Electrical_Loads.xlsx

XLSX spreadsheet 12 KB Posted Mar 30, 2017

Attached to: T-38A/B and A-10 Automatic Dependent Surveillance-Broadcast (ADS-B) Federal contract opportunity
Solicitation number: FA822017R0001
Issued by: Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

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Electrical Loads

Other files attached to T-38A/B and A-10 Automatic Dependent Surveillance-Broadcast (ADS-B), newest first.
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FA822017R0001_______0001.pdf	PDF	Mar 30, 2017
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AC Loads

AC Loads (VA)
Right generator
Phase A	Rated	CRUISE	Phase B	Rated	CRUISE	Phase C	Rated	CRUISE
LEFT FLAP ACTUATOR	575	0	LEFT FLAP ACTUATOR	816	0	LEFT FLAP ACTUATOR	690	0
RIGHT FLAP ACTUATOR	575	0	RIGHT FLAP ACTUATOR	816	0	RIGHT FLAP ACTUATOR	690	0
RIGHT FUEL PUMP	380	380	RIGHT FUEL PUMP	380	380	RIGHT FUEL PUMP	380	380
INST PWR SEAT	553	553	ENG IGN & R AUTOSYN INST	257	257	RIGHT FUEL QUANTITY	36	36
RADIO TRANSFER RELAY	40	40	FLOOD LIGHT	111	111	NOSE EQUIP COOLING LEFT & CONT	658	658
TRANS-RECT NO. 2	256	256	UTILITY LIGHT	15	15	TRANS-RECT NO. 2	256	256
BUS MONITOR	40	40	AN/ARN-118 TACAN	515	515	BUS MONITOR	40	40
CABIN AIR VALVES	183	183	STU PWR SEAT	553	553	OXY QTY	102	102
CANOPY SEAL	58	58	ELECT TEST	40	0	CABIN COND	67	67
ENG ANTI-ICE	430	430	TRANS-RECT NO. 2	256	256	ATTITUDE GYRO	129	129
RATE GYRO & ATTITUDE GYRO	129	129	BUS MONITOR	40	40	CAUTION & WARNING INDICATION	70	70
TRIM CONTROL	50	50	PITOT HEATER	300	300
			ATTITUDE GYRO	167	167
			ATTITUDE IND FLT DIR COMPUTER	80	80
	RT A Total	2119		RT B Total	2674		RT C Total	1738

Left generator
Phase A			Phase B			Phase C
POSITION LIGHTS	275	275	LANDING AND TAXI LAMP	1002	0	BEACON LIGHT	126	126
CONSOLE LIGHT	38	38	LANDING AND TAXI LIGHT CONT	248	0	INST LIGHT	63	63
LEFT FUEL PUMP	380	380	LEFT FUEL PUMP	380	380	LEFT FUEL PUMP	380	380
TRANS-RECT NO. 1	256	256	TRANS-RECT NO. 1	256	256	TRANS-RECT NO. 1	256	256
BUS MONITOR	40	40	BUS MONITOR	40	40	BUS MONITOR	40	40
ANGLE-OF-ATTACK HEATER	140	140	ANGLE-OF-ATTACK COMPUTER	44	44	AN/APX-64 AIMS	84	84
LEFT FUEL QUANTITY & AUTOSYN INST	132	132	STABILITY AUGMENTER	10	10	AIMS COMPUTER	45	45
ECM POWER	1368	1368	ECM POWER	1368	1368	STABILITY AUGMENTER	42	42
						ECM POWER	1368	1368
	LT A Total	2629		LT B Total	2098		LT C Total	2404

DC Loads

DC Loads (A)
Baseline			After Modification
AIM System	0.93		Position Lights	0.08
Rate Gyro	1.89		ECM Controller	2
AN/AIC-18	0.61
ILS ARN/147	1.25
AN/ARN-118 TACAN RT	1
UHF ARC-164 R/T (front)	4.21
UHF ARC-164 R/T (rear)	4.21
Right Engine Start & Afterburner Control System	0.02
Left Engine Start & Afterburner Control System	0.02
Ignition Inverter (Starting- Two Attempts)	1.32
Left Fire Detector System	0.02
Right Fire Detector System	0.02
Firewall Valves & Front Cockpit Warning Lights System	0.83
Right Generator Control System	0.3
Left Generator Control System	0.3
Right Nozzle Position Indicator, Flap Position Indicator Sys	0.24
L Nozzle Position Indicator System	0.07
Crossfeed Valve System (0.03 minutes)	0
Emergency Flood Lights	0.51
Bus Monitor & Rear Cockpit Warning Lights System	0.82
Right Flap Control (Takeoff & Landing)	0
Left Flap Control (Takeoff & Landing)	0
Speed Brake System (Landing)	0.01
Landing Gear Warning System	0
Landing Gear Control Safety & Steering System	1.89
ARU-42 Standby Attitude Indicators (2)	0.57
AOA Lamps	0.24
50 A battery contactor	0.21
	Load	Capacity		Load	Capacity
Aircraft Total	21.49	50		23.57	50

File details come from the government source that posted it. Updated Nov 14, 2017.