Boeing 757-2Q8

Service difficulty reports · 2,798

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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 = '7572Q8'
  ORDER BY difficulty_date DESC"

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SDR FOTR20150918059Skin · damagedAFT CARGO COMPARTMENT, FUSELAGE SKIN BS 1320-1340 & STR 25L&26L, FOUND TOOLING MARK. REPAIRED ON FAS EA 15501, REV IR NR 40822, W/O N293DH-01-02.Jul 23, 2015 · N293DH · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR DALA2015072404624Frame · dentedDENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R. TRIMMED-OUT DENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R AND ACCOMPLISHED A PERMANENT CAT"B" REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT MEASURE 9.040" X 1.080" X 0.5" RT THRESHOLD INSPECTION TJul 23, 2015 · N346BC · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015072404623Frame · dentedDENT ON FWD CARGO RT FRAME AT BS 800 ABOVE STR 23R. ACCOMPLISHED A PERMANENT CAT"B" REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT SIZE 1.08" X 0.94" X 0.5"R. THRESHOLD INSPECTION TO START AT BEFORE 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTERJul 23, 2015 · N346BC · Boeing 7572Q8 · Fuselage Main, FrameSDR FOTR20150726058Skin · scratchedFUSELAGE HAS SCRATCHED AREA BS 670-680 BETWEEN STRINGERS 23 - 24R. REPAIRED ON NE40825 W/O N293DH-01-02.Jul 22, 2015 · N293DH · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR DALA2015072304621Gate · corrodedR1 DOOR GATE, LOWER GATE HAS CORROSION ALONG BOTH LOWER EDGES IN ONE 14" LONG AREA AND SEVERAL SPOTS IN A 19" LONG AREA FROM FWD TO AFT CORNERS. REMOVED AND INSTALLED NEW R-1 DOOR LOWER GATE IAW AMM 52-11-38-004-001 AND IAW AMM 52-11-38-404-009.Jul 22, 2015 · N338BC · Boeing 7572Q8 · Service DoorsSDR DALA2015072304620Frame · damagedFRAME DAMAGED BS 580, ACCOMPLISHED PERMANENT MAJOR REPAIR ON FWD CARGO LT FRAME AT BS 580 BETWEEN STR 22 - 26L IAW ER/A 536959-14AD REVISION ORIGINAL SECTION I.Jul 22, 2015 · N338BC · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015072304622Skin · damagedLEFT WING INBD FLAP T/E WEDGE PANEL LOWER SURFACE IS DAMAGED, DENTED, PUNCTURED, AND CRACKED MF BS 223 TO MF BS 240. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON LT WING INBD FLAP T/E WEDGE IAW SRM 51-70-10, TRIMOUT DIMENSION: 17" X 9.5". COMPLIED WITH ALL SJul 21, 2015 · N346BC · Boeing 7572Q8 · Trailing Edge FlapsSDR DALA2015072304619Crease Beam · corrodedCORROSION ON RT CREASE BEAM INBD CHORD BETWEEN BS 730 - 742. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15. R & R THE CREASE BEAM ANGLE IAW SRM 41-40-02, PAGE 2, PAR B AND PAGE 6, PAR D, DWG 143N8328.Jul 21, 2015 · N338BC · Boeing 7572Q8 · Fuselage Main, StructureSDR DALA2015072204538Girt Bar · damagedL1 DOOR, GIRT BAR MECHANISM, FWD & AFT GIRT BAR CRANKS HAVE PLAY AT HINGE. REMOVED CRANK, PN 140N2769-1, FOUND TO BE OUT OF LIMITS IAW DWG 140N2769, DIAMETER 0.5009, MAX ALLOWABLE 0.5006, INSTALLED NEW CRANK, PN 140N2769-1 IAW CMM 52-11-07. REMOVED CRANK, R Jul 21, 2015 · N338BC · Boeing 7572Q8 · Emergency EquipmentSDR DALA2015072204536Floor Support · corrodedCORROSION ON MAIN CABIN FLOOR SUPPORT, BS 376 - 378, BL0. REMOVED CORROSION ON MAIN CABIN FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 AD1, DETAIL III. R & R MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02, PG 6, 7 REF DWG 141N5191, REV A.Jul 21, 2015 · N338BC · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR DALA2015072204535Gate · corrodedL1 DOOR, LOWER GATE HAS CORROSION ALONG LOWER EDGE IN 8 PLACES FROM FWD TO AFT CORNER. REMOVED CORROSION ON L-1 DOOR LOWER GATE FROM FWD TO AFT IAW SRM 52-10-02. ORIGINAL MATERIAL DIMENSION ON LOWER EDGE OF LOWER GATE IS 4.92" IAW DWG 141N6206, MATERIAL LOSS Jul 21, 2015 · N338BC · Boeing 7572Q8 · Passenger/Crew DoorsSDR DALA2015072504694Box Beam · corrodedCORROSION ON BOXBEAM BETWEEN BS 1661 AND BS 1681, LBL 54. REMOVED AND INSTALLED NEW BOX BEAM IAW SRM 51-40-02, PARA 7D, PG 6&7, 51-40-02, 4B PG2, AND DWG 146N5230.Jul 20, 2015 · N346BC · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR DALA2015080704900Structure · corrodedCORROSION ON BOXBEAM BETWEEN BS 1640 AND BS 1661, LBL 54. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R BOX BEAM IAW SRM.Jul 19, 2015 · N346BC · Boeing 7572Q8 · Fuselage Main, StructureSDR DALA2015071904533Frame · dentedTWO DENTS ON FWD CARGO FRAME AT BS 700, ABOVE STR 24L. TRIMMED OUT DENTS FOUND ON FRAME IAW SRM 53-00-07, FIG 201, REPAIR 5. INSTALLED AND ACCOMPLISHED A PERMANENT CAT "B" MAJOR REPAIR.Jul 18, 2015 · N346BC · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201507182263Cover · looseSLIDE COVER ON L1 DOOR IS LOOSE. SECURED L1 DOOR ESCAPE SLIDE COVER IAW AMM 25-66-9-414-101.Jul 18, 2015 · N996FD · Boeing 7572Q8 · Emergency EquipmentSDR DALA2015072204539Unknown · odorELECTRICAL BURNING ODOR IN THE CABIN BETWEEN ROWS 21 AND 22, NO SMOKE OR OTHER INDICATIONS AFTER TURN RECIRCULATION FAN ODOR DISAPPEARED. REACTIVATED RECIRC FAN. PERFORMED OPS CHECK OF FAN. FAN OPS NORMAL. INSPECTED CABIN FOR ODOR, NO SMELL NOTED. ACFT OK Jul 17, 2015 · N712TW · Boeing 7572Q8 · Air Distribution SystemSDR DALA2015071804532Frame · dentedDENT ON FWD CARGO LT FRAME AT BS 660 FROM STR 24-25L. INSTALLED & ACCOMPLISHED A PERMANENT REPAIR CAT "B" IAW SRM 53-00-07, REPAIR 5, FIG 201, DETAIL III.Jul 17, 2015 · N346BC · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015072204537Coffeemaker · odorELECTRIC BURNING ODOR FROM AFT GALLEY COFFEEMAKER. R & R AFT GALLEY COFFEEMAKER, LT SIDE IAW AMM 25-33-01, OPS CHECKS OK.Jul 16, 2015 · N704X · Boeing 7572Q8 · Buffet/GalleysSDR DALA2015072004534Floor Support · corrodedAFT CARGO BAY HAS SEVERAL AREAS OF CORROSION ON CARGO FLOOR SUPPORT BOTH UPPER AND LOWER SURFACES BETWEEN BS 1200 - 1344, RBL 10.45. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, PG 7 & 21, DWG 146N5390, AND ER/A 491157-14MA, REV A.Jul 16, 2015 · N338BC · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR DALA2015071704453Skin · dentedRIGHT INBD MAIN FLAP T/E WEDGE UPPER AND LOWER SKINS HAVE 15" X 11" AREA DENTED 62"-77" FROM OTBD END. ACCOMPLISHED PERMANENT REPAIR OF THE DISCREPANT AREA ON RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.Jul 16, 2015 · N346BC · Boeing 7572Q8 · Trailing Edge FlapsSDR DALA2015071404357Frame · dentedDENT FOUND ON THE FWD FRAME AT BS 660 BETWEEN STRINGERS 24-25L. ACCOMPLISHED A PERMANENT CAT "B" REPAIR IAW SRM 53-00-07, REP 5, DETAIL III.Jul 13, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015071304284Floorbeam · corrodedCORROSION ON BS 345 FLOORBEAM UPPER TEE, BETWEEEN BL 0 AND LBL 20. BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, FIG 101, DETAIL III. CUT OUT THE DAMAGE SECTION BETWEEN RBL 35 TO LBL 50.5. FABRICATED A REPAIR, Jul 12, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA2015071204283Seat Track · corrodedFOUND SEAT TRACK LBL 45.5 BS 1280 CORRODED. FOUND THE SEAT TRACK CORRODED 100 PERCENT WITH LENGTH 4" X 1". TRIMMED-OUT DAMAGED SECTION, FABRICATED A REPLACEMENT & ACCOMPLISHED A PERMANENT REPAIR CAT "A" BETWEEN BS 1240 - 1250 IAW SRM 53-00-52, REPAIR 3, FIGJul 11, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015071204282Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK INBD AND OTBD FLANGES, BETWEEN BS 680 AND 740, RBL 45.5. BLENDED AREAS AND FOUND OUT OF LIMITS IAW SRM 53-00-52, AD 1, PAGE 104. REMOVED AND REPLACED THE SEAT TRACK IAW 51-40-02, PAGE 4 AND DWG 143N5120.Jul 11, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR20150711053Floorbeam · corrodedMAIN CABIN BS 680 FLOORBEAM UPPER SURFACE HAS CORROSION ON UPPER SURFACE LBL 45 TO LBL 62.Jul 11, 2015 · N380DH · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FOTR20150711052Skin · not reportedREPLACE REPAIR ON BELLY JUST FORWARD OF THE AFT PRESSURE BULKHEAD S30 APPROXIMATELY BS 1700. REPLACED ON FAS WO VQ-BJK-01-02.Jul 11, 2015 · N380DH · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FOTR20150711051Stringer · corrodedE & E BAY AT BS 492, STRINGER 19R CORROSION. REPAIRED.Jul 11, 2015 · N380DH · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FOTR20150711050Frame · damagedUPPER FUSELAGE INTERIOR, BS 365.25 FRAME IS DAMAGED BETWEEN STRINGERS 3 - 4L.Jul 11, 2015 · N380DH · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015071004264Crease Beam · corrodedCORROSION ON RT CREASE BEAM BS 1613 - 1616. REMOVED TWO AREAS OF CORROSION. FOUND BLENDOUT AREA TO BE OUT OF LIMITS IAW SRM 53-60-13 ADI. CUTOUT DAMAGED SECTION OF CREASE BEAM & INSTALLED A PERMANENT CAT "A" REPAIR IAW SRM 53-00-13, REPAIR 2 PAGE 202-206.Jul 9, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, StructureSDR DALA2015070904194Frame · dentedAFT CARGO BAY UPPER FLANGE OF FRAME HAS ONE DENT BS 1440, BS S26L. INSTALLED & ACCOMPLISHED A CAT "B" PERMANENT REPAIR ON THE FRAME IAW SRM 53-00-07, REPAIR 5, FIG 201.Jul 8, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015070804155Keel Fitting · crackedCORROSION AT INBD CORNER OF LOWER KEEL STRUCTURE COMMON TO LT MLG DOOR HINGE T-CHORD AT BS 1118, LBL 5. FABRICATED & INSTALLED REPLACEMENT PART IAW SRM 51-40-05, SRM 53-40-71.Jul 7, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, KeelSDR DALA2015070704153Keel Fitting · corrodedCORROSION AT AFT INBD CORNER OF LOWER KEEL STRUCTURE COMMON TO RT MLG DOOR HINGE T-CHORD AT STA 1118, RBL 5. REMOVED CORROSION ON AFT INBD CORNER OF LOWER KEEL STRUCTURE COMMON TO RT MLG DOOR HINGE T-CHORD AT BS 1118, RBL 5. ORIGINAL MATERIAL AT BLENDED AREA Jul 6, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, KeelSDR DALA2015070704152Keel Fitting · corrodedCORROSION ON LOWER KEEL STRUCTURE COMMON TO LT MLG DOOR HINGE T-CHORD AT BS 1075 TO BS 1100, LBL 6. REMOVED CORROSION ON LOWER KEEL STRUCTURE COMMON TO LT MLG DOOR HINGE T-CHORD AT BS 1075 TO BS 1100 LBL6. GREATEST MATERIAL LOSS MEASURE 2.4" X 1.4" X .065" OJul 6, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, KeelSDR DALA2015070704151Frame · dentedAFT CARGO BAY UPPER FLANGE OF FRAME HAS ONE DENT, BS 1540, S25L. FOUND TO BE OUT OF LIMITS AND REPLACED.Jul 6, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015070704150Frame · dentedAFT CARGO BAY UPPER FLANGE OF FRAME HAS ONE DENT AT BS 1500 S23L. FOUND OUT OF LIMITS IAW SRM 53-00-07, REP 5 DETAIL III. REPAIRED IAW SRM 53-00-07, REPAIR 5, DETAIL III.Jul 6, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201507042152Oxygen Box · leakingCAPTAIN`S OXYGEN PRESS TO TEST DOOR BROKEN. COURIER OXYGEN MASK INOPERATIVE. SWAPPED NR 3 COURIER POSITION OXYGEN STOWAGE BOX TO CAPTAIN`S POSITION TO MAKE CAPTAINS POSITION SERVICEABLE IAW AMM 35-11-51-4-99. REMOVED AND REPLACED THE COURIER NR 3 OXYGEN MASJul 4, 2015 · N993FD · Boeing 7572Q8 · Crew Oxygen SystemSDR FOTR20150918061Skin · corrodedCORROSION FOUND ON WING/TO BODY STRUCTURE AT BS 1290 LT SIDE, 27L FUSELAGE SKIN. REPAIRED ON FAS EA 15487, REV IR NR 40399, W/O N293DH-01-02.Jul 2, 2015 · N293DH · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR DALA2015071004265Skin · damagedRT WINGLET FOUND WITH COMPOSITE DAMAGE. REPAIRED THE WINGLET IAW SRM 51-70-17,57-31-01, AND 51-21-10-377-003.Jul 2, 2015 · N823DX · Boeing 7572Q8 · Wing, Plate/SkinSDR DALA2015070204092Floorbeam · corrodedFOUND CORROSION ON THE FLOORBEAM AT BS 700, LBL 62. REMOVED THE CORROSION AND REPAIRED IAW ER/A 536956-14 REV ORIGINAL.Jul 1, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA2015070204091Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT BS 720, LBL 62. REMOVED THE CORROSION AND REPAIRED IAW ER/A 536957-14, REV ORIGINAL.Jul 1, 2015 · N823DX · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR DALA2015070204090Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK OTBD FLANGE, BETWEEN BS 700 - 740, RBL 24.7. REMOVED AND REPLACED THE SEAT TRACK AND SUPPORT IAW SRM 53-30-52, SRM 51-40-02 AMM 51-21-10-377-003 & DWG 143N5080.Jul 1, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR20150725058Frame · chafedMAIN CABIN INTERIOR FRAME, BS 1280 HAS A SMALL CHAFE MARK BETWEEN STR 11R AND STR 12R. REPAIRED THE FRAME.Jun 30, 2015 · N293DH · Boeing 7572Q8 · Fuselage Main, FrameSDR DALA2015070104087Skin · damagedLEFT WING FLAP PANEL 555AL, HONEYCOMB STRUCTURE IS DAMAGED AT ONE CORNER. REPAIRED IAW SRM 51-70-10.Jun 30, 2015 · N823DX · Boeing 7572Q8 · Trailing Edge FlapsSDR DALA2015070104085Floor Support · corrodedCORROSION ON MAIN FLOOR SUPPORT BS 1675, RBL 55. REMOVED THE CORROSION IAW SRM 53-00-51, R & R THE FLOOR SUPPORT BETWEEN BS 1660-1680 IAW SRM 51-40-02, PG 3-7 AND 29.Jun 30, 2015 · N823DX · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR DALA2015070104084Floor Support · corrodedCORROSION ON MAIN FLOOR SUPPORT, BS 1660 - 1680, RBL 55. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 7-8 AND 21.Jun 29, 2015 · N823DX · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR DALA2015063004003Cargo Track · corrodedCORROSION ON FWD CARGO TRACK SUPPORT AFT MOUNT FITTING ON DOOR SILL AT BS 607. REMOVED CORROSION FROM TIE DOWN FITTING LWR PLATE FOUND TO BE EXFOLIATED 90 PERCENT AND OUT OF LIMITS REF SRM 53-00-53, FIG 101, PAGE 105 AND R & R TIE DOWN FITTING LWR PLATE ON FJun 29, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015063004002Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK CROWN /BOTTOM AT BS 1320 TO 1323, RBL 24. ACCOMPLISHED PERMANENT CAT"B" REPAIR IAW SRM 53-00-52, REPAIR 3, FIG 201.Jun 29, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015063004001Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK CROWN BOTTOM AT BS 1308 TO 1320, RBL 24.75. ACCOMPLISHED PERMANENT CAT"B" REPAIR IAW SRM 53-00-52, REPAIR 3, FIG 201.Jun 29, 2015 · N823DX · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201506292115Light · inoperativeONE EXT EMER LIGHT INOPERATIVE. RELAMPED IAW SMP, OPERATIONS NORMAL IAW AMM 33-51-00-5.Jun 29, 2015 · N995FD · Boeing 7572Q8 · Emergency LightingSDR DALA2015063004000Intercostal · corrodedUPON REMOVAL OF LT TRANSITION PANEL IN AFT CARGO ON NR 100-200 FOUND INTERCOSTAL UPPER ANGLE WITH CORROSION BETWEEN BS 1480-1500 ABOVE STR 26L. REMOVED CORROSION INTERCOSTAL UPPER ANGLE BETWEEN STA 1480-1500, STR 26L IAW SRM 53-00-04, FIG 101. MATERIAL ORIGIJun 28, 2015 · N823DX · Boeing 7572Q8 · Fuselage Miscellaneous Structure
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