Registered owner
Frasch Randy
Location
Missoula, MT
Owner type
Individual
Serial number
764
Type
Rotorcraft
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 30, 1989
Certificate issued
February 11, 2015
Expires
February 29, 2028
Mode S code
AC462C

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

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Airworthiness directives that may apply · 55

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: 69 ADs
19641
19671
19691
19721
19732
19751
19772
19781
19792
19811
19823
19881
19892
19903
19911
19921
19944
19951
19963
19971
19982
20011
20022
20032
20041
20063
20073
20083
20091
20102
20111
20124
20152
20171
20182
20211
20221
20232
20241
20261
See all 71 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N890JRMatched 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 Enstrom F-28F aircraft

FAA incident reports

No FAA accident or incident reports matched to N890JRMatched 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 Enstrom F-28F aircraft

Service difficulty reports · 6

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

SDR 98ZZZX1348Control Cable · bindingTHROTTLE CONTROL CABLE INTERNAL BINDING CAUSES PARTIAL TO FULL LOSS OF THROTTLE CONTROL. UNIT IN SERVICE 20 WEEKS.Mar 6, 1998 · N890JR · Enstrm F28F · Power LeverSDR 97ZZZX2773Rod End Bearing · wornACCELERATED LATERAL BEARING WEAR. EXCEEDED LIMITS WITHIN 304 HOURS. THIS ROD END NORMALLY LASTS UP TO 1,000 HOURS IN SERVICE. INSTALLED 2 NEW 01-691-04 BEARINGS.May 19, 1997 · N890JR · Enstrm F28F · Tail Rotor Control SystemSDR 97ZZZX2554Rod End Bearing · wornACCELERATED LATERAL BEARING WEAR. EXCEEDED LIMITS WITHIN 304 HOURS. THIS ROD END NORMALLY LASTS UP TO 1,000 HRS IN SERVICE. INSTALLED 2 NEW 01-691-04 BEARINGS.May 19, 1997 · N890JR · Enstrm F28F · Tail Rotor Control SystemSDR 96ZZZX5175Relay · stuck contactsPOINTS IN RELAY FUSE TOGETHER CAUSING RUNAWAY TRIM ACTION RESULTING IN UNCONTROLLED ATTITUDES OF ACFT. REQUIRES TWO PILOTS ON CYCLIC TO OVERRIDE AND LAND ACFT. RELAY MFG (SIEMENS) HAS INDICATED THIS MAY NOT BE THE CORRECT RELAY FOR THIS APPLICATION. INSTALLSep 11, 1996 · N890JR · Enstrm F28F · Main Rotor ControlSDR 96ZZZX5540Yoke · crackedCRACKS FOUND BETWEEN CONTROL ROD AND UNIVERSAL YOKES. CRACK RUNS DOWN THE WEB BETWEEN BOTH AT 2 LOCATIONS. SUBMITTER STATED THIS IS SECOND FOUND THIS MONTH. THE OTHER CRACKED SWASHPLATE IS S/N 11-897-88H WITH SIMILAR TIME IN SERVICE. CRACKED SWASHPLATE YOKJun 7, 1996 · N890JR · Enstrm F28F · Main Rotor Mast/SwashplateSDR 96ZZZX4185Swashplate Yoke · crackedCRACKS FOUND BETWEEN CONTROL ROD AND UNIVERSAL YOKES. CRACK RUNS DOWN THE WEB BETWEEN BOTH AT 2 LOCATIONS. THIS IS SECOND FOUND THIS MONTH. THE OTHER CRACKED SWASHPLATE IS S/N 11-897-88H WITH SIMILAR TIME IN SERVICE. CRACKED SWASHPLATE YOKE REMOVED FROM SEJun 7, 1996 · N890JR · Enstrm F28F · Main Rotor Mast/Swashplate

STCs that may be installed · 73

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

See all 73 STCs