Difference between revisions of "EC-135/Limitations"

From
Jump to: navigation, search
(Center of Gravity Limits)
(Airspeed Limits)
 
(3 intermediate revisions by the same user not shown)
Line 29: Line 29:
 
The zero station plane is located at the nose of the aircraft.
 
The zero station plane is located at the nose of the aircraft.
 
{|
 
{|
|Max Forward CG: |153 in
+
|Max Forward CG: ||153 in
 
|-
 
|-
|Max Aft CG: |172 in
+
|Max Aft CG: ||172 in
 
|-
 
|-
|Max Lateral CG: |+/- 8 in from center line
+
|Max Lateral CG: ||+/- 8 in from center line
 
|}
 
|}
  
 
===Fuel Limits===
 
===Fuel Limits===
Main Tank 154 gallons 1047 lb 474.3 kg
+
 
Left tank 16 gallons 109 lb 49.2 kg
+
{|
Right tank 14 gallons 95 lb 43.1 kg
+
|Main Tank: ||154 gallons ||1047 lb ||474.3 kg
Total 184 gallons 1251 lb 566.7 kg
+
|-
 +
|Left tank: ||16 gallons ||109 lb ||49.2 kg
 +
|-
 +
|Right tank: ||14 gallons ||95 lb ||43.1 kg
 +
|-
 +
|Total: ||184 gallons ||1251 lb ||566.7 kg
 +
|}
  
 
===Airspeed Limits===
 
===Airspeed Limits===
Never Exceed Speed (Vne): 160 knots
+
 
Power-Off Never Exceed Speed (Vne): 90 knots
+
{|
 +
|Never Exceed Speed (Vne): ||160 knots
 +
|-
 +
|Power-Off Never Exceed Speed (Vne): ||90 knots
 +
|}

Latest revision as of 19:03, 23 October 2021

SECTION 2. LIMITATIONS

WARNING IF ANY LIMITATION HAS BEEN EXCEEDED, MAINTENANCE ACTION MAY BE REQUIRED AND NECESSARY BEFORE NEXT FLIGHT. ENTER DURATION AND AMOUNT OF EXCESS IN LOGBOOK.

1 General

This helicopter shall be operated in compliance with this section.

2 Kind of Operation

This helicopter is certified for day and night operations in VMC (Visual Meteorological Conditions) and IMC (Instrument Meteorological Conditions).

3 Basis of Certification

This helicopter is certified in the Normal category according to SLAR-9923, first issued Feb. 29, 1993 with Category A engine isolation requirements.

4 Minimum Flight Crew/Maximum Number of Occupants

The minimum flight crew for this helicopter is one pilot operating from the right crew seat. The maximum number of occupants including flight crew is 8.

5 Mass and Load Limits

Max Gross Weight: 6,415 lb
Min Gross Weight for Flight: 3,300 lb
Max Floor Loading Limit: 122 lb/sq-ft

6 Center of Gravity Limits

The zero station plane is located at the nose of the aircraft.

Max Forward CG: 153 in
Max Aft CG: 172 in
Max Lateral CG: +/- 8 in from center line

7 Fuel Limits

Main Tank: 154 gallons 1047 lb 474.3 kg
Left tank: 16 gallons 109 lb 49.2 kg
Right tank: 14 gallons 95 lb 43.1 kg
Total: 184 gallons 1251 lb 566.7 kg

8 Airspeed Limits

Never Exceed Speed (Vne): 160 knots
Power-Off Never Exceed Speed (Vne): 90 knots