Runway Edge High Intensity Bidirectional Elevated Light

Fig. 1: BPE-2-150
Runway Edge
High Intensity
Bidirectional Elevated Light
Type BPE
Compliance with Standards
FAA: AC 150/5345-46A
ICAO: Para. 5.3, for use as runway edge light
in Category I, II and III conditions
NATO: STANAG 3316
Fig. 2
Uses
– High intensity edge lighting for runways up to 60 m width in cat. I, II and III.
– Medium intensity runway edge and threshold/runway end lighting. The light
features also an omnidirectional component for circling guidance.
Features
• Of low-profile and small in size: To withstand heaviest jet blast, even when
installed at threshold/runway end.
• Low-maintenance design: Minimum number of parts, every part simple and
functional, spare parts holding limited to a minimum.
• Fast re-lamping: Inner lenses and outer dome remain clamped to upper body.
Only two wingscrews to remove.
• Repeatable and stable photometrics: Uses a PKX30d quartz halogen lamp,
precision-prefocused and accurately positioned in the lower body. Smooth
outer glass dome surface will not retain dirt. Interval between cleanings can be
extended without affecting light output significantly.
• Long lamp life:
–1000 hours at full intensity (6.6A)
–2000 to 4000 hours in practice, since the lighting system often operates at lower intensity settings.
• Energy saver: High-efficiency optics need only 100 W or 150 W lamps where
other lights require 200 W. Reduced heat dissipation entails longer life of
gaskets, glassware and internal wiring.
• Versatile optical system: 2-piece inner glass lens allows for any combination of
colours. 180 degree blanking screen available.
• Easy to install: Design avoids twisting of electric wires. Non-seizing,
polyurethane ball-joint for easy levelling and azimuth alignment. Dedicated
aiming device available.
• Circling guidance: Intensity of omnidirectional light component exceeds the
ICAO requirement, making night VFR operations safer.
• Adaptable to special environmental conditions:
Provision for installation of a location marking rod or flag for heavy snow fall
areas.
A.03.111e
Construction (Fig. 3)
Fig. 3
1.Outer dome, glass, externally smooth.
2.Positioning ring for inner lenses.
3.180° Inner prismatic lenses, glass, through-coloured or clear.
4.O-ring gasket – Heat resistant.
5.Clamping ring – Stainless steel.
6.Upper body, die-cast aluminium alloy.
7.Lamp, quartz halogen, prefocus PKX30d.
8.Lower body, die-cast aluminium alloy.
9.Wire strain reliever
10.Ball joint, polyurethane
11.Frangible stem, die-cast aluminium alloy.
12.2-pole plug to FAA L-823 with heat resistant wires.
1
2
7
3
4
8
9
10
5
6
Finish
11
Phosphating and baked polyester electrostatic powder coating.
Colour: aviation yellow
Stainless steel hardware.
12
Electrical Supply
6.6 A, through a 100, 150 or 200 W isolating transformer.
See catalogue leaflet A.06.110.
Fig. 4
Photometric Performances
Vert.
Degr.
Lamp: 100, 150 or 200 W – 6.6 A prefocus halogen lamp –
PKX30d 1000 hours rated life at full intensity.
White Light – 150 W lamp – Toe-in 3.5 °
500CD
20
BPE-2-150
Colour
Lamp
(W)
Aver.
Intens.
Cd.
Beam spread
Horiz.
Vert.
Runway edge
ICAO 45m
White
150
13326
-2 to 9°
0 to 7°
ICAO 45m
White
200
14505
-2 to 9°
0 to 7°
ICAO 60m
White
150
11413
-2 to 11°
0 to 7°
ICAO 60m
White
200
13586
-2 to 11°
0 to 7°
ICAO 60 m
Yellow
150
6016
-2 to 11°
0 to 7°
FAA L-862
White
150
13700
-2 to 9°
0 to 7°
White
200
14900 -2 to 9°
0 to 7°
Runway edge M.I.
White
100
8463
-2 to 9°
0 to 7°
Threshold M.I.
Green
100
1711
-2 to 7.5°
2 to 7°
Green
100
1777
-1.5 to 1.5°
3.5 to 5.5°
Red
100
1365
-4.5 to 4.5°
0.2 to 1°
Runway edge
Threshold M.I.
FAA L-861
Runway End M.I.
Runway end
ICAO
Red
150
3203
-6 to + 6° 0.25 to 4.75°
ICAO
Red
200
4160
-6 to + 6° 0.25 to 4.75°
Notes:1)45 W – 6.6 A – lamp available for solving specific cases.
Contact factory for performance figures.
2)Outside main beams, intensity in white light never falls below 50 cd from 0 to 15 degrees vertical. This meets ICAO and FAA requirements for circling guidance purposes.
3)Omnidirectional blue dome available on request.
16
1000CD
500CD
1000CD
12
8
5000CD
5000CD
4
0
-20 16
12
8
4
0
4
8
12 +16
Hor.
degr.
Installation
Installation
– On conduit elbow TC2. (Fig. 5) or anchor stake PA 2
(see cat. leaflet A.05.111).
– On mounting plate T300/3 (see cat. leaflet A.05.111).
– On L-867 steel base. (Fig. 6 – see cat. leaflet A.05.120).
The stability has to be ensured through appropriate means (e.g. concrete).
Levelling and aiming in azimuth of the light are easily performed with the
dedicated aiming device supplied on request.
Ordering Code
BPE 2 150 C/Y S
Lamp rating
Fig. 5
Fig. 6
100W
Fig. 7: Outline Dimensions (mm)
= 100
150W
= 150
200W
= 200
Colour
Clear
Yellow
Red Green
Blank
165
=C
= Y =R
= G = N left beam*
right beam*
*see Fig. 8
Accessories and options
– Aiming device.
– Snow flag.
300
280
Special requirements to be specified in full text
Complete, delete or modify as necessary
Packing Data
2” GAS
11 TPI
BPE-2-150, without inner lenses nor lamp; net weight: 2.7 kg
4 each In cardboard box 70 x 40 x 24 cm;
gross weight: 11.5 kg.
N.B. Inner lenses and lamps are packed separately.
Fig. 8: Colour Coding
Yellow on left-hand as side seen from here
C/C
C
Y
R
G
N
Y/C
Y/C
Runway Centre line
C/Y
C/Y
C/C
Yellow on right-hand side as seen from here
Clear
Yellow
Red
Green
blank
Arrow on
outer dome
Suggested Specification
The light shall be suitable for direct installation
on any standard mounting system with 2“ 11 TPI tapped hole. The optical system
shall consist of a double lens. Its outer
component shall have an externally smooth
surface to prevent accumulation of dirt. The
inner lens shall be in two halves, throughcoloured when required. The light shall resist
jet blast from the heaviest present day aircraft
and shall be frangible in case of impact.
Registered Office:
ADB
Airfield Solutions
Leuvensesteenweg 585
B-1930 Zaventem
Belgium
Phone: +32 (2) 7221711
Fax: +32 (2) 7221764
info.adb@adb-air.com
www.adb-air.com
© ADB
all rights reserved
order number DOCA03111EV2
subject to modifications
www.comith.be
The Runway Edge Light shall be high intensity,
elevated, in full compliance with FAA L-862
specification (AC 150/5345-46A) and with
ICAO Annex 14, Vol. I, para. 5.3. for use
in Category I, II and III systems and with
STANAG 3316. The prefocus halogen lamp
shall be 150 W, 6.6 A, rated life not less than
1000 hours at full intensity. The lamp shall be
fitted with lamp retaining clips and fool proof
positioning device. Overall height of the light,
when installed, shall not exceed 300 mm and
its total weight shall be 3 kg or less. The light
shall consist of alu­-minium alloy castings, heat
resistant glass optical parts and plain stainless
hardware. Gaskets and electrical wiring shall
be high temperature resistant. It shall be
possible to level and aim the light without need
for special tools.