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N5388J

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1980 Cessna 404 · Continental GTSI0-520-F-K

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Registered owner
Richland Aviation Inc
Location
Sidney, MT
Owner type
Corporation
Serial number
404-0666
Year built
1980
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
September 17, 1980
Certificate issued
August 24, 2026
Expires
August 31, 2033
Mode S code
A6D19E
Cessna 404Airframe model · 8 seats · 2 engines · 26 registeredTCDS A25CEAirframe · Cessna 404Engine modelContinental GTSI0-520-F-K

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 20

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

1978In forceSuperseded2026
See all 20 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 1
SAIB CE-14-11Landing Gear; Nose Landing Gear TrunnionsIssued Feb 25, 2014

NTSB investigations

No NTSB investigations matched to N5388JMatched 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 404 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.

Incident 20200831009539ILanding: Rollout · Albuquerque, NMOn augest 31, 2020, at 1841 MST, a Cessna 404, N5388J, registered to [privacy data omitted] (gnba - part 135 operator) experienced a right main landing gear collapse on roll out on runway 21 at the Albuquerque Sunport (abq). Visual meteorological conditions…Aug 31, 2020 · Minor damage

Service difficulty reports · 3

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

SDR GNB2009F00000Sleeve · crackedAFTER TAKEOFF, PILOT FELT ENGINE RUNNING ROUGH. ACFT RETURNED TO FIELD. MX DISCOVERED NR 2 CYLINDER UPPER DECK NOZZLE TUBE CRACKED. POSSIBLE WEAK WELD OF OUTSIDE TUBE. RECOMMENDED CLOSER ATTENTION TO LEANING ON LINES WHEN WASHING ON ENGINE AND INSPECTING AMay 26, 2009 · N5388J · Cessna 404 · Reciprocating Engine Cylinder SectionSDR 2005FA0000621Control Cable · damagedDURING INSPECTION, FOUND CABLE TO BE BLENDED AT FAIRLEAD APPROX 6 INCHES FROM AFT END OF CABLE. PROBABLE CAUSE FROM NEW STYLE (STAINLESS STEEL) CABLE. NEW STYLE LASTED ONLY FRACTION OF TIME AS OLD STYLE. (SW01200504154) (K)Apr 11, 2005 · N5388J · Cessna 404 · Elevator Control SystemSDR 98ZZZX1553Bolt · failedSHORTLY AFTER TAKEOFF, PILOT FELT MINOR SHAKE IN LT ENGINE. A VISUAL INSPECTION (IN-FLIGHT) REVEALED SMALL AMOUNT OF OIL STREAMING BACK. PILOT RETURNED TO AIRPORT. MAINTENANCE PERSONNEL NOTED NR 6 INTAKE ROCKER BOX HAD A HOLE FROM THE INSIDE OUT. REPLACED Mar 1, 1998 · N5388J · Cessna 404 · Reciprocating Engine Power Section

STCs that may be installed · 157

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

See all 157 STCs