Draft_-_Attachment_003_BHMT-M_System_Specification.pdf

AVNS-PRF-10269

CAGE CODE 81996

21 July 2010

U.S. ARMY AVIATION and MISSILE COMMAND

Redstone Arsenal, Alabama 35898-5000

PERFORMANCE SPECIFICATION

ITEM SPECIFICATION

FOR THE

UH-60M BLACK HAWK MAINTENANCE TRAINER

(BHMT-M)

Prepared by:

Utility Helicopters Project Manager’s Office

SFAE-AV-UH

Sparkman Center, Building 5308

Redstone Arsenal, AL 35898-5000

DISTRIBUTION STATEMENT D: Distribution authorized to Department of Defense and

U.S. DOD contractors only, for administrative or operational use, as of 28 April 2000. Other requests shall be referred to the Utility Helicopters Project Office.

CAGE CODE 81996

AUlllENTICATEDBY:

Roger Olson

Production Support Branch Chief

Technical Management Division, UHPO

DATE: II A ID

I HAVE READ TilE CONTENTS OF AVNS-PRF-10269, RELATIVE TO ACQUISITION REFORM, AND CERTIFY

THAT IT MEETS TilE REQUIREMENTS OF MIL-STD-

96 AS.A.PROGfAM-UNlQUE S ECIFICATION.

I HAVE READ TilE CONTENTS OF AVNS-PRF-10269

AND CERTIFY THAT IT IS A USER PRODUCT-BASED

DOCUMENT.

' DATE: !) /0

Patricia T. Martin

U.S. Army Aviation and Mi ilc Command and PEO.

Aviation Standards Executive

APPROVED

FOR USE AS A FUNCTIONAL BASELINE BY:

Terence W. Reeves

COLAV

Commanding US Army Aviation Logistics School, Fort Eustis, VA 23604

DATE: lf .4Ulrf¢

— iii —

SUBMITTED BY: _________________________________ DATE: ______________

Richard A. King

UH Project Office

APM, TADSS

AUTHENTICATED BY: __________________________________ DATE:_________

Roger Olson

Production Support Branch Chief

Technical Management Division, UHPO

I HAVE READ THE CONTENTS OF AVNS-DTL-10269,

RELATIVE TO ACQUISITION REFORM, AND CERTIFY

THAT IT MEETS THE REQUIREMENTS OF MIL-STD-

961E AS A PROGRAM-UNIQUE SPECIFICATION.

________________________________ DATE: __________

Patricia T. Martin

U.S. Army Aviation and Missile Command and PEO. Aviation

Standards Executive

I HAVE READ THE CONTENTS OF AVNS-DTL-10269

AND CERTIFY THAT IT IS A USER PRODUCT-BASED

DOCUMENT.

Terence W. Reeves

COL AV

Commanding, US Army Aviation Logistics School, Fort

Eustis, VA 23604

APPROVED FOR USE AS A FUNCTIONAL BASELINE BY:

COL L. Neil Thurgood

Project Manager, Utility Helicopters

— iv —

TABLE OF CONTENTS

1 SCOPE

1.1 Identification

1.2 System Overview

2 APPLICABLE DOCUMENTS

2.1 General

2.2 Government Documents

2.2.1 Specifications, Standards, and Handbooks

2.2.2 Other Government Documents, Drawings, and Publications

2.3 Non-Government Documents

2.4 Order of Precedence

3 REQUIREMENTS

3.1 Definitions

3.2 Physical and Functional Characteristics

3.2.1 Computer Architecture Systems

3.2.1.1 Computer Core System

3.2.1.1.1 Computer Core System Response Time

3.2.1.2 Host Computer

3.2.1.2.1 Remote Host Computer System

3.2.1.2.2 Aural Cues in Real Time

3.2.1.2.3 Audio System (AS) Output

3.2.1.2.4 Host Interface Capability

3.2.1.2.5 Graphics Computer System (GCS) Interface with Host Computer

3.2.1.2.5.1 Graphics

3.2.1.3 Graphic Distribution System (GDS)

3.2.2 Device Software Systems

3.2.2.1 Trainer System Software (TSS)

3.2.2.1.1 Trainer System Software Wiring

3.2.2.2 Student Station System Software (SSSS)

3.2.2.2.1 Fault Implementation

3.2.2.2.1.1 Integrated Training Suite Faults

3.2.2.2.1.2 Power During Fault

3.2.2.2.2 System Alarm

3.2.2.2.2.1 Heat Shutdown

3.2.2.2.3 Intercommunications System (ICS) between Instructor and Students

3.2.2.2.3.1 Audio System Intercommunications

3.2.2.2.3.2 Audio System (AS) Operations

3.2.2.2.3.3 Aural Cueing

3.2.2.2.3.4 Alerts

3.2.3 Instructor Operator Station (IOS)

3.2.3.1 IOS Remote Desktop

3.2.3.1.1 IOS Remote Desktop Monitoring

3.2.3.2 IOS Interactive Electronic Technical Manuals (IETM

3.2.3.2.1 IOS IETM Software Update

3.2.3.3 Daily Operational Readiness Test (DORT)

3.2.3.3.1 DORT Report

3.2.3.4 Student Action Log (SAL)

3.2.3.4.1 SAL Function

— v —

3.2.3.4.2 SAL Access

3.2.3.5 IOS Menu

3.2.3.5.1 IOS Menu Format

3.2.3.5.2 IOS Input

3.2.3.6 IOS Unique Function

3.2.3.6.1 IOS Key Switch

3.2.3.6.2 IOS Shutdown

3.2.3.6.3 IOS Connection to Emergency Power Off (EPO) Switches

3.2.3.6.4 IOS Temperature Monitoring

3.2.3.7 Headset Jacks

3.2.3.7.1 Headsets

3.2.3.7.2 Wireless Headset

3.2.3.8 IOS Cabinetry

3.2.3.8.1 IOS Structure Size

3.2.3.8.2 IOS Cabinet Writing Surface

3.2.3.8.3 IOS Cabinet Drawers

3.2.3.8.4 IOS Monitor

3.2.3.9 IOS Portability

3.2.3.9.1 IOS Casters

3.2.4 Student Station (SS) Physical Attributes

3.2.4.1 SS Dimensions

3.2.4.1.1 SS Length

3.2.4.1.2 SS Height

3.2.4.1.3 SS Width

3.2.4.1.4 SS Weight

3.2.4.2 Device Mobility

3.2.4.2.1 SS Towing

3.2.4.2.2 Interface with Tugs

3.2.4.2.3 Device Transportability

3.2.4.3 SS Center of Gravity

3.2.4.4 Alignment

3.2.4.5 Jacking Points

3.2.4.6 Tail Rotor Rigging

3.2.4.7 Student Station Access

3.2.4.7.1 Physical Device Accessibility

3.2.4.7.2 Access for Maintenance

3.2.4.8 Student Station Steps

3.2.4.9 Student Station Sound Proofing

3.2.4.10 Intercommunications System (ICS) Hook-Ups

3.2.4.11 Operational Sounds Speakers

3.2.4.12 Temperature Sensors

3.2.4.12.1 Temperature Sensors Warning

3.2.4.12 .2 Additional Temperature Sensors

3.2.4.12.3 Standard Equipment Temperature

3.2.4.13 Emergency Power Off (EPO) System

3.2.4.13.1 EPO Installation Sites

3.2.4.13.2 EPO Installation Type

3.2.4.13.3 EPO Switch Labels

3.2.4.14 Electromagnetic Emission

3.2.4.15 Electrostatic Discharge (ESD) Assembles and Equipment

3.2.4.15.1 ESD Symbol Visibility

— vi —

3.2.4.15.2 ESD Caution Statement

3.2.4.16 Aircraft Wiring System (AWS)

3.2.4.16.1 AWS Interface

3.2.4.16.2 AWS Connectors

3.2.4.16.3 AWS Cable Runs

3.2.4.16.4 Standards for AWS

3.2.4.17 Trainer Unique Wiring

3.2.4.18 Electrical Systems

3.2.4.19 Connector Type and Backshell

3.2.4.20 Alternating Current (AC)

3.2.4.21 Direct Current (DC)

3.2.4.22 Auxiliary Outlet

3.2.4.23 Lighting System

3.2.4.23.1 Trainer Lighting

3.2.4.24 Display Viewing

3.2.4.25 Built-In Test (BIT)

3.2.4.26 Panels and Switches

3.2.4.27 Busses

3.2.4.27.1 Buss Couplers and Terminators

3.2.4.28 Aircraft Component Fasteners

3.2.4.29 Identification (ID) Plate Compliance

3.2.4.29.1 Auxiliary Unit ID Plate

3.2.4.30 Toxic Products

3.2.4.31 Exterior Color

3.2.4.32 Interior Color

3.2.4.33 Corrosion Prevention

3.2.4.34 Product Marking

3.2.4.34.1 Exterior Markings

3.2.4.34.2 Trainer Peculiar Component Marking

3.2.4.34.3 Markings - Environment

3.2.4.34.4 Markings - Cleaning

3.2.4.34.5 Color of Markings

3.2.4.34.6 Printed Wiring Boards Markings

3.2.4.34.7 Marking Distances

3.2.4.34.8 Utility of Markings

3.2.4.34.9 Plug-In Assemblies Markings

3.2.4.34.10 Socket Markings

3.2.4.34.11 Auxiliary Unit Markings

3.2.4.34.12 Warning Markings for Modified Equipment

3.2.4.34.12.1 Warning Markings for Simulated Equipment

3.2.4.34.13 Type of Lettering

3.2.4.34.14 Type of Numbers

3.2.4.34.15 Government Furnished Equipment (GFE) Auxiliary Units

3.2.4.34.16 Permanent Coding

3.2.4.34.17 Plug-In Side of Socket

3.2.4.34.18 Reverse Side of Plug-In

3.2.4.34.19 Alternative Location

3.2.4.34.20 Unmodified Commercial Items

3.2.4.35 Terminals

3.2.4.35.1 Terminal Location

3.2.4.35.2 Terminal Trainer Peculiar Equipment (TPE)

— vii —

3.2.4.35.3 Terminal Exemptions

3.2.4.36 Terminal Blocks

3.2.4.36.1 Terminal Block Location

3.2.4.36.2 Terminal Blocks Trainer Peculiar Equipment

3.2.4.36.3 Terminal Blocks Exemptions

3.2.4.37 Strips

3.2.4.37.1 Strip Location

3.2.4.37.2 Strip Trainer Peculiar Equipment (TPE)

3.2.4.37.3 Strip Exemptions

3.2.4.38 Trainer-Use-Only Identification

3.2.4.39 Sticker or Nameplate Location

3.2.4.40 Interchangeability of Trainer Peculiar Equipment (TPE) Parts

3.2.5 Student Station (SS) System Components

3.2.5.1 Assembly Components

3.2.5.2 Constructed Components

3.2.5.3 Modeled Components

3.2.5.4 Active Vibration Control System (AVCS)

3.2.5.4.1 AVCS Replication

3.2.5.4.2 AVCS Vibration

3.2.5.5 Stabilator

3.2.5.5.1 Trainer’s Stabilator

3.2.5.6 SS Flight Controls

3.2.5.6.1 Flight Control Rigging

3.2.5.7 Flight Management System (FMS)

3.2.5.7.1 Flight Management System (FMS) Replication

3.2.5.8 Multi Function Displays (MFD) Replication

3.2.5.9 Flight Director/Display Control Panels (FD/DCP) Replication

3.2.5.10 Engine Instrument and Crew Alert System (EICAS)

3.2.5.10.1 EICAS Warnings

3.2.5.10.2 EICAS Multi-Function Display

3.2.5.11 Reversionary Panel

3.2.5.12 Master Warning System (MWS)

3.2.5.13 Avionics Systems

3.2.5.13.1 Line Replaceable Unit (LRU) Size

3.2.5.14 Components for Multi-Function Slew Controllers

3.2.5.15 Landing Gear System

3.2.5.16 Brake System

3.2.5.17 Tail Wheel and Tail Wheel Lock System

3.2.5.17.1 Tail Wheel System

3.2.5.18 Main Landing Gear

3.2.5.19 Integrated Vehicle Health Management System (IVHMS)

3.2.5.19.1 IVHMS Faults

3.2.5.19.2 IVHMS On-Board Systems (OBS)

3.2.5.19.3 IVHMS Ground Station Computer (GSC)

3.2.5.20 Locating Device

3.2.5.21 Drive Train

3.2.5.21.1 Transmission Chip Detectors

3.2.5.21.2 Main Rotor System Rotation

3.2.5.21.3 Tail Rotor Revolutions per Minute (rpm)

3.2.5.21.4 Power Plant and Drive Train Indications

3.2.5.22 Rotor Brake System

— viii —

3.2.5.22.1 Rotor Model and Control

3.2.5.22.2 Rotor Brake Pad Observation

3.2.5.22.3 Rotor Brake Pads

3.2.5.22.4 Malfunction of Quadrant’s Solenoid

3.2.5.22.5 Clearance of Solenoid Malfunction

3.2.5.22.6 Rotor Brake Indications

3.2.5.23 Gust Lock

3.2.5.24 Rotor Systems

3.2.5.25 Main Rotor System

3.2.5.25.1 Reduction of Blades

3.2.5.25.2 Type of Blade

3.2.5.26 Tail Rotor Systems

3.2.5.27 Power Plants

3.2.5.27.1 Installation of Engine Components

3.2.5.27.2 Engine Performance

3.2.5.27.3 Individual Engine Operation

3.2.5.27.4 Engine Warnings and Alerts

3.2.5.28 Hydraulic System

3.2.5.28.1 Hydraulic Pressure Control

3.2.5.28.2 Hydraulic Pressure Simulation

3.2.5.28.3 Hydraulic System Drain Back

3.2.5.29 Pitot Static System

3.2.5.30 Air Data Computer System

3.2.5.31 Outside Air Temperature (OAT) Indication

3.2.5.32 Fuel System

3.2.5.32.1 Fuel Tank

3.2.5.32.2 Fuel Modeling

3.2.5.32.3 Fuel Controls

3.2.5.33 Fuel Low Level Warning System

3.2.5.34 Submerged Fuel Boost Pump System

3.2.5.35 Fuel Prime Boost System

3.2.5.35.1 Pump Sound

3.2.5.35.2 Radiating Pump Sound

3.2.5.36 Pressure Refuel/Defuel System

3.2.5.37 Fuel Quantity System

3.2.5.37.1 Fuel Quantity in Tanks

3.2.5.37.2 Fuel Depletion

3.2.5.38 Crashworthy External Fuel System (CEFS)

3.2.5.38.1 CEFS Tank Exterior Features

3.2.5.38.2 CEFS Tank Weight and Balance

3.2.5.38.3 CEFS Tank Interface

3.2.5.38.4 CEFS Tank Viewing Window

3.2.5.39 External Stores Support System (ESSS)

3.2.5.40 Crew Seating

3.2.5.41 Gunner Seats

3.2.5.42 Troop Seating

3.2.5.43 Utility System

3.2.5.43.1 Utility System Panels and Switches

3.2.5.44 Fire Detection System

3.2.5.45 Fire Extinguishing System

3.2.5.45.1 Fire Extinguishing System Discharge

— ix —

3.2.5.45.2 Bottle Recharging

3.2.5.46 Windshield Wiper and Windshield Anti-Ice Systems

3.2.5.46.1 Windshield Anti-Ice System

3.2.5.47 Blade De-Ice System

3.2.5.47.1 Blade De-Ice System Indications

3.2.5.48 Cargo Hook System

3.2.5.48.1 Squib

3.2.5.48.2 Squib Replenishing

3.2.5.48.3 Cargo Hook System Control

3.2.5.48.4 Pendant

3.2.5.49 Heating and Ventilation System

3.2.5.50 Auxiliary Power Unit (APU) System

3.2.5.51 Navigation Systems

3.2.5.51.1 Navigation Systems Connections

3.2.5.52 Digital Clock

3.2.5.53 Communication Systems

3.2.5.53.1 Communication Systems Connections

3.2.5.54 Aircraft Test Sets (ATS)

3.2.5.54.1 Test Set Capability

3.2.5.55 Aircraft Survivability Equipment (ASE)

3.2.5.55.1 ASE Connections

3.2.5.56 Aviation Ground Support Equipment (AGSE)

3.2.5.57 Peculiar Ground Support Equipment (PGSE)

3.2.5.58 Preventive Maintenance Daily (PMD)

3.2.5.59 Preventive Maintenance Service (PMS)

3.2.5.60 40-Hour Inspection

3.2.5.61 120-Hour Inspection

3.2.6 Power Supply

3.2.6.1 Power Supply Power Source

3.2.6.2 Power Supply Generation of Hydraulic Pressure

3.2.6.3 External Hydraulic Pressure Control

3.2.6.4 Power Supply Portability

3.2.7 Maintenance Platform (MP)

3.2.7.1 MP Occupational Safety and Health Administration (OSHA) Requirements

3.2.7.2 MP Design

3.2.7.3 MP Support Requirements

3.2.7.4 MP Color

3.2.7.5 MP Shape

3.2.7.6 MP Access Steps

3.2.7.6.1 MP Step Dimensions

3.2.7.6.2 MP Step Safety Marking

3.2.7.7 MP Work Area

3.2.7.8 MP Safety Hand Rails

3.2.7.9 MP Separate from Trainer

3.2.7.10 MP Casters

3.2.7.11 MP Leveling Capability

3.2.7.12 MP Mobility

3.2.7.13 MP Lighting

3.2.7.14 MP Safety Padding

3.2.7.15 MP Front and Rear

3.2.7.15.1 MP Front Section Coverage

— x —

3.2.7.15.2 MP Front Section Access

3.2.7.15.3 MP Front Section Engine Cowlings

3.2.7.15.4 MP Front Section Hand Rails

3.2.7.15.5 MP Rear Section Coverage

3.2.7.15.6 MP Rear Extension

3.2.7.15.7 MP Rear Interference

3.2.7.15.8 Capability of the MP Rear Section

3.2.7.15.9 MP Rear Height

3.2.7.16 MP Quick Disconnects

4 VERIFICATION

4.1 General

4.2 Physical and Functional Characteristics

4.2.1 Computer Architecture Systems

4.2.1.1 Computer Core System

4.2.1.1.1 Computer Core System Response Time

4.2.1.2 Host Computer

4.2.1.2.1 Remote Host Computer System

4.2.1.2.2 Aural Cues in Real Time

4.2.1.2.3 Audio System (AS) Output

4.2.1.2.4 Host Interface Capability

4.2.1.2.5 Graphics Computer System (GCS) Interface with Host Computer

4.2.1.2.5.1 Graphics

4.2.1.3 Graphic Distribution System (GDS)

4.2.2 Device Software Systems

4.2.2.1 Trainer System Software (TSS)

4.2.2.1.1 Trainer System Software Wiring

4.2.2.2 Student Station System Software (SSSS)

4.2.2.2.1 Fault Implementation

4.2.2.2.1.1 Integrated Training Suite Faults

4.2.2.2.1.2 Power During Fault

4.2.2.2.2 System Alarm

4.2.2.2.2.1 Heat Shutdown

4.2.2.2.3 Intercommunications System (ICS) between Instructor and Students

4.2.2.2.3.1 Audio System (AS) Intercommunications

4.2.2.2.3.2 Audio System (AS) Operations

4.2.2.2.3.3 Aural Cueing

4.2.2.2.3.4 Alerts

4.2.3 Instructor Operator Station (IOS)

4.2.3.1 IOS Remote Desktop

4.2.3.1.1 IOS Remote Desktop Monitoring

4.2.3.2 IOS Interactive Electronic Technical Manuals (IETM) Capability

4.2.3.2.1 IOS IETM Software Update

4.2.3.3 Daily Operational Readiness Test (DORT)

4.2.3.3.1 DORT Report

4.2.3.4 Student Action Log (SAL)

4.2.3.4.1 SAL Function

4.2.3.4.2 SAL Access

4.2.3.5 IOS Menu

4.2.3.5.1 IOS Menu Format

4.2.3.5.2 IOS Input

— xi —

4.2.3.6 IOS Unique Function

4.2.3.6.1 IOS Key Switch

4.2.3.6.2 IOS Shutdown

4.2.3.6.3 IOS Connection to Emergency Power Off (EPO) Switches

4.2.3.6.4 IOS Temperature Monitoring - Demonstration

4.2.3.7 Headset Jacks

4.2.3.7.1 Headsets

4.2.3.7.2 Wireless Headset

4.2.3.8 IOS Cabinetry

4.2.3.8.1 IOS Structure Size

4.2.3.8.2 IOS Cabinet Writing Surface

4.2.3.8.3 IOS Cabinet Drawers

4.2.3.8.4 IOS Monitor

4.2.3.9 IOS Portability

4.2.3.9.1 IOS Casters

4.2.4 Student Station (SS) Physical Attributes

4.2.4.1 SS Dimensions

4.2.4.1.1 SS Length

4.2.4.1.2 SS Height

4.2.4.1.3 SS Width

4.2.4.1.4 SS Weight

4.2.4.2 Device Mobility

4.2.4.2.1 SS Towing

4.2.4.2.2 Interface with Tugs

4.2.4.2.3 Device Transportability

4.2.4.3 SS Center of Gravity

4.2.4.4 Alignment

4.2.4.5 Jacking Points

4.2.4.6 Tail Rotor Rigging

4.2.4.7 Student Station Access

4.2.4.7.1 Physical Device Accessibility

4.2.4.7.2 Access for Maintenance

4.2.4.8 Student Station Steps

4.2.4.9 Student Station Sound Proofing

4.2.4.10 Intercommunications System (ICS) Hook-Ups

4.2.4.11 Operational Sounds Speakers

4.2.4.12 Temperature Sensors

4.2.4.12.1 Temperature Sensors Warning

4.2.4.12 .2 Additional Temperature Sensors

4.2.4.12.3 Standard Equipment Temperature

4.2.4.13 Emergency Power Off (EPO) System

4.2.4.13.1 EPO Installation Sites

4.2.4.13.2 EPO Installation Type

4.2.4.13.3 EPO Switch Labels

4.2.4.14 Electromagnetic Emission

4.2.4.15 Electrostatic Discharge (ESD) Assembles and Equipment

4.2.4.15.1 ESD Symbol Visibility -

4.2.4.15.2 ESD Caution Statement

4.2.4.16 Aircraft Wiring System (AWS)

4.2.4.16.1 AWS Interface

4.2.4.16.2 AWS Connectors

— xii —

4.2.4.16.3 AWS Cable Runs

4.2.4.16.4 Standards for AWS

4.2.4.17 Trainer Unique Wiring

4.2.4.18 Electrical Systems

4.2.4.19 Connector Type and Backshell

4.2.4.20 Alternating Current (AC)

4.2.4.21 Direct Current (DC)

4.2.4.22 Auxiliary Outlet

4.2.4.23 Lighting System

4.2.4.23.1 Trainer Lighting

4.2.4.24 Display Viewing

4.2.4.25 Built-In Test (BIT)

4.2.4.26 Panels and Switches

4.2.4.27 Busses

4.2.4.27.1 Buss Couplers and Terminators

4.2.4.28 Aircraft Component Fasteners

4.2.4.29 Identification (ID) Plate Compliance

4.2.4.29.1 Auxiliary Unit ID Plate

4.2.4.30 Toxic Products

4.2.4.31 Exterior Color

4.2.4.32 Interior Color

4.2.4.33 Corrosion Prevention

4.2.4.34 Product Marking

4.2.4.34.1 Exterior Markings

4.2.4.34.2 Trainer Peculiar Component Marking

4.2.4.34.3 Markings – Environment

4.2.4.34.4 Markings Cleaning

4.2.4.34.5 Color of Markings

4.2.4.34.6 Printed Wiring Boards Markings

4.2.4.34.7 Marking Distances

4.2.4.34.8 Utility of Markings

4.2.4.34.9 Plug-In Assemblies Markings

4.2.4.34.10 Socket Markings

4.2.4.34.11 Auxiliary Unit Markings

4.2.4.34.12 Warning Markings for Modified Equipment

4.2.4.34.12.1 Warning Markings for Simulated Equipment

4.2.4.34.13 Type of Lettering

4.2.4.34.14 Type of Numbers

4.2.4.34.15 Government Furnished Equipment (GFE) Auxiliary Units

4.2.4.34.16 Permanent Coding

4.2.4.34.17 Plug-In Side of Socket

4.2.4.34.18 Reverse Side of Plug-In

4.2.4.34.19 Alternative Location

4.2.4.34.20 Unmodified Commercial Items

4.2.4.35 Terminals

4.2.4.35.1 Terminal Location

4.2.4.35.2 Terminal Trainer Peculiar Equipment (TPE)

4.2.4.35.3 Terminal Exemptions

4.2.4.36 Terminal Blocks

4.2.4.36.1 Terminal Block Location

4.2.4.36.2 Terminal Blocks Trainer Peculiar Equipment (TPE)

— xiii —

4.2.4.36.3 Terminal Blocks Exemptions

4.2.4.37 Strips

4.2.4.37.1 Strip Location

4.2.4.37.2 Strip Trainer Peculiar Equipment (TPE

4.2.4.37.3 Strip Exemptions

4.2.4.38 Trainer-Use-Only Identification

4.2.4.39 Sticker or Nameplate Location

4.2.4.40 Interchangeability of Trainer Peculiar Equipment (TPE) Parts

4.2.5 Student Station (SS) System Components

4.2.5.1 Assembly Components

4.2.5.2 Constructed Components

4.2.5.3 Modeled Components

4.2.5.4 Active Vibration Control System (AVCS)

4.2.5.4.1 AVCS Replication

4.2.5.4.2 AVCS Vibration

4.2.5.5 Stabilator

4.2.5.5.1 Trainer’s Stabilator

4.2.5.6 SS Flight Controls

4.2.5.6.1 Flight Control Rigging

4.2.5.7 Flight Management System (FMS)

4.2.5.7.1 Flight Management System (FMS) Replication

4.2.5.8 Multi Function Displays (MFD) Replication

4.2.5.9 Flight Director/Display Control Panels (FD/DCP) Replication

4.2.5.10 Engine Instrument and Crew Alert System (EICAS)

4.2.5.10.1 EICAS Warnings

4.2.5.10.2 EICAS Multi Function Display (MFD)

4.2.5.11 Reversionary Panel

4.2.5.12 Master Warning System (MWS)

4.2.5.13 Avionics Systems

4.2.5.13.1 Line Replaceable Unit (LRU) Size

4.2.5.14 Components for Multi-Function Slew Controllers

4.2.5.15 Landing Gear System

4.2.5.16 Brake System

4.2.5.17 Tail Wheel and Tail Wheel Lock System

4.2.5.17.1 Tail Wheel System

4.2.5.18 Main Landing Gear

4.2.5.19 Integrated Vehicle Health Management System (IVHMS)

4.2.5.19.1 IVHMS Faults

4.2.5.19.2 IVHMS On-Board Systems (OBS)

4.2.5.19.3 IVHMS Ground Station Computer (GSC)

4.2.5.20 Locating Device

4.2.5.21 Drive Train

4.2.5.21.1 Transmission Chip Detectors

4.2.5.21.2 Main Rotor System Rotation

4.2.5.21.3 Tail Rotor Revolutions per Minute (rpm)

4.2.5.21.4 Power Plant and Drive Train Indications

4.2.5.22 Rotor Brake System

4.2.5.22.1 Rotor Model and Control

4.2.5.22.2 Rotor Brake Pads Observation

4.2.5.22.3 Rotor Brake Pads

4.2.5.22.4 Malfunction of Quadrant’s Solenoid

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4.2.5.22.5 Clearance of Solenoid Malfunction

4.2.5.22.6 Rotor Brake Indications

4.2.5.23 Gust Lock

4.2.5.24 Rotor Systems

4.2.5.25 Main Rotor System

4.2.5.25.1 Reduction of Blades

4.2.5.25.2 Type of Blade

4.2.5.26 Tail Rotor Systems

4.2.5.27 Power Plants

4.2.5.27.1 Installation of Engine Components

4.2.5.27.2 Engine Performance

4.2.5.27.3 Individual Engine Operation

4.2.5.27.4 Engine Warnings and Alerts

4.2.5.28 Hydraulic System

4.2.5.28.1 Hydraulic Pressure Control

4.2.5.28.2 Hydraulic Pressure Simulation

4.2.5.28.3 Hydraulic System Drain Back

4.2.5.29 Pitot Static System

4.2.5.30 Air Data Computer System

4.2.5.31 Outside Air Temperature (OAT) Indication

4.2.5.32 Fuel System

4.2.5.32.1 Fuel Tank

4.2.5.32.2 Fuel Modeling

4.2.5.32.3 Fuel Controls

4.2.5.33 Fuel Low Level Warning System

4.2.5.34 Submerged Fuel Boost Pump System

4.2.5.35 Fuel Prime Boost System

4.2.5.35.1 Pump Sound

4.2.5.35.2 Radiating Pump Sound

4.2.5.36 Pressure Refuel/Defuel System

4.2.5.37 Fuel Quantity System

4.2.5.37.1 Fuel Quantity in Tanks

4.2.5.37.2 Fuel Depletion

4.2.5.38 Crashworthy External Fuel System (CEFS)

4.2.5.38.1 CEFS Tank Exterior Features

4.2.5.38.2 CEFS Tank Weight and Balance

4.2.5.38.3 CEFS Tank Interface

4.2.5.38.4 CEFS Tank Viewing Window

4.2.5.39 External Stores Support System (ESSS)

4.2.5.40 Crew Seating

4.2.5.41 Gunner Seats

4.2.5.42 Troop Seating

4.2.5.43 Utility System

4.2.5.43.1 Utility System Panels and Switches

4.2.5.44 Fire Detection System

4.2.5.45 Fire Extinguishing System

4.2.5.45.1 Fire Extinguishing System Discharge

4.2.5.45.2 Bottle Recharging

4.2.5.46 Windshield Wiper and Windshield Anti-Ice Systems

4.2.5.46.1 Windshield Anti-Ice System

4.2.5.47 Blade De-Ice System

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4.2.5.47.1 Blade De-Ice System Indications

4.2.5.48 Cargo Hook System

4.2.5.48.1 Squib

4.2.5.48.2 Squib Replenishing

4.2.5.48.3 Cargo Hook System Control

4.2.5.48.4 Pendant

4.2.5.49 Heating and Ventilation System

4.2.5.50 Auxiliary Power Unit (APU) System

4.2.5.51 Navigation Systems

4.2.5.51.1 Navigation Systems Connections

4.2.5.52 Digital Clock

4.2.5.53 Communication Systems

4.2.5.53.1 Communication Systems Connections

4.2.5.54 Aircraft Test Sets (ATS)

4.2.5.54.1 Test Set Capability

4.2.5.55 Aircraft Survivability Equipment (ASE)

4.2.5.55.1 ASE Connections

4.2.5.56 Aviation Ground Support Equipment (AGSE)

4.2.5.57 Peculiar Ground Support Equipment (PGSE)

4.2.5.58 Preventive Maintenance Daily (PMD)

4.2.5.59 Preventive Maintenance Service (PMS)

4.2.5.60 40-Hour Inspection

4.2.5.61 120-Hour Inspection

4.2.6 Power Supply

4.2.6.1 Power Supply Power Source

4.2.6.2 Power Supply Generation of Hydraulic Pressure

4.2.6.3 External Hydraulic Pressure Control

4.2.6.4 Power Supply Portability

4.2.7 Maintenance Platform (MP)

4.2.7.1 MP Occupational Safety and Health Administration (OSHA) Requirements

4.2.7.2 MP Design

4.2.7.3 MP Support Requirements

4.2.7.4 MP Color

4.2.7.5 MP Shape

4.2.7.6 MP Access Steps

4.2.7.6.1 MP Step Dimensions

4.2.7.6.2 MP Step Safety Marking

4.2.7.7 MP Work Area

4.2.7.8 MP Safety Hand Rails

4.2.7.9 MP Separate from Trainer

4.2.7.10 MP Casters

4.2.7.11 MP Leveling Capability

4.2.7.12 MP Mobility

4.2.7.13 MP Lighting

4.2.7.14 MP Safety Padding

4.2.7.15 MP Front and Rear

4.2.7.15.1 MP Front Section Coverage

4.2.7.15.2 MP Front Section Access

4.2.7.15.3 MP Front Section Engine Cowlings

4.2.7.15.4 MP Front Section Hand Rails

4.2.7.15.5 MP Rear Section Coverage

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4.2.7.15.6 MP Rear Extension

4.2.7.15.7 MP Rear Interference

4.2.7.15.8 Capability of the MP Rear Section

4.2.7.15.9 MP Rear Height

4.2.7.16 MP Quick Disconnects

5 PACKAGING

6 NOTES

6.1 Acronyms and Abbreviations

6.2 Definitions

6.3 Guidance Documentation

APPENDIX A - BHMT-M TASK LIST FIDELITY MATRIX OVERVIEW

List of Figures

Figure 1. ESD Symbol Figure 2. ESD Caution Statement Figure 3. Example of ID Plate Figure 4. Example of Warning Sign for Ground Trainer Use Only

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1 SCOPE

1.1 Identification

The UH-60M BLACK HAWK Maintenance Trainer (BHMT-M) is a training device that will be used by the United States Army Aviation School (USAALS) for training system familiarization, component identification, servicing, Maintenance Operational Checks (MOCs), Fault Isolation Procedures (FIPs), Remove/Install (R/I), and repair of the UH-60M aircraft in support of Military Occupational Specialty

(MOS) 15T10 and 15T30 personnel. All equipment functions, operations, responses and interfaces will replicate those of a UH-60M aircraft configuration MY-VII, ship #31 (M31).

1.2 System Overview

The major configuration items, Computer Systems, Software Systems, Instructor Operator Station (IOS), Student Station (SS), Aircraft Test Sets, Power Supply, and Maintenance Platform create the complete training environment.

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2 APPLICABLE DOCUMENTS

2.1 General

The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, documents users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed.

2.2 Government Documents

2.2.1 Specifications, Standards, and Handbooks

MIL-STD-130N Identification Markings of US Military Property 17 Dec 2007

MIL-HDBK-454B Standard General Requirements for Electronic Equipment 22 Sep 1994

MIL-STD-1553B (4) Digital Time Division Command/Response Multiples Data Bus 15 Jan 1995

Copies of the above specifications, standards, and handbooks are available from http://assist.daps.dla.mil

2.2.2 Other Government Documents, Drawings, and Publications

ARINC 429 Application-Specific Standards for Aircraft Avionics 16 Jul 2004

EM 0051 Interactive Electronic Technical Manual for Army Models 01 Aug 2008

UH-60A, UH-60L, EH-60A, UH-60Q and HH-60L

Helicopters

SMPTE 292 Broadcast Digital Standard 06 Dec 2007

TM 1-1520-280-10 Operator’s Manual for Army UH-60M Helicopter 14 Aug 2009

TM 1-1520-280-23 Aviation Unit and Intermediate Maintenance for Helicopters 31 Mar 2008

TM 1-1520-280-CL Operator and Crew Member’s Checklist 04 Aug 2008

TM 55-1500-345-23 Painting and Marking of Army Aircraft 12 Jun 1986

TM 55-1500-344-23 Cleaning & Corrosion Control, Volume 1 Corrosion Program 01 June 1990

Volume 2 Aircraft, Volume 3 Avionics and Volume 4 Consumable Materials

(Unless otherwise indicated, copies of the above specifications may be obtained from Utility Helicopters

Project Office, SFAE-AV-UH, Sparkman Center, Building 5308, Redstone Arsenal, AL 35898-5000.)

2.3 Non-Government Documents

EIA RS-471 Electronic Industries Assoc. For Symbols and Labels for Electronics Aug 1988

(Unless otherwise indicated, copies of the above specification may be obtained from Utility Helicopters

Project Office, SFAE-AV-UH, Sparkman Center, Building 5308, Redstone Arsenal, AL 35898-5000.)

http://assist.daps.dla.mil/

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2.4 Order of Precedence

In the event of a conflict between the text of this specification and the references cited, the text of this specification takes precedence. Nothing in the specification, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

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3 REQUIREMENTS

3.1 Definitions

Definitions of terms used in this document are listed in Section 6.

3.2 Physical and Functional Characteristics

Systems installed in this Training System shall be populated with components that meet identified physical and functional fidelities. Physical and functional fidelity requirements for components are defined in paragraph 6.2. The BHMT-M System is comprised of the following main components:

3.2.1 Computer Architecture Systems

3.2.2 Device Software Systems

3.2.3 Instructor Operator Station (IOS)

3.2.4 Student Station (SS) Physical Attributes

3.2.5 Student Station (SS) System Components

3.2.6 Power Supply

3.2.7 Maintenance Platform

3.2.1 Computer Architecture Systems

The device computer architecture systems shall consist of the following:

Computer Core System

Host Computer

Graphic Distribution System

3.2.1.1 Computer Core System

The computer core system shall allow for future unused processing capacity growth of 50 percent.

3.2.1.1.1 Computer Core System Response Time

Computer core system response time for training functions shall be in real time.

3.2.1.2 Host Computer

The host computer shall be accessed from the IOS through the use of internal host family control.

3.2.1.2.1 Remote Host Computer System

The host computer system and instructor operating station shall have remote capabilities to function as a redundant system.

3.2.1.2.2 Aural Cues in Real Time

Aural cues shall respond to host computer commands in real time to ensure that proper cues are heard throughout the Intercommunication Systems (ICS) with aural cueing system responding to normal and abnormal aircraft system operations.

3.2.1.2.3 Audio System (AS) Output

The host computer shall supply the sounds for the AS.

3.2.1.2.4 Host Interface Capability

The host computer system shall interface with all the additional computer systems through network protocol capable of real-time applications.

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3.2.1.2.5 Graphics Computer System (GCS) Interface with Host Computer

The GCS shall interface with the host computer through an Ethernet protocol of real-time applications.

3.2.1.2.5.1 Graphics

The GCS shall generate the graphics for the following displays:

a) Multi Function Displays (MFD) Quantity – 4

b) Flight Management System (FMS) Quantity – 2

c) Electronic Stand-By Instrument (ESIS) Quantity – 1

d) Flight Director/Display Control Panels (FD/DCP) Quantity – 2

e) Ground Station Computer (GSC) Quantity – 1

f) Instructor Operator Station (IOS) Display Quantity – 2

3.2.1.3 Graphic Distribution System (GDS)

The GDS shall have a function for repeating crew station displays at the IOS for selection by the instructor and operator.

3.2.2 Device Software Systems

The device software systems shall consist of the following:

Trainer System Software (TSS)

Student Station System Software (SSSS)

3.2.2.1 Trainer System Software (TSS)

The TSS shall operate and control the complete training system.

3.2.2.1.1 Trainer System Software Wiring

The TSS shall interface with all the wiring systems to induce system faults as identified in Appendix A, to allow students to perform the Maintenance Operational Check (MOC).

3.2.2.2 Student Station System Software (SSSS)

The SSSS shall consist of real and non-real-time Computer Software Components (CSC)s required to simulate or stimulate the Student Station (SS) to meet functional fidelity training task requirements as identified in Appendix A.

3.2.2.2.1 Fault Implementation

The SSSS shall control the input of faults through the IOS.

3.2.2.2.1.1 Integrated Training Suite Faults

The SSSS shall support an integrated training suite with the ability to add additional faults.

3.2.2.2.1.2 Power During Fault

The SSSS shall not affect the fault status by SS power.

3.2.2.2.2 System Alarm

The SSSS shall provide an audio and visual cueing alarm to alert the instructor that the system has detected a condition which may cause safety concerns or heat damage to equipment.

3.2.2.2.2.1 Heat Shutdown

The SSSS warnings shall allow the instructor 5 minutes or 5 degrees, whichever comes first, to shut down the trainer before there is a hard shut down due to heat.

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3.2.2.2.3 Intercommunications System (ICS) between Instructor and Students

The ICS SSSS shall replicate the aircraft system with the capability of providing communication between the instructor and students.

3.2.2.2.3.1 Audio System Intercommunications

The device AS shall provide the intercommunication between the instructor and the students inside and outside of the SS.

3.2.2.2.3.2 Audio System (AS) Operations

The SSSS AS shall not impede operation of the SS ICS.

3.2.2.2.3.3 Aural Cueing

The device AS shall provide computer generated simulated aircraft sounds to support training tasks in and around the trainer as identified in Appendix A.

3.2.2.2.3.4 Alerts

The aircraft aural alerts and warnings, heard on the aircraft headsets, shall be heard only through user headsets.

3.2.3 Instructor Operator Station (IOS)

A device IOS shall be provided to enable the instructor to monitor and control the training scenario, insert system faults, check system status, run Daily Operational Readiness Test (DORT), and monitor student progress in real time.

3.2.3.1 IOS Remote Desktop

The device IOS shall have the capability to remote desktop all of the systems on the internal net to support trainer operation and maintenance.

3.2.3.1.1 IOS Remote Desktop Monitoring

The IOS remote desktop shall provide the capability for the instructor to monitor SS displays or the

Integrated Vehicle Health Management System (IVHMS) ground station.

3.2.3.2 IOS Interactive Electronic Technical Manuals (IETM

The IOS shall run the IETM.

3.2.3.2.1 IOS IETM Software Update

The IOS shall include the ability to update the IETM software.

3.2.3.3 Daily Operational Readiness Test (DORT)

The DORT shall provide the trainer maintenance personnel and the instructor a means of determining the status of all of the hardware and software devices located in the SS.

3.2.3.3.1 DORT Report

The DORT report shall be saved to a location on the hard drive that maintenance personnel can access to determine faults or trends.

3.2.3.4 Student Action Log (SAL)

A SAL shall be stored on the IOS.

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3.2.3.4.1 SAL Function

The SAL shall track those student actions that are functionally required to perform tasks identified in

Appendix A.

3.2.3.4.2 SAL Access

The SAL shall be accessible to the instructor at all times.

3.2.3.5 IOS Menu

The IOS shall provide a graphical menu system for Instructor and Operator interaction.

3.2.3.5.1 IOS Menu Format

All menus shall have the same nomenclature and format.

3.2.3.5.2 IOS Input

The IOS menu selections shall be made using input devices that respond in real time.

3.2.3.6 IOS Unique Function

The IOS functions shall be transparent to the student.

3.2.3.6.1 IOS Key Switch

The IOS shall have a power-enabled key switch.

3.2.3.6.2 IOS Shutdown

The IOS shall allow for system shutdowns.

3.2.3.6.3 IOS Connection to Emergency Power Off (EPO) Switches

The IOS shall connect to a network of EPO switches, which when pressed, immediately disables facility power distribution to the trainer.

3.2.3.6.4 IOS Temperature Monitoring

The IOS shall monitor temperature sensors mounted throughout the SS and IOS.

3.2.3.7 Headset Jacks

Two wired headset jacks, using commercial aviation headsets, shall be located on the front of the IOS.

3.2.3.7.1 Headsets

Six commercial aviation headsets shall be provided with the trainer to meet functional fidelity training task requirements as identified in Appendix A.

3.2.3.7.2 Wireless Headset

One wireless commercial aviation headset shall be provided for instructors use from the IOS to meet functional fidelity training task requirements as identified in Appendix A.

3.2.3.8 IOS Cabinetry

The IOS structure shall use commercial cabinetry constructed of ruggedized materials designed to withstand daily usage for a minimum of 36 months.

3.2.3.8.1 IOS Structure Size

The IOS structure shall be 42 inches tall with the width and depth required to support device computers.

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3.2.3.8.2 IOS Cabinet Writing Surface

The IOS cabinet shall include a minimum 12x12 inch writing surface.

3.2.3.8.3 IOS Cabinet Drawers

The IOS cabinet shall include lockable storage drawers for instructional material.

3.2.3.8.4 IOS Monitor

There shall be two IOS monitors mounted to the cabinet.

3.2.3.9 IOS Portability

The IOS shall be movable by one person.

3.2.3.9.1 IOS Casters

The IOS shall be on heavy-duty lockable casters.

3.2.4 Student Station (SS) Physical Attributes

3.2.4.1 SS Dimensions

Dimensions for the SS shall be the same as the actual aircraft.

3.2.4.1.1 SS Length

The SS shall represent the airframe from the forward most tip travel of a 10-foot trainer unique main blade to station 820 (maximum tail rotor blade length with a tail rotor pair parallel to the floor).

3.2.4.1.2 SS Height

The SS height shall be the same as the aircraft with one tail rotor blade, perpendicular to the ground

(unfolded) with landing gear struts properly serviced.

3.2.4.1.3 SS Width

The SS width shall be the same as the aircraft with Crashworthy External Fuel System (CEFS) tanks installed.

3.2.4.1.4 SS Weight

Maximum gross weight of the SS shall not hinder the device mobility.

3.2.4.2 Device Mobility

The SS shall be movable, within the facility, on the aircraft’s landing gear (main and tail).

3.2.4.2.1 SS Towing

The SS shall be towable at speeds of less than 15 mph.

3.2.4.2.2 Interface with Tugs

The SS shall interface to tugs using standard tow-bar P/N AA1730-1251.

3.2.4.2.3 Device Transportability

The SS shall be transportable by air suspension trailer over U.S. highways.

3.2.4.3 SS Center of Gravity

The SS center of gravity shall be within 14 inches of station 343 to allow the device to be lifted by the main rotor head.

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3.2.4.4 Alignment

The SS critical alignment position relationships shall be maintained in accordance with the aircraft specifications in those areas required for training the identified tasks.

3.2.4.5 Jacking Points

The SS jacking points shall be installed in the same location as on the aircraft and support the final trainer weight using Aviation Ground Support Equipment (AGSE).

3.2.4.6 Tail Rotor Rigging

The SS dimensional accuracy of the tail pylon, based on the UH-60M production aircraft, shall allow successful rigging of the tail rotor.

3.2.4.7 Student Station Access

The SS shall have all the access and inspection provision listed in WP0002 00 of TM 1-1520-280-23.

3.2.4.7.1 Physical Device Accessibility

The SS equipment shall be constructed in such a manner so that it does not limit access for troubleshooting.

3.2.4.7.2 Access for Maintenance

The SS shall be constructed to allow maintenance personnel access to service the trainer without degrading any of the training tasks.

3.2.4.8 Student Station Steps

The SS shall have all steps, handholds, and walkways that are shown in WP0002 00 of TM-1-1520-280-

23.

3.2.4.9 Student Station Sound Proofing

Sound proofing shall be installed in the SS to replicate the aircraft.

3.2.4.10 Intercommunications System (ICS) Hook-Ups

The SS ICS shall contain hook-ups for the instructor and students, in the crew stations, and to the aircraft exterior maintenance headset jacks.

3.2.4.11 Operat