# Service difficulty reports: N236US, cancelled Aug 11, 2000 A list on [N236US, cancelled Aug 11, 2000](https://openairdocs.org/deregistered/N236US-2000-08-11.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAA000192](https://openairdocs.org/sdr/USAA000192.md): Skin · cracked · Feb 11, 2000 · N236US · Boeing 737201 · Fuselage Main, Plate/Skin > TPA - 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) - [SDR USAA990736](https://openairdocs.org/sdr/USAA990736.md): Skin · cracked · Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA990735](https://openairdocs.org/sdr/USAA990735.md): Skin · cracked · Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA990734](https://openairdocs.org/sdr/USAA990734.md): Web · cracked · Jul 17, 1999 · N236US · Boeing 737201 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAASB99142](https://openairdocs.org/sdr/USAASB99142.md): Charger · failed · Jun 14, 1999 · N236US · Boeing 737201 · Emergency Lighting > ORD - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAA990039](https://openairdocs.org/sdr/USAA990039.md): Skin · cracked · Jan 14, 1999 · N236US · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAASB98167](https://openairdocs.org/sdr/USAASB98167.md): Seal · out of position · Jul 2, 1998 · N236US · Boeing 737201 · Service Doors > PIT - 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. PRESS - [SDR USAASB98153](https://openairdocs.org/sdr/USAASB98153.md): Engine · overtemp · Jun 21, 1998 · N236US · Boeing 737201 · Engine (Turbine/Turboprop) > PIT - 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 E - [SDR USAASB98035](https://openairdocs.org/sdr/USAASB98035.md): Anti-Ice Duct · leaking · Feb 10, 1998 · N236US · Boeing 737201 · Air Intake Anti/De-Ice System > TPA - 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 AT - [SDR USAASB98025](https://openairdocs.org/sdr/USAASB98025.md): Windshield · defective · Jan 30, 1998 · N236US · Boeing 737201 · Flight Compartment Windows > ORF - 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 - [SDR USAA970303](https://openairdocs.org/sdr/USAA970303.md): Skin · cracked · Oct 24, 1997 · N236US · Boeing 737201 · Passenger/Crew Doors > ROA - 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) - [SDR USAA970302](https://openairdocs.org/sdr/USAA970302.md): Skin · cracked · Oct 24, 1997 · N236US · Boeing 737201 · Fuselage Main, Plate/Skin > ROA - 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) - [SDR USAASB96175](https://openairdocs.org/sdr/USAASB96175.md): Battery Pack · failed · Aug 31, 1996 · N236US · Boeing 737201 · Emergency Lighting > CLT - 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) - [SDR USAASB96171](https://openairdocs.org/sdr/USAASB96171.md): Light Ballast · burned · Aug 30, 1996 · N236US · Boeing 737201 · Passenger Compartment Lighting > IAH - 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 E - [SDR USAA960568](https://openairdocs.org/sdr/USAA960568.md): Floor Beam · cracked · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor Beam > INT - 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) - [SDR USAA960567](https://openairdocs.org/sdr/USAA960567.md): Floor Beam · cracked · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor Beam > INT - 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) - [SDR USAA960565](https://openairdocs.org/sdr/USAA960565.md): Floor Beam · broken · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor Beam > INT - 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) - [SDR USAA960564](https://openairdocs.org/sdr/USAA960564.md): Stringer · corroded · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/Stringer > INT - 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) - [SDR USAA960563](https://openairdocs.org/sdr/USAA960563.md): Floor Beam · corrosion · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Floor Beam > INT - 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- - [SDR USAA960562](https://openairdocs.org/sdr/USAA960562.md): Stringer · cracked · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/Stringer > INT - 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) - [SDR USAA960561](https://openairdocs.org/sdr/USAA960561.md): Angle · corrosion · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Miscellaneous Structure > INT - 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) - [SDR USAA960560](https://openairdocs.org/sdr/USAA960560.md): Beam · corroded · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Miscellaneous Structure > INT - 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- - [SDR USAA960559](https://openairdocs.org/sdr/USAA960559.md): Stringer · cracked · Aug 22, 1996 · N236US · Boeing 737201 · Fuselage Main, Longeron/Stringer > INT - 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) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N236US-2000-08-11/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.