1969 Cessna 401A for sale

1969 Cessna 401A

Multi Engine Piston

PROJECT
$49,000
Location Galesburg, Illinois
Total Time 5,700 hrs
Seats 8
Reg # N401AK
Engine CONTINENTAL TSIO-520-VB
Cruise 210 kts (389 km/h)
ICAO Type C402
✓ Clean NTSB 3 ADs ✓ Verified recently ⚠ High time

Aircraft Details

Seller reported

Description

N401KA is a 1969 Cessna 401A Project Owners Passing Forces Sale, Aircraft is Located at the Kewanee, IL Airport KEZI, Always Stored in Hanger, No Corrosion or Hail Damage, Last Flown 2007, Will Need to be Trailed Away! TTAF: 5700, L/H Engine Model TSIO-520-E, S/N 183541-R, TSMO: 1041, R/H Engine Model TSIO-520-E, S/N 514404, TSMO: 1134, R/H Prop McCauley 3AF320C87-NR 1974 P22EA S/N 746908 TSOH 5 (1997) Blades S82NC-5.5 S/N F32476YS/F32485YS/F33237YS, L/H Prop McCauley 3AF32C87-KNR 1969 P22EA S/N 693508 TSOH 5 (1997) Blades S82NC-5.5 S/N F16412YS/F16468YS/F16656YS, Call Mary

Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.

Price Comparison

Source Price Action
Scott Delawder
barnstormers.com
$49,000

Estimate Monthly Payment

Cessna 401A loan calculator

AeroGurus

AeroGurus Data & Analysis

Independent data from FAA, NTSB, and market analysis

About This Cessna 401A

This 1969 Cessna 401A (N401AK) is a 8-seat multi engine piston with 5,700 hours on the airframe.

The 401A cruises at 210 kts (389 km/h) with a range of 1,000 nm (1,852 km) — ideal for short hops and local flights. Service ceiling of 26,000 ft allows operation above most weather.

Operating costs: Fuel burn is 38 GPH (144 L/h), which at current 100LL avgas prices (~$6.20/gal) means approximately $236/hr in fuel alone. Total variable cost including maintenance reserves is approximately $390/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $35,000. With 5,700 hours on the airframe, this aircraft has exceeded TBO (1,400 hrs) — verify engine status and overhaul reserve.

NTSB records show 0 incidents for this airframe — a clean safety record. There are 3 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

Safety record: 0 NTSB incidents
Airframe: 5,700 hours — verify engine time vs TBO (1,400 hrs)
Check 3 ADs compliance — mandatory before flight
Budget $570 for pre-purchase inspection

Cessna 401A — Model Specs

Model specification

Standard specs for this model. Actual aircraft may differ.

Seats
8
Cruise Speed
210 kts (389 km/h)
Max Speed
225 kts (417 km/h)
Range
1,000 nm (1,852 km)
Ceiling
26,000 ft (7,925 m)
Max Weight
6,300 lbs (2,858 kg)
Useful Load
2,200 lbs (998 kg)
Horsepower
300 HP
Fuel Capacity
102 gal (386 L)
Fuel Burn
38 GPH (144 L/h)
Engines
2
TBO
1,400 hrs

Estimated Cost of Ownership

AeroGurus estimate

CESSNA 401

Fuel Burn
38.0 GPH
~$247/hr
Variable Cost
$390/hr
fuel + mx + reserves
Annual Fixed
$35,000/yr
hangar + insurance + annual
Engine Overhaul
$48,000
every 1,400 hrs

AeroGurus estimates based on industry averages for the CESSNA 401. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.

Ownership & Registration

FAA registration data pending for N401AK.

Location & Ownership

FAA records

Aircraft Location

Galesburg, Illinois

Seller reported 184 more aircraft in Illinois →

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.

We'll check N401AK against the NTSB accident database.

Airworthiness Directives — Cessna 401A

ADs are mandatory safety instructions issued by the FAA. 3 recent ADs found for this aircraft type.

2009-04-04 2009-03-02

Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, and 402B Airplanes

View full AD →
2005-20-25 2005-11-09

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 →
2005-12-12 2005-06-22

Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 411, and 411A Airplanes

View full AD →

Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.

Service Difficulty Reports — Cessna 401A

SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.

Engine Turbine POWER LOSS
2015-04-16

(CAN) DURING TAKEOFF, THE PILOT ADVANCED BOTH PLAS TO TAKEOFF & NOTICED THAT THE NR 1 ENG DID NOT RESPOND FROM THE IDLE SPEED OF 28% N1. THE PILOT ABORTED THE MISSION & RETURNED TO THE GATE & TRIED AGAIN WITH NO ABILITY TO ADVANCE POWER ON THE SUSPE...

Reciprocating Engine UNKNOWN
2015-03-05

SHORTLY AFTER TAKE-OFF AT APPROXIMATELY 200 FT AGL, PILOT NOTICED PARTIAL LEFT ENGINE POWER LOSS WITH ENGINE FUEL FLOW SURGING FROM MINIMUM TO MAXIMUM. DECLARED AN EMERGENCY RETURNED AND LANDED . NOTICED WHEN PULLING POWER BACK TO LAND PROBLEM LEFT...

Power Plant FAILED
2013-03-05

APPROXIMATELY 1.5 HRS INTO FLIGHT, PILOT NOTED RT ENGINE MANIFOLD PRESSURE DROPPED AFTER SWITCHING FUEL TANKS ADJUSTED POWER, ENGINE MANIFOLD PRESSURE DROPPED AND SURGED, PILOT NOTICED OIL ON TOP OF RT ENG COWL AND OIL PRESSURE LOW AND SURGING, RED...

Flight Controls BROKEN
2012-07-09

ON APPROACH PILOT SELECTED FULL FLAPS, HEARD LOUD POP AIRCRAFT WANTED TO ROLL RIGHT. CORRECTED WITH AILERON, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENCE. INSPECTED AIRCRAFT FOUND THAT A FLOOR PANEL CLIP NUT HAD BECOME CAUGHT IN FLAP DRIVE GEAR/...

Landing Gear BROKEN
2009-07-09

(CAN) RT MLG COLLAPSED DURING TURN TO LINE UP FOR TAKEOFF. PARTS FOUND FAILED AFTER COLLAPSE. ADJUSTING SCREW PN 0841113-3 FOUND SHEARED. BOLT ATTACHING BELLCRANK ASSY TO LANDING GEAR TRUNNION FOUND SHEARED. BOLT PN NAS464P4-26 FOUND SHEARED. MO...

Stabilizers BROKEN
2009-03-30

DURING RETURN FLIGHT, PILOTS NOTICED SLOPPY RUDDER CONTROL, THEY INVESTIGATED AND FOUND VERY LITTLE RUDDER INPUT FROM LT PEDAL ON BOTH PILOT AND CO-PILOTS SIDE. USING RUDDER TRIM FOUND THEY COULD CONTROL RUDDER. THEY FOUND CLOSEST AIRPORT ENROUTE W...

Fuselage DAMAGED
2005-12-15

CAPTAINS OUTBOARD RUDDER PEDAL MOUNT BLOCK INTERCOSTAL AT STN 118.55, REPAIRED DUE TO CRACKED.

Reciprocating Engine CRACKED
2005-07-12

CRACKED BETWEEN SPARK PLUG BOSS AND EXHAUST CYLINDER. TYPICAL OF THE CYLINDERS. (K)

Reciprocating Engine CRACKED
2005-07-12

RT ENGINE NR 5 CYLINDER. LOW COMPRESSION. (K)

Reciprocating Engine CRACKED
2005-06-10

CRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 3. (K)

Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.

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Prices and listings re-checked on a rolling cycle — most within a few days · Data: FAA Registry, NTSB · About our data
Disclaimer: All prices, cost estimates, and market values shown are based on asking prices from third-party sources and are provided for informational purposes only. AeroGurus is not an appraiser, broker, or financial advisor. Always obtain a professional appraisal and independent inspection before making a purchase decision. Actual transaction prices may differ from asking prices.