N300AU, cancelled Sep 5, 2008

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 = 'N300AU' AND deregistration_id = 'N300AU-2008-09-05'
  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 USAA051413Skin · debondedNR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH.Nov 22, 2005 · N300AU · Boeing 737301 · Leading Edge DevicesSDR USAA051199Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH.Oct 12, 2005 · N300AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA200509002Skin · cracked2 INCH CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT STA 727E - 747 STRINGER 23L. REMOVED REPAIR DOUBLER, FABRICATED NEW DOUBLER AND FILLERS AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201.Sep 15, 2005 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB05108Pump · leakingPHL - FLT803 - ON CLIMB-OUT FROM PHL, CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON GEAR RETRACTION. SYSTEM "A" HYDRAULIC QUANTITY DROPPED TO LESS THAN ONE-QUARTER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER ISep 3, 2005 · N300AU · Boeing 737301 · Hydraulic Pump (Electric/Engine), MainSDR USAA041111Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M)Dec 28, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA041110Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M)Dec 28, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USA2004F00036Charger · failedMAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD.May 13, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR USA2004F00037Battery Pack · dischargedMAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD.May 8, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR USAA040191Skin · crackedPIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DOUBLER, TRIPLER AND FILLERS PER EA 78356. (M)May 7, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040055Stringer · crackedCLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVAL PER SRM 53-00-01 DETAIL XI FIG 229. (M)Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040054Stringer · crackedFOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVED PER SRM 53-00-01 FIG 229 DETAIL XI. (M)Mar 8, 2004 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAASB03170Battery Pack · malfunctionedMAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY LIGHT EXTINGUISHES AFTER APPROXIMATELY FIVE SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Sep 18, 2003 · N300AU · Boeing 737301 · Emergency LightingSDR USAA030171Skin · crackedFOUND SKIN CRACKED 1 INCH, AFT OF FS 727D BELOW S23R. INSTALLED DOUBLER PER EA 94615. (M)Aug 21, 2003 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030012Skin · corrodedPIT - FOUND SKIN CORRODED 2 INCHES BY 4 INCHES, BELOW CABIN FLOOR STATION 1016 AT BL 0 AFT PRESSURE BULKHEAD, CORROSION LEVEL 2, TASK NR C53-107-02. REMOVED CORRODED SECTION, INSTALLED DOUBLERS AND SPLICE PER SRM 53-80-08 AND 51-40-02, EA 75070. (M)Jan 16, 2003 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB02210Door · out of rigIND - FLT 338 - ON CLIMB-OUT FROM IND, EN ROUTE TO CLT, THE FORWARD MAIN ENTRY DOOR WARNING LIGHT ILLUMINATED. CREW REPORTED THE HANDLE COMES UP IN FLIGHT WHEN PRESSURIZED AND THE LIGHT WILL GO OFF AND ON AS HANDLE IS PRESSED DOWN TO CLOSED POSITION. FLIGHT Nov 24, 2002 · N300AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA020417Elevator · delaminatedPIT - FOUND LEFT ELEVATOR SPLINTERING AND DELAMINATED, STATION 95, 81, 100 INBOARD SIDE. ACCOMPLISHED SKIN AND CORE REPAIRS PER SRM 55-20-01, 51-70-17 AND EA 75277. (M)Nov 7, 2002 · N300AU · Boeing 737301 · Elevator, Plate/SkinSDR USAA020418Stringer · crackedPIT - FOUND SHELF CRACKED 1 INCH LONG, AFT END OF RIGHT 18A SHELF, FED OF STATION 727. REMOVED AND REPLACED SHELF PER SRM 51-10-02. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA020419Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH DIAMETER, S27L AND STATION 336 IN FRAME OF EYE OPENING. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020421Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .75 INCH LONG, STATION 357 AND STRINGER 16L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020422Stringer · crackedPIT - FOUND STRINGER CRACKED .375 INCH LONG, STRINGER 17R BETWEEN STATION 616-639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA020423Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .5 INCH LONG, SHEAR TIE S2L AT STATION 639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, StructureSDR USAA020424Frame · crackedPIT - FOUND FRAME CRACKED .375 INCH, STATION 663 AND STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND STRINGER SPLICES PER EA 74814. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020425Clip · crackedPIT - FOUND CLIP CRACKED .5 INCH LONG, STATION 663 STRINGER 10L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020426Bracket · crackedPIT - FOUND BRACKET CRACKED .5 INCH LONG, STATION 663 STRINGER 8L AND 9L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020427Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH LONG, FS 663 STRINGER 4L. REMOVED TIE CLIP, HFEC INSPECTION OF STRINGER AND CLIP PER SRM 51-40-02 AND NDT 0-4-53-10. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA020428Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH LONG, FS 480 STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020429Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, STATION 480 STRINGER 8R AND 9R. REMOVED DAMAGED AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020432Stringer · crackedPIT - FOUND SHELF WITH 1 INCH LONG CRACK, AFT END OF LEFT 18A SHELF, FORWARD OF STATION 727. REMOVED AND REPLACED 18A SHELF PER SRM 51-10-02. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA020415Skin · crackedPIT - FOUND LEADING EDGE REMOVABLE SKIN WITH CRACKS, 1 INCH BY 1 INCH AREA BEYOND 25 PERCENT MAXIMUM LIMITS, 14 EACH BLENDED AREAS, LEFT HORIZ STABILIZER LEADING EDGE STATION 86.66-151.75. BLENDED AND POLISHED PER SRM 55-10-01. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Horizontal Stabilizer, Plate/SkinSDR USAA020420Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH BY 7 INCH AREA, STATION 303 AND 310 AT STRINGER 4L. FABRICATED WEB, STRAP AND T-FITTING PER SRM 53-02-04. (M)Nov 4, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020416Support · corrodedPIT - FOUND SUPPORT CORRODED SEVERAL AREAS, BS 960 Z-ANGLE SUPPORT, AFT ENTRY THRESHOLD DOOR JAM. CORROSION, LEVEL 2, TASK NR C53-107-01. REPLACED Z-ANGLE PER BOEING DWG 65-52878. (M)Oct 2, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020369Structure · chafedPIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER TYPICAL REPAIR 57-50-17. (M)Sep 27, 2002 · N300AU · Boeing 737301 · Wing, Control SurfacesSDR USAA020371Mount · wornPIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. (M)Sep 25, 2002 · N300AU · Boeing 737301 · Engine Mount SectionSDR USAA020414Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH LONG, STATION 616 RIGHT SIDE FRAME LOWER INBOARD END. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74856. (M)Sep 20, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020365Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, STATION 616 RIGHT SIDE, FRAME LOWER INBOARD END CABIN FLOOR. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74256. (M)Sep 20, 2002 · N300AU · Boeing 737301 · Fuselage Main, FrameSDR USAA020364Skin · delaminatedPIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIES OF GRAPHITE FABRIC PER EA 74841, SRM 55-40-01, 51-70-17. (M)Sep 19, 2002 · N300AU · Boeing 737301 · Rudder, Plate/SkinSDR USAA020367Skin · crackedRIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA.Sep 17, 2002 · N300AU · Boeing 737301 · AileronsSDR USAA020282Mount · wornPIT - FOUND ENGINE MOUNT STRUT WORN BEYOND LIMITS, ENGINE MOUNT MAIN SLEEVE REPAIR. REAMED, CHAMFERED, BLENDED AND ROTOPEENED THE FITTING BORE PER TYPICAL 54-50-10 REV A. (M)Jul 23, 2002 · N300AU · Boeing 737301 · Engine Mount SectionSDR USA2002F00053Sensor · failedAFTER TAKEOFF, CREW WAS UNABLE TO MOVE THE LANDING GEAR SELECTOR HANDLE PAST THE OFF POSITION TO RETRACT THE GEAR. CREW ALSO TRIED THE GEAR OVER RIDE WITH NO HELP. DUE TO THE TAKEOFF WARNING HORN SOUNDING AFTER THE FLAPS WERE FULLY RETRACTED, CREW THINKS THJun 2, 2002 · N300AU · Boeing 737301 · Landing Gear Position and WarningSDR USAA020184Rib · corrodedPIT - FOUND RUDDER CORRODED 3 INCHES BY 12 INCH AREA, COVER FACE OF RIB BEHIND BALANCE WEIGHTS ON BEAM. REPLACED RIB PER SRM 51-10-02, 51-20-01, 51-20-00 AND 51-40-02. (M)Apr 30, 2002 · N300AU · Boeing 737301 · Rudder, Spar/RibSDR USAASB01349Wire · disconnectedBWI - PILOT REPORTED THE WIRING FOR THE EMERGENCY EXIT LIGHTS UNDER SEAT 21C IS DISCONNECTED AND THE LIGHTS ARE INOPERATIVE. MAINTENANCE RECONNECTED AND SECURED WIRING. OPS CHECK OF LIGHTS GOOD. (M)Dec 23, 2001 · N300AU · Boeing 737301 · Light System WiringSDR USAA011393Structure · damagedPIT - FOUND RUDDER DAMAGED, NR 7 HINGE AREA RSTA 225-235 LEADING EDGE. PER SRM 51-70-17 2 EXTRA PLIES WITH HALF OVERLAP PER EA 73066. (M)Dec 17, 2001 · N300AU · Boeing 737301 · Rudder StructureSDR USAA011394Structure · damagedPIT - FOUND RUDDER 8 INCH BY .750 INCH GOUGED, CLOSE TO T/E WEDGE BETWEEN R STA 121164 AND 174.12. REPAIRED PER SRM 51-70-17 WITH 2 EXTRA PILES WITH .5 OVERLAP PER EA 73065. (M)Dec 17, 2001 · N300AU · Boeing 737301 · Rudder StructureSDR USAA011395Skin · damagedPIT - FOUND RUDDER SCREW PULLED THROUGH SKIN, LEFT SKIN PANEL AT R STATION 225 APPROXIMATELY. TWO EXTRA REPAIR PLIES WITH .5 INCH PER PLY OVERLAP PER EA 73064. (M)Dec 17, 2001 · N300AU · Boeing 737301 · Rudder, Plate/SkinSDR USAASB01083Door · not closedBWI - FLT 1568 - ON CLIMB-OUT FROM DCA, AT APPROXIMATELY 4,500 FEET, THE FLIGHT ATTENDANT ADVISED CREW OF A LOUD AIR NOISE COMING FROM THE FORWARD ENTRY DOOR. SIMULATANEOUSLY, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. FLIGHT DIVERTED TO BWI AND LANDED Mar 20, 2001 · N300AU · Boeing 737301 · Passenger/Crew DoorsSDR USAASB01009Wire Harness · out of positionLGA - MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHTING AT SEAT 16C INOPERATIVE. MAINTENANCE REPOSITIONED WIRING HARNESS FOR SEAT ROW 16ABC EMERGENCY EXIT PATH LIGHTING. OPS CHECK GOOD. (M)Jan 18, 2001 · N300AU · Boeing 737301 · Light System WiringSDR USAASB00223Charger · failedCLT - PILOT REPOTED THAT THE EMERGENCY EXIT PATH LIGHTS FROM SEAT ROWS 5 TO 11 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY AND THE BATTERY PACK (P/N AD2013-1A). OPS CHECK GOOD. (M)Aug 19, 2000 · N300AU · Boeing 737301 · Emergency LightingSDR USAASB00089Power Supply · failedTPA - DURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSY FOR THE ESCAPE SLIMar 28, 2000 · N300AU · Boeing 737301 · Emergency LightingSDR USAA991435Skin · crackedPIT - DURING RON VISIT, FOUND 1.0625 INCH LONG CRACK ON FUSELAGE SKIN AT RT SIDE, STATION 767 STRINGER 22 TO 23 RT. REMOVED CRACK WITH CUTOUT. INSTALLING EXTERNAL DOUBLER PER SRM 53-00-00-01, FIG 201, EA 53528. (M)Dec 9, 1999 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB99290Cabin Pressure · failedPIT - FLT 2380 - DURING CLIMB-OUT FROM PIT, THE AUTO PRESSURIZATION SYSTEM FAILED TO STANDBY. CREW WAS UNABLE TO CONTROL CABIN IN STANDBY OR MANUAL MODE. CABIN CONTINUED TO CLIMB WITH OUTFLOW VALVE CLOSED. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHDec 8, 1999 · N300AU · Boeing 737301 · Cabin Pressure Control System
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