Single-engine piston

N9190A

1989 Piper Turbo Lance II

Registered 1 NTSB/FAA record
Built
1989
Serial
32R-7887064
Class
Single-engine piston
Engines
Lycoming TIO-540 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
New Braunfels, TX
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Registration record

N9190A on the FAA register

Type
1989 Piper Turbo Lance II (FAA: Piper PA-32RT-300T)
Serial
32R-7887064
Engines
Lycoming TIO-540 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
New Braunfels, TX
Certificate issued
2024-12-12
Airworthiness date
1989-08-26
Registration expires
2031-12-31
Airworthiness class
Standard · normal
Mode S (hex)
ACBA73
Mode S (octal)
53135163
Seats (type)
7
Weight class
up to 12,499 lb
Range (type)
648 nm
Cruise (type)
175 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2031-12-31
    Registration expires (renewal due).
  • 2024-12-12
    Certificate of registration issued as N9190A to the current registrant.
  • 1991-03-05
    Accident at Leander, TX; damage: substantial.
  • 1989-08-26
    Airworthiness date on the current FAA record (standard category (normal)).
  • 1974-07-01
    N9190A previously assigned to a Cessna 170A (s/n 18951); cancelled.
Overview

About N9190A

N9190A is a 1989 Piper Turbo Lance II (FAA model PA-32RT-300T), serial number 32R-7887064. It is registered to an individual in New Braunfels, Texas. The current certificate of registration was issued on December 12, 2024 and expires on December 31, 2031.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming TIO-540 series engine and 7 seats. Published figures for the type give a cruise speed of about 175 knots and a range of about 648 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated August 26, 1989.

N9190A has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
175 kt
Range
648 nm
Power / thrust (each)
300
Takeoff over 50 ft
1,875 ft
Landing over 50 ft
1,760 ft
Fuel burn
19 gph

Published figures for the Piper Turbo Lance II type. They describe the model, not this airframe's equipment or condition. Piper Turbo Lance II specs, prices and for-sale inventory →

Safety record

Accident & incident history

1991-03-05 Accident · Leander, TX Damage: Substantial NTSB · FTW91LA047
Reported aircraft: Piper PA-32RT-300T
Probable cause: THE PILOT'S FAILURE TO MAINTAIN A PROPER DESCENT RATE DURING THE FINAL APPROACH.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Browse: Piper aircraft for sale· Piper Turbo Lance II overview· Aircraft registered in Texas· Registry by state· FAA registry stats

Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.