Section 4 - Performances

Stall Speed

Weight: 1180 kg

Throttle Levers: IDLE

Landing Gear: Down

CG: Most Forward (16.5%)

No ground effect

WEIGHT [kg]	BANK ANGLE [deg]	FLAPS 0°	FLAPS T/O	FLAPS FULL
KIAS	KCAS	KIAS	KCAS	KIAS	KCAS
1180 (FWD C.G.)	0	66	64	56	56	53	54
15	67	65	57	57	54	55
30	70	69	60	60	58	58
45	77	76	67	67	64	64
60	93	90	81	79	78	76

Take-Off Performances

Weight = 1180 kg Flaps: T/O Speed at Lift-Off: 65 KIAS Speed Over 50ft Obstacle: 70 KIAS Throttle Levers: Full Forward Runway: Grass	Corrections Headwind: - 2.5m for each kt (8 ft/kt) Tailwind: + 10m for each kt (33ft/kt) Paved Runway: - 6% to Ground Roll Runway slope: + 5% to Ground Roll for each +1%
Pressure Altitude [ft]		Distance [m]
Temperature [°C]	ISA
-25	0	25	50
S.L.	Ground Roll	208	258	313	374	290
At 50 ft AGL	266	331	404	485	373
1000	Ground Roll	230	284	346	413	315
At 50 ft AGL	294	366	447	537	407
2000	Ground Roll	254	315	382	457	343
At 50 ft AGL	326	406	495	595	444
3000	Ground Roll	281	348	423	505	374
At 50 ft AGL	401	499	610	733	529
4000	Ground Roll	311	385	468	560	408
At 50 ft AGL	401	499	610	733	529
5000	Ground Roll	345	427	519	620	445
At 50 ft AGL	445	555	677	814	579
6000	Ground Roll	383	474	575	688	486
At 50 ft AGL	495	617	753	906	633
7000	Ground Roll	425	526	639	764	531
At 50 ft AGL	551	686	839	1008	693
8000	Ground Roll	472	585	710	849	581
At 50 ft AGL	614	765	934	1123	759
9000	Ground Roll	525	650	790	945	635
At 50 ft AGL	685	853	1042	1253	833
10000	Ground Roll	585	724	879	1052	696
At 50 ft AGL	764	952	1163	1399	914

Weight = 930 kg Flaps: T/O Speed at Lift-Off: 65 KIAS Speed Over 50ft Obstacle: 70 KIAS Throttle Levers: Full Forward Runway: Grass	Corrections Headwind: - 2.5m for each kt (8 ft/kt)) Tailwind: + 10m for each kt (33ft/kt Paved Runway: - 6% to Ground Roll Runway slope: + 5% to Ground Roll for each +1%
Pressure Altitude [ft]		Distance [m]
Temperature [°C]	ISA
-25	0	25	50
S.L.	Ground Roll	100	127	158	194	146
At 50 ft AGL	131	167	207	254	190
1000	Ground Roll	112	142	177	216	160
At 50 ft AGL	146	186	231	283	209
2000	Ground Roll	125	159	197	242	175
At 50 ft AGL	163	208	258	316	229
3000	Ground Roll	140	177	221	270	192
At 50 ft AGL	204	260	323	395	277
4000	Ground Roll	156	198	247	302	212
At 50 ft AGL	204	260	323	395	277
5000	Ground Roll	175	222	277	338	233
At 50 ft AGL	229	291	362	443	305
6000	Ground Roll	196	249	310	379	256
At 50 ft AGL	257	326	406	496	335
7000	Ground Roll	220	280	348	426	282
At 50 ft AGL	288	366	455	557	370
8000	Ground Roll	247	314	391	478	312
At 50 ft AGL	323	411	512	626	408
9000	Ground Roll	278	353	440	538	344
At 50 ft AGL	364	462	575	704	450
10000	Ground Roll	313	397	495	605	380
At 50 ft AGL	409	520	648	792	498

Take-Off Rate Of Climb

Power Setting: Maximum Continuous Power Flaps: Take-Off Landing Gear: Up
Weight [kg]	Pressure Altitude [ft]	Climb Speed VY [KIAS]	Rate of Climb [ft/min]
Temperature [°C]	ISA
-25	0	25	50
1180	S.L.	85	1347	1154	982	826	1048
2000	82	1200	1010	841	688	933
4000	79	1054	867	701	551	818
6000	76	908	725	561	413	704
8000	73	763	583	422	277	589
10000	70	618	441	283	141	474
12000	67	473	300	145	5	359
14000	64	330	159	7	-130	244
930	S.L.	85	1803	1575	1372	1189	1451
2000	82	1630	1406	1206	1026	1315
4000	79	1457	1238	1041	864	1180
6000	75	1286	1070	877	703	1045
8000	72	1114	902	713	542	909
10000	69	944	735	549	382	774
12000	65	774	569	387	222	639
14000	62	604	404	224	63	503

Enroute Rate Of Climb

Power Setting: Maximum Continuous Power Flaps: Up Landing Gear: Up
Weight [kg]	Pressure Altitude [ft]	Climb Speed VY [KIAS]	Rate of Climb [ft/min]
Temperature [°C]	ISA
-25	0	25	50
1180	S.L.	84	1392	1205	1038	887	1102
2000	83	1249	1066	901	753	991
4000	81	1108	927	766	620	880
6000	79	966	789	630	487	768
8000	77	826	651	495	355	657
10000	75	685	514	361	223	546
12000	73	545	377	227	92	434
14000	71	406	241	93	-39	323
930	S.L.	82	1873	1649	1449	1269	1527
2000	81	1703	1483	1286	1109	1393
4000	79	1533	1317	1124	950	1260
6000	77	1364	1151	962	791	1127
8000	75	1196	987	800	632	994
10000	73	1028	823	639	474	861
12000	71	860	659	479	317	727
14000	69	693	496	319	160	594

One-Engine Rate Of Climb

Power Setting: Maximum Continuous Power (operative engine), propeller feathered (inoperative engine) Flaps: Up Landing Gear: Up
Weight [kg]	Pressure Altitude [ft]	Climb Speed VY [KIAS]	Rate of Climb [ft/min]
Temperature [°C]	ISA
-25	0	25	50
1180	S.L.	80	362	261	171	89	206
1000	80	324	224	134	53	176
2000	80	285	186	97	17	146
3000	79	247	148	60	-19	116
4000	79	209	111	24	-55	85
5000	79	171	74	-13	-91	55
6000	79	132	36	-49	-127	25
7000	78	94	-1	-86	-163	-5
930	S.L.	79	574	455	349	253	390
1000	79	529	411	305	211	355
2000	79	483	367	262	168	319
3000	78	438	322	219	126	284
4000	78	393	278	176	83	248
5000	78	348	235	133	41	213
6000	78	304	191	90	-1	178
7000	77	259	147	47	-43	142

Cruise Performances

Weight: 1150 kg										
Pressure Altitude: 0 ft										
		ISA - 30°C (-15°C)	ISA (15°C)		ISA + 30°C (45°C)		
RPM*	MAP	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**
	[inHg]			[lt/hr]			[lt/hr]			[lt/hr]
2250	29.5	103%	143	28.6	97%	145	27.1	92%	146	25.8
2250	28	88%	134	24.5	83%	136	23.2	79%	138	22
2250	26	69%	122	19.2	65%	124	18.2	62%	125	17.3
2250	24	59%	115	16.6	56%	116	15.7	53%	117	14.9
2250	22	46%	103	12.8	43%	103	12.1	41%	103	11.5
2250	20	39%	96	11	37%	95	10.4	35%	94	9.9
2100	28	84%	132	23.5	80%	134	22.2	76%	135	21.1
2100	26	66%	121	18.5	63%	122	17.5	60%	123	16.7
2100	24	57%	114	16	54%	114	15.1	52%	115	14.4
2100	22	43%	100	12.1	41%	100	11.5	39%	100	10.9
2100	20	37%	92	10.2	35%	91	9.7	33%	89	9.2
1900	26	61%	117	17.1	58%	118	16.2	55%	119	15.4
1900	24	53%	110	14.9	50%	111	14.1	48%	111	13.4
1900	22	41%	97	11.4	39%	97	10.8	37%	96	10.2
1900	20	35%	89	9.6	33%	88	9.1	31%	85	8.7
*Propeller RPM										
**Fuel Consumption for each Engine										

Weight: 1150 kg										
Pressure Altitude: 3000 ft										
		ISA - 30°C (-15°C)	ISA (15°C)	        ISA + 30°C (45°C)		
RPM*	MAP	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**
	[inHg]			[lt/hr]			[lt/hr]			[lt/hr]
2388	26.4	92%	141	25.7	87%	143	24.3	83%	144	21.1
2250	26.4	89%	139	25	85%	141	23.6	80%	143	22.4
2250	26	85%	137	23.9	81%	138	22.6	77%	140	21.5
2250	24	72%	128	20	68%	129	18.9	64%	130	18
2250	22	57%	116	16	54%	117	15.1	51%	118	14.3
2250	20	48%	108	13.4	45%	108	12.7	43%	108	12.1
2250	26.4	85%	137	23.9	81%	138	22.6	77%	140	21.4
2100	26	82%	134	22.8	77%	136	21.6	73%	137	20.5
2100	24	69%	125	19.2	65%	127	18.1	62%	128	17.2
2100	22	54%	114	15.2	51%	114	14.3	49%	115	13.6
2100	20	45%	104	12.6	43%	104	11.9	41%	104	11.3
2100	26.4	78%	132	21.9	74%	134	20.7	70%	135	19.6
1900	26	75%	130	20.9	71%	131	19.8	67%	132	18.8
1900	24	63%	121	17.7	60%	122	16.7	57%	123	15.9
1900	22	50%	110	14.1	48%	110	13.3	45%	110	12.6
1900	20	42%	101	11.7	40%	101	11.1	38%	100	10.6
*Propeller RPM										
**Fuel Consumption for each Engine										

Weight: 1150 kg										
Pressure Altitude: 6000 ft										
		ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)		
RPM*	MAP	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**
	[inHg]			[lt/hr]			[lt/hr]			[lt/hr]
2388	26.4	92%	141	25.7	87%	143	24.3	83%	144	21.1
2250	26.4	89%	139	25	85%	141	23.6	80%	143	22.4
2250	26	85%	137	23.9	81%	138	22.6	77%	140	21.5
2250	24	72%	128	20	68%	129	18.9	64%	130	18
2250	22	57%	116	16	54%	117	15.1	51%	118	14.3
2250	20	48%	108	13.4	45%	108	12.7	43%	108	12.1
2250	26.4	85%	137	23.9	81%	138	22.6	77%	140	21.4
2100	26	82%	134	22.8	77%	136	21.6	73%	137	20.5
2100	24	69%	125	19.2	65%	127	18.1	62%	128	17.2
2100	22	54%	114	15.2	51%	114	14.3	49%	115	13.6
2100	20	45%	104	12.6	43%	104	11.9	41%	104	11.3
2100	26.4	78%	132	21.9	74%	134	20.7	70%	135	19.6
1900	26	75%	130	20.9	71%	131	19.8	67%	132	18.8
1900	24	63%	121	17.7	60%	122	16.7	57%	123	15.9
1900	22	50%	110	14.1	48%	110	13.3	45%	110	12.6
1900	20	42%	101	11.7	40%	101	11.1	38%	100	10.6
*Propeller RPM										
**Fuel Consumption for each Engine										

Weight: 1150 kg										
Pressure Altitude: 9000 ft										
		ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)		
RPM*	MAP	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**	PWR	KTAS	F.C.**
	[inHg]			[lt/hr]			[lt/hr]			[lt/hr]
2388	21.1	75%	137	20.9	71%	139	19.7	67%	140	18.7
2250	21.1	73%	136	20.3	69%	137	19.2	65%	138	18.2
2250	20	65%	130	18.3	62%	131	17.2	58%	131	16.3
2250	18	53%	118	14.9	50%	119	14	48%	118	13.3
2100	21.1	69%	133	19.4	65%	134	18.3	62%	135	17.4
2100	20	62%	127	17.4	59%	128	16.4	56%	128	15.6
2100	18	51%	116	14.2	48%	116	13.4	46%	116	12.7
1900	21.1	64%	128	17.8	60%	129	16.8	57%	130	15.9
1900	20	57%	122	16	54%	123	15.1	51%	123	14.3
1900	18	47%	112	13.2	44%	112	12.4	42%	111	11.8
*Propeller RPM										
**Fuel Consumption for each Engine

Landing Performances

Weight = 1150kg Flaps: LAND Short Final Approach Speed: 70 KIAS Throttle Levers: Idle Runway: Grass	Corrections Headwind: -5m for each kt (16 ft/kt) Tailwind: +11m for each kt (36 ft/kt) Paved Runway: -2% to Ground Roll Runway slope: -2.5% to Ground Roll for each +1%
Pressure Altitude [ft]		Dinstance [m]
Temperature [°C]	ISA
-25	0	25	50
S.L.	Ground Roll	183	202	220	238	213
At 50 ft AGL	288	312	335	358	326
1000	Ground Roll	190	209	228	247	219
At 50 ft AGL	297	324	345	369	334
2000	Ground Roll	197	217	237	256	226
At 50 ft AGL	306	331	356	381	342
3000	Ground Roll	204	225	245	266	232
At 50 ft AGL	325	352	379	405	360
4000	Ground Roll	212	233	255	276	239
At 50 ft AGL	325	352	379	405	360
5000	Ground Roll	220	242	264	287	247
At 50 ft AGL	335	363	391	418	369
6000	Ground Roll	228	251	275	298	254
At 50 ft AGL	346	375	403	431	378
7000	Ground Roll	237	261	285	309	262
At 50 ft AGL	357	387	416	445	388

Weight = 930kg Flaps: LAND Short Final Approach Speed: 70 KIAS Throttle Levers: Idle Runway: Grass	Corrections Headwind: -5m for each kt (16 ft/kt) Tailwind: +11m for each kt (36 ft/kt) Paved Runway: -2% to Ground Roll Runway slope: -2.5% to Ground Roll for each +1%
Pressure Altitude [ft]		Dinstance [m]
Temperature [°C]	ISA
-25	0	25	50
S.L.	Ground Roll	150	166	181	196	175
At 50 ft AGL	233	252	271	290	264
1000	Ground Roll	156	172	187	203	180
At 50 ft AGL	240	260	280	299	270
2000	Ground Roll	162	178	194	211	185
At 50 ft AGL	248	268	288	309	277
3000	Ground Roll	168	185	202	219	191
At 50 ft AGL	263	285	307	328	291
4000	Ground Roll	174	192	209	227	197
At 50 ft AGL	263	285	307	328	291
5000	Ground Roll	181	199	217	235	203
At 50 ft AGL	272	294	317	339	299
6000	Ground Roll	188	207	226	244	209
At 50 ft AGL	280	304	327	350	307
7000	Ground Roll	195	215	234	254	215
At 50 ft AGL	289	313	338	361	315

Balked Landing Climb Gradient

Flight conditions (ISA and SL):

Weight: 1180kg
Throttle levers: Both FULL FORWARD
Flaps: T/O
Landing Gear: DOWN
Weight: MTOW (1180 kg)
Speed: 66KIAS
Climb Gradient: 10.8% (6.2°)

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