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Boeing 737 aircraft maintenance manual download.Boeing 737-300 Series Maintenance Manual
Also See for Series Wiring diagram manual supplement - 15 pages. Table Of Contents. Quick Links Download this manual. Notice: This is confidential and proprietary information of General Aerospace and may not be used or disclosed by the recipient. General Aerospace. By receipt hereof, in addition to any obligation the recipient has under any confidentiality agreement. Aerospace and that it will keep confidential all information contained herein. Table boeing 737 aircraft maintenance manual download Contents.
Previous Page. Next Page. Aircrafts Boeing Maintenance Manual Engine pages. Transponder Detail B. The transponders are located on the E2 electronic equipment rack on E shelf. The coding of a mode A reply can consist of up to fifteen pulses. Вот ссылка of these pulses carry the identification number. Two others, called framing pulses, come before and after the twelve information pulses.
The last is a bofing identification pulse to aid the radar operator. In the Pre-selector the signal is passed through a bandpass filter tuned to MHz. Читать далее troubleshooting procedures make use of the self-test features donwload the ATC transponder and ATC system tests to isolate aircarft.
These procedures are in a tree-type format. One is an operational test; the other is a system test. The operational test maanual a fast check of источник ATC system and no test equipment is needed. The system test first does the operational test. Transponder 2 is mode Boeing 737 aircraft maintenance manual download, skips Mode S steps boeing 737 aircraft maintenance manual download check of Transponder 2. General 1 This system test is a more complete check of the ATC system.
Also, make sure to correct for other factors that would change the sensitivity maingenance. The subject has two tasks. The first task is the removal of the ATC antenna. Equipment 1 Sealing gun - 6-inch length maintennance, Senco Research, or equivalent not required for material furnished in tubes 2 Bonding meter AMM 3 Varnish brush - 1- or 2-inch Commercial 4 Spatula Commercial E. This procedure has two tasks. The first task is the removal of the ATC transponder.
The second task is the installation of the ATC transponder. Узнать больше subject has two tasks. Print page 1 Print document 35 pages. Cancel Delete. Sign In OR. Don't have an account? Sign up! Restore password.
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Boeing 737 aircraft maintenance manual download.Boeing B737 Maintenance Manual
One is an operational test; the other is a system test. The operational test is a fast check of the ATC system and no test equipment is needed. The system test first does the operational test. Transponder 2 is mode C, skips Mode S steps for check of Transponder 2.
General 1 This system test is a more complete check of the ATC system. Also, make sure to correct for other factors that would change the sensitivity measurement. The subject has two tasks. The first task is the removal of the ATC antenna. Equipment 1 Sealing gun - 6-inch length cartridge, Senco Research, or equivalent not required for material furnished in tubes 2 Bonding meter AMM 3 Varnish brush - 1- or 2-inch Commercial 4 Spatula Commercial E.
This procedure has two tasks. The first task is the removal of the ATC transponder. The second task is the installation of the ATC transponder. This subject has two tasks. This test does not give specific levels of performance for any of the functions of the ELT but it does indicate that the system is functioning in a satisfactory manner.
That is, if the G-switch circuit has a failure, there will be a single flash then 3 flashes would appear if there was a transmitter problem and so on. These procedures include checks required in the United Sates. Remove the four screws from the battery pack.
Before proceding further, read the following advisory to avoid damage to the ELT. For detailed instructions refer to step 19 and Figure 3. Reinstall the four Phillips head screws and tighten securely. NOTE: Allow the unit to run 30 seconds before making the measurement to allow the oscillator to stabilize. Exercise extreme caution to avoid causing a short circuit condition which will blow the fuses on the battery pack. The measured steady state current should not exceed milliamps mA. When the Page 1 is the main menu screen.
The frequency must read between Carefully disconnect the harness from the 8-pin connector on the small circuit board in the battery pack. Do not short connector pins. Position the end cap and connector assembly onto the ELT and tighten the two thumbscrews securely.
Attach antenna to fuselage with six non-Torx drive screws and flat washers. Apply sealant to the screw threads before installing them. Any obvious damage to any ELT system component should be rectified before proceeding. NOTE: Do not touch the end of the ignition lead with your hands or with a dirty cloth. Oil or grease can cause the ignition lead to operate incorrectly. NOTE: The sensors have different connections for the different types of cables connectors.
Make sure you use the correct ssensor box. Related Papers. By Luis Eduardo Medrano. FAA 12 A. By chhotu nain. Download pdf. Remember me on this computer. Enter the email address you signed up with and we'll email you a reset link.
Boeing 737 aircraft maintenance manual download.Boeing 737-300/400/500 Aircraft Maintenance Manual
To browse Academia. Skip to main content. By using our site, you agree to our collection of information through the use of cookies. To learn more, view our Privacy Policy. Log In Sign Up. Download Free PDF. Raven Oppier. Download PDF. A short summary of this paper. General A. The ignition system Fig. The purpose of the system is to produce an electrical spark to ignite the fuel and air mixture in the engine combustion chamber during the start cycle and to provide continuous ignition during takeoff, landing and operation in adverse weather conditions.
The left, right or the two spark igniters can be selected during the start cycle or for continuous ignition operation. The ignition system test consists of the operation of the engine ignition system and an operational check of: the spark igniters the start lever ignition limit switch the engine igniter selector switch the engine start switch. The test applies to each engines. Make sure you do the test in the sequence provided in the procedure. Access 1 Location Zones No. NOTE: The position light for the shutoff valve for the engine fuel is bright when the valve is in operation.
It is dim when the valve is closed and off when the valve is open. General 1 This task includes an optional procedure to use an Ignition Tester for trou- ble-shooting of the ignition system. Ignition System - Optional Trouble-Shooting with the Tester NOTE: This procedure is done when there is a problem with the ignition system to find which part of the ignition system is unsatisfactory.
NOTE: Do not touch the end of the ignition lead with your hands or with a dirty cloth. Oil or grease can cause the ignition lead to operate incorrectly. NOTE: The sensors have different connections for the different types of cables connectors. Make sure you use the correct ssensor box. Related Papers. By Luis Eduardo Medrano. FAA 12 A. By chhotu nain. Download pdf. Remember me on this computer. Enter the email address you signed up with and we'll email you a reset link.
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