Matches in DBpedia 2014 for { ?s <http://dbpedia.org/property/eng1Note> ?o. }
- AMS_Carat eng1Note "Max power: 44kW at 3000 rpm, Max continuous power: 40kW".
- ATOL_495 eng1Note ":::::1x Rotax 912 iS on LSA version".
- Adamoli-Cattani_fighter eng1Note "- actual power 119 kW".
- Aero_HC-2_Heli_Baby eng1Note "::or 1x Avia M 110H 4-cyl air-cooled piston engine rated at".
- Aerosport_Rail eng1Note "De-rated to 25hp each".
- Aichi_S1A eng1Note "at take-off".
- Albatros_D.XII eng1Note "**second prototype - 1x BMW IIIa 6-cyl.water-cooled in-line piston engine developing 138 kW".
- Antoinette_III eng1Note "at 1,100 rpm".
- Antonov_An-180 eng1Note "at take off".
- Arado_Ar_195 eng1Note "for take-off".
- Arado_Ar_197 eng1Note "for take-off".
- Arado_Ar_65 eng1Note "for take-off, continuous maximum power".
- Arado_Ar_67 eng1Note "::: at".
- Arado_Ar_67 eng1Note "for take-off".
- Arado_Ar_68 eng1Note "300.0".
- Arado_Ar_68 eng1Note "60.0".
- Arado_Ar_80 eng1Note ":::::or :::1 x Rolls-Royce Kestrel VI rated :::1 x Rolls-Royce Kestrel V rated for take-off and at".
- Arado_Ar_80 eng1Note "at".
- Arado_Ar_96 eng1Note ":::Ar 396A-1: 1 x Argus As 411MA inverted V-12 air-cooled piston engine".
- Auster_Atom eng1Note "at 2350 rpm".
- Avia_BH-21 eng1Note "@ 1,850rpm".
- Aviatik_(Berg)_D.II eng1Note "1".
- Aviatik_Alliance_Aleks-251 eng1Note "in prototype".
- Avro_684 eng1Note "at 3,000 rpm at".
- BAT_F.K.26 eng1Note "at 1,450 rpm".
- BAT_F.K.27 eng1Note "at 1,850 rpm".
- Bachem_Ba_349 eng1Note "::::: Marschofen auxiliary chamber".
- Bachem_Ba_349 eng1Note "main chamber".
- Bates_Monoplane eng1Note "3".
- Bell_309_KingCobra eng1Note "or alternative engine, 1 Pratt & Whitney Canada T400-CP-400 turboshaft,".
- Beneš-Mráz_Be-50_Beta-Minor eng1Note "for take-off".
- Bereznyak-Isayev_BI-1 eng1Note "1100.0".
- Birdman_Project_102 eng1Note "to 25 hp".
- Bloch_MB.150 eng1Note "::::or 1 x Gnome-Rhône 14N-49 engine rated at".
- Bloch_MB.300 eng1Note "at".
- Blohm_&_Voss_BV_141 eng1Note "at sea level".
- Blohm_&_Voss_BV_141 eng1Note "at".
- Blohm_&_Voss_BV_141 eng1Note "for take-off at sea level".
- Blohm_&_Voss_BV_142 eng1Note "for take-off".
- Blohm_&_Voss_BV_144 eng1Note "for take-off at sea level".
- Blohm_&_Voss_BV_155 eng1Note ":::: at :::: at".
- Blohm_&_Voss_BV_155 eng1Note "for take-off".
- Blohm_&_Voss_BV_222 eng1Note "for take-off".
- Blohm_&_Voss_BV_238 eng1Note "at".
- Blohm_&_Voss_BV_238 eng1Note "for take-off".
- Blohm_&_Voss_Ha_137 eng1Note "::: at".
- Blohm_&_Voss_Ha_137 eng1Note "for take-off".
- Blohm_&_Voss_Ha_139 eng1Note "for take-off".
- Blohm_&_Voss_Ha_140 eng1Note "at".
- Blohm_&_Voss_Ha_140 eng1Note "for take-off".
- Boeing_XB-59 eng1Note "14000".
- Bombardier_Challenger_850 eng1Note "for take=off in ISA + 8°C".
- Bonomi_BS.19_Alca eng1Note "or".
- Bonomi_BS.22_Alzavola eng1Note "or".
- Breda_Ba.88 eng1Note "::Ba.88M: 2 x Fiat A.74 RC.38 14-cyl. air-cooled radial piston engines".
- Breda_Ba.88 eng1Note "for take-off".
- CANT_Z.1010 eng1Note "Licence built de Havilland Gipsy Major".
- CANT_Z.1011 eng1Note "270000.0".
- Cameron_D-38 eng1Note "with V-belt reduction".
- Caproni_CH.1 eng1Note "at".
- Caproni_Ca.49 eng1Note "224".
- Caproni_Vizzola_F.5 eng1Note "at take-off".
- Carden-Baynes_Auxiliary eng1Note "L.E. Baynes noted 8-9 hp maximum at 3,500 rpm".
- CarterCopter eng1Note "for take-off".
- Cessna_Citation_Latitude eng1Note "est.".
- Cessna_Citation_Longitude eng1Note "est.".
- Cessna_Citation_Sovereign eng1Note "at sea level up to *Maximum continuous thrust: up to".
- Chernov_Che-24 eng1Note "liquid cooled flat four".
- Colomban_MC-30_Luciole eng1Note "Direct Drive".
- Comp_Air_Jet eng1Note "for take-off".
- Comper_Kite eng1Note "take-off maximum at 3,500 rpm".
- DFS_228 eng1Note "::::: at operational altitude".
- DFS_228 eng1Note "at sea level".
- DFW_C.V eng1Note "or C.III N.A.G.".
- Dago_Red eng1Note "race tuned".
- Daimler_L15 eng1Note ". Removable for use as glider".
- Dassault_Communauté eng1Note "+ residual thrust".
- De_Bothezat_helicopter eng1Note ".".
- Denel_Dynamics_Bateleur eng1Note ":::or 1x Subaru EA-82T 4-cyl. four stroke horizontally opposed piston engine, rated at 86kW".
- Dewoitine_D.30 eng1Note "these were fitted in 1935. It is not certain if these or the lower powered Qa variant initially used provided the performance shown below.".
- Dornier_Do_11 eng1Note ":::::: at".
- Dornier_Do_11 eng1Note "for take-off".
- Dornier_Do_12 eng1Note "** or 1 × Argus As 10 inverted V-8 air-cooled piston engine rated at".
- Dornier_Do_17 eng1Note "with 1,000 PS for take-off".
- Dornier_Do_317 eng1Note "::Do 317B - 2x Daimler-Benz DB 610A/B rated at".
- Dornier_Rs.II eng1Note "1".
- Douglas_Cloudster_II eng1Note "ref| states two Continental W-670 of equivalent rating.|group=nb".
- Douglas_Dolphin eng1Note "::or 2x Pratt & Whitney R-1340-96 Wasp engines ;".
- E-Genius eng1Note "at 2,000 rpm, max".
- Eta_(glider) eng1Note "approximately".
- Eurocopter_EC135 eng1Note "or 2 x Pratt & Whitney Canada PW206B turboshaft engines rated at".
- Extra_EA-400 eng1Note "for takeoff, continuous".
- F_L_S_Z_Der_Kricket_DK-1 eng1Note "approximate power".
- Fairey_FB-1_Gyrodyne eng1Note "at 3,000 rpm".
- Farner_HF_Colibri_1_SL eng1Note ", coupled to drive a single, foldable propeller".
- Fiat_AN.1_(aircraft) eng1Note "maximum at 1,700 rpm".
- Fieseler_Fi_5 eng1Note "for take-off".
- Fliegende_Panzerfaust eng1Note "Total weight 150 kg".
- Focke-Wulf_Fw_300 eng1Note ":::or 4 x Daimler-Benz DB 603E inverted V-12 liquid-cooled piston engines".
- Fokker_50 eng1Note ":::Fokker 60: 2x Pratt & Whitney Canada PW127B turboprop engines".