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FWD
BAC-291 LEFT SIDE SHOWN (BAC-292 RIGHT SIDE OPPOSITE) (INBOARD SURFACE SHOWN)
Power Terminals - No. 1 Window
Figure 501
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(a)
6L13 or 6L15, PITOT HEAT CAPT MAIN
(b)
6L14 or 6L16, PITOT HEAT L AUX
(c)
6L17, L AOA HEAT
(d)
6L21, PITOT HEAT R AUX
(e)
6L22, PITOT HEAT F/O MAIN
(f)
6L23, R AOA HEAT
(g)
6L24, TAT PROBE HEAT
~............................................................... | Table 501 | ................................................................. | | | NOMINAL OPERATING | | WINDOW | RESISTANCE (OHMS) | VOLTAGE (VOLTS) | ................................................................. | No. 1 | 11.15 max/9.12 min | 186 | ................................................................. |*[1] No. 2 | 28.2 max/23.0 min | 109 | ................................................................. |*[2] No. 2 | 25.9 max/19.1 min | 109 | ................................................................. |*[1] No. 3 | 38.5 max/31.5 min | 109 | ................................................................. |*[2] No. 3 | 29.6 max/21.8 min | 109 | 2..............…........................….......................1 *[1] WINDOWS WITH WIRE RESISTANCE HEATERS *[2] WINDOWS WITH ELECTRICALLY CONDUCTIVE COATING
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FLIGHT COMPARTMENT WINDOW ANTI-ICING - APPROVED REPAIRS
_______________________________________________________
1. General_______
A. This procedure contains one task. The task is the connection of the spare window temperature sensor.
B. The captain's and first officer's No.1, No.2, and No.3 windows are electrically heated. Each window has a control and a spare temperature sensor.
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