M
C
310R P
C
O
H
310
H 1.0
1.0 1
23 M
2010
M
C
C
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310R P
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1.0 2
23 M
2010
M
E F MA IMUM R T L
C
310R P
O
A CE A D
ECIFICA I
.
..
H
EIGHT: .. 5535 P 5500 P 5400 P 4900 P
. .
F *SPEED, BEST PO ER MI TURE: M S L
.
. .
M
R C 75% P 7500 F . *RANGE, RECOMMENDED LEAN MI TURE: M R C 75% P 7500 F (600 P U F ) 75% P 7500 F (978 P U F ) 75% P 7500 F (1218 P U F ) M R 10,000 F (600 P U 10,000 F
(978 P
10,000 F
(1218 P
RATE OFACLIMB AT SEAL LE EL: E O E I SER ICE CEILING: A E O E I TAKEOFF PERFORMANCE: (82 KIAS, 15 G R T D (O 50 F O LANDING PERFORMANCE: (93 KIAS, 35 G R T D (O 50 F O STANDARD EMPT EIGHTS: (A 310R .. 310R II BAGGAGE ALLO ANCE: ING LOADING: PO ER LOADING:
.. ..
.
.. ..
U U
F
)
F
) F
.. . )
. 207 KTAS
.
.
195 KTAS
. 494 N 2.62 H . 884 N 4.63 H . 1132 N 5.91 H
M , 193 KTAS M , 193 KTAS M , 194 KTAS
616 N 4.12 H . . 1152 N 7.87 H . . 1511 N 10.46 H
M , 148 KTAS M , 145 KTAS M , 144 KTAS
..
1662 F 370 F
P P
M M
.... 19,750 F 7400 F F ) F
5500 P
) 1335 F . 1700 F
.. 5400 P
) ..
.. 640 F 1790 F
) ) . . . ..
. 30.73 P . 9.65 P
1.0 3
.. . P P
3347 P 3589 P 950 P S F H
23 M
2010
M
FUEL CAPACIT : (T ) S (100 G A A A OIL CAPACIT : (T ) ENGINES: S C ,F I 285 R H PROPELLERS: C S ,F NOTE: R 45% *S
U T T T
) (40 G (63 G (63 G
,T
310R P
O
H
. U U U
E A 2700 P F
C
) ) )
.. .. L
.. 102 G 143 G 166 G 207 G .. 25 Q
. . T
..
. . ..
IO 520 M
RPM B
6 4.5 D ,
,,
.. 0850334 26 ,
,
45
. E
M
C
.
1.0 4
23 M
2010
M
C
310R P
O
H
EC I 2 I I A I AB E F C INTRODUCTION AIRSPEED LIMITATIONS ENGINE LIMITATIONS EIGHT LIMITS MANEU ER LIMITS
I
. .5 ... 6 . 7 .. 9 .. 10
E
FLIGHT LOAD FACTOR LIMITS FLIGHT CRE LIMITS OPERATION LIMITS FUEL LIMITATIONS
10 . 10 10 . 11
D C I S
2
P
O
H ,
,
, , ,
, ,
.
1.0 5
23 M
2010
M
AI
EED I I A I
(S
AI
F
C
310R P
O
H
2 1)
EED I I A I
F
AB E
21
1.0 6
23 M
2010
M
AI
C
EED I DICA
F
310R P
O
H
AB E
22
E GI E I I A I N E E E . M
E M M O
: 2 : T C N : IO 520 M L T
M C
O
(A A
:
)
1.0 7
23 M
2010
M
O
: N
R (1) (2)
. O
O
H
P
:2 : M C A : 0850334 26 B :3 : 6 4.5 : (A 30 I S ) L P 13.9 +/ 0.2 F 81.7 +/ 0.3 L : 2700 RPM
I
.M
M
:
O
2100 2700 RPM (R
D
,C
A
C
: (1) N (2) M P (1) N
: O
(1) N (2) M .O P : (1) M (2) N (3) M H (1) N (2) M
2500 RPM (G R )
A )
: O
.O T
. C
310R P
:
P. N . M .P .N . D . B
E . T
C
15.0
24.5
75 240 F (G 240 F (R R )
A )
O
) A )
O
10 PSI (R R 30 60PSI (G 100 PSI (R R )
O
: 200 460 F (G 460 F (R R )
T
H .M
P
(G
A )
A )
1.0 8
23 M
2010
M
,F
F : (1) M (2) N
O O ( ) G
R
( ) B ( )
T
EIGH M M M M M
R
O
310R P
2.5 PSI (R R ) 15.0 24.5 H .M 45% P 59.0 P 55% P 71.0 P 65% P 82.0 P 75% P 94.0 P 75% C
S
P
107.0 P
A S L T (19.7 PSI) 150.0 P
( ) B
(3) M
C
C
A
T 2000 F 4000 F 6000 F 155.0 P
O
H
(G A ) (6.5 PSI) (7.6 PSI) (8.8 PSI) (10.25 PSI) (12.0 PSI)
P S (20.5 PSI)
146.5 P
P C P S 134.0 P (17.0 PSI) 124.0 P (15.0 PSI) 116.0 P (13.5 PSI) (21.7 PSI) (R R )
I I R T L
5535 : P 5500 : P : 5400 P F : 4900 P B C . L R L 120 . N B 350 . A C (S 96) 200 . A C (S 124) 160 . A C (S 126) 160
: . . .E
S
(4 P 6( P
S S
89 ). S ). S
109. 109 132. 111 132.
1.0 9
23 M
2010
M
A E
E
C
310R P
O
H
I I
T
.A
,
,
.
F IGH
AD FAC
I I
T
150%
,
. A D
T
5500 P
. L . L
,
F IGH C E M
,
0
: +3.80 1.52G 35 +2.0G
I I F
C
FAR 91
.
E A I G I I T
FR ,
. IFR
FAA.
1.0 10
23 M
2010
M
F E F
I I A I
P
(S
F
C
O
H
2 3)
: . M . M
F
310R P
: 2.5 PSI (0 P P H ) : 21.7 PSI (155.0 P P H (A F G C ): . 100LL G A F (B ). . 100 (F 100/130) G A F
F E
)
(G
).
AB E
F
23
1.0 11
23 M
2010
M
C
EC I E E GE C AB E
FC
310R P
3 CED
O
H
E
E
INTRODUCTION EMERGENC PROCEDURES ABBRE IATED CHECKLISTS E I P F P E D E L F S E E S A B F F I A I F P
.. . 12 . . 13 . . 13
P P P E
.. P
E I
... .. . .... . . . .. ... . .. ..
..
P E
P
S
E
. 26 E
.
S
I
18 19 20 23 24 25 25 26 26
.. . 27
D C I S
3
P .T
O
H .A .
1.0 12
23 M
2010
M
C
310R P
O
H
E E GE C CED E ABB E IA ED CHEC I P
A
C .
AI C
EED F
AFE
E A I
: 1. T 2. L 3. S
D . . . .
A M I O E O E
E GI E I
I G
1. T 2. P 3. M F A M P A C
E GI E FAI 1. T 2. B
C O I I
S E
I B B
E A I E
E GI E EC
4. 5. 6. 7. 8. 9.
5500 P 5400 P ,S L
CED
S A R
CED
.. ..80 KIAS . 92 KIAS 95 KIAS UP) . 106 KIAS ..
C C
S S
(F
E
E
CLOSE FEATHER IDLE CUT OFF S F S S
OFF P
OFF OFF OFF (O
S
)
OFF CLOSE
F ED
I G A E FF (
B
92 IA )
CLOSE IMMEDIATEL AS REQUIRED
1.0 13
23 M
2010
M
E GI E FAI 1. 2. 3. 4. 5. 6.
E AF E
M P T F L I
A E FF (
. I
F
E
.. F
FF
EE
F . . . .
13. A S
C E S
F A M A A P
310R P
92 IA
AS REQUIRED FULL FOR ARD FULL FOR ARD UP , G CHECK UP E DETERMINE:
7. E B 6 8. C C 50 F O 9. C B S E 10,000 F 10. T T ADJUST 5 11. C 12. I
A
C
G
O
I
H
)
, RETRACTED
FOOT OFF RUDDER RETARD THROTTLE SET PROP CONDITION LE ER
R
E SECURE OFF F P OFF S OFF OFF LAND
92 KIAS C S
(I
106 KIAS
; 94 KIAS
) :
1.0 14
23 M
2010
M
E GI E FAI
ED
1. I 2. B
E I
. . . . .
F F F S F Q O P M
.
M
. I . . F
H
ON
CHECK
F
E
)
FOOT OFF RUDDER RETARD THROTTLE SET PROP CONDITION LE ER
E F
E
IDLE CUT OFF OFF F P OFF S OFF S OFF OFF CLOSE ADJUST
S
F E
S
C .
SECURE:(P F
M F A M P A C
O
:
CHE CK I , MAIN TANKS CHECK O T S CHECK ON
E
.. M P . F
DETERMINE, E ,
ADJUST
3. I
4. O
310R P
I G F IGH
S
. . . . . . .
C
ASASREQUIRED REQUIRED AS REQUIRED E
• •
A P
F MAIN TANK 1000 AGL MAIN TANK. I , .C
5. T 6. E 7. A S
. A . C T
, .
F P ON F AS REQUIRED ADJUST 5
L A P
DECREASE LAND
1.0 15
23 M
2010
E GI E I 1. 2. 3. 4. 5. 6. 7. 8.
F A A M P P A L
C
E
)
310R P
O
H
E A I E A DI G S
MAIN TANK F P ON (O A C IN AS REQUIRED S OFF (O FULL FOR ARD 106 KIAS G DO N
9. F DO N 10. S DECREASE 11. A M C S E GI E I
M
E A I EG
S
)
93 KIAS 80 KIAS
A
D(
A
92 IA )
A
I G
L , . I
, 15
1. T
FULL FOR ARD
2. M
AS REQUIRED
3. P
R
C
4. L
G
UP
5.
F
UP,
6. C
F
OPEN
7. C
B
S
ESTABLISH
E
R
C
S
106 KIAS
; 94 KIAS
10,000 8. T
T
ADJUST 5
1.0 16
23 M
2010
M
AI
C
O
H
A
A
O 1. A
P
F
P
,
U
S
CHEC K OFF I ON
LO ,
2. M 3. F
ON
FOR ARD AS REQUIRED FOR ARD
7. S
B
PRESS
8. P
S
ACTI ATE
9. S
P
10. A
F
11. M
F
200 F
AS REQUIRED ON
H E GI E FAI F
2. L
ED
I GC
I E F IGH
UP G
UP
3. P
6. L
RELEASE LO
INCREASE
14. A
5. A
S P
AS REQUIRED
12. P
4. C
OFF,
MAIN TANK
6. P
1.
OFF ,
.
S S
4. T 5. M
13. C
:
IDLE CUT OFF, 15
B
310R P
FEATHER F
CLOSE 111 KIAS R
FORCED LANDING (C
P
L
)
1.0 17
23 M
2010
M
FI E FI E
CED
C
310R P
O
H
E
HE G
D (E
,
A
D
) 1. T
CLOSE
2. B
AS REQUIRED
3. M
IDLE CUT OFF
4. B
OFF (U
5. M
G
OFF (U
B ) G
B )
6. E I F IGH
I G
1. B
E GI E FI E
A
F
2. A
P
E . T
CLOSE
. P
FEATHER
. M . F . C .
IDLE CUT OFF S
OFF
F
CLOSE
M
. P
OFF S
. A 3. C
H
OFF
SECURE
OFF (O
S
)
OFF OFF
4. L
1.0 18
23 M
2010
M
I F IGH CABI FI E 1. E
C
310R P
O
H
E
L
REDUCE
2. A 3.
OPEN
4. C
A C
OPEN
; CLOSE
5. L
E E GE C DE CE EFE
ED
CED
1. T
ADJUST
4.
F
5. L
UP G
6. M 7. A
UP B INITIATE 220 KIAS
E
A
1. T
HE IC C
FULL FOR ARD
3. M 5. L
DI I
IDLE
2. P 4.
E
FULL FOR ARD
3. M
B
E
IDLE
2. P
I
CED
ADJUST F
DO N 35 G
DO N
6. M
B
INITIATE
7. A
138 KIAS
1.0 19
23 M
2010
M
E E GE C F
A DI G
CED A DI G ( S
CH ECK (O
2. L
G
DO N
. N
INITIATE(K 100 KIAS
. A S . C D
E M UNLATCH
. M S
) )
15 OFF
OFF
S
OFF
. L
A
NOSE HIGH
CED A DI G (C
)
IDLE CUT OFF
2. P 3. F
15
IDLE CUT OFF
. M
1. M
H
UP
. A
F
O
E
100 KIAS
L
G
.
310R P
)
1. L
3. L
F
CED
C
FEATHER S
OFF
4. A S
E
5. A
111 KIAS
6. I S
B
H G
. L .
F
. B
AS REQUIRED
D
. N
S
. L
G F
L
)
UP 97 KIAS
. B .
INITIATE(K : DO N 15
. A . C
OFF UNLATCH
L S
.
: DO N
S
. C 7. I R
S
OFF
S D
OFF UNLATCH
A
NOSE HIGH
1.0 20
23 M
2010
M
A DI G
I HF A
1. L
G
AI GEA L
C
310R P
O
H
I E
DO N
2. F
S
SELECT
3. F
S
MAIN TANKS
4. 5.
F
DO N 35
6. I
,
,
7. L 8. U 9. A 10. S
A DI G
I H DEFEC I E
1. F
S
2. F
S
3.
SELECT MAIN TANKS HEAD IND
4. L 5. 6. A
AI GEA
G F
7. B
DO N DO N 35 ALIGN AIRPLANE
S
OFF
8. L
L.
9. G
L
10. M
INITIATE IDLE CUT OFF
11. U 12. A 13. F 14. A
S
OFF E ACUATE
1.0 21
23 M
2010
M
A DI G
I HF A
1. L
E GEA
G
L B
3. A
100 KIAS A
5. N
310R P
O
H
I E
DO N
2. P 4. L
C
MO E AFT 15
F
NOSE HIGH
HOLD OFF
6. B
MINIMUM
7. T
RETARD
8. C 9. M
FULL AFT
A DI G
I H DEFEC I E
1. I S
H
S
. B
:
P
. L
G
MO E AFT
DO N
. A
100 KIAS
. L
A
. N .
E GEA
F
HOLD OFF
B
MINIMUM
. T
RETARD
. C .
15
NOSE HIGH
FULL AFT
M
2. I R
S . L
S
:
G
UP
. A
100 KIAS
. A S
E
. C
D
. L .
NOSE HIGH IDLE CUT OFF
. M . F
F OFF
UNLATCH A
M
15
M
S S
OFF OFF
1.0 22
23 M
2010
M
A DI G
I H
F A
1. M
310R P
O
H
)
AS REQUIRED
2. P 3. F
(0 E
C
FULL FOR ARD S
MAIN TANKS
4. M
A
5. L
S
G
105 KIAS
DO N
DI CHI G 1. L
G
UP
2. A 3.
HEAD IND F
4. P
; PARALLE L S ELLS
DO N 35 AS REQUIRED (300 F
P
5. A
93 KIAS
6. A
DESCENT ATTITUDE
F E
E
E E GE C
E GI E D I E F E 1. F
S
2. A 3. C 4. M 5. A S
D
CED
)
E
E
MAIN TANK F
F
FAI
M
P
ON
OPEN ADJUST A P
LAND
6. F
1.0 23
23 M
2010
M
E EC A
E
ICA A
E
FAI
1. E
L
2. I C
E(
C
E E GE C
310R P
CED
O
H
E
)
REDUCE
B
I T
B
D
:
. T . R . T . I 3. I C
, N
T
:
. S . I
,
. I
,
. I
,
. I ,
1.0 24
23 M
2010
M
A
E
A
FAI
1. E
E (D
L
2. I C
C
310R P
O
H
)
REDUCE
B
A
T
:
. T . R . T . I
,
. I
D.
,
. R . I
,
3. I C
B
H
N
T
:
. T . C . T . I
,
. I .
D.
,
R
. I
,
. R .
A I
I
,
IC B
1. A
FAI
M
2. E
F IGH I AC
E
S A
OFF P
E FAI
,
S
ON
E E GE C
E (A
D
CED G
E
)
1. F 2. A 3.
P
CHECK
1.0 25
23 M
2010
M
B
C I
ICI G F
1. A
S
2. E
AI I
S A
E
FI A C
( )
INCREASE
3. M
( ) LEAN
E GI E I
CH
CH
1. P 2. P
2.
E
E OFF (O
S
)
OFF (O B
S ) PULL (O
E
S S
H
CED
PULL OUT
CED
C
E E GE C E I 1. R
MAINTAIN
S
HA E FAI
H
HA E
E A I E
1. P
O
CE
E ICI G E E GE C
2. P
E E
310R P
OPEN
A
1. A
A IC
C
S
)
I D
PULL PUSH OUT
1.0 26
23 M
2010
M
C
310R P
O
H
I 1. T
CLOSE IMMEDIATEL
2. A
NEUTRALI E
3. R
HOLD FULL RUDDER
4. C 5. I
FOR ARD BRISKL , E
6. A
INCREASE PO ER
(I N
)
: . R . I . C
NEUTRALI E E (I U )
DECREASE PO ER
PULL
.A
1.0 27
23 M
2010
M
C
EC I A AB E
310R P
H
4 CED
FC
O
E
E
INTRODUCTION P
28 I
.
NORMAL PROCEDURES AMPLIFIED CHECKLISTS A
S
B S
S
B
T
.
29
.. ..
31
O
31
E
. 32 .. 33
E
.. 34
T
34
B
T
..
35
T
36
A
T
..
38
C
..
38
C
.
39
D
.
B
L
B
L
A
41 42
L
42
S
I
41
..
43
D C I S
4
P
O
H
. T .
1.0 28
23 M
2010
M
EF IGH I
C
310R P
O
H
EC I
1.0 29
23 M
2010
M
C
310R P
O
H
1.0 30
23 M
2010
M
C
A A AI
310R P
CED
IFIED CHEC
EED F
AFE
O
H
E I E A I
1.0 31
23 M
2010
M
BEF
E
A
D
3. C
LATCHED L
SECURE
B
,
S
H
ADJUST
SECURE
S S
BOTH ENGINES SET TO MAIN TANKS
7. L
G
S
8. M 9. P
DO N
FULL RICH FULL FOR ARD
10. T
OPEN ONE INCH
11. C
B
IN
12. E
A
13. E
A
14. A
M
15. A
F
16. B
F P S P
R
18. L
G
OFF ON
AS REQUIRED L
20. A
23. F
T
I
L
SET
SET (O
S
)
SET AS REQUIRED
A C C
ON
LOCKED FULL OPEN CHECK
A C
25. A
C
PRESS TO TEST C
F Q
OFF OFF
OFF
P
19. A
21. C 22. F
S S
S
A
17. L
26. A
H
REMO E
,S
5. B
24. C
O
C
2. C
6. F
310R P
I G E GI E
1. P
4. S
C
L
IN ON
1.0 32
23 M
2010
M
A
C
310R P
O
H
I G E GI E
1. P
CLEAR
2. M
S
3. E
S
4. A 5. T
ON
. S
B
PRESS
. P
S
L
F
P 800
6. O P
E
E
RIGHT
LO 1000 RPM
10 PSI . I
7. A
LEFT, R
30
,
60
, ON AND CHECK
1.0 33
23 M
2010
M
BE
C
310R P
O
H
E A II G 1. P
B
2. A 3. A 4.
S
ON
SET F
5. L 6. C
COMPLETE
M UP
AS REQUIRED T
AS REQUIRED
. I
: . C . D
A K K
OPEN AS REQUIRED
. T . C . H
C H R
OPEN
HEAT AS REQUIRED
. I
: . C
A K
. C
H
. H 7. B
K
S
OPEN S
R
FAN D
A
AS REQUIRED
RELEAS E (P
, ).
A II G 1. T 2. B 3. F
AS REQUIRED CHECK I
CHECK
1.0 34
23 M
2010
M
BEF
C
310R P
O
H
E A E FF
1. B
SET
2. E
R
COMPLETE
. T
1700 RPM
. A
CHECK
.
S
. M
CHECK 4.75
5.25
H .
CHECK 150 RPM
50
RPM . P P
.
CHECK
1200 RPM;
RPM (F
E
I
CHECK
. T
2100 RPM
. G
CHECK (R
RPM,
RPM).
.
P
FULL FOR ARD
.
T
RETARD TO IDLE
3. F 4. F
Q S
5. A
CHECK CONFIRMMAIN TANKS SELECTED LEFT AND RIGHT ENGINES A C
6. C
F
7. T
T
SET
8.
F
UP
9. F
I
10. L
TAKEOFF
D
SET CLOSED
L
13. A
F
14. F
17. B
, A
12. A
16. S
IN
LOCKED FULL OPEN
AS REQUIRED
11. A C
15. I
F
)
CLEAR P
C P
ON CHECK
E B
S
AS REQUIRED H
SECURE
RELEASE
1.0 35
23 M
2010
M
C
310R P
O
H
A E FF A
A E FF
1. P
FULL THROTTLE
2. M
*
LEAN
3. E
I
CHECK
4. A M 5. E 6. L
2700 RPM
C C
O
92 KIAS
S
80 KIAS
R
83 KIAS 5500
(R
S
5
)
1.0 36
23 M
2010
M
A I
E F
1.
F
3. P
FULL THROTTLE
LEAN
5. B
RELEASE
6. P
CHECK 2700 RPM
7. E
C
*
N
H
*
4. M
O
O
DO N 15 SET
9. L
310R P
A CE A E FF
2. B
8. A M
C
R C
70 KIAS S
82 KIAS
5500
80 KIAS (R
S
5
: S
)
, S.
,
, . I
, . A
,
RPM
2100,
,
.
1.0 37
23 M
2010
AF E
M
C
F
U
310R P
O
H
A E FF
1. B
APPL
2. L
G
3.
RETRACT
F
4. B
A
5. B
R
(R
UP C
S
C
85 KIAS
S
S
89 KIAS
15,000
107 AS KI
5
00 55 ).
C I B C
I EC I B 1. P
2500 RPM
2. A
115 KIAS
3. M 4. C
H
ADJUST F
5. A
A I
24.5 130 KIAS
OPEN F
P
ON
12,000
C I B
1. P
FULL THROTTLE
2. Q
F
3. P
S . P
L
2700 RPM TIGHTEN
(
PHASING (O K
S S
I
)
)L
ADJUST
1.0 38
23 M
2010
M
C
C
310R P
O
H
I E 1. C
P
2100
2. M
2500 RPM ,
F
H .
OAT
.
OPEN
4. P
S NCHRONI E
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F
6. P
S
L
T
K F
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S
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T
OFF
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T
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LO
(
)
LO
T
OFF
. C 8. F
24.5
.
R 3. C
15.0
LEAN
LO
S
L
. I
E
LEFT MAIN, R E
RIGHT MAIN
40
,
MAIN TANKS
63
,
MAIN TANKS
60 . I 90 . U . I
,
MAIN TANKS
, 180
AU ILIAR TANKS
. I
,
9. I
, . M
SELECT
:
C
1.0 39
23 M
2010
M
. H
C
. O
10. T N
C
310R P
O
H
P F
F . D
)
T
ADJUST
I
C
: N
F
50%
(I
70%
T
M
I
P
. T
RPM
. A (24.5
H .M
% 2500 RPM)
75
. ,
H .
,
, ,
F
.
, .
1.0 40
23 M
2010
M
C
310R P
O
H
DE CE 1. F
S
2. P 3. C
LEFT AND RIGHT ENGINES SET TO MAIN TANKS AS REQUIRED
F
AS REQUIRED
4. M
ADJUST
5. A
SET
N
: D I
,
.
T
500
.
T
.
RPM
BEF
(
).
ON; U
L
E A DI G
1. S
B
2. P 3. F
S
9. M 10. P 11. M
S
)
BOTH ENGINES SET TO MAIN TANKS F
5. A
7. L 8. L
SECURE OFF (O
S
4. A 6.
H
S P
ON
A C F
CHECK IN
DO N 15 G G
P
DO N
158 KIAS 138 KIAS L C
I
OFF
FULL RICH FULL FOR ARD M
E
A
S
93 KIAS
5400
(R
S
5
) 12. A M
C
S
80 KIAS
1.0 41
23 M
2010
M
BA
C
310R P
O
H
ED A DI G 1. I
2700 RPM
2. M
AS REQUIRED
3. B
L
4. L
5.
T G
S
RETRACT
F
15
7. C
F
OPEN
8.
F
UP
85 KIAS IFR
IFR
6. T
AF E A DI G 1. A F
P
2. C
F
OPEN
3.
F
UP
LO
1.0 42
23 M
2010
M
H
310R P
O
H
D 1. P
B
2. A
SET
M
S
3. A S
E
4. A
F
OFF B
P
,A
IDLE
6. M
IDLE CUT OFF A
8. M
S
OFF
B
S
11. C
L
INSTALL
13. C
OFF
OFF,
10. M 12. F
S
OFF
S
9. A
M
OFF
5. T 7. B
N
C
S
OFF
OFF D
CLOSE
:
IDLE CUT OFF, .T
,
OFF H.
,
,
OFF .
1.0 43
23 M
2010
M
C
EC I E F AB E
310R P
O
H
5 A CE
FC
E
INTRODUCTION
45
AIRSPEED CALIBRATION
.
46
ALTIMETER CALIBRATION
48
TEMPERATURE RISE DUE TO RAM RECO ER O
..
O
50
TEMPERATURE CON ERSION F TO C
.. 51
PRESSURE CON ERSION INCHES OF MERCUR TO MILLIBARS STALL SPEEDS
.
52 53
IND COMPONENT NORMAL TAKEOFF DISTANCE
.
54
..
55
.
57
MA IMUM PERFORMANCE TAKEOFF DISTANCE
56
ACCELERATE STOP DISTANCE ACCELERATE GO DISTANCE
58
RATE OF CLIMB M
C
C O
.
C
59 ... 60
E
I
.. 61
BALKED LANDING CLIMB R
C
.
ONE ENGINE INOPERATI E SER ICE CEILING TIME, FUEL AND DISTANCE TO CLIMB M C
62
. 63
C
64
C
.
65
CRUISE PERFORMANCE 2,500 F
..
.. 66
5,000 F
..
.. 66
7,500 F
..
.. 67
10,000 F
.. 67
15,000 F
.. 68
RANGE PROFILE
69
ENDURANCE PROFILE
.. 70
HOLDING TIME
. 71
TIME, FUEL AND DISTANCE TO DESCEND NORMAL LANDING DISTANCE FUEL FLO
.. 72 73
SCHEDULE
74
1.0 44
23 M
2010
M
I
C
310R P
O
H
D C I S
5
P
O
H
. S . T
, ,
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,
,
,
,
A.
45
. T
, .1 H .
H .
29.92,
100
100
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T
, .P 1. T
:
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S
,A
G ,L
, 2. C
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E
.
T
, .
1.0 45
23 M
2010
M
AI
C
310R P
O
H
EED CA IB A I A
A IC
CE
1.0 46
23 M
2010
M
AI A
E
C
310R P
O
H
EED CA IB A I A E
A IC
CE
1.0 47
23 M
2010
M
A
C
I E E C A
A IC
310R P
O
H
EC I CE
1.0 48
23 M
2010
M
A A
C
I E E C E
A E
310R P
O
H
EC I
A IC
CE
1.0 49
23 M
2010
M
C
310R P
O
H
1.0 50
23 M
2010
M
C
310R P
O
H
1.0 51
23 M
2010
M
E I CHE
F
C
EC E C
310R P
E
O
H
I I IBA
1.0 52
23 M
2010
M
C
A
310R P
O
H
EED
1.0 53
23 M
2010
M
C
I DC
310R P
O
H
E
1.0 54
23 M
2010
M
A
C
310R P
A E FF DI
O
H
A CE
1.0 55
23 M
2010
M
A I
E F
C
310R P
O
A CE A E FF DI
H
A CE
1.0 56
23 M
2010
M
C
ACCE E A E
310R P
DI
O
H
A CE
1.0 57
23 M
2010
M
C
ACCE E A E G DI
310R P
O
H
A CE
1.0 58
23 M
2010
M
C
310R P
O
H
1.0 59
23 M
2010
M
A E
C
FC I B
C
310R P
O
H
I EC I B
1.0 60
23 M
2010
M
A E
FC I B
C
310R P
E E GI E I
O
H
E A I E
1.0 61
23 M
2010
M
C
310R P
O
H
1.0 62
23 M
2010
M
E E GI E I
C
310R P
E A I E E
O
H
ICE CEI I G
1.0 63
23 M
2010
M
C
310R P
O
H
1.0 64
23 M
2010
M
C
310R P
O
H
1.0 65
23 M
2010
M
C I H EC
C
I E E F
310R P
O
H
A CE
E DED EA
I
E
1.0 66
23 M
2010
M
C I H EC
C
I E E F
310R P
O
H
A CE
E DED EA
I
E
1.0 67
23 M
2010
M
C I H EC
C
I E E F
310R P
O
H
A CE
E DED EA
I
E
1.0 68
23 M
2010
M
C
A GE
310R P
O
H
FI E
1.0 69
23 M
2010
M
E D
C
A CE
310R P
O
H
FI E
1.0 70
23 M
2010
M
H
C
310R P
O
H
DI G I E
1.0 71
23 M
2010
M
C
I E, F E A D DI
310R P
A CE
O
H
DE CE D
1.0 72
23 M
2010
M
A
C
310R P
A DI G DI
O
H
A CE
1.0 73
23 M
2010
M
C
F E F
310R P
CHED
O
H
E
1.0 74
23 M
2010
M
C
EC I
310R P
FC
H
6
EIGH & BA A CE/E AB E
O
I
E
I
E
INTRODUCTION AIRPLANE
75
EIGHING FORM
76
EIGHT AND MOMENT TABLES
I
.. 77
D C I S
6
P
O
H
.
1.0 75
23 M
2010
M
AI
A E
C
310R P
O
H
EIGHI G F
1.0 76
23 M
2010
M
C
EIGH A D
310R P
E
O
H
AB E
1.0 77
23 M
2010
M
C
EIGH A D
310R P
E
O
H
AB E
1.0 78
23 M
2010
M
C
EC I
310R P
O
H
7
E AB E
FC
E
INTRODUCTION
80
PILOT S LO ER S ITCHES
81
AIRCRAFT PO ER METER
. 82
PILOT S SIDE S ITCHES
.. 83
HORI ONTAL SITUATION INDICATOR (HSI) ARTIFICIAL HORI ON (AH) .
..
85 87
..
ENGINE INSTRUMENTS
.
.
AUTOMATIC DIRECTION FINDER (ADF)
.
.
92
.
94
.
101
AUTOPILOT THROTTLE QUADRANT FUEL S STEMS
. .
88
. 107
MISCELLANEOUS S STEMS
.
PREFLIGHT UTILIT
.
CREDITS AND DISCLAIMER INFORMATION
. .
1.0 79
111 115 116
23 M
2010
M
I
S
C
310R P
O
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D C I
7 M
C
310R. T
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,
1.0 80
23 M
2010
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2010
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23 M
2010
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23 M
2010
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,
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FLT INST
ENG INST FUEL SEL .F
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1.0 84
23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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C
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
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23 M
2010
M
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23 M
2010
M
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23 M
2010
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23 M
2010
M
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23 M
2010
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C
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23 M
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