N514AU, cancelled Jul 2, 2008
Service difficulty reports · 87
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 = 'N514AU' AND deregistration_id = 'N514AU-2008-07-02' 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.
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 = 'N514AU' AND deregistration_id = 'N514AU-2008-07-02' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2008FA0000435Cylinder · crackedAFTER AIRCRAFT TOW, FLUID WAS OBSERVED LEAKING FROM .5 INCH CRACK (APPROXIMATE) IN THE OUTER CYLINDER OF THE LT MLG SHOCK STRUT. THE CRACK IS LOCATED APPROXIMATELY 26 INCHES BELOW THE SHOCK STRUT AIR VALVE. (K)SDR USAA920081115Stringer · crackedMCN - MAJOR REPAIR - B1 CHECK - CRACKED STRINGER, BS 927, S22L. REPAIRED STRINGER, BS 927, S22L IAW B737 SRM 53-00-03 FIGURE 201.SDR USAA920081163Frame · crackedMCN - MAJOR REPAIR - LEASE RETURN - CRACKED FRAME, BS 492, S24R. REPLACED FRAME, BS 492, S24R IAW B737 SRM 51-40-02.SDR USAA920070832Web · crackedCLT - MAJOR REPAIR - NR 6007491, CRACKED WEB, BS 294.5, S7L. REPLACED WEB, BS 294.5, S7L IAW B737-300 SRM 51-40-02.SDR USAA920070831Tie Clip · crackedCLT - MAJOR REPAIR - NR 6007482, CRACKED FRAME TIE CLIP, BS 360, S14L - S15L. REPLACED FRAME TIE CLIP, BS 360, S14L - S15L IAW B737-300 SRM 51-40-02.SDR USAA920070830Fitting · crackedCLT - MAJOR REPAIR - NR 6007479, CRACKED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L. REPLACED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L IAW B737-300 SRM 51-40-02.SDR USAA920070829Door Frame · crackedCLT - MAJOR REPAIR - NR 6007659, CRACKED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02.SDR USAA920070828Door Frame · crackedCLT - MAJOR REPAIR - NR 6007658, CRACKED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02.SDR USAA070580Beam · crackedSTA 259.5 AT NOSE W/W CEILING WL 192.5, BL 0, RADIUS OF NOSE GEAR ACT BEAM. REPLACED GUSSET PER SRM 51-10-02, DEFECT SIZE: .75 INCH.SDR USAA061396Frame · crackedSTA 492.4 S24R CRACKED. REPAIRED IAW SRM 53-30-15 EA 98295, DEFECT SIZE: .50 INCH.SDR SB06097Switch · shortedCLT - FLT1770 EN ROUTE FROM MYR TO CLT, CREW REPORTED THAT BOTH THE CAPTAIN'S AND FIRST OFFICER'S FIRE WARNING LIGHTS FLASH CONSTANTLY DURING FLIGHT AND WHILE TAXING AFTER LANDING. SEEMS TO BE ASSOCIATED WITH TURBULENCE IN FLIGHT AND BUMPS ON THE TAXIWAYS ANSDR USAA050063Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M)SDR USAA050218ASkin · crackedCLT - FOUND SKIN CRACKED 1.375 INCH, FS 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR 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.SDR 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.SDR USAA040701Floor Support · bentSUPPORT, .2500 INCH X 20 INCH AREA, BENT/LIFTING METAL, BS540 BETWEEN IB AND OB SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-2.SDR USAA040655Doubler · crackedPIT - FOUND DOUBLER AND SKIN CRACKED .75 INCH LONG, OPENING FOR ACCESS PANEL 5727L, LEFT PYLON NACELLE STATION 180 OUTBOARD SIDE. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M)SDR USAA040653Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .125 INCH, IN FRAME AT FS 767 LOWER OVERHEAD BIN ATTACH POINT, RIGHT SIDE. INSTALLED REPAIR ANGLES 1 AND 2 PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA040652Window Frame · crackedPIT - FOUND WINDOW FRAME CRACKED .25 INCH, UPPER OUTBOARD CORNER OF CAPTAIN WINDOW FRAME. REMOVED DAMAGE, DOUBLER INSTALLED PER SRM 53-10-01. (M)SDR USAA040706Fitting · corrodedPIT - Q2, R-1 LUG .1250 BY .2500 INCH AREA, CORROSION; NO LEVEL OR TASK, RT HORIZ STAB R-1 LUG. CLEANED CORROSION, REMOVED AND REPLACED BUSHING, CAB PLATED IAW SRM 55-10-10, NDTM 0-4-53-10.SDR USAA040705Floor Support · corrodedPIT,Q2, FLOOR SUPPORT .1250 INCH X .2500 INCH AREA, CORROSION, LEVEL 1; TASK NR C53-107-02. FLOOR SUPPORT, BETWEEN STA 312 AND 344, APPROX. 10 INCHES LT OF CENTER. CLEANED, TREATED, PRIMED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-06B.SDR USAA040677Anchor Fitting · corrodedANCHOR FITTINGS; CORROSION; LEVEL 1; TASK NR C53-107-02, ANCHOR FITTINGS AT STA 993R. REPLACED FITTINGS IAW SRM 51-10-2.SDR USAA040657Floor Support · crackedPIT - FOUND FLOOR SUPPORT HAS TWO CRACKS .25 INCH, NR 6 SLAT BOARD, 1 AT 4 INCH AND 1 AT 5 INCH OUTBOARD OF DEICING TUBE, 1 AT 5 INCH. CLEANED, TREATED AND PRIMED, REPLACED FLOOR SUPPORT. (M)SDR USAA040654Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED 1 INCH LONG, BS 538, STRINGER 22, PACK RAM AIR INLET AREA. FABRICATED AND INSTALLED REPAIR ANGLES PER TR 53-50-03. (M)SDR USAA040635Rib · crackedPIT - FOUND RIB CRACKED .5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M)SDR USAA040645Keelbeam · wornPIT - FOUND KEEL BEAM .1875 INCH DIAMETER METAL WEAR AROUND FASTENER HOLES, L/N KEEL BEAM LOWER FLANGE BETWEEN BS 704-727. DOUBLER STRAP INSTALLED PER EA 79006. (M)SDR USAA040644Keelbeam · wornPIT - FOUND KEEL BEAM WITH DEEP METAL WEAR .1875 INCH AT FASTENER HOLES, KEEL BEAM LOEWR FLANGE BETWEEN BS 727-704. INSTALLED STRAP DOUBLER PER EA 79007. (M)SDR USAA040658Spar · crackedPIT - FOUND UPPER CHORD CRACKED MORE THAN .343, BUT LESS THAN .6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14. OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M)SDR USAA040656Fitting · crackedPIT - FOUND FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING NR 2 HOLE 5:30 POSITION. REPLACED RT MLG SUPPORT FITTING AND INSTALLED UPPER WING CHORD DOUBLER PER EO 5702V054, EA 78985 AND 78986. (M)SDR USAA040647Web · corrodedPIT - FOUND WEB CORRODED BETWEEN STATION 794 TO 847, BETWEEN STATION 794 TO 847. WEB AND STRAP REPLACEMENT ON AIR CARGO DOOR SILL PER DWG 65-47957. (M)SDR USAA040702Structure · wornRUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025.SDR USAA040638Skin · chafedPIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY .125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M)SDR USAA040662Skin · chafedPIT - FOUND RUDDER WITH CHAFE MARKS .25 INCH BY .20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040661Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040660Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040659Structure · crackedPIT - FOUND RUDDER CRACKED 1 INCH WITH DELAMINATION, LOWER LEFT LEADING EDGE. REMOVED DAMAGE, INSTALLED REPAIR PLYS PER EA 79025, SRM 51-70-17. (M)SDR USAA040700Support Angle · corrodedANGLE SUPPORT, .1250 INCH X .1250 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 794, S-25R. REPLACED ANGLE IAW SRM 51-40-02.SDR USAA040704Angle · crackedANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03.SDR USAA040675Hinge Fitting · wornHINGE FITTING WORN .0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69-39228.SDR USAA040663Angle · crackedPIT - FOUND ANGLE CRACKED 2 INCHES, RT WING ROOT, BS 540 AT S22R. REPLACED CREASE BEAM SECTION PER SRM 51-40-00. (M)SDR USAA040703Floor Support · crackedFLOOR SUPPORT, .5 INCH CRACK, DAMAGE AREA FLOORBEAM, STA727B, LBBL 8-10. MODIFIED REPAIR ANGLE IAW TR 53-10-06B, INSTALLED DOUBLER.SDR USAA040708Floorbeam · corrodedT-CAP, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 328 BL 0, RBL 59 INCH, 3 AREAS. INSTALLED NEW T CAP PER SRM 53-10-51.SDR USAA040637Skin · chafedPIT - FOUND RUDDER CHAFED 1 INCH BY .125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M)SDR USAA040643Stiffener · corrodedPIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BETWEEN STATION 312-328 RBL 11. REPLACED STIFFENER PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M)SDR USAA040639Skin · crackedPIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)SDR USAA040669Bushing · corrodedPIT - FOUND BUSHING CORRODED .25 INCH BY .125 INCH AREA, LEFT HORIZONTAL NR 12 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)SDR USAA040668Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, LEFT HORIZ STABILIZER STAB NR 9 LUG. MADE NEW BUSHING PER SRM 55-10-10. (M)SDR USAA040666Bushing · corrodedPIT - FOUND BUSHING CORRODED .25 INCH BY .25 INCH AREA, RIGHT HORIZ STAB R10 LUG. MADE NEW BUSHING AMS 4640 PER SRM 55-10-10. (M)SDR USAA040665Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH, RIGHT HORIZ STAB, R-8 CLEVIS BUSHING. MADE NEW BUSHINGS WITH AMS 4640 PER SRM 55-10-10. (M)SDR USAA040664Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, RT HORIZ STAB R-10 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)
Back to N514AU, cancelled Jul 2, 2008