Air Mobility Plan, 2008 - The Black Vault
Air Mobility Plan, 2008 - The Black Vault
Air Mobility Plan, 2008 - The Black Vault
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C-5 Roadmap<br />
(b)(5)<br />
Enhanced Surveillance/IFF Mode 5<br />
Enhanced Surveillance (EHS) expands the capability of elementary surveillance by requiring the<br />
following additional information: selected vertical intention, track and turn report, and heading and<br />
speed report. Selected vertical intention includes barometric pressure setting and the altitude to which<br />
the aircraft has been cleared. <strong>The</strong> track and turn report includes roll angle, true track angle, ground<br />
speed, track angle rate, and true airspeed. <strong>The</strong> heading and speed report contains magnetic heading,<br />
indicated airspeed, Mach number, barometric altitude rate, and inertial vertical rate. <strong>The</strong> Flight<br />
Management System (FMS) software in the VIA/AIU requires updating. EHS is designed to improve<br />
airspace safety by reducing ground controller workload, which continues to increase exponential as<br />
airspace utilization increases. <strong>The</strong> international civil aviation organization (ICAO) mandate for these<br />
functions is March 2009.<br />
IFF Mode 5 is a new military identification program that is being implemented DOD-wide. <strong>The</strong> AF<br />
plans to begin the C-5 implementation in FY10 with the entire fleet completed by FY15. Mode 5<br />
provides longer range, improves range accuracy, increases security against exploitation and spoofing,<br />
improves identification of friend and foe, reduces garbling and mutual interference, and reduces IFF<br />
interference with civil air traffic control systems. <strong>The</strong> current Mode IV IFF is not <strong>Air</strong>borne Information<br />
Management System (AIMS)-certified which also poses future certification issues.<br />
Selective Availability Anti-Spoofing Module<br />
SAASM is an anti-tampering capability that significantly enhances the GPS precise positioning<br />
service (PPS) signal security. It consists of an architecture change to the GPS navigation receiver<br />
that essentially eliminates the probability that the GPS navigation signal can be compromised with<br />
current spoofing equipment. SAASM allows for unclassified black key encryption security systems<br />
as opposed to the classified red key encryption security system used today. SAASM uses crypto-nets<br />
which allow mission planners to tailor sets of receivers that could receive PPS signals. SAASM<br />
allows for automatic over-the-air re-keying of black key encryption which significantly reduces<br />
security requirements.<br />
Troop Floor Corrosion Prevention<br />
Stress panels in the troop compartment latrine have significant corrosion. To replace the panels,<br />
maintenance personnel must remove the entire latrine. This causes a 3-week PDM delay. PDM<br />
will install the C-5B-designed latrine on the C-5A. <strong>The</strong> C-5B latrine has a one-piece fiberglass floor<br />
pan, fiberglass walls, and a larger holding tank. Thirteen C-5A aircraft kits have been installed.<br />
PDM currently has kits ready for installation. AMC programmed kit installation through the R&PC<br />
process. <strong>The</strong> requirement is approximately $2.3 million.<br />
TF39 Thrust Reverser End Shoe/Slider Support Beam<br />
Program is applicable to C-5 aircraft that will be flying TF-39 engines. It eliminates the track jumping<br />
failure mode of the thrust reverser. Track jumping is caused by the translating cowl end shoe pulling<br />
away from the pylon beam wear surface under load and engaging the side of the beam when the<br />
reverser is stowed. <strong>The</strong> engagement can result in an asymmetrical stow and damage to the unit. <strong>The</strong><br />
slider support beam modification will extend the overlap engagement point of the translating cowl<br />
(the “end shoe”) from approximately a .5 inch to a 1.5 inch wear surface by affixing a slider beam to<br />
the pylon beam assembly.<br />
56<br />
FOR OFFICIAL USE ONLY (FOUO)<br />
OCT 07