A1250860-122M Turbo Inlet Modified

CESSNA PART NUMBERS 1250860-4, 1250860-105, AND 1250860-122 ARE REPLACED BY FAA APPROVED NEW PMA PART NUMBER A1250860-122M

FITS CESSNA MODELS:

TP206A, TP206B, TP206C, TP206D, TP206E S/N P206-0001 and P20600604 through P20600647, TU206, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G S/N 676 and U20603522 and on, T207, T207A, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, T210R

This Turbo Inlet Modified is manufactured in a state of the art facility by a team of expert welders and fabricators, using the highest quality aerospace grade 321 stainless steel providing reliable service and performance in high temperature exhaust systems conditions.

AIRCRAFT: CESSNA 206/207/210 TURBO /206/207/210 TURBO MODIFIED

PART CATEGORY: TURBO INLET MOFIDIED

MATERIAL: 321 STAINLESS STEEL

PART CONDITION: FAA APPROVED NEW PMA

AWI new, overhauled and repaired parts meet the FAA airworthiness requirements.

THIS AWI FAA APPROVED NEW PMA REPLACES CESSNA PART NUMBER 1250860-4, 1250860-105 AND 1250860-122

AIRWORTHINESS DIRECTIVE (AD) AD 71-09-07R1 STATES EVERY 50 HOURS INSPECT AND PRESSURE TEST HEAT EXCHANGER