30001 Fuselage Installation

This 102-31034-1 Skin is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang aircraft.Part Number:...

This 102-310317 Cover Assy - Fuselage Oil Cooler is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang...

This 102-310295-1 Intercostal - Coolant Door is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang aircraft...

This 102-310265 Cover - Access Door - Aft Scoop is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang...

This 109-31541-10 Former Assy - Engine Removable is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51D and preceding applicable Mustang aircraft.Part Number:...

This 102-310222 Stud - Fuselage Carb Air Duct is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang aircraft...

This 102-310118 Cover Assy - Coolant Radiator is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang aircraft...

This 102-31071-42 Seal is in NS condition designed and engineered by North American Aircraft in the 1940's using original manufacturing methods and materials for the P-51B, P-51C, and P-51D and preceding applicable Mustang aircraft.Part Number:...

FAA-PMA approved design and ready for install.Part Number: 73-33578-TU - Take Up Spring As a preventative measure and safety enhancement, AirCorps recommends the installation of a spring between the retract rod and the extrusion in the gear well on the...

Drawing available on AirCorps Library https://app.aircorpslibrary.com/Drawing/Viewer/109-31669/

Drawing available on AirCorps Library https://app.aircorpslibrary.com/Drawing/Viewer/106-318220/