N9375B

Question 1

Stall speeds, power off, max gross, V_S & V_S0

Answer 1

Wings level, flaps up: 49 MPH IAS
Wings level, full flaps: 38 MPH IAS

Increase 12 to 13 MPH at 40 degrees bank.

Question 2

Max flaps extended, V_FE

Answer 2

102 MPH IAS

Question 3

Maneuver speed, V_A

Answer 3

127 MPH IAS

Question 4

Max structural cruising, V_NO

Answer 4

144 MPH IAS

Question 5

Never exceed, V_NE

Answer 5

180 MPH IAS

Question 6

Rotation speed, V_R

Answer 6

60 MPH IAS

Question 7

Best angle of climb speed, V_X

Answer 7

@ sea level & 2350 Ibs:
61 MPH IAS, flaps up,
60 MPH IAS, flaps 20 deg.
Increase 1 MPH per 1000 ft

Question 8

Best rate of climb, VY

Answer 8

@ sea level & 2350 Ibs:
84 MPH IAS, flaps up.

Decreases 1 MPH for every 2500 ft up to 10,000 ft and reduce 9 to 10 MPH @ 1700 Ibs.

Question 9

Normal climb speed

Answer 9

80 to 90 MPH IAS

Question 10

Best glide, power off, flaps up, V_BG

Answer 10

70 MPH IAS

Question 11

Normal approach speed

Answer 11

65 to 75 MPH IAS, flaps down,

70 to 80 MPH IAS, flaps up.

Question 12

Short field approach speed over obstacle

Answer 12

@ 2350 Ibs:
63 MPH IAS (Cessna),
~36 MPH IAS (MASA STOL).

@ 1700 Ibs:
54 MPH IAS (Cessna).

Full flaps.

Question 13

Empty weight

Answer 13

1484.5 lbs (includes full oil and unusable fuel)

Question 14

Max gross weight

Answer 14

2350 lbs

Question 15

Useable fuel

Answer 15

43 gal or 258 lbs (6 lbs/gal)

Question 16

Cruise mixture setting

Answer 16

75 deg F rich of peak

Question 17

Climb mixture setting

Answer 17

100 deg F rich of peak

Question 18

Take off mixture setting above 3000 ft

Answer 18

150 deg F rich of peak

Question 19

Power setting, 72%, sea level

Answer 19

2400 RPM
23.0 in Hg
9.0 GPH
(Probably a little higher due to Powerflow tuned exhaust)

Question 20

Power setting, 72%, 2500 ft

Answer 20

2400 RPM
22.5 in Hg
9.1 GPH
(Probably a little higher due to Powerflow tuned exhaust)

Question 21

Power setting, 72%, 5000 ft

Answer 21

2400 RPM
22.0 in Hg
9.1 GPH
(Probably a little higher due to Powerflow tuned exhaust)

Question 22

Take off distance over 50 ft obstacle

Answer 22

Cessna POH approximately:
Sea level, 59 F: 700-1400 ft
5000 ft, 41 F: 1000-2000 ft

MASA STOL approximately:
Sea level: < 800 ft

Increase 10% for each 25 F above standard atmosphere

Ground run a little more than half.

Cessna POH:
sea level & 59 F:
1340 ft @ 2350 Ibs, 680 ft @ 1700 Ibs.

@ 5000 ft & 41 F:
1980 ft @ 2350 Ibs, 940 ft @ 1700 Ibs.

MASA STOL @ sea level & 59 F:
< 810 ft @ 2250 lbs

Question 23

Max rate of climb

Answer 23

Cessna POH:
@ sea level & 59 F:
850 fpm @ 2350 Ib,
1395 fpm @ 1700 Ib.

@ 10.000 ft & 23 F:
380 fpm @ 2350 lb,
790 fpm @ 1700 lb.

Question 24

Landing distance over 50 ft obstacle

Answer 24

Cessna POH approximately:
Sea level, 59 F: 900-1200 ft
5000 ft, 41 F: 1000-1300 ft

MASA STOL approximately:
Sea level: < 600 ft

Ground roll a little more than half.

Cessna POH:
sea level & 59 F:
1154 ft @ 2350 Ibs,
895 ft @ 1700 lbs.

@ 5000 ft & 41 F:
1290 ft @ 2350 Ibs,
980 ft @ 1700 Ibs.

Ground roll a little more than half.

MASA STOL @ sea level & 59 F:
< 595 ft @ 2250 lbs