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 USAA060150Web · crackedLOCATION: STA 601, S18R ACTION: REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 97260, DEFECT SIZE: .250 INCH.Jan 27, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060149Skin · gougedLOCATION: LWR L/B CORNER AT L/E OF LT MID FLAP. REMOVED OLD REPAIR, INSTALLED NEW IAW SRM 57-53-01 DEFECT SIZE: 4 INCHES.Jan 27, 2006 · N422US · Boeing 737401 · Trailing Edge FlapsSDR USAA060157Angle · crackedLOCATION: BS540 AT STR 22R. FABRICATED AND INSTALLED REPAIR PARTS IAW TR 53-50-03, DEFECT SIZE: 1 INCH.Jan 27, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060151Skin · erodedLWR END OF VERT STAB L/E. SANDED AND REPAIRED AREA WITH COMPOSITE REPAIR, DEFECT SIZE: 6 INCHES X 3 INCHES.Jan 27, 2006 · N784AU · Boeing 7374B7 · Vertical Stabilizer, Plate/SkinSDR USAA060152Angle · crackedLOCATION: RT WING 135.5 RIB LOWER CHORD ANGLE CRACKED BETWEEN S2 AND S3. TRIMMED TEE REPAIR IAW EA 97288, DEFECT SIZE: 2.5 INCH.Jan 27, 2006 · N775AU · Boeing 7374B7 · Wing, Attach FittingsSDR USAA060153Angle · crackedLOCATION: BS 294 FWD SERVICE DOOR. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-02/03/05/06, DEFECT SIZE: 1INCH.Jan 27, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060154Strap · crackedSTA 312 RBL 32 ACTION: FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-51 DEFECT SIZE: 1INCH.Jan 27, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060143Rib · crackedLOCATION: WBL 135.5 RIB 12 INCHES FWD OF AFTS ACTION: REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 97288, DEFECT SIZE: 1 INCH.Jan 25, 2006 · N775AU · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA060144Shear Tie · damagedLOCATION: FRAME 500C AT STR 14R. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 97321, DEFECT SIZE: .187 INCH.Jan 25, 2006 · N775AU · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA060146Fitting · crackedRT WING, RT MLG SUPPORT FITTING REPLACEMENT. FABRICATED REPAIR (T) FITTINGS IAW EA 97282. DEFECT SIZE: 1.25 INCHES. (K)Jan 25, 2006 · N784AU · Boeing 7374B7 · Wing, Landing Gear Attach FittingsSDR USAA060147Fitting · crackedLT WING FUEL TANK WBL 135.5 RIB LOWER CHORD. FABRICATED REPAIR TEE, FILLERS AND VERTICAL STIFFENER IAW EA 97288 DEFECT SIZE: 1 INCHJan 25, 2006 · N775AU · Boeing 7374B7 · Wing, Attach FittingsSDR USAA060142Skin · lightning strikeLOCATION: STA 500 BETWEEN S24R AND S25R. INSTALLED FILLER AND DOUBLER IAW SRM 53-00-01. DEFECT SIZE: .5 INCH X .5 INCH.Jan 25, 2006 · N406US · Boeing 737401 · Fuselage Main, Plate/SkinSDR SB06009Clamp · brokenDURING CRUISE, CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN WAS CLIMBING THROUGH 10,500 FEET. CREW ACCOMPLISHED QUICK REF PROCEDURES WHICH REQUIRED THEM TO DEPLOY CABIN OXYGEN MASKS. CREW TRIED SEVERAL MODES TO RECOVER CABIN WITH NO HELP. FLIGHT DIVERTED AND LJan 22, 2006 · N427US · Boeing 7374B7 · Cabin Pressure Control SystemSDR USAA0511Floorbeam · corrodedBS 986.5 CABIN FLOORBEAM LBL 18, 21, 24, 30 CORRODED. REPLACED T-CAP IAW TR 53-60-01A, DEFECT SIZE: SEVERAL 1INCH X 1INCH CORRODED AREAS.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA0512Angle · crackedBETWEEN STA 927 AND 947.5 AT BL 0 CRACK. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA0513Frame · crackedSTA 440, S-8L CRACKED. FABRICATED ANGLES FROM NR 1133534 AND 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA0514Frame · crackedSTA 907, BELOW S-8L CRACKED. FAB FROM ANGLES 1133534 & 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: FRAME CRACKED 0.25 INCH.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA0515Tie Clip · crackedSTR 4R, BS 727E CRACKED. INSTALLED NEW CLIP CC 1133482, INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA0516Floorbeam · corrodedCORROSION ON FLOORBEAM STA 328 RBL 21. INSTALLED DOUBLER IAW SRM 53-00-51 FIG 201, DEFECT SIZE: SHEETMETAL ITEM 1030M EVIDENCE OF CORROSION ON FLOORBEAM 1 X 2 INCH, STA 328 RBL 21.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR SWAA060094Bulb · inoperativeDURING SCHEDULED C1 CHECK, FOUND LT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.Jan 5, 2006 · N693SW · Boeing 737317 · Emergency LightingSDR PIDA06001Web · crackedINNER WEB OF THE FORWARD CARGO DOOR IS CRACKED. REPAIRED DAMAGE IAW SRM 52-00-01 AND 51-70-13.Dec 29, 2005 · N390WL · Boeing 7373G7 · Cargo/Baggage DoorsSDR AWXA200600015Regulator · stuckEMERGENCY EQUIPMENT, DURING C 16 CHECK DISCOVERED CAPTAIN'S OXYGEN MASK DEMAND REGULATOR STUCK IN EMERGENCY POSITION. MAINTENANCE REMOVED AND REPLACED THE O2 MASK IAW TASK CARD R1B35001. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN DOES NOT CONFIRM FAULT.Dec 28, 2005 · N323AW · Boeing 7373Y0 · Crew Oxygen SystemSDR USAA051552Skin · crackedRSB 727E RS24, MAJOR REPAIR, CUT OUT CRACK, FABRICATED AND INSTALLED 9.5 IN X 13 IN DOUBLER IAW SRM 53-00-01 FIG 201 DEFECT SIZE: 2TDec 14, 2005 · N591US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA051556Seat Track · crackedLOCATION: BS727B RBL 24.75 (RT IB SEAT TRACK FLOOR BEAM) ACTION: FABRICATED AND INSTALLED NEW SECTION OF TRACK/BEAM IAW SRM 53-00-52 EA 97204 DEFECT SIZE: .250 INCH.Dec 14, 2005 · N783AU · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051550Skin · crackedLOCATION: IB SIDE OF NR 1 ENGINE PYLON. INSTALLED DOUBLER IAW TR 54-50-07, DEFECT SIZE: .250 IN.Dec 14, 2005 · N591US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR AWXA200501480Light · inoperativeEEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT AT ROW 5, LT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Dec 3, 2005 · N328AW · Boeing 7373B7 · Emergency LightingSDR SB05158Battery Pack · dischargedMAINTENANCE REPORTED THE AFT LT EMERGENCY EXIT LIGHT ABOVE THE R2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Nov 27, 2005 · N409US · Boeing 737401 · Emergency LightingSDR USAA200511002Skin · cracked2.5 INCH CRACK FOUND AT STA 727E AT STRINGER 23L. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.Oct 31, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05129Engine · failedPIT - FLT 391 - ON CLIMBOUT FROM PIT, AT FL140, CREW REPORTED A LOUD BANG FROM THE NR 1 ENGINE. SIMULTANEOUSLY, SMOKE FILLED THE COCKPIT, THE NR 1 ENGINE OVERTEMP LIGHT ILLUMINATED AND THE AIRCRAFT YAWED. ENGINE CAME TO AN ABRUPT STOP. CREW SECURED THE ENGIOct 11, 2005 · N778AU · Boeing 7374B7 · Engine (Turbine/Turboprop)SDR SB05097Charger · inoperativeMAINTENANCE REPORTED THE BATTERY CHARGER FOR THE AFT ENTRY DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD.Aug 23, 2005 · N520AU · Boeing 7373B7 · Emergency LightingSDR USAA051030Skin · damagedCLT - Q6 - PYLON SKIN, 1.3 INCH, GROOVE IB SIDE OF NR 2 ENGINE PYLON AT WING L/E JUNCTION. REPAIRED IAW TYPICAL REPAIR IAW TR. (K)Aug 19, 2005 · N588US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA051031Skin · crackedCLT - C5 - SKIN, 3 INCH CRACK, 727B-737C AT STRINGER 23R. INSTALLED DOUBLER IAW SRM. (K)Aug 19, 2005 · N417US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA051032Pan · crackedCLT - C4 - PAN AND SERVICE DOOR, .25 INCH CRACK, BS 1000, STRINGER S26R. INSTALLED DOUBLER IAW EA. (K)Aug 19, 2005 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR SB05094Light · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD.Aug 17, 2005 · N442US · Boeing 7374B7 · Emergency LightingSDR USAA051022Frame · crackedBFM - Q2 - FLAME, 2.45 INCH LT, CRACKED FWD CARGO FRAME BS 500 BL 0. TRIM OUT CRACK, FAB REPAIR, INSTALLED DOUBLER IAW EA. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051023Intercostal · crackedBFM - Q2 - FLOORBEAM INTERCOSTAL, .250 INCH CRACK, BET STA 328, 344 CABIN FLOORBEAM. INSTALLED REPAIR DOUBLER, TREATED AND PRIMED IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051024Floorbeam · corrodedBFM - Q2 - FLOORBEAM UPPER CHORD, 50 INCH CORROSION; NO LEVEL OR TASK; FS 986.5, LBL 0 TO LBL 50 INCH. FABED PART FLOORBEAM UPPER CHORD, INSTALLED IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051025Stringer Clip · crackedBFM - Q2 - STRINGER CLIP, .250 INCH CRACK, STA 277; STR 9 L STR CLIP. INSTALLED REPAIR STRINGER CLIP STA 907 IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051026Shear Tie · crackedBFM - Q2 - SHEAR TIE CLIP, .250 INCH CRACK, STA 277, SHEAR TIE CLIP, STR 9L TO 10L. INSTALLED SHEAR CLIP ON STR STA 277 IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA051027Gate · corrodedBFM - Q2 - DOOR GATE SKIN, 29 INCH L X .250 INCH W, CORROSION; LEVEL 2; TASK C53-100-01, AFT ENTRY DOOR BOTTOM GATE LOWER EDGE OF SKIN. REMOVED AND REPLACED AFT ENTRY DOOR BOTTOM GATE IAW MM, SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Passenger/Crew DoorsSDR USAA051028Shear Tie · crackedBFM - Q2 - SHEAR TIE CLIP, .050 INCH CRACKED, STA 277, STR 8L TO 9L SHEAR TIE CLIP. INSTALLED REPAIR PART, SHEAR CLIP, STA 277 IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA051029Splice · crackedBFM - Q2 - STRINGER SPLICE, .250 INCH, STA 907, STR; CRACK ON FASTENER HEAD, STA 907, STRINGER CRACK ON FASTENER HEAD. INSTALLED REPAIR/ FAB SPLICE ON STRINGER IAW SRM. (K)Aug 17, 2005 · N444US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051008Angle · corrodedCLT - Q6 - ANGLE, KEEL BEAM HAS FRETTING WEAR ON IT 17 IN X 1 INCH, CORRODED, STA 727-710, LBL 8. REMOVED SURF CORROSION, BLENDED AND TREATED IAW SRM, DWG. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051009Keelbeam · corrodedCLT - Q6 - ANGLE, ON KEELBEAM COMPOSITE SKIN ATTACH ANGLE HAS FRETTING WORN INTO IT, 5 INCHES X 1 INCH. CORROSION, STA 673, STA 678, LBL 8. REMOVED CORROSION, BLENDED, AND TREATED IAW SRM, DWG. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA051010Support Beam · corrodedCLT - Q6 - LT MLG SUPPORT BEAM OB LUG FACE AND HEAVY WEAR/ MATERIAL LOSS ON IB LUG FACE 2 INCH X 2 INCH TYPICAL. LT MLG SUPPORT BEAM; STABILIZER BEAM FITTING ASSY. CLEANED AND TREATED CORROSION, INSTALLED BUSHINGS IAW SRM. (K)Aug 16, 2005 · N588US · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA051004Bracket · crackedCLT - Q1 - BRACKET, 1 INCH, CRACK, STA 360, STR 7L BRACKET. REMOVED DAMAGED BRAKET, FRABRICATED NEW BRACKET AND INSTALLED, ISW SRM AND DWG. (K)Aug 15, 2005 · N449US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA051005Skin · crackedCLT - Q6 - LOWER SKIN, 1.7 INCH CRACK LOWER SKIN APPROX STAB STA 129 AT AFT SPAR, HORIZONTAL STAB. REPAIRED AND INSTALLED DOUBLER AND FILLER IAW EA. (K)Aug 15, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR USAA051006Skin · crackedCLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)Aug 15, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR USAA0514007Channel · crackedCLT - Q1 - SPLICE CHANNEL, 1 INCH CRACK, BS 360, S-15L STRINGER SPLICE CHANNEL. REMOVED DAMAGED SLICE AND INSTALLED NEW SLICE IAW SRM. (K)Aug 15, 2005 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050993Frame · crackedCLT, Q6, FRAME .125 INCH CRACK, STRINGER 9 LT STA 500A. REPAIRED IAW TR 53-10-20B. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Frame
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