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 USAA050114Floorbeam · corrodedPIT - Q6 - FLOORBEAM, .5 INCH X .5 INCH, CORROSION; LEVEL 1; TASK NR C53-107-01; TOP SURFACE OF FLOORBEAM 20 INCH RT OF BL0, BS312; INSTALLED BEAM DOUBLER IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050115Gate · corrodedPIT - Q6 - AFT ENTRY LWR EXHAUST, 1 INCH X 1 INCH AREA (4 PLACES) CORROSION; LEVEL 1; TASK NR C53-107-01; LOWER EXHAUST GATE LOWER IB SURFACE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA050116Web · corrodedPIT - Q6 - SHEAR WEB, 2 INCH X 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 1016, LBL 16 SHEAR WEB; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02 AND MFG DWG. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050117Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 1 INCH DIA AREAS ( 8 EA ); CORROSION; LEVEL 1; TASK NR C53-107-02; FLOOR SUPPORT BS 967-986.5, RBL 17 INCHES. DEFECTIVE PART, REPLACED WITH IDENT PART IAW SRM AND MFG DWG. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050118Sill · corrodedPIT - Q6 - DOOR SILL, 1 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SVC DOOR SILL (AFT) AT NUT PLATE. REPAIRED IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050119Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 16 INCH WIDE SPREAD CORROSION; CORROSION; LEVEL 1; TASK C53-107-01, 02; BS 312 AND 328 BL0 RT 10 INCHES; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050154Floor Support · crackedPIT - Q6 - FLOOR SUPPORT, 1 INCH CRACK; STA 540, BL0.0; REPLACED SUPPORT BRACKET IAW SRM 53-00-51. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050155Skin · crackedPIT - Q6 - SKIN, APPROX 1 INCH CRACK; NR 2 ENG OB WING/LEADING EDGE AT SLAT STA3.25, LWR SKIN PANEL. FABRICATED SKIN FILLER/ DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA050156Skin · crackedPIT - Q6 - NR 1 SLAT, 1 INCH CRACK; LOWER SKIN AFT ROW RIVETS AT NR 2 AUX TRACK. INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050157Door Frame · crackedPIT - Q6 - DOOR EDGE FRAME, .1250 INCH CRACK; FWD SERVICE DOOR, UPPER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Service DoorsSDR USAA050158Door Frame · crackedPIT- Q6 - DOOR EDGE FRAME, .2500 INCH CRACK; FWD SERVICE DOOR, LOWER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Service DoorsSDR USAA050159Intercostal · crackedPIT - Q6 - INTERCOSTAL, NUMEROUS CRACKS, .5 INCH. .7500 INCH, 1.5 INCH; SCREW HOLES UPPER FLANGE OF INTERCOSTAL, BS 380-400. REPAIR ANGLE INSTALLED IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050160Skin · crackedPIT - Q6 - NR 6 SLAT, .5 INCH CRACK; LOWER SKIN AFT ROW RIVET 4 INCHES FROM OB END; INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050165Channel · crackedPIT - Q6 - CHANNEL, .7500 INCH CRACK; ST277, BL0, FWD CABIN FLOOR; DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040894Tie Clip · crackedPIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 500B, STR 13,LT. FABRICATED IAW MFG DWG 69-45156 AND INSTALLED IAW SRM 51-40-02.Dec 15, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA041101Strap · corrodedPIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K)Dec 14, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA041100Support · crackedPIT - Q05 - SUPPORT, .075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM.Dec 8, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA041030Skin · crackedPIT - B CK - SKIN, 3 INCH CRACK, SKIN AT STA 740, STR 18R. INSTALLED DOUBLER IAW SRM.Dec 6, 2004 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA041076Skin · crackedPIT - B-CHECK - SKIN, 3 INCH CRACK, STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. (K)Dec 6, 2004 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA041065Mount · corrodedPIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage, Equipment Attach FittingsSDR USAA041066Mount · corrodedPIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage, Equipment Attach FittingsSDR USAA041067Frame · corrodedPIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG DWG 65C22910. (K)Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA041068Skin · corrodedPIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K)Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA041069Intercostal · crackedPIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K)Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA041071Skin · chafedPIT - Q5 - SKIN, 9 INCHES X .5 INCH X .0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR SCHEME IAW SRM. (K)Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040987Skin · crackedCLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01.Dec 1, 2004 · N590US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA041070Frame · corrodedPIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORROSION, PRIMED AND PAINTED ISW SRM. (K)Dec 1, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA041072Frame · corrodedPIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K)Dec 1, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA041031Spar · damagedPIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB END, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM.Nov 24, 2004 · N514AU · Boeing 7373B7 · AileronsSDR USAA041032Skin Panel · damagedPIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRING MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM.Nov 24, 2004 · N514AU · Boeing 7373B7 · AileronsSDR USAA041033Spar · damagedPIT - Q2 - SPAR, .50 INCH X .25 INCH AREA COMPOSITE DAMAGE/ DELAMINATION. LT AILERON L/E SPAR 26 INCHES FROM OB END UPPER FLANGE. REMOVED DAMAGED AREA AND TAPER SANDED FLANGE, INSTALLED REPAIR PLYS IAW EA, SRM.Nov 24, 2004 · N541AU · Boeing 7373B7 · AileronsSDR USAA041074Floorbeam · corrodedPIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 13 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K)Nov 24, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA040953Support Angle · crackedPIT - Q5 - SUPPORT ANGLE, .1250 INCH CRACK, STA 260 C/L. REPAIRED WITH NEW PART IAW MFG DWG 65-45833. REPAIRED WITH NEW PART IAW MFG DWG 65-45833.Nov 23, 2004 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040951Spoiler · delaminatedPIT - Q5 - SPOILER, 4 BY 6 INCH AREA, DELAMINATION. REMOVED AND REPLACED SPOILER IAW MM 27-62-91.Nov 23, 2004 · N516AU · Boeing 7373B7 · SpoilersSDR USAA041052Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041053Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041054Skin · damagedPIT - Q5 - SKIN SURFACE, 3 INCH LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178 AND 13 INCHES FROM FWD SPAR. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041055Skin · chafedPIT - Q5 - SKIN SURFACE, 1.5 INCH LONG, TAPERING DEPTH, DEEP CHAFE WEAR, RUDDER LOWER RT L/E CORNER. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041056Skin · damagedPIT - Q5 - SKIN SURFACE, SEVERAL AREAS OF 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041060Frame · separatedPIT - Q5 - CONDUCTIVITY FRAME, 15 INCHES X 12 INCHES, SEPARATION, RUDDER TOP LT SURFACE, UPPER LT CONDUCTIVITY FRAME SEPARATING FROM RUDDER. INSTALLED NEW CONDUCTIVITY FRAME IAW MM AND BAC 5010 AND DWG 65C25841.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Spar/RibSDR USAA041061Skin · gougedPIT - Q5 - SKIN SURFACE, 5 INCH LONG GOUGE, RUDDER LT SIDE STA 186, NEAR T/E. INSTALLED REPAIR PLYS IAW SRM.Nov 23, 2004 · N516AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA041073Skin · delaminatedPIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K)Nov 22, 2004 · N518AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040981Stringer · crackedPIT - Q5 - STRINGER, .25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40-09, 51-30-01.Nov 21, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA040939Frame · crackedPIT - Q1 -FRAME, 1 INCH CRACK, RT STA 601 BELOW S17R, FRAME TO FLOORBEAM ATTACH POINT. INSTALLLED REPAIR ANGLE IAW EA 79352.Nov 19, 2004 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA040970Fitting · crackedPIT - Q1 - FITTING, .25 INC CRACK, RT MLG SUPPORT FITTING, NR 2 HOLE; MODIFIED PART INSTALLED, REPLACED IAW EO 5702V054.Nov 18, 2004 · N435US · Boeing 7374B7 · Wing, Landing Gear Attach FittingsSDR USAA040978Skin · bulgedPIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537.Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040979Skin · crackedPIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537.Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040977Skin · crackedPIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Nov 17, 2004 · N518AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA040974Failsafe · crackedPIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1.Nov 16, 2004 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040975Skin · corrodedPIT - Q6 - WING SKIN CUTOUT, .5 INCH X .75 INCH AT (4) LOCATIONS, CORROSION; NO LEVEL OR TASK; LT WING 7403L PANEL FUEL BOOST PUMP ACCESS AREA. REMOVED CORROSION AND REPAIRED IAW DRAFT EA 79514.Nov 16, 2004 · N516AU · Boeing 7373B7 · Wing, Plate/Skin
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