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Aircraft record

N9622V1990 Christen Industries INC A-1

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Sep 2022)1 AD may apply4 service difficulty reports

Registration
Valid
expires Apr 30, 2027
Based in
Anchorage, AK
owner city / state
Owners
1
since 2002
NTSB events
2
substantial, 2022
ADs may apply
1
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Anchorage, AK
Certificate issued
May 1, 2002
Expires
Apr 30, 2027
Airworthiness
Standard · Normal
Airworthiness date
Mar 10, 1995

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Christen Industries INC
Model
A-1
Year
1990
Serial number
1154
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AD6646

Engine

Make and model
Lycoming O&Vo-360 Ser
Type
Reciprocating
Power
180 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2002 – nowIndividual ownerAnchorage, AK · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (2)

Accident · substantial damage

Sep 1, 2022 · Point Mackenzie, AK

The pilot’s improper monitoring and failure to maintain airspeed during a critical phase of flight, which resulted in an exceedance of the airplane’s critical angle of attack, an aerodynamic stall, and subsequent impact with terrain.

Damage
Substantial
Injuries
Minor
Report
ANC22LA072

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC22LA072)

Accident · substantial damage

Jun 19, 2006 · Takotna, AK

The pilot's excessive use of brakes during the landing roll. A factor associated with the accident was soft terrain.

Damage
Substantial
Injuries
None
Report
ANC06CA077

From NTSB records; matched by N-number.Read NTSB report (search CAROL for ANC06CA077)

Accident history for this model

ADs published since 1998 that may apply (1)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2020-16-06Horizontal Stabilizer StructureSep 1, 2020Airframe (A-1)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (4)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Hydraulic power · vent line · blockedJan 2, 2006

    BOTH LT FUEL VENT LINES BLOCKED BY ICE. ENGINE STOPPED DURING TAXI TO RUNWAY. ALTHOUGH PREFLIGHT LISTS CHECKING FUEL VENT LINES ARE CLEAR, THIS NEEDS TO BE EMPHASIZED MORE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · vent line · blockedDec 3, 2005

    ENGINE STOPPED DUE TO BLOCKED FUEL VENT LINE. THIS OCCURRED ON THE GROUND DURING TAXIING. NO DAMAGE TO PLANE. PROBABLE CAUSE WAS SNOW BUILD UP ON THE WING EXTENDING OVER THE ENDS OF THE VENT LINES FOLLOWED BY FREEZING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · vent line · blockedDec 3, 2005

    ENGINE STOPPED DUE TO BLOCKED FUEL VENT LINE. THIS OCCURRED ON THE GROUND DURING TAXIING. NO DAMAGE TO PLANE. PROBABLE CAUSE WAS SNOW BUILD UP ON THE WING EXTENDING OVER THE ENDS OF THE VENT LINES FOLLOWED BY FREEZING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Flight controls · flap arm · bolts incorrectDec 26, 1996

    FLAP CABLE ATTACH BOLTS AT WING BELLCRANK FOUND TO BE INSTALLED UPSIDE DOWN. IPC SHOWS BOLTS INSTALLED HEAD UP. NUT STRIKES ADJACENT RIB AT FLAPS DOWN POSITION. NO RECORD OF FLAP MAINTENANCE IN A/C RECORDS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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