CFM International CFM56-3B2

Service difficulty reports · 635

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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 engine_model_key = 'CFM563B2'
  ORDER BY difficulty_date DESC"

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SDR DL733040998Controller · malfunctionedAT 26K ALT CABIN BEGAN TO RISE RAPIDLY, EMERGENCY DESCENT WAS INITIATED. THE CABIN REACHED 15K, MASKS DROPPED. PERFORMED ALL REQUIRED TESTS, NO TROUBLE FOUND.Oct 28, 2004 · N948WP · Boeing 737301 · Cabin Pressure ControllerSDR USAA040931Attach Angle · crackedPIT - Q1 - ATTACH ANGLE, .5 INCH LONG CRACK, FRAME 706, STR S-11L. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02, 51-40-03.Oct 28, 2004 · N435US · Boeing 737500* · Fuselage Main, Attach FittingsSDR USAA040944Skin · delaminatedPIT - Q5 - NR 2 SLAT SKIN, 3 INCH BY 4 INCH AREA, DELAMINATION, OB END T/E. REMOVED DAMAGE SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10.Oct 28, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040900Skin · crackedPIT - Q5 - NR 4 SLAT SKIN, 6 FASTENER HOLES, .1250 INCH TO .2500 INCH CRACK. FASTENER HOLES, LOWER SKIN AREA BELOW ACTUATOR ATTACH POINT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, FIG 206.Oct 27, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040921Bracket · crackedPIT - Q1 - BRACKET, 1 INCH CRACK, STA 927 AT 24.7L SUPPORT BRACKET. MANUFACTURED PART AND INSTALLED IAW SRM 51-41 AND MFG DWG 69771901.Oct 27, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040945Skin · delaminatedPIT - Q5 - SKIN TO CORE, 7 INCHES BY 2.5 INCH AREA DELAMINATED, IB RT AFT FLAP TOP SURFACE 34.5 INCHES- 42 INCHES FROM OB END. REMOVED UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER IAW SRM 51-70-10.Oct 27, 2004 · N516AU · Boeing 7373B7 · Trailing Edge FlapsSDR AWXA200401160Wire · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.Oct 26, 2004 · N309AW · Boeing 7373G7 · Light System WiringSDR USAA040767Skin · crackedCLT, RON, SKIN- INCH CRACK, BS727E AT STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231.Oct 26, 2004 · N430US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040899Support Angle · crackedPIT - Q5 - SUPPORT ANGLE, 1 INCH LONG, CRACKED. SUPPORT DOWNLOCK VIEWER LT FWD CORNER, STA 259.5. REPLACED PART IAW DWG 65-45833.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040901Skin · crackedPIT - Q5 - SKIN, 1.5 INCH CRACK, FWD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-01.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040943Skin · delaminatedSKIN AND CORE, 4 INCH BY 4 INCH AREA, IB T/E NR 4 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED DOUBLER, NEW CORE IAW 51-70-10.Oct 26, 2004 · N516AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040968Crease Beam · corrodedPIT - Q5 - CREASE BEAM WEB, .75 INCH (6 AREAS), CORROSION; NO LEVEL OR TASK, BETWEEN STA 420 AND STA 440, RT SIDES. CREASE BEAM WEB MFG IAW DWG 65-96956 AND BACD2003.Oct 26, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040889Floorbeam · mismanufacturedPIT-Q5- FLOORBEAM, INCORRECT MATERIAL FROM MFG. FLOORBEAM UPPER CHORD REMOVED AND REPLACED IAW EA 68822A, FLOOR STA 328.Oct 25, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA040950Skin · gougedPIT - Q5 - SKIN, .025 INCH DEEP AND AT 10 INCHES LONG, GOUGED, STA 887-867, STR 1. CUT OUT DAMAGE INSTALLED SHIMS, FILLERS, STRAPS, DOUBLER AND TRIPLER IAW EA 79291.Oct 25, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040776Pin · corrodedPIT, C3, PIN ASSEMBLIES- 1INCH X 1INCH AREA, CORROSION; NO LEVEL OR TASK LT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IWA WA 79359/ DRAFT EO 5502V025.Oct 24, 2004 · N448US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA040775Pin · corrodedPIT - C3, PIN ASSEMBLIES, 1 INCH BY 1 INCH AREA, CORROSION; NO LEVEL OR TASK. RT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IAW EA 79359/ DRAFT EO 5502V025.Oct 24, 2004 · N448US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA040773Bulkhead · crackedPIT - C2, BULKHEAD SKIN, 1 INCH CRACK, FWD PRESSURE BULKHEAD RBL 57, WL 210. INSTALLED DOUBLER IAW SRM 53-10-08 FIG 211.Oct 24, 2004 · N777AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040780Stiffener · crackedPIT, FPBH INSP, STIFFENER TWO CRACKS, .5000 INCH X .7500 INCH LENGTH. STA 178 FPBH WL 218 UNDER HORIZON STIFFENER. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK-42-93801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040779Stiffener · crackedPIT, FPBH INSP, STIFFNER 1 INCH CRACK IN LENGTH, STA 178 UNDER HORIZON STIFFNER WL 218 RT SIDE. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK42-93801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040778Bulkhead · crackedPIT, FPBH INSP, FPBH WEB-.3750 INCH CRACK, STA 178 FWD PRESSURE BULKHEAD LT RADAR ANTENNAE MOUNT. DOUBLER INSTALLED IAW EO 53-V153, JOB CARD MK-4293801.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040777Skin · crackedPIT - RON, SKIN WITH .5000 INCH CRACK, FWD STA 380 BETWEEN STR 28R AND BL0. INSTALLED DOUBLER IAW EA 79322.Oct 22, 2004 · N779AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040913Clip · crackedPIT - Q1- CLIP, .1250 INCH CRACK AT STA 663.75 AND STR S-10R. REMOVED AND REPLACED CLIP IAW SRM 51-40-03.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040914Clip · crackedPIT - Q1- CLIP, .2500 INCH CRACK AT STA 807, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040915Clip · crackedPIT - Q1 - CLIP, .1250 INCH CRACK, STA 807 AND STR 10R. REMOVED AND REPLACED CLIP IAW SRM 51-10-02.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040918Frame · corrodedPIT - Q1 - FRAME, 2 INCH BY 1.5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-101-01, FRAME OUTER CHORD BS 227.8, WL 208.1 AND 2 INCH. REMOVED CORROSION, TREATED AND PRIMED, REINSTALLED FASTENERS IAW SRM 51-40-03.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040933Intercostal · corrodedPIT - Q1 - INTERCOSTAL, .75 INCH BY 3 INCHES, CORROSION; LEVEL 1;TASK NR C53-107-02, FRAME 328, LBL 11. CHANGED INTERCOSTAL IAW SRM 51-10-02, 51-20-01, 51-40-01.Oct 22, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR SB04147Battery Pack · dischargedFOUND EXTERIOR EMERGENCY LIGHTS OVER R1 AND L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK.Oct 21, 2004 · N524AU · Boeing 7373B7 · Emergency LightingSDR USAA040888Pan · tornPIT, Q5, FLOOR PAN, .5 INCH TEAR, LBL 18 INCH AT STA 986.5. INSTALLED FILLER/DOUBLER IAW SRM 51-70-13, FIG 1.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040907Tie Clip · crackedPIT - Q1 -CLIP, .1250 INCH CRACK FROM RIVET AT FRAME STA 663.75, STR S10L. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-2, 51-40-03 AND MFG DWG 65-46541.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040910Stringer Clip · crackedPIT - Q1 - CLIP, .2500 INCH CRACK, RIVET OF STRINGER CLIP, STA 767 S4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040911Stringer Clip · crackedPIT - Q1 - STRINGER TIE CLIP, .2500 INCH CRACK, STA 380, STR 2 LT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040923Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, STA 867 BETWEEN STR 8L AND STR 9L. INSTALLED DOUBLER IAW TYP REP 53-10-20A.Oct 21, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040941Channel · crackedPIT - Q5 - CHANNEL, .5 INCH CRACK, STA 540 LBBL 0, RBBL U CHANNEL. REPLACED CHANNEL IAW SRM 53-00-03.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040946Floor Panel · corrodedPIT - Q5 - FLOOR PANEL, 1 INCH BY 5 INCH AREA CORROSION, LEVEL 1; TASK NR C53-107-02, PANEL NR 99, STA 1016. REPLACED FLOOR PANEL NR 99 IAW SRM 51-70-12.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Floor PanelSDR USAA040948Frame · corrodedPIT - Q5 - ANTENNA MOUNT FRAME, 3 INCHES L BY 1 INCH W, CORROSION; LEVEL 1; TASK NR C53-107-01, VHF ANTENNA NR 2 MOUNT. REPAIRED IAW SM 51-10-2 AND 51-40-00.Oct 21, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040763Skin · crackedCLT, RON, SKIN-1.250 CRACK, BS 942 STRINGER 24L. INSTALLED DOUBLER IAW EA 95924.Oct 20, 2004 · N419US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA040908Clip · crackedPIT - Q1 - CLIP, .5 INCH CRACK, BS 578, S8R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40.Oct 20, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040909Clip · crackedPIT - Q1 -CLIP, .5 INCH CRACK AT BS578, S8L. DEFECTIVE PART REPLACED WITH IDENT PART IAW IDENT PART IAW SRM 51-40.Oct 20, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040890Stiffener · crackedPIT- Q5 - VERTICAL STIFFENER, .7500 INCH CRACK, VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERT STIFFENER IAW EA 79313/ EO5704V245 (DRAFT).Oct 19, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040898Door Frame · crackedPIT - Q5 - FRAME, .5 INCH CRACK. FWD SERVICE DOOR SURROUND FRAME AT 294.5 AND S17R. FABRICATED DOUBLER IAW SRM 51-70-11.Oct 19, 2004 · N516AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA040949Support Angle · corrodedPIT - Q5 - SUPPORT ANGLE, 1.2500 INCH BY .5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, FLOOR SUPPORT, STA 859. BURNISHED, TREATED AND PRIMED IAW TYP REP 53-10-06B.Oct 19, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040758Skin · crackedCLT - RON, SKIN 1.5 INCH CRACK, BS 727D AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229.Oct 18, 2004 · N422US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA040897Frame · crackedPIT- Q5 - FRAME, 2 INCH CRACK, STA 440 S9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A.Oct 18, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040774Beam · crackedPIT, FPBH INSP, VERTICAL CORD-.750 INCH LONG CRACK. IB RADIUS OB VERTICAL CORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA79303.Oct 15, 2004 · N445US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA040756Beam · crackedPIT, FPBH, VERTICAL CHORD, .750 INCH LONG, IB RADIUS OF VERTICAL CHORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA 79303.Oct 15, 2004 · N445US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA040892Stringer Clip · crackedPIT- Q5- STRINGER TIE CLIP, 1.25 INCH CRACK, BS 360, STR 4, RT. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 51-10-02.Oct 15, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040893Stringer Clip · crackedPIT- Q5- STRINGER TIE CLIP, .2500 INCH CRACK, BS 344, STR8, RT. FABRICATED IAW MFG DWG 66-244553 AND INSTALLED IAW SRM 51-40-01.Oct 15, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040896Angle · crackedPIT - Q5 - ANGLE, .5 INCH CRACK, STA 380 AT STR 15R. FABRICATED REPAIR ANGLE IAW SRM 51-70-11.Oct 14, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040754Keelbeam · crackedPIT, C5, KEELBEAM, 2 INCH LONG CRACK, KEELBEAM RT SIDE JUST AFT OF STA 540. INSTALLED REPAIR ANGLE IAW EA 79268.Oct 12, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA040755Window Frame · crackedPIT, C5, WINDOW FRAME, .2500 INCH CRACK, CAPTAINS WINDOW POST BETWEEN NR 1 AND NR 2 WINDOWS TOP, FWD CORNER. INSTALLED DOUBLER IAW SRM, FIG 103.Oct 12, 2004 · N521AU · Boeing 7373B7 · Fuselage Main, Structure
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