EC-135/Limitations - Revision history

Kelly: /* Airspeed Limits */

2021-10-23T19:03:38Z

‎Airspeed Limits

Kelly: /* Fuel Limits */

2021-10-23T19:03:07Z

‎Fuel Limits

Kelly: /* Fuel Limits */

2021-10-23T19:02:47Z

‎Fuel Limits

Kelly: /* Center of Gravity Limits */

2021-10-23T19:01:45Z

‎Center of Gravity Limits

Kelly: /* Center of Gravity Limits */

2021-10-23T19:01:17Z

‎Center of Gravity Limits

Kelly: /* Center of Gravity Limits */

2021-10-23T19:01:07Z

‎Center of Gravity Limits

Kelly: /* Mass and Load Limits */

2021-10-23T19:00:26Z

‎Mass and Load Limits

Kelly: /* General */

2021-10-23T18:59:42Z

‎General

Kelly: Created page with "SECTION 2. LIMITATIONS WARNING IF ANY LIMITATION HAS BEEN EXCEEDED, MAINTENANCE ACTION MAY BE REQUIRED AND NECESSARY B..."

2021-10-23T18:58:19Z

Created page with "SECTION 2. LIMITATIONS WARNING IF ANY LIMITATION HAS BEEN EXCEEDED, MAINTENANCE ACTION MAY BE REQUIRED AND NECESSARY B..."

New page

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.


===General===
This helicopter shall be operated in compliance with this section.
Kind of Operation
This helicopter is certified for day and night operations in VMC (Visual Meterological Conditions) and IMC (Instrument Meterological Conditions).
Basis of Certification
This helicopter is certified in the Normal category accoding to SLAR-9923, first issued Feb. 29, 1993 with Category A engine isolation requirements.
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.
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
Center of Gravity Limits
The zero station plane is located at the nose of the aircraft.
Max Forward CG: 153 in in
Max Aft CG: 172 in
Max Lateral CG: +/- 8 in from center line
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
Airspeed Limits
Never Exceed Speed (Vne): 160 knots
Power-Off Never Exceed Speed (Vne): 90 knots

@@ Line 39: / Line 39: @@
 {|
-|Main Tank	||154 gallons	||1047 lb	||474.3 kg
+|Main Tank:	||154 gallons	||1047 lb	||474.3 kg
 |-
-|Left tank	||16 gallons	||109 lb	||49.2 kg
+|Left tank:	||16 gallons	||109 lb	||49.2 kg
 |-
-|Right tank	||14 gallons	||95 lb	||43.1 kg
+|Right tank:	||14 gallons	||95 lb	||43.1 kg
 |-
-|Total	||184 gallons	||1251 lb	||566.7 kg
+|Total:	||184 gallons	||1251 lb	||566.7 kg
 |}

@@ Line 29: / Line 29: @@
 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
 |}

@@ Line 34: / Line 34: @@
 |-
 |Max Lateral CG:	|+/- 8 in from center line
-|]
+|}
 ===Fuel Limits===

@@ Line 18: / Line 18: @@
 ===Mass and Load Limits===
-Max Gross Weight:	6,415 lb
+{|
-Min Gross Weight for Flight:	3,300 lb
+|Max Gross Weight:	||6,415 lb
-Max Floor Loading Limit:	122 lb/sq-ft
+|-
 ===Center of Gravity Limits===

@@ Line 49: / Line 49: @@
 ===Airspeed Limits===
 Never Exceed Speed (Vne):	160 knots
-Power-Off Never Exceed Speed (Vne):	90 knots
+{|

@@ Line 7: / Line 7: @@
 ===General===
 This helicopter shall be operated in compliance with this section.
 Kind of Operation
-This helicopter is certified for day and night operations in VMC (Visual Meterological Conditions) and IMC (Instrument Meterological Conditions).
+===Kind of Operation===
-Basis of Certification
+This helicopter is certified for day and night operations in VMC (Visual Meteorological Conditions) and IMC (Instrument Meteorological Conditions).
-This helicopter is certified in the Normal category accoding to SLAR-9923, first issued Feb. 29, 1993 with Category A engine isolation requirements.
-Minimum Flight Crew/Maximum Number of Occupants
+===Basis of Certification===
 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.
 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
 Center of Gravity Limits
 The zero station plane is located at the nose of the aircraft.
 Max Forward CG:	153 in in
 Max Aft CG:	172 in
 Max Lateral CG:	+/- 8 in from center line
 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
 Airspeed Limits
 Never Exceed Speed (Vne):	160 knots
 Power-Off Never Exceed Speed (Vne):	90 knots