๐Ÿ›ฉ๏ธ

L-410NG โ€” Test Flight Checklist

เธ•เธฒเธก AFM Section 4: Normal Procedures โ€” Do-L410NG-1210.2 (EASA Approved)
๐Ÿ“‹ DOC-REF: AFM 4-Series
โœˆ๏ธ Aircraft: L-410NG
โš™๏ธ Engine: GE H85-100
๐Ÿ”„ Prop: AV-805A-317
๐Ÿ–ฅ๏ธ G3000 Integrated
๐Ÿ“Š
เธ„เธงเธฒเธกเธ„เธทเธšเธซเธ™เน‰เธฒ / Progress
0 / 85 items
1
๐Ÿ›ซ PRE-FLIGHT EXTERNAL INSPECTION(AFM 4-2)
โ–ฒ
โœ“ Item Check
Nose Cover Locks
Front Fuselage
CLOSED
Skin, Lights Glazing NO DAMAGE
Rotary Ice Detector NO DAMAGE
Pitot Static Probes
RIGHT + LEFT PITOT
COVER REMOVED
NO BLOCKAGE
Windshield Wipers NO DAMAGE
Emergency Exit CLOSED & LOCKED
Tire Condition (Nose) NO DAMAGE / DEFORMATION
PROPER INFLATION
Servo Control Tie Rods (Nose) NO DAMAGE
Engine Cowling LH/RH
Check for damage, leaks, security
SECURE, NO LEAKS
Propeller LH/RH
Blades, hub, pitch mechanism
NO DAMAGE
CLEAR OF FOREIGN OBJECTS
Main Gear LH/RH Tire NO DAMAGE
PROPER INFLATION
Brake Condition (LH + RH) NO OVERHEATING
SECURE
Wing Leading Edge
No ice/snow/frost contamination
CLEAN
COLD SOAKED FUEL CHECK
Flap Condition SECURE, NO DAMAGE
Fuel Vent CLEAR
Tail Section (V/STAB) NO DAMAGE
Antennas SECURE, NO DAMAGE
2
๐Ÿ–ฅ๏ธ COCKPIT PRE-FLIGHT(AFM 4-5)
โ–ผ
โœ“ Item Check
Flight Controls
Aileron, Elevator, Rudder + Trim
MOVE FREELY TO
EXTREME POSITIONS
Oxygen Bottle Pressure CHECK
Oxygen Mask + Connector CHECK
Oxygen Selector VERIFY FREE MOVEMENT
NORMAL + 100%
Emergency Pressure Selector ROTATE TO ON
LISTEN FOR FLOW โ†’ OFF
Flight Director Controls CHECK
EFIS Control Panel SET
Avionic Switches
As required
SET
Lighting
INSTRUMENT / EXT
SET
3
๐Ÿ‘จโ€โœˆ๏ธ COPILOT COCKPIT PRE-FLIGHT(AFM 4-5)
โ–ผ
โœ“ Item Check
BATTERY I, II Switches AS REQUIRED
Clock SET UP, TIME
Landing Gear Lever Lock REMOVE AND STORE
IN STOWAGE POCKET
CVR Test
Depress for 5 sec
GREEN LED does not
illuminate = FAULT
Fuel Quantity
L.H. + R.H.
___ kg (lb)
BATTERY, EXT POWER VOLTAGE IN GREEN BAND
COM I (LEFT) CHECKED
Flight Data Recorder CHECKED
4
โš™๏ธ BEFORE ENGINE STARTING(AFM 4-10)
โ–ผ
โœ“ Item Check
BEFORE START Test
G3000 Touch Screen โ†’ Aircraft Systems
ALL โ†’ GREEN PASS
FIRE DETECTION Test CHECK PASS
Voice alerts verified
SMOKE FRONT BAG Test CHECK PASS
SMOKE REAR BAG Test CHECK PASS
(Rear bag installed)
LH / RH FIRE EXT Minimum Oil Level Test CHECK PASS
Passenger Cabin Lights CONDITION CHECK
Emergency Exit Door LOCKED + SEALED
Pilot Seats SET TO REQUIRED POSITION
Seat Belts SECURE
5
๐Ÿ”„ ENGINE STARTING(AFM 4-11)
โ–ผ
โœ“ Item Check
Battery Switches BAT I + BAT II ON
PROPELLER lever LH/RH FEATHER position
THROTTLE lever LH/RH IDLE
Condition Levers CUTOFF
IGNITION Switch LH/RH IGN L (start), then GND
STARTER Engage Observe N1, EGT rise
Engine Parameters
N1, EGT, Np, FF
NORMAL RISE
NO WARNING
PROPELLER Governor Beta mode โ†’ check
6
๐Ÿš BEFORE TAXI(AFM 4-12)
โ–ผ
โœ“ Item Check
BRIEFING
Route, weather, performance, EMER
COMPLETE
FMS / GPS Programming SET
ALTIMETER Settings (PFD) SET QNH
FLIGHT INSTRUMENTS NORMAL
BRAKE Test PRESSURE OK
7
๐Ÿ”ฌ ENGINE RUN-UP(AFM 4-14)
โ–ผ
โœ“ Item Value
MP ( manifold pressure) 1800 RPM / 38" MP
1800 psi min cylinder
EGT (Exhaust Gas Temp) Monitor within limits
Magneto Check DROP < 150 RPM
Carb Heat APPLY โ†’ RPM DROP
RETURN โ†’ RPM RESTORE
Propeller Governor Test RPM STABLE
Autofeather Test
If equipped
TESTED
ARM circuit verified
HYDRAULIC Pressure 3000 psi
8
๐Ÿš€ BEFORE TAKEOFF(AFM 4-15)
โ–ผ
โœ“ Item Value / Standard Status
Flight Controls
Aileron, Elevator, Rudder
Full deflection โ€” no binding
Trim Takeoff setting
FLAPS 15ยฐ (or per AFM)
Landing Lights ON
Strobe Lights ON
Pitot Heat ON
Pressurization Leak check (if equipped)
AUTO FEATHER Switch ARMED
Ground Spoilers / Auto Bank OFF (then ARM before TO)
Weight & Balance Within limits
9
โœˆ๏ธ IN-FLIGHT TEST(GE H85-100 + G3000)
โ–ผ
โœ“ System / Test Procedure Standard
CLIMB POWER MP, RPM, EGT, Fuel Flow monitoring Per AFM climb spec
CRUISE POWER 1800 RPM, 38" MP Per AFM cruise
PROPELLER FEATHERING Test feathering on ground (if safe) Feathers smoothly
AUTO FEATHER Test in flight if possible Activates correctly
LANDING GEAR Extend/Retract cycle Normal indication
FLAPS 15ยฐ โ†’ 30ยฐ โ†’ 45ยฐ Check all positions Airspeed within limits
G3000 PFD / MFD All displays normal No red flags
AUTOPILOT Engage, track, disconnect Functions correctly
VHF COM / NAV Tx/Rx test, VOR, DME Signal normal
TRANSPONDER Mode C Responds correctly
ELECTRICAL Both ALTs, battery Normal readings
DE-ICE (Boots + Windshield) Activation check System operates
ABC System Auto-Bank test Activates/retracts OK
10
๐Ÿ›ฌ LANDING & POST-FLIGHT(AFM 4-25)
โ–ผ
โœ“ Item Check
BRAKE Test Normal braking on touchdown
REVERSE (if equipped) Thrust reverser operation
Engine Cool-down Allow idle cool before shutdown
PROPELLER BRAKE Apply per AFM
POST-FLIGHT INSPECTION Exterior walk-around
TECHNICAL LOG Snag entry if any
11
โš ๏ธ EMERGENCY PROCEDURES QUICK REF(AFM Section 3)
โ–ผ
โœ“ Emergency Key Actions
Engine Fire on Ground Condition โ†’ CUTOFF | Fire Ext โ†’ LH/RH | Evacuate
Engine Failure After TO Land immediately | AUTO FEATHER activates | ABC deactivates
Engine Fire in Flight Condition โ†’ CUTOFF | Fire Ext | May need runway
Smoke / Fire in Cabin Vents โ†’ closed | Smoke hood | Fire extinguisher
Electrical Fire GEN off | Battery off | Fire extinguisher
Pressurization Failure Oxygen masks | Descend 10,000ft | Land ASAP
Landing Gear Failure Gear up or partial | Belly landing procedures
๐Ÿ“ Flight Crew Signatures
PIC Name & Signature
Co-Pilot Name & Signature
Date / Aircraft Reg