Reflex Marine FROG-6 HC6-01 620, User Manual

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User Manual FROG-6
UM-0007-REV.06 Page 49
6.8.1 Load Test Procedure
Table 4 details the required proof load tests that are applicable to the FROG-6 (See Note *).
Following the load tests, a post load test visual inspection should be conducted as recommended in
Section 6.7 .
Table 4: Proof Load Tests – FROG-6
Load Test Number 1 2
Components Under Test i. Main Lift-Eye.
ii. Central Column Load
Bearing Assembly.
iii. Seats and Floor
Structure.
i. Back-Up Lift-Eye.
ii. Central Column Load
Bearing Assembly.
iii. Seats and Floor Structure.
Test Proof Load 1770 kg (3894 lb) 1770 kg (3894 lb)
Test Proof Load
Distribution 1180 kg (2596 lb) on the seats
and spread equally between
them.
590 kg (1298 lb) placed on the
floor and distributed evenly. 1180 kg (2596 lb) on the seats and
spread equally between them.
590 kg (1298 lb) placed on the floor
and distributed evenly.
Basis of Test Proof Load Twice Maximum Gross Weight,
less Tare Weight**
= 2 x 1200 kg
– 630 kg = 1770 kg
Twice Maximum Gross Weight, less
Tare Weight**
= 2 x 1200 kg
– 630 kg = 1770 kg
Crane Hook Load 2400 kg 2400 kg
Test Method Lift the unit and hold static for 3
minutes. Lift the unit and hold static for 3
minutes.
*-Note See Appendix G for Brazil unit (622) differences
**
Note: The Tare Weight of the FROG-6 is approximately 630 kg but may vary slightly. Each FROG-6 must be weighed
prior to load test.
6.8.2 Inspection Data Plate
An inspection data plate will be issued and attached by the test house, which should show:
i. Tare Weight (kg).
ii. Pay load / SWL (kg).
iii. Maximum gross load (kg).
iv. The load test date (DD/MMM/YYYY).
v. Test load (kg).
vi. The serial number of the FROG-6: HC6-XXX (where XXX is unit I.D. No).
vii. The model number of the FROG-6: HC6-01 (620) or HC6-01 (621) or HC6-01 (622) or HC6-01
(640).
Note: All masses should be stamped in kg and with the imperial mass shown in brackets in lbs where
necessary.
e.g. TARE WEIGHT 630 kg (1389 lbs)
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