Introduction

By -


TTP
B1-L1
ATA01
Cessna 172
B2-L1



Type Rated Training Course Requirement 
Type Rated Training Course - Cessna Lycoming 
Good Maintenance Practices 

  Maintenance Data


Maintenance Manual 
Wiring Diagram Manual,
Illustrated Parts Catalog
Single Engine Structural Repair Manual.
Technical Publications are also available for the various components and systems which are not covered in MM. 

 Maintenance Manual 
Page Numbering System.-- consists of three-element numbers separated by dashes. 
When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number (22-00-00), the information is applicable to the entire system.
When the section/subsystem element number is followed with zeros in the subject/unit element number (22-10-00), the information is applicable to the subsystem within the system.
The subject/unit element number is used to identify information applicable to units within the subsystems. The subject/unit element number progresses sequentially from the number -01 in accordance with the number of subsystem units requiring maintenance information.
All system/subsystem/unit (chapter/section/subject) maintenance data is separated into specific types of information: description and operation, troubleshooting, maintenance practices
 Effective Pages - A list of effective pages is provided at the beginning of each maintenance manual chapter. All pages in the specific chapter are listed in numerical sequence on the Effectivity Page(s) with the date of issue for each page.
Illustrated Parts Catalog (IPC) includes the illustration and identification of replacement parts and assemblies necessary for maintenance of the specified aircraft model. The Catalog gives the information available at the time of publication.

IPC is prepared in accordance with the Air Transport Association 2200 Specification Format.
Chapter 11 contains procurable placards. Country designated placards are specified by foreign certification authorities and put into groups identified by an International Civil Aviation Organization (ICAO) identifier in the page footer.

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  pressure. Vacuum gag e gives a direct indication of the
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 in position on the studs
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