MAINTENANCE MANUAL
STEMME TSA-M
MAINTENANCE MANUAL
STEMME TSA-M
(10) Replace damaged items.
(11) Install engine cowling (refer to 72-10-00).
(12) Perform an engine test run (refer to 05-20-00).
D. Violent Stop of the Engine
In event that the propeller was touching ground or the engine was inadvertently stopped
violently (shock loading) the engine with the propeller gear box must be disassembled and
inspected by an authorized workshop.
CAUTION: ONLY QUALIFIED TECHNICIANS (AUTHORIZED BY AVIATION AUTHORITY
AND AFTER SUCCESSFUL ATTENDANCE OF THE RELEVANT ROTAX
TRAINING COURSE) ARE AUTHORIZED TO PERFORM THIS WORK.
Check additional equipment (external alternator, hydraulic governor, ignition unit, coolant and oil
hoses) for damage.
Page 202
05-50-00
UNSCHEDULED MAINTENANCE CHECKS
1. General
A. Special checks are to be carried out only in circumstances, outside routine inspections, where
event have occurred that may have caused damage to the aircraft or an impairment of
airworthiness possibly during the operation of the aircraft.
Furthermore, the 25-hour inspection necessary for a newly delivered aircraft and its engine, as
well as for overhauled engines and after extensive airframe repairs, falls under the special checks
since it must only be carried out once after the first 25 hours of operation of the aircraft.
2. Special Checks
A. 25-Hour Inspection
After the first 25 hours of operation an inspection within the specifications of a 100-hour
inspection is to be completed (Refer to 05-20-00).
B. Hard Landing Concerning the Landing Gear and Tail Boom
After an excessively hard landing or other unusual loads of the landing gear a thorough inspection
of the affected components and their attachment is required. Even if no obvious defects are
detectable, a visual inspection must be carried out. Examination contains parts of 100 hours
inspection listed in the STEMME S6 Inspection Time Intervals Chart (Refer to section "Scheduled
Maintenance Checks" of this chapter) concerning the landing gear.
C. Engine Fire
After an engine fire perform the following steps:
WARNING: IF SUSPECTED THAT PARTS OF THE STRUCTURE OR OF THE COWLING AS
WELL AS THE MAIN LANDING GEAR DOORS WOULD BE ABLE TO HAVE
BEEN DAMAGED BY THE HIGH TEMPERATURES (DETECTABLY AMONG
OTHER THINGS BY BLISTERING ON THE PROTECTIVE COATING), THE
MANUFACTURER IS TO BE CONTACTED FOR THE APPRAISAL OF THE
DEFECTS BEFORE THE AIRCRAFT IS PUT INTO OPERATION AGAIN.
(1) Disconnect battery (refer to 24-30-00).
(2) Remove engine cowling (refer to 72-10-00).
(3) Examine engine cowling. Check for signs of fire damage.
(4) Examine electrical cables for damaged insulation.
(5) Examine fuel lines for damage of the fire-protection sleeves.
(6) Check oil lines for damage of the fire-protection sleeves.
(7) Check air filter element for fire damage.
(8) Examine engine mount and shock mounts for any fire damage.
(9) Check landing gear hydraulic system (hydraulic hoses, actuators, pressure
05-50-00
Page 201
Nov 18/11
Nov 18/11
EFFECTIVITY
Model S6-RT
To Next Page
Loading...
Need help?
General
