Location
Lewes, DE
Owner type
LLC
Serial number
421C0604
Year built
1978
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 18, 1978
Certificate issued
April 29, 2026
Expires
April 30, 2033
Mode S code
AC3694

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 33

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

1972In forceSuperseded2026
ADs by the year they took effect: 36 ADs
19722
19762
19771
19782
19803
19842
19861
19891
19901
19921
19941
19951
19961
19971
19983
20001
20011
20041
20053
20081
20162
20182
20232
See all 36 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N88604Matched 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 421C aircraft

FAA incident reports

No FAA accident or incident reports matched to N88604Matched 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 421C 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 98ZZZX3692Bolt · brokenPILOT NOTICED WHITE SMOKE COMING FROM LEFT TOP COWLING LOUVERS. SHUT ENGINE DOWN AND LANDED. MAINTENANCE FOUND BROKEN ROCKER SHAFT BOLT. REPLACED BOTH BOLTS AND GASKET. PERFORMED LEAK CHECK AND RUN-UP. ALL CHECKED GOOD.Jun 17, 1998 · N88604 · Cessna 421C · Reciprocating Engine Cylinder SectionSDR 98ZZZX990Bolt · failedPILOT REPORTED OIL LEAKING FROM RIGHT ENGINE. FOUND HOLE IN NR 5 CYLINDER ROCKER COVER. HEAD OF BOLT BROKE OFF THAT ATTACHES ROCKER ARM AND SHAFT TO CYLINDER ASSEMBLY. NEW BOLTS INSTALLED AND NEW ROCKER COVER.Feb 10, 1998 · N88604 · Cessna 421C · Reciprocating Engine Cylinder SectionSDR 97ZZZX3699Clamp · crackedOVERBOARD EXHAUST PIPE CLAMP HAD 2 INCH CRACK AROUND CLAMP. REMOVED CLAMP AND INSTALLED NEW ONE.Jul 25, 1997 · N88604 · Cessna 421C · Engine Collector/Tailpipe/NozzleSDR 97ZZZX192Air Filter · failedCABIN PRESSURIZATION WEAK, INSPECTED PRESSURIZATION HEAT EXCHANGER IN WING. BOTH EXCHANGERS PLUGGED WITH FELT MATERIAL. SUSPECT FELT MATERIAL CAME FROM ENDS OF PAPER AIR FILTERS. VACUUM AND CLEANED HEAT EXCHANGERS, TEST FLIGHT CHECK, AND NORMAL.Dec 16, 1996 · N88604 · Cessna 421C · Cabin Pressure Control SystemSDR 95ZZZX1166Shaft Gear · failedDURING DISASSEMBLY OF THIS ENGINE, THE 'NEW STYLE' STARTER CLUTCH (REF: SB M92-10) GEAR GEETH WERE STARTING TO FAIL. ALSO, REF: CRITICAL SB 94-4.Feb 16, 1995 · N88604 · Cessna 421C · Reciprocating Engine Rear SectionSDR 95ZZZX1165Shaft Gear · failedDURING DISASSEMBLY OF THIS ENGINE, THE 'NEW STYLE' STARTER CLUTCH (REF: SB M92-10) GEAR TEETH WERE STARTING TO FAIL. ALSO, REF: CRITICAL SB 94-4.Feb 16, 1995 · N88604 · Cessna 421C · Reciprocating Engine Rear Section

STCs that may be installed · 258

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

See all 258 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N88604 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.