INSPECTION OF HOSE ASSEMBLY, HYDRAULIC PRIMARY SYSTEM FOR CHAFING, P/N 7-311830102-5, ON HOSE CLAMP P/N HS4501SS09NB

URGENT

TB 1-1520-238-20-68

DEPARTMENT OF THE ARMY TECHNICAL BULLETIN

INSPECTION OF HOSE ASSEMBLY,

HYDRAULIC PRIMARY SYSTEM FOR

CHAFING, P/N 7-311830102-5, ON HOSE

CLAMP P/N HS4501SS09NB

Headquarters, Department of the Army, Washington, D. C.

13 November 1995

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

NOTE

THIS PUBLICATION IS EFFECTIVE UNTIL SUBJECT AH-64A AIRCRAFT HAVE BEEN INSPECTED, UNLESS

SOONER RESCINDED OR SUPERSEDED.

1. Priority Classification. Routine

a. Aircraft in Use. Upon receipt of this Technical Bulletin (TB) the condition status symbol of the cited aircraft will be

charged to a red horizontal dash//-//. The red horizontal dash// may be cleared when the inspection of paragraph 8 below

is completed. The affected aircraft shall be inspected as soon as practical but no later than the task/inspection suspense

date. Failure to comply with the requirements of this message within the time frame will cause the status symbol to be

upgraded to a red //-//.

b. Aircraft in Depot Maintenance. Aircraft will not be issued until compliance with this TB has been completed.

c. Aircraft Undergoing Maintenance. Aircraft will not be issued until compliance with this TB has been completed.

d. Aircraft in Transit.

(1) Surface/Air Shipment. Within 10 hours or 14 days of arrival.

(2) Ferry Status

(a) Inspect at final destination.

(b) Those Aircraft that have DD250 and are at McDonnell Douglas Helicopter Systems will be inspected

prior to ferry to final destination.

This TB supersedes USAATCOM Aviation Safety Action Message 051916Z October 95 AH-64-96-ASAM-01