Dimensions/Area

By -
TTP
B1-L1
ATA06
Cessna 172
B2-L1



Airplane Station: The airplane is laid out according to fuselage stations (FS) and wing stations (WS). These stations provide fixed reference points for all components located on or within the airplane.
 Fuselage Stations begin at the firewall (FS 0.00) and extend to the tailcone area (FS 230.18). 
Wing Stations begin at the root (WS 23.62) and extend to the tip (WS 208.00). Both Fuselage Stations and Wing Stations are measured in inches. For example, FS 185.50 is 185.50 inches aft of the firewall (FS 0.00).
Zone : The Model 172 is divided into numbered zones to provide a method for locating components and/or placards throughout the airplane. The zones are identified by a three-digit number as shown in the example below. 
First digit in the sequence denotes the major zone (300 series for aft of cabin, 500 series for left wing, etc.). 
Second digit in the sequence further divides the zone into sub major zone (Zone 510 for inboard portion of the left wing and Zone 520 for outboard portion of the left wing, etc..).
Third digit further divides the sub major zones into subdivisions (if no subdivision is needed, this digit is typically assigned as 0 (zero).
Length (Overall) 27’ - 2”                         Height (Maximum) 8’ - 11”
Wing Span (Overall) 36’ - 0”                   Tail Span 11’ - 4”
Landing Gear Track Width 8’ - 4 1/2”
FUSELAGE DIMENSIONS
Cabin Width (Maximum Sidewall to Sidewall) 3’ - 3 1/2”
Cabin Height (Floorboard to Headliner) 4’ - 0”
MAXIMUM WEIGHT        Ramp 172R 2457 Pounds     172S      2558 Pounds
                                       Takeoff 172R 2450 Pounds   172S    2550 Pounds
                                       Landing 172R   2450 Pounds  172S     2550 Pounds



PTP 
 Cessna 172
B1
LOC

B2
LOC

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

LEVELING

By -
TTP B1-L1 ATA08 Cessna 172 B2-L1             PTP Cessna 172 B1 LOC SGH B2 LOC SGH Required tools, equipment and materials-. Leveling Points Lateral Leveling. (1) Find two points that are the same on each upper door sill of the left and right cabin doors. (2) Put a level in position across these points. NOTE: Out-of-level tolerance for wing tips is three inches total. (3) Make a note of the airplane's lateral position. (4) If applicable, put jacks in position at the wings and tail jacking points. (a) Adjust the wing jacks as required to get the necessary lateral position. Longitudinal Leveling. (1) Find the two screws on the left side of the airplane tailcone that are in line with water line zero. (2) Remove the screws. (3) Install studs or long screws of applicable length (approximately two inches long). (4) Put the level...
Read more

FAA AD 2015-19-07 Lycoming Fuel Injected Reciprocating Engines

By -
           (1) Initial Inspecton _, inspect the fuel injector fuel lines and clamps between the fuel manifold and the fuel injector nozzles. Use MSB No. 342G,  to perform the inspection. Replace any fuel injector fuel line or clamp that fails the inspection required by the Fuel Line Inspection and Installation Checklist in MSB No. 342G.          (2) Re-inspect after any maintenance is done on the engine where any clamp on a fuel injector fuel line was disconnected, moved, or loosened, and within every 110 hours TIS and after each engine overhaul. 
Read more