Section 4 - Performances

Updated on 13 Feb 2023
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Article Summary

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
WEIGHT [kg]	BANK ANGLE [deg]	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	ISA
S.L.	Ground Roll	208	258	313	374	290
S.L.	At 50 ft AGL	266	331	404	485	373
1000	Ground Roll	230	284	346	413	315
1000	At 50 ft AGL	294	366	447	537	407
2000	Ground Roll	254	315	382	457	343
2000	At 50 ft AGL	326	406	495	595	444
3000	Ground Roll	281	348	423	505	374
3000	At 50 ft AGL	401	499	610	733	529
4000	Ground Roll	311	385	468	560	408
4000	At 50 ft AGL	401	499	610	733	529
5000	Ground Roll	345	427	519	620	445
5000	At 50 ft AGL	445	555	677	814	579
6000	Ground Roll	383	474	575	688	486
6000	At 50 ft AGL	495	617	753	906	633
7000	Ground Roll	425	526	639	764	531
7000	At 50 ft AGL	551	686	839	1008	693
8000	Ground Roll	472	585	710	849	581
8000	At 50 ft AGL	614	765	934	1123	759
9000	Ground Roll	525	650	790	945	635
9000	At 50 ft AGL	685	853	1042	1253	833
10000	Ground Roll	585	724	879	1052	696
10000	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	ISA
S.L.	Ground Roll	100	127	158	194	146
S.L.	At 50 ft AGL	131	167	207	254	190
1000	Ground Roll	112	142	177	216	160
1000	At 50 ft AGL	146	186	231	283	209
2000	Ground Roll	125	159	197	242	175
2000	At 50 ft AGL	163	208	258	316	229
3000	Ground Roll	140	177	221	270	192
3000	At 50 ft AGL	204	260	323	395	277
4000	Ground Roll	156	198	247	302	212
4000	At 50 ft AGL	204	260	323	395	277
5000	Ground Roll	175	222	277	338	233
5000	At 50 ft AGL	229	291	362	443	305
6000	Ground Roll	196	249	310	379	256
6000	At 50 ft AGL	257	326	406	496	335
7000	Ground Roll	220	280	348	426	282
7000	At 50 ft AGL	288	366	455	557	370
8000	Ground Roll	247	314	391	478	312
8000	At 50 ft AGL	323	411	512	626	408
9000	Ground Roll	278	353	440	538	344
9000	At 50 ft AGL	364	462	575	704	450
10000	Ground Roll	313	397	495	605	380
10000	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	ISA
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	ISA
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	ISA
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
RPM*	MAP [inHg]	ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)
RPM*	MAP [inHg]	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [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
RPM*	MAP [inHg]	ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)
RPM*	MAP [inHg]	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [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
RPM*	MAP [inHg]	ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)
RPM*	MAP [inHg]	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [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
RPM*	MAP [inHg]	ISA - 30°C (-15°C)			ISA (15°C)			ISA + 30°C (45°C)
RPM*	MAP [inHg]	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [lt/hr]**	PWR	KTAS	F.C. [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	ISA
S.L.	Ground Roll	183	202		220	238	213
S.L.	*At 50 ft AGL*	288	312		335	358	326
1000	Ground Roll	190	209		228	247	219
1000	*At 50 ft AGL*	297	324		345	369	334
2000	Ground Roll	197	217		237	256	226
2000	*At 50 ft AGL*	306	331		356	381	342
3000	Ground Roll	204	225		245	266	232
3000	*At 50 ft AGL*	325	352		379	405	360
4000	Ground Roll	212	233		255	276	239
4000	*At 50 ft AGL*	325	352		379	405	360
5000	Ground Roll	220	242		264	287	247
5000	*At 50 ft AGL*	335	363		391	418	369
6000	Ground Roll	228	251		275	298	254
6000	*At 50 ft AGL*	346	375		403	431	378
7000	Ground Roll	237	261		285	309	262
7000	*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	ISA
S.L.	Ground Roll	150	166		181	196	175
S.L.	*At 50 ft AGL*	233	252		271	290	264
1000	Ground Roll	156	172		187	203	180
1000	*At 50 ft AGL*	240	260		280	299	270
2000	Ground Roll	162	178		194	211	185
2000	*At 50 ft AGL*	248	268		288	309	277
3000	Ground Roll	168	185		202	219	191
3000	*At 50 ft AGL*	263	285		307	328	291
4000	Ground Roll	174	192		209	227	197
4000	*At 50 ft AGL*	263	285		307	328	291
5000	Ground Roll	181	199		217	235	203
5000	*At 50 ft AGL*	272	294		317	339	299
6000	Ground Roll	188	207		226	244	209
6000	*At 50 ft AGL*	280	304		327	350	307
7000	Ground Roll	195	215		234	254	215
7000	*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°)

What's Next

Section 5 - Weight & Balance

Table of contents

Stall Speed
Take-Off Performances
Take-Off Rate Of Climb
Enroute Rate Of Climb
One-Engine Rate Of Climb
Cruise Performances
Landing Performances
Balked Landing Climb Gradient