- Registered owner
- Colorado Jet Solutions Inc
- Location
- Conifer, CO
- Owner type
- Corporation
- Serial number
- TC-633
- Year built
- 1964
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 17, 1964
- Certificate issued
- May 14, 2014
- Expires
- May 31, 2027
- Mode S code
- A030D1
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental I0-470 model are included below.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 2 |
|---|---|
| 1972 | 3 |
| 1973 | 3 |
| 1974 | 5 |
| 1975 | 1 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 1 |
| 1981 | 1 |
| 1984 | 1 |
| 1985 | 1 |
| 1988 | 2 |
| 1989 | 1 |
| 1990 | 1 |
| 1991 | 3 |
| 1993 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 4 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 3 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 1 |
| 2022 | 3 |
| 2023 | 5 |
Airframe · Beech 95-B55 (T42A)
AD 2023-10-02Indicating/Recording System, NavigationAD 2022-03-15Fuel Quantity IndicatorAD 2009-25-01Shoulder harnessessInformation bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Beech 95-B55 (T42A)
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-13-22Electrical Power System Circuit Breaker SwitchSAIB CE-12-36Flight Controls: AileronSAIB CE-11-28Airplane Fuel and Electrical Systems on Hawker Beechcraft Corporation Twin Engine Airplanes.SAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-07-18Elevator and rudder control surface hinge halvesEngine · Continental I0-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N111KFMatched 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 Beech 95-B55 (T42A) aircraft
FAA incident reports
No FAA accident or incident reports matched to N111KFMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech 95-B55 (T42A) aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR R2J2002F00001Floor Support · corrodedAT ANNUAL INSPECTION AFTER FINDING CRACKS IN AREA OF DOOR STEP, THE BAGGAGE FLOOR WAS COMPLETELY REMOVED. FOUND INSULATION ON UNDERSIDE OF FLOOR BOARD, HAD RETAINED SOME MOISTURE, CAUSING UNDER FLOOR STRUCTURE TO CORRODE. AIRCRAFT IS 1964 MODEL. SUGGEST A SSDR 98ZZZX4256Citcuit Breaker · failedTECHNICIAN WAS CYCLING CIRCUIT BREAKERS DURING ANNUAL INSPECTION. TWO CIRCUIT BREAKERS WOULD NOT OPEN. A 1-AMP AND 3-AMP BREAKER POWERING AVIONICS AUDIO SYSTEM WERE REPLACED. AS A PRECAUTION TO PREVENT FIRE HAZARD FROM NOT TRIPPING, 1-AMP BREAKER DID DISENGSDR 98ZZZX81Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND CRACKING IN TAIL AT FS 271.92 BULKHEAD. REPAIRED PER BEECHCRAFT SI 990. AREA VERY HARD TO INSPECT. SI 990 ALSO HAS INSPECTION CRITERIA. CRACKING FOUND ON 3 AIRCRAFT AT THIS STATION WHILE C/W SI 990. SUBMITTER SUGGESTED BULL
STCs that may be installed · 453
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 95-B55 (T42A)
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