Automatic Braking System (ABS) (Stabilized: Jul 2012)
€68.00
Aircraft Lightning Environment and Related Test Waveforms
€158.00
Recommended Wheel Tie Bolt Preload Procedure
Photometric Data Acquisition Procedures for Impact Test (Stabilized: Nov 2011)
€94.00
Deicing Facility Operational Procedures
€149.00
Use of HVOF Thermal Spray Coatings for Hard Chrome Replacement in Landing Gear Applications
€77.00
Aerial Refueling Lights - Design Criteria
€97.00
Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, SOLID SHANK, SELF-ALIGNING, AIRFRAME, TYPE I, -65 TO 300 °F
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, EXTERNAL THREAD, SELF-ALIGNING, AIRFRAME, TYPE II, -65 TO 300 °F
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, HOLLOW SHANK, SELF-ALIGNING, AIRFRAME, TYPE III, -65 TO 300 °F
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, INTERNAL THREAD, SELF-ALIGNING, AIRFRAME, TYPE IV, -65 TO 300 °F
BEARING, BALL, AIRFRAME, ANTI-FRICTION, HEAVY DUTY
BEARING, BALL, AIRFRAME, ANTI-FRICTION, INTERMEDIATE DUTY, CORROSION RESISTANT NITROGEN STEEL (CREN)
BEARING, BALL, AIRFRAME, ANTI-FRICTION, SELF-ALIGNING, DOUBLE ROW, HEAVY DUTY
