84-09-01 BEECH: Amendment 39-4847. Applies to Models and Serial Numbers of 33, 35, 36, 50, 55, 56, 58 (except 58P), 58TC, and 95 series airplanes listed below with seating capacity for more than five occupants.
MODELS
SERIAL NUMBERS
E33, F33, G33
CD-1119 through CD-1304
E33A, F33A
CE-180 through CE-918, CE-920 through CE-922, CE-924, CE-926 and CE-928
E33C, F33C
CJ-1 through CJ-155
35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35TC, V35A, V35A-TC, V35B and V35B-TC
D-1 through D-10347, D-10349 through D-10352, D-15001 and D-15002
36, A36
E-1 through E-1421, E-1423 through E-1550, E-1552 through E-1568, E-1570 through E-1580, E-1582 through E-1593
A36TC
EA-1 through EA-20, EA-22 through EA-27, EA-29 through EA-32
50
H-1 through H-11
B50, C50
CH-12 through CH-360
D50, D50A, D50B, D50C, D50E
DH-1 through DH-347
E50
EH-1 through EH-70
F50
FH-71 through FH-93, FH-95 and FH-96
G50
GH-94, GH-97 throughGH-119
H50
HH-120 through HH-149
J50
JH-150 through JH-176
95-55, 95-A55, 95-B55, 95-B55A
TC-1 through TC-349, TC-351 through TC-2339, TC-2341 through TC-2354
95-C55, 95-C55A, D55, D55A, E55, E55A
TC-350, TE-1 through TE-1151, TE-1153 throughTE-1180
95-B55B (T42A)
TF-1 through TF-70
56TC, A56TC
TG-2 through TG-94
58, 58A
TH-1 through TH-1026, TH-1028 through TH-1061, TH-1063 through TH-1066, TH-1068 through TH-1079
58TC, 58TCA
TK-1 through TK-106, TK-109
95, B95, B95A, D95A, E95
TD-2 through TD-721
Compliance: Required as indicated, unless already accomplished.
To assure adequate emergency egress provisions, within the next 100 hours time-in- service after the effective date of this AD, accomplish the following:
(a) Visually inspect the openable window installation located on the side opposite the entry door to determine:
(1) That Beech P/N 96-534051-61 or equivalent release pin has a red handle.
(2) That any curtain bars and/or curtains installed are attached to the openable window and not on the window frame so that they will not restrict egress in the event of an emergency.
(3) That the tab on the handle assembly does not catch on the back of the hooks on the window.
(b) If, as the result of the inspection required by Paragraph a), any deficiencies in the above mentioned requirements are noted, prior to further flight:
(1) Paint the handle of the existing release pin red.
(2) Either remove the curtains and curtain bars or modify the curtain installation by attaching the bars to the openable window.
(3) Trim tab on the back of the handle assembly as required so it doesn't catch on the back of the hooks on the window.
(c) Replace existing placard with either Beech placard P/N 58-530258-1 (screwed- on type) or 58-530258-3 (adhesive back) as required which reads as follows:
"EMERGENCY EXIT LIFT LATCH-PULL
PIN PUSH WINDOW OUT."
Locate placard below openable window on the molding.
(d) An equivalent means of compliance with this AD may be used if approved by the Manager, Aircraft Certification Office, Federal Aviation Administration, Room 238, Terminal Building 2299, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 269-7000.
This AD supersedes AD 76-04-07, Amendment 39-2525.
This amendment becomes effective on May 25, 1984.