- Registered owner
- Yanks Air Museum
- Location
- Baldwin Park, CA
- Owner type
- Corporation
- Serial number
- 66300
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Restricted, agriculture and pest control, forest
- Airworthiness date
- July 20, 1960
- Certificate issued
- August 26, 2022
- Expires
- August 31, 2029
- Mode S code
- A2EAA1
Consolidated Vultee P4Y-2TCDS TC AR-29Airframe · Consolidated Vultee P4Y-2Engine modelWright C14AB AC BA
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 N2872GMatched 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 N2872GMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007001Spar 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 200600083Spar Cap · crackedWHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING. THE MAJOR CRACK IS A 4-5 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.