Eclipse 550 - User Manual

CHAPTER - 31 HIGHLIGHTS
(Summary of Changes)
Revision No. TR31-3 Aug 19/19
TO: HOLDERS OF THE AIRCRAFT MAINTENANCE MANUAL (06-123838)
Pages that have been added or revised are summarized below. Remove and insert the affected
pages as listed, and enter the above revision number with issue date into the Record of Revisions
sheet.
This Temporary Revision incorporates and supersedes previously released temporary
revisions for the chapters listed below.
Do not remove this page. Keep it in place as a record of previous changes.
CH/SE/SU
Page Block No. Description of Change
31-40-00
PgBlk 501 Added FADEC Fault test with engine run.
Eclipse 550 Aircraft Maintenance Manual — 06-123838
Temporary Revision No. 31-3
31-HIGHLIGHTS
Page 1
Aug 19/19
© 2019 Eclipse Aerospace, Inc.

Summary

Temporary Revision 31-3 Highlights

Summary of Changes for TR31-3

Lists pages added or revised, including FADEC Fault test with engine run.

Aircraft Computer Systems Adjustment and Test Procedures

General Aircraft Computer System Information

Overview of Aircraft Computer System (ACS) and FADEC components.

Left APC Component Test Matrix

Introduces the component test matrix for the Left APC.

Equipment and Materials for Maintenance

Job Set-Up Procedures

Single Left ACS Test Procedure

Single Right ACS Test Procedure

GPS Operation Test

Job Close-Up Procedures

Eclipse 550 Specifications

General

Manufacturer	Eclipse Aerospace
Aircraft Type	Very Light Jet
Engines	2 × Pratt & Whitney Canada PW610F turbofans
Thrust per engine	900 lbf (4.0 kN)
Maximum Cruise Speed	375 knots
Range	1, 125 nautical miles
Service Ceiling	41, 000 feet
Seating Capacity	6
Height	11 feet
Rate of Climb	3, 424 feet per minute
Cabin Height	4 feet 2 inches
Max Takeoff Weight	6, 000 pounds