N2134M

CESSNA 172S · 2003 · Valid Registration

Registered owner: CHRISTIANSEN AVIATION LLC, DE (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
U.S. Aviation AcademyOperator2026-05-13 – 2026-05-13Operator named in NTSB report
WESTWIND AVIATION INC (W10A)Operator2013-09-01 – 2013-09-01Operator named in NTSB report

Accident & incident history

Acc · 2026-05-13 Operator named in NTSB report
CESSNA 172S None injury Part 91U.S. Aviation Academy Not yet finalized — may be revised.
Source: NTSB case CEN26LA187
Acc · 2013-09-01 Operator named in NTSB report
CESSNA 172S None injury Part 91WESTWIND AVIATION INC
Source: NTSB case WPR13CA397
Accident · 1986-01-30 Unresolved
Piper PA-28-161 Fatal injuryoperator not yet resolved
Source: NTSB case LAX86FA102

Maintenance disclosures

O · 2006-07-11 Unresolved
ATA 2710

DURING AN ANNUAL INSPECTION OF THE RT WING, THE AILERON CROSSOVER CABLE WAS FOUND TO BE FRAYED AT THE WEAR BLOCK. PROBABLE CAUSE IS THAT THE WEAR BLOCK IS CAUSING FRICTION AND WEAR ON THE CABLE. A RECOMMENDED SOLUTION IS TO REMOVE THE WEAR BLOCK. (K)

Source: SDR 2006FA0000725 · FAA SDRS
O · 2005-09-14 Unresolved
ATA 5720

WHILE INSPECTING FOR STORM DAMAGE, DURING THE INSPECTION OF THE AILERON CABLES, FOUND A FLAT SPOT ON THE LT AILERON CROSSOVER CABLE AT THE AILERON CABLE ABRASION STRIP ATTACHED TO A RIB ASSEMBLY LOCATED AT WING STATION 71.19. FURTHER INVESTIGATION FOUND THE CABLE BEGINNING TO FRAY. THE CAUSE IS THE CABLE WEARING ON THE ABRASION STRIP. TO SOLVE THIS PROBLEM, THE ABRASION STRIP BE LOWERED OR A PULLEY BE INSTALLED. (K)

Source: SDR 2005FA0001328 · FAA SDRS
O · 2004-12-22 Unresolved
ATA 6113

DURING ANNUAL INSPECTION, FOUND PROP SPINNER FWD BULKHEAD CRACKED AROUND 2 BOLT HOLES. RECOMMENDATION: MANUFACTURE BULKHEAD STRONGER OR THICKER. (K)

Source: SDR 2005FA0000147 · FAA SDRS