- Registered owner
- Fresh Air Aviation Inc
- Location
- Charlevoix, MI
- Owner type
- Corporation
- Serial number
- 282
- Year built
- 1983
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 25, 2005
- Certificate issued
- August 14, 2006
- Expires
- May 31, 2028
- Mode S code
- A48D97
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 4 |
|---|---|
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 2 |
| 1988 | 2 |
| 1989 | 1 |
| 1991 | 2 |
| 2002 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2014 | 1 |
| 2022 | 3 |
Airframe · Partenavia P.68C
AD 2022-20-10Rudder StructureAD 2022-03-15Fuel Quantity IndicatorAD 2021-26-15Stabilizer Control SystemInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Partenavia P.68C
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemNTSB investigations
No NTSB investigations matched to N3927UMatched 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 Partenavia P.68C aircraft
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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2023FA0000630Bolt · failedMAIN LANDING GEAR LEAF SPRING INNER ATTACH BOLT P/N NAS1106-24 ON LH SIDE OF AIRCRAFT, FAILED MID SHANK ABOVE THE THREADS, 50HR AFTER INSTALLED DURING REPETITIVE INSPECTION BROUGHT ON BY MANDATORY SERVICE BULLETIN-99. BOLT FAILURE CAUSED DEFORMATION OF THE FUSSDR 9FHA2014FA0000336Tube · splitLEFT MAIN TIRE WENT FLAT UPON TAXIING IN FROM LANDING. TIRE AND INNER TUBE REPLACED WITH NEW. TIRE WAS A 7.00 X 6, 8PR. INNER TUBE TR20, S02602. TIRE AND TUBE TIME IN SERVICE: 219.5, LANDINGS APPROX.:400. INNER TUBE FAILURE WAS A SLIT ON SIDEWALL DEVELOPINSDR 2013FA0000629Crankcase · crackedA CRACK WAS DISCOVERED IN THE CRANKCASE AT THE LOWER FORWARD CYLINDER BASE STUD OF THE NR 2 CYLINDER OF APPROXIMATELY 1.5 INCHES. STARTS FROM THE BOTTOM OF STUD AREA AND TRAVELS DOWN AND AFT. A SLIGHT AMOUNT OF OIL LEAKING FROM AROUND THE BASE OF CYLINDER ATSDR YNQA20130314001Frame · crackedDURING 100 HR INSPECTION FOUND FATIGUE CRACKS ON FRAME MEMBERS OF FUSELAGE SECTION NR 8 AT MAIN LANDING GEAR FORWARD TRUSS MOUNTING BRACKET ON BOTH LEFT AND RIGHT SIDE. THESE CRACKS EMINATED FROM BOTTOM BOLT HOLES AND AT OUTSIDE FLANGE RADIUS OF FRAME. THEY
STCs that may be installed · 143
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Partenavia P.68C
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA03420ATPropeller model MTV-12-B-C-F/CF183-59b propeller installedSTC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.
Earlier aircraft with this N-number · 1
This aircraft carried N3927U before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.