Attachment_D_SRD_Evaluation_Table_Final_Draft.pdf

SRD Evaluation Table

Req # Requirement Description How Requirement is Met Aircraft Requirements

Program Requirements

3.1.1

Solution shall mitigate avionics obsolescence for 20+ years as defined in a DMSMS plan

(MANDATORY).

System Requirements

3.2.1

The avionics suite shall allow for non-proprietary interfaces to the newly installed system

3.2.7

The integrated avionics system suite shall fit within the pre-modified aircraft allowable space (MANDATORY). This requirement does not apply to antennas.

CSO Aircraft Integration Requirements

3.3.1

The aircraft avionics shall maintain data bus connection with the CSO platform on the 21 CSO modified aircraft (MANDATORY).

Angle of Attack (AOA) Indication

3.5.2.1

The modified T-1A aircraft shall provide an AOA instrument display that compares the relative wind to the chord line of the wing

Standby Instruments

3.5.3.1

Attitude, airspeed, magnetic compass, and altimeter instruments shall be provided in locations that can be read and controlled from both the pilot and copilot positions

Other

3.5.4.1

RAT, engine vibration, fuel temperature, and hydraulic pressure indication shall be provided and visible at all times from both the pilot and copilot positions

Displays

3.6.3

The displays shall incorporate redundancy such that the mission can be completed in the event of any single point failure in the EFIS

3.6.6

The modified T-1A aircraft shall provide the capability for crew members in the pilot and copilot seats the ability to independently control the formats of their respective displays (MANDATORY).

Navigation Departure, En-Route, and Terminal Navigation

3.7.1.1

The aircraft shall comply with the following civil aviation standards for departure, en-route, and terminal area navigation: RNAV-2 Route, RNP-2 en-route, RNAV-1 Terminal Area, RNP-1 Terminal area and vertical navigation (en-route and terminal) (MANDATORY).

FMS

3.7.4.2

Capability to display both primary and secondary flight plans on multi-functional display(s) shall be provided (MANDATORY).

3.7.4.4

The FMS shall be capable of NAS Q and T (RNP 2) routes, RNAV SIDs and STARs (RNP 1), and RNAV approach operations (MANDATORY).

Navigation Displays

3.7.5.3

A multicolor MFD(s) shall be mounted at a central location and display primary weather radar, moving map, TCAS II (MANDATORY).

This display shall be used as a backup to the pilot's or copilot's displays (MANDATORY).

EFIS

3.7.6.3

The EFIS shall incorporate redundancy such that the mission can be completed in the event of any single point failure such that if one signal generator fails, the remaining signal generator shall supply information to both the pilot and copilot displays (MANDATORY).

TCAS II / Transponder

3.7.7.1

The modified T-1A aircraft shall provide a TCAS II with a control unit located in the flight deck at a position to be controllable from the pilot and co-pilot positions

3.7.7.4 Current capability to “ident” using the existing button on the yoke shall be maintained (MANDATORY).

Weather Radar

3.7.8.4 The weather radar shall provide the ability for auto tilt, sector scan, and gain adjustments (MANDATORY).

3.7.8.5 provide weather radar information to the EHSI and MFD with selectable navigation graphics overlays

Radio/Radar Altimeter

3.7.9.1

The modified T-1A aircraft shall provide a dedicated radio/radar altimeter for tracking the aircraft distance from terrain within an altitude range of 20 to 2,000 ft

3.7.9.2

The radio/radar altimeter displays shall provide for pilot and copilot adjustment to any altitude within the range of the indicator

Ground Collision Avoidance

3.7.10.1 The modified T-1A aircraft shall meet the requirements for TAWS Class A (MANDATORY).

3.7.10.3

The modified T-1A aircraft shall provide for manual, temporary inhibiting of warnings during landing with flaps less than 30 degrees and terrain avoidance while flying at 500 feet AGL and up to 330 knots Calibrated Air Speed (KCAS)

Approach and Landing

3.8.3

VOR course, bearing, and distance to station (if paired with DME) shall be displayed on EHSI when selected

3.8.5 provide dual ILS Category I systems

3.8.10 provide an ADF system with digital filtering, or the equivalent, that provides a homing presentation

3.8.11 ADF bearing shall be displayed on

EHSI when selected (MANDATORY).

3.8.12

The modified T-1A shall provide a DME subsystem that incorporates a DME frequency hold function

3.8.13 provide a marker beacon system which detects and displays the inner and outer air field markers

3.8.14 provide for the digital display of NGA/DOD enroute and terminal area approach and departure charts FLIP at both the pilot and copilot positions (MANDATORY).

3.8.15

Alphanumeric identifier or channel information of the selected ground based NAVAID shall be displayed on the EHSI (MANDATORY).

VHF & UHF Transmitters and Receivers

3.9.1

The modified T-1A aircraft shall have an ICS with a minimum of one VHF radio, one UHF radio, “hot-mic” capability in the normal operating mode, and the ability to monitor all navigational radio aids (MANDATORY). Hot-mic is defined as the Push-To-Talk is not used during inter-plane communication.

3.9.5 provide two navigation and communication radio interface sources, controllable and accessible from the pilot and copilot seat

3.9.15

All crew positions and the avionics rack shall have intercom panels with individual volume and on and off controls (MANDATORY).

3.9.16

The Public Announcement system shall provide audible information in all areas of the cabin during operations at maximum cabin noise levels, with the engines operating on the ground and in flight

3.9.21

The control for silencing all external radio signals shall be mounted on both yokes and the jump seat intercom control panel

3.9.27

In addition to the capabilities listed in 3.9.1 – 3.9.26, CSO modified aircraft shall have the following capability as part of the ICS:

Private channel for communications between pilot, co-pilot, jump and observer only (MANDATORY).

Private channel for communications between instructor, CSO and observer only (MANDATORY).

Private channel for communications between pilot, jump, instructor and observer only (MANDATORY).

Threat 1 and Threat 2 system audio shall be selectable at all crew stations (MANDATORY).

Call button (MANDATORY).

Selectable Hot mic/Hot listen capability (MANDATORY).

AutoPilot

3.10.1

The modified T-1A aircraft shall provide a three-axis autopilot system with automatic disengage feature (MANDATORY).

3.10.2 provide a preflight and maintenance BIT capability for the autopilot

3.10.3

The autopilot shall provide for coupled approaches and coupled lateral and vertical enroute navigation (MANDATORY).

3.10.4 Capability to disengage autopilot with button on yoke shall be retained (MANDATORY).

3.10.5 The modified T-1A aircraft autopilot shall compensate for Dutch roll tendencies (MANDATORY).

Flight Directors

3.11.1 The modified T-1A aircraft shall provide dual independent flight directors (MANDATORY).

3.11.2

Flight directors shall function with the autopilot and the instrument approach subsystems to provide Category I ILS capability with separate remote course and heading selection controls and a single cue command steering presentation

Crash Survivable Flight Data Recorder (CSFDR)

3.13.1

Current capabilities of the FDR and number of recorded parameters shall be maintained as a minimum

3.13.3

All functionality in the current Aircraft Structural Integrity software program shall be maintained

Cockpit Lighting

3.15.1 The flight deck panel lighting shall be balanced over the full range of adjustment (MANDATORY).

Maintainability

3.16.1

For LRUs installed as part of the T- 1A AMP, removal of a failed LRU shall not require removal of any other LRU (MANDATORY).

Environmental, Safety, and Occupational Health

3.17.9

No single-point failure or malfunction of a component within the modified T-1A aircraft shall cause a sequence of events leading to a catastrophic effect on the modified T-1A aircraft or personnel

Simulator Requirements OFT Requirements

4.1.1

The modified OFT shall replicate the modified aircraft in functionality, appearance, and lay-out

4.1.4

A modified OFT shall still be able to operate with legacy OFT simulators in networked exercises

4.1.5 The modified OFT as a minimum shall retain current capabilities of the IOS (MANDATORY).

4.1.8 IOS space requirements shall be

retained (MANDATORY).

4.1.9 The modified OFT shall maintain all record, replay, and fly out capability

4.1.10

Current ECL System for pitch, roll, yaw flight and sticker shaker controls shall be retained

4.1.13

The modified OFT software shall be compatible with existing software within the simulator system

4.1.14

The modified OFT shall retain the FAA AC 120-45A Level C (6) simulation fidelity capabilities

4.1.15

The modified OFT shall be operated in accordance with the tolerance specified in FAA AC 120-45A

4.1.16

The new equipment installed shall include the functionality of malfunction insertion by the instructor (MANDATORY).

4.1.17

A maximum of 5 individual malfunctions shall be active at any one time during a given mission profile (MANDATORY).

4.1.18 ACCS shall work in single and network configurations

4.1.20

The modified OFT shall include a non-proprietary procedure for updating the DAFIF or equivalent

4.1.21

The modified OFT shall maintain aircraft system simulation capability of the cockpit lighting system

4.1.24

The modified OFT shall not degrade safety in the performance of any tasks associated with the operations maintenance, instruction, enhancements/modifications, and support (MANDATORY).

ICS

4.1.26.2 ICS shall be compatible with the

existing ACCS (MANDATORY).

4.1.26.3

All normal and abnormal sounds which provide audio cues to the student in the cockpit during all phases of flight and ground operations shall not be degraded

4.1.26.4

Engine aural simulation shall be from start through all operational performance conditions through engine shut-down (MANDATORY).

Software Development

4.1.27.1

All new or modified software shall follow accepted commercial developmental guidelines such as

IEEE/EIA 12207 (MANDATORY).

Power

4.1.28.1 Modification to the OFT shall not require changes to the facility power

4.1.28.3

Equipment shall be compatible with the emergency power-off system and not sustain any damage during unexpected power down

Environmental Conditions

4.1.29.1 A modified OFT shall not increase the operating temperature within the simulator (MANDATORY).

4.1.29.2

All components added to the OFT shall operate in temperatures from 59 to 86 degrees F with a relative humidity between 30 to 80% non-condensing (MANDATORY).

4.1.29.3

All components added to the OFT shall be able to be stored in temperatures from 14 to 122 degrees F with a relative humidity between 10 to 80% non-condensing

PTT Requirements

4.2.1 The PTT shall provide hands-on avionics training prior to aircraft or simulator events (MANDATORY).

4.2.2

The PTT shall be a representation of the cockpit to include pilot displays, multi-function display(s), auto-pilot controls, audio controls, navigation, and communication controls

4.2.2.1 The PTT shall have same tactile feel

as the aircraft (MANDATORY).

4.2.3

PTT shall provide the capability to allow student training on: radio management (navigation and communication tuning), audio panel/intercom control, transponder control, display control, navigation and data entry, flight planning, auto-pilot control, heading, and course and altitude selection (MANDATORY).

4.2.4

Displays in the PTT shall provide a dynamic response as the simulation passes over a waypoint or station

4.2.5 The PTT shall have the ability reposition to different training locations (MANDATORY).

4.2.6

The PTT shall allow the operator to select AIR or GROUND as an initial condition to perform a mission

4.2.7 The PTT shall not occupy more than 62 square feet of floor space

4.2.9 Approach plates on the PTT and OFT

shall be identical (MANDATORY).

4.2.10 The PTT shall provide a maintenance mode for troubleshooting

SRD Evaluation Table