Aircraft Fleet

Specification may change without prior notice. Aircraft and component maintenance life remaining and technical data subject to verification prior to purchase or lease.

Type Certificate Holder: AIRBUS HELICOPTERS
Aircraft Model: EC225LP
Engine Model: 2 x Turbomeca Makila 2A1
Flight Crew: 1 or 2
Maximum Passengers: 25
Maximum Airspeed: Vne Power On: 175 kt below 5,000 ft DA, above 5,000 ft: -3 kt/1,000 ft
Maximum Take-Off Weight: 11,000 kg
Operating Limitations: VFR day and night, IFR, non-icing conditions. Flight in full icing conditions is permitted only when other equipment items as listed in relevant approved RFMS are installed. Flight in limited icing conditions is permitted only when equipment items listed in relevant approved RFMS are installed.

Type Certificate Holder: AIRBUS HELICOPTERS
Aircraft Model: AS332L1
Engine Model: 2 x Turbomeca Makila 1A1
Flight Crew: 1 or 2
Maximum Passengers: 24
Maximum Airspeed: Vne Power On 310 km/h (167kt) at ISA sea Level for M ≤ 8,350 kg, 278 km/h (150kt) at ISA sea Level for M > 8,350kg
Maximum Take-Off Weight: 8,600 kg
Operating Limitations: VFR day and night. IFR day and night. Non-icing conditions. Flight in limited icing conditions is permitted on AS 332L and L1 models only when equipment items listed in relevant approved flight manual supplements are installed

Type Certificate Holder: AIRBUS HELICOPTERS
Aircraft Model: AS350B3
Engine Model: 1 x Turbomeca Arriel 2B or Arriel 2B1 or Arriel 2D
Flight Crew: 1
Maximum Passengers: 5 (6 when fitted with the forward two-place optional seat)
Maximum Airspeed: Refer to Flight Manual
Maximum Take-Off Weight: 2,250 kg or 2,370 kg if incorporating mod OP-3369.
Operating Limitations: Day VFR flight. Night VFR flight, when the additional equipment required by operational regulations is installed and serviceable.

Type Certificate Holder: Airbus Helicopters Deutschland GmbH
Aircraft Model: MBB-BK117B-2
Engine Model: 2 x Honeywell International Inc. LTS101-750B-1
Flight Crew: 1 or 2
Maximum Passengers: 7 (10 if the kit described in RFMS 10-8 is installed and operated)
Maximum Airspeed: VNE 150 KIAS at MSL. Refer to approved RFM for reduction in VNE with altitude and other speed limitations
Maximum Take-Off Weight: 3,350 kg
Operating Limitations: VFR day and night. Non-icing conditions. For IFR, Category A operation refer to approved RFM Additional limitations for TO and LDG refer to approved RFM

Type Certificate Holder: Airbus Helicopters Deutschland GmbH
Aircraft Model: EC135P2+
Engine Model: 2 x Pratt & Whitney Canada PW 206B2
Flight Crew: 1 or 2
Maximum Passengers: 7
Maximum Airspeed: VNE 155 KIAS at MSL
Maximum Take-Off Weight: 2,910 kg (2,950 kg in accordance with RFMS 9.1-5, RFMS 9.1-6 and RFMS 9.1-7 from s/n 1055 and subsequent or after SB EC135-62-028)
Operating Limitations: VFR day and night. Non-icing conditions. For IFR, Category A operation see additional equipment requirements and limitations in the relevant approved RFMS

Type Certificate Holder: Airbus Helicopters Deutschland GmbH
Aircraft Model: EC135T2+
Engine Model: 2 x Turbomeca Arrius 2B2
Flight Crew: 1 or 2
Maximum Passengers: 7
Maximum Airspeed: VNE 155 KIAS at MSL
Maximum Take-Off Weight: 2,910 kg (2,950 kg in accordance with RFMS 9.1-5, RFMS 9.1-6 and RFMS 9.1-7 from s/n 1055 and subsequent or after SB EC135-62-028)
Operating Limitations: VFR day and night. Non-icing conditions. For IFR, Category A operation see additional equipment requirements and limitations in the relevant approved RFMS

Type Certificate Holder: AIRBUS HELICOPTERS
Aircraft Model: EC130T2
Engine Model: 1 x Turbomeca Arriel 2D
Flight Crew: 1
Maximum Passengers: 6 (7 if modification OP-3673 or OP-3888 is installed)
Maximum Airspeed: VNE power on 155 kt at sea level less 3 kt/1,000 ft. 136 kt at sea level less 3 kt/2,000 ft below Hp 12,750ft for reduced VNE area (Refer to Flight Manual)
Maximum Take-Off Weight: 2,500 kg
Operating Limitations: Day VFR flight. Night VFR flight, when the additional equipment required by operational regulations is installed and serviceable.

Type certificate Holder: Leonardo S.p.A. Helicopters
Aircraft Model: AW119MKⅡ
Engine Model: 1 x Pratt & Whitney Canada PT6B-37A
Flight Crew: 1 or 2
Maximum Passengers: 7
Maximum Airspeed: VNE 152 KIAS. Refer to approved RFM for reduction in VNE with altitude and other speed limitations
Maximum Take-Off Weight: 2,850 kg
Operating Limitations: VFR day and night. Non-icing conditions. Additional limitations for TO and LDG refer to approved RFM Section 1

Type certificate Holder: Leonardo S.p.A. Helicopters
Aircraft Model: A109E
Engine Model: 2 x Pratt & Whitney Canada PW206C
Flight Crew: 1 or 2
Maximum Passengers: 7
Maximum Airspeed: VNE 168 KIAS Power on. Refer to approved RFM for reduction in VNE with altitude and other speed limitations
Maximum Take-Off Weight: 2,850 kg or 3,000 kg
Operating Limitations: VFR/IFR day and night. Non-icing conditions. Equivalent Cat A operations

Type certificate Holder: Leonardo S.p.A. Helicopters
Aircraft Model: AW169
Engine Model: 2 x Pratt & Whitney Canada PW210A
Flight Crew: 1 or 2
Maximum Passengers: 8 (10 if the kit 10 Seats Internal Arrangement P/N 6F2520F00111 is installed)
Maximum Airspeed: VNE Power On AEO 165 kts. For reduction of the VNE with Density Altitude (HP/OAT), see RFM
Maximum Take-Off Weight: 4,600 kg or 4,800 kg if P/N 6F0000F00211 is installed
Operating Limitations: VFR/IFR day and night operations in non-icing conditions

Type Certificate Holder: Bell Helicopter Textron Canada Limited
Aircraft Model: 206L-4
Engine Model: 1 x Rolls-Royce Corporation (Allison) 250-C30P
Flight Crew: 1
Maximum Passengers: 6
Maximum Airspeed: Basic VNE is 140 KIAS sea level to 3,000 feet density altitude
Maximum Take-Off Weight: 2,018.5 kg (internal loading)
Operating Limitations: Refer to approved RFM

Type Certificate Holder: Bell Helicopter Textron Canada Limited
Aircraft Model: 407
Engine Model: 1 x Rolls-Royce Corporation (Allison) 250-C47B or 250-C47B/8
Flight Crew: 1
Maximum Passengers: 6
Maximum Airspeed: Basic VNE is 140 KIAS sea level to 3,000 feet density altitude
Maximum Take-Off Weight: 2,268 kg (internal loading). 2,381 kg (internal loading) when equipped with kit 407-706-020
Operating Limitations: Refer to approved RFM

Type Certificate Holder: Bell Helicopter Textron, Inc.
Aircraft Model: 214ST
Engine Model: 2 x General Electric CT 7-2A or T700/T2C
Flight Crew: 2 (IFR), 1 or 2 (VFR)
Maximum Passengers: 18
Maximum Airspeed: Vne (IAS) varies with pressure altitude and temperature
Maximum Take-Off Weight: 7,938 kg
Operating Limitations: Model 214ST helicopters are eligible for Category A when operating in accordance with the procedures and limitations of FAA Approved Model 214ST RFM Supplement 8