Suspension Geometry Data

ModelCamberCastorKPIWheel AlignmentCamberWheel Alignment
Spitfire Mk I & II2°POS6 3/4°1/16″-1/8″ T.I1/2°POS1/16″-1/8″ T.0
Spitfire Mk III3°POS3 1/2°5 3/4°1/16″-1/8″ T.I1/2°POS1/16″-1/8″ T.0
Spitfire Mk IV3°POS5 3/4°1/16″-1/8″ T.I1°neg1/32″-3/32″ T.0
GT.62 3/4°POS3 1/2°1/16″-1/8″ T.I1/16″-1/8″ T.0
GT.6 + and GT.6 Mk II2 3/4°POS3 1/2°1/16″-1/8″ T.I0+- 1/32″
GT.6 Mk III2 3/4° POS3 1/2°1/16″-1/8″ T.I0+- 1/32″
TR.42 1/2° POS2 3/4°6 1/2°0-1/16″ T.I
TR.4A1/2° POS2 3/4°8 1/2°1/16″-1/8″ T.I1/2°POS0-1/16″ T.I
TR.2501/2° POS2 3/4°8 1/2°1/16″-1/8″ T.I1/2°POS0-1/16″ T.I
TR.61/4° POS2 3/4°8 3/4°1/16″-1/8″ T.I1/2° POS0-1/16″ T.I
Stag1° POS10 1/2°1/16″-1/8″ T.I1 1/2°POS0-1/16″ T.I

NOTES: 
1. Maximum permissible difference between left and right hand castor and camber is 1 degree.
2. Subject to note 1, the maximum tolerance of camber, castor and KPI. angles is +- 1°.
3. The use of the Swivel Plates is essential, partially when checking Spitfire rear suspensions. Without the use of the plates, side thrust can cause a difference of approximately 15%.