84-09-01: Window Emergency Egress Provision

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.