CL-126C CREW CHECKLIST & QUICK REFERENCE HANDBOOK Copyright © 2008 by Bombardier Aerospace All rights reserved. Printed in Canada. Subject: Learjet 45 Checklist (U.S. Units) — Change 2 The following summary describes the changes that are incorporated with this change. NORMAL PROCEDURES After Landing/Clearing Relocated “Standby Attitude Indicator — Cage”” step to Shut- Runway down procedure. Even though the gyro is caged, it is still func- tioning and normal taxiing procedures and tarmac irregularities may contribute to excess wear and tear on the unit. Shutdown Added step to cage the standby attitude indicator after the air- craft has been parked. PERFORMANCE DATA TAKEOFF Added shading and the statement that shaded areas are for interpolation only. This statement was erroneously left out on some tables. EMERGENCY PROCEDURES General Changes Updated Tab references. Miscellaneous formatting changes throughout section. No change to content. Cabin/Cockpit Fire, Revised step to use Clearance Delivery Radio to tune COM 1. Smoke or Funes LR GEN FAIL Deleted reference to the 38 amp-hr Ni-Cad battery, as the duration time of 1.0 hr is the same for Lead-Acid or Ni-Cad batteries. Revised step to clarify the conditions that will exist with emer- gency battery until main batteries have been depleted.. Loss of Both Genera- Deleted reference to using RMU 1 to tune COM 1 as RMU 1 is tors and Both Main not available if main battery is not on-line. Batteries Moved RMU 1 from operative to inoperative column. L REV UNSAFE R REV UNSAFE Clarified procedure by adding step to reduce speed to 160 UNL or DEP KIAS or below as required to maintain level flight. During Takeoff Above V1 Speed In flight Added the work “level” to clarify the procedure step. CL-126C Highlights-1 Change 2 ABNORMAL PROCEDURES General Changes Miscellaneous formatting changes throughout section. L CHK IC SW Added amber CAS messages to indicate that there is a mis- R CHK IC SW match between the loaded IC-600 software and the approved LR CHK IC SW configuration software ID file, or that the program enable dis- crete is active. These CAS messages will appear in ground mode, and are inhibited on takeoff. Landing Gear Free Fall Revised procedure to clarify action after GEAR FREEFALL lever step has been initiated. Normal Electrical Added footnotes to Operative/Inoperative Table to clarify what System Failure Land- instruments are operative with main batteries not depleted. ing Main Hydraulic Sys- Separated step “3a” into two separate steps to clarify the ver- tem Failure Landing biage to check that brake accumulator reservoir pressure is adequate before activating the HYD XFLOW switch for flap extension. ADVISORY/STATUS General Changes Miscellaneous formatting changes throughout section. No change to content. SUPPLEMENTAL DATA General Changes Miscellaneous formatting changes throughout section. No change to content. DC Power Distribution Deleted reference to 10 Amp-Hr as it is no longer available. (Dual Generator Regardless of which battery is installed, the duration is 1 hour. Failure) Master EICAS Index Updated Tab references. Added reference to L CHK IC SW, R CHK IC SW, and LR CHK IC SW CAS message. APU Amps High Changed to N/A as it indicates a normal system response for excessive electrical loads being placed on the APU generator. APU FAIL Revised NO GO or MEL RELIEF column to harmonize with DDG and MMEL. Highlights-2 CL-126C Change 2 LIST OF EFFECTIVE PAGES Use this List of Effective Pages to determine the current status of the Crew Checklist and Quick Reference Handbook. Pages affected by the current change are indicated by an asterisk (*) immediately preceding the page number. Dates of issue for original and changed pages are: Original ............................................ O ........................................April 1998 Reissue............................................ A .............................. December 1999 Reissue............................................ B .................................. October 2004 Reissue............................................ C .................................. October 2008 Change ............................................1 ....................................... June 2009 Change ............................................2 .....................................March 2010 Page Change Aircraft Affected/Effectivity Code Title ............................................... C All *LOEP-1 thru LOEP-7..................... 2 All *LOEP-8 (Added)............................ 2 All *LOR ............................................... 2 All *TCL-1 ............................................ 2 All i ..................................................... C All ii..................................................... 1 All iii and iv ......................................... C All Normal Procedures N-1 thru N-13................................. C All N-14 .............................................. 1 Aircraft 45-002 & on not modified by SB 45-11-4 N-14.1............................................ 1 Aircraft 45-002 & on modified by SB 45-11-4 N-15............................................... C All *N-16 thru N-18............................... 2 All N-19 and N-20............................... 1 All Performance Data *P-1................................................. 2 All *P-2................................................. 2 D P-2.1 ............................................. 1 E P-2.2.............................................. 1 F P-3................................................. 1 D P-3.1.............................................. 1 E P-3.2.............................................. 1 F P-4................................................. 1 D P-4.1.............................................. 1 E P-4.2.............................................. 1 F P-5................................................. 1 D P-5.1 ............................................. 1 E P-5.2.............................................. 1 F Denotes pages presented in either U.S. or metric units. CL-126C Change 2 LOEP-1 Change 2 Page Change Aircraft Affected/Effectivity Code P-6 ................................................. 1 D *P-6.1 .............................................. 2 E P-6.2 .............................................. 1 F *P-7 ................................................. 2 D *P-7.1 .............................................. 2 E P-7.2 .............................................. 1 F *P-8 ................................................. 2 D *P-8.1 .............................................. 2 E P-8.2 .............................................. 1 F *P-9 ................................................. 2 D *P-9.1 ............................................. 2 E *P-9.2 .............................................. 2 F *P-10 ............................................... 2 D *P-10.1 ............................................ 2 E P-10.2 ............................................ 1 F *P-11................................................ 2 D *P-11.1 ............................................ 2 E *P-11.2............................................. 2 F *P-12 ............................................... 2 D *P-12.1 ............................................ 2 E *P-12.2 ............................................ 2 F *P-13 ............................................... 2 D *P-13.1 ........................................... 2 E *P-13.2 ............................................ 2 F P-14 ............................................... 1 D P-14.1 ............................................ 1 E P-14.2 ............................................ 1 F P-15 ............................................... 1 D *P-15.1 ........................................... 2 E P-15.2 ............................................ 1 F *P-16 ............................................... 2 D *P-16.1 ............................................ 2 E P-16.2 ............................................ 1 F *P-17 ............................................... 2 D *P-17.1 ........................................... 2 E *P-17.2 ............................................ 2 F *P-18 ............................................... 2 D *P-18.1 ............................................ 2 E *P-18.2 ............................................ 2 F *P-19 ............................................... 2 D *P-19.1 ........................................... 2 E *P-19.2 ............................................ 2 F *P-20 ............................................... 2 D *P-20.1 ............................................ 2 E *P-20.2 ............................................ 2 F *P-21 ............................................... 2 D *P-21.1 ........................................... 2 E *P-21.2 ............................................ 2 F Denotes pages presented in either U.S. or metric units. CL-126C Change 2 LOEP-2 Page Change Aircraft Affected/Effectivity Code P-22............................................... 1 All P-23............................................... 1 D and E P-23.2............................................ 1 F P-24............................................... 1 D and E P-24.2............................................ 1 F P-25............................................... 1 D and E P-25.2............................................ 1 F P-26............................................... 1 D and E P-26.2...........................................