N560AU, cancelled Mar 8, 2007

Service difficulty reports · 70

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N560AU' AND deregistration_id = 'N560AU-2007-03-08'
  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 USAA050589Stiffener · crackedCLT - FOUND STIFFENER CRACKED .4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M)May 3, 2005 · N560AU · Boeing 737301 · Nacelle/Pylon Miscellaneous StructureSDR USAASB04010Charger · inoperativePHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Jan 21, 2004 · N560AU · Boeing 737301 · Emergency LightingSDR USAASB03221Fuse · inoperativeDCA- MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS ON SEAT ROWS 6, 7, 8, 9 AND 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE IN POWER SUPPLY ABOVE SEAT ROW 10 CEILING. OPERAITONAL CHECK GOOD. (M)Dec 24, 2003 · N560AU · Boeing 737301 · Emergency LightingSDR USAA030194Skin · crackedFOUND SKIN CRACKED 2.250 INCH, JUST BELOW S23R AT FS 730. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)Sep 10, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030193Skin · crackedFOUND SKIN CRACKED .750 INCH, FUSELAGE JUST ABOVE S24R FORWARD OF FS 727E. INSTALLED DOUBLR/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)Sep 10, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030187Skin · crackedCLT - FOUND SKIN CRACKED 2.5 INCHES, FUSELAGE SKIN JUST BELOW S19R AT FS 760. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Sep 8, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030117Skin · damagedPIT - FOUND RUDDER WITH SKIN DAMAGE, 24 INCH OVAL ONE LAYER DAMAGE, LEFT SIDE OF RUDDER 107 INCH FROM BOTTOM 12 INCHES FROM TRAILING EDGE. WET LAY UP REPAIR PER SRM 51-70-17 AND EA 76292. (M)Jul 17, 2003 · N560AU · Boeing 737301 · Rudder, Plate/SkinSDR USAA030119Floorbeam · crackedPIT - FOUND FLOORBEAM CRACKED APPROX 1 INCH, BS 328 RBL 10.0. DOUBLER INSTALLED PER EA 76205. (M)Jul 17, 2003 · N560AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA030118Angle · crackedPIT - FOUND ANGLE HAS .375 INCH CRACK, NR 5 LE SLAT ACTUATOR ATTACH FITTING ANGLE. FABRICATED REPAIR ANGLE FROM 17-7 PH PER EA 76202. (M)Jul 11, 2003 · N560AU · Boeing 737301 · Wing Miscellaneous StructureSDR USAA030116Support Fitting · crackedPIT - FOUND MLG BEAM AFT SUPPORT FITTING HAS APPROX .5 INCH CRACK, UPPER OUTBOARD HOLD ON MLG BEAM AFT SUPPORT FITTING, RSS 224.14. OVERSIZED HOLE AND INSTALLED STRAP ACROSS UPPER REAR SPAR CHORD PER EA 76210. (M)Jul 8, 2003 · N560AU · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA030089Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED APPROX 6 INCHES BY 1 INCH, FLOORBEAM BETWEEN STATION 344 AND 360 10 INCHES LBBL. MANUFACTURED AND INSTALLED T-CAP PER EA 76223 SRM CHAPTER 51. (M)May 22, 2003 · N560AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA030060Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .1875 INCH, BELTFRAME CRACKED AT STATION 303.9 STRINGER 13L. DOUBLER INSTALLED PER EA 76233. (M)May 22, 2003 · N560AU · Boeing 737301 · Fuselage Main, StructureSDR USAA030079Angle · crackedPIT - FOUND RUDDER CRACKED .5 INCH, RUDDER LOWER FORWARD SEAL PLATE ANGLE. INSTALLED WET LAYUP REPAIR PER EA 76293, SRM 51-70-17 AND 51-60-00. (M)May 22, 2003 · N560AU · Boeing 737301 · Rudder StructureSDR USAA030050Skin · corrodedFOUND SKIN CORRODED 1 INCH AREA AND .5 INCH AREA, AROUND FASTENER, BL 0 STATION 1016 RADIAL STIFFENER. CORROSION LEVEL 1. REMOVED DAMAGED END OF STIFFENER, INSTALLED NEW SECTION AND SPLICE PER BOEING DRAWING 65C28106. (M)May 6, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030083Bear Strap · crackedFOUND BEAR STRAP CRACKED .1875 INCH, MED BEAR STRAP BS 304 UPPER AND LOEWR HINGE CUTOUT. INSTALLED DOUBLERS PER EA 76233. (M)May 5, 2003 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030147Nut Plate · corrodedPIT - FOUND NUTPLATE CORRODED .75 INCH BY 1 INCH AREA, FS 727A-727B 21 LT. INSTALLED DOUBLER PER SRM 53-00-3. CORROSION LEVEL 1, TASK NR C53-107-01. (M)May 1, 2003 · N560AU · Boeing 737301 · FastenersSDR USAA030096Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .75 INCH LONG, AT RIVET FOR LOWER OVERHEAD BIN, BETWEEN S8L AND S9L, FS 440. PER TYPICAL REPAIR PER 53-10-20A. (M)Apr 30, 2003 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA030082Frame · crackedPIT - FOUND FRAME CRACKED .1875 INCH, SMALL CRACK IN FRAME AT RIVET STATION 360 LEFT, BETWEEN 58-59. REMOVED DAMAGED AND INSTALLED DOUBLERS PER TR 53-10-20A. (M)Apr 27, 2003 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA030059Fitting · crackedFOUND FITTING CRACKED 1.5 INCHES LONG, FITTING IN HORIZONTAL STABILIZER CENTER SECTION OF RIGHT THRUST BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Apr 25, 2003 · N560AU · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA020177Skin · crackedPIT - FOUND SKIN AND WEB PLATE CRACKED .625 INCH, BS 360-380, AT BL 10. SKIN DOUBLER ADDED PER TYPICAL REPAIR 53-30-07 AND EA 73800. (M)Apr 16, 2002 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01346Light · inoperativeCLT - PILOT REPORTED THE FLOOR PATH EMERGENCY LIGHTING, AT SEAT ROW 13C, IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 13C. OPERATIONAL CHECK GOOD. (M)Dec 20, 2001 · N560AU · Boeing 737301 · Emergency LightingSDR USAASB99278Indicator · failedCLT - FLT 2202 - DURING CLIMB-OUT FROM CLT, THE FLAPS FAILED TO RETRACT AS FLAP INDICATOR FAILED AT 5 DEGREES FLAPS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP PONov 25, 1999 · N560AU · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAA991218Antenna Base · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 12 INCH AREA OF CORROSION BETWEEN STRINGER 28 LT AND RT AFT OF STATION 500 ANTENNA BASE, CORROSION LEVEL 2. REPLACED ANTENNA BASE PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991215Shear Tie · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 420 STRINGER 4 LEFT SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-2. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991214Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500 RIGHT STRINGER 15 SHEAR TIE DAMAGE AT STRINGER AND FRAME. REMOVED AND REPLACED PER SRM 51-10-2. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991213Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 2 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991212Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 3 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991211Skin · crackedCLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER PER EA 65982 AND TR 54-50-04D. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA991210Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 10 INCH AREA OF CORROSION AT AFT ENTRY DOOR FLOOR Z-ANGLE, CORROSION LEVEL 1. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA991208T-Cap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TEN 1 INCH BY 1 INCH AREAS OF CORROSION ON UPPER CAP OF T-CAP STATION 967, CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-05. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991207Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT AFT ENTRY DOOR Z-ANGLE (CHANNEL), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED AFT ENTRY DOOR Z-ANGLE PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA991206Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FLOOR), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Service DoorsSDR USAA991205Seat Track · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 727B-947 SEAT TRACK, CORROSION LEVEL 2. INSTALLED SEAT TRACK PER SRM 53-00-52. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA991204Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH MULTIPLE AREA OF CORROSION AT BS 986.5, RBL 44 - LBL 45, FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED FLOORBEAM T-CAP PER TR 53-60-01 AND SRM 53-00-51 FIG 202. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991198Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 908 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991197Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND SRM 53-00-07. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991196Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991195Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 827 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991194Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.2 5INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991193Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991192Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991191Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727 STRINGER 14L OUTER CHORD ANGLE. REPAIRED DOUBLER AND TRIPLER PER EA 65952. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991190Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK IN FUSE FRAME AT FASTENER HOLE BS 480 BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991189Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACKS IN 2 PLACES STATION 178 WEB A AND WEB B, LBL 1 AND RBL 1 SKIN. INSTALLED DOUBLER PER SRM 53-10-08. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991188Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS AT BS 663, LBL 32 CEILING PRESSURE DECK. INSTALLED DOUBLER PER TR 53-60-04 AND SRM 53-60-51. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991187Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RIGHT HORIZONTAL STABILIZER LOWER SURFACE STATION 111-166 SKIN. INSTALLED DOUBLER AND FILLER PER SRM 55-10-01 AND TR 55-10-07A. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991186Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK THROUGH RIVET HOLE BS 847, STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991185Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .250 INCH CRACK AT BS 727B STRINGER 4L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991184Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 807 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991183Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 887 STRINGER 91 BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)Nov 11, 1999 · N560AU · Boeing 737301 · Fuselage Main, Frame
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