N527AU, cancelled Mar 30, 2011

Service difficulty reports · 82

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 = 'N527AU' AND deregistration_id = 'N527AU-2011-03-30'
  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 USAA2008123092338Skin · crackedCLT - MAJOR REPAIR - RON - NR 6095204, CRACKED FUSELAGE SKIN AT BS 727E, S24L. REPAIRED FUSELAGE SKIN AT BS 727E, S24L IAW B737 SRM 53-00-01-2R-31.Dec 30, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA2008121692235Skin · crackedCLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, LBL 24. REPAIRED FUSELAGE SKIN AT BS 727D, LBL 24 IAW B737 SRM 53-00-01 REPAIR 31.Dec 15, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA920080906Charger · failedMX CHECK - PHL - RIGHT HAND MIDDLE EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD.Apr 21, 2008 · N527AU · Boeing 7373B7 · Emergency LightingSDR USAA920080196Skin · corrodedCLT - MAJOR REPAIR - RON - CORROSION ON FUSELAGE SKIN, BS 986, S27L - S27R. REPAIRED FUSELAGE SKIN, BS S27L - S27R IAW USAIRWAYS EA 1000160.Jan 18, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA920080195Shear Tie · corrodedCLT - MAJOR REPAIR - RON - CORROSION ON SHEAR TIE, BS 986, S27L - S27R. REPAIRED SHEAR TIE, BS S27L - S27R IAW B737 SRM 53-00-07.Jan 18, 2008 · N527AU · Boeing 7373B7 · Fuselage Internal Mounting StructureSDR SB07059Circuit Card · unknownPHL FLT1407 - AFTER TAKEOFF FROM PHL, CREW RECEIVED BOTH MAIN LANDING GEAR RED UNSAFE LIGHTS AFTER RAISING GEAR AND RETURNING GEAR LEVER TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES, CONSULTED MAINTENANCE AND RETURNED TO FIELD AT PHLAug 3, 2007 · N527AU · Boeing 7373B7 · Landing Gear Position and WarningSDR SB07040Slide · no testPHL - THE FORWARD RIGHT HAND SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED THE ANNUAL OPERATIONAL TEST WHEN IT TWISTED DURING DEPLOYMENT. MAINTENANCE REPLACED THE SLIDE. INSPECTED OK FOR SERVICE.May 18, 2007 · N527AU · Boeing 7373B7 · Escape SlideSDR USAA200609003Skin · crackedFOUND 1.8750 INCH LONG CRACK IN SKIN AT STA 727 LONGERON 22L. CUT OUT CRACKED AREA/HFEC/INSTALLED DOUBLER IAW SRM 53-00-01.Sep 17, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA060580Structure · puncturedOUTBOARD OF NR 5 SPOILER PUNCTURED. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCH.Apr 10, 2006 · N527AU · Boeing 7373B7 · SpoilersSDR USAA060448Skin · puncturedNR 6 SPOILER TOP CENTER OF SPOILER PANEL PUNCTURE. MAJOR REPAIR, IAW TR 27-60-01, DEFECT SIZE: 1 INCH.Mar 10, 2006 · N527AU · Boeing 7373B7 · SpoilersSDR USAA060446Skin · puncturedOUTBOARD OF NR 5 SPOILER PUNCTURE. REMOVED DAMAGE INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCHES.Mar 10, 2006 · N527AU · Boeing 7373B7 · SpoilersSDR USAA060445Skin · delaminatedSTA WBL 170-160 AND 181 UPPER FIXED WING T/E DELAMINATED. REMOVED DAMAGE AND APPLIED A COMPOSITE REPAIR IAW EA 78270, DEFECT SIZE: 3 INCHES.Mar 9, 2006 · N527AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA060409Repair · unknownRIGHT ELEVATOR LOWER SURFACE 9 INCHES I/B OF O/B END AND 16 INCHES AFT OF FRONT SPAR. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 2.5 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/StructuresSDR USAA060410Repair · unknownRIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF RIGHT. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/StructuresSDR USAA060411Repair · unknownRIGHT ELEVATOR, LOWER SURFACE 30 INCHES O/B OF I/B END AND 12 INCHES AFT OF RIGHT DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/StructuresSDR USAA060412Repair · unknownRIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF FRONT SPAR DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7 · Empennage StructureSDR USAA060407Rib · crackedIN SPAR LOWER AFT SUPPORT RIB 135.5 CRACKED. REPAIRED IAW 97467, DEFECT SIZE: 1.250 INCH.Mar 3, 2006 · N527AU · Boeing 7373B7 · Wing, Rib/BulkheadSDR USAA060388Door Frame · crackedFOUND AFT CARGO DOOR/AFT FRAME CRACKED STA 847 STR 24R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13, DEFECT SIZE: 1".Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA060390Fitting · crackedFOUND CRACK RIGHT MAIN LANDING GEAR SUPPORT FITTING AT HOLE B/2. INSTALLED REPAIR PER TR 57-40-13 REV A, DEFECT SIZE: .125".Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR USAA060380Frame · crackedFOUND FRAME CRACKED BS 787 BETWEEN S-8R AND S9-R AT OVERHEAD BIN ATTACH POINT. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE: .125".Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060389Angle · corrodedFOUND CORROSION ON TRANSITION ANGLE STA 767-790 AT NUT PLATES. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE: .250".Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060371Frame · crackedFOUND CRACK BS 380 BETWEEN S-8R AND S-9R AT OVERHEAD BIN LOWER ATTACH. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE: .125 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060382Frame · crackedFOUND FRAME CRACKED LT BODY STA 480. REMOVED AND REPLACED PSU BRACKET WITH FABRICATED PARTS IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060383Bracket · crackedFOUND CRACKED PSU RAIL BRACKET AT RT BODY STA 480. REMOVED AND REPLACED PSU RAIL BRACKET WITH FABRICATED IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA060384Frame · crackedFOUND CRACK AT FRAME STA 827 BETWEEN S8L. FABRICATED FRAME REPAIR ANGLES AND INSTALLED PER T/R 53-10-20C, DEFECT SIZE: .125 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060385Frame · crackedFOUND CRACK STA 807 BETWEEN S8L-9L AT OVERHEAD BIN LOWER ATTACH POINT. REMOVED AND REPLACED FRAME SUPPORT BRACKETS IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060386Intercostal · crackedAD 2005-20-03 INSP/REPAIR OF INTERCOSTALS FOUND CRACK COMMON TO MAIN ENTRY DOOR. REMOVED AND REPLACED CRACKED INTERCOSTAL WEB AND STRAP WITH FABRICATED PARTS IAW SRM 53-10-04 REPAIR DEFECT SIZE: .25.Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060356Clip · crackedFWD SIDE OF BS 294.5 AND STR 11L. REMOVED CRACKED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW BOEING DWG 69-62054, DEFECT SIZE: .50 INCH.Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060357Splice · crackedBS 907 AND STR 4R CRACKED. REMOVED OLD SPLICE AND DRILLED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02, DEFECT SIZE: .50 INCH.Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060358Bracket · crackedAFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS BOEING DWG 69-42159, DEFECT SIZE: .50 INCH.Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060353Floorbeam · corrodedBS 312 FLOORBEAM CORRODED FROM RBL 8 TO RBL 36. MAJOR REPAIR SRM 53-10-51 FIG 201, REPAIR 5, DEFECT SIZE: .25 INCH.Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA060329Bracket · crackedAFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING DWG 69-42159, DEFECT SIZE: .25 INCH.Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060332Channel · crackedSTRINGER 15L AND BS 360 CRACKED. REMOVED AND REPLACED WITH NEW EXTENSION CHANNEL IAW DGW 65-61777, DEFECT SIZE: .25 INCH.Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060331Angle · crackedBS 360 S-14 LT. REMOVED AND REPLACED WITH NEW ANGLE IAW DWG 65-4566 AND SRM 51-10-02, DEFECT SIZE: .25 INCH.Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060330Angle · crackedAT 13L AND BS 360 CRACKED. REMOVED CRACKED ANGLE, REPLACED WITH NEW ANGLE IAW DWG 69-48204 AND SRM 51-10-02, DEFECT SIZE: .25 INCH.Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060314Tie Clip · crackedFOUND CRACK BS 343 AT STRINGER 11R. REMOVED FABRICATED AND INSTALLED TIE CLIP IAW BOEING DWG 69-38939-5 AND SRM 51-10-02, DEFECT SIZE: .025".Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060328Angle · corrodedFOUND Z-ANGLE CORRODED STA 967-987 AT STR 17L. INSTALLED NEW Z ANGLE PER SRM 51-10-02, DEFECT SIZE: 2" BY 20".Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060322Frame · crackedFOUND FRAME CRACKED STA 847 BETWEEN S8R AND 9R. REPAIRED PER 53-10-20C DEFECT SIZE: .25".Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA060321Angle · crackedFOUND ANGLE CRACKED INSIDE OF FRAME, 294.5 R AT S17R. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: .25".Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060281Pan · corrodedLEFT PAN STA 987 LBL 37 CORROSION AT NUT PLATE. BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 1"X1.5"Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060287Skin · corrodedNR 2 VHF ANTENNA. REMOVE CORROSION , TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA060284Skin · corrodedNR 1 VHF ANTENNA. REMOVED CORROSION TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA060280Angle · corrodedSTA 984 AND STA967. REMOVED LIGHT CORROSION LESS THEN .002 IAW SRM 51-10-02. DEFECT SIZE: .002"Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060278Floorbeam · corrodedSTA 957 RBL 18 TO RBL 44. REMOVED SURFACE CORROSION IAW SRM 51-10-02. DEFECT SIZE:Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA060277Floorbeam · corrodedSTA 967 LBL28 TO LBL44. REMOVED LIGHT CORROSION LESS THEN .002 IAW SRM 53-60-51. DEFECT SIZE: .002Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA060274Web · crackedBS 294.5 AND S12L WEB IS CRACKED. CUT OUT DAMAGED WEB, HFEC, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02. DEFECT SIZE: 1 INCHFeb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA060273Skin · crackedLOWER SURFACE OF NR 6 SLAT, INBOARD END AT STOP PADS. REMOVED AFFECTED RIVETS, CUT OUT DAMAGE FABRICATED REPAIR PANEL AND INSTALLED IAW SRM 57-43-01 R-6. DEFECT SIZE: .250 INCHFeb 16, 2006 · N527AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA060283Floorbeam · corrodedT-CAP 967 CORROSION AT RBL 5 AND RBL 28. REPAIRED AND BLENDED LIGHT CORROSION IAW SRM 53-60-51. DEFECT SIZE: .002"Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA060255Floorbeam · corrodedSTA 98.7 RBL 2 TO RBL 36 CORROSION. REMOVED CORROSION IAW SRM 53-60-51, DEFECT SIZE: .002.Feb 15, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA060253Web · crackedBS 294.5 AND S16L CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-02, DEFECT SIZE: .500 INCH.Feb 15, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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