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 USAA050812Support Angle · crackedCLT - Q2 - SUPPORT ANGLE, 1 INCH, CRACK, STA 540 AND STR 22R. FABRICATED AND INSTALLED REPAIR PART. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050813Skin · dentedCLT - Q - SKIN, 2 INCH X 3 INCH DENT, BS328 AND S23R. REPAIR DOUBLER IAW SRM.Jun 29, 2005 · N425US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA050814Floor Support · corrodedCLT - Q5 - STA 328-344, LBL9, 2 INCH X 2 INCH, CORROSION, FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050815Stiffener · corrodedCLT - Q5 - FLOOR STIFFENER, 2 INCH X 16 INCH CORROSION, STA 312-328, LBL12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050816Floor Support · corrodedCLT - Q5 - FLOOR SUPPORT, 2 INCH X 2 INCH CORROSION, STA 312-328, RBL 13. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER SUPPORT IAW SRM. (K)Jun 29, 2005 · N441US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050817Skin · crackedCLT - C3 - SKIN, .75 INCH CRACK, RT PYLON AT CORNER OF CUTOUT FOR PANEL NR 5828R, NAC, STA 166.5. INSTALLED DOUBLER IAW TYPICAL REPAIR SRM. (K)Jun 29, 2005 · N430US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA050818Door Frame · crackedCLT - C3 - FWD SERVICE DOOR, .6 INCH CRACK, FWD SERVICE DOOR FRAME LOWER AFT CORNER AFT LIGHTING HOLE. INSTALLED DOUBLER IAW EA. (K)Jun 29, 2005 · N430US · Boeing 7374B7 · Service DoorsSDR USAA050800Skin · wornMID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K)Jun 27, 2005 · N441US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA050801Skin · gougedCLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K)Jun 27, 2005 · N441US · Boeing 7374B7 · Trailing Edge FlapsSDR USAA050802Rib · gougedCLT - C4 - RIB, 4 INCHES X .5 INCH, GOUGE, RT WING, WBL 417 JUST OB OF OB FOREFLAP. CUTOUT DAMAGE AND INSTALLED DOUBLER IAW EA. (K)Jun 27, 2005 · N421US · Boeing 737401 · Wing, Rib/BulkheadSDR USAA050738Channel · crackedCLT - C4- CHANNEL, 1 INCH CRACK, NR 3 SLAT JUST BELOW ROD END ACTUATOR ATTACHMENT POINT (L) CHANNEL. FABRICATED AND INSTALLED NEW CHANNEL. (K)Jun 7, 2005 · N589US · Boeing 737301 · Leading Edge DevicesSDR USAA050736Angle · corrodedCLT - Q3/QX4 - Z ANGLE, .25 INCH X .25 INCH CORROSION; LEVEL 1; TASK C53-107-01, LBL 60, STA 951-986. REMOVED AND REPLACED REPAIR PARTS IAW EA. (K)Jun 7, 2005 · N445US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050737Skin · crackedCLT - Q3/QX4 - WING L/E SKIN, .2500 INCH CRACK AND DENT; L/E SKIN ABOVE IB KREUGER FLAP. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM. (K)Jun 7, 2005 · N445US · Boeing 7374B7 · Leading Edge DevicesSDR DU4R108Pan · corrodedRT FLOOR PAN AT BS 1016 WL208.1 CORRODED. S/O 109001, N/R 22825May 31, 2005 · N312FL · Boeing 7373L9 · Fuselage Miscellaneous StructureSDR 102Seat Track · gougedCABIN LT IB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22850May 27, 2005 · N312FL · Boeing 7373L9 · Fuselage, Seat/Cargo Attach FittingsSDR 80Skin · gougedAIRCRAFT DAMAGE BELOW AFT PIT FROM BELT LOADER BS 755-790, S-25R. LOG PAGE ITEM NR1 PG. 158526,S/O 109001, N/R 22583.May 2, 2005 · N312FL · Boeing 7373L9 · Fuselage Main, Plate/SkinSDR F3L2005F00000Engine · leakingAPPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR 2 ENG ALSO GOING TO ZERO. NR 1 ENG OIL PRESS THEN DROPPED TO ZERO, NR 2 ENG OIL PRESS DROPPED TO MApr 22, 2005 · N313FL · Boeing 737300 · Turbine Engine Oil SystemSDR F3LA200500018Cover · missingAIR RETURN TO DEN, ON CLIMB-OUT, BOTH ENGINE OIL QUANTITY INDICATORS WENT TO ZERO. BOTH OIL PRESSURE INDICATORS WENT TO ZERO. BOTH LOW OIL PRESSURE LIGHTS ILLUMINATED. ENGINES OPERATED APPROXIMATELY 15 MINUTES IN THAT CONDITION UNTIL LANDING, WHICH WAS WITHApr 22, 2005 · N313FL · Boeing 7373L9 · Turbine Engine Oil SystemSDR USAA050436Stringer Clip · crackedCLT - Q6 -TIE CLIP, (.5 INCH CRACK), STATION 578.0991, STRINGER 8R. REPLACED TIE CLIP IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050437Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK) STRINGER 4R STA 908.0903. INSTALLED SLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA050438Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK), STRINGER 4L, STATION 908.0906. INSTALLED SPLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA050439Support Angle · crackedCLT - Q6 - SUPPORT ANGLE, (.075 INCH) CRACK, STRINGER 11R, STATION 354. INSTALLED NEW ANGLE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050431Floorbeam · corrodedCLT - Q4 - FLOORBEAM, (.5 INCH) CORROSION. STA 312, BL 0 TO RBL 10. SPLICED IN NEW T-CAP IAW SRM. (K)Mar 30, 2005 · N440US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA050428Skin · crackedCLT - Q6 - EXTERNAL SKIN, 1 INCH, CRACKED, FWD CARGO DOOR HANDLE CUTOUT. (K)Mar 29, 2005 · N442US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA050429Skin · crackedCLT - Q6 - EXTERNAL SKIN, (1 INCH CRACK), AFT CARGO DOOR HANDLE CUTOUT. INSTALLED DOUBLER. (K)Mar 28, 2005 · N442US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA050430Skin · damagedCLT - Q6 - RUDDER SKIN, (.5 INCH X .5 INCH) COMPOSITE DAMAGE, RUDDER T/E STA 151. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)Mar 28, 2005 · N442US · Boeing 7374B7 · Rudder, Plate/SkinSDR USAA050390Rib · crackedCLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K)Mar 24, 2005 · N442US · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA050378Attach Fitting · damagedCLT - DROP IN FITTING, .020 INCH, ELONGATED. RT PYLON MID BULKHEAD UPPER LINK ATTACH FITTING. REWORKED HOLES IAW EA. (K)Mar 18, 2005 · N611AU · Boeing 7572B7 · Nacelle/Pylon, Attach FittingsSDR USAA050375Skin · crackedCLT - RON - SKIN, 1.75 INCHES, CRACKED, STA 727E, STR 18L. INSTALLED DOUBLER IAW SRM. (K)Mar 16, 2005 · N587US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA050376Frame · crackedCLT - Q6 - FRAME, .125 INCH, CRACKED, STA 787, STR8/9L. INSTALLED DOUBLER IAW TR 53-10-20B. INSTALLED DOUBLER IAW TR. (K)Mar 16, 2005 · N442US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050377Tie Clip · crackedCLT - Q6 - TIE CLIP, SRM 51-10-02, CRACKED, STA 787, STR 24R. REPLACED TIE CLIP. (K)Mar 16, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050427Attach Angle · wornCLT - Q4 - ATTACH ANGLE, (.75 INCH X .50 INCH) WORN, LT HORIZONTAL STABILIZER TIP BL249-81. REPLACED WITH FABRICATED ANGLE IAW SRM. (K)Mar 16, 2005 · N440US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA050364Skin · crackedPIT - RON - SKIN, 4.500 INCH CRACK, STA 727A, 727B, STR 22R. INSTALLED DOUBLER IAW SRM. (K)Mar 15, 2005 · N517AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050362Frame · crackedCLT - Q6 - FRAME, .250 INCH CRACK, STA 867, STR 8/9L. INSTALLED DOUBLER REPAIR IAW TR. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA050361Tie Clip · crackedCLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 10L, BS 685. REPLACED TIE CLIP IAW SRM. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050360Tie Clip · crackedCLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 4R, BS 867. REPLACED TIE CLIP IAW SRM. (K)Mar 15, 2005 · N442US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA050410Skin · crackedCLT - Q6 - FUSELAGE SKIN, (.5 INCH) CRACK., RT WW BEADED PRESSURE DECK STA 664RBL 40. INSTALLED FILLERS AND TRIPLER IAW TR. (K)Mar 12, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050349Skin · crackedCLT - Q6 - SKIN, 2.25 INCH X 7 INCHES. PREVIOUS REPAIR, SCAB PATCH INSTALLED, STATION 178, STRINGER S17R. INSTALLED SPLICE STRAP IAW EO 5300V157. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050350Skin · damagedCLT - Q6 - SKIN, 2.25 INCH X 7 INCH, PREVIOUS REPAIR, SCAB PATCH, STATION 178, STRINGER 17L. SPLICE STRAP INSTALLED IAW EO 5300V157. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA050351Support Fitting · crackedCLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK, MLG AFT SUPPORT FITTING. REPAIRED IAW TR57-40-13. (K)Mar 10, 2005 · N519AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA050354Support Fitting · crackedCLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK. LT WING MLG SUPPORT FITTING. ACCOMPLISHED REPAIR IAW TR 57-40-13. (K)Mar 10, 2005 · N519AU · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR USAA050363Forging · crackedCLT - C5 - FORGING, .3 INCH, CRACKED, FWD SERVICE DOOR CUTOUT UPPER FWD UPPER CORNER. REMOVED CRACKED REVEL AND REPLACED IAW DWG NR 65-55878. (K)Mar 10, 2005 · N527AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050411Rib · crackedCLT - Q6 - RIB, (2 EA- 1.5 INCH AND .3750 INCH) CRACK. LT WING RIB AT WS 505 UPPER FLANGE RADIUS 20 INCHES FROM L/E OF RIB. FABRICATED REPAIR DOUBLER IAW EA. (K)Mar 10, 2005 · N442US · Boeing 7374B7 · Wing, Rib/BulkheadSDR USAA050342Wedge · wornCLT - Q2 - NR 4 SLAT, 2 INCH X 2 INCH, WEAR. NR 4 SLAT T/E WEDGE LOWER SKIN IB. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)Mar 7, 2005 · N519AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050343Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, SEVERAL .250 INCH CRACKS, NR 5 SLAT LOWER SKIN L/E. INSTALLED REPAIR DOUBLER. (K)Mar 7, 2005 · N519AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050344Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, 38 INCH CRACK, NR 5 SLAT LE SKIN. INSTALLED REPAIR DOUBLER IAW SRM. (K)Mar 7, 2005 · N519AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050345Angle · crackedCLT - Q6 - ANGLE, .025 INCH CRACK, STATION 500G-520 BL0. REPLACED WITH FABRICATED PART IAW SRM 51-30-01, DWG NR 69-35365, AND SRM 51-10-02. (K)Mar 7, 2005 · N442US · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA050346Skin · crackedCLT - Q6 - FUSELAGE SKIN, .5 INCH CRACK, LOWER HINGE CUT-OUT FWD SERVICE DOOR. INSTALLED REPAIR DOUBLER IAW TR 52-10-13. (K)Mar 7, 2005 · N519AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050341Stringer Clip · crackedCLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 500A, STRINGER 16R. REPLACED WITH FABRICATED CLIP IAW SRM. (K)Mar 4, 2005 · N442US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA050340Skin · delaminatedCLT - Q2 - NR6 SPOILER, 2 INCH X 6 INCH, DELAMINATION. NR 6 SPOILER TOP SURFACE IB, 6 INCHES FROM T/E. APPLIED COMPOSITE REPAIR IAW SRM. (K)Mar 3, 2005 · N519AU · Boeing 7373B7 · Spoilers
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