CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
5
−
2
FAA Approved
Reissue 2
Revision 5
5
−
2.
NOISE CHARACTERISTICS
NOTE
:
No determination has been made by the Federal Aviation Administration that the
noise levels of this aircraft are or should be acceptable or unacceptable for
operation at, into, or out of, any airport.
The MD900 meets the FAR Part 36-J noise requirements at the certified maximum
gross weight of 6770 lb for level flight at 0.9 V
H
.
Table 5
−
1. FAA Noise Levels
MD900 NOISE CHARACTERISTICS
−
6770 lb (3071 kg)
ENGINE: PW 207E
Configuration:
Clean aircraft, doors
on, no external kits.
0.9 V
H
(SL at 25
°
C)
90 KTAS
81.49 dBA
The MD900 meets the FAR Part 36-J noise requirements at the certified maximum
gross weight of 6500 lb for level flight at 0.9 V
H
.
Table 5
−
2. FAA Noise Levels
MD900 NOISE CHARACTERISTICS
−
6500 lb (2948 kg)
ENGINE: PW 207E
Configuration:
Clean aircraft, doors
on, no external kits.
0.9 V
H
(SL at 25
°
C)
118 KTAS
81.2 dBA
Summary of Contents for MD900 Explorer
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