2-22 PREFLIGHT CHECK

COCKPIT AREA

  1. Open canopy
  2. Positive Control Check
  3. Assistant opens Spoilers, Check Linkages etc.
  4. Exchange Battery for Radio, Radio Set & On
  5. Close canopy

RIGHT WING

  1. Strut attach points
  2. Leading Edge
  3. Wing tip, wheel assy
  4. Aileron hinges, pins, push
  5. rods, movement
  6. Trailing edge
  7. Fuselage to tail area

TAIL ASSEMBLY

  1. Hinge points, rudder
  2. Hinge points, elevator
  3. Push rods to elevator horn
  4. Stabilizer struts
  5. Stabilizer attachment to fuselage
  6. Rudder cable connection to horn
  7. Tail wheel assembly
  8. Left side fuselage to wing

LEFT WING

  1. Trailing edge
  2. Aileron hinges, pins, push rods, movement
  3. Wingtip, wheel assembly
  4. Leading edge
  5. Strut fittings

FUSELAGE (COCKPIT AREA, LEFT SIDE)

  1. Canopy hinges, pins cable
  2. Skid plate condition
  3. Tire pressure
  4. Tow release
  5. Air vent
  6. Pitot/Static ports

FUSELAGE (Cockpit)

  1. Instruments set
  2. Belts, condition, Back seat belts secure (Solo)
  3. Canopy latch
  4. Dive brakes closed/locked
  5. Rear door and window
  6. Documents
  7. Wing Pins/Control Hookups

TOW ARRANGEMENTS

  1. Tow rope & rings
  2. Review signals
  3. Make sure tow pilot knows required speed

COCKPIT CHECK

ABBCCCDDE

Belts,Ballast,Controls

Canopy,Cable,Dive Brakes closed/locked

Direction of Wind, Emergency plans

LANDING (BEFORE REACHING IP)

TTAADD

Traffic, Trim, Altitude,Airspeed,

Direction of Wind, Dive Brakes

 

 

Weight & Balance N2747Z

Weight Arm Moment

Aircraft Empty Weight 551 x 97.3 = 53611.3

Front Seat _____ x 42.8 = ________

Rear Seat _____ x 74.7 = ________

Nose Weight 15 x -16.0 = -240

Totals ______ _________

 

 

____________ / _____________ = ____________

(total moment) (gross weight) (C.G.)

 

C.G. Range 78.2 to 86.1

Max gross weight 900lb