1980 Cessna 404
Multi Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Description
HISTORY
Delivered new to UK distributor Northair Aviation in July 1980. Sold to Donington Aviation of the UK December 1982. Sold to Interflight of the UK May 1986. Sold to Aviation Beaufort of Jersey January 1990. Sold to Capital Aviation of the UK July 2000. Sold to Fly (CI) of Alderney/Guernsey May 2007. Reconnaissance Ventures Ltd purchased the aircraft in November 2011 it remained with them, on the UK register, until November 2020 when it was sold to MIKC of Latvia.
AIRFRAME
Aircraft type : Cessna 404
Serial number : 404-0644
Registration : YL-UFO
Year of manufacture : 1980
Total hours : 18,931
Total cycles : 19,219
Last flight : 3rd December 2023
ENGINES (L/R)
Manufacturer: Continental
Type: GTSIO-520-M
Hours Since New: tba / tba
Hours Since Overhaul: 1,286 / 1,391
Overhaul Interval (FH): 1,600 / 1,600
PROPELLERS (L/R)
Manufacturer: McCauley
Type: 3FF32C501
Hours Since Overhaul: 1,824 / 1,725
Date Of Overhaul: May 2020 / Feb 2020
Overhaul Interval (FH): 2,000 / 2,000
Overhaul Interval (months) 72 / 72
AVIONICS
Garmin GNS 430W VHF Com / VHF Nav / GPS (No.1)
Bendix/King KX-165A VHF Com / VHF Nav (No.2)
Bendix/King KR-805 ADF
Garmin GTX 330 Transponder
Bendix/King KN-64 DME
Bendix/King KFC-225 Autopilot
Kannad 406 AS ELT
EQUIPMENT
Dual camera holes.
Crew cargo doors.
De-icing system.
Cleveland wheels brakes
NOTE
Image showing rear camera holes taken from sister ship YL-IES.
Rear camera hole aperture approx. 20.5 inches (521mm) fore to aft, approx. 18.25 inches (464mm) wide at the lower skin.
Forward camera hole measures approx. 22.5 inches (572mm) fore to aft, approx. 17.25 inch (438mm) wide at the lower skin.
Engine
Manufacturer: Continental Type: GTSIO-520-M Hours Since New: tba / tba Hours Since Overhaul: 1,286 / 1,391 Overhaul Interval (FH): 1,600 / 1,600 PROPELLERS (L/R) Manufacturer: McCauley Type: 3FF32C501 Hours Since Overhaul: 1,824 / 1,725 Date Of Overhaul: May 2020 / Feb 2020 Overhaul Interval (FH): 2,000 / 2,000 Overhaul Interval (months) 72 / 72 AVIONICS Garmin GNS 430W VHF Com / VHF Nav / GPS (No.1) Bendix/King KX-165A VHF Com / VHF Nav (No.2) Bendix/King KR-805 ADF Garmin GTX 330 Transponder Bendix/King KN-64 DME Bendix/King KFC-225 Autopilot Kannad 406 AS ELT EQUIPMENT Dual camera holes. Crew & cargo doors. De-icing system. Cleveland wheels & brakes NOTE Image showing rear camera holes taken from sister ship YL-IES. Rear camera hole aperture approx. 20.5 inches (521mm) fore to aft, & approx. 18.25 inches (464mm) wide at the lower skin. Forward camera hole measures approx. 22.5 inches (572mm) fore to aft, & approx. 17.25 inch (438mm) wide at the lower skin.
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Kevin Wright
avpay.aero
|
Contact for Price
|
— | Apr 05, 2026 | — | Active |
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Cessna 404 loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 404
This 1980 Cessna 404 is a 10-seat multi engine piston with 18,931 hours on the airframe. There are currently 6 404 aircraft listed for sale with asking prices ranging from $150,000 to $693,117.
The 404 cruises at 200 kts (370 km/h) with a range of 1,100 nm (2,037 km) — suitable for regional and medium-distance travel.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 2 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 404 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Location not available
Title Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB safety data coming soon.
Airworthiness Directives — Cessna 404
ADs are mandatory safety instructions issued by the FAA. 2 recent ADs found for this aircraft type.
The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, and 441 Airplanes
View full AD →Cessna Aircraft Company Models T303, 402C, 404, 414A, and 421C Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 404
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
ON DEPARTURE FROM KBFL, THE LEFT ENGINE LOST POWER SHORTLY AFTER TAKEOFF, THE ENGINE RETAINED PARTIAL POWER AND THE PROPELLER WAS NOT FEATHERED. THE PILOT IMMEDIATELY RETURNED TO KBFL. INSPECTION OF THE ENGINE REVEALED A LARGE HOLE THROUGH THE TOP OF...
PILOT REPORTED RIGHT LANDING GEAR WOLD NOT EXTEND, WHEN SELECTED. THE EMERGENCY BLOW DOWN BOTTLE WAS ACTIVATED AND ALL GEARS CAME DOWN AND LOCKED.
ENGINE FAILED IN FLIGHT. NUMBER 1 CONNECTING ROD AND (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. RIGHT MAGNETO BROKEN OFF ITS MOUNT. THE ENGINE HAS BEEN IN SERVICE SINCE 05/2017. IT IS A FACTORY REBUILT ENGINE. THIS IS THE SECOND ENGINE I...
ENGINE DEVELOPED LOW OIL PRESSURE IN FLIGHT APPROX 20 PSI. REMOVED AND CLEANED OIL PRESSURE RELIEF PLUNGER. FOUND CARBON BITS IN OIL FROM CAVITY. ABOUT 20 HOURS LATER THE LOW OIL PRESSURE RETURNED. REMOVED OIL PRESSURE RELIEF PLUNGER. MORE CARB...
ENGINE FAILED IN FLIGHT. NR 5 AND NR 6 CONNECTING ROD (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. HOLES IN BOTH SIDES OF CASE BELOW NR 5 AND NR 6 CYLINDERS ABOVE OIL PAN FLANGE. THE ENGINE HAS BEEN IN SERVICE SINCE 07/2016. IT IS A FACTORY...
WHILE ON A ONE MILE FINAL APPROACH, THE RIGHT HAND ENGINE DEVELOPED A SEVERE VIBRATION AND BEGAN TO LOSE POWER. THE AUXILIARY FUEL PUMP WAS SELECTED TO HIGH BUT THE LOSS OF POWER DID NOT IMPROVE. THE ENGINE WAS SHUTDOWN AND THE PROPELLER FEATHERED. T...
DEPARTED, SELECTED GEAR UP AND SHORTLY AFTER BEGAN TO GET A PETROLEUM ODOR IN THE CABIN. IMMEDIATELY AFTER THAT THE LEFT HYD FLOW ANNUNCIATOR LIGHT ILLUMINATED, FOLLOWED BY THE RIGHT. ACTIVATED THE EMERGENCY LANDING GEAR EXTENSION BLOW DOWN SYSTEM...
WHILE IN CRUISE FLIGHT, THE PILOT NOTICED THE LT ENG OIL PRESS DROPPING. ONCE THE OIL PRESS DROPPED BELOW THE GREEN ARC, SHUT DOWN THE LT ENG & CONTACTED CTR. DIVERTED TO ALTERNATE AIRPORT, MADE AN UNEVENTFUL LANDING. THE OIL WAS BEING DUMPED OVER...
DURING FLIGHT, THE LT ENGINE ALTERNATOR STOPPED PRODUCING POWER DUE TO THE DRIVE CLUTCH SLIPPING. AFTER LANDING, REMOVED ALTERNATOR AND CHECKED THE DRIVE CLUTCH. COULD TURN THE CLUTCH BY HAND WITH SOME FORCE. REPLACED THE CLUTCH, REGULATOR AND ALT...
THE ACFT HAD TOTAL ELECTRICAL FAILURE DURING FLIGHT, DUE TO BOTH CHARGING SYSTEMS FAILING TOGETHER. RT ALTERNATOR FAILED DURING CRUISE, SHORTLY AFTER LT ALTERNATOR FAILED DUE TO A FAILED DRIVE CLUTCH. THE RT ALTERNATOR APPEARED TO HAVE AN INTERNAL ...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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