Boeing 757-2Y0

Service difficulty reports · 830

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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 = '7572Y0'
  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 FDEA201301080052Skin · misrepairedEXTERNAL SKIN MISREPAIRED BS 535.5 BETWEEN S22 AND 23R ACCOMPLISHED EA F-5330-165118. CAT "B" MAJOR REPAIR.Jan 8, 2013 · N973FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201212304405Skin · dentedFUSELAGE SKIN DENTED BS 365-385 BETWEEN S-17 TO 18R. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, FIG 201 REPAIR 16. MAJOR REPAIR.Dec 30, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201212104273Web · damagedMAIN DECK- CARGO DOOR CUTOUT ON FUSELAGE SILL AREA LOWER SILL WEB HAS A PUNCTURE LOCATED JUST AFT OF NR 1 DOOR LATCH FITTING. A REPAIR WAS ACCOMPLISHED ON THE LOWER DOOR SILL WEB BY EA 757-5331-16-F4054. MAJOR REPAIR.Dec 10, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201212054250Track · failedTHE CARGO HANDLING SYS, ROLLER RAILS WILL NOT LOCK INTO THE SEAT TRACK CROWNS BETWEEN STA, S660-780 RBL 24.75 AND 45.5. DISCEPANT SEAT TRACKS ARE INCOMING. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD , A REPAIR WAS PERFORMED ON STAM EA 757-5335-16-F4048 Dec 5, 2012 · N961FD · Boeing 7572Y0 · Cargo CompartmentsSDR FDEA201212044245Skin · corrodedLT INBD FLAP, FRONT INBD PANEL HAS CORROSION. REMOVED CORROSION ON LT INBD FLAP INBD PANEL IAW-SRM-51-10-02. CHECK LIMIT ORIG MAT .125 MAT LOSS .030 FOUND OUT OF LIMIT IAW-SRM-57-53-01, FIG 101, DET VIII PG 106, WORK ACCOMPLISHED ON EA F-5750-162474. CAT "ADec 4, 2012 · N961FD · Boeing 7572Y0 · Trailing Edge FlapsSDR FDEA201211214119Stringer Clip · corrodedFOUND CORROSION AT BS 1661 S26R STINGER CLIP. REPAIRED IAW SRM 53-00-03 REPAIR 2.Nov 21, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Attach FittingsSDR FDEA201211144019Skin · dentedDENT IN FUSELAGE AT BS 380 STRINGER 4R A FUSELAGE EXTERNAL SKIN REPAIR WAS ACCOMPLISHED BETWEEN STA 377-418 IAW EA 757-5311-16-F3939 REV- . MAJOR REPAIR.Nov 14, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201211134002Seat Track · damagedMAIN DECK CARGO SEAT TRACK AT BS 1640-1540 LBL 25 HAS AREAS WITH NICKS, SCRATCHES, AND CORROSION. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL III, FIG 101 SH 2. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5120. Nov 13, 2012 · N973FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211103933Crease Beam · damagedCREASE BEAM AT BS 1040 -1180, RBL 60 HAS EXISTING HOLES WITH SHORT EDGE DISTANCE. R & R CREASE BEAM INNER CHORD BS 1040-1180, RBL 63 IAW DWG 144N5214 AND SRM 51-40-02. MAJOR REPAIR.Nov 10, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201211093928Skin · dentedSKIN DENTED BS 1630 BETWEEN S17 TO 18R. DENT REPAIRED IAW EA 757-5361-16-F3919. MAJOR REPAIR.Nov 9, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201211093926Skin · misrepairedFUSELAGE SKIN MISREPAIRED BS 395 BETWEEN S1 TO 3L. REPAIRED IAW EA 757-5311-16-F3891, REV-.Nov 9, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201211083914Stringer · corrodedSTRINGER 17R BS 1420-1440 CORRODED REPAIRED EA 757-5361-16-F3901. MAJOR REPAIR.Nov 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201211083912Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 1540-1640, LBL 45, HAS SEVERAL AREAS WITH NICKS, SCRATCHES AND CORROSION. REMOVED CORROSION IAW-SRM-51-10-02, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-52, FIG 101 DETAIL I SHEET 2. R & R SEAT TRACK IAW-SRM-51-40-02Nov 8, 2012 · N973FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211073904Panel · corrodedNR 2 SLAT COVE PANEL JUST BELOW INBD MAIN TRACK FITTING HAS CORROSION. REMOVED CORROSION ON COVE PANEL IAW SRM 51-10-02. REMOVED .019 FROM ORIGINAL THICKNESS OF .050 AND .031 WAS REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DETAIL III, VNov 7, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201211063886Skin · dentedFUSELAGE SKIN DENTED BS 1500 -1520 BETWEEN S24 TO 25R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01 FIG 201 REPAIR NR 7. MAJOR REPAIR.Nov 6, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201211023813Structure · misrepairedCARGO DOOR LWR FWD CORNER MISREPAIRED. REPAIRED IAW-SRM-52-30-01 FIG.201 REPAIR 4 THIS IS A CAT."B" REPAIR,MAJOR.Nov 2, 2012 · N961FD · Boeing 7572Y0 · Cargo/Baggage DoorsSDR FDEA201211013808Skin · damagedLEFT WING TOP OTBD WINGTIP HAS A LIGHTING STRIKE. FOUND LIGHTENING STRIKE TO BE ON SCREW AND SPLICE STRAP. REMOVED AND REPLACED OUTBOARD RIB LT WING SPLICE STRAP AND SCREW IAW SRM 51-40-02 AND DWG 112N5027. MAJOR REPAIRNov 1, 2012 · N961FD · Boeing 7572Y0 · Wing, Plate/SkinSDR FDEA201211013802Floorbeam · misrepairedFLOORBEAM AT BS 324 APPROX RBL 12 MISREPAIRED. REPAIRED IAW-SRM- 51-40-02 AND SRM-53-10-08, REPAIR 1. MAJOR REPAIR.Nov 1, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201210303779Strap · corrodedRT APU INLET DOOR FLANGE TO FUSELAGE HAS CORROSION REMOVED CORROSION FROM FWD STRAP IAW SRM 51-10-02 ORIGINAL MATERIAL . 10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. R & R FWD STRAP STA 1787 S-3R TO S-6R IAW SRM 51-40-02 AND DWG 148NOct 30, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210293772Support · corrodedAPU DOOR INLET UPPER SUPPORT BS 1787 - 1825 S3R CORRODED. REMOVED CORROSION AT APU INLET UPPER SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MATERIAL .063 MATERIAL REMAINING .023 MATERIAL REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15 FIG 101 DETOct 29, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210293771Support · corrodedAPU INLET LOWER SUPPORT BS 1787 -1825 S6R CORRODED. REMOVED CORROSION AT APU INLET SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MAT .063 MATERIAL REMOVED .040 MATERIAL REMAINING .023 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15, FIG 101, DETAIL II. R & R Oct 29, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210293769Floorbeam · damagedFLOORBEAM UPPER TEE AT BS 1640 HAS SEVERAL NICKS, SCRATCHES AND CORROSION. R & R FLOORBEAM IAW-SRM-51-40-02 AND DWG 146N5089, CAT."A" MAJOR REPAIR.Oct 29, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201210273762Panel · crackedNR 2 SLAT COVE PANEL CRACKED JUST INBD OF OTBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.Oct 27, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210273761Panel · crackedNR 2 SLAT COVE PANEL CRACKED JUST INBD OF INBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.Oct 27, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210253751Panel · corrodedNR 1 SLAT HAS CORROSION AROUND FASTENERS BEHIND OTBD MAIN SLAT COVE PANEL. CLEANED CORROSION IAW SRM-51-10-02, REMOVED .025 FROM ORIGINAL THICKNESS OF .050 AND .025 REMAINING.FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DETAIL IV PG.104. LOCATED AND DOct 25, 2012 · N961FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA201210243741Web · crackedFOUND WEB, BS 660-680 S17R CRACKED. WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL V, PAGE 103. R & R WEB IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.Oct 24, 2012 · N961FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA201210243739Rib · corrodedRT WING T/E AT 812, RIB WITH ATTACHED BONDING JUMPER SHOWS EVIDENCE OF CORROSION BETWEEN MATING SURFACES. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57- 51-09, FIG.101, DETAIL VI, A1. FABRICATED NEW RIB. R & R RIB IAW-SRM-51-40-02, CAT."A" MAJOR REPAIR.Oct 24, 2012 · N973FD · Boeing 7572Y0 · Wing, Rib/BulkheadSDR FDEA201210223707Skin · dentedEXTERNAL FUSELAGE SKIN DENTED BS 660-680 BETWEEN S25 - 26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REPAIR 7. NO CRACKS FOUND AROUND DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-00-01 REPAIR Oct 22, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201210193698Crease Beam · corrodedCREASE BEAM WEB AT BS 1420-1440 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG.101, DET III PG.103, A2. REMOVED AND REPLACED WEB IAW SRM 51-40-02 & DWG 146N5590. MAJOR REPAIR.Oct 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201210173657Floorbeam · corrodedUPPER DECK FLOORBEAM AT STA 1680 UPPER FLANGE LOWER SURFACE NUT PLATE STRIPS AT RBL 38, 46, AND 50 ARE CORRODED AND MISSING NUT PLATES. BLENDED OUT CORROSION ON FLOORBEAM UPPER FLANGE LOWER SURFACE STA 1681 RBL 38, 46, AND 50 IAW SRM 51-10-02. ORIGINAL THICOct 17, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201210163631Crease Beam · damagedLT INBD CREASE BEAM AT BS 1370-1290 HAS NICKS, SCRATCHES AND CORROSIONS, TOP & BOTTOM SURFACES INCLUDED. R & R CREASE BEAM BS 1290-1370 IAW SRM-51-40-02 AND REF DWG 146N5590, CAT "A" MAJOR REPAIR.Oct 16, 2012 · N973FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201210063575Flange · corrodedAPU INTAKE DUCT CUT-OUT AFT FLANGE HAS CORROSION AT BS 1825. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. REPAIRED AFT STRAP IAW SRM 53-80-15, FIG 202, REPAIR NR1, MAJOR REPAIR.Oct 6, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201209283503Skin · misrepairedSKIN MISREPAIRED AT BS 667 BETWEEN S27R TO S-28R REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16. MAJOR REPAIR.Sep 28, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201209253438Frame · misrepairedFRAME MISREPAIRED AT BS 1280 STR 9-13L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 REPAIR 3.Sep 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209253437Frame · misrepairedFRAME MISREPAIRED AT 1280 STR 9-13R. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 DETAIL I REPAIR 3.Sep 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209193359Seat Track · gougedMAIN CABIN AREA BETWEEN BS 700 - 780 LBL 45 SEAT TRACK NICKED, GOUGED, AND SCRATCHED. REPAIR CLASSIFIED AS A MINOR REPAIR.Sep 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209193358Seat Track · gougedMAIN CABIN AREA BETWEEN BS 640- 685 LBL 25 SEAT TRACK WITH NICKS, GOUGE, AND SCRATCHES. REPAIR CLASSIFIED AS A MINOR.Sep 19, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR U2RA2012092148603Skin · dentedFUSELAGE EXTERIOR BS 1620 - 1640, BETWEEN S23-24R, TWO EACH DENTS FOUND IN SKIN.Sep 18, 2012 · N763CA · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR U2RA2012092148601Stringer Splice · crackedAFT CARGO COMPARTMENT AT BS 1620 STRINGER SPLICE 23R WAS FOUND CRACKED.Sep 18, 2012 · N763CA · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR U2RA2012092148602Skin · dentedFUSELAGE EXTERIOR SKIN BETWEEN BS 1580 AND 1600 AND BETWEEN S25-26R DENTED.Sep 18, 2012 · N763CA · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201209113285Frame · dentedCABIN FRAME HAS A DENT BS 377, STR 6R. COMPLIED WITH EA F-5310-162465Sep 11, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, FrameSDR FDEA201209043223Floorbeam · corrodedCABIN FLOORBEAM HAS CORRISION BS 324, RBL 32 TO RBL 64. REMOVED AND REPLACED FLOORBEAM TEE IAW SRM 51-40-02 AND DWG 141N293. MAJOR REPAIR.Sep 4, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201209013205Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 740, LBL 45 - 60 HAS CORROSION ON UPPER ANGLE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM UPPER ANGLE IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR.Sep 1, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201208143002Crease Beam · corrodedMAIN CABIN AREA BETWEEN BS 1220- 1260, STR 17L CREASE BEAM CORRODED. R & R IAW SRM 51-40-02 AND DWG 146N5590. MAJOR REPAIR.Aug 14, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201208082900Stringer · corrodedSTRINGER 17R , BS 1320-1380 CORRODED.Aug 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201208082899Floorbeam · corrodedMAIN CABIN SEC 41, AREA AT BS 345, LBL 4 HAS CORROSION ON FLOORBEAM. FLOORBEAM REPAIRED IAW SRM 53-00-01, FIG 201, PG 201, REPAIR 3 AND DWG 141N5160. MAJOR REPAIR.Aug 8, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201208062864Seat Track · damagedSEAT TRACK BS 1540 - 1640 RBL 45, NICKED, GOUGED, AND CORRODED. REMOVED DAMAGE IAW SRM 51-10-02, SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-00-52. DETAIL VII PG 102, FIG 101 R & R STEAT TRACK IAW SRM 53-00-52 AND DWG 146N5125. MAJOR REPAIR.Aug 6, 2012 · N961FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208042841Floorbeam · corrodedFLOORBEAM UPPER TEE, BS 1640 BL 0 - RBL 65, CORRODED. R & R FLOORBEAM IAW DWG 146N5500 SH 1, REV D AND SRM 51-40-02. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 AND SRM 53-00-51, FIG 101, SH4. MAJOR REPAIR.Aug 4, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201207282732Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION BS 365, LBL 34- RBL.70. REPAIRED FLOORBEAM UPPER TEE IAW SRM 53-00-51, FIG 201, REPAIR 3. THIS IS A CAT "A" MAJOR REPAIR.Jul 28, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA201207252678Crease Beam · corrodedSTRINGER 17R CREASE BEAM WEB, BS 1360-1380 CORRODED. REPAIR CONSIDERED MINOR.Jul 25, 2012 · N961FD · Boeing 7572Y0 · Fuselage Main, Structure
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