PILOTS HEARD STRANGE NOISE COMING FROM FORWARD TRANSMISSION AND LANDED IN LARGE OPEN FIELD. INTERNAL FAILURE OF FORWARD TRANSMISSION, EXCESSIVE METAL PARTICLES WERE FOUND IN THE OIL.\\
16. COMPONENT AND PART FAILURE/MALFUNCTION DATA
Major Component Information
a. Nomenclature
b. Type/Design/Series
c. Part Number
d. NSN
e. MFG Code
f. Part Serial No
ROTOR AND XMSN
Part Information
a. Nomenclature
c. Part Number
d. NSN
e. MFG Code
f. Part Serial No
TRANSMISSION
114D12005
1615004072823
77272
A7739
g. Cause Failure
Functional Group
Material
Maintenance
Design
Manufacture
04 - ROTOR AND TRANSMISSION 05 - MAIN TRANSMISSION
DEFINITE ROLE
NONE
- -
Type Failure
Cause Failure
008 - NOISY
-
999 - UNDETERMINED
-
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
Person # 1
c. Grade
d. Sex
e. Duty
O3
PC - PILOT IN COMMAND
f. SVC
g. UIC
h. Role
i. On Controls
A - ACTIVE ARMY
WC5LAA
U - UNKNOWN
No Yes
j. Lab Test
k. Hrs Slept 24
l. Hrs Worked 24
m. Hrs Flown 24
Yes No
n. RL
o. FAC
p. Injury
q. MTDS Total Flt Hrs
1 2 3
1 2 3
-
0
Person # 2
c. Grade
d. Sex
e. Duty
W3
PI - PILOT
f. SVC
g. UIC
h. Role
i. On Controls
A - ACTIVE ARMY
WC5LAA
U - UNKNOWN
No Yes
j. Lab Test
k. Hrs Slept 24
l. Hrs Worked 24
m. Hrs Flown 24
Yes No
n. RL
o. FAC
p. Injury
q. MTDS Total Flt Hrs
1 2 3
1 2 3
-
0
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
CCAD FINAL EIR 805427 CONCLUSIONS: NO EVIDENCE OF ABNORMAL WEAR OR DAMAGE COULD BE DETECTED THAT WOULD CONTRIBUTE TO THE REPORTED GRINDING NOISE.\\