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TUL: 5746 E Apache St. Tulsa, OK 74115
FXE: 2199 NW 53rd Street Fort Lauderdale, FL 33309

Part#: A1250860-157M

1250860-157M: NEW PMA CESSNA 206/207/210 TURBO MODIFIED LEFT FRONT STACK ASSEMBLY

Brand: Aerospace Welding Minneapolis

$1,887.97

In stock

In Stock

Overhaul is a process of returning a part to service using approved data to clean, inspect, and replace parts as required. This process may be performed by any qualified shop possessing the data and parts. The approved data may include the inspection and reuse of parts found within a given tolerance range.

Rebuilt is a process of returning a part to service using approved data to clean, inspect, and replace parts as required. This process is performed by the manufacturer and will replace parts with wear regardless of tolerance range. The unit is returned to new tolerances.

Customer property overhaul uses the same guidelines as an Overhaul with the customers property. It is a process of returning a part to service using approved data to clean, inspect, and replace parts as required. This process may be performed by any qualified shop possessing the data and parts. The approved data may include the inspection and reuse of parts found within a given tolerance range.

Factory Overhaul is a process of returning a part to service using approved data to clean, inspect, and replace parts as required. This process may be performed by any qualified shop possessing the data and parts. The approved data may include the inspection and reuse of parts found within a given tolerance range.

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Description

AMOC-WHEN INSTALLED, THE FOLLOWING AEROSPACE WELDING INC. PART NUMBER RELIEVE THE OWNER/OPERATOR OF AD 71-09-07 R1, PARAGRAPH (a) REPETITIVE 50 HOURS TIS PRESSURE TEST INSPECTION AND REPLACE IT WITH A REPETITIVE PRESSURE TEST INSPECTION REQUIREMENT OF 100 HOURS TIS OR AT ANNUAL INSPECTION WHICHEVER OCCURS FIRST.

AWI PART NUMBER A1250860-157M IS A FAA APPROVED PMA REPLACEMENT FOR CESSNA PART NUMBERS 1250860-157, 1250860-203 AND KNISLEY PART NUMBER K1250860m-203

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

With STC SA5010NM installed: TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G

With STC SA5012NM installed: T207, T207A, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N

This Left Front Stack Assembly is manufactured in a state of the art facility by a team of expert welders and fabricators, using the highest qualtiy 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: LEFT FRONT STACK ASSEMBLY

ATTACHMENT: 4 BOLT FLANGE WITH CADMIUM PLATED HARDWARE KIT

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 1250860-157 AND 1250860-203

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

AND FITS THESE CESSNA AIRCRAFT:

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

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