DG Flugzeugbau LS4 Maintenance Manual page 115

Annual inspection checklist
Page 2 of 3
Serial No.:
Canopy
S/N: ________
Locking mechanism
Emergency release funct.
Window
Ventilation system
Canopy opener fixing
Gas strut operation
LS latch (for jettison)
Lift force:____ (8-15 kg)
(18-33 lbs)
Rudder
Finish condition
Shell
Ventilation openings
Drive
Fixed bearing + washer
Bearings
Connecting means
Landing gear
Undercarriage + axle
Tyre
Springing
Bearings + joints
Folding strut overcenter
Gas strut
Folding strut preset load
Doors
Drive rods
Cockpit locking -
Connecting means
Wheel brake system
C.G. hook + drive
Ground conn. to contr. stick
Baggage comp. cover
Oxygen bottle receptacle
Fixed ballast at front/rear
Place: _________ Date: ________ Stamp: __________ Signature: _______________
Issued: May 2011
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
Maintenance Manual LS4
Reg. Signs:
Equipment
Minimum instrumentation
Additional Instrumentation
Operating range marks
Limit marks
Vacuum flasks
Pneumatic tubing
Instruments functioning
Total energy unit
Systems free from leaks
Total pressure
Static pressure
T.E. system
Electrical wiring
Battery + fitting
Battery main fuse
Tail fin battery
Tail fin battery main fuse
Radio operation
Antenna system
SWR: ______
Communication check
Tow Hooks
C.G. hook
-Function + automatic rel.
-S/N: __________
-Op.Limit: __________
Nose hook function
-S/N: __________
-Op.Limit: ___________
Release cable end play
existent with gear down
Data placard
Placards accord. to Maint.
Manual
Compass deviation list
Adjustments
Wings and horizontal tail
Tangential play
Zero position of controls
Year of Manuf.:
Adjustments cont.
Control surface deflections
according to section 5
Air brake extension min.,
147 mm inboard
Air brake locked, lateral gap
min. 1 mm at inner end
min.2.5 mm at outer end
Air brake locked, cockpit
Lever min. 6mm from
stop #
Control surface friction
Control surf. rear edge play
Landing gear locking
Trim system function
Harness condtion
Multiple point buckle funct.
Op.Limit: ___________
Ballast system function
Absolutely tight?
General
Registration signs
Nationality marks
Fireproof type placard
External colour marking
Checklist
Minimum cockpit load
Flight Manual
Maintenance Manual
TN-AD status
TB-AD-List up to date
Certificate of Airworthiness
Logbook notation
Placard notations
Non-exist. of foreign matter
Wings flex number (support
fuselage in front of landing
gear) ________ / Minute
14-2