Registered owner
Donohue Andrew
Location
Tulsa, OK
Owner type
Individual
Serial number
172RG0947
Year built
1981
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
August 26, 1981
Certificate issued
May 5, 2025
Expires
May 31, 2032
Mode S code
AD719F

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

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Airworthiness directives that may apply · 78

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1963In forceSuperseded2026
ADs by the year they took effect: 83 ADs
19631
19641
19661
19671
19681
19693
19712
19732
19742
19773
19792
19805
19815
19821
19832
19851
19861
19882
19892
19901
19912
19921
19951
19963
19972
19984
20001
20012
20021
20041
20052
20066
20071
20082
20091
20102
20111
20122
20171
20201
20211
20222
20231
20242
20261
See all 84 ADs

Information bulletins that may apply · 21

Advisory, not mandatory.

See all 33 bulletins

NTSB investigations

No NTSB investigations matched to N9654BMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 172RG aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR CQN2004F00000Bulkhead · crackedCRACKS WERE LOCATED AT LT AND RT RELIEF CUTS OF STATION 124.00 UPPER FUSELAGE BULKHEAD. PROBABLE CAUSE FOR LT SIDE IS AUX POWER RECEPTACLE AND RT SIDE COULD BE FROM LANDING STRESSES.Sep 30, 2004 · N9654B · Cessna 172RG · Fuselage Main, BulkheadSDR 20010613CW009Actuator · crackedFOUND ONE ACTUATOR CRACKED.May 25, 2001 · N9654B · Cessna 172RG · Landing Gear ActuatorSDR 99ZZZX3121Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9654B · Cessna 172RG · Fuselage Main, Longeron/StringerSDR 99ZZZX3120Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9654B · Cessna 172RG · Fuselage Main, Longeron/StringerSDR 99ZZZX3119Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9654B · Cessna 172RG · Fuselage Main, Longeron/StringerSDR 99ZZZX3118Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9654B · Cessna 172RG · Fuselage Main, Longeron/Stringer

STCs that may be installed · 310

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 310 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N9654B before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.