N526AU, cancelled Aug 25, 2008

Service difficulty reports · 86

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 = 'N526AU' AND deregistration_id = 'N526AU-2008-08-25'
  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 USAA920081310Battery · dischargedMCN - B01 - EEL - SEVERAL EMERGENCY LIGHTS OUT IN CABIN. REPLACED CENTER EMERGENCY BATTERY IAW B737 AMM 33-51-51-2. (S)Jul 2, 2008 · N526AU · Boeing 7373B7 · Emergency LightingSDR USAA920080651Skin · crackedCLT - MAJOR REPAIR - C6 CHECK - CRACKED FUSELAGE SKIN BS 727E, S22L. REPAIRED FUSELAGE SKIN, BS 727E. S22L IAW B737 SRM 53-00-01.Mar 20, 2008 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA920080652Flap · delaminatedCLT - MAJOR REPAIR - C6 CHECK - RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP IAW B737 SRM 27-51-39.Mar 16, 2008 · N526AU · Boeing 7373B7 · Trailing Edge FlapsSDR SB07084Light · noneDFW - MAINTENANCE REPORTED THE FLOOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 9 AND 11, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE FOUND THAT THIS IS A NORMAL SITUATION. THESE LIGHTS ARE NOT OPERATIONAL PER MM 33-51-12-0, SECTION 3, PARAGRAPH A, SENTENCE 4.Sep 28, 2007 · N526AU · Boeing 7373B7 · Light System WiringSDR USAA070260Skin · crackedSEVERAL .125 INCH CRACKS, NR 2 SLAT LOWER TRAILING EDGE SKIN BETWEEN HET TUBE & INBOARD AUX TRACK HAS CRACK. CUT OUT DAMAGE & INSTALLED DOUBLER PER SRM 57-43-01, DEFECT SIZE: .125 INCH.Apr 4, 2007 · N526AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA200701004Tie Clip · crackedA 1 INCH CRACK FOUND AT STA 294.5, STR 11, CLIP. REMOVED & REPLACED CRACKED TIE CLIP PER EO 5305V203 (DROP-IN A/C).Jan 19, 2007 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB06102Windshield · crackedPHL FLT1428 - EN ROUTE FROM RDU TO PHL, CREW REPORTED THE CAPTAINS'S NR 1 WINDOW OUTER PANE CRACKED. OBSERVED ARCING FROM THE UPPER RIGHT SIDE, THEN CRACKING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD Oct 19, 2006 · N526AU · Boeing 7373B7 · Flight Compartment WindowsSDR USAA060591Skin · crackedFOUND SKIN CRACKED, BS 328 S17R. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER IAW SRM 53-10-01 REP 2, DEFECT SIZE: .75".Apr 18, 2006 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050880Flange · wornCLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)Jul 14, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA050838Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050839Beam · crackedCLT - FOUND BEAM CRACKED 1.25 INCH, AFT OF RIGHT AILERON AT TRAILING EDGE. INSTALLED A NEW BEAM IAW SRM 57-51-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · AileronsSDR USAA050840Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED, TRANSITION ANGLE IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, INSTALLED TRANSITION ANGLE IAW SRM 51-10-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050841Floorbeam · corrodedCLT - FOUND FLOORBEAM TEE CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05, SRM 53-00-51. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050842Intercostal · crackedCLT - FOUND INTERCOSTAL SUPPORT CRACKED 1.4 INCHES, FS 295 AT STRINGER S16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15M SRM 51-10-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050843Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050844Angle · corrodedFOUND CHORD ANGLE CORRODED .8 INCHES, LOWER CHORD ANGLE AT BS 227.8. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 96645 AND BOEING DWG 69-38740. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050845Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 6 INCHES, AFT OF FORWARD E/E DOOR AT BL 0, BS 219.8 TO 227.8. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED NEW PART IAW EA 96645 AND BOEING DWG 69-38740. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050846Skin · delaminatedCLT - FOUND ELEVATOR TOP SKIN CRACKED 3 INCHES TOP SURFACE. MAJOR, COMPOSITE REPAIR IAW EA 96681. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Elevator, Plate/SkinSDR USAA050832Stringer · corrodedCLT - FOUND STRINGER CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACED OUT OF LIMITS STRINGER SECTIONS IAW SRM 53-60-53 AND TR 53-10-06B. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050833Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050834Web · corrodedCLT - FOUND WEB CORRODED 10 INCHES, UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050835Stringer · corrodedCLT - FOUND STRINGERS CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACE OUT OF LIMITS STRINGER SECTION IAW SRM 53-60-53 AND TR 53-10-06B. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050823Skin · dentedPIT - FOUND SKIN DENTED 2 INCHES BY 2 INCHES, DENT ONE BS 500-500A, S20R-S21R, DENT 2 AND 3 AT BS 500A-500B S19R-S20R. CUT OUT THREE DENTS, FABRICATED TRIPLERS, SIZE OF REPAIR IS 44.5 INCH BY 23 AT 10.22 LBS IAW SRM 53-00-01. (M)Jul 1, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050819Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND AND STATION 827. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-02. (M)Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050820Web · corrodedCLT - FOUND WEB CORRODED 10 INCHES, WEB UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR 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 USAA050811Bracket · wornCLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Wing, Attach FittingsSDR USAA050810Skate Angle · wornCLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach FittingsSDR USAA050809Angle · corrodedCLT - Q2 - L-ANGLE, 6 INCH FRETTING, L-ANGLE AT BS 1016 FORWARD OF THE RT FWD VERTICAL FIN MOUNT. FABRICATED AND REPLACED NEW L ANGLE. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050808Angle · crackedCLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050807Floor Support · crackedCLT - Q2 - FLOOR SUPPORT, 1 INCH CRACK, FLOOR SUPPORT AT STA 500D IN A/C DISTRIBUTION BAY. REMOVED DAMAGED WEB, FABRICATED NEW WEB IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050806Intercostal · dentedCLT - Q2 - INTERCOSTAL, 2 INCHES X 1 INCH, DENT, STR 25L BETWEEN FRAMES 440 AND 420. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050805Mount · corrodedCLT - Q2 - LAV MOUNT, 1 INCH X 3 INCHES, CORROSION, LT AFT LAV OB MOUNT. FABRICATED AND INSTALLED NEW MOUNT IAW WITH DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050804Threshold · corrodedCLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050803Stringer · corrodedCLT - Q2 - CARGO FLOOR STRINGER, 6 INCH, CORROSION, AFT CARGO FLOOR STRINGERS AT STA 736 FROM LBBL 17.2 TO RBBL 13.8. REMOVED AND TREATED CORROSION IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050781Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED, .4 INCH AND .3 INCH, STATION 908, S4L. REMOVED OLD STRINGER SPLICE, INSTALL NEW SPLICE IAW SRM 53-00-01 FIG 229. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050780Channel · wornCLT - FOUND L-CHANNEL FRETTING WEAR .5 INCH BY 3 INCHES, FORWARD OF THE LEFT FORWARD VERTICAL FIN MOUNT AT BS 1016 NR 2412. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-20-05. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach FittingsSDR USAA050779Tear Strap · debondedCLT - FOUND TEAR STRAP DISBOND 15 INCHES, BS 867-887, S17-19 RT. INSTALLED RIVETS THROUGH SKIN AND STRAPS AS REQUIRED IAW SRM 53-00-01 FIG 225. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050778Tear Strap · debondedCLT - FOUND TEAR STRAP DISBOND 8 INCHES, BS 857, S16R-S17R. INSTALLED RIVETS TO SECURE IAW SRM 53-00-01, FIG 225 DET 3. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050777Tear Strap · debondedCLT - FOUND DEBONDED TEAR STRAP 11 INCHES, BS 877, S16R-17R. ADDED RIVETS IAW SRM 53-00-01 FIG 225 DET 3. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050775Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 STRINGER 9L. CUT OUT CRACK, INSTALLED NEW REPAIR ANGLES IAW 53-10-20B. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050774Floorbeam · corrodedFOUND FLOORBEAM CORRODED 3 INCHES, BS 967, LBL 43. FABRICATED NEW T-CAP FOR FLOORBEAM PER SRM 53-00-51, SAME AS PREVIOUS REPAIR. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050773Skin · gougedCLT - FOUND SKIN GOUGED .125 INCH BY 1 INCH BY .060 INCH, LEADING EDGE RADIUS OF LEFT FOR FLAP .22 INCH FROM INBOARD END. REMOVED DAMAGED AREA, 2.5 INCH BY 1 INCH, INSTALLED EXTERNAL DOUBLER 7.5 INCH BY 6 INCHES IAW SRM 57-53-01 FIG 201. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA050772Angle · corrodedCLT - FOUND TRANSITIONAL ANGLE CORRODED 2 SQUARE INCHES, UNDERSIDE OF NUTPLATE OF RIGHT TRANSITION ANGLE AT DOOR FRAME BS 496. REMOVED DAMAGE, FABRICATED REPAIR AND REPLACEMENT PART INSTALLED IAW 737 SRM 51-10-02. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050771Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 3 INCHES, RT TRANSITION ANGLE AT BS 492.4. REMOVED DAMAGED PART. FABRICATED AND INSTALLED NEW PART IAW 737 SRM 51-10-02. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050770Support Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED 1 INCH, LOWER EDGE OF INTERCOSTAL AT FORWARD SIDE OF STATION 328, RBL 32. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT PART, AND INSTALLED. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050769Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05 AND SRM 53-00-51. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050749Angle · crackedCLT - FOUND L-ANGLE CRACKED 4 INCHES, RT SIDE STATION 291.5-295.5 AT FLOOR LEVEL. REMOVED DAMAGED. FABRICATED AND INSTALLED REPAIR PART IAW BOEING DWG 69-37402. (M)Jun 9, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050742Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, NR 2 PYLON LEADING EDGE SKIN. TRIMMED OUT DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER. (M)Jun 8, 2005 · N526AU · Boeing 7373B7 · Nacelle/Pylon, Bulkhead/FirewallSDR USAA050743Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 480 STRINGER 15R. REPLACED TIE CLIP IAW SRM 51-10-02. (M)Jun 8, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
Back to N526AU, cancelled Aug 25, 2008