Raytheon Beechcraft Bonanza 35 Series, Руководство по ремонту

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BONANZA 35 SERIES SHOP MANUAL
Page 12
Aug 29/03
B21
Section 7
B. POWER PLANT (Continued) MECH INSP
f. Inspect the upper deck pressure reference lines and the fuel injection reference
manifold for loose connections, leaks and possible chafing.
g. Check and calibrate the turbine inlet temperature indicator.
h. Check manifold pressure controller linkage for wear.
49. FILTERS - Inspect pressure system in-line filter for condition, cleanliness and security.
Refer to Parker-Hannifin Airborne Service Letter 59 or subsequent. Refer to Section 8
for additional information.
50. PRESSURE PUMP (Airborne) - Inspect as required by Parker - Hannifin Service Letter
43A or subsequent. Refer to Section 8 for additional information.
PRESSURE PUMP (Aero Accessories Pump Part Number AA216CW) - Initially inspect
at 600 hours time-in-service in accordance with Aero Accessories Service Letter No.
004 and thereafter as directed by the Service Letter. Refer to Section 8 for additional
information.
51. FILTERS - Inspect pressure system in-line filter for condition, cleanliness and security.
Replace pressure system in-line filter and all other individual instrument air filters in
accordance with the Overhaul and Replacement Schedule in Section 8.
52. MAIN ENGINE FUEL PUMP (TRW or Thompson Model TF1900)- Inspect drive pin
every 300 hours. Refer to TRW Service Bulletin ESD 182D or subsequent.
C. CABIN AND BAGGAGE COMPARTMENT
1. SKIN - Inspect skins for deformation, cracks and loose or missing rivets. If damage is
found, check adjacent structure.
2. STRUCTURE - Check for cracks and deformation. Check for loose or missing rivets and
concealed damage.
3. CABLES, PULLEYS AND TURNBUCKLES - Check the flight control components,
cables and pulleys. Replace control system components (pushrods, turnbuckles, end
fittings, castings, etc.) that have bulges, splits, bends, or cracks. Check control cables,
pulleys, and associated equipment for condition, attachment, alignment, clearance and
proper operation. Replace cables that have more than 3 broken strands in any 3-foot
length of cable or evidence of corrosion. Check cables for proper tension.
NOTE - It is
important to operate controls through their full range so that the cables move away from
pulleys and all portions of the cables are exposed for inspection.
4. AILERON QUADRANT (D-1 thru D-1500) - Inspect for condition, attachment and proper
operation such as binding.
5. LANDING GEAR GEARBOX AND ACTUATING LINKAGE - Check for leakage, wear,
condition and attachment. Check for unusual noise. Remove oil filler plug and check oil
level by engaging and turning the emergency hand crank 1/2 turn to determine that oil
is being picked up on the worm gear. The oil level should be maintained no more than
necessary to cover 1/2 of the diameter of the worm gear. Install oil filler plug.
6. FLAP MOTOR AND SHAFTS - Check for condition, security and wear at all points.
Check drive shaft housing for security and check jam nuts for tightness.
100-HOUR OR ANNUAL INSPECTION (Continued)