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Piper · 1976–1978

Piper Lance (1976-1978)

piperlanceretractablelow-wingsix-seatcross-countryhaulerComplex300hpcherokee-six-airframe

Specifications

Performance

Cruise

155KTAS

Range

900nm

Climb

1000fpm

Ceiling

14,600ft

Fuel Burn

15.5gph

Fuel Cap.

94gal

MPG

11.5mpg

Stall (Vs0)

55KIAS

T/O roll

960ft

Ldg roll

720ft

Size & weight

Seats

6

Useful Load

1620lbs

Full-fuel payload

1,056lbs

Max gross

3,600lbs

Wingspan

32.8ft

Length

27.7ft

Engine

Engine

Lycoming IO-540-K1G5D

Power

300hp

TBO

2,000hrs

Overhaul

$52k

Owning it

Hull insurance

$2k/yr

Parts

good

Mechanics

common

Gear

Retractable

IFR

Yes

Category

certified

Full specification

V-speeds

Vne188 KIAS
Vno149 KIAS
Va109 KIAS
Vs167 KIAS
Vx78 KIAS
Vy96 KIAS
Best glide105 KIAS

Airframe

Empty weight
1,980 lbs
Max fuel weight
564 lbs
Height
7.9 ft
Wing position
low

Obstacle performance

Takeoff over 50 ft
1,660 ft
Landing over 50 ft
1,490 ft

Paperwork

Type certificate
A3SO
Certification basis
CAR 3

These figures are typical for the model, not a specification for any individual aircraft. Real-world numbers vary with year, installed equipment, weight, modifications and engine condition — often by more than you would expect. Use them to compare types, and confirm anything you would act on against the Pilot's Operating Handbook for that specific airframe and a prebuy inspection.

Pricing

Typical

$145k

Range

$105k – $195k

Annual all-in

~$31k/yr

All-in at ~100 flying hours a year, using the midpoint of each range — the same figures broken out under “Cost to own” below. Your number will differ, and mostly for two reasons. Experience sets your insurance: a 2,000-hour pilot with recent training pays 30–40% less than a 200-hour owner, and student owners pay 20–40% more — on the same aircraft that is often a doubling. Location sets your hangar: a T-hangar runs $200–400 a month in the Midwest against $400–1,500 in a coastal metro, and an outside tie-down is less again. Engine reserves move too — a local shop reusing your serviceable cylinders can come in 30–50% under the national specialty-shop pricing we quote, though you trade the warranty and turnaround that comes with it. Reserves are money set aside toward a future overhaul, not a bill this year, and the annual inspection figure is the shop’s labor to look — whatever they find is separate.

Cost to own — estimate

Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel, maintenance and the engine reserve do.

100
20300
$6.50
$3$10
Fuel (15.5 gph)
$10,075
Engine reserve
$2,600
Propeller reserve
$175
Maintenance, parts & wear items ($22/hr)
$2,200
Insurance
$2,400–$4,850
Hangar
$5,451–$13,628
Annual inspection (labor only)
$2,500
Databases & subscriptions
$700
Total per year
$31,415
Per flight hour
$314
Miles flown / year (at cruise)
17,837 mi
Cost per mile
$1.76/mi
300 nm
100 nm1,000 nm
Time in the air
1 hr 56 min
Fuel burned
30 gal
Out of pocket
$291

Fuel, engine reserve and wear only. Insurance, hangar and the annual are already paid whether you make the trip or not, so they are not charged here.

Estimate, not a quote. Where a line shows a range, the total, per-hour and per-mile figures use its midpoint— insurance moves most with your experience and time in type, hangar with where you base the aircraft, so your own number could sit at either end. Annual inspection is the shop's labor to open and inspect — what they find is the maintenance line, which covers oil changes, plugs, tires, brakes, hoses, lights, a battery and vacuum pump amortised over their life, and the unscheduled squawks that are the largest and least predictable part of it. Reserves are sinking funds toward an overhaul, not a bill you pay this year — and note that a propeller is due on hours or calendar time, typically six years, so flying less does not put it off forever.

Title & Escrow partnerExample placement

Strengths

    Weaknesses

      Overview

      The 1976 Piper PA-32R-300 Lance is the first retractable-gear Cherokee Six -- the Cherokee Six 300 airframe with retractable landing gear, providing 6-seat cabin and 1,620 lb useful load with cruise speed approaching the smaller A36 Bonanza. Production: approximately 1,200 units across 1976-1979.

      The Lance line evolved through two distinct variants:

      • Lance (1976-1977): Standard conventional tail, PA-32R-300
      • Lance II (1978-1979): Distinctive T-tail variant, PA-32RT-300

      In 1980 the Lance was renamed the Saratoga SP with a new tapered wing and conventional tail, ending the brief Lance era.

      The T-Tail Controversy

      The 1978-1979 Lance II's T-tail generated significant pilot debate:

      • T-tail aesthetic was distinctive (popular at the time for new-design singles)
      • Aerodynamically refined (claimed +3 KTAS cruise)
      • BUT: Reduced pitch authority at low speeds
      • Lance II is sensitive to weight aft of CG limit
      • T-tail combined with rear loading on Six fuselage created marginal handling

      Piper returned to a conventional tail with the 1980 Saratoga SP, citing pilot feedback. Lance IIs (T-tail) command lower prices than equivalent Lance (conventional tail) examples.

      Performance

      Representative Lance (PA-32R-300, IO-540-K1G5D 300 HP):

      • Cruise: 155 KTAS at 7,500 ft (75% power)
      • Climb: 1,000 FPM at gross
      • Fuel burn: 15.5 GPH cruise
      • Range: 900 NM with reserves at 94 gal fuel
      • Useful load: 1,620 lbs (excellent for 6-seat retractable)

      The Lance's 1,620 lb useful load is meaningfully better than the equivalent A36 Bonanza (1,200 lbs) at lower acquisition cost. Trade-offs: 15 KTAS slower cruise and shorter range.

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      Valuation Factors

      VariantConditionPrice Range
      Lance (1976-1977, conventional tail)Well-maintained$120,000-$185,000
      Lance II (1978-1979, T-tail)Well-maintained$105,000-$165,000

      T-tail Lance II discount reflects market preference for conventional tail. Conversion of T-tail Lance II to conventional tail is not available -- structural modification is impractical.

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      ADs & Common Problems

      Universal PA-32 concerns plus Lance-specific:

      1. T-tail elevator authority (Lance II): Verify rigging and elevator condition; T-tail elevator wear is harder to detect.
      2. Lycoming IO-540 cylinder condition: Borescope all 6 cylinders.
      3. Retractable gear hydraulics: Inspect gear motor, hydraulic pump, and gear doors.
      4. Spar AD compliance (AD 2020-26-16): Inspect main spar.
      5. W&B documentation: Lance is sensitive to aft CG loading; verify current W&B is accurate.

      For sale (0)

      No listings for this model right now.

      What buyers usually weigh against the Piper Lance (1976-1978) — aircraft flown for the same kind of mission.