Mar 2017 Page 33
DATA ACQUISITION FLIGHT RECORDER Type D51615-202-XXX or D51615-
202-XXX-090 with CCU Type D51616-XXXX and CAM Type D51623-XXXX
Installation and Operating Manual with Illustrated Parts
List
Commercial in Confidence
PIM434-I
© Penny & Giles Aerospace Ltd. No part of this work may be reproduced or distributed by any means
without prior permission in writing from the copyright owner.
Crash Survival
Impact Shock
Subjected as a minimum to an acceleration pulse with the
energy content of a half sine wave of 6.5 millisecond duration
and a peak acceleration of 3400 ‘g’, as defined in ED-112,
section 1, Chapter 2-4.2.1.
Penetration Resistance
Subjected to a penetration force produced by a 227 kg (500
lb.) weight dropped from a height of 3m (10 ft, 2 in) with a
point of contact being a circular steel pin of 6.5 mm (0.25 in)
diameter, as defined in ED-112, section 1, Chapter 2-4.2.2.
Static Crush
Subjected to a 22.25 kN (5000 lb.) static crush on at least four
points and all diagonals for a continuous period of 5 minutes
each, as defined in ED-112, section 1, Chapter 2-4.2.3.
High Temperature Fire
Subjected to a “high temperature” fire test of 60 minutes
duration producing a minimum thermal flux of 158 kW/m
2
(50,000 Btu/ft
2
/hour) and a typical flame temperature of
1100°C, as defined in in ED-112, section 1, Chapter 2-4.2.4.
Low Temperature Fire
Subjected to a 260°C “low temperature” fire test of 10 hours
duration, as defined in in ED-112, section 1, Chapter 2-4.2.5.
Deep Sea Pressure
Subjected to a pressure of 60 MPa (equivalent to immersion in
seawater at a depth of 20,000 ft) for a period of 30 days, as
defined in in ED-112, section 1, Chapter 2-4.2.6.
Sea Water Immersion
Subjected to a sea water immersion test at a depth of 3m (10
ft 2 in) for a period of 30 days.
Fluid Immersion
Subjected to a variety of aircraft fluid immersion tests for a
period of 48 hours, as defined in in ED-112, section 1, Chapter
2-4.2.7.
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