UFC 3-535-01
17 November 2005
Table 13-2. List of Standards, Specifications, and Drawings
Doc. No.
Title
FAA-E-910
Structural Steel.
FAA-E-982
PAR 56 Lamp Holder.
FAA-E-1315
FAA-E-2159
Runway End Identifier Lighting System (REIL).
FAA-E-2325
Medium Intensity Approach Light System with Alignment Indicator Lights.
FAA-E-2491
Approach Light, Semi-flush, Steady Burning.
Sequenced Flashing Lighting System Elevated and Semi-flush with
FAA-E-2628
Dimming and Monitoring.
FAA-E-2651
Omni Directional Approach Lighting System (ODALS).
FAA-E-2689
Dual Mode High Intensity Approach Lighting System (ALSF-2/SSALR).
FAA-E-2702
Low Impact Resistant Structures.
FAA-E-2756
Four Box PAPI.
FAA Drawing C-6046
Frangible Coupling Type I and Type IA, Details.
ALSF-2 Approach Lighting System 6'-0" to 128'-0" Low Impact Resistant
FAA Drawing D-6076
(LIR) Structures.
FAA Drawing D-6155
ALSF-2, 6' to 128' and MALS, 40' to 128' LIR Structures.
MIL-L-7158
Light, Beacon, Rotating, 24-inch
13-16
CONSIDERATIONS FOR ADDITIONAL EQUIPMENT REQUIREMENTS
This paragraph provides characteristics and features for some equipment or
subsystems beyond the minimum required by FAA standards. These have been
identified as improving system performance, or in the case of computerized control
system, provide criteria for equipment not yet covered by FAA standards but for which
components are commercially available and often used for newer installations.
13-16.1
Constant Current Regulator
The following features and characteristics for L-828 and L-829 constant current
regulators typically result in a better and more safe installation.
13-16.1.1
Display of line voltage, line current, and load voltage.
Built-in meter monitoring output current, true RMS, with at least 3 percent
13-16.1.2
accuracy.
13-16.1.3
Remote back indication for the individual brightness steps (providing
positive signal to tower that CCR is on the selected step).
13-16.1.4
The capacity of the regulator must be rated in nominal KVA (kilovolt-
amperes) output (instead of KW). KVA rating is recommended in order to better
correspond with field circuit loads and current steps. When the load is almost
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