMAGE 1 REV 113. REPAIRED IAW EA F-5330-T0312884. REPAIR CLANov 3, 2014 · N780FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014110492651Light · inoperativeFORWARD LUMINESCENT EXIT LIGHTS DOOR 1L & 1 RIGHT AS WELL AS FWD MOST FLOOR EEL INOPERATIVE. REPLACED FWD MOST EEL CABIN ENTRANCE IAW MM33-51-96. ALL LUMINESCENT LIGHTS OPERATIONS CHECKED GOOD.Nov 3, 2014 · N576UA · Boeing 757222 · Emergency LightingSDR FDEA201410313429Intercostal · corrodedFORWARD CARGO BAY BS 590 INTERCOSTAL CORRODED. REMOVED AND REPLACED IAW DWG 143N6603 SHT 1 REV B. REPAIR CLASSIFIED AS MAJOR.Oct 31, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410293416Frame · corrodedFRAME BS 1661 STRINGER 25L TO 25R CORRODED ON AFT LOWER FLANGE. R & R FRAME IAW DWG 146N1032 & SRM 51-40-02 DUE TO CORROSION FOUND WITH MATERIAL LOSS CLEANUP OF .047 OF ORIGINAL .063 OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. MAJOR REPAIR.Oct 29, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410283410Frame · corrodedBS 1620 STRINGER 22R - 23R, FRAME FOUND TO BE CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1030, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.Oct 28, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410283407Strap · corrodedDURING REMOVAL OF ANCHOR NUT FROM OUTER STRAP ON THE APU AIR INLET DOOR CUT OUT FOUND OUTER STRAP FOUND EXFOLIATION CORROSION AT BS 1825 STRINGERS 3 - 6R. FOUND OUT OF LIMITS IAW SRM 53-80-15 TABLE 101 ALLOWABLE DAMAGE 1 REV 112. STRAP REMOVED AND REPLACED IOct 28, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410283412Skin · dentedEXTERNAL FUSELAGE SKIN DENT STATION 1620 - 1640 BETWEEN STRINGER 25R TO 26R. ACCOMPLISHED EA F-5330-T0312714 FUSELAGE PLATES & SKINS FUSELAGE SKIN DENT REPAIR STATION 1621 TO 1640 BETWEEN STRINGER 25R TO 26R. CAT B MAJOR REPAIR.Oct 28, 2014 · N784FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410283411Floorbeam · damagedPREVIOUS OPERATOR REPAIR MAIN CABIN FLOORBEAM STATION 500 LBL 45 BROKEN OFF THE END. COMPLY WITH F-5100-7-5001 PT 1 ATTACHMENT B REPAIR DOUBLER LOCATED AT BL0 TO LBL 24.75 AT STATION 500 BL0 TO LBL 24.75 FLOORBEAM. A REPAIR WAS EVALUATED ON NR 60003073000001Oct 28, 2014 · N784FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201410263391Deck Plate · corrodedBS 1681 - 1700 RBL 20 - 24 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201410263393Deck Plate · corrodedBS 1700 - 1720 RBL 22 - 52 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201410263395Deck Plate · chafedBS 1718 RBL 12 DECK PLATE CUT OUT FOUND CHAFED AT THE EDGE. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201410263394Deck Plate · corrodedBS 1681 - 1705 LBL 5 - RBL 5 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201410263392Deck Plate · corrodedBS 1681 - 1700 RBL 38 - 52 DECK PLATE FOUND CORRODED. REPAIRED IAW EA F-5310-T0311813 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201410263386Skin · scratchedSKIN HAS A SCRATCH AT BS 1700 - 1720 BETWEEN STRINGERS 5 - 6R. REPAIRED IAW SRM 53-00-1 FIG 201 REPAIR 16 REV 113. REPAIR CLASSIFIED AS MAJOR.Oct 26, 2014 · N780FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014102792617Battery · dischargedPER A CHECK, SEAT EEL FROM SEAT 32 TO SEAT 38, INOPERATIVE. REPLACED BATTERY & BATTERY CHARGER IAW MM 33-51-07-0201. OPERATIONS CHECKED OK.Oct 26, 2014 · N588UA · Boeing 757222 · Emergency LightingSDR CALA2014102792616Connector · disconnectedPER A CHECK, SEAT EEL AT SEAT 30, INOPERATIVE. FOUND CONNECTOR UNDER SEAT DISCONNECTED. SECURED CONNECTOR. OPERATIONS CHECKED OK.Oct 26, 2014 · N588UA · Boeing 757222 · Light System WiringSDR FDEA201410243367Seat Track · chafedBS 1470 - 1480 RBL 45.5 SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 112. REWORKED AREA EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 DETAIL 1 FIG 101 REV 113. SEAT TRACK REMOVED AND TRIMMED IAW SRM 53-00-52 Oct 24, 2014 · N780FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410243371Fitting · damagedNR 2 PYLON AFT ENGINE MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE. REPAIRED IAW EA F-5450-T0311678. REPAIR CLASSIFIED AS MAJOR.Oct 24, 2014 · N780FD · Boeing 757222 · Engine Mount SectionSDR FDEA201410243370Fitting · damagedPYLON NR 1 PYLON AFT ENG MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE.Oct 24, 2014 · N780FD · Boeing 757222 · Engine Mount SectionSDR FDEA201410233362Fitting · damagedNR 2 ENGINE AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG HOLES FOUND OVERSIZED AFTER BUSHING REMOVAL. REPAIRED IAW EA F-7120-T0312222. REPAIR CLASSIFIED AS MINOR.Oct 23, 2014 · N780FD · Boeing 757222 · Engine Mount SectionSDR FDEA201410233361Fitting · damagedNR 1 ENGINE AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG HOLES FOUND OVERSIZED AFTER BUSHING REMOVAL. REPAIRED IAW EA F-7120-T0312223.Oct 23, 2014 · N780FD · Boeing 757222 · Engine Mount SectionSDR FDEA201410233340Stringer · dentedFORWARD CARGO STRINGER 27L BS 577 DENTED. REPAIRED STRINGER IAW SRM 53-00-53 REPAIR 2.Oct 23, 2014 · N784FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR CALA2014102492570Brake · lack of lubeRECEIVED TE FLAP DISAGREE MSG WHEN FLAP HANDLE FROM 20 TO 25. FOUND TRANSMISSION OVLD INDICATOR TRIP 1, 5 & 8. RESET TRIP OVLD INDICATOR & LUBED FLAP TRANS TORQUE BRAKE. CYCLED FLAPS, NO FAULTS NOTED.Oct 23, 2014 · N564UA · Boeing 757222 · Trailing Edge Flap Control SystemSDR CALA2014102492569Light · disconnectedEMERGENCY EXIT LIGHT STRIP AT ROW 30 DISCONNECTED. ATTACHED LIGHT STRIP, LIGHT TESTED OK.Oct 21, 2014 · N562UA · Boeing 757222 · Emergency LightingSDR FDEA201410193305Frame · corrodedAFT CARGO BS 1380 S17-18R FRAME FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10- 02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 ALLOWANLE DAMAGE 2 REV 113. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 113, DWG 146N8511 SHT 1 REV J. REPAOct 19, 2014 · N780FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410183300Frame · corrodedCORROSION FOUND ON AFT FUSELAGE FRAME WEB AT BS 1681 BETWEEN STRINGERS 28 - 29R. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.Oct 18, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410183299Frame · corrodedHIDDEN DAMAGE AFT FUSELAGE AT STATION 1710 BETWEEN STRINGER 28R & 29R FRAME WEB AFT FACE HAS CORROSION.Oct 18, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410173250Strap · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT MIDDLE STRAP FOUND CORRODED AT BS 1825 STRINGERS 3 - 6R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-15 FIG 101 TABLE 101 ALLOWABLE DAMAGE 1 REV 113. REPAIRED IAW SRM 53-80-15 FIG 202 DETAIL II REPAIR 1 REV 11Oct 17, 2014 · N780FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201410173292Skin · crackedNUMBER 9 SLAT COVE SKIN CRACKED AT OTBD MAIN TRACK FITTING. R & R CRACKED COVE SKIN IAW SRM 51-40-02. MAJOR REPAIR.Oct 17, 2014 · N784FD · Boeing 757222 · Leading Edge DevicesSDR FDEA201410173291Floorbeam · crackedSTATION 1681 LBL 57 FLOORBEAM WAS FOUND CRACKED AFTER REMOVAL OF THE PRESS WEB. CHECKED CRACK OF FLOOR BEAM FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED FLOORBEAM & STRINGER CLIPS. FABRICATED NEW FLOORBEAM, INSTALLED FLOORBEAM & LT & RT STRINGER CLOct 17, 2014 · N784FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201410173234Stringer · corrodedHIDDEN DAMAGE STRINGER 27L STATION 1661 - 1720 CORRODED BETWEEN STRINGER & SKIN. R & R STRINGER STATION 1661 - 1720, STRINGER 27L IAW SRM 51-40-02. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL I. MAJOR REPAIR.Oct 17, 2014 · N783FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201410163228Frame · corrodedAFT PIT BS 1580 STRINGER 28L - 30 FRAME & SHEAR TIE CORRODED. REMOVED AND REPLACED FRAME AT STA 1580, FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF .011" OF ORIGINAL 0.63", IAW SRM 53-00-07, FIG 101, DETAIL I, AND IAW SRM 51-40-02 AND DWG 140N2002. MAJOROct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410163229Frame · corrodedAFT CARGO BAY BS 1640, STRINGER 26 - 28L FRAME CORRODED. REMOVED COROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DEATIAL II. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032. MAJOR REPAIR.Oct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014102492558Skin · puncturedAPU COMPARTMENT INTERNAL SKIN HAS PUNCTURE THRU THE BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON. REPAIR APU COMPARTMENT INTERNAL SKIN IAW ECRA 5350-02153 & MUST BE INSPECTED AT INTERVALS NOT TO EXCEED 500 FLIGHT INSPECTION IAW PART 2 OF ECRA. AT NOct 16, 2014 · N544UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410163227Floorbeam · corrodedBS 365, LBL 7, WL 208, FLOORBEAM UPPER ANGLE CORRODED. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG. 101, DETAIL III. REPAIRED THE FLOORBEAM ANGLE BETWEEN LBL 15 - RBL 69, IAW SRM 53-00-51, FIG. 201, REPAIR 8. MAJOR REPAIR.Oct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, StructureSDR CALA2014102192533Skin · puncturedAPU COMPARTMENT INTERNAL FUSE SKIN HAS PUNCTURE THRU THE HONEYCOMB BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON. REPAIR APU COMPARTMENT INTERNAL SKIN AT BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON IAW ECRA 5350-02153.Oct 16, 2014 · N544UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014102192529Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM AFT FACE BS 1681 BL 57RT. REPAIRED MAIN CABIN FLOORBEAM AT BS 1681 RBL 57 IAW ECRA 5310-06284 & ALL REQUIRED NDT.Oct 15, 2014 · N544UA · Boeing 757222 · Fuselage Main, Floor BeamSDR CALA2014102192528Floorbeam · corrodedCORROSION ON BOTTOM SIDE OF UPPER T CAP AT BS 1681 RBL 47. REPAIRED MAIN CABIN FLOORBEAM UPPER CAP AT BS 1681 RBL 47 IAW SRM 53-60-51 REPAIR 4 FIG 201.Oct 15, 2014 · N544UA · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201410153167Frame · dentedAFT PIT FRAME STATION 1480 INNER FLANGE DENTED STRINGER 25L. R & R AFT PIT FRAME AT STATION 1480 IAW SRM 51-40-02 & DWG 146N1015. MAJOR REPAIR.Oct 15, 2014 · N784FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410143157Skin · dentedLEFT WING INBD FLAP OTBD SIDE BOTTOM DENT 36 INCHES FROM BOTTOM EDGE & 35 INCHES FROM OTBD EDGE. REPAIRED LT WING INBD FLAP OTBD SIDE IAW SRM 51-70-10 REPAIR 2 EA F-5750-T0312337 WINGS FLIGHT SURFACES LT WING INBD FLAP OTBD BOTTOM SKIN REPAIR, RSC TRACKING ONOct 14, 2014 · N784FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201410133144Support Angle · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED BETWEEN BS 1790 - 1825 STRINGER 3R. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 112. SUPPORT ANGLE REMOVED AND REPLACED IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.Oct 13, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410133143Support Angle · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1790- 1825 STRINGER 6R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3152 SHT 1 REV AND DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.Oct 13, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410133142Support Angle · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1789, STRINGER 6R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3141 SHT 1 REV B AND DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.Oct 13, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410133141Support Angle · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORROSION AT BS 1789, STRINGER 3R. REMOVED AND REPLACED THE SUPPORT ANGLE IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.Oct 13, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410133133Doubler · scratchedFUSELAGE EXTERIOR SKIN, WHILE PERFORMING EA F-5330-T0308700PT1 FOUND DOUBLER HAS SCRATCHES AT STATION 1350 STRINGER 1 - 2R. SCRATCH ON DOUBLER CLEARED & TREATED IAW SRM 51-10-02 REV 112 & SRM 51-20-01 REV 112. FOUND NO SIGNIFICANT MATERIAL LOST. PART 1 OF EOct 13, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410123116Support · damagedAFTER CARRIAGE SUPPORT REMOVAL ON RT WING, OTBD TE MAIN FLAP FRONT SPAR HAS THREE HOLES FOUND ELONGATION AT NR 8 CARRIAGE FWD SUPPORT FITTING ATTACH AREA. REPAIRED IAW EA F-5750-T0312509. REPAIR CLASSIFIED AS MINOR.Oct 12, 2014 · N780FD · Boeing 757222 · Wing, Control Surface Attach FittingsSDR FDEA201410123115Angle · corrodedBS 700 - 740 L2 DOOR LOWER SILL ANGLE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 112 AND FOUN OUT OF LIMITS IAW SRM 53-30-15 FIG 101 ALLOWABLE DAMAGE 2 REV 113. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02 REV 113 AND DWG 143N8322 SHT 1 REV KOct 12, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous Structure
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