What was found
DENT ON LEFT SIDE FUSELAGE 29 INCH AFT OF FWD BULK HEAD 8 INCH BELOW STATIC AREA .047. MOVING TO DIAGRAM FOR DENT TYPE 1, BACK INTO AIRBUS SRM REQUIREMENTS CAPITAL D IS .100 AND LITTLE D IS 19 INCHES.MOVING WITHIN R4 OR R5 AS THAT SHOWS A 45 DEGREE ANGLE FROM THE CENTER OF 12.8" AND OUR DAMAGE IS 19" FROM THE CENTER OF THE STATIC 53-11-11-283-012, THE AREA HAS BEEN IDENTIFIED AS AREA 2. TO FIGURE 4 IT IS DETERMINED THAT THE DAMAGE DOES NOT FALL OF THE STATIC PORT PROBE. WE ALSO SEE THAT R3 HAS A MAX DISTANCE PORT PROBE. REQUEST DIP. AERODYNAMIC REQUIREMENTS FOR ALLOWABLE DAMAGE AND DENTS, DIMENSION A IS 1.0" AS PER SRM 53-00-11-283-005 FIGURE 001 SHEET 53-00-11-283-004, 2. PROCEDURE (3) AERODYNAMIC 01. REQUEST DIP APPROVED DIP PER SRM TASK 53-11-11-283-012 FIGURE 7 FOR DENT TOMC-APPROVAL FROM SC1ELBYC COMMENT LOCATED AT LH FRAME 3 AREA APPROXIMATELY 8 INCHES BELOW STATIC PORT AREA. DENT DIMENSION A=1", D=.1", X=3.8", AND Y=3.1". DENT NOT IN RIVETED OR STIFFENED AREA AND MEETS THE AERODYNAMIC REQUIREMENTS FOR RVSM. TYPE 1 DENT IN ZONE 1, AREA 2, CATEGORY C, REQUIRES PERMANENT REPAIR WITHIN 5000FC OR 10000FH FROM NOW. DIP 53-DIP PLEASE UPDATE TEXT WITH DENT LOCATION IN RELATION TO FRAME AND STRINGER NUMBER. INCLUDE THE EXACT MEASUREMENTS OF DENT REF SRM 53-11-11-283-012 FIGURE 1 SHEET 1 (A,D,X, AND Y DIMENSIONS) MAKE NOTE IF DENT IS IN RIVETED OR STIFFENED AREA. PHOTO ADDED PREVIOUS PHOTO INCORRECT, ATTACHE 2 PHOTOS ARE CORRECT OF DENT FOUND DENT TO BE WITHIN ALLOWABLE LIMITS