Installation of Systron-Donner Model 8160-20-P10 angular rate sensor in lieu of presently installed rate gyros in pitch- axis computer, roll-axis computer, and stability augmentation computers.
Installation of Systron-Donner Model 8160-20-P10 angular rate sensor in lieu of presently installed rate gyros in pitch- axis computer, roll-axis computer, and stability augmentation computers.
Please contact modification supplier for further details.
STC Status: Issued
STC Date: 23/07/76
Responsible Office: Chicago Aircraft Certification Office (ACE-115C), Tel: (847) 294-7358
McDonnell Douglas Corporation