- Registered owner
- Grant Aviation Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 20700431
- Year built
- 1978
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 27, 1978
- Certificate issued
- October 19, 2020
- Expires
- October 31, 2027
- Mode S code
- A9EBBA
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 62
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 1 |
| 1977 | 4 |
| 1979 | 4 |
| 1980 | 2 |
| 1981 | 2 |
| 1985 | 3 |
| 1986 | 1 |
| 1987 | 3 |
| 1988 | 5 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 2 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 6 |
See all 73 ADs
Information bulletins that may apply · 19
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC02LA066Accident · No injuriesLimited investigationFinal reportChevak, AKThe pilot's failure to attain the proper touchdown point resulting in an undershoot, and subsequent collision with gravel terrain.NTSB ANC02LA006Accident · No injuriesLimited investigationFinal reportKobuk, AKThe pilot's failure to maintain adequate clearance from objects during the initial climb after takeoff, and subsequent collision with a tree. A factor was the presence of trees along the runway.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20020630016859AChevak, AK(-23) On June 20, 2002, at about 1450 Alaska daylight time, a wheel equipped Cessna 207 airplane, N7384U, sustained substantial damage as a result of a landing accident at Chevak, Alaska. The airplane was operated by flight Alaska, inc. as a 14 CFR part 135…Accident 20011023031999AKobuk, AK(-23) Airman stated that he was ill and probably should not have flown on the day of the accident. He also said that he was practicing a short-field takeoff using 20 degrees of flaps. As soon as the aircraft lifted off, he lowered the nose in order to…
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EPUA20180302001Bushing · wornTHE ENGINE HAD EXPERIENCE FREQUENT ALTERNATOR BELT THROWING PROBLEMS. NO FIX WAS FOUND. THE DECISION WAS MADE TO HAVE THE ENGINE INSPECTED FOR DEFECTS. FOUND EXCESSIVELY WORN CRANKSHAFT COUNTERWEIGHT BUSHINGS. THIS IS BELIEVED TO BE THE REASON THE ALTERNATSDR EPUA20141107003Bladder · deterioratedDURING CRUISE ACFT ENG EXPERIENCED A LOSS OF ENG POWER, MISSING & STUTTERING. INSPECTED THE FUEL SYS & DETERMINED THAT THE RT FUEL BLADDER MATERIAL WAS DETERIORATING & CLOGGING THE FUEL FILTER SYS & STARVING THE ENG OF FUEL.SDR EPUA20140122001Feeder Cable · chafedDURING FLIGHT BURNING SMELL & SMOKE WAS NOTICED BY FLIGHT CREW IN THE FLIGHT COMPARTMENT. AS A PRECAUTIONARY MEASURE, THE MASTER SWITCH WAS TURNED OFF WHICH ALLEVIATED THE ACCUMULATION OF ADDITIONAL SMOKE & SMELLS. THE ACFT LANDED WITHOUT INCIDENT. PERSONNESDR EPUA20131030002Diode · failedBURNING ODOR IN CABIN DURING FLIGHT. MAINTENANCE DISCOVERED THAT DIODE THAT IS CONNECTED BETWEEN THE LANDING LIGHT AND TAXI LIGHT SWITCHES SHOWED SIGNS OF HEAT DAMAGE AND WAS VERY HOT TO THE TOUCH. REPLACEMENT OF THE DIODE REMEDIED THE PROBLEM.SDR EPUA20130212001Magneto · damagedENGINE VERY ROUGH WITH LOSS OF POWER, RT MAGNETO WAS REPLACED DUE TO INTERNAL DAMAGE.SDR 2005FA0001026Antenna · inoperativeFOUND LOWER UAT ANTENNA BAD DURING UAT UPGRADE. (AL05200502611) (K)SDR 2000ZZZX829Sprocket · mismanufacturedAFTER INSTALLATION OF PART, OPS CHECK FOUND TRIM CHAIN TO RIDE NORMALLY FOR TWO-THIRDS OF TURN ON SPACER BEFORE RIDING UPON TEETH OF SPROCKET AND JUMPING OFF. INSPECTED SPROCKET AND DETERMINED SOME OF THE TEETH MISS-CUT UPON MANUFACTURE.
STCs that may be installed · 343
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 207A
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