- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 402C0050
- Year built
- 1979
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 30, 1979
- Certificate issued
- August 25, 2021
- Expires
- August 31, 2028
- Mode S code
- A78083
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.
On this page
Airworthiness directives that may apply · 79
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 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 2 |
| 1975 | 1 |
| 1976 | 2 |
| 1977 | 1 |
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 2 |
| 1982 | 1 |
| 1984 | 1 |
| 1985 | 1 |
| 1987 | 2 |
| 1988 | 4 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 3 |
| 2004 | 1 |
| 2005 | 5 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 3 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 3 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 6 |
See all 95 ADs
Information bulletins that may apply · 24
Advisory, not mandatory.
See all 25 bulletins
NTSB investigations
No NTSB investigations matched to N5826CMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 402C aircraft
FAA incident reports · 16
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19910930052989INormal Cruise · Billings, MTLeft engine failure in flight. Continued to destination. Landed safely. Found camshaft had failed.Incident 19910710036109IForced/Precautionary Landing · Billings, MTSmoke from right engine on departure. Returned. Pilot reported engine had higher than normal fuel flow indication.Incident 19901220062199IForced/Precautionary Landing · Billings, MTCabin heater failed on climb. Returned. Landed safely.
See all 16 incident reportsService difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR KW7R2023011228002Clevis Bolt · wornDURING SCHEDULED INSPECTION OF RUDDER PEDAL TORQUE TUBE AND ATTACHING ARMS PER CESSNA INSPECTION OPERATION 73 USING SUPPLEMENTAL INSPECTION NUMBER 27-20-05 INSPECTION PROCEDURES: UPON REMOVAL OF THE RUDDER PEDAL ASSEMBLY, THE CLEVIS BOLTS (ITEM #90 IN IPC) SECSDR HYIA20190930001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK MEASURES APPROXIMATELY 2.00 INCHES IN LENGTH, AND BEGINS AT THE TOP INBOARD TURBO BRACKET MOUNTING HOLE ON THE AFT FACE OF THE BSDR HYIA20170510001Exhaust Valve · brokenPILOT REPORTED LEFT ENGINE RUNNING ROUGH IN CRUISE. MAINTENANCE INSPECTED AND FOUND THE NUMBER TWO CYLINDER EXHAUST VALVE BROKEN AND PUSHROD BENT. ENGINE HAS BEEN REMOVED FOR TEARDOWN ANALYSIS; FURTHER DETAIL WILL BE PROVIDED UPON RECEIPT OF TEARDOWN REPORT.SDR HYIA20160913143Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160913142Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160803048Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160802002Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20150320003Governor · defectivePILOT REPORTED LT PROPELLER SPEED ERRATIC & DIFFICULT TO CONTROL. PERFORMED A RUN UP & PROP RIGGING FOR FULL POWER, CLIMB POWER RPM CHECK. THE REPLACED & OPERATIONALLY CHECKED THE PROP GOVERNOR WITH NO FURTHER DEFECTS NOTED.SDR HYIA20150130001Escape Hatch · openPILOT REPORTED ON DESCENT CREW HATCH OPENED FWD SAFETY LATCH PREVENTED IT FROM OPENING COMPLETELY. VISUALLY INSPECTED CREW DOOR. CLEANED & LUBRICATED LOCKING MECHANISM. NO DEFECTS FOUND. OPERATIONS CHECKED GOOD.SDR HYIA20141124001Exhaust Valve · brokenWHILE IN CRUISE POWER, COULD FEEL AN ENG STARTING TO RUN ROUGH. UNTIL THE RT OIL PRESS & RT CYLINDER HEAD TEMPERATURE STARTED TO DROP HE WAS UNSURE WHICH SIDE. IT WAS APPROX 3 - 4MIN FROM WHEN HE FIRST FELT THE ROUGHNESS UNTIL THE RT ENG OIL PRESS & CYLINDERSDR HYIA02262014002Wire · damagedSMOKE FROM WIRES LEADING TO WINDSHIELD, WHERE CONNECTS TO CONTROL PEDESTAL.SDR HYIA08032013001Pump · faultyRT ENGINE POWER LOSS AND LOSS OF FUEL FLOW IN CRUISE POWER SETTING. PUMP FOUND FAULTY.SDR HYIA20140414010Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A
STCs that may be installed · 321
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 402C
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