1983 Cessna 172P
Single Engine Piston
Aircraft Details
Seller reportedDescription
1983 Cessna 172P (TAA)(Full Glass Panel)(Autopilot) Full Glass Panel (Installed April 2023) -DYNON SKYVIEW HDX PFD and MFD -DYNON SKYVIEW FULL AXIS AUTOPILOT -GTN 750XI -GSB 15 Charging Ports Extended Range Tanks 784.2 Useful Load Plush Leather Inteiror Recent FULL IFR Pitot Static Inspection (Due March 2028) Recent Annual (Due April 1rst 2027) Long History of Oil Anaysis Beuatiful Polished Prop Engine (O-320-D2J) -TSMOH 1,755.1 -TT 9,739.1 -Sep 2012 Engine MOH Long History of 100 Hour Inspections and 50 Hour Oil Changes
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 |
|---|---|---|---|---|---|---|
|
Jono Kloster
trade-a-plane.com
|
$195,000
|
Jacksonville, FL | Jun 02, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 172P
This 1983 Cessna 172P (N86ER) is a 4-seat single engine piston with 9,739 hours on the airframe. There are currently 13 172P aircraft listed for sale with asking prices ranging from $85,500 to $324,900. This aircraft is priced above the market average at $195,000.
The 172P cruises at 122 kts (226 km/h) with a range of 640 nm (1,185 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 8.5 GPH (32 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $47/hr in fuel alone. Total variable cost including maintenance reserves is approximately $110/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $16,000. With 9,739 hours on the airframe, this aircraft has exceeded TBO (2,000 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 1 airworthiness directive 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 172P — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 172P
AeroGurus estimates based on industry averages for the CESSNA 172P. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N86ER.
Location & Ownership
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 N86ER against the NTSB accident database.
Airworthiness Directives — Cessna 172P
ADs are mandatory safety instructions issued by the FAA. 1 recent AD found for this aircraft type.
Cessna Aircraft Company Models 172N, 172P, R172K, 172RG, F172N, F172P, FR172J, and FR172K Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 172P
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
NR 4 CYLINDER HEAD CRACKED ACROSS COOLING FINS IN FLIGHT. CREW NOTICED LOSS OF POWER/SHUDDER.
CAM GEAR WAS IMPROPERLY INSTALLED/SEATED DURING INITIAL MANUFACTURING WHICH CAUSED EXCESSIVE WEAR AND DAMAGE TO THE CAM GEAR DURING ROTATION AGAINST THE DISTRIBUTOR GEAR. THIS WAS THE FIRST 500HR INSPECTION SINCE MANUFACTURE.
AMMETER SHOWING DISCHARGE, NO VOLTAGE TO FIELD.
ELT FOUND INOPERATIVE DURING INSPECTION.
FLAPS FAILURE ON FINAL. LOOKED TO THE FLAPS AND SAW RIGHT FLAP FULL DOWN WITH LEFT FLAP FULL UP. RAISED THE FLAP LEVER TO 0 AND RIGHT FLAP WENT FULL UP. LANDED WITH NO FLAPS.
DISPLAY LIGHTS UNREADABLE.
UNKNOWN, TIRE LOST AIR FOR UNKNOWN REASONS.
RIGHT FUEL TANK, 5" CRACK ALONG THE REAR OF THE FUEL FILLER NECK ATTACHMENT WELD
RIGHT FUEL TANK, 6" CRACK ALONG REAR OF FILLER NECK ATTACHMENT WELD
ON AUGUST 23, 2022 AN ENGINE EXAMINATION WAS CONDUCTED AT AIR SALVAGE OF DALLAS UNDER FAA OVERSIGHT. A GVI ON THE NUMBER 1 CYLINDER FOUND 4 SMALLER DIAMETER STUDS AND 1 LARGER DIAMETER STUD FRACTURED. THESE DECK STUD BOLTS EXHIBITED FATIGUE FAILURE/I...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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