STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 62
MAINTENANCE MANUAL STEMME S12
During lifting and lowering of the aircraft, the wing chord should remain almost horizontal.
The fuselage with wing removed should be supported
• either in a felt-covered, adapted rigid tray, width 1 m / 3.28 ft and length 0.4 m / 15.75 in
directly in front of the landing gear doors, or
•
by removing the front wing attachment bolts and by replacing the bolts by round steel
bars of St 37 or similar, Ø 19.8 ± 0.1 mm / 0.78 ±.004 in, 0.30 m / 11.81 in length. The steel
bars must be inserted by 0.15 m / 5.91 in and must be secured against displacement. The
fuselage can be suspended or supported at these bolts.
For rigging and derigging refer to the S12 Aircraft Flight Manual, chapter 4.
For transport refer to the S12 Aircraft Flight Manual, chapter 8.

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English