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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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)SDR USAA050991Stringer Splice · crackedCLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K)SDR 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)SDR 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)SDR 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)SDR 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)SDR USAA050984Beam · crackedCLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K)SDR USAA050971Skin · crackedCLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR USAA050943Lug · corrodedCLT - Q6 - LUGS, CORROSION; NO LEVEL OR TASK, L2/L5 BORES, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHINGS IAW SRM. (K)SDR 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)SDR 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)SDR USAA050948Bushing · corrodedCLT - Q6 - LUG/BUSHING, CORROSION, L6 LUG, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR USAA050881Balance Arm · wornCLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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 SDR USAA050880Flange · wornCLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)SDR DU4R0507153Skin · dentedFUSELAGE SKIN HAS DENT AT BS 480 S-26R - S-28R.SDR DU4R0507144Frame · crackedBS 178 BULKHEAD RT SIDE AFT SIDE FRAME HAS EVIDENCE OF CRACK ABOVE AND BELOW WL 207.SDR DU4R0507145Bulkhead · crackedCRACK APPROX. 5.5 INCHES BELOW WL 207 IB SIDE LBL 5.7 APPROX. 1.2 INCH IN LENGTH AT BS 178 BULKHEAD.SDR DU4R0507148Skin · dentedDENT AT RT EXTERNAL FUSELAGE SKIN AT BS 391.5 BETWEEN S-22R AND S-23R.SDR 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.SDR 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.SDR 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)SDR USAA050804Threshold · corrodedCLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K)SDR 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)SDR 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)SDR 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)SDR USAA050808Angle · crackedCLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K)SDR 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)SDR 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)SDR 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)
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