N394US, cancelled Jul 18, 2006

Service difficulty reports · 47

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 = 'N394US' AND deregistration_id = 'N394US-2006-07-18'
  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 SB05116Bracket · missingORD - PILOT REPORTED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE.Sep 19, 2005 · N394US · Boeing 7373B7 · Escape SlideSDR USAA050452Frame · brokenCLT - FOUND FORMER BROKEN, STATION 535 WL 165, LBL 60. REPLACED FORMER. (M)Apr 2, 2005 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR SB05032Circuit Breaker · burnedAFTER LANDING CREW STOPPED A/C ON TAXIWAY & REPORTED TO INBOUND RAMP, FIRE & SMOKE IN COCKPIT. CREW STATED, "ON TAXI-IN, FIRE ERUPTED FROM F/O LWR C/B PNL. USED PORTABLE HALON FIRE EXTINGUISHER & EVACUATED A/C. ENG 1 & 2 & APU FIRE EXTINGUISHER BOTTLES DISCHFeb 23, 2005 · N394US · Boeing 7373B7 · AC Power Distribution SystemSDR USAA040834Skin · crackedSKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01.Oct 8, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040507Skin · crackedPIT - FOUND SKIN CRACKED 1.250 INCH, STATION 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)Aug 12, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040360Skin · crackedPIT - FOUND SKIN CRACKED APPROXIMATELY .375 INCH CRACK, AFT CARGO DOOR FORWARD FRAME CUTOUT. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER PER EA 78434. (M)Jul 26, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040344Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M)Jul 16, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040206Skin · crackedSERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAGE 207.May 6, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA030218Skin · crackedFOUND SKIN CRACKED 2.375 INCH, STATION 740 AND S23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Oct 28, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB03074Odor · detectedTEN MINUTES AFTER TAKEOFF FROM CLT, FLIGHT ATTENDANT REPORTED AN ELECTICAL ODOR ALONG WITH A SLIGHT HAZE IN THE CABIN FROM SEAT ROWS 4 THROUGH 14. AS A PRECAUTION, CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENJun 7, 2003 · N394US · Boeing 7373B7 · Air Distribution SystemSDR USAA030080Skin · crackedFOUND SKIN CRAKCED .75 INCH LONG CRACK, SKIN AFT ENTRY DOOR LOWER HINGE CUTOUT STATION 947.5, STRINGER 14L. DOUBLER AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01 AND EA 76329. (M)May 22, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA030081Skin · crackedPIT - FOUND SKIN CRACKED .75 INCH LONG, SKIN AFT SERVICE DOOR LOEWR HINGE CUTOUT STATION 947.5, STRINGER 14R. DOUBLE AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01. (M)May 22, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02186Slide · malfunctionedDURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIONAL CHECK FAILED. MSep 30, 2002 · N394US · Boeing 7373B7 · Escape SlideSDR USA2002F00092Slide · failedDURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIONAL CHECK FAILED. MSep 30, 2002 · N394US · Boeing 7373B7 · Escape SlideSDR USAASB02115Wire · brokenCLT - FOUND MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEAT ROW 20C. OPERATIONAL CHECK GOOD. (M)Jun 16, 2002 · N394US · Boeing 7373B7 · Light System WiringSDR USAA020198Stringer · crackedPIT - FOUND SHELF WITH .25 INCH CRACK ON EACH SIDE OF FASTENER, AFT END OF S18 LEFT SHELF AT AFT INBOARD FASTENER. REPLACED 18A SHELF ASSEMBLY PER SRM 51-40-02. (M)May 22, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020191Frame · corrodedPIT - FOUND FRAME CRACKED 1 INCH BY 3 INCH CORRODED AREA, FS 500B, BETWEEN STRINGERS 27L AND 28L. REMOVED CORROSION PER SRM 51-40-02. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020199Stringer · corrodedPIT - FOUND SHELF WITH 3 AREAS OF CORROSION, 1 INCH ROUND, 2 INCH BY 2 INCH, 2 INCH BY 3 INCH, 6 INCHES TO 8 INCHES AFT OF STATION 706 ON LEFT 18A SHELF. REMOVED CORROSION PER SRM 51-10-02. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020200Stringer · corrodedPIT - FOUND 1 INCH ROUND CORRODED AREA, BETWEEN STATION 695 AND 706 ON LEFT SIDE 18A SHELF INBOARD. REMOVED CORROSION PER SRM 51-10-02. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020192Frame · corrodedPIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH CORRODED AREA, STATION 500B, BETWEEN STRINGERS 28L AND 28R. INSTALLED FABRICATED SHEAR TIE PER SRM 51-70-11. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020193Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FS 887 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020194Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FS 827 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020195Support · crackedPIT - FOUND ANTENNA SUPPORT ZEE 1.25 INCH CRACK, HORIZONTAL LEG OF ANTENNA ZEE SUPPORT STATION 727D AND 727C. REPLACED ZEE SUPPORT PER SRM 51-40-05. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA020196Doubler · crackedPIT - FOUND DOUBLER CRACKED 1 INCH, ANTENNA DOUBLER BETWEEN STATION 727D AND 727E. REPLACED ZEE SUPPORT AND MOUNT BRACKET PER SRM 51-40-05. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020197Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, FRAME 807 LEFT AT FASTENER STRINGER 9. INSTALLED ANGLES, SHIMS, STRAP PER T/R 53-10-14A. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020216Doubler · corrodedPIT - FOUND ANTENNA DOUBLER CORRODED SIX .25 INCH BY .25 INCH AREAS, ANTENNA MOUNT NUTPLATE BRACKETS BETWEEN STATION 727D. REMOVED CORROSION AND REPLACED CHANNEL PER SRM 53-30-53, 51-40-05. CORROSION LEVEL 1, TASK NR C53-208-01. (M)May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA020171Skin · corrodedPIT - FOUND RIB AND SKIN WITH HEAVY CORROSION 4 INCHES LONG BY 1 INCH WIDE, RUDDER COUNTER BALANCE STRUCTURE, RUDDER STATION 121.64. LEVEL 2 CORROSION. (M)Apr 24, 2002 · N394US · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA020170Frame · crackedPIT - FOUND FRAME CRACKED .062 INCH, FRAME 480 LEFT SIDE BETWEEN S8L AND S9L. REPAIRED PER TYPICAL REPAIR 53-10-14A. (M)Apr 15, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020172Frame · crackedPIT - FOND FRAME CRACKED .064 INCHES LONG, FRAME 400 RIGHT SIDE BETWEEN S8R AND S9R. ACCOMPLISHED TYPICAL REPAIR 53-10-14A. (M)Apr 15, 2002 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAASB01115Fuse · blownTPA - MAINTENANCE FOUND THE FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO 5 AMPS FUSES. OPS CHECK GOOD. (M)Apr 27, 2001 · N394US · Boeing 7373B7 · Emergency LightingSDR USAASB01114Light · inoperativeTPA - MAINTENANCE FOUND SEAT 5C EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SPLICE. OPS CHECK GOOD. (M)Apr 27, 2001 · N394US · Boeing 7373B7 · Emergency LightingSDR USAASB01106Transmission · failedIAD - FLT 1083 - ON APPROACH TO DCA, CAPTAIN REPORTED THAT THE FLAPS WERE STUCK AT 10 DEGREES. CREW CHECKED ALL CIRCUIT BREAKERS AND TRIED ALTERNATE METHOD WITH NO HELP. FLIGHT DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. Apr 20, 2001 · N394US · Boeing 7373B7 · Trailing Edge Flap Control SystemSDR USAA000850Skin · crackedCLT - FOUND SKIN FUSELAGE CRACKED 1.5 INCH, BS 727D PLUS 17.5 INCH JUST ABOVE STRINGER 23R. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 202 AND TR 53-60-03. (M)Jun 14, 2000 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA000451Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 2.125 INCHES, STRINGER 24L JUST FORWARD OF BS 727E. INSTALLED EXTERNAL DOUBLER PER EA 66901. (M)Mar 23, 2000 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB99215Stud · looseDFW - FLT 870 - CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW AND CLIMBING THROUGH 17,000 FT, THE NR 1 ENGINE OIL TEMPERATURE ROSE ABOVE THE RED RADIAL. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DFW. FLIGHT LANDED WITHOUT FAug 31, 1999 · N394US · Boeing 7373B7 · Engine Oil Indicating SystemSDR USAA990798Skin · crackedTPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK BELLY SKIN AFT EQUIPMENT COOLING EXHAUST STA 380 FUSELAGE SKIN. INSTALLED REPAIRED DOUBLER PER TR 53-30-07. (X)Aug 3, 1999 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA990279Skin · crackedCLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AFT WING TO BODY FAIRING SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01. (M)Mar 31, 1999 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980371Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF CREASEBEAM INNER CHORD RBBL BETWEEN STATION 294.5 TO STATION 331. CORROSION TASK NR C53-107-02. INSTALLED SPLICE PER DRAWING 6545875 AND SRM 51-10-02. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980370Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 11 INCH AREA OF CORROSION ON UPPER FLOORBEAM CHORD STATION 1016 LBL 15, CORROSION TASK NR C53-107-02. INSTALLED 11.5 INCH DOUBLER PER SRM 53-00-51 FIG 203. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980369Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON 'T' CAP OF FLOORBEAM 65 INCH BY 3.5 INCH STATION 312 LBL 8 RBL 56 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. FABRICATED 'T' CAP ANGLES PER TR 53-10-03. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980368Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBEAM BOARD SCREW HOLES .5 INBY .5 BY 70 INCH STATION 328 BETWEEN RBL 14 TO RBL 56 UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP SECTION PER SRM 53-10-51. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980367Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBOARD SCREW HOLES .5 INCH BY .5 INCH BY 25 INCH STATION 344 BETWEEN LBL 14 TO RBL 11 UPPER CHORD FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T' CAP AND SPLICED ANGLES PER TR 53Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980366Skin · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT SERVICE DOOR INSIDE UPPER FRAME SKIN, UPPER HINGE ARM CLOSEOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 62249. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980174Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 2.675 INCH CRACK IN THE SKIN AT RIGHT BS 727D AT S23R. INSTALLED DOUBLER PER REPAIR DOCUMENT EA 61668. (X)Apr 25, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB97318Battery Pack · dischargedPVD - MAINTENANCE FOUND THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Nov 21, 1997 · N394US · Boeing 7373B7 · Emergency LightingSDR USAASB97046Seal · leakingLGA - FLT 2238 - DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE AND RETURNED TO FIELD AT LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE E/E DOOR SEAL LEAKING EXCESSIVELY. REPOSITIONED DOOR SEAL PER MM 52-48-41 AND 52-09-12. PERFORMED LEAK CFeb 12, 1997 · N394US · Boeing 7373B7 · Electrical/Electronic Compartment DoorsSDR USAASB96246Engine · bird strikeDAB - FLT 282 - UPON ROTATION WITH THE NOSE JUST OFF THE RUNWAY, THE AIRCRAFT STRUCK A FLOCK OF BIRDS. SEVERE VIBRATION WAS FELT FROM THE NR 2 ENGINE. THE CAPTAIN DID NOT SHUT DOWN THE ENGINE BUT KEPT IT IN IDLE WHILE THEY RETURNED TO FIELD AT DAB. NO EMERGNov 26, 1996 · N394US · Boeing 7373B7 · Engine (Turbine/Turboprop)
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