Landing Gear.

Slides:



Advertisements
Similar presentations
Hydraulic Systems & Undercarriage
Advertisements

Drive Right Chapter 3 Basic Vehicle Control
Malibu/Mirage PA46-310/350 Landing Gear & Brakes
Dennis Fire Appliances Operations & use. PTO Step 1 Move slide cover towards the drivers seat to lock out the gearbox Step 2 Select drive on the gear.
Cessna C500 Fuel System hello and welcome to my talk on the c500 fuel system.
Hydraulic fluid flow through an HWH dual cylinder (Synchronized) room extension.
In this presentation you will:
Cessna Citation II Flight Controls
Copyright © 2014 Delmar, Cengage Learning Electrical Accessories Instructor Name: (Your Name) 10 CHAPTER.
MODULE V CDL Pre-route Victoria Creech Training Representative.
AST 473 Cessna Citation II Landing Gear and Brakes
GO ORDNANCE !!! ORDNANCECORPS 1 Antenna Mast Group We will now trace the electrical circuits of the antenna mast mast group. Be fore we get started you.
Office of Aviation Safety American Airlines Flight 1400 St. Louis, Missouri Captain David Tew Operational Factors.
Number One In The World For a Reason ® ® Holmatro Hydraulic Rescue Tool What You Need to Know to Maintain your Rescue Tool System © 4/2004 Holmatro.
Landing Gear.
B757 Review Questions.
TO SERVE WITH PRIDE AND DEDICATION. TO SERVE WITH PRIDE AND DEDICATION SCOPE… Landing Gear & Brake System -Brake System Schematic Main Wheel Assembly.
Indicates primary inverter is inop. Operational secondary and auxiliary inverters will Maintain power to all fixed frequency busses.
Actuators.
AIRCRAFTS HYDRAULIC SYSTEM
HYDRAULICS & PNEUMATICS
AccuMax Multi-Point Injection Mechanics
B757 Review Questions.
B757 Review Questions.
APPROVED TRAINING MANUAL’S LESSON PLANS AND COURSEWARE STAR MARIANAS AIR, INC. Recurrent – Flight Crew Part III – Aircraft Ground Training Section 2 –
EZ Reach 40 Training & Procedure Manual. Unit Capacity One of the most important considerations when operating this machine is the Bucket Capacity of.
INTRODUCTION Hydraulics is based on the fact that liquids are incompressible Hydraulic system is a system where liquid under pressure is used to transmit.
Ladder Diagram Symbols Flashcard Exercise Get Started.
Lesson 12: Aircraft Landing Gear
Hydraulic Circuits.
CH-47D Auxiliary Power Unit
E Co 1/214th AVN Regt C-12 Landing Gear.
310 Series Basic Leveling Procedure
Downloaded from HOW TO AVOID A GEAR-UP LANDING Presented By Larry Enlow Aviation Safety Inspector Federal Aviation Administration Orlando.
Ladder Concept.
Fluid Power Control.
HOW TO AVOID A GEAR-UP LANDING Presented By Larry Enlow Aviation Safety Inspector Federal Aviation Administration Orlando Flight Standards District Office.
FLIGHT CONTROLS AND HYDRAULICS. FLIGHT CONTROLS The flight control systems are mechanical linkages, actuated by conventional controls, and are used to.
By John Templeton.  Definition- the science that deals with the laws governing water or other liquids in motion and their applications in engineering;
UH-60 HYDRAULIC SYSTEM BY: CW2 Ron Nelson.
Fluid Power Control.
Air Line Pilots Association, International EMB 145 Oral Questions Overhead “D” Select “Slide Show” Use the space bar on your computer to advance the presentation.
Fluid Power Control.
Pre-Trip Inspection Guide
EC 130 B4 Initial Pilot Ground School Chapter 9 Hydraulic System.
Copyright © 2017 by Pearson Education, Inc. All Rights Reserved Automotive Brake Systems, 7e James D. Halderman Automotive Brake Systems CHAPTER ABS Components.
CH-47D Cargo Handling System
Shuttle Loss of Sensors
For system diagrams and component identification
LANDING GEAR SYSTEMS THIS TRAINING MANUAL HAS BEEN PREPARED FOR MAINTENANCE TECHNICIANS AND DOES NOT SUPERSEEDED INFORMATION CONTAINED IN APPLICABLE AIRCRAFT.
Mcq.
HYDRAULIC & PNEUMATIC CIRCUITS
Pneumatics Module 9 Time delay valve.
OBJECTIVES Describe the fundamentals of brake systems.
Landing gear systems.
OBJECTIVES Describe the operation of a pressure-differential switch and a brake fluid level sensor switch. Describe the operation of a residual check valve.
Actuators & Directional Control Valves
PA-28R-201 Systems Andy Philbin.
DANGER DANGER DANGER INTAKE DANGER INTAKE DANGER DANGER DANGER R R E E
T-6B On-Board Oxygen Generation System (OBOGS)
Game Tutorial, How it works
Game Tutorial, How it works
Landing Gear and Brakes
310 Series Basic Leveling Procedure
Created: 15 Aug 2015 Updated: 20 Sep 2015
T-6B On-Board Oxygen Generation System (OBOGS)
Hydraulic Flow Control • Metering Fluid Flow
Fluid Power System Electrical Control
Presentation transcript:

Landing Gear

Terminal Learning Objective Action: Identify the subsystems of the C-12T2/U landing gear system and explain the basic operating principles. Condition: Using student handout and classroom notes. Standard: IAW the IGRV SEP

RISK ASSESSMENT LEVEL: IV, D, LOW ENVIRONMENTAL CONSIDERATIONS: SAFETY REQUIREMENTS: NONE RISK ASSESSMENT LEVEL: IV, D, LOW ENVIRONMENTAL CONSIDERATIONS: NO IMPACT

C-12T2/U Landing Gear System Description Electrically Activated Switches, relays, electrically powered valves are actuated when the landing gear switch is moved in the cockpit Hydraulically Operated Pressurized fluid is moved to the landing gear hydraulic actuators to raise and lower the landing gear.

C-12 Landing Gear System Cockpit Switches

C-12 Landing Gear System Fill Reservoir

C-12 Landing Gear System Fill Reservoir

C-12 Landing Gear System Fluid Level Dipstick

C-12 Landing Gear System Main Reservoir

C-12 Landing Gear System Reservoir / Power Pack

C-12 Landing Gear System Accumulator

C-12 Landing Gear System Description 3 lines from the pump to each gear actuator Retraction (becomes return line during extension) Extension (becomes return line during retraction) Emergency Gear are held up with hydraulic pressure 2474 psi to 2775 psi Gear are held down with over-center locks

C-12 Landing Gear System Retraction Operations

C-12 Landing Gear System Extension Operations

C-12 Landing Gear System Emergency Extension Operations

C-12 Landing Gear System Check Valves

C-12 Landing Gear System Nose Gear Landing/Taxi Lights

C-12 Landing Gear System Turning Limits

C-12 Landing Gear System Crush Block

C-12 Landing Gear System Nose Gear Torque Knee

C-12 Landing Gear System Shimmy Dampner

C-12 Landing Gear System Main Gear Drag Brace

C-12 Landing Gear System Main Gear Down Lock

C-12 Landing Gear System Main Gear Door

C-12 Landing Gear System Main Gear Door

C-12 Landing Gear System Main Gear Torque Knee

C-12 Landing Gear System Safety Switch

C-12 Landing Gear System Brake Fluid Reservoir

C-12 Landing Gear System Main Brakes

C-12 Landing Gear System Pilot Brakes

C-12 Landing Gear System Co-Pilot Brakes

C-12 Landing Gear System Parking Brake Set

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Landing Gear Warning Horn

C-12 Landing Gear System Questions??????????

C-12 Landing Gear System

C-12 Landing Gear System Review Questions The landing gear are help in the position with ____________ and are held down with ____________.

C-12 Landing Gear System Review Questions The landing gear are help in the position with hydraulic pressure and are held down with over-center locks.

C-12 Landing Gear System Review Questions The brakes use the same type of hydraulic fluid used by the landing gear system. TRUE or FALSE The brakes use hydraulic fluid from the same reservoir as the landing gear system.

C-12 Landing Gear System Review Questions The brakes use the same type of hydraulic fluid used by the landing gear system. TRUE The brakes use hydraulic fluid from the same reservoir as the landing gear system. FALSE

C-12 Landing Gear System Review Questions The timer logic relay in the landing gear system will activate after the gear motor has been operating for ________.

C-12 Landing Gear System Review Questions The timer logic relay in the landing gear system will activate after the gear motor has been operating for 14 seconds.

C-12 Landing Gear System Review Questions The timer logic relay activates for gear retraction operations only. TRUE or FALSE

C-12 Landing Gear System Review Questions The timer logic relay activates for gear retraction operations only. FALSE

C-12 Landing Gear System Review Questions If the pilot raises the landing gear control switch, and the landing gear selector valve fails to operate: The gear will retract normally. The gear will not retract. The timer logic relay will activate after 14 seconds. The landing gear warning horn will activate. The gear handle light will illuminate. The three green down lights for the gear will extinguish.

C-12 Landing Gear System Review Questions If the pilot raises the landing gear control switch, and the landing gear selector valve fails to operate: The gear will retract normally. The gear will not retract. The timer logic relay will activate after 14 seconds. The landing gear warning horn will activate. The gear handle light will illuminate. The three green down lights for the gear will extinguish.

C-12 Landing Gear System Review Questions The pilot places the gear control switch in the up position. Once the landing gear is fully retracted, the uplock pressure switch fails to operate: The gear will retract normally. The landing gear pump motor will shut down when the gear is fully retracted. The landing gear pump motor will be shut down by the timer logic relay. The landing gear down indicator lights (green) will remain illuminated. The gear relay circuit breaker will open.

C-12 Landing Gear System Review Questions The pilot places the gear control switch in the up position. Once the landing gear is fully retracted, the uplock pressure switch fails to operate: The gear will retract normally. The landing gear pump motor will shut down when the gear is fully retracted. The landing gear pump motor will be shut down by the timer logic relay. The landing gear down indicator lights (green) will remain illuminated. The gear relay circuit breaker will open.

C-12 Landing Gear System Review Questions The parking brake can be set from ____________. The left seat The right seat Either seat The toilet

C-12 Landing Gear System Review Questions The parking brake can be set from ____________. The left seat The right seat Either seat The toilet

C-12 Landing Gear System What is an unsafe gear indication? What would you do if one main gear or the nose gear green light failed to illuminate? What are you going to do if one gear fails to extend? Main Gear Nose Gear What are you going to do if one gear fails to extend after manual extension?

C-12 Landing Gear System Summary System description Normal system operations Emergency system operations Brake system Landing gear warning system Abnormal operations