- Registered owner
- Lsa LLC
- Location
- Kalispell, MT
- Owner type
- LLC
- Serial number
- 4129
- Year built
- 1941
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- March 27, 1959
- Certificate issued
- June 11, 2022
- Expires
- June 30, 2029
- Mode S code
- A98F1D
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Wright C9GC&D model are included below.
On this page
Airworthiness directives that may apply · 7
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1990 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 2011 | 1 |
| 2023 | 1 |
| 2026 | 1 |
Airframe · Douglas SUPER DC-3
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2011-12-01Equipment/FurnishingsAD 93-14-12Crewmember Protective Breathing Equipment UnitsAD 92-06-15Prevent Structural Failure Of WingsAD 90-05-08Revise Inspection ProgramAD 78-18-02Elevator Control SystemInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Douglas SUPER DC-3
SAIB NM-15-03Flight ControlsNTSB investigations
No NTSB investigations matched to N715FMatched 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 Douglas SUPER DC-3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N715FMatched 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 Douglas SUPER DC-3 aircraft
Service difficulty reports
No reports matched to N715FGeneral 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 Douglas SUPER DC-3 aircraft
STCs that may be installed · 15
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Douglas SUPER DC-3
STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC SA02268CHInstallation of Airwolf Filter Corp. Air Oil SeparatorSTC SA01406NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and
rotary wingSTC SA02930NYInstallation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) InstrumentsSTC SA1315WEInstallation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.STC ST00165DEInstallation Of Oilamatic Preoiler system.STC SA3-425Installation of one-piece windshield, electrically heated or bird-proof.STC ST02196AKReduction of payload to 7500 pounds and limitation of passenger seats to 19 or few.STC SA4149WEInstallation of a flap and landing gear aural warning system.STC SA02168AKInstallation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.STC ST233CHLimit maximum payload capacity to7500 lbs. maximum.STC SA4-1210Installation of Eonnex cover on aircraft surfaces.STC SA3241WEInstallation of turbopropeller Rolls-Royce Dart 510 engines, Dowty Rotol (c)R-130/4-20-4/12E propellers, and associated system and equipment modifications.STC SA4-1002Alternate fuel source installation in aircraft with approved fuel flow- meter and Wright R-1820 or C9 Series engines.STC SA1-14Relocation of airspeed pitot head.