ABBREVIATED AVIATION ACCIDENT REPORT (AAAR)
Source	AAAR
1. Case Number	1a. Date of Accident	1b. Time	1c. Aircraft Serial Number	2a. Classification		2b. Category
20000424003	Apr 24 2000	0930	8900168	D		FLIGHT
3. Type of Aircraft	4. Period Of Day	5. No Acft Involved	6. Nearest Installation
CH47D	DAY	1	02955 - FT WAINWRIGHT (AIM), AK
7. Accident Location		a. On Post	b. On Airfield	d. ALASKA
8. Organization Involved in Accident
Unit	UIC7	UIC6	UIC5	UIC4	UIC3	UIC2	MACOM	Station
WHT7B0					WHT7AA	W0EBAA	W32FAA	02955
B CO					4/123AB	ARTSPBD	USARPAC	FT WAINWRIGHT (AIM), AK
9. Organization Accountable for Accident
WHT7B0					WHT7AA	W0EBAA	W32FAA	02955
B CO					4/123AB	ARTSPBD	USARPAC	FT WAINWRIGHT (AIM), AK
10. Estimated Accident Cost
a. Total Loss	b. Aircraft Damage		c. Man Hrs	d. Man Hrs Cost	e. Other Mil Damage		f. Civilian Damage
No	$3112		5	$80	$0		$0
g. Injury		h. Total This Aircraft		i. Total Accident
$0		$3192		$3192
11. General Data
a. Mission				S/M	b. Flight Plan		c. Data Recorder
S - SERVICE				SINGLE	VFR
d. Night Vision		e. Fire		f. Fluid Spillage		g. Field Training
		NONE
12. Flight Data
a. Emergency		Duration		Phase of Operation
		2.5		B - STATIONARY (ENGINE RUNNING)
		AGL	KIAS		Weight		Overgross
					32000
b. Termination		Duration		Phase of Operation
				B - STATIONARY (ENGINE RUNNING)
		AGL	KIAS		Weight		Overgross
13. Type Event
84 - Power Train			91 - Electrical System			-
14. Accident Cause Factors			Human Error		Material Failure		Environmental
			NO		DEFINITE		NO
15. Summary
After hot refueling, the #2 normal engine beep failed to respond to normal inputs. The #2 emergency beep auto/manual switch was placed in the manual position to control the engine manually. The #2 n2 control box was replaced and the cannon plug was cleaned. No further incidents occurred.
16. COMPONENT AND PART FAILURE/MALFUNCTION DATA
Part Information
a. Nomenclature			c. Part Number		d. NSN	e. MFG Code	f. Part Serial No
CONTROL BOX			SYLZ75614		6110011834852	05624
g. Cause Failure				Functional Group
Material	Maintenance	Design	Manufacture	03 - ENGINE/POWER PLANT 19 - CONTROLS
DEFINITELY				80 - THROTTLE 90 - SYNCHRONIZED
Type Failure				Cause Failure
356 - LOW ENGINE POWER		-		572 - RPM TOO LOW			-
17. ENVIRONMENTAL
a. General		(1) IMC		(2) VMC		(3) Unknown
b. Environmental Conditions
1. Weather Conditions				2. Other Conditions
(a) Hail				(a) Animals
(b) Sleet				(b) Fowl
(c) Fog				(c) Surface
(d) Drizzle				(d) Noise
(e) Rain				(e) Chemicals
(f) Snow				(f) Radiation
(g) Lightning				(g) Glare
(h) Thunderstorm				(h) FOD
(i) Gusty Winds				(i) Temperature
(j) Freezing Rain				(j) Vibration
(k) Other				(k) Dust
c. Aircraft Icing		No Yes		d. Turbulence			No Yes
19. MOON ILLUMINATION DATA
a. Above Horizon		b. Visible		c. Degrees Above Horizon		d. Percent Illumination		e. Clock Position
No Yes		No Yes
20. WIRE STRIKE DATA
a. Wire Strike		b. WSPS Installed			c. WSPS Engaged
No Yes		No Yes			No Yes
d. WSPS Cut Wire		e. WSPS Functioned			f. Wires Struck
No Yes		No Yes			Number wires	0	Dia.(inches)
21. PERSONNEL DATA
22. IMPACT/PROTECTIVE/ESCAPE/SURVIVAL/RESCUE DATA
a. Aircraft Space Compromised			b. Escape/Survival Difficulties			c. Protective/Restraint Equip Functioned
No Yes			No Yes			No Yes
24. FINDINGS AND RECOMMENDATIONS
Findings
Not Reported
Recommendations
Not Reported