Installation of Litton LCD engine instruments to replace original electro- mechanical production engine instruments.
Installation of a No. 1 emergency power supply system.
Installation of a No. 2 emergency power supply system.
Relocate of engine start/ windshield wiper controls.
Increase in zero fuel weight to 46,000 pounds for airplanes having ASC 70, Parts I and II.
Installation of Intercontinental Dynamics engine parameter indicator P/N 585-37805-001.
Installation of Safe Flight fuel performance computer.