# N262AT: Quicksilver Manufacturing SPORT I - Status: Valid registration - Airframe: [Quicksilver Manufacturing SPORT I](https://openairdocs.org/model/quicksilver-manufacturing-sport-i) (registry code 05902RO, 1 seats) - Engine: [Suzuki G10](https://openairdocs.org/engine/suzuki-g10) (registry code 59299) - Serial number: 001 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Experimental, registered before 01/31/08 - Airworthiness date: January 28, 2008 - Certificate issued: June 6, 2007 - Expires: July 31, 2027 - Mode S code: A2867D - Registered owner: [Abreu Orlando](https://openairdocs.org/faa-owner/ABREU%20ORLANDO) - Location: Adjuntas, PR, RQ - Owner type: Individual - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=262AT - Page: https://openairdocs.org/aircraft/N262AT From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Quicksilver Manufacturing SPORT I) None in force. ### Matched by engine (Suzuki G10) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N262AT. ## FAA accident and incident reports None matched to N262AT. ## Reports on N262AT not matched to an aircraft (1) They name N262AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19970613045649I](https://openairdocs.org/incident/19970613045649I), Jun 13, 1997: Aerosp ATR42300 (N262AT), Fort Wayne, IN, Minor damage. (-5) Windshield cracked in flight (outside layer only, windshield did not fall out). Aircraft deverted to fwa and landed without incident. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N262AT not matched to an aircraft (26) They name N262AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR SVU2004F00002](https://openairdocs.org/sdr/SVU2004F00002), Dec 31, 2003: CONVERTER. INTERMITTENT. FDAU FAULT. (WO NR 34225) - [SDR 2001F00106](https://openairdocs.org/sdr/2001F00106), Jun 2, 2001: GEAR SHAFT. SHEARED. AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUT DOWN AND AIRCRAFT DIVER - [SDR 2001F00105](https://openairdocs.org/sdr/2001F00105), Jun 2, 2001: GEAR SHAFT. SHEARED. AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERT - [SDR 2000ZZZM14](https://openairdocs.org/sdr/2000ZZZM14), Oct 26, 1999: BATTERY PACK. DISCHARGED. EMERGENCY BATTERY LOW VOLTAGE AT STATION 10WL, 10WL, 15WL, AND 29WL. REMOVED AND REPLACED BATTERY PACK 10WL, 18WL, 15WL AND 29WL AS PER MM 33-50-00. (M) - [SDR SIMA973511](https://openairdocs.org/sdr/SIMA973511), Dec 18, 1997: THRESHOLD. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LAVATORY THRESHOLD CORRODED OUT OF LIMITS AT FRAME 39. MAINTENANCE REMOVED AND REPLACED THRESHOLD IAW - [SDR SIMA973494](https://openairdocs.org/sdr/SIMA973494), Dec 15, 1997: SKIN. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE PASSENGER CREW DOOR INNER SKIN CORRODED AT BOTTOM SIDE. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 5 - [SDR SIMA973493](https://openairdocs.org/sdr/SIMA973493), Dec 15, 1997: ZEE MEMBER. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE RIGHT AFT ZEE MEMBER BETWEEN FRAME 39 AND FRAME 41 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND IN - [SDR SIMA973492](https://openairdocs.org/sdr/SIMA973492), Dec 15, 1997: FLOOR BEAM. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW - [SDR SIMA973491](https://openairdocs.org/sdr/SIMA973491), Dec 15, 1997: SEAT TRACK. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED - [SDR 98ZZZX74](https://openairdocs.org/sdr/98ZZZX74), Dec 15, 1997: SEAT TRACK. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED - [SDR 98ZZZX73](https://openairdocs.org/sdr/98ZZZX73), Dec 15, 1997: SEAT TRACK. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED - [SDR 98ZZZX72](https://openairdocs.org/sdr/98ZZZX72), Dec 15, 1997: SEAT TRACK. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED - [SDR 98ZZZX71](https://openairdocs.org/sdr/98ZZZX71), Dec 15, 1997: FLOOR BEAM. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW - [SDR 98ZZZX70](https://openairdocs.org/sdr/98ZZZX70), Dec 15, 1997: FLOORBEAM. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW - [SDR 98ZZZX69](https://openairdocs.org/sdr/98ZZZX69), Dec 15, 1997: FLOOR BEAM. CORRODED. SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW - [SDR SIMA972134](https://openairdocs.org/sdr/SIMA972134), Aug 1, 1997: POWER SUPPLY. INOPERATIVE. ORD - FLT 4341 - FORWARD FLOOR EMERGENCY LIGHT INOP. RAI'D EMERGENCY POWER SUPPLY AND BATTERY PACK OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA972031](https://openairdocs.org/sdr/SIMA972031), Jul 22, 1997: BULB. LOOSE. MSN - FLT 4046 - FORWARD NR 1 FLOOR PROXIMITY LIGHT INOPERABLE. ITEM MEL'D PER 33-22 AND AIRCRAFT RETURNED TO SERVICE. ON OVERNIGHT VISIT, FOUND LIGHT BULB LOOS - [SDR SIMA9701871](https://openairdocs.org/sdr/SIMA9701871), Jul 6, 1997: BATTERY PACK. DISCHARGED. ORD - FLT 4034 - REMOVED AND REPLACED BATTERY PACK AT 10W1. PERFORMED SYSTEM OPS CHECK AND RETURNED AIRCRAFT TO SERVICE. (X) - [SDR SIMA9701341](https://openairdocs.org/sdr/SIMA9701341), May 14, 1997: LIGHTS. INOPERATIVE. PIA - FLT 4144 - EMERGENCY FLOOR LIGHT ROW 2, 3, AND 5 INOP. CHECK EMERGENCY FLOOR LIGHTING, DEFERRED PER SIMMONS MEL 33-22. AIRCRAFT WAS RETURNED TO SERVICE. M - [SDR SIMA9700071](https://openairdocs.org/sdr/SIMA9700071), Jan 7, 1997: POWER SUPPLY. FAILED. ORD - FLT 4147 - FORWARD EMERGENCY EXIT SIGNS ARE INOP. REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA963511](https://openairdocs.org/sdr/SIMA963511), Dec 16, 1996: PRESS SWITCH. FAILED. ORD - FLT 4171 - CREW REPORTED AN AIRFRAME/AIRBLEED FAULT FOLLOWED BY A HYDRAULIC LOW PRESSURE AND AN ACRIC SMELL IN THE COCKPIT. RAI'D AIRFRAME AIRBLEED PRESSU - [SDR SIMA963441](https://openairdocs.org/sdr/SIMA963441), Dec 9, 1996: BOLT. BROKEN. MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND THE LEFT MAIN LANDING GEAR ACTUATOR BRACKET FORWARD LOWER BOLT BROKEN OFF. MAINTENANCE REMOVED AND REPLAC - [SDR SIMA963324](https://openairdocs.org/sdr/SIMA963324), Nov 27, 1996: TRUNNION LEG. FAILED INSP. ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IA - [SDR SIMA953141](https://openairdocs.org/sdr/SIMA953141), Nov 10, 1995: EEL. INOPERATIVE. RFD - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW JIC 33512-0 - [SDR SIMA951022](https://openairdocs.org/sdr/SIMA951022), Apr 12, 1995: CONTROL ROD. CORRODED. MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE RUDDER TAB CONTROL ROD APPEARED TO BE CORRODED ON INTERNAL ROD. THE ROD WAS REMOVED AND CLEANED OF CORROSI - [SDR SIMA951021](https://openairdocs.org/sdr/SIMA951021), Apr 12, 1995: BELL CRANK. CORRODED. MQT - MAINTENANCE REPORTED THE RIGHT AILERON BELL CRANK JUST OUTBOARD OF FLAP, AFT BEARING CORRODED. THE BELL CRANK WAS REMOVED AND REPLACED AND OPS TEST GOOD. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Quicksilver Manufacturing SPORT I aircraft: https://openairdocs.org/model/quicksilver-manufacturing-sport-i/aircraft.md - The Suzuki G10 engine: https://openairdocs.org/engine/suzuki-g10.md --- 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.