Service difficulty report · Steering Sys · Cndair CL6002B19

Difficulty date
December 24, 2010
Submitted
December 29, 2010
Operation
Air carrier
Aircraft
N970EV
Make and model
Cndair CL6002B19
Aircraft serial
7527
Aircraft time
21,103 hours, 18,693 cycles
Engine
Ge CF34*
Part
Steering Sys
Condition
Out Of Adjust
Location
Nlg
Stage of operation
CL
How discovered
O
Nature of condition
J
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

AFTER T/O, MLG DISAGREE MESSAGE ILLUMINATED WITH LT & RT MLG SHOWING UP & WHITE, NLG INDICATING RED HASH MARKED BOX. ACFT RETURNED TO DEPARTURE. EMERGENCY DECLARED. C/W FUNCTIONAL TEST OF NOSE WHEEL STEERING SYS IAW AMM 32-51-00. REMOVED NLG SHOCK STRUT ASSY, INSTALLED NLG SHOCK STRUT ASSY. INSTALLED NLG LT TRUNNION PIN, & INSTALLED NLG RT TRUNNION PIN IAW AMM 32-21-01. INSTALLED NLG SWIVEL ASSY TO GREASE INSERT & ELECTRO HYD MODULE, RECONNECTED NLG BOTTOM DRAG BRACE TO NLG SHOCK STRUT, RECONNECTED NLG EXTENSION/RETRACTION ACTUATOR ON NLG SHOCK STRUT. ATTACHED DISCONNECTED NLG CONTROL ROD TO NLG SHOCK STRUT. CONNECTED NLG ELECTRICAL CONNECTOR P62, P4GC, P63 & ALL RELECTED ELECTRICAL CONNECTORS ALL IAW AMM 32-21-01 . LUBRICATE NLG IAW AMM 12-20-32-640-801. PRESSURIZED SHOCK STRUT WITH NITROGEN IAW AMM 12-12-32. BLEED HYD SYS NR 3 IAW AMM 29-10-00. C/W FUNCTIONAL TEST OF THE EXTENSION & RETRACTION SYS REQUIRE IAW AMM 32-30-00. C/W FUNCTIONAL TEST OF NOSEWHEEL STEERING SYS REQUIRE IAW AMM 32-51-00 / RII C/W IAW GMM 3-3 FOR INSTALLATION RIGGING. OPS CHECKS NLG SHOCK STRUT ASSY.