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GROUND HANDLING AND<br />

SERVICING HANDBOOK<br />

HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.<br />

BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.<br />

(c) Release the towing lever to lock the towbar head to the nose landing<br />

gear tow fitting.<br />

(6) Connect the other end of the towbar (GSE 027) to the tractor.<br />

C. Towing with Towbar<br />

CAUTION: OBEY THE SAFETY PRECAUTIONS DURING THE TOWING<br />

OPERATIONS: A TECHNICIAN MUST STAY IN THE COCK-<br />

PIT TO SET THE EMERGENCY/PARKING BRAKE, IF NEC-<br />

ESSARY. ALL PERSONS IN THE COCKPIT MUST BE IN A<br />

SEAT AND THE SEATBELT MUST BE FASTENED.<br />

(1) Pressurize the main hydraulic system (GHSH TASK 29-10-00-901-803-A/<br />

200).<br />

(2) Make sure that there is a technician in the cockpit to set the emergency<br />

parking brake if necessary.<br />

(3) Release the emergency/parking brake.<br />

(4) Tow the aircraft slowly straight ahead before you try to do a turn. The maximum<br />

speed recommended for aircraft towing is the walking speed.<br />

NOTE: • During the towing operation, use the emergency/parking<br />

brake only if the towbar (GSE 027) uncouples from the towing<br />

vehicle or from the aircraft.<br />

• If the aircraft emergency/parking brake is applied during the<br />

towing operation, regardless of the speed, do a check of the<br />

integrity of the shear pin of the towbar head (GSE 026).<br />

• If during the towing operation, the towbar head (GSE 026)<br />

shear pin is broken, do the inspection of the NLG (Nose<br />

Landing Gear) for damage and replacement of the shear pin<br />

,as given in step (5) of this procedure.<br />

(5) Nose Landing Gear - Inspection (Figure 203)<br />

WARNING: MAKE SURE THAT THE AIRCRAFT IS IN A SAFE<br />

CONDITION BEFORE YOU DO THE MAINTENANCE<br />

PROCEDURES. THIS IS TO PREVENT INJURY TO<br />

PERSONS AND/OR DAMAGE TO THE EQUIPMENT.<br />

(a) Make sure that the wheel chocks are in position against the landing<br />

gear wheels.<br />

(b) In the cockpit, make sure that the landing-gear control lever is in the<br />

DN position.<br />

(c) Use a flashlight and a mirror, if necessary, to examine these components<br />

of the NLG:<br />

• Main fitting<br />

• Sliding tube<br />

• Retraction actuator<br />

EFFECTIVITY: ALL 09-10-01-<strong>500</strong>-801-A/200<br />

Page 202<br />

Rev.06 - OCT 09/09<br />

Copyright © by <strong>EMB</strong>RAER S.A - All rights reserved - See title page for details.

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