CESSNA 421A / 421B Golden Eagle Exhaust System Itemized Parts List
Item | Part # | Description | Condition |
---|---|---|---|
01 | 5155156-213 | STACK – RH – INBOARD | OVERHAUL |
02 | 5155156-22 | RISER – RH – FWD – INBOARD | OVERHAUL |
03 | 5155156-23 | RISER – RH – CENTER – INBOARD | OVERHAUL |
04 | 5155156-24 | RISER – RH – REAR – INBOARD | OVERHAUL |
05 | 9910379-16 | CROSSOVER – RH – 5 BOLT | OVERHAUL |
05 | 996-46 | CROSSOVER – RH – 3 BOLT | OVERHAUL |
06 | 9910379-18 | ELBOW – RH – 5 BOLT | OVERHAUL |
06 | 996-52 | ELBOW – RH – 3 BOLT | OVERHAUL |
07 | 5155156-207 | STACK ASSY – RH – OUTBOARD | OVERHAUL |
08 | 5155156-19 | RISER – RH – FWD – OUTBOARD | OVERHAUL |
09 | 5155156-18 | RISER – RH – CENTER – OUTBOARD | OVERHAUL |
10 | 5155156-17 | RISER – RH – REAR – OUTBOARD | OVERHAUL |
11 | 9910314-1 | SLIP JOINT | OVERHAUL |
12 | 9910379-20 | TURBO INLET – RH | OVERHAUL |
13 | A5155156-48 | TAILPIPE – RH | NEW PMA |
14 | A5155156-49 | BYPASS | NEW PMA |
15 | A5155157-4 | SLEEVE | NEW PMA |
16 | 5155156-205 | STACK ASSY – LH – INBOARD | OVERHAUL |
17 | 5155156-12 | RISER – LH – REAR – INBOARD | OVERHAUL |
18 | 5155156-13 | RISER – LH – CENTER – INBOARD | OVERHAUL |
19 | 5155156-14 | RISER – LH – FWD – INBOARD | OVERHAUL |
20 | 966-54 | ELBOW – LH – 3 BOLT | OVERHAUL |
20 | 9910379-17 | ELBOW – LH – 5 BOLT | OVERHAUL |
21 | 966-50 | CROSSOVER – LH – 3 BOLT | OVERHAUL |
21 | 9910379-15 | CROSSOVER – LH – 5 BOLT | OVERHAUL |
22 | 5155156-204 | STACK ASSY – LH – OUTBOARD | OVERHAUL |
23 | 5155156-9 | RISER – LH – FWD – OUTBOARD | OVERHAUL |
24 | 5155156-8 | RISER – LH – CENTER – OUTBOARD | OVERHAUL |
25 | 5155156-7 | RISER – LH – REAR – OUTBOARD | OVERHAUL |
26 | 9910379-19 | TURBO INLET – LH | OVERHAUL |
27 | A5155156-47 | TAILIPIPE – LH | NEW PMA |
N/S | 628260 | CYLINDER GASKET WITH HARDWARE | NEW |
Details
Subject to AD 2000-01-16
AWI is authorized by the FAA to meet the overhaul requirements (paragraph “G”) on AD 2000-01-16.
Visual inspection every 50 hrs or 30 days
Remove tailpipes inspect for cracks every 12 months
Inspect & pressure test exhaust system every 12 months
Replace multi-segment V-band clamps every 500 hours
Remove the exhaust system from the slipjoints aft to all turbo charger components every 2,500 hours or 12 years which ever occurs first.
CONTINENTAL GTSIO-520-D 375 H.P.
Check all Slip Joints for Freedom of movement
Check all parts for internal pitting