Public Record · As of May 5, 2026
N9HU
Stinson L-5 · 1944 View Type →
Status
Registration Valid
Type
Fixed Wing Single Engine
Engine
LYCOMING 0-435A/0-435C
Last Cert Issue
—
01 / Registration
Filed with the Federal Aviation Administration
Every cell below is a literal field from the FAA Aircraft Registry. Click any value to open the FAA registry record for N9HU.
Tail Number
N9HU
Serial Number
44-17334
Make
STINSON
Model
L-5
Year of Manufacture
1944
Mfr / Model Code
8630202
Type Aircraft
Fixed Wing Single Engine
Type Engine
Reciprocating
Engines
1
Seats
2
Engine Manufacturer
LYCOMING
Engine Model
0-435A/0-435C
Horsepower
190 hp
Weight Class
CLASS 1
Certification
Standard · code 1
Registrant
ALAMO LIAISON GROUP · Corporation
Address
2352 S LOOP 1604 W · SAN ANTONIO, TX 78264-3719
FAA Region
2 · County 029
Status
Registration Valid
Airworthiness Date
—
Cert Issue Date
—
Expiration Date
—
Last FAA Action
—
Mode S Hex (ICAO24)
AC6B3C
Mode S (Octal)
53065474
Live position via ICAO24 AC6B3C
External services. Live tracks are unaffiliated with TallyAero or the FAA.
02 / NTSB Records
Events on file with the National Transportation Safety Board
-
Oct 26, 2024
Pleasanton, Texas
Airport · PEZ Pleasanton Municipal Airport
03 / Airworthiness Directives
Applicable to STINSON L-5
Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.
-
Jun 26, 2003
Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers with Aluminum Blades
This amendment revises an existing airworthiness directive (AD), that is applicable to Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) series and HA-A2V20-1B series propellers with aluminum blades. That AD currently requires initial and repetitive dye penetrant and eddy current inspections of the blade and an optical comparator inspection of the blade re…
-
Jan 2, 2003
Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers with Aluminum Blades
The Federal Aviation Administration (FAA) proposes to revise an existing airworthiness directive (AD), applicable to Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) series and HA-A2V20-1B series propellers with aluminum blades. That AD currently requires initial and repetitive dye penetrant and eddy current inspections of the blade and an optical compara…
-
Aug 27, 1997
Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers With Aluminum Blades
This amendment supersedes four existing airworthiness directives (ADs), applicable to Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) series propellers with aluminum blades, that currently require inspections for cracks in blade shanks and clamps. This amendment requires initial and repetitive dye penetrant and eddy current inspections of the blade and a…
04 / Service Difficulty Reports
FAA SDR filings
The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →
05 / Related
More on Stinson L-5 in the Atlas
Stinson L-5 type page → — 72 registered · 3 ADs · 23 NTSB records
Recent NTSB events · this type
-
Jun 14, 2018
Thomson, Georgia None
Atlas event → -
Mar 17, 2003
Carrollton, Georgia None
Atlas event → -
Sep 14, 2002
Spanish Fork, Utah None
Atlas event → -
Sep 26, 2000
WHEELING, Illinois None
Atlas event → -
Sep 29, 1999
WOODWARD, Oklahoma None
Atlas event →
Search the full US registry → · All airworthiness directives → · Accident & safety surface →
06 / Sources & Methodology
Every fact on this page links to its primary US-government source
- FAA Aircraft Registry →
Refreshed May 5, 2026
Available
- NTSB CAROL →
Refreshed May 5, 2026
Available
- Federal Register (FAA Airworthiness Directives) →
Refreshed May 5, 2026
Available
- FAA Service Difficulty Reports →
Refreshed May 5, 2026
Unavailable
We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.