Location
Murrieta, CA
Owner type
LLC
Serial number
17280641
Year built
1999
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
February 15, 1999
Certificate issued
August 4, 2026
Expires
August 31, 2033
Mode S code
ABF086

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.

On this page

Airworthiness directives that may apply · 85

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

1964In forceSuperseded2026
ADs by the year they took effect: 99 ADs
19641
19661
19672
19681
19692
19712
19721
19734
19742
19751
19773
19781
19792
19821
19881
19891
19912
19921
19931
19951
19964
19972
199810
19991
20001
20011
20021
20032
20043
20054
20066
20073
20087
20092
20102
20112
20125
20132
20151
20171
20181
20211
20222
20231
20242
20261
See all 102 ADs

Information bulletins that may apply · 27

Advisory, not mandatory.

See all 34 bulletins

NTSB investigations

No NTSB investigations matched to N869CPMatched 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 172R aircraft

FAA incident reports

No FAA accident or incident reports matched to N869CPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 172R aircraft

Service difficulty reports · 5

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

SDR 2009FA0000924Bulkhead · crackedPROPELLER SPINNER FWD BULKHEAD HAS CRACKS AROUND BOLT HOLES. CAUSE IS FROM NORMAL WEAR. COULD BE PREVENTED BY INSTALLING A RING UNDER BOLTS SIMILAR TO THE ONE USED IN THE PROPELLER. INSTALLATION IAW SB NR SB221B. (K)Oct 2, 2009 · N869CP · Cessna 172R · Propeller Spinner SectionSDR 2001FA0000571Nut Plate · brokenDURING 100 HOUR INSPECTION, TECHNICIAN FOUND LOWER ELEVATOR STOP NUTPLATE BROKEN AND FIBER LOCK PORTION OF PART SEPARATED FROM THE REST OF NUTPLATE DETAIL REPEATED ELEVATOR CONTACT WITH STOP BOLT WHEN AIRCRAFT IS PARKED AND CONTROL LOCK IS IN, SUCH AS IN WINDYNov 16, 2001 · N869CP · Cessna 172R · Horizontal Stabilizer StructureSDR 20001018SH031Mount · tornCONDITION: COWLING MOUNT TORN. CORRECTIVE ACTION: REPLACED WITH NEW. (X)Oct 15, 2000 · N869CP · Cessna 172R · Engine Cowling SystemSDR 20000508SH007Light · chafedPILOT REPORTED THE RADIO LIGHTS WERE FLICKERING WHILE ENGINE WAS RUNNING. UPON INSPECTION, WIRING BUNDLE THAT RUNS HORIZONTALLY ACROSS BOTTOM OF INSTRUMENT PANEL WAS FOUND CHAFING ON ''''RADIO INSTRUMENT LIGHT POTENTIOMETER'''' PN S2091-9 (REF: R1002 I CESSNApr 17, 2000 · N869CP · Cessna 172R · Communications SystemSDR 99ZZZX2583Firewall · crackedC/W CESSNA SB 98-53-02. FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX. CRACK EXTENDED THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 2 INCHES IN LENGTH. ALSO, FOUND LOWER COWL SHOCK MOUNTS, P/N J7444-36, TORN. THIS ACFT SERJun 25, 1999 · N869CP · Cessna 172R · Fuselage Main, Structure

STCs that may be installed · 391

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

See all 391 STCs