Standard Practices - Propeller

By -

Comments

Post a Comment

Popular posts from this blog

VACUUM SYSTEM

By -
TTP B1-L3 ATA37 Cessna 172 B2-L2   V acuum system has a filter, vacuum gage, vacuum instruments, regulator valve, vacuum manifold,  low vacuum annunciator switches, engine-driven vacuum pumps and related plumbing.   With   Garmin G1000, the source of vacuum air is in the cabin and is pulled through the  system by the engine-driven vacuum pumps. This air goes through the gyro filter at the cabin inlet source  before it goes through the vacuum gage and gyro instruments. The vacuum is controlled by the regulator  valve. The regulator valve is on the aft side of the firewall. The vacuum air is then pulled through the  vacuum manifold and past the low vacuum annunciator switches and then into the vacuum pumps. Without Garmin G1000, vacuum pressure is measured by the low vacuum annunciator   switches in the engine compartment. The vacuum gage in the instrument panel shows the vacuum  pres...
Read more

Power Plant

By -
Image
TTP Cessna 172 Cat.B1 L-3 ATA71 Power Plant Cat.B2 L-1 Textron Lycoming IO-360-L2A engine is direct drive, four cylinder, fuel injected, horizontally opposed,  and air cooled. The cylinders, numbered from front to rear, are staggered to have individual throws on the  crankshaft for each connecting rod. The right front cylinder is number 1 and cylinders on the right side of  the engine are identified by odd numbers 1 and 3. The left front cylinder is number 2 and the cylinders on  the left side are identified as 2 and 4.  IO-360-L2A Technical Description 172R Rated Horsepower at 2400 RPM 160 172S* Rated Horsepower at 2700 RPM 180 Number of Cylinders 4  Horizontally Opposed Displacement 361.0 Cubic Inches Bore 5.125 Stroke 4.375 Compression Ratio 8.5:1 Firing Order 1-3-2-4 Magnetos:      Right  Slick 4371 (25°BTDC)                         Left...
Read more

WINGS AND WING STRUTS

By -
Image
TTP B1-L3 ATA57 Cessna 172 B2-L1 Wing is a strut braced type, with two main spars and suitable ribs for the attachment of the  skin. Skin panels are riveted to ribs, spars and stringers to complete the structure.  All metal , piano  hinged aileron, flap and detachable wing tip are mounted on each wing assembly.  Each wing also  incorporates an integral fuel bay located between the two spars at the inboard portion of the wing.  Each  wing is supported in position by a single lift strut which consists of a streamlined tube riveted to two end  fittings for attachment at the wing and at the fuselage.     PTP B1-L1 ATA57 Cessna 172 B2-L1 571001 Wing Surfaces and Tips - Inspect for skin  damage, loose rivets, and condition of paint.    571002 Wing Struts and Strut Fairings - Check for  dents, cracks, loose screws and rivets, and  condition of paint 571004 Wing Spar...
Read more