N236US, cancelled Aug 11, 2000

Service difficulty reports · 23

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 = 'N236US' AND deregistration_id = 'N236US-2000-08-11'
  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 USAA000192Skin · crackedTPA - FOUND .5 INCH SKIN CRACK, STATION 540, JUST BELOW LAP AND STRINGER 14L SKIN. INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 AND EA 66144. (M)Feb 11, 2000 · N236US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990736Skin · crackedPIT - DURING RON CHECK, FOUND .5 INCH LONG CRACK AT STATION 727A STRINGER 18 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M)Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990735Skin · crackedPIT - DURING RON CHECK, FOUND A .75 INCH CRACK AT STATION 747 STRINGER 18 RT AND A .75 INCH LONG CRACK AT STATION 767 STRINGER 19 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M)Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990734Web · crackedPIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED SHEETMETAL DOUBLERS AND FILLERS PER TYPICAL REPAIR 53-10-12 REV A AND EA 52440. (M)Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB99142Charger · failedORD - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Jun 14, 1999 · N236US · Boeing 737201 · Emergency LightingSDR USAA990039Skin · crackedCLT - DURING PCI CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSE SKIN STATION 727 BELOW STRINGER 17R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Jan 14, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98167Seal · out of positionPIT - FLT 856 - AFTER TAKEOFF FROM PIT, AIRCRAFT FAILED TO PRESSURIZE. A LOUD AIR NOISE WAS HEARD COMING FROM DOOR R1. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE-INSTALLED THE R1 DOOR SEAL AND SECURED THE SERVICE DOOR. PRESSJul 2, 1998 · N236US · Boeing 737201 · Service DoorsSDR USAASB98153Engine · overtempPIT - FLT 1894 - AFTER TAKEOFF FROM PIT, THE NR 1 ENGINE ENCOUNTERED HIGH OIL TEMPERATURE. FLT RETURNED TO FIELD AT PIT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ENGINE WAS NOT SHUT DOWN IN FLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 EJun 21, 1998 · N236US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAASB98035Anti-Ice Duct · leakingTPA - FLT 1874 - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT APPROXIMATELY 25 MILES NORTH OF TPA. CREW FOLLOWED EMERGENCY PROCEDURES FOR OVERHEAT PROBLEM. WHEN THRUST LEVER WAS BROUGHT TO IDLE, THE LIGHT WENT OUT. FLIGHT RETURNED TO FIELD ATFeb 10, 1998 · N236US · Boeing 737201 · Air Intake Anti/De-Ice SystemSDR USAASB98025Windshield · defectiveORF - FLT 1279 - CAPT REPORTED VIA ACARS THAT FLIGHT WAS RETURNING TO FIELD AT ORF DUE TO A LOUD AIRLEAK COMING FROM THE F/O'S WINDSHIELD. NOISE WAS TOO LOUD TO COMMUNICATE IN COCKPIT. CLIMBED TO 5,000 FEET TO SEE IF THERE WOULD BE ANY CHANGE, BUT NOISE GOT Jan 30, 1998 · N236US · Boeing 737201 · Flight Compartment WindowsSDR USAA970303Skin · crackedROA - DURNG BX CHECK VISUAL INSPECTION, FOUND 1.125 INCH CRACK AFT ENTRY DOOR SKIN AFT UPPER CORNER. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 52-00-3 FIG 5. (M)Oct 24, 1997 · N236US · Boeing 737201 · Passenger/Crew DoorsSDR USAA970302Skin · crackedROA - DURING BX CHECK VISUAL INSPECTION, FOUND 3 INCH SKIN CRACK STATION 950 STRINGER 24L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIG 6. (M)Oct 24, 1997 · N236US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96175Battery Pack · failedCLT - MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS FLASHING. MAINTENANCE REMOVED AND REPLACD THE BATTERY PACK FOR THE OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (M)Aug 31, 1996 · N236US · Boeing 737201 · Emergency LightingSDR USAASB96171Light Ballast · burnedIAH - FL 1183 - ON DESCENT INTO IAH, CREW DETECTED SMELL OF SMOKE IN THE COCKPIT. WHILE LOOKING FOR THE SOURCE, THE SMOKE ALARM IN THE FORWARD LAV WENT OFF. SHORTLY AFTER, SMOKE WAS SPOTTED ABOVE THE LEFT FORWARD JUMP SEAT. CREW WENT ON OXYGEN AND STARTED EAug 30, 1996 · N236US · Boeing 737201 · Passenger Compartment LightingSDR USAA960568Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 45 INCH FLOOR BEAM. INSTALLED NEW CHANNEL AND DOUBLERS, REPAIRED PER EA 41421. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960567Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 25 CABIN FLOOR BEAM. INSTALLED NEW CHANNELS AND DOUBLERS PER EA 41421. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960565Floor Beam · brokenINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND UPPER 'T' OF FLOOR BEAM BROKEN INTO STATION 663 BL0. INSTALLED DOUBLER ON T-CAP AND WEB. REPAIRED PER BOEING DRAWING 65C34537. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960564Stringer · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH CORRODED AREA STRINGER 27L, STATION 967. CUT OUT DAMAGE AND INSTALLED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960563Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 6 INCH AT STATION 947.5 FLOOR BEAM. REPAIRED T-CAP, DOUBLERS AND REPAIR ANGLES. REPAIRED PER TR 53-10-05C. SUBMITTER STATES, CORROSION ATTRIBUTED TO CHEMICAL SPILL. CORROSION TASK NR C53-Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960562Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS IN FASTENER HOLES FOR STRINGER 15R TO STATION 532. CUT OUT DAMAGED AREA AND FABRICATED AND REPLACED DAMAGED SECTION WITH STRINGER. REPAIRED SPLICE REPAIR PER SRM 53-10-3 FIG 1. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960561Angle · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCH STATION 277 TO 340 'Z' ANGLE RIGHT SIDE. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960560Beam · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 420 TO BS 500, STRINGER 26R BEAM. FABRICATED AND REPLACED WITH NEW BEAM. SPLICED AT 420 AND 500. REPAIRED PER SRM 53-00-53 AND SRM 53-10-5. CORROSION TAKS NR 53-208-Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960559Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS AT FASTENER HOLES STATION 532, STRINGER 15R. REMOVED DAMAGED SECTION OF STRINGER AND PERFORMED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. (M)Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/Stringer
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