| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG ANGLE | 89.0 DEGREES MINIMUM AND 91.0 DEGREES MAXIMUM |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM |
| FIRST LEG HOLE DIAMETER | 0.295 INCHES MINIMUM AND 0.309 INCHES MAXIMUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5604 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | STEEL COMP 630 |
| MOUNTING HOLE TYPE | PLAIN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET, AFT-INNER DUCT |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.236 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | CUT OUT |
| SECOND LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM |
| SECOND LEG HOLE DIAMETER | 0.274 INCHES MINIMUM AND 0.288 INCHES MAXIMUM |
| SPECIAL FEATURES | 1ST LEG CONTAINS A NUT PLATE AND IS BENT DOWN 6.0 DEG MIN TO 8.0 DEG MAX; NEW INNER AFT DUCT BKT P/N 1864M70G01 (19EA) REPLACES P/N 5053M17G01 BUT NOT INTERCHANGABLE. THIS BKT IS 0.050 IN. SHORTER TO ACCOMMODATE THE THICKER COMBUSTION CASE MID FLANGE. IPB MUST BE CODED TO STATE 19 AFT INNER BRACKETS (P/N 1864M70G01, PPN 84214) ARE REQUIRED FOR 9550M17G15 CDN ASSEMBLY OTHERWISE AN INTERFERENCE PROBLEM WILL OCCUR IN THE FIELD PER GE AIRCRAFT ENGINES CHANGE IN DESIGN (CID) NUMBER 808627 |
| STYLE DESIGNATOR | OFFSET ANGLE |