SPECIAL PROVISIONS TO MESSAGE REQUIREMENTS (AIRCRAFT).

TB 1-1520-240-20-167

c. Wholesale Stock (Including Depot Stock, Depot Maintenance and Single Stock Fund). Provide Local POC,

address and phone number. Report compliance with this message IAW para 8 to Wholesale POC NLT 24 May 2006.

6. SPECIAL PROVISIONS TO MESSAGE REQUIREMENTS (AIRCRAFT).

a. Aircraft in AVIM or Depot Level Maintenance. Commanders, Facility Managers and Contractors will not issue

aircraft until they are in compliance with this message.

Aircraft at Contractor Facility. DD 250 aircraft will be in compliance with this message prior to departure.

c. Aircraft in Transit. Unit Commanders in receipt of deployment orders and are unable to comply prior to the

date specified in para 4.a. may defer initial requirements IAW Surface/Air Shipment or Ferry Status Instructions, as

appropriate.

(1)

Surface/Air Shipment. Comply with message requirements within 10 days of arrival.

(2)

Ferry Status. Comply with message requirements within 10 days of arrival at final destination.

(3) Aircraft Away From Home Station. Comply with message requirements within 10 days of arrival at final

destination.

7. TECHNICAL PROCEDURES/INSTRUCTIONS.

a. Inspect Aircraft LCT Actuator, Aft, PN 145CS114-2, NSN 1680-01-120-7641 to determine if one of the fol-

lowing serial numbers is installed:

34-238

40-702

40-706

42-997

55-312

90-792

56-2221

59-1140A

73-1118

108-613

116-459

(1)

If any of the eleven LCT Actuators are installed proceed to para 7.b.

(2)

If none of the eleven LCT Actuators are installed proceed to para 7.c.

b. Inspect the suspect LCT Actuator's lower rod end fitting to ensure that the anti-rotational lugs (tabs) are

facing opposite the LCT Actuator motor.

NOTE

See Ch-47D/F Maintenance Manual TM 1-1520-240-23-9, Task 11-206, Step 12, MH-47E Mainte-

nance Manual TM 1-1520-252-23-13, Task 11-224, Step 8, or MH-47G Maintenance Manual

TM 1-1520-272-23-13, Task 11-224, Step 8, for a visual guide to proper orientation of the

anti-rotational lugs that should face opposite the actuator motor. Please note that the Forward

Actuator Task is referenced only because it provides the better visual guide to correct anti-rotational

lug orientation. This orientation is the same for Aft and Forward Actuators.

(1) If the LCT Actuator is found to be non-conforming make the following red //X// entry on the

DA Form 2408-13-1 "LCT Actuator SN "XXXXX" requires replacement IAW CH-47-06-ASAM-03". Proceed to

para 7.d. Enter "XXXXX" as serial number of suspect LCT Actuator.

(2)

If the LCT Actuator is found to be conforming, proceed to para 7.c.