CSP-HE/HS-1
ROTORCRAFT FLIGHT MANUAL
MD 500
(Models 369HE/HS/HM)
Revision 6
F-ix
SUMMARY OF REVISIONS
TO THE ROTORCRAFT FLIGHT MANUAL
NOTE:
Revisions are listed below by number with appropriate remarks.
Section II pages marked [C]* indicate FAA approved color pages.
Black-and-white reproductions of color pages are not considered to be “FAA
Approved”.
REVISION
NUMBER
REMARKS
Revision 6
Section I: Removed company logo from all pages and replaced refer−
ences to McDonnell Douglas with MDHI.
Section II: Figure 2−5. Corrected error in oil pressure range on
4−pack instrument cluster.
Paragraph 2−11. Updated fuel specification designations and added
alternate fuels.
Section III: Removed company logo from all pages.
Paragraph 3−9. Added malfunctions procedures for low engine oil
pressure and loss of torque indication.
Section IV: Paragraph 4−1. Added check for torque stripe paint across
tail rotor retainer nut, tang washer, and fork assembly.
Paragraph 4−3. Corrected starter time limit note.
Section VI: Removed company logo from all pages.
Section VII: Removed company logo from all pages. Updated Table
7−1.
Section VIII: Removed company logo from all pages.
Section IX: Table 9−1 and Table 9−2. Added part number for cargo
hook kit.
Removed company logo from all pages.
Paragraph 9−5. Corrected maximum load combination gross weight.
