CFM International CFM56-3B2

Service difficulty reports · 635

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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 engine_model_key = 'CFM563B2'
  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 USAA040976Support Angle · crackedPIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03.Nov 16, 2004 · N515AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040980Stringer · crackedPIT - Q5 - STRINGER, .75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221.Nov 15, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA041042Skin · delaminatedPIT - Q1 - UPPER AND LOWER SKIN, 3.5 INCH X 2 INCH AREA, DELAMINATION, LT IB AFT FLAP OB END UPPER AND LOWER SURFACE. REMOVED DISBONDED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP SKIN DOUBLER IAW SRM.Nov 15, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040982Tie · crackedPIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART.Nov 13, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040930Gusset · crackedPIT - Q1 - GUSSET, .7500 INCH CRACK, BS 927 UNDER RT IB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Nov 12, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040867Skin · crackedSKIN, 1.5 INCH CRACK, STA 727D AT STR 23 RT. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01.Nov 11, 2004 · N439US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040929Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, FRAME 727F BETWEEN S8L AND S9L. CUT OUT CRACKED SECTION AND INSTALLED REPAIR ANGLES IAW TYP REP 53-10-20A AND EA 79502.Nov 11, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040940Stringer Clip · crackedSTRINGER CLIP, .2500 INCH CRACK, BS 663.75, STRINGER 10 LT. DEFECTIVE PART REPLACED WITH IDENT PN.Nov 11, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA041057Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, SEVERAL AREAS 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041058Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 3 INCHES LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178, 13 INCHES FROM FWD SPAR. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041059Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 1 INCH X .2500 INCH AREA, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE STA 0 L/E. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040891Stiffener · crackedPIT- Q6 - VERTICAL STIFFENER, 1.2500 INCH CRACK, AT RBBL 6.15, STA 663.75. REPLACED VERTICAL STIFFENER IAW EA 79313 AND EO 5704V245 (RAFT).Nov 10, 2004 · N516AU · Boeing 7373B7 · Wing Main, Frame StructureSDR USAA040936Skin · wornPIT - Q1 - SKIN, 1 INCH BY 1.5 INCHES WEAR, KNIFE EDGE WEAR, 1 INCH AFT OF FWD CORNER AT RUDDER STA. INSTALLED REPAIR PLIES IAW EA 79467, SRM 51-70-17.Nov 10, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA040938Skin · damagedPIT - Q1- SKIN, 2 INCH BY 2 INCH AREA, CARBON FIBER DAMAGE, 120.5 INCH UP FROM BOTTOM, 6.25 INCH FORWARD OF T/E. FILLED AND INSTALLED REPAIR PLIES IAW 51-70-17 AND EA 79467.Nov 10, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA040983Structure · crackedPIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 10, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040967Skin · corrodedPIT - Q6 - WING SKIN CUT OUT, 1.2500 INCH X .2500 INCH AT 4 LOCATIONS, CORROSION; NO LEVEL OR TASK, RT WING BOOST PUMP CUT OUT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.Nov 9, 2004 · N516AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA041041Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION 28 INCH FWD OF T/E, 39 INCH UP FROM BOTTOM. PREPARED DAMAGED AIR, INSTALLED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041044Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA OF DAMAGE, RUDDER LT SIDE 98.5 INCH FROM BOTTOM AND 9.25 INCHES FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041045Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA, SINGLE LAYER DAMAGE. RUDDER LT SIDE 105./5 INCHES FROM BOTTOM AND .3750 FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI PLY REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041046Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 1 INCH AREA DAMAGE, RUDDER LT SIDE 95.5 INCHES FROM BOTTOM AND 20 INCHES FWD OF T/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041047Skin · damagedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DAMAGE, 37 INCH FWD OF T/E, 48 INCH UP FROM BOTTOM. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI-LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041048Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION, 32 INCHES FWD OF T/E, 54.5 INCH UP FROM BOTTOM LT SIDE. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTILAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041050Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .3750 INCH X .1875 INCH AREA, DELAMINATION, 3 INCH AFT OF NR 6 HINGE CUTOUT. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA041051Skin · corrodedPIT - Q1 -RUDDER TOP LAYER, .1250 INCH X .1250 INCH X .005 INCH DEEP PIT, 8.25 INCH FWD OF T/E, 72 INCHES DOWN FROM TIP. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA040843Skin · crackedSKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 7, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040841Skin · delaminatedSKIN, 4 INCH BY 14 INCH AREA DELAMINATION, LT OB FOREFLAP T/E IB END. DEFECTIVE PART REPLACED WITH IDENT PN.Nov 5, 2004 · N776AU · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040919Angle · crackedPIT - Q1 - T-ANGLE, 3 INCH BY 4 INCH AREA CRACKED AND PULLED. OUTBD SLING ATTACH POINT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Nov 5, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040934Skin · delaminatedPIT - Q1 - FLAP, 3.5 INCH BY 5 INCH AREA, DELAMINATED, OB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040935Skin · delaminatedPIT - Q1 - FLAP, 4.5 INCHES BY 5 INCHES DELAMINATION, IB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA040937Skin · delaminatedPIT - Q1 - SLAT 15 INCH BY 6 INCH DELAMINATION. NR 3 SLAT IB END. REMOVED TOP SKIN AND CORE, INSTALLED INTERNAL DOUBLER, CORE, TOP SKIN TYP REP 57-42-03, SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7 · Leading Edge DevicesSDR USAA040984Bulkhead · crackedPIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 209 DETAIL II.Nov 5, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040840Bulkhead · crackedC3, BULKHEAD WEB, 3 CRACKS, .1250 INCH, FPBH BS 178, RBL 6, WL 210 AND 213. DOUBLER INSTALLED IAW EO 5300V153.Nov 4, 2004 · N776AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040905Attach Angle · crackedPIT - Q5 - ANGLE, 6 INCH LONG CRACK, HORIZ STAB CTR SECTION THRUST BEAM ATTACH ANGLE LT SIDE. REMOVED AND REPLACED ANGLE, REPLACED IAW TYP REP SRM 51-00-30. REMOVED AND REPLACED IAW TYP REP SRM 51-00-30.Nov 4, 2004 · N516AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040920Skin · incorrectPIT - Q1- SKIN, 12 INCH BY 6 INCH INCORRECT DOUBLER REPAIR, FRAME ST 344 S19R. OLD DOUBLER REMOVED AND NEW DOUBLER INSTALLED TO COMPLY WITH NEW SRM DIRECTIONS IAW SRM 53-00-01, FIG 231.Nov 4, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA040839Bulkhead · crackedPIT - C3, SKIN, 2 CRACKS, 1 INCH IN LENGTH TOTAL, FPBH WL 234, BL7R. DOUBLER REPAIR IAW SRM 53-10-08, FIG 209.Nov 3, 2004 · N776AU · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA040903Angle · crackedHORIZ STAB CENTER SECTION THRUST BEAM ATTACH ANGLE RT SIDE. REMOVED AND REPLACED ANGLE IAW TYP REP REMOVED AND REPLACED SRM 51-00-30.Nov 3, 2004 · N516AU · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA040924Track · crackedPIT - Q1 - TIE DOWN TRACK, CORROSION AND CRACK, 2 INCH BY 4 INCH AREA AND 1 INCH CRACK. CORROSION; LEVEL 1: TASK NR C 53-208-01, BS 727F, S 26L. CUT OUT DAMAGED SECTION AND SPLICED IN NEW IAW SRM 53-00-53, FIG 202.Nov 3, 2004 · N435US · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040932Angle · corrodedPIT - Q1 - ZEE ANGLE, 2 INCH BY 3 INCH AREA, CORROSION LEVEL 1, TASK NR C53-100-1, BS 796, S25R IN AFT CARGO BIN. REMOVED ZEE ANGLE, AND INSTALLED NEW IAW SRM 51-10-2.Nov 3, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040947Strap · corrodedPIT - Q5 - STRAP, .2500 INCH BY .2500 INCH IN 66 AREAS, CORROSION; LEVEL 1; TASK NR-C53-107-02, AFT CARGO DOOR FRAME SECTION S25R, STA 807-848. REPLACED PART IAW SRM 53-00-07.Nov 3, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040926Frame · crackedPIT - Q1 - FRAME, .1250 INCH CRACK, BS787 AT S9L-S8L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR ANGLES IAW TYP REP 53-10-02A.Nov 2, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA041043Skin · delaminatedPIT - Q1 - TOP SKIN, 3 INCH X 3 INCH AREA AND LOWER SKIN DAMAGE 1 INCH SQUARE, DELAMINATION AND SKIN DAMAGE, NR 4 SLAT TOP SURFACE T/E. INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER IAW SRM.Nov 2, 2004 · N435US · Boeing 7374B7 · Leading Edge DevicesSDR USAA040925Seat Track · crackedPIT - Q1 - SEAT TRACK, .75 INCH LONG CRACK, IB RT SEAT TRACK STA 727B, UPPER FLANGE LOWER SURFACE AT VERTICAL RADIUS. CUT OUT SECTION AND REPLACED NEW AND DOUBLERS IAW SRM 53-00-52.Nov 1, 2004 · N435US · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040922Duct · crackedPIT - Q1 - AIR DUCT, .5 INCH CRACK, LT RAM AIR DUCT UPPER SIDEWALL AT STA 540 AND S-22L. INSTALLED DOUBLER IAW TYP REP 53-50-03.Oct 31, 2004 · N435US · Boeing 7374B7 · Air Distribution SystemSDR USAA040838Angle · crackedANGLE, 3 INCHES, CRACK, ANGLE, FWD SVC DOOR, INTERIOR STRUCTURE JUST BELOW WINDOW. REPLACED L ANGLE IAW SRM 51-40-02.Oct 30, 2004 · N776AU · Boeing 7374B7 · Service DoorsSDR USAA040928Clip · crackedPIT - Q1 - ATTACH CLIP, .5 INCH CRACK, STA 706, STR 1. REMOVED AND REPLACED WITH INDENT PART IAW SRM 51-40-02 AND 51-40-03.Oct 30, 2004 · N435US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA040902Support Fitting · crackedPIT - Q5 - L/G SUPPORT FITTING, .2500 INCH CRACK, LT MLG SUPPORT FITTING AT REAR SPAR. REMOVED AND REPLACED WITH NEW FITTING IAW EO 5702V054.Oct 29, 2004 · N516AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA040912Frame · crackedPIT - Q1- FRAME, 1 INCH CRACK AND .7500 INCH CRACK (2 CRACKS) BS 616 AT S17L AND BS 616 AT S17R. CUT OUT DAMAGE, INSTALLED FILLERS AND NESTED ANGLES IAW TYP REP 53-62-01.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040916Frame · crackedPIT - Q1 - FRAME, .2500 INCH CRACK, BS 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR IAW TYP REP 53-10-20A.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040917Intercostal · crackedPIT - Q1 - MOUNT/INTERCOSTAL WITH 2 INCH CRACK AND 2 INCH BY 4 INCH CORRODED AREA, BS 727D TO BS 727E AT S 28L. REMOVED CORROSION, TREATED AND PRIMED. REPLACED INTERCOSTAL MOUNT IAW SRM 51-10-2.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA040927Clip · brokenPIT - Q1 - ATTACH CLIP, BROKEN, FRAME 706, STR S1. REMOVED BROKEN TIE CLIP AND REPLACED WITH SAME IAW SRM 51-40-02 AND 51-40-03.Oct 29, 2004 · N435US · Boeing 7374B7 · Fuselage Miscellaneous Structure
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