The auxiliary power unit Model GTC 85-71 located in the forward end of the left hand main landing gear wheel well fairing has been replaced by an AiResearch Gas turbine compressor Model GTCP85-98CK(A).

Please contact modification supplier for further details.

STC Status: Reissued
STC Date: 05/06/03
Responsible Office: Atlanta Aircraft Certification Office (ACE-115A), Tel: (404) 474-5500

Lockheed Aircraft Corporation

• 382E
• 382F
• 382G