- Registered owners
- Owens Russell A TrusteeOwens Lynn P Trustee
- Location
- San Diego, CA
- Owner type
- Co-owned
- Serial number
- 17/U15
- Year built
- 2012
- Type
- Glider
- Engine
- 4 cycle
- Airworthiness
- Light sport, glider
- Airworthiness date
- January 14, 2013
- Certificate issued
- April 2, 2013
- Expires
- April 30, 2029
- Mode S code
- A9BEE8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included below.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N727PXMatched 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 Phoenix Air Sro U-15 PHOENIX aircraft
FAA incident reports
No FAA accident or incident reports matched to N727PXMatched 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 Phoenix Air Sro U-15 PHOENIX aircraft
Service difficulty reports
No reports matched to N727PXGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Phoenix Air Sro U-15 PHOENIX aircraft
Reports on N727PX not matched to an aircraft · 14
They name N727PX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2006FA0000814Frame · damagedDURING SCHEDULE INSP REQUIRED BY AD, FOUND 8.5 WEB SEPARATION AT FUSELAGE BS 950, RT BETWEEN STRINGER S-9 AND S-10. PARTIAL FRAME REPLACEMENT BETWEEN S-9 AND S-12 WAS ACCOMPLISHED. INSTALLED KIT NR 65C35283-2. ALL WORK DONE IAW DWG, SRM, SB, AND AD. (K)SDR 2003F00340Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM, AFT LOWER FLANGE, AT 21 INCHES AND 30 INCHES FROM INBOARD END. ELEVATOR STATION 17.20 TO 47.20, CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-06. (M)SDR 2003F00338Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM UPPER FORWARD FLANGE, 27 INCHES FROM INBOARD END AT ELEVATOR STATION 17.20 TO 44.20 CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-6. (M)
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.