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could cause thermal burns and may explode.
NOISE
Sound pressure levels in this helicopter during some operating conditions exceed the Surgeon General’s hearing
conservation criteria as defined in TB MED 501. Hearing protection devices, such as the aviator helmet or ear plugs,
are required to be worn by all personnel in and around the helicopter during its operation.
HIGH VOLTAGE
All ground handling personnel must be informed of high voltage hazards when working near the HF antenna.
TOXIC MATERIALS
The basic stinger missile round and captive flight trainer (CFT) contain mercury thallium. If the IR domes should
break, do not touch the basic stinger missile round or CFT in the vicinity of the IR dome. This material is toxic to
unprotected skin. Avoid all contact with the released material unless protective equipment is being worn, such as a
respirator, gloves, and chemical goggles. If the skin or eyes are exposed to the spilled material, immediately flush
with large quantities of water. Any person exposed to the released materials should be promptly referred to a
physician.
The coolant reservoir, when fully charged, contains high pressure argon gas (up to 6200 psi). When moving or
storing the coolant reservoir, the protective collar must be installed to protect the male disconnect coupling from
being damaged or broken. When handling the coolant reservoir, extreme care must be taken not to drop, damage, or
break any portion of the coolant reservoir. If the coolant reservoir is damaged, high pressure gas could escape
causing the coolant reservoir to become a self-propelled projectile.
Personnel must never be positioned immediately in front of a CFT during operation. The front window can blow out
causing injury to personnel.
WEAPONS AND AMMUNITION
Observe all standard safety precautions governing the handling of weapons and live ammunition when not in use,
point all weapons in a direction away from personnel and property in case of accidental firing.
• Do not walk in front of weapons.
• To avoid potentially dangerous situations, follow all procedural warnings in this text.
• Due to lack of data, structural and aerodynamic effects on the aircraft in the event of a missile/rocket hangfire are
unknown.
• Weapons in containers that fall more than 84 inches are considered unsafe and should only be handled by
qualified personnel.
• DO NOT load a missile round which has been dropped from two or more feet onto a hard surface.
PYLON STORES JETTISON
All jettison safety pins shall be installed when the helicopter is on the ground. Safety pins shall be removed prior to
flight. Failure to do so will prevent jettison of pylon stores.
RADIOACTIVE MATERIALS
Self-luminous dials and ignition units contain radioactive materials. If such an instrument or unit is broken or
becomes unsealed, avoid personnel contact.
b
*TM 1-1520-248-10
i
Technical Manual ) HEADQUARTERS
) DEPARTMENT OF THE ARMY
No. 1-1520-248-10 ) Washington, D.C., 15 November 2001
TECHNICAL MANUAL
OPERATOR’S MANUAL
FOR
ARMY OH-58D
HELICOPTER
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS
You can help improve this manual. If you find any mistakes or if you know of a way to improve the
procedures, please let us know. Mail your letter or DA Form 2028 (Recommended Changes to
Publications and Blank Forms), directly to Commander, U.S. Aviation and Missile Command, ATTN:
AMSAM-MMC-MA-NP, Redstone Arsenal, AL 35898-5000. A reply will be furnished to you. You may
also send in your comments electronically to our e-mail address: 2028@redstone.army.mil or FAX us at
(256) 842-6546/DSN 788-6546.
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
TABLE OF CONTENTS
PAGE
CHAPTER 1 INTRODUCTION ......................................................................................... 1-1
CHAPTER 2 HELICOPTER AND SYSTEMS DESCRIPTION AND OPERATION
Section I Helicopter..................................................................................................... 2-1
Section II Emergency Equipment.............................................................................. 2-22
Section III Engine and Related Systems .................................................................. 2-22
Section IV Fuel System ................................................................................................. 2-32
Section V Flight Control System................................................................................. 2-32
Section VI Hydraulic System ........................................................................................ 2-37
Section VII Power Train System ................................................................................... 2-38
　
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