# N224US: 2025 Costruzioni Aeronautiche Tecna P2008 - Status: Valid registration - Airframe: [Costruzioni Aeronautiche Tecna P2008](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2008) (registry code 060007Q, 2 seats) - Engine: [Rotax 912ULS2](https://openairdocs.org/engine/rotax-912uls2) (registry code 55599) - Serial number: 224 - Year built: 2025 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Light sport, airplane - Airworthiness date: October 24, 2025 - Certificate issued: August 28, 2026 - Expires: August 31, 2033 - Mode S code: A1F1B0 - Registered owner: [Vector Flight Leasing LLC](https://openairdocs.org/faa-owner/VECTOR%20FLIGHT%20LEASING%20LLC) - Location: [Cumming, GA](https://openairdocs.org/faa-place/GA/Cumming) - Owner type: LLC - Owner's area on the map: 34.2233° N, 84.1755° W: Placed by OpenAirDocs at the center of ZIP code 30040, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=224US - Page: https://openairdocs.org/aircraft/N224US 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 (Costruzioni Aeronautiche Tecna P2008) None in force. ### Matched by engine (Rotax 912ULS2) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N224US. ## FAA accident and incident reports None matched to N224US. ## Reports on N224US not matched to an aircraft (1) They name N224US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19960319009709I](https://openairdocs.org/incident/19960319009709I), Mar 19, 1996: Boeing 737201 (N224US), Greensboro, NC. Narrative: while departing from Piedmont Triad International Airport, Greensboro, NC the control tower noticed fire in the one engine. The crew was informed… ## 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 N224US not matched to an aircraft (43) They name N224US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR USAA000664](https://openairdocs.org/sdr/USAA000664), May 4, 2000: SKIN. CRACKED. TPA - FOUND SKIN CRACKED .25 INCH, AFT ENTRY DOOR UPPER HINGE CUTOUT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 21A. (M) - [SDR USAA000649](https://openairdocs.org/sdr/USAA000649), May 1, 2000: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 1.24 INCH AND 1.7 INCH, BS 727A PLUS 3 INCHES, STRINGER 18L AND BS 727A PLUS 2 INCHES. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAA000648](https://openairdocs.org/sdr/USAA000648), May 1, 2000: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 1.25 INCH, STATION 727A PLUS 6 INCHES, STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3. (M) - [SDR USAASB00103](https://openairdocs.org/sdr/USAASB00103), Apr 4, 2000: CHARGER. FAILED. BNA - PILOT REPORTED THAT THE EMERGENCY PATH LIGHTS ILLUMINATED ON 4 ROWS IN THE CABIN. MAINTENANCE CYCLED CIRCUIT BREAKERS FOR TR1, 2 AND 3. OPERATIONAL CHECK - [SDR USAASB00100](https://openairdocs.org/sdr/USAASB00100), Mar 27, 2000: BATTERY PACK. INOPERATIVE. PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT OVER THE FIRST CLASS SECTION IS FLASHING. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY PACK AT SEAT ROW 2. - [SDR USAA000191](https://openairdocs.org/sdr/USAA000191), Feb 11, 2000: SKIN. CRACKED. CLT - FOUND SKIN WITH 1 INCH CRACK, BS 755, STRINGER 18R, RT FUSELAGE SKIN. CUTOUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1. (M) - [SDR USAASB99273](https://openairdocs.org/sdr/USAASB99273), Nov 18, 1999: POWER SUPPLY. FAILED. CLT - PILOT REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY WITH SWITCH IN AUTO POSITION OR OFF POSITION. MAINTENANCE FOUND THE AFT FLIGHT ATTENDAN - [SDR USAA990139](https://openairdocs.org/sdr/USAA990139), Feb 25, 1999: SKIN. CRACKED. CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK IN FUSELAGE SKIN BS 727A PLUS 19 INCHES S18R. INSTALLED DOUBLER PER SRM 53-30-03. (M) - [SDR USAASB98276](https://openairdocs.org/sdr/USAASB98276), Oct 19, 1998: SERVO. FAILED. CLT - FLT 357 - DURING CRUISE AT FL330 WITH AUTOTHROTTLE ENGAGED, NR 1 THROTTLE BEGAN MOVING 1 OR 2 INCHES IN EITHER DIRECTIONS. POWER WAS CHANGING WITH THROTTL - [SDR USAA980415](https://openairdocs.org/sdr/USAA980415), Sep 16, 1998: SKIN. CRACKED. CLT - DURING RON CHECK VISUAL WITH EDDY CURRENT INSPECTION, VERIFIED A 2 INCH CRACK ON SKIN STA 787 BETWEEN STR 22L AND STR 23L. INSTALLED NEW FILLER AND DOUBLE - [SDR USAA980397](https://openairdocs.org/sdr/USAA980397), Sep 5, 1998: SKIN. CRACKED. PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 3.75 INCH CRACK ON SKIN BETWEEN STATION 771 AND 775 2 INCH ABOVE STRINGER 17L. FOUND 5.5 INCH CRACK ON SKIN BETWEEN - [SDR USAASB98180](https://openairdocs.org/sdr/USAASB98180), Jul 12, 1998: LIGHT. INOPERATIVE. ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT IN THE COCKPIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) - [SDR USAA980173](https://openairdocs.org/sdr/USAA980173), Apr 23, 1998: SKIN. CRACKED. CLT - DURING PILOTS REPORT A 2.75 INCH CRACK WAS FOUND IN THE SKIN BS 759-761.75 STRINGER 24L. INSTALLED FILLER AND DOUBLER PER REPAIR DOCUMENT SRM 53-30-3 FIG - [SDR USAASB97329](https://openairdocs.org/sdr/USAASB97329), Nov 26, 1997: BATTERY PACK. DISCHARGED. PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTING AT THE AFT ENTRY AND AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHEC - [SDR USAASB97292](https://openairdocs.org/sdr/USAASB97292), Oct 20, 1997: BATTERY PACK. DISCHARGED. LGA - AFT SERVICE AND ENTRY DOOR EMERGENCY LIGHT EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY CHARGING UNIT. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97260](https://openairdocs.org/sdr/USAASB97260), Sep 19, 1997: BATTERY PACK. DISCHARGED. TPA - AFT EXTERIOR ESCAPE LIGHTS AT R2 AND L2 DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE LEFT REFLECTOR AND BATTERY PACK (61-0478-9). OPERATIONAL CHECK SYS - [SDR USAASB97259](https://openairdocs.org/sdr/USAASB97259), Sep 19, 1997: BATTERY PACK. DISCHARGED. TPA - EMERGENCY LIGHTS AFT GALLEY (LOWER INSIDE) INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97226](https://openairdocs.org/sdr/USAASB97226), Aug 18, 1997: BATTERY PACK. DISCHARGED. ALB - BOTH INSIDE AFT ESCAPE SLIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAASB97131](https://openairdocs.org/sdr/USAASB97131), May 15, 1997: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATION CHECK GOOD. (M) - [SDR USAA960665](https://openairdocs.org/sdr/USAA960665), Oct 4, 1996: FRAME. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACKED FRAME .75 INCH LONG STATION 727 JUST BELOW STRINGER 13L. INSTALLED REPAIR DOUBLERS, REPAIRED PER EA 5148 - [SDR USAA960664](https://openairdocs.org/sdr/USAA960664), Oct 4, 1996: STRINGER. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG 1 INCH WIDE BS 1003 TO BS 1014 STRINGER. REMOVED DAMAGE AND FABRICATED REPAIR, REPAIRED PER SRM 53-1 - [SDR USAA960663](https://openairdocs.org/sdr/USAA960663), Oct 4, 1996: KEEL BEAM. DAMAGE. INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND THREE ACCESS PLATE MOUNTING FLANGE HOLES DAMAGED IN KEEL BEAM, RIGHT SIDE KEEL BEAM LOWER CHORD OUTBOARD FLANGE F - [SDR USAA960658](https://openairdocs.org/sdr/USAA960658), Sep 27, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .75 INCH CRACKS, LBL 25 INCHES LONG FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED DOUBLER, REPAIRE - [SDR USAA960657](https://openairdocs.org/sdr/USAA960657), Sep 27, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKS BL 0 INCH LONG FLOOR BEAM WEB STATION 707 TO STATION 712, WL 203.5. INSTALLED REPAIR WEB, RE - [SDR USAA960656](https://openairdocs.org/sdr/USAA960656), Sep 27, 1996: SKIN. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK EXTERNAL SKIN DOUBLER FORWARD SERVICE DOOR LOWER HINGE. INSTALLED NEW DOUBLER, REPAIRED PER TR 5 - [SDR USAA960655](https://openairdocs.org/sdr/USAA960655), Sep 27, 1996: SKIN. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK CORNER OF HINGE CUT OUT FORWARD SERVICE DOOR SKIN. INSTALLED DOUBLER, REPAIRED PER TR 52-40-03A. - [SDR USAA960654](https://openairdocs.org/sdr/USAA960654), Sep 27, 1996: STUB BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 597 STUB BEAM WEB RBL 60 TO RBL 62, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. - [SDR USAA960653](https://openairdocs.org/sdr/USAA960653), Sep 27, 1996: BULKHEAD. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLER, REPAIRED PER DRAWING - [SDR USAA960652](https://openairdocs.org/sdr/USAA960652), Sep 27, 1996: BULKHEAD. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLERS, REPAIRED PER DRAWING - [SDR USAA960651](https://openairdocs.org/sdr/USAA960651), Sep 27, 1996: FRAME. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN CIRCUFERENTIAL FRAME STATION 328 3 INCHES BELOW STRINGER STRINGER 20R. FABRICATED 707576 .040 MA - [SDR USAA960650](https://openairdocs.org/sdr/USAA960650), Sep 27, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACKS IN FOUR PLACES, RBL 25 INCHES LONG, FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED WEB RE - [SDR USAA960649](https://openairdocs.org/sdr/USAA960649), Sep 27, 1996: SUPPORT CHANNEL. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRCK RBL 45 SEAT TRACK SUPPORT CHANNEL ABOVE UPPER INBOARD BOLT. INSTALLED DOUBLERS, REPAIRED PER EA 414 - [SDR USAA960648](https://openairdocs.org/sdr/USAA960648), Sep 27, 1996: WEB. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO CRACKS 1 INCH BY 3 INCH CREASE BEAM WEB 2 INCHES AFT OF STATION 639 PLUS 1 INCH FORWARD OF STATION 663 FRAME - [SDR USAA960647](https://openairdocs.org/sdr/USAA960647), Sep 27, 1996: SUPPORT CHANNEL. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LBL BS 520, WL 207.5 SUPPORT CHANNEL. FABRICATED DOUBLER CHANNEL RADIUS FILLERS, INSTALLED CHANNEL - [SDR USAA960646](https://openairdocs.org/sdr/USAA960646), Sep 27, 1996: STRINGER. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACKS EMITTING FROM FASTENER HOLES (2) STRINGER 15L BS 525. CHANNEL REPAIR INSTALLED ON STRINGER, REP - [SDR USAA960645](https://openairdocs.org/sdr/USAA960645), Sep 27, 1996: STUB BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 578 STUB BEAM WEB LBL 61.5 TO LBL 62.5, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51- - [SDR USAA960644](https://openairdocs.org/sdr/USAA960644), Sep 27, 1996: FRAME. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG CRACK STATION 747 STRINGER 19 L CIRCUMFERENTIAL FRAME. INSTALLED DOUBLERS, REPAIRED PER SRM 53-10-4. - [SDR USAA960643](https://openairdocs.org/sdr/USAA960643), Sep 27, 1996: STRINGER. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 1 INCH BY 3 INCH SECTION AROUND RIVETS, BS 363 TO BS 500 PLUS 13 INCHES. REPLACED STRINGER - [SDR USAA960642](https://openairdocs.org/sdr/USAA960642), Sep 27, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 675 WL 202.5 LONGITUDINAL FLOOR BEAM LOWER CHORD. INSTALLED REINFORCING ANGLE/SPLICE, REPAIRE - [SDR USAA960641](https://openairdocs.org/sdr/USAA960641), Sep 27, 1996: FLOOR BEAM. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK RBL 45 LONG FLOOR BEAM LOWER CHORD STATION 695 WL 202.5. INSTALLED REPAIR ANGLE, REPAIRED PER EA - [SDR USAASB96048](https://openairdocs.org/sdr/USAASB96048), Mar 19, 1996: ENGINE. FAILED. GSO - FL 8028 - AT APPROXIMATELY 600 FEET AGL AFTER TAKEOFF FROM GSO, THE LEFT ENGINE EXPLODED. TOWER ADVISED CREW THAT ENGINE WAS TRAILING SMOKE AND FIRE. FLIG - [SDR USAASB96020](https://openairdocs.org/sdr/USAASB96020), Jan 26, 1996: GASPER FAN. FAILED. CHS - EN ROUTE MCO-IAD - CREW NOTED ELECTRICAL IN SMELL IN CABIN. FLIGHT DIVERTED TO CHS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE GASPER FA - [SDR USAA951235](https://openairdocs.org/sdr/USAA951235), Nov 22, 1995: STRINGER. CORROSION. ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 30 INCH BY 2 INCH CORROSION AT STRINGER 27 LEFT BS 947 TO 977. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. (M ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Costruzioni Aeronautiche Tecna P2008 aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2008/aircraft.md - The Rotax 912ULS2 engine: https://openairdocs.org/engine/rotax-912uls2.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.