206 Cargo Pod Installation Manual

using a jack, support the entire pack assembly firmly against fuselage. Be careful not to exert enough pressure to deform or spread edges of cargo pack. 5) Check centerline of pack assembly (7) with centerline marked on lower fuselage skin. Check position of existing holes locations on pod (5, Figure 1) in cargo pack with fuselage skin below the door sills. Holes should align with lower rivet line on both sides of aircraft. Adjust pack fore and aft so that holes fall between rivets as shown in Figure 1. 6) When pack assembly (7) is positioned correctly, drill thirty-one #10 (.193) holes through pack and fuselage, using hole locations scribed into the pack as a guide. CAUTION: Use a drill stop or some other device to assure that the drill does not go beyond the rivnut depth. 7) Remove pack assembly and enlarge #10 holes in fuselage to ¼” and cut slots as shown (use a Rivet key punching tool if available). Install Rivets (8), (10), and (11) in fuselage skin. 8) Apply seal (2) to cargo pack (7) holding in place with masking tape. If a sealer caulk is necessary, assure that it is non-corrosive to aluminum. 9) Attach pack assembly to fuselage using screws and washers (9). Use an ice pick to put holes in the seal for the fasteners. D. (Refer to Figure 3) Installation of Seals and Fairings 1) Cement seals (3) to inboard side of fairings (5) and (12) using contact cement. Cut- out area in seals should be centered in relation to rectangular openings in fairings, with split end of seal aft. 2) Split aft ends of fairings to match split ends of seals, place fairings over landing gear springs, and position so bead at top of fairing matches bead edge of cargo pack. Using holes in fairings as a guide, drill five #26 (.147) holes in each side of cargo pack. 3) Remove fairings and enlarge #26 holes in cargo pack to #12 (.189). Install Rivnuts (6) in cargo pack and reattach fairings, using screws (4). 4) Clean fairings (5 and 12) and prime with zinc chromate primer. ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 7 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 E. (Refer to Figure 4) Cowl Flap Modification (Models 206, P206, U206 and Stationair) (NOT APPLICABLE TO 206H AND T206H MODELS) 1) Disconnect cowl flap controls (4) and install links (7) and checknuts (9). Retain existing checknuts (6) on cowl flap control as shown. Cessna supplied links (#1213626-1) can be substituted for (7). 2) With cowl flap control in closed position, adjust cowl flaps (by turning links) until cowl flap is 1.05” open at aft end. Openings to be measured between centerline of cowl flap at projected aft edge to lower firewall. Tighten checknuts (6) and (9). 3) Position baffles (1, 2, 3 & 5) with forward end of flange resting on flange of existing baffles, aft end of baffle aligning with aft end of existing baffle, and lower corner of angular cutoff aligning with upper aft corner of existing baffle. Use Cessna part # 1213509-1, 2, 3, 4 for aircraft serial numbers through U20601604. Use Aerocet part #10-20010-R, L and Aerocet part #10-20012-R, L for aircraft serial numbers U20601605 and on. Cessna baffles #1213687-1, 2, 3, 4 may be substituted for the Aerocet baffle parts #10-20010 and #10-20012. 4) Using holes in baffles as a guide, drill twelve #10 (.193) holes in existing baffles. Deburr holes and secure new baffles to existing baffles with screws (11) and (10). Options to substitute with rivets as shown in (11). 5) Adjust clearance of cowl flap baffles. Clearance between baffles and edge of cutout in engine cowl should be 1/8” (.125). Adjust by hand, bending baffles. Check for clearance with engine drain tubes. 6) Check cowl flap travel. Cowl flaps should be 1.05” open when control is in “closed” position and approximately 6.00” open when control is in “open” position. F. (Refer to Figure 3) Cowl Flap Modification (Model TP206 & TU206) (NOT APPLICABLE TO 206H AND T206H MODELS) NOTE: Baffles (1, 2, 3 & 5) are not required on turbocharged aircraft 1) Disconnect cowl flap controls (4) and install links (7) and checknuts. Retain existing checknuts (6) on cowl flap control as shown. 2) With cowl flap control in closed position, adjust cowl flaps (by turning links) until cowl flap is 2.50” open at aft end. Tighten checknuts (6) and (9). 3) Check cowl flap travel. Cowl flaps should be 2.50” open when control is in “closed” position, and approximately 8.00” open when control is in “open” position. ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 8 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 G. Model T206H Airplane Exhaust Pipe Extension Installation 1) For Model T206H, also install exhaust pipe extension as follows: a) Using Aerocet Part #10-20021 or Cessna Part #1250999-1 Exhaust Extension as a template, drill four (4) Number 29 (0.136 inch diameter) holes in exhaust pipe. NOTE: Extension must be flush with the exhaust pipe. It may be necessary to grind off approximately 1.5 inches of bead on exhaust pipe or reshape exhaust pipe in order to provide tight fit. b) Attach extension using MS51861-34C Screws. ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 9 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 10 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 11 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 12 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 ISSUE DATE: PO Box 2119 PAGE 265 Shannon Lane 13 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2 PO Box 2119 ISSUE PAGE DATE: 265 Shannon Lane 14 of 14 6/07/1994 INCORPORATED Priest River ID 83856 FILE NO. REVISION DATE: TITLE: 206 Cargo Pod Installation Manual A-10014 3/10/2009 REVISION: 2