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Owner self-reported — never independently field-inspected
Last inspection record: 1982/12/15
Location confidence
No coordinate anomaly detected
Terrain cross-check (USGS 3DEP)
FAA 884 ft MSL · USGS ground 822 ft · Δ 62 ft
Differential consistent with an elevated / rooftop pad
Structure cross-check (Overture / OSM)
On a building footprint — height not tagged in the source
Building height ≈ 19 ft — measured independently of the FAA record
Cross-source consensus
Corroborated — terrain and structure agree (2/2 sources)
Cross-checked against independent public data — USGS 3DEP terrain, Overture/OSM building footprints, the federal hospital registry, and measured dimensions. The State of the U.S. Heliport Record →
eVTOL readiness
CONDITIONALConversion feasibility · four readings, one line each
Obstruction screen
Clear
No obstructions within 0.5 nm on the FAA obstacle file.
Geometry
Meets the FATO footprint
Recorded pad side 100 ft against a 100 ft eVTOL FATO.
Structural FATO
Unverified
The full 100 × 100 ft FATO must be load-bearing. The FAA does not record structural capacity, so no record can confirm it.
Overall
Conditional
Obstruction screen passed. Geometry and structural capacity remain open. Site validation required.
This pad already covers the eVTOL landing footprint as it stands.
recorded pad eVTOL FATO
Recorded pad (limiting side)
100 ft
eVTOL FATO required
100 ft
FAA EB-105 vertiport pattern — 2× a ~50 ft eVTOL controlling dimension, plus a 125 ft safety-area side.
Load-bearing FATO
100 × 100 ft must be structural
No heliport precedent — typically the binding gate for rooftop and hospital pads.
Measured against FAA pad geometry and federal FATO sizing (EB-105). The obstruction screen is the only reading the engine verdict rests on; geometry and structural capacity are stated separately and never folded into it. A dimensional pre-screen — site-level validation required, and independent of the underwriting risk score.
Jurisdiction has adopted NFPA 418 in fire/building code.
FAA facility data
FAA LID
9NY3
AIX ID
aix:hp:8AKRFV2Z
Lat / Lng
42.09730, -76.22465
Elevation
884 ft MSL
Pad dimensions
100 × 100 ft
Surface type
CONC
Activation date
1972/04
Last inspection
1982/12/15
Last owner update
2025/11/12
FAA OEAAA airspace determinations2
Airspace clearance
On file as archived / procedural records — no standing clearance to track.
Filing activity
Most recent determination 2006-03-14
NRAARCH-DeterminedASN 2006-AEA-111-NRA2006-04-21
Heliport · 1 ft AGL — New construction- adding a new hangar for producing a new Presidential Marine One helicopter at Lockheed Martin-Owego. New facility is about 300 yards aways from where Navy MH-60 helicopters are produced.\r\nCHANGE NAME TO: LOCKHEED MARTIN VXX HELIPORT (9NY3). PRIVATE/PRIVATE USE
NRAARCH-DeterminedASN 2006-AEA-29-NRA2006-02-08
Heliport · 1 ft AGL — Some construction here we're DEACTIVATING the private use Heliport\r\nFAA Site # 15887.02*H
Blueprint
The record vs. what we measured
59/100
DATA INTEGRITY
Surface elevation
The FAA record places this pad at 884 ft. USGS terrain plus the building put the actual rooftop at 840 ft — a -44 ft difference the federal record doesn’t carry.
eVTOL footprint
Footprint assessment available.
SIGNALFEDERAL RECORDMEASURED
Surface elevation884 ft840 ft · USGS+structure
Structurenot on recordOn a building
Pad dimensions100 ft side (filed)100 ft side · measured
Coordinate integrityas filedterrain cross-checked
Independent inspectionowner self-reportednone on record
✓Federal record
→
✓Cross-checkedUSGS · Overture · dimensions
→
3Physically verifiedGround Truth capture
Obstructions, exact FATO geometry, surface condition, and downwash exposure require a physical Ground Truth capture — not shown above as measured. A field verification completes the record and writes the measured truth to this facility’s authority.
This page is the public data-integrity record. The full RiskIndex assessment — Q1–Q5 compliance, dimensional / FATO analysis, an underwriting-grade risk score, peer benchmark, and a sealed Site Intelligence Report — is available on request.