Jeff's C208B Wheel Aligment

Step 1 - Precheck

Aircraft Regristration

Date

Empty Weightlbs

Fuel Weightlbs

Total Weightlbs

Step 2 - For Each Gear:

1 - Remove Axle and Shims

2 - Clean Axle and Shims

3 - Install ONLY Axle with NO Shims

4 - Ensure No shim are installed

Step 3 - Prep

1 - Regrease, grease plates if necessary

Step1 - Enter Camber

LH° RH°

Step2 - Enter Toe (mm)

X X

Y Y

Z Z

LH ReadingsRH Readings

Camber Camber

Toe Toe

Correction LHCorrection RH

Camber Camber

Toe Toe

Limits

Camber View(+1.0 or -1.0)

Toe0° (+0 or -0.53)

Select LH Shim

Select RH Shim

Step1 - Enter Camber

LH° RH°

Step2 - Enter Toe (mm)

X X

Y Y

Z Z

Limits

Camber View(+1.0 or -1.0)

Toe0° (+0 or -0.53)

LH ReadingsRH Readings

Camber Camber

Toe Toe

Error LHError RH

Error Camber Error Camber

Error Toe Error Toe

Error Toe inch Error Toe inch

Wheel Alignment

Aircraft:

Date:

Precheck

Emty Weight:

fuel Weight:

Total Weight:

Run1 - Mesurements

LH Camber:RH Camber:

LH Toe:RH Toe:

Suggestion - Move Wheel

LH Camber:RH Camber:

LH Toe:RH Toe:

Shim Installed

Limits

Camber:

Toe:0° (+0° or -0.53°)

Toe inch:0" (+0" or -0.1")

Outcome

LH Camber:RH Camber:

LH Camber error:RH Camber error:

LH Toe:RH Toe:

LH Toe inch:RH Toe inch:

Corrective Action

Wheel was aligned using the following shim: LH( ) and RH( ). This resulted with the following measurement: LH(camber: , Toe: ) and RH(camber: , Toe: ). All was done IAW C208b MM chapter 32-10-00 - MAIN LANDING GEAR - ADJUSTMENT/TEST para #2 and #3.

Shim12641009-1

Shim22641009-2

Shim32641009-3

Bolt LongNAS1309-56

Bolt ShortNAS1309-40

NutMS21044N9

Spacer Thick2641021-1

Spacer mid2641021-2

Spacer Thin2641021-3

Washer ThickNAS1149F0963P

Washer ThinNAS1149F0932P

Save Work

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