AD/MU-2/32 - Replacement of Series Relay and Modification to the Two Battery System
1AD/MU-2/32 - Replacement of Series Relay and Modification to the Two Battery System
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/MU-2/32 - Replacement of Series Relay and Modification to the Two Battery System.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/32 Replacement of Series Relay and Modification
to the Two Battery System
Applicability: MU-2B (Airplanes with MU-2 Series Bulletin No. 093 incorporated).
2/84
MU-2B-20 (S/N 124, 165 through 169, 171 through 181, 183 through 222 and 233).
MU-2B-30 (S/N 502, 505 through 508 and 510 through 547).
Document: Mitsubishi SB 156 dated 3 August 1972 and Japan Civil Aviation Bureau AD No.
TCD-859-72 dated 4 September 1972.
Compliance: Before issue of Australian Certificate of Airworthiness.
Background: Advice from manufacturer of possibility that excessive arcing will occur in series relay of the two battery system, resulting in possible damage to the aircraft.