N393US, cancelled Jul 5, 2013

Service difficulty reports · 60

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 = 'N393US' AND deregistration_id = 'N393US-2013-07-05'
  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 SB06003Charger · faultyDCA - DURING FLIGHT, THE EMERGENCY EXIT LIGHTS AT THE SEATS AND AT THE BOTTOM OF THE FORWARD ENTRY AND SERVICE DOORS ILLUMINATED AND WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY AT STATION 400 PER MM 33-51-00. ALJan 10, 2006 · N393US · Boeing 7373B7 · Emergency LightingSDR USAA050884Skin · crackedCLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)Jul 18, 2005 · N393US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR SB05075Shutoff Valve · leakingPHL FLT 1085 AFTER TAKEOFF AND GEAR RETRACTION, CREW REPORTED A SUBSTANTIAL DROP IN THE A-HYDRAULIC SYSTEM QUANTITY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLIGHT CONTROL SHUTOJun 28, 2005 · N393US · Boeing 7373B7 · Hydraulic System, MainSDR SB05044Wire · brokenBOS COCKPIT EMERGENCY LIGHT SWITCH NOT WORKING PROPERLY. MAINTENANCE REPAIRED A BROKEN WIRE ABOVE ROW 20ABC.Apr 5, 2005 · N393US · Boeing 7373B7 · Light System WiringSDR SB05042Battery Pack · faultyMAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD.Mar 30, 2005 · N393US · Boeing 7373B7 · Emergency LightingSDR USAA050062Skin · crackedPIT - FOUND SKIN CRACKED 2.5 INCHES, 1 INCH ABOVE S23L AT BS 745. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)Jan 13, 2005 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040386Skin · delaminatedFOUND SKIN AND CORE BONDED 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED NEW CORE AND TOP SKIN PER BOEING SRM 51-70-10. (M)Jul 21, 2004 · N393US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040387Skin · delaminatedPIT - FOUND SKIN AND CORE BOND DELAMINATED 3 INCH BY 4 INCH AREA, UPPER INBOARD END T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)Jul 21, 2004 · N393US · Boeing 7373B7 · Leading Edge DevicesSDR USAASB04030Tube · leakingAFTER TAKEOFF FROM CLT, THE RIGHT MLG WOULD NOT RETRACT. THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESURE LIGHT WAS ALSO ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, SELECTED THE HYDRAULIC PUMP TO OFF AND DECLARED AN EMERGENCY. FLIGHT RETURNMar 15, 2004 · N393US · Boeing 7373B7 · Hydraulic System, MainSDR USAA040007Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, BS 178 LEFT SIDE FRAME AT WL 207. SPLICED FRAME AT WL 212 EPR EO 5300V157 PART F. (M)Jan 9, 2004 · N393US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA04000BBulkhead · crackedFOUND WEB CRACKED .5 INCH, BULKHEAD WEB BS 178, WL 218, RBBL 5.7. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 7, 2004 · N393US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAASB03155Battery Pack · inoperativeCLT - MAINTENANCE REPORTED THE CABIN OVERHEAD BIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD. (M)Aug 27, 2003 · N393US · Boeing 7373B7 · Emergency LightingSDR USAA030154Skin · crackedPIT - FOUND SKIN PANEL CRACKED 10 INCHES AND SEVERAL .25 INCH THROUGH .5 INCH LONG CRACKS AND DISBONDED, LAPJOIJNT S-10L BS 360-540 ALONG 15 FT SECTION OF FUSELAGE SKIN. INSTALLED THREE NEW SKIN PANELS .080 INCH PER EA 76610A. (M)Aug 19, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA030153Skin · crackedPIT - FOUND SKIN CRACKED 2.4 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER SRM 53-60-01 FIG 207. (M)Aug 19, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA030138Skin · crackedPIT - FOUND SKIN CRACKED .125 INCH BY .25 INCH CRACKING AT RIVET HEADS, APPROX 40, AND DISONDING, LEFT SIDE STATION 360-540 STRINGER 10 LEFT. REMOVED SKIN PANEL STATION 360-540, INSTALLED 3 SECTIONS WITH 2 SPLICE AT STATION 420 AND 480 PER EA 76610. (M)Aug 14, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB03010Pump · faultyPHL - FLT 390 - EN ROUTE FROM CLT-DTW, THE 'A' HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED WITH THE PUMP CYCLING ON AND OFF. DECISION WAS MADE TO DIVERT TO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLAREDJan 15, 2003 · N393US · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), MainSDR USAA020329Skin · crackedPIT - FOUND SKIN CRACKED 2.1 INCH, STATION 727E ABOVE STRINGER 24L IN AFT FUSELAGE SKIN. CRACKED AREA CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)Aug 1, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020309Stringer · corrodedPIT - FOUND STRINGER CORRODED ON ENDS OF STRINGER STATION 323.7 AND BL 0 TO S28R. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020297Door Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER FORWARD CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA020298Door Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER AFT CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA020293Attach Angle · crackedPIT - FOUND ANGLE CRACKED .75 INCH, INT ATTACH ANGLE FORWARD STATION 291.5, S12R AND S13R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA020294Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, INT ATTACH ANGLE FORWARD OF STATION 291.5, S11R AND S12R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BOEING DWG 65-45807-31. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA020296Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, INT DOOR FRAME ON FUSELAGE AT FORWARD UPPER CORNER. FABRICATED NEW ANGLE PER EA. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA020299Stringer · crackedPIT - FOUND STRINGER CRACKED .125 INCH, AT RIVET STATION 927 AT STRINGER 8R AND 9R. REMOVED CRACK AND INSTALLED OVERSIZED FASTENER PER 51-40-05. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020300Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907, STRINGER 8L-9L AT RIVET. REMOVED CRACKED AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-10-14A. (M)Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA020225Skin · delaminatedPIT - FOUND RUDDER DELAMINATED SEVERAL PLACES FROM .25 INCHES TO 6 INCHES, 1 PLY DEEP, RIGHT/LEFT RUDDER, R STATION 121.64 TO 0.00. COMPLETED 200-230 DEGREE WET LAY UP PER SRM 51-70-17 PER EA 74241. (M)Jul 2, 2002 · N393US · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA020310Skin · crackedPIT - FOUND SKIN CRACKED 3 INCHES, ABOVE LEFT NLG DOOR JUST FORWARD OF STATION 259.5. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER EA 61654B. (M)Jul 2, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020295Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCHES LONG, FORWARD SERVICE DOOR AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01 FIG 202. (M)Jun 19, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA020308Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, CAPTAINS WINDSHIELD NR 1 UPPER LEFT CORNER OF WINDOW POST. INSTALLED EXTERIOR DOUBLER PER SRM 53-10-01 FIG 210 PAGE 233. (M)Jun 19, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB02017Regulator · failedBOS - FLT 926 - CLIMBING-OUT FROM PHL, EN ROUTE TO PWM AT FL250, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CREW TRIED TO RESET BLEED WITH NO HELP. WITH NR 2 BLEED INOPERATIVE, PRESSURIZATION WAS OK AT FL250 FOR 15 MINUTES, BUT THEN THE CABIN PRESSURE BEGJan 19, 2002 · N393US · Boeing 7373B7 · Pneumatic Distribution SystemSDR USAA020104Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, VERTICAL ANGLE AT STATION 363. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED CHANNEL PER NR 313A1355. (M)Dec 30, 2001 · N393US · Boeing 7373B7 · Nacelle/Pylon StructureSDR USAA011364Skin · crackedPIT - FOUND ON WALK AROUND, FOUND SKIN CRACKED 3 INCHES, NR 6 SLAT BOTTOM INBOARD END. CUT OUT DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, FIG 206. (M)Nov 15, 2001 · N393US · Boeing 7373B7 · Leading Edge DevicesSDR USAASB01282Charger · failedCLT - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACKS (P/N 2013-1A) AND THE RIGHT FORWARD CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Oct 3, 2001 · N393US · Boeing 7373B7 · Emergency LightingSDR USAA010162Crossbeam · corrodedPIT - FOUND ENGINE MOUNT CROSSBEAM CORRODED, BEARING BORE OF CROSS BEAM. CORROSION LEVEL 1. ENLARGED BORE .010 CHANFERED BORE, MPI ROTO PEEN. INSTALLED OVERSIZED BEARING PER TYP REP 54-50-09. (M)Jan 10, 2001 · N393US · Boeing 7373B7 · Engine Mount SectionSDR USAASB00280Uplock Switch · failedGSO - FLT 1658 - ON CLIMB-OUT, AFTER GEAR RETRACTION, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO FIELD AT GSO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENOct 1, 2000 · N393US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAASB00220Control Cable · out of adjMCO - FLT 808 - AFTER TAKEOFF FROM MCO, CREW WAS UNABLE TO RAISE LANDING GEAR. THE GEAR SELECTOR LOCKED AT MID-POINT. UPON FLAP TO ZERO, THE WARNING HORN BEGAN SOUNDING. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAREAug 18, 2000 · N393US · Boeing 7373B7 · Drag Control SystemSDR USAASB00219Solenoid · faultyMCO - FLT 676 - AFTER TAKEOFF FROM MCO, CREW RAISED GEAR HANDLE TO STOW THE GEAR BUT THE HANDLE STOPPED BEFORE REACHING THE GEAR UP POSITION. DURING TROUBLESHOOTING, CREW RECEIVED A WARNING HORN. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. Aug 17, 2000 · N393US · Boeing 7373B7 · Landing Gear Retraction/Extension SystemSDR USAASB00127Adc · failedCLT - FLT 463 - CLIMB-OUT FROM CLT, AT FL 230, OFF FLAGS APPEARED ON CAPTAIN''S AIRSPEED INDICATOR AND ALTIMETER. CREW WAS UNABLE TO ENGAGE A-SYSTEM AUTOPILOT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. Apr 27, 2000 · N393US · Boeing 7373B7 · Air Data ComputerSDR USAASB00044Shutoff Valve · leakingPIT - FLT 8054 - INBOUND TO PIT, FROM IAH, SYSTEM A HYDRAULICS FAILED. CREW DECLARED AN EMERGENCY AND HAD TO MANUALLY EXTEND LANDING GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. LANDING GEAR WAS PINNED BEFORE BEING TOWED TO THE GATE. MAINTENANCE FOUND THEFeb 18, 2000 · N393US · Boeing 7373B7 · Hydraulic System, MainSDR USAASB99222Seal · tornTPA - FLT 1469 - EN ROUTE FROM CLT TO TPA, ABOVE GAINESVILLE FLORIDA AT FL310, FLIGHT LOST PRESSURIZATION. THE CREW FELT A THUMP IN THE CABIN ALONG WITH A RISE IN CABIN ALTITUDE OF 4,000 FEET PER MINUTE. CREW DECLARED AN EMERGENCY AND QUICKLY DESCENDED TO 10Sep 7, 1999 · N393US · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAASB98264Warning Light · illuminatedPIT - FLIGHT WAS EN ROUTE FROM BOS, WHEN THE CREW RECEIVED A RIGHT MLG UNSAFE INDICATION. AIRCRAFT MADE AN UNEVENTFUL LANDING AT PIT. (M)Oct 5, 1998 · N393US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA980465Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AROUND FASTENERS .5 INCH BY .5 INCH BY 37 INCH STAITON 312 BETWEEN LBL 14 AND RBL 23 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED NEW T-SECTION WITH DOUBLER PER SRM 53-10-Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980443Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORRODED AREA BS 967 RBL 49 BEAM INST PAX FLOOR. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-10-05. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980442Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK SHEAR BEAM WEB 518A RIGHT BS 721. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980441Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2 INCH CORRODED AREA BS 827 BETWEEN STRINGER 28L AND STRINGER 28R RBL 2 BOTTOM FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980440Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CRACKED AREA .25 INCH FORWARD SERVICE DOOR OPENING LWR FWD CORNER BS 294 STRINGER 17R FLOOR LEVEL. INSTALLED DOUBLER PER SRM 51-70-11. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980425Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS .5 INCH BY .5 INCH BY 26 INCH BS 328 LB 12 TQ RBL 14, WL 208.1 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER SRM 51-70-12. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980424Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 2 INCH CORRODED AREA STATION 1006 BEAM T-CAP RBL 10. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-58-53500-012. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980423Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION BS 986.5 LBL 4, 11, 21 AND LOWER SURFACE LBL 36 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP UPPER CHORD PER SRM 53-00-51 AND EA 62431. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980422Splice · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND STRINGER SPLICE CRACKED AROUND 4 RIVET HOLES .125 INCH EACH STRINGER AT STATION 907 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-40-02. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous Structure
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