TM 1-1520-240-BD
CHAPTER 2
AIRFRAME
SECTION I. INTRODUCTION
2-1. SCOPE.
a.
This chapter contains methods for assessing
battlefield damage to the primary structure of the CH-
47D airframe, classification of damage, rules for
deferring repair, and expedient field fixes of battlefield
damaged airframe structures.
b.
Aircraft structure is classified as primary and
secondary structure.
(1) The primary structure is the basic structure
which holds the aircraft together. Any serious damage
to any element of the primary structure will restrict the
combat capability of the aircraft. The primary structures
for each major airframe subassembly are defined
throughout this chapter.
(2) Secondary structures are mounted on the
primary structure. No amount of structural damage to
secondary structures will restrict combat capability from
a structural safety point of view; however, secondary
structure may be required for aerodynamic reasons or to
accomplish or support mission functions.
2-2. ASSESSMENT PROCFDURERS. The battlefield
structural damage assessment consists of two steps: an
initial assessment, and a detailed assessment. The
initial assessment is a quick visual assessment to
decide whether or not a detailed assessment should be
made. A detailed assessment involves the identification
of all damage to primary structural elements, possibly
some cleanup and measurement of the damage and of
the damaged elements. This process requires damage
measurement and determination of the corresponding
damage limits. An overall view of all the aircraft zones
used in damage assessment is shown in Figure 2-1.
NOTE
The
standards
contained
herein
allow aircraft to be flown with battle
damage substantially in excess of
peacetime
limits.
Under
no
circumstances shall this manual be
used wholly or in part for peacetime
maintenance
of
the
aircraft.
Assessment of aircraft battle damage
requires extreme care and diligence
and
strict
adherence
to
the
instructions
and
standards
contained in this manual. If at any
stage of damage assessment the
assessor believes that oversights or
errors
have
been
made,
the
assessment shall be stopped at that
point and TM 1-1520-240-BD repeated
from the beginning. Under no
circumstances
shall
the
requirements of this manual be
waived or circumvented without the
express approval of the commander
or his designated representative.
WARNING
·
Battle damaged areas should be
inspected for unexploded ordnance
before attempting repairs. Disposal
of unexploded ordnance should be
accomplished
by
qualified
EOD
personnel.
·
Loaded weapons, or weapons being
loaded or unloaded, shall be pointed
in a direction which offers the least
exposure to personnel or property in
the
event
of
accidental
firing.
Personnel shall remain clear of
hazardous
area
of
all
loaded
weapons.
·
Ground safety pins must be installed
in pilot and gunner arming/firing
handles of canopy removal system
whenever the helicopter is on the
ground. Pins should be installed by
crew.
2-1