Cessna 172R

TTP B1-L3 ATA25 Cessna 172 B2-L1 Flight Compartment covers those items installed in the cabin area, including seats, seat restraints systems, carpets and interior panels. Emergency equipment covers the emergency locator transmitter installed behind the aft baggage compartment. It also covers the carbon monoxide detector installed forward of the instrument panel on airplanes that are equipped with Garmin G1000. Soundproofing and insulation covers the material used to deaden sound throughout the airplane. AMSAFE Inflatable Restraint System - AAIR is a self-contained, modular, three-point restraint system that will help to protect occupants from head-impact injury during an accident. The AAIR system has four core components: the air bag assembly, the inflation assembly, the electronics module assembly (EMA), and the cable interface assembly. Cargo tie-downs are provided for the airplane to accommodate a variety of loading ...

TTP B1-L2 ATA23 Cessna 172 B2-L3 Speech communication -  radio equipment used for reception and  transmission of voice communication. Audio integrating system   system which controls  the output of the communications and navigation receivers into the pilot and passengers  headphones and speakers, and the output of the pilot’s microphone into the communications transmitters. Static discharging  wicks used to dissipate static electricity. Cessna 172 with the Garmin G1000, the center of the Garmin G1000 is the GIA 63 Integrated Avionics Unit (IAU), which is in the tailcone. The GIA 63 operates as a primary communications center that connects all of the Line Replaceable Units (LRUs) with the Primary Function Display (PFD) and Multi-Function Display (MFD). The GIA 63 has the GPS receiver, VHF NAV/COM receivers, and system integration microprocessors. The GIA 63W has the Wide Area Augmentation System (WAAS...

TTP Cessna 172 Cat.B1 Level -3 ATA54 Nacelles/Pylons  Cat.B2 Level -1 TTP B1-L1 ATA05 Cessna 172 B2-L1

TTP B1-L3 ATA51 Cessna 172 B2-L1 Damage Classification, assessment and repair Single Engine Structural Repair Manual 1996 and On. STRUCTURES- F uselage is of semimonocoque construction and consists of three major sections: forward  section, center section, and tailcone section. Construction consists of formed bulkheads,  longitudinal stringers, reinforcing channels and skin. Frame members of the cabin section are  constructed of formed bulkhead channels. Bulkheads are formed "U" channel sections. Principal  material is 2024- 0 alclad aluminum alloy which, after forming, is heat treated to a 2024-T42  condition and painted with epoxy primer. All bulkheads in the fuselage are constructed of formed  sheet metal or reinforced sheet metal. Wings are of all-metal, strut-braced, semi monocoque construction, utilizing two spars. Each  wing consists of an outer wing panel with an integral fuel bay, an a...

TTP B1-L1 ATA20 Cessna 172 B2-L1 Chapter 20 describes standard maintenance practices and safety precautions applicable to all aspects of the airframe and related systems. 1.     Material and Tool Cautions describes general cautions and warnings  applicable to maintenance on or around the airplane. 2.     Torque Data provides tables, formulas, requirements and torque limits for  various type fasteners. 3.     Safetying describes the proper methods and use of safety wire/lockwire, cotter  pins and lock clip installations. 4.     Solvents describes characteristics of solvents which are commonly used during maintenance, cleaning and inspection of various airframe and related components.    PTP Cessna 172 B1 LOC SGH B2 LOC SGH   Torque Data To ensure security of in...

TTP Cessna 172 Cat.B1 Level -1 ATA05 Time Limit/ Maintenance Check Cat.B2 Level -1 Inspection Requirements (1) Traditional (Annual/100 Hour) inspection program -   Section 5-10-01. (2) Progressive Care inspection program which allows the work load to be divided into smaller  operations that can be accomplished in a shorter time period. Section 5-12-00. (3) Phase Card inspection program which is geared toward high-utilization flight operations  (approximately 600 or more flight hours per year). This system utilizes 50-hour intervals  (Phase 1 and Phase 2) to inspect high-usage systems and components. At 12 months or 600  flight hours, whichever occurs first, the airplane undergoes a complete (Phase 3) inspection. Inspection Time Limit Chart Legend -  Each page of Section 5-10-01, contains the five columns that follow: REVISION STATUS - This column supplies the date that a given i...