Technical data

13773-001
57-30
Page 2 30 Nov 2000
(b) Solvent clean the access panel and opening.
CAUTION: Parting agent (Frekote or silicone-free automotive wax) must be applied to
the access panel mating surfaces. This will assure easier access panel
removal in the future.
(c) Apply parting agent (Frekote or silicone-free automotive wax) to the access panel mating
surface.
(d) Faying surface seal fuel tank access panel. (Refer to 20-10)
(e) Position fuel tank access panel to wing.
(f) Install screws securing access panel to wing.
(g) After sealant has cured, fill fuel tank. (Refer to 12-10)
(h) Inspect fuel system for any signs of leakage. Repair as needed.
(i) Connect battery. (Refer to 24-30)
(j) Remove airplane ground from exhaust outlet.
(3) Removal - Wing Panels
(a) Determine access panel(s) to be removed. (Refer to 6-00)
(b) Remove screws securing access panel to wing.
(c) Remove access panel.
(4) Installation - Wing Panels
(a) Determine access panel(s) to be installed. (Refer to 6-00)
(b) Position access panel to wing.
(c) Install screws securing access panel to wing.
B. Wing Skin
The wing is manufactured from composite laminate materials. Refer to Chapter 51 for composite repair
procedures.
Extrusion Gun Seal-
ant
MIL-S-8802 Type 2
Class B*
CS3204 C1.B
GC408B
P/S 890B
PR1440B
EC1675B
AC-240B
Chem Seal - Flame
Master
Goal
PRC Aerospace
Sealants
PRC Aerospace
Sealants
3M
Dynamold Aerospace
Fillet, faying surface,
and injection seal in
fuel tanks. Install and
seal windows. Seal
fuel system enclo-
sure in cabin.
* When ordering MIL-S-8802 sealants make sure that an appropriate work life is specified. Work life
is specified by adding the desired work life in the product dash number after the Class designa-
tion, e.g. A-1/2, A-2, B-1/2, B-2, etc.
Approved Sealants
Item P/N or Spec. Supplier Application