BRISTELL S-LSA, Руководство по техническому обслуживанию и инспекции

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6. CHAPTER - CONTROLS
Document: SLSA-MIP-5-4-0-US Date of Issue: 05/2016 Revision: -
6-15
Check condition and lubrication of bail arm lever bushings. If the bushing is
contaminated, then carefully remove contamination and grease it with lubricant grease.
Set the bail arm lever (3) to the position (see Fig. 6-12), insert the bolt into the hole in
the lever and the hinge (4) and secure it with the castle nut and cotter pin. Tighten the
nut slightly.
NOTE
The lever after installing must not show axial play and its travel must be smooth without
hitching.
Connect both push rod ends (2) with the bail arm lever (3).
Close the access hole on the bottom skin under the luggage compartment.
Check elevator deviations (see 6.4.3.3) and check control plays (see 6.4.1.2).
6.3.14 Removal of bail arm in rear fuselage
Type of maintenance: heavy
Authorization to perform:
LSA mechanic or A&P mechanic (Airframe and Power plant)
Tools needed:

wrench size 7/16 in (11)

Phillips screwdriver

pliers
Attachment of bail arm is shown in Fig. 6-13.
Unscrew the access hole cover (1) attachment screws on the starboard side of the
fuselage in front of the fin spar.
Disconnect push rod ends (2) from the arm (3)
– unscrew the nuts and remove the bolts
(4).
Remove arm (3) from bracket (5)
– remove cotter pin (8), unscrew the castle nut (7),
and remove bolt (6).
Fig. 6-13
Bail arm in rear fuselage
1 - Access hole cover 2 - Rod end
3 - Bail arm 4 - Bolt
5 - Bracket 6 - Bolt
7 - Castle nut 8 - Cotter pin
9 - Nut