Cessna 172R

TTP B1-L1 ATA07 Cessna 172 B2-L1 Cessna 172 airplane may be lifted with a hoist of two-ton capacity attached by rings , which are optional  equipment installed by Service Kit, or by means of suitable slings.      Front sling should be hooked to  each upper engine mount, and the aft sling should be positioned around the fuselage at the first bulkhead  forward of the leading edge of the stabilizer. If the optional hoisting rings are used, a minimum cable  length of 60 inches for each cable is required to prevent bending of the eyebolt-type hoisting rings.  If  desired, a spreader jig may be fabricated to apply vertical force to the eyebolts PTP   Cessna 172 B1 LOC B2 LOC

TTP B1-L1 ATA09 Cessna 172 B2-L1 Towing -   Moving the airplane by hand is accomplished by using the wing struts and landing gear struts as  push points.    Tow bar attached to the nose gear should be used for steering and maneuvering the  airplane on the ground.    When no tow bar is available , press down on the tailcone at a bulkhead to  raise the nose wheel off the ground. With the nose wheel clear of the ground, the airplane can be  turned by pivoting about the main wheels. CAUTION: WHEN TOWING THE AIRPLANE, NEVER TURN THE NOSE WHEEL MORE THAN  30 DEGREES EITHER SIDE OF CENTER , OR THE GEAR WILL BE DAMAGED. DO NOT PUSH  ON CONTROL SURFACES OR ANY PORTION OF THE HORIZONTAL STABILIZER. WHEN  PUSHING ON THE TAILCONE, ALWAYS APPLY PRESSURE AT A BULKHEAD TO AVOID  DAMAGING THE SKIN.                  PTP Cessna 172 B1 LOC SGH B2 LOC SGH

TTP B1-L3 ATA32 Cessna 172 B2-L1                       Fixed, tubular spring, steel main gear struts that are bolted into the fuselage bottom. Attached to the outboard end of each strut is a die-cast aluminum wheel and disc brake assembly. Steering nose wheel that is linked through the rudder pedals to give ground control. Shock Strut - The shock strut is made of top and bottom machined cylinders that contain a mixture of oil and air. The top and bottom cylinders give changes in the shock-absorb rates. Torque Links - The torque links give a mechanical link between the top and bottom parts of the shock strut and help to keep the nose wheel aligned with the airframe. Nose wheel Steering - operates through the use of the rudder pedals. The spring-loaded steering rod assemblies connect the nose gear steering arm assembly to the arms on the rudder pedals. The steering gives up to approximately 10 degrees each side of neutral, aft

PTS B1-L3 ATA32 Cessna 172 B2-L1 PTP Cessna 172 B1 LOC FOT SGH R/I MEL TS B2 LOC FOT SGH R/I MEL TS Shimmy Damper Servicing  at  every 100 hours :   (1) Remove the shimmy damper.   (2) While you hold the damper in a vertical position with the fitting end pointed down, pull the fitting end of the damper shaft to its limit of travel.   (3) While you hold the damper in this position, fill the damper through the open end of the cylinder withhydraulic fluid.   (4) Push the shaft up slowly to seal off filler hole.   (5) Clean the damper with solvent. Make sure that the shaft comes out through the filler hole until the damper is installed on the aircraft.   (6) Install the damper on the airplane. Shimmy Damper Servicing (Lord Shimmy Damper) Lord Shimmy Dampers do not need special servicing. lubricate the nose wheel shimmy damper pivots

TTP B1-L3 ATA27A Cessna 172 B2-L1 CONTROL SURFACE TRAVELS/CABLE TENSION SETTINGS AILERONS   Up Travel 20 Degrees, ±1 Degree                    Down Travel 15 Degrees, ±1 Degree           Cable Tension (Carry Through) 40 ±10  lb      RUDDER                     Right 16 Degrees 10 Min; ±1 Degree                     Left 16 Degrees 10 Min; ±1 Degree                     Right 17 Degrees 44 Min; ±1 Degree                      Left 17 Degrees 44 Min; ±1 Degree ELEVATOR                 Up Travel 28 Degrees, +1 or -0 Degree           Down Travel  23 Degrees, +1 or -0 Degree                     Elevator Cable Tension 30±1 lb ELEVATOR TRIM TAB                 Up Travel 22 Degrees, +1 or -0 Degree           Down Travel 19 Degrees, +1 or -0 Degree          Elevator Trim Cable Tension 20 Pounds, +0 or -5 Pounds FLAPS         Flap Setting: 0 Degree (UP) 0 Degree 10 Degrees 10 Degrees, +0 or -2 Degrees 20 Degrees 20 Degrees, +0 or -2

ATA01 Introduction ATA05 Time limit ATA06 Dimension ATA07 Lifting ATA08 Leveling&Weighing ATA09 Towing&Taxiing ATA10 Parking&Mooring ATA11 Placard&Marking ATA12 Servicing ATA20 Standard Practices  ATA23  Comm ATA24 Electrical Power ATA25 Equip&Furnishin ATA27 Flight Control ATA28 Fuel  System   ATA31 Instrument ATA32 L/G ATA33 Light ATA34 Navigation ATA37 Vacuum  ATA51 SP-Structure ATA52 Cabin Door ATA53 Fuselage ATA54 Nacelles  ATA55 Stabelizer ATA56 Window ATA57 Wing ATA60 SP- Propeller ATA61  Propeller  ATA70 SP-Engine ATA71 Power Plant ATA73 Engine Fuel  ATA74 Ignition System ATA76 Engine Control ATA77 Engine Indicating System ATA78 Exhaust System ATA79 Engine Oil System ATA80 Starting System