- Registered owner
- 4y-2 LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- 66302
- Year built
- 1945
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, exhibition
- Airworthiness date
- May 26, 1959
- Certificate issued
- January 10, 2008
- Expires
- April 30, 2029
- Mode S code
- A2EA7E
Consolidated Vultee P4Y-2TCDS TC AR-29Airframe · Consolidated Vultee P4Y-2Engine modelWright R-2600-35
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
Airframe · Consolidated Vultee P4Y-2
AD 2003-18-01Wing front sparSuperseded and historical ADs · 1
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N2871GMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Consolidated Vultee P4Y-2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N2871GMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Consolidated Vultee P4Y-2 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR KGBR2010072300003Rod Bearing · failed(KGBR) AFTER TAKEOFF AND UPON CLIMB TO ALTIUDE, THE NR 2 ENGINE OIL PRESSURE DROPPED RAPIDLY AND THE ENGINE OIL TEMPATURE INCREASED RAPIDLY. THE FLIGHT CREW IMMEDIATELY SHUTDOWN THE ENGINE AND RETURNED TO THE AIRPORT. UPON INVESTIGATION BY THE MX CREW, IT ISSDR 2007002Spar Cap · crackedWHILE PERFORMING AD 2003-18-01, CRACKS WERE FOUND UNDER THE LT LOWER, FWD, SPAR CAP DOUBLER IN THE CAP, SPAR WEB AND THE DOUBLER ITSELF. CRACKS WERE ALSO FOUND IN THE WING SKIN CUTOUTS AT ALL 4 LOWER CENTER WING BELT FRAME CUT-OUTS. RT FWD LOWER SPAR CAP CRACSDR 200700105Spar Cap · crackedWHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING. THE MAJOR CRACK IS A 1.5 INCH CRACK IN THE FWD LT LOWER SPAR CAP AFT ANGLE AT THE WING ATTACH POINT TO THE BELT FRAME. THE CRACK IS IN THE ANGLE (SPAR CAP AFT LEG), DOUB
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.