Registered owner
Sunrise Aviation Inc
Owner type
Corporation
Serial number
172S10561
Year built
2007
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
June 27, 2007
Certificate issued
December 10, 2015
Expires
December 31, 2028
Mode S code
A71629

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 56

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

1967In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19671
19681
19691
19712
19732
19742
19772
19791
19821
19881
19911
19921
19963
19971
19984
20001
20011
20032
20043
20053
20064
20073
20087
20092
20101
20112
20125
20132
20151
20171
20181
20211
20221
20231
20242
20261
See all 71 ADs

Information bulletins that may apply · 23

Advisory, not mandatory.

See all 28 bulletins

NTSB investigations

No NTSB investigations matched to N556ERMatched 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 172S aircraft

FAA incident reports

No FAA accident or incident reports matched to N556ERMatched 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 172S 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 2019FA0000030Hinge Fitting · corrodedDURING ROUTINE SURVEILLANCE, THE CENTER RUDDER HINGE HALF WAS OBSERVED WITH SEVERE EXFOLIATION/INTER-GRANULAR CORROSION.Feb 5, 2019 · N556ER · Cessna 172S · Rudder StructureSDR 2010FA0000979Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N556ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000978Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N556ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000977Control Cable · frayedCABIN OVERHEAD CTR PANEL REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULDAug 23, 2010 · N556ER · Cessna 172S · Aileron Control SystemSDR 201001043Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N556ER · Cessna 172S · Aileron Control System

STCs that may be installed · 351

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

See all 351 STCs