Archer Checkliste

Cruise -> below 75%
Climb -> above 5000ft DA (density altitude)
 

SETTING FOR BEST POWER (65%):

Cruise -> Peak EGT Mixer 50°F to rich (-2 Teilstriche)  or
           -> Peak RPM Mixer +1cm to rich

Climb -> Peak EGT Mixer 100°F to rich (-4 Teilstriche)  or
          -> Peak RPM Mixer +2cm to rich

MASS FACTOR:
Speed reduction on Final:  1 kt per 30 kg below MTOM

WIND FACTOR:
Speed increments on Final:
-> if windspeed or gust > 10% of vfinal
Add 1/2 of headwind component to vfinal

FINAL APPROACH SPEED = vfinal - Mass factor + Wind factor

BANK FACTOR:
if bank angle for turning final is more than 25°
-> add 5 kt to vintermediate

v_Initial APCH_80
v_intermediate_70
v_final_63

Runway .................. Wind, RWY, Touch down on __
Airspace ................. Einschränkungen
Routing................... via ___ @ ___ft, Downwind @ ___ ft, 80 kts
Emergencies.......... Missed APCH G/A, ___ circuit @ ___ft

Merke: RARE

Departure 
Take off procedure:
............. Wind, Temp., TOW (POB), RWY COND. -> Type of TKOF

Climb profil:
............... Safe altitude ___ft, vx_63, vy_79, @ ___ft vcc_87

Airspace:
............... Einschränkungen

Routing:
............... leaving via ___

Emergencies
Any Malfunction on GND:
............. Throttle idle, break, leave RWY via __

Engine failure on Climbout:
............  Nose down, Best glide_73, LDG straight ahead with Full Flaps

Major malfunction after TO:
............. Inner Circuit, Full stop

Merke: TCAR

1. Flaps............................................... UP  

2. Power ............................................. CHECKED

OAT >10°C min 2’ 
OAT <10°C min 5

1. Alternator.............................. OFF  

2. Throttle ................................. IDLE  

3. Magnetos grounding ............ AS REQUIRED / AT IDLE  

4. Mixture ................................. CUT OFF  

5. Magnetos ............................. OFF, KEY REMOVED

1. Power ................................... FULL OPEN  

2. Carburetor heat .................... OFF  

3. Attitude................................. ROTATE according Speed  

4. Speed above 55 + pos ROC FLAPS RETRACT

1. Carburetor heat .................... OFF

1. Speed................................... BELOW 103  

2. Flaps..................................... 40  

3. Speed................................... V FINAL ___ 

1. Power ................................... SET  (on circuit about 1700 RPM)

2. Speed................................... BELOW 103  

3. Flaps..................................... 25  

4. Speed................................... 70  

5. Start...................................... DESCENT 

1. Speed................................... BELOW 103  

2. Flaps..................................... 10  

3. Speed................................... 80

1. Mixture ................................. ADJUST  (1cm nach reich alle 1000 ft)

2. Attitude................................. FOR DESCENT  

3. Power ................................... RPM ___  

4. Trim....................................... ADJUST 

1. Mixture ................................. ADJUST  

2. Power ................................... SET  

3. Attitude................................. ADJUST  

4. Trim....................................... ADJUST 

1. Altitude ................................. (... FT / FL ...)  

2. Attitude................................. ADJUST  

3. Power ................................... RPM ___  (on circuit about 2000 RPM)

4. Trim....................................... ADJUST  

5. Mixture ................................. ADJUST 

1. Reaching ___ FT / FL

1. Speed................................... V CC 87  

2. Fuel pump ............................ OFF / PRESSURE CHECKED 

MIN 400 FT AAL 

1. Runway & Heading Indicator COMPARE  

2. Time...................................... CHECKED  

3. Take off power...................... SET / MNM 2200 RPM

4. Speed................................... RISE 

Merke: HTPS

1. Wind (RTF / Windsock)......... DIRECTION / SPEED  

2. Runway ................................ IDENTIFIED  

3. Approach sector................... FREE  

4. Lights (Landing / Strobe)...... ON

Merke: WRAL

1. Power ................................... 2000 RPM SET  

2. Oil pressure ......................... CHECKED / GREEN ARC  

3. Fuel pressure........................ CHECKED / GREEN ARC  

4. Alternator output .................. POSITIVE  

5. Annunciator warnings .......... CHECKED / OFF ex pitot heat  

6. Magnetos L/R....................... DROP ___ RPM (MAX 175), DIFFERENCE ___ RPM (MAX 50)

7. Carburetor heat .................... FUNCTION CHECKED  

8. Mixture ................................. FUNCTION CHECKED  

9. Throttle idle .......................... BETWEEN 500 AND 700 RPM  

10. Power ................................. 1000 RPM SET 

1. Power ................................... 1000 RPM SET  

2. Parking brake ....................... SET  

3. Taxi (Landing) light................ OFF

1. Brakes ................................. CHECKED  

2. Attitude indicator.................. ERECTED / STABLE  

3. Slip indicator ........................ L/R TURN: BALL MOVES  

4. Heading indicator................. L/R TURN: DEC-/INCREASIN

1. Taxi (Landing) light................ ON  

2. Power ................................... IDLE  

3. Parking brake ....................... RELEASED 

1. Block Off Time....................... TABULATED

2. Heading indicator.................. HDG BUG SET TO ACT RWY ___  

3. Taxi area ............................... FREE

Merke: BH

1. Fuel pump ............................ ON  

2. Mixture ................................. RICH  

3. Prime .................................... according PRIMING TABLE  

4. Throttle ................................. 0.5 CM OPEN  

5. Starter................................... ENGAGE  (max. 10'')

6. Power ................................... 1000 RPM SET  

7. Oil pressure .......................... OBSERVE  

8. Fuel pump ............................ OFF, PRESSURE CHECKED

Starter nicht länger als 10“ betätigen. 
Wartezeit zwischen Startversuch = 1min