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actuators, and IFF antenna connectors.
2. Static port  Check. Secure door.
CAUTION 6. Transmission cowling  Check; cowling for
damage and security, and inlet blast shield (if
installed) for condition and obstructions.
Absence of lateral rocking motion about
aft crosstube center mounting bolt could * 7. Transmission  Check; lines, cables, and
result in ground resonance and airframe connections for condition and leaks,
structural damage. transmission oil level. Secure door.
3. Landing gear  Check crosstubes, skid, skid 8. Particle separator  Check condition and
shoes, and weight on gear switch. Check aft unobstructed.
crosstube mount and check lateral rocking
motion about the aft center mounting bolt by * 9. Engine compartment  Check lines, cables,
applying light oscillating pressures at the aft and connections for condition and leaks, and
upper intermediate fuselage. overall condition of engine components.
Secure door.
4. Underside of fuselage  Check; condition,
antennas, and cargo suspension assembly (if 10. Fuselage  Check; condition, drain lines and
installed). vents, AC external power receptacle, lights,
AVR-2A aft sensor unit, if installed, and
5. F u e l sample  D r a i n and check f o r antennas.
contamination.
11. Oil tank  Check; tank condition and filler
8-11. INTERMEDIATE FUSELAGE  RIGHT cap secure.
SIDE  AREA 2.
8-12. TAILBOOM  RIGHT SIDE  AREA 3.
O * 1. Weapons system  Check.
* 1. Tailboom  Check condition as other items
2. UWP  Check. are checked:
8-5
TM 1-1520-248-10
O a. AN/ALQ-144 IR Jammer Transmitter and CAUTION
mount  Check; condition, security,
electrical cables, and covert windows for
cleanliness. Prior to servicing engine oil, refer to
procedures contained in paragraph 2-95
b. Driveshaft cover  Check; condition and to preclude over-servicing and engine
security. damage or possible engine failure.
c. Antennas  Check. * 2. Engine oil level  Check.
d. Horizontal stabilizer  Check condition, 3. Oil tank compartment  Check; oil cooler
expandable bolts, and position light. blower, driveshaft, oil lines, and oil filter
bypass indicator button in. Secure door.
8-13. TAILBOOM  AFT  AREA 4. 4. Fuselage  Check; condition, lights, AVR-2A
aft sensor unit, if installed, antennas, and
* 1. Tailboom  Check; condition as other items heater vent.
are checked:
CAUTION
a. Vertical f i n  Check; condition and
antenna connections.
To prevent damage to e l e c t r i c a l
b. Tail skid  Check; condition and security. components all equipment placed in aft
electrical compartment shall be clear of
electrical components and properly
c. Lights  Check. secured.
* 2. Tail rotor gearbox  Check condition, oil
l e v e l , f i l l e r cap secure, and e l e c t r i c a l 5. Aft electrical compartment  Check; (OH-
connections. 58D) ESC/ (OH-58D(R)) ECU connections
and PA sensing port unobstructed, condition
and connections on electrical avionic
* 3. Tail rotor  Check.
components, circuit breakers in, aft battery
connected (if installed), AVTR tape installed
8-14. TAILBOOM  LEFT SIDE  AREA 5. as desired and secure loose equipment.
Secure door.
* 1. Tailboom  Check condition as other items
are checked: * 6. Engine compartment  Check; lines, cables
and connectors for condition and leaks, fuel
a. Driveshaft cover  Check condition and filter bypass indicator and engine oil filter
security. bypass indicator buttons in, and overall
condition of engine components. Secure door.
b. Antennas  Check.
* 7. Transmission  Check; lines, cables, and
c. Horizontal stabilizer  Check condition, connections for condition and leaks,
expandable bolts, and position light. transmission oil filter bypass indicator button
in. Secure door.
O d. AN/ALQ-144 IR Jammer Transmitter and
mount  Check; condition, security, 8. Particle separator  Check; condition and
electrical cables, and covert windows for unobstructed.
cleanliness.
* 9. Hydraulic reservoir  Check fluid level.
Secure door.
8-15. INTERMEDIATE FUSELAGE  LEFT
SIDE  AREA 6. 10. Transmission cowling  Check; cowling for
damage and security, and inlet blast shield (if
1. Oil cooler fan exhaust  Check. installed) for condition and obstructions.
8-6
 
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OPERATOR’S MANUAL FOR ARMY OH-58D HELICOPTER 2(74)