CFM International CFM56-3B2

Service difficulty reports · 635

Newest first. General aviation reporting is voluntary.

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 USAA050992Frame · crackedCLT, Q6 FRAME, 1.4 INCH CRACK, BS 616 RT BOTTOM OF FRAME INNER CHORD BS 616 RT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW TR 53-62-01. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050991Stringer Splice · crackedCLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050990Support · crackedCLT, Q6, PSU SUPPORT RAIL, 2 CRACKS, .1250 INCH, .1875 INCH, CRACK, BS 727D BETWEEN S8L AND 9L. DAMAGE REMOVED, INSTALLED REPAIR ANGLES IAW SRM. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050987Floorbeam · crackedBFM, Q2, TEE CHORD, .5 INCH CRACK, CABIN FLOORBEAM AT STA 312 RBL 35. FABRICATED NEW UPPER CHORD, LOCATED DRILLED AND INSTALLED ALL REPAIR PARTS IAW SRM. (K)Aug 5, 2005 · N444US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050989Floor Support · crackedBFM - Q2 - CHANNEL, 1 INCH AND 1.25 INCH, CRACKS (2), PAX CABIN FLOOR SUPPORT (CHANNEL) AT STA 540 LBL 1. DEFECTIVE PART REPLACED WITH IDENT PART. (K)Aug 5, 2005 · N444US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050988Support · corrodedBFM, Q2, ZEE SUPPORT, 100 INCHES, CORROSION; LEVEL 1 TASK C53-202-01, AFT CARGO COMPT RT SUPPORT ZEE STA 727C-747. FABRICATED AND INSTALLLED NEW ZEE SUPPORT IAW SRM. (K)Aug 5, 2005 · N444US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050984Beam · crackedCLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K)Aug 5, 2005 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050971Skin · crackedCLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K)Aug 3, 2005 · N511AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050970Skin · crackedCLT - Q1 - SKIN, 1 INCH CRACK, STA 727D, BELOW S-23L (NEAR LIGHT). CUT OUT CRACK, FABRICATED DOUBLER AND FILLER, INST 12 INCH X 12 INCH DOUBLER IAW SRM. (K)Aug 3, 2005 · N449US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR A6WA200540276Vane · wornRT OB FLAP VANE, OB FLAP VANE FITTING WORN EVEN WORN LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED IAW REO. REMOVED OLD VANE FITTING FROM RT OB FLAP AS WS296.073 AND INSTALLED NEW VANE FITTING IAW REO. (K)Aug 3, 2005 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR USAA050946Bushing · corrodedCLT - Q6 -LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L1,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050945Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, LT,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA0540944Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L2, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050942Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L5, AFT FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050943Lug · corrodedCLT - Q6 - LUGS, CORROSION; NO LEVEL OR TASK, L2/L5 BORES, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHINGS IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050941Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK. L5, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050947Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L3, AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050948Bushing · corrodedCLT - Q6 - LUG/BUSHING, CORROSION, L6 LUG, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050906Stiffener · corrodedCLT - Q6 - STIFFENER, .5 INCH X 6 INCH CORROSION; NO LEVEL OR TASK. STR 26R, BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION, ATTACH FITTING AND STIFFENER IAW SRM. (K)Jul 28, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050903Skin · crackedCLT - C1 - FUSELAGE SKIN, .75 INCH CRACK, GROUND AIR SERVICE CONNECTION DOOR CUTOUT AT AREA BETWEEN BS 520-BS 540. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K)Jul 27, 2005 · N404US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA050904Shear Tie · corrodedCLT - C1 - SHEAR TIE, .3125 INCH HOLE, 4.5 INCH CORROSION, STA 867 BOTTOM OF FUSELAGE BETWEEN SHEAR TIE AND SKIN. REMOVED CORRODED SHEAR TIE AND REPLACED WITH NEW SHEAR TIE. (K)Jul 27, 2005 · N404US · Boeing 737401 · Fuselage Internal Mounting StructureSDR USAA050905Shear Tie · corrodedCLT - C1 - SHEAR TIE, 5.5 INCH X 1.0 INCH CORROSION, BETWEEN SHEAR TIE AND SKIN AT STA 867 BOTTOM OF FUSELAGE. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW SRM. (K)Jul 27, 2005 · N404US · Boeing 737401 · Fuselage Internal Mounting StructureSDR USAA050902Panel · crackedCLT - C1 - PANEL, 2 INCH CRACK, TOP OF LT WING PANEL JUST OB OF GROUND SPOILER. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE AND DOUBLER IAW SRM. (K)Jul 27, 2005 · N404US · Boeing 737401 · Wing, Plate/SkinSDR USAA050900Angle · corrodedCLT - Q6 - TRANSITION ANGLE, 12 INCH X 1 INCH, CORROSION, AFT CARGO STA 737-767. REMOVED DAMAGE, FABRICATED NEW PART AND INSTALLED IAW SRM. (K)Jul 21, 2005 · N588US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA050899Skin · wornCLT - Q - SKIN, 12 INCHES X .250 INCH X .015 INCH, SKIN WEAR, BS870, WL306.5, LBL3. INSTALLED REPAIR DOUBLER AND INSTALLED NEW RUB STRIPS IAW EA, WEIGHT CHANGE OF 1.5 LBS. (K)Jul 21, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050901Support Fitting · crackedCLT - Q5 - AFT SUPPORT FITTING, 1 INCH, CRACKED, FASTENER HOLE AT MLG BEAM ATTACH PT TO AFT SPAR ON AFT SUPPORT FITTING UP CHRD. REPAIR OF FITTING INCLUDED REAMING OF DISCREP HOLE, SHIMMING IAW EA. (K)Jul 21, 2005 · N441US · Boeing 7374B7 · Wing, Landing Gear Attach FittingsSDR USAA050897Support Angle · crackedCLT - C-6 - SUPPORT ANGLE, .75 INCH CRACK. SUPPORT ANGLE FOR UPPER FIXED T/E PANEL OB OF NACELLE, LT WING. FABRICATED AND INSTALLLED NEW ANGLE, SRM. (K)Jul 20, 2005 · N419US · Boeing 737401 · Wing Main, Frame StructureSDR USAA050898Vertical Support · crackedCLT - C6 - VERTICAL STIFFNER, .5 INCH CRACK, WS 537 VERTICAL STIFFNER FWD NR 2 ARERON HINGE, RT WING. DRILLED NEW ANGLE AND INSTALLED IAW SRM. (K)Jul 20, 2005 · N419US · Boeing 737401 · Wing Miscellaneous StructureSDR USAA050881Balance Arm · wornCLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)Jul 18, 2005 · N441US · Boeing 7374B7 · Rudder StructureSDR USAA050882Angle · crackedCLT - Q5 - ANGLE, .375 INCH, CRACKED AT STA 601LT SIDE BODY WING TERMINAL FORGING ANGLE CRACKED ON AFT SIDE. REMOVED DAMAGED AND INSTALLED REPAIR ANGLE IAW SRM. (K)Jul 18, 2005 · N441US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050883Skin · crackedCLT - C1 - SKIN, .75 INCH CRACK, BS530 BL0, WL148.5 FUSELAGE SKIN AT THE GROUND CONDITIONED AIR CUT OUT. INSTALLED DOUBLER IAW SRM. (K)Jul 18, 2005 · N404US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA050885Vertical Support · crackedBFM - Q6 - VERTICAL STIFFENER, 1.0 INCH RACK, CRACKED, WHEEL WELL FWD BULKHEAD 663 LBL 6.15. REPLACED STIFFENER IAW EA AND SRM. (K)Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050886Web · dentedBFM - Q6 - WEB SKIN, 18 INCH X 2.0 INCH X .040 INCH DENT. BS 1016, BTW STR 24R-27R. FAB DOUBLER, FILLER, NEW SKIN SECTION, INSTALLED IAW EA AND SRM. (K)Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500812Generator · malfunctionedNR 1 ENGINE GENERATOR HAD LOW OIL PRESSURE AND HIGH OIL TEMP. DISCONNECTED GENERATOR AND RETURNED TO GEG. APU WAS ON MEL. MX R & R APU BLEED VALVE, CLEARED APU MEL. ISSUED MEL FOR NR 1 ENGINE GENERATOR. VENDOR TEAR DOWN REPORT SHOWS THAT CSD HAD VERY HIGH Jul 15, 2005 · N315AW · Boeing 7373S3 · Alternator-Generator DriveSDR USAA050880Flange · wornCLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)Jul 14, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, KeelSDR DU4R0507153Skin · dentedFUSELAGE SKIN HAS DENT AT BS 480 S-26R - S-28R.Jul 7, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/SkinSDR DU4R0507144Frame · crackedBS 178 BULKHEAD RT SIDE AFT SIDE FRAME HAS EVIDENCE OF CRACK ABOVE AND BELOW WL 207.Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, FrameSDR DU4R0507145Bulkhead · crackedCRACK APPROX. 5.5 INCHES BELOW WL 207 IB SIDE LBL 5.7 APPROX. 1.2 INCH IN LENGTH AT BS 178 BULKHEAD.Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, BulkheadSDR DU4R0507148Skin · dentedDENT AT RT EXTERNAL FUSELAGE SKIN AT BS 391.5 BETWEEN S-22R AND S-23R.Jul 6, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/SkinSDR SB05077Charger · inoperativeMAINTENANCE REPORTED THE EMERGENCY EXIT SIGN BETWEEN THE AFT LAVATORIES, OVER THE R2 DOOR AND OUTSIDE OF THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD.Jun 30, 2005 · N519AU · Boeing 7373B7 · Emergency LightingSDR DU4R0507135Skin · dentedCREASE IN DENT AT BS 971 BETWEEN S-24L-25L 2 INCHES X .86 A/Y = 23.3. S/O NR 109002, OPS NR 25863.Jun 30, 2005 · N311FL · Boeing 7373S1 · Fuselage Main, Plate/SkinSDR USAA050803Stringer · corrodedCLT - Q2 - CARGO FLOOR STRINGER, 6 INCH, CORROSION, AFT CARGO FLOOR STRINGERS AT STA 736 FROM LBBL 17.2 TO RBBL 13.8. REMOVED AND TREATED CORROSION IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050804Threshold · corrodedCLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050805Mount · corrodedCLT - Q2 - LAV MOUNT, 1 INCH X 3 INCHES, CORROSION, LT AFT LAV OB MOUNT. FABRICATED AND INSTALLED NEW MOUNT IAW WITH DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050806Intercostal · dentedCLT - Q2 - INTERCOSTAL, 2 INCHES X 1 INCH, DENT, STR 25L BETWEEN FRAMES 440 AND 420. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050807Floor Support · crackedCLT - Q2 - FLOOR SUPPORT, 1 INCH CRACK, FLOOR SUPPORT AT STA 500D IN A/C DISTRIBUTION BAY. REMOVED DAMAGED WEB, FABRICATED NEW WEB IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050808Angle · crackedCLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050809Angle · corrodedCLT - Q2 - L-ANGLE, 6 INCH FRETTING, L-ANGLE AT BS 1016 FORWARD OF THE RT FWD VERTICAL FIN MOUNT. FABRICATED AND REPLACED NEW L ANGLE. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050810Skate Angle · wornCLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach FittingsSDR USAA050811Bracket · wornCLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Wing, Attach Fittings
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