- Registered owner
- Moody Bible Institute Of Chicago
- Location
- Spokane, WA
- Owner type
- Corporation
- Serial number
- U20606708
- Year built
- 1983
- Type
- Fixed wing single engine
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- April 4, 1983
- Certificate issued
- May 25, 1999
- Expires
- May 31, 2027
- Mode S code
- ADC401
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1974 | 1 |
| 1975 | 1 |
| 1977 | 2 |
| 1979 | 3 |
| 1985 | 3 |
| 1986 | 3 |
| 1987 | 1 |
| 1988 | 2 |
| 1990 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 2000 | 2 |
| 2002 | 1 |
| 2006 | 1 |
| 2009 | 1 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 2 |
| 2024 | 1 |
See all 31 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Cessna U206G
SAIB AIR-21-16FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt InspectionSAIB CE-12-41Flight Controls Loose Glide ScrewSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-39Leveling and Weighing: Maximum landing gross weight limitation for Cessna U206F, U206G, TU206F, TU206G series airplanes equipped with Flint Aero STC SA4366WESAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsSAIB CE-05-27R1StabilizersNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2024FA0000071Magneto · failed inspFOUND FACTORY DEFECT WHILE PERFORMING FIRST 500-HOUR INSPECTION MAGNETO WITH TT 477.6 IN ACCORDANCE WITH SERVICE SUPPORT MANUAL X42001. COIL TAB HAD NOT BEEN INSTALLED PARALLEL WITH HOUSING TO COVER MATING SURFACE, AS SPECIFIED IN 6-2.4 5.C. THIS HAD RESULTESDR 2017FA0000375Lifter · spalledTHIS ENG IS A FACTORY ENG WITH ONLY 192.7 HRS TT. OUR ACFT FLY ROUGHLY 400 HRS A YEAR. WE HAVE CHANGED OUR OIL TYPE SINCE THE LAST ENG CHANGE TO EXON ELITE 20W50 AND BEGAN USING CAMGAURD ADDITIVE TO PREVENT THIS DEFECT. MOODY AVIATION IN SPOKANE WA FLIES TWSDR 2017FA0000370Lifter · spalledLIFTERS WITH SEVERE SPALLING AND ONE CAM LOBE THAT WAS WORN OUT OF TOLERANCE DUE TO A VERY BAD LIFTER. THIS LIFTER IS FACTORY AND IS DEFECTIVE AT 192.7 HRS.SDR 2017FA0000369Lifter · spalledLIFTERS FOUND WITH SEVERE SPALLING AND ONE CAM LOBE THAT WAS WORN OUT OF TOLERANCE DUE TO A VERY BAD LIFTER. THIS LIFTERS IS FACTORY AND IS DEFECTIVE AT 192.7 HRS.SDR 2017FA0000366Lifter · spalledLIFTERS FOUND WITH SEVERE SPALLING AND ONE CAM LOBE THAT WAS WORN OUT OF TOLERANCE DUE TO A VERY BAD LIFTER. THIS LIFTER IS FACTORY AND IS DEFECTIVE AT 192.7 HRS.SDR 2017FA0000365Lifter · spalledLIFTERS WITH SEVERE SPALLING AND ONE CAM LOBE THAT WAS WORN OUT OF TOLERANCE DUE TO A VERY BAD LIFTER. THIS LIFTER IS FACTORY AND IS DEFECTIVE AT 192.7 HRS.SDR 2017FA0000337Lifter · spalledTHIS ENGINE IS A FACTORY ENGINE WITH ONLY 192.7 HOURS TT. OUR ACFT FLY ROUGHLY 400 HOURS A YEAR. WE HAVE CHANGED OUR OIL TYPE SINCE THE LAST ENGINE CHANGE TO 20W50 AND BEGAN USING ADDITIVE TO PREVENT THIS DEFECT. WE HAVE REPLACED SPALLED AND DEFECTIVE LIFTESDR 2017FA0000334Lifter · spalledTHE ENGINE IS A FACTORY ENGINE WITH ONLY 192.7 HOURS TT. OUR ACFT FLY ROUGHLY 400 HOURS A YEAR. WE HAVE CHANGED OUR OIL TYPE SINCE THE LAST ENGINE CHANGE TO 20W50, AND BEGAN USING ADDITIVE TO PREVENT THIS DEFECT. WE HAVE REPLACED SPALLED AND DEFECTIVE LIFTESDR 2011FA0000278Points · crackedACFT WAS DISCOVERED TO HAVE AN INOPERATIVE LT MAGNETO DURING A PILOT OPERATED ENG RUN. TROUBLESHOOTING FOUND THE FLAT SPRING PORTION OF THE CONTACT POINT ASSY HAD CRACKED THROUGH APPROX HALFWAY ALONG THE LENGTH OF THE SPRING AND ACROSS ITS ENTIRE WIDTH. THE
STCs that may be installed · 415
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna U206G
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller
Earlier aircraft with this N-number · 1
This aircraft carried N9861Z before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.