- Registered owner
- Vantage Air Corp
- Location
- Kalispell, MT
- Owner type
- Corporation
- Serial number
- 562
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 20, 2007
- Certificate issued
- January 30, 2026
- Expires
- January 31, 2033
- Mode S code
- A72E98
Dehavilland DHC-6-300TCDS A9EAAirframe · Dehavilland DHC-6-300Engine modelPratt & Whitney PT6A-27 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A-27 model are included below.
On this page
Airworthiness directives that may apply · 70
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 3 |
|---|---|
| 1968 | 1 |
| 1969 | 1 |
| 1971 | 3 |
| 1973 | 1 |
| 1974 | 3 |
| 1975 | 5 |
| 1976 | 2 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 5 |
| 1981 | 2 |
| 1982 | 1 |
| 1983 | 2 |
| 1987 | 2 |
| 1990 | 3 |
| 1992 | 1 |
| 1993 | 2 |
| 1994 | 3 |
| 1995 | 4 |
| 1996 | 1 |
| 1997 | 4 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2002 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2008 | 5 |
| 2009 | 1 |
| 2011 | 2 |
| 2014 | 1 |
| 2018 | 1 |
| 2019 | 1 |
| 2022 | 5 |
| 2023 | 1 |
Airframe · Dehavilland DHC-6-300
AD 2023-10-02Indicating/Recording System, NavigationAD 2022-11-12Engine ControlsAD 2022-11-09Wing StructureInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · Pratt & Whitney PT6A-27 series
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxNTSB investigations
No NTSB investigations matched to N562CPMatched 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 Dehavilland DHC-6-300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N562CPMatched 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 Dehavilland DHC-6-300 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR S9BA20110006Fire Detector · contaminatedRIGHT ENGINE FIRE LIGHT CAME ON DURING TAKEOFF. INSPECTED RT ENGINE, WHEN OPENING THE LOWER COWLING A LARGE AMOUNT OF WATER POURED OUT, INSPECTED FIRE DETECTORS AND ENGINE RUN NO DEFECTS NOTED IAW MM 26-00. AIRCRAFT WAS SUBJECT TO HEAVY RAIN ON PREVIOUS NIGHTSDR S9BA20110002Engine · seizedLEFT PROPELLER DOES NOT TURN, LOCKED, CAUSED BY HOT START. REMOVED LT ENGINE AND PROPELLER. INSTALLED LT ENGINE AND PROP ALL WORK ACCOMPLISHED IAW WORK CARD 72-00. ENGINE RUNS SAT NO LEAKS NOTED.SDR S9BA20100009Fire Loop · false activationLT FIRE BELL/ LIGHT ACTIVATED ON TAKEOFF. POWER WAS REDUCED AND INDICATION EXTINGUISHED. RETURNED TO BLOCKS. RAN LT ENGINE AT HIGH POWER SETTING FIRE WARNING ILLUMINATED. R & R BOTH 450C THERMAL FIRE SENSORS. GROUND TEST OK WORK PERFORMED IAW MM 26-10-00. OPSDR S9BA20090014Control Handle · odorUNUSUAL ODOR NOTED IN FLIGHT: RETURNED TO DEPARTURE AS A PRECAUTION. FOUND DME INDICATOR HEAD HOT AND SMELLED BURNED. REPLACED INDICATOR, OPS CHECK GOOD IAW INSTALL MANUAL.SDR S9BA2009002Adapter · corrodedRIGHT NACELLE ENGINE MOUNT ADAPTOR PLATE CORRODED. REMOVED AND REPLACED ENGINE MOUNT ADAPTOR PLATE IAW RD6-54-006.SDR S9BA2009001Adapter · corrodedLT NACELLE ENGINE MOUNT ADAPTOR PLATE CORRODED. REMOVED AND REPLACED ENGINE MOUNT ADAPTOR PLATE IAW RD6-54-006.SDR S9BA2008029Turbine · damagedRIGHT ENGINE MAKES NOISE WHEN PROP MOVED BY HAND. REMOVED AND REPLACED RIGHT ENGINE AND PROPELLER AS A QEC ASSEMBLY. SPLIT ENGINE AT C-FLANGE AND FOUND POWER TURBINE RUB.SDR S9BA2008028Counterweight · looseLEFT PROPELLER BLADE NR 3 COUNTER WEIGHT LOOSE. BOTH MOUNTING BOLTS WERE INSTALLED WITH LOCKING PINS. REMOVED AND REPLACED PROPELLER. SENDING PROPELLER TO REPAIR STATION FOR EVALUATION. INSPECTED ALL AIRCRAFT IN FLEET FOR LOOSE PROPELLER WEIGHTS. NONE FOUSDR S9BA2008025Bellcrank · wornDURING AD 89-24-06 FOUND ELEVATOR BELL CRANK WORN. REMOVED AND REPLACED ELEVATOR BELL CRANK. NO OTHER DEFECTS NOTED. (S)SDR S9BA2008024Blade · wornUNUSUAL NOISE NOTED IN COMPRESSOR SECTION (NR 2 ENG) UPON START UP. REMOVED ENGINE FROM SERVICE, ENGINE RETURNED TO ENGINE SHOP, FOUND 1ST STAGE BLADE RUB. ENGINE PENDING REPAIR. (K)SDR S9B2008F00001Compressor · noisyUNUSUAL NOISE NOTED IN COMPRESSOR SECTION NR 2 ENGINE, UPON START UP, REMOVED ENGINE FROM SERVICE WILL CLOSE SDR WHEN SOURCE OF NOISE IS FOUND AND CORRECTED. (K)SDR S9BA200800015Longeron · damagedDURING SCHEDULED 125HR INSPECTION FOUND: RT ENGINE NACELLE IB LONGERON DAMAGED FORWARD OF LEADING EDGE AT STATION 60.8. REMOVED AND REPLACED RT NACELLE IB LONGERON ASSY IAW AC 43-131B CHP7 EMERGENCY MEASURES EXECUTED: NO AIRCRAFT. GROUNDED: BEING REPAIRED DURSDR S9BA200700024Wire · shortedLT GENERATOR WOULD NOT COME ON-LINE AFTER START. FERRIED AC BACK TO BASE SSB. FOUND SHORTED WIRE ON GEN. FIELD RELAY DUE TO LACK OF HEAT SHRINK TUBING ON SOLDERED TERMINAL JOINT.
STCs that may be installed · 285
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 285 STCs