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An 2 Checklist

The document provides a checklist for preflight inspection, starting procedures, warm up, engine testing, and checks before taxiing an Antonov AN-2 aircraft. It includes over 50 individual inspection and procedure items to verify components, settings, and instrument readings are within normal ranges at each stage. The checklist ensures the aircraft and engine are thoroughly checked and prepared prior to taxi, takeoff, and flight.
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© Attribution Non-Commercial (BY-NC)
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0% found this document useful (0 votes)
1K views18 pages

An 2 Checklist

The document provides a checklist for preflight inspection, starting procedures, warm up, engine testing, and checks before taxiing an Antonov AN-2 aircraft. It includes over 50 individual inspection and procedure items to verify components, settings, and instrument readings are within normal ranges at each stage. The checklist ensures the aircraft and engine are thoroughly checked and prepared prior to taxi, takeoff, and flight.
Copyright
© Attribution Non-Commercial (BY-NC)
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 18

1a

ANTONOV AN-2
Check-list

Normal procedures
Unusual procedures
Emergency procedures
Figures, numbers & facts

N82AN

1b

Courtesy of Dr. Phil Clarke


& Revised by John Webster

2a

PREFLIGHT INSPECTION:
1. Cockpit check:
1. Control lock................................REMOVED & STOWED
2. Parking brake...............................................................SET
3. Log book, flight doc. & legal forms...................ON BOARD
4. All switches..................................................................OFF
5. Magneto switch.................................................." 0 " (OFF)
6. Windows.................................................................CLEAN
2. Engine group:
1. Propeller..CLEAN, TURNED CCW 15 - 20 times
2. Engine cowling latches............ALL CLOSED & LOCKED
3. Oil cooler................................................................CLEAN
4. Dust filter (if installed)..........................CHECK POSITION
5. Oil purge............(bottle stowed)..............................DONE
6. Oil quantity.................................CHECKED (50 - 70 litres)
3. Main landing gear:
1. Tires condition & pressure (40 PSI ).............OK
2. Brakes....................................................................CLEAN
3. Check shock absorber compression according to scale:

90 9 mm when airplane weight is 3600 Kg


117 17
"
"
" " 4200 Kg
135 14
"
"
" " 4800 Kg
148 15
"
"
" " 5250 Kg
154 15
"
"
" " 5500 Kg

7920 lbs
9240 lbs
10,560 lbs
11,550 lbs
12,100 lbs

4. Left & right wings:


1. Fabric skin.................................................NO DEFECTS
2. Tie downs & Control locks...............................REMOVED
3. Carrying tapes holding & tighting...........NOT TOO WEAK
4. Lower surface of upper wing.........NO GASOLINE LEAKS
5. Pitot cover.......................................................REMOVED
6. OAT probe cover.............................................REMOVED
7. Navigation & landing lights glasses.....................CLEAN
8. Side fuselage........NO CRACKS, NO DEFORMATIONS
5. Tail section:
1. Shock absorber compression......NORMAL... (50-70 mm)
2. Shock absorber.........................................NO OIL LEAKS
3. Tire pressure......................................................NORMAL
4. Fabric skin of control surfaces....................NO DEFECTS
5. Navigation light...........................................UNDAMAGED
6. Tie downs & Control locks...............................REMOVED
7. Fairing mounting screws..........TIGHT & NONE MISSING
6. Pax - Cargo cabin:
1. Cargo loading, arrangement & mounting..................OK
2. Rear section loading...................................................OK
3. Doors.............................................................SECURED
4. All "remove before flight" flags..REMOVED & COUNT=8

PREFLIGHT

2b
BEFORE STARTING:
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
20.
21.
22.
23.
24.
25.
26.
27.
28.

Propeller(within 10 minutes) PULLED CCW 15 - 20 times


Oil collector can.....................................REMOVED & STOWED
Doorstep..............................................REMOVED & SECURED
Emergency manhole................................CLOSED & SECURED
Magneto switch.........................................................." 0 " (OFF)
Flight controls..............................FREEDOM OF MOVEMENTS
Air system charging valve.................................................OPEN
Air pressure.......................................................... CHECK > 30
Parking brake......................................................................SET
Brake pressure system............................................CHECK > 6
Battery switch......................................................................ON
Bus voltage.................................................................... > 24 V
On control desk, switch ON:
10
fuel tank meter
engine unit gages
flap position & oil cooler shutters indicators
OAT + mixt. T
oil cooler shutters
cowl flaps
fire ext.
warning bell f
Rotating Beacon
Left & Right fuel gages..............................CHECK QUANTITY
Trim tabs........set to neutral....... (3 GREEN INDICATORS LIT)
Oil coolers shutters & cowl flaps............CHECK DEFLECTION
Fuel selector valve......................................................" BOTH "
Fire Extinguisher....................CHECKED (yellow indicator ON)
"Chip Monitoring" button..............................PRESS TO TEST

ENGINE START: if CHT & Oil T > 05 (if not: oil dilution)
1.
2.
3.
4.
5.
6.
7.
8.
9.

Propeller(within 10 minutes) PULLED CCW 15 - 20 times


Propeller control...
.........................FORWARD (Low Pitch)
Mixture control... ..............................BACKWARD (Full Rich)
Fuel master lever.....................................OPEN = FORWARD
Carburetor heater.. ..........................................................OFF
Oil cooler shutter........................................................CLOSED
Cowl flaps...................................................................CLOSED
Fuel pressure (with manual pump)...........................0.25 - 0.35
Primer pump to cylinders.........if CHT < 80 :
2 - 6 injections MAX in the summer (or soon after stop)
6 - 10 injections MAX in the winter
10. Primer pump lever.......................................................LOCKED

BEFORE STARTING - START

3
a

11. MAKE SURE PROP. AREA IS....................................... CLEAR


12. Magneto switch..............................................................OFF " 0 "
13. " Starting seqence " switch.....................................................ON
14. Starter....................ON.........................Until 8 ON AMPMETER
15. Then toggle the switch to interconnect engine shaft
16. Magneto switch........................................................BOTH " 1+2 "
17. After start: fuel pressure with manual pump..................025 - 0.35
Rem: if engine fires back into carburetor, do a few smooth
injections with the primer pump, without touching the throttle
18. Throttle (when engine runs smoothly)...................700 - 800 RPM
19. Check oil pressure..... Normal (> 3).....within 10 sec, if not: STOP
20. "Starting sequence" switch....................................................OFF
21. Generator...............................................................................ON
22. A/C Converter.........................................................................ON
23. Primer pump lever........................................................LOCKED

ENGINE WARM UP:


1. Throttle 1000 RPM until.... Oil T rises, but in less than 3 minutes
2. Throttle 1200 RPM until..........................CHT >100 & Oil T >30
3. Throttle 1600 RPM until..........................CHT >120 & Oil T >50

ENGINE TEST:
- to be done in 4 minutes MAX (insufficient cooling)
- control wheel in backward position all-through the test
1. Establish max. continuous rated power...........................2100 / 9
2. Check "in the green":
Oil pressure..............................4 - 5
Fuel pressure..................0.25 - 0.35
Oil T..................................60 - 70
CHT.......................................< 215
3. Throttle. .................................................................... 2000 RPM
4. Magnetos check (15 sec. each)....................... drop < 60 RPM
5. Throttle.... ...................................................................1900 RPM
6. Propeller.. ............"coarse pitch".........result = 1450 - 1550 RPM
7. Propeller.... .............."fine pitch".........result = 1900 RPM by itself
Rem: repeat 2 or 3 times in cold weather
8. Throttle. ..................................................................... 2100 RPM
9. Set with propeller gov..
1900 RPM & then with throttle 10-15:
engine speed as a result must remain constant
10. Throttle. ................900 RPM................then swiftly back to 1900:
Rem: engine may increase to 2000 - 2050 but stabilize
to 1900 in 3-5 sec.

WARM UP - TEST

1. Throttle.. .................................................................1850 RPM :


A/C voltage................................... > 75.5 V
mixture check : 1-2 cm from extreme forward position
carburetor heater
check (10-15 sec): 150 - 250 RPM
drop. Warning: backfire should not occur this moment
2. Set take-off power for 10 - 15 sec, must have:
Engine speed: 2150 - 2200 RPM
M.P: 10.5 (if more, do not set max throttle for take-off)
3. Set throttle to....................................................IDLE (< 20sec) :
Engine speed.................550 RPM
Oil pressure............................ 1.5
Fuel pressure........................ 0.15
Oil T.............................. 60 - 75
Generator OFF: check Gen warning ON & note the
negative deviation (to the left) of the ampmeter pointer
Generator: ON
4. Add throttle: Gen warning should go OFF at 900-1100 RPM
5. 2 or 3 engine transitions...... IDLE <-> 2100 RPM (in 2 - 3 sec),
CHT must be > 120

BEFORE TAXI:
1. Pax & cargo doors.....................................CLOSED & LOCKED
2. All necessary switches..........................................................ON
3. Flaps upper & lower................................................OPERATIVE
4. Engine control lever positions. ...... ...... ....................CORRECT
5. Indications of engine gages..............NORMAL "All in the green"
6. Fuel quantity in each tank..........................................CHECKED
7. A/C Converter.........................................................OPERATIVE
8. "Artificial horizon, course indic. & gyro compass" switches..ON
9. Gyro instruments.......................................................SLAVED
10. Navigation instruments...............................CHECKED & SET
11. GPS....................................................................................ON
12. Transponder.....(1200)...." STDBY "......& 2 switches.......ON
13. Air pressure in pneumatic system.................................... > 40
14. Wheel chocks.............................................CHECK REMOVED
15. Tail wheel ..............................................................UNLOCKED
16. Block time..............................................................RECORDED

Note : Tail wheel locking has been disabled on this aircraft.

BEFORE TAXI

3b

4a

TAXI :
1. Lights...............................................................AS REQUIRED
2. If snow or OAT................................................................... < 0
pitot heat...........................................................ON
keep mixture T > 8 with carburetor heater... .......ON
3. All necessary switches.........................................................ON
4. Brakes......................................................................CHECKED
5. In turns, gyro indications.........................................CORRECT
6. ROTATING BEACON ..ON

BEFORE TAKE-OFF:
1.
2.
3.
4.
5.
6.
7.
8.

Voltage & Load meter...................................................CHECK


Navigation instruments & Com's ......................CONFIRM SET
Carburetor heater..... .......................................................OFF
Mixture..... ..........................................................FULL RICH
Fuel selector valve....................................................." BOTH "
Altimeters.........................................................................SET
Gyro compass.........SLAVED & SET TO RUNWAY HEADING
Set trim tabs:
Elevator........DOWN: If heavy for 10 sec.; if not 3 - 5 sec.
Rudder..........RIGHT for 3 seconds
9. Flaps..................................SET FOR TAKE-OFF (usually 15)
10. Flight controls............................FREEDOM OF MOVEMENTS
11. Artificial horizon.......................CHECK NORMAL INDICATION
12. Transponder......................................................set on "Alt "
13. Engine gages.........normal indications: " ALL IN THE GREEN "
14. Cowl flaps & Oil cooler shutters.....................................OPEN
15. Lights..............................................................AS REQUIRED
16. Pax seat belts....................................................FASTENED
17. Take-off time....................................................RECORDED
18. Parking brake....................................................RELEASED

TAXI - BEFORE TAKE OFF

TAKE-OFF:
1. Without flaps:
Engine parameters..........................9 / 2100
Speed up to...................................140 Km/h 75 Kts
then resume climb
2. With flaps (wind < 20 Kts): reduces take-off distance by 35 %
If 15: engine...................................9 / 2100
If 25: engine...................................9 / 2100
If 30 (max weight)......................10.5 / 2200
rotation speed...........................85 - 90 Km/h 48 Kts
Speed-up to ..................................120 Km/h 65 Kts
Flaps over 150 Ft..............gradually drawn-in
Full drawing of flaps at...................140 Km/h 75 Kts
then resume climb

CLIMB:
1. Establish initially.............................9 / 2050 (9 / 2100 if urgent)
2. When altitude > 150 Ft.............................................8.5 / 1850
3. Speed..................................................140 - 150 Km/h 78 Kts
Rem: if max. rate of climb required, keep 5 of flaps
until passing 1500 Ft before retracting.
4. Check :
Oil T...................... < 70
CHT ......................< 215
5. Lights................................................................CONSIDERED

CRUISE:
1. Engine parameters (RPM - M. P.)...................CHECK TABLE
2. Check :
Oil T........................................ 60 - 75
CHT: 120 - 215 (recommended: 150 - 215)
Oil Pressure.................................... 4 - 5
Fuel Pressure........................ 0.25 - 0.35
Compressor pressure...................45 - 50
Voltages.......................> 28.5 V & > 75 V
3. Check mixture T for carburetor heater
need.......if < 0an..
.....................................AS REQUIRED (Max CHT: 215)
4. Flaps................................................................................. 0 ?

TAKE OFF - CLIMB - CRUISE

4b

5a
a
a
a
a
a
a
a

DESCENT :
1. Establish................................ 5.2 / 1500 (= 180 Km/h 97 Kts)
2. Maximum speed for descent:
Quiet air.......................220 Km/h 119 Kts
Turbulent air.................190 Km/h 102 Kts
3. Maintain ..........................................CHT > 120 & Oil T > 50
Rem: if necessary close cowl flaps & oil cooler or descent by steps

4.
5.
6.
7.
8.
9.

Carburetor heater
ON If.................................... OAT < -15
Fuel selector.............................................................." BOTH "
Parking break...CONFIRM OFF & PRESSURE IN BRAKES "0"
Air pressure ............................................................check > 40
Flaps........................................................RESYNCHRONISED
Flaps..as required

3.
4.
5.
6.
7.

Speed.........................................................< 140 Km/h 75 Kts


Flaps....................................CHOOSE SETTING (usually 15)
Landing lights......................................................................ON
Tail wheel locking..............................................CONSIDERED
CROSS WIND....CONSIDERED

D
E
S
C
E FINAL:
N
T
1. Throttle.. ............................................................................< 5
2. Propeller.... .........................................................FULL PITCH
:

CLEAR OF RUNWAY:
1.
2.
3.
4.
5.
6.
7.

Tail wheel.............................................................UNLOCKED
Landing lights...................................................................OFF
Taxi light..........................................................CONSIDERED
Pitot heat..........................................................................OFF
Flaps....................................................................................0
Transponder.............................................................." STBY "
Cowl flaps & Oil cooler shutters....................................OPEN

DESCENT - FINAL - CLR

5b
COOLING DOWN & SHUT DOWN:
1. Avionics & XPDR switches.................................................OFF
2. Set throttle.........................................................700 - 800 RPM
3. Cowl flaps & Oil cooler shutters.......................................OPEN
4. Let CHT cool down.......................................................< 120
5. Electrical switches & radios.................................................OFF
6. For a few seconds: throttle........1700 RPM, then.........800 RPM
7. Fuel master valve. .....................................................CLOSED
8. Throttle...PROGRESSIVELY INCREASED DURING SHUT-OFF
9. Cowl flaps & Oil cooler shutters......if T < 100...........CLOSED
10. Air system charging valve............................................CLOSED
11. Controls & ailerons......................................................LOCKED
12. Oil & Air system purges...................................................DONE
If parked outside....................AIRCRAFT MUST BE TIED-DOWN
And Control Locks installed.

Flight Plan Closed ?

COOLING DOWN & SHUTDOWN

10

6a

ENGINE TEST GRAPHIC

11

ACCEPTABLE AIRSPEEDS (Km/h)

In turbulent air:
< 190
Diving (2200 RPM) = VNE = 300
To extend flaps:
< 150
With 30 flaps:
< 150
With 40 flaps:
< 130
Minimum in horizontal flight: 120

(Kts)
102
160
85
85
70
65

WIND LIMITATIONS (in Kts):


Take-off & Landings:
Head wind
45 Cross wind
90 Cross wind, no flaps
90 Cross wind, flaps
Taxiing:

Normal
airstrip

Slippery
airstrip

32
14
14
8
32

16
8
6
6
16

AIRSPEED INDICATOR (Km/h)

(Kts)

160
121-160
54 -121
54-70

VNE:
Yellow zone:
Green arc:
Flaps white arc:

300
225 300
100 225
100 130

RATE OF CLIMB at Max. Landing Weight (5250 Kg)


With 8.5 / 1850 @ 140 Km/h 75 Kts:

FL 0 to FL 65 : 600 Ft/min
FL 65 to FL 90 : > 400 Ft/min
FL 90 to FL 120 : > 200 Ft/min
FL 120 to FL 150 : > 100 Ft/min
Rem: service ceiling = 4400 metres at 5250 Kg
=14,400 ft. at 11,550 lbs.

OPERATIONAL SPEEDS

12

6b

FUEL CONSUMPTION (From T.O. to LDG):

FUEL SEQUENCE:
1. T.O. & Climb: BOTH
2. Before leveling: RIGHT for 120 - 150 litres
3. then: LEFT for 120 - 150 litres
4. then: RIGHT for 120 - 150 litres...
5. When total remaining fuel is about 300 litres: BOTH
Notes:
Fuel alarm = less than 110 litres remain (55 litres in each tank)
Continuous use of BOTH: more fuel used from the LEFT tank

FUEL

13

7b
CARGO WEIGHT versus FUEL QUANTITY IN TANKS:
It is possible to take-off with a crew of two + 75 litres of oil
taking ... Kg of cargo, with litres of fuel on board
1000=2200 lbs
1200=317 gal (max. fuel)
1150=2530 lbs
1000=264 gal
1300=2860 lbs
800=211 gal
1450=3190 lbs
600=160 gal
1600=3520 lbs
400=106 gal
1750=3850 lbs
200 =53 gal (min. T.O. fuel)
MAXIMUM PAYLOAD CALCULATION:

... litres of fuel X 0.72 = ... litres of oil X 1 = ... crew


X 80 = PAYLOAD =

2120 Kg
Kg
Kg
Kg
Kg

4660 lbs

ENGINE & ACCESSORY UNITS DATA:


CHT.....................................150 - 215, mini. OAT for starting +5
Oil T.......................................60 - 75,
"
Fuel Pressure:
at power..................0.25 - 0.35
at idle................................0.15
Oil pressure..................................4 - 5
Starter:
max consecutive startings........................................4
min breaks between startings sequences.........20 sec
time of switching ON the electric motor............13 sec
time of turning it manually.............................5 - 6 min
Compressor:
pressure...........................45 50 Kg/sq.cm
max temp................................110
time of max filling from 0........11 min
Converter:
voltage..................................28.5 V
loading current.......................100 A
max loading........150 A in max 2 min

PAYLOAD - CARGO vs FUEL - DATA

14

8a

ENGINE MANUAL START (Low batteries, no G.P.U.):


1. Propeller control.
................FORWARD (Low fine pitch)
2. Mixture control....... .................................FORWARD (Full rich)
.........................................700 - 800 RPM Position
3. Throttle...
4. Fuel master lever.. ..............................................FORWARD
5. Carburetor heater... ........................................................OFF
6. Oil cooler shutters.......................................................CLOSED
7. Cowl flaps...................................................................CLOSED
8. Magnetos..........................................................................OFF
9. Manually turn the prop.............................5 - 6 REVOLUTIONS
10. Fuel Pressure (with manual pump)...........................0.25 - 0.35
11. Primer pump to cylinders:
2 - 3 injections MAX in the summer
5 - 8 injections MAX in the winter
12. Primer pump lever..............................................................OFF
13. Battery................................................................................ON
14. Manual crank:
inserted into the special sleeve behind the copilot
turned clockwise gradually increasing speed 'till 80 RPM
15. Starter.................................................................................ON
16. Magnetos...................................................(1+2)............" BOTH "
17. Check oil pressure....Normal (>3)...within 10 sec, IF NOT: STOP
18. " Starter sequence " switch............................................."OFF "
19. Generator.............................................................................ON
20. Primer pump lever.......................................................LOCKED

Note : Most An-2 aircraft in U.S. have had the


manual starting Crank disabled.

MANUAL START

15

8b
AT ENGINE START IF FUEL BURNS WHEN
CARBURETOR BACKFIRES:
1. Magnetos........................................................" OFF "
2. Starter control.......................................................ON
Rem: Do not touch throttle at this time

3. If flames do not go out: "FIRE EXTING."...............ON

ENGINE FIRE:
1.
2.
3.
4.
5.

Fuel master lever........ ..............................CLOSED


Fuel selector.................................................CLOSED
Magnetos & Converter...................................." OFF "
Cowl flaps.....................................................CLOSED
" FIRE EXTING. " button............................PRESSED

CARB. BACKFIRE -ENGINE FIRE

16

9a

AIR START:
Cure the problem first:
1. Fuel Selector BOTH
2. Low fuel pressure (<0.25).............MANUAL PUMP
3. Fuel shut-off valve...............................FORWARD
4. Too much lean.....................................FULL RICH
5. Carb. icing (mixture T low)....CARB. HEATER ON
Air start: Rem: propeller will always keep turning
1. Set speed...............150 - 160 Km/h 80-85 Kts
2. Throtlle......................................................800 RPM
3. Magnetos....................................... 2-1..." BOTH "
4. Fuel tanks.................................................." BOTH "
5. Fuel Pressure with manual pump.............0.25 - 0.35
6. Mixture...................................................FULL RICH
7. Engine should restart at this point
Rem: if engine has been stopped for a long time, use
the starter for a few seconds.
GLIDING:

130 Km/h - 70 Kts


100 m

800 m
Engine....................................................STOPPED
Propeller.............................................FEATHERED
Any turn .......................= 60 metres loss in altitude

FLY THE AIRPLANE

AIR START - GLIDING

17

18

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