Type Certificate Holder: Airbus S.A.S. Aircraft Model: A319 Engine Model: 2 x CFM 56-5B5 jet engines Flight Crew: 2 Maximum Passengers: 145 Maximum Airspeed: 350 kt (VMO) Maximum Take-Off Weight: 75,500 kg Operating Limitations:
VFR day and night. Non-icing conditions. See the appropriate EASA approved Airplane Flight Manual
Type Certificate Holder: ATR-GIE Avions de Transport Régional Aircraft Model: ATR 42-500 Engine Model: 2 x Pratt & Whitney Canada PW 127E Flight Crew: 2 Maximum Passengers: 60 Maximum Airspeed: Refer to approved Airplane Flight Manual Maximum Take-Off Weight: 18,600 kg Operating Limitations: Day, Night, VFR and IFR. Icing Conditions. All Weather Capabilities CAT II
Type Certificate Holder: Honda Aircraft Company LLC Aircraft Model: HA-420 Engine Model: 2 x GE Honda Aero Engines HF120-H1A Flight Crew: 1 or 2 Maximum Passengers: 5 Maximum Airspeed: VMO (Max Operating Speed): 270 KIAS Maximum Take-Off Weight: S/N 42000012 thru 42000125: 4,808 kg. S/N 42000011, 42000126 and up: 4,853 kg
Operating Limitations: VFR Day and Night. IFR Day and Night.
Type Certificate Holder: Textron Aviation Inc. Aircraft Model: B300 Super King Air Engine Model: 2 x Pratt & Whitney of Canada, Ltd. PT6A-60A Flight Crew: 1 or 2 Maximum Passengers: 15 Maximum Airspeed: VMO (Max Operating Speed) 263 kts (up to 21,000 ft ). 263 – 194 kts above 21,000 ft up to 35,000 ft Maximum Take-Off Weight: 6,803.9 kg Operating Limitations: VFR Day and Night. IFR Day and Night. Icing Conditions
Type Certificate Holder: Textron Aviation Inc. Aircraft Model: 208B Engine Model: 1 x Pratt & Whitney of Canada Ltd. PT6A-114 or PT6A-114A Flight Crew: 1 or 2 Maximum Passengers: 9 (FAA), 12 (EASA) Maximum Airspeed: VMO (Max Operating) 175 KIAS. See POH/AFM for variations with weight and altitude Maximum Take-Off Weight: 3,968.9 kg Operating Limitations: VFR Day and Night, IFR Day and Night
Type Certificate Holder: Viking Air Limited Aircraft Model: DHC-6 Series 300 Engine Model: 2 x Pratt & Whitney Canada Inc. PT6A-27 Flight Crew: 1 or 2 Maximum Passengers: 20 Maximum Airspeed: VMO (Max Operating) S/L 160 Knots (Landplane) Maximum Take-Off Weight: 5,670 kg Operating Limitations: Day, Night, VFR and IFR when equipped
Type Certificate Holder: Embraer S.A. Aircraft Model: EMB-145LU Engine Model: 2 x Rolls-Royce Corp. USA AE3007A1 or AE3007A1 P turbofan engines Flight Crew: 2 Maximum Passengers: 50 Maximum Airspeed: Refer to approved Airplane Flight Manual Maximum Take-Off Weight: 21,990 kg Operating Limitations: All Weather Capabilities CAT II
Type Certificate Holder: Airbus Helicopters Deutschland GmbH Aircraft Model: EC135 T3H Engine Model: 2 x Arrius 2B2 Flight Crew: 1 or 2 Maximum Passengers: 7 Maximum Airspeed: VNE 150 KIAS at MSL Maximum Take-Off Weight: 2,980 kg Operating Limitations:
VFR day and night. Non-icing conditions. For IFR, Category A operation see additional equipment requirements and limitations in the relevant EASA-approved RFMS
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: 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
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