- Registered owner
- Muller Clifford L
- Location
- Breezy Point, MN
- Owner type
- Individual
- Serial number
- JA1207069
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- July 20, 2021
- Expires
- July 31, 2028
- Mode S code
- A40C8A
- Kit
- Javron Inc PA-18 REPLICA
From the FAA registry file of October 24, 2026.
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 N360CMMatched 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 Muller Clifford L PA-18 REPLICA aircraft
FAA incident reports
No FAA accident or incident reports matched to N360CMMatched 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 Muller Clifford L PA-18 REPLICA aircraft
Service difficulty reports
No reports matched to N360CMGeneral 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 Muller Clifford L PA-18 REPLICA aircraft
Reports on N360CM not matched to an aircraft · 7
They name N360CM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR ABXR2020032000016Intercostal · damagedPERMANENT REPAIR NEEDS INSTALLED AT STA 1043 RBL 54.75-RBL 74.75 MAIN DECK FLOOR PANEL AND INTERCOSTAL DAMAGE. INSTALLED INTERIM REPAIR AT STA 1043 RBL 54-75-74.75 MAIN DECK FLOOR TRACK DAMAGE IAW B767-300 SRM 51-40-05 51-40-02 P.9 AND AMES INTERM REPAIR DOC SDR IXXA20200323006Skin · crackedAIRCRAFT GROUNDED FOR ATI-767 C CHECK 18. IN COMPLIANCE OF TASK CARD 53-730-00-01. "GVI EXTERIOR SECTION 48 LH", THE FOLLOWING DISCPRENCY WAS IDENTIFIED: LH AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L.FABRICATED AND INSTALLED REPAIRSDR ABXR2020032000015Skin · crackedL/H AFT FUSELAGE EXTERIOR SKIN IS CRACKED STA 1654.5 BETWEEN STRINGER 3L-4L. REMOVED DAMAGE ON L/H AFT FUSELAGE SKIN AT STA 1554E PER B767 SRM 58-80-01 REPAIR 4. CAT A REPAIR NO OTHER ACTIONS REQ IAW B767SRM 51-00-06
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.
Earlier aircraft with this N-number · 2
These aircraft carried N360CM before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.