W DOC AIRBUS | AMM A320F

SPOP 167 - Application of PWA 36515 Primer [PW11]


TASK 70-28-00-910-805-A
SPOP 167 - Application of PWA 36515 Primer


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
GUN - HOT AIR
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P18-018)
primer, epoxy, corrosion inhibiting
(Material No.P18-025)
protective tape
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 70-27-00-910-804-A
SPOP 208 - Degreasing of Parts by Solvent Wiping
3. Job Set-up
Subtask 70-28-00-860-053-A ** ON A/C NOT FOR ALL
A. Not Applicable
4. Procedure
Subtask 70-28-00-910-053-A ** ON A/C NOT FOR ALL
A. Application of PWA 36515 Primer
   (1) Do the SPOP 208 procedure to clean the area where primer is specified (Ref. AMM TASK 70-27-00-910-804).
   (2) Mix the components of the P18-018primer, epoxy, corrosion inhibiting.
NOTE: protective tape (Material No.P18-025) may be used as an alternative when specified by repair.
     (a) Refer to the manufacturer's instructions for the procedure to mix the P18-018primer, epoxy, corrosion inhibiting.
     (b) The mixed P18-018primer, epoxy, corrosion inhibiting must have an equal consistency that is without bubbles, grit, floating pigments or caked pigments.
   (3) Apply the P18-018primer, epoxy, corrosion inhibiting to the surface.
   (4) Cure the P18-018primer, epoxy, corrosion inhibiting at a temperature between 65 deg.F (18 deg.C) and 85 deg.F (29 deg.C) for at least one hour.
   (5) Cure the P18-018primer, epoxy, corrosion inhibiting at a temperature between 145 deg.F (63 deg.C) and 155 deg.F (68 deg.C) with the GUN - HOT AIR for at least one hour.
[Rev.10 from 2021] 2026.04.01 02:20:35 UTC