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PIPER Aztec PA-23-250 Model Guide

PIPER Aztec PA-23-250 · Model Guide

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Overview

The PIPER Aztec PA-23-250 is a six-place, twin-engine piston airplane with two 250 hp Lycoming engines. The figures here come mainly from the Aztec "E" operating manual and checklist. They cover a normally aspirated version and a turbocharged version. Check any airplane against its own flight manual and weight and balance report.

  • The Aztec E comes normally aspirated (IO-540-C4B5) or turbocharged (TIO-540-C1A). Both are rated 250 hp per engine, with a 5200 lb gross weight.
  • Standard useful load is 2158 lbs normally aspirated and 1971 lbs turbocharged. Fuel capacity is 144 gal, of which 140 gal is usable.
  • Published cruise is up to 210 mph at 4,000 ft normally aspirated, or up to 245 mph at 22,000 ft turbocharged.
  • Check the records for SB 540B (stabilator tip tubes, Aztec F) and SB 1022 (induction air filter).

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
51 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Engine power (hp)
·
250
Usable fuel (gal)
·
140
Useful load (lb)
·
2,158
Empty weight (lb)
·
3,042
Max fuel capacity (gal)
·
144
Max landing weight (lb)
·
4,940
Max takeoff weight (lb)
·
5,200

Performance

Landing roll (ft)
·
850
Best rate of climb (fpm)
·
1,490
Takeoff ground roll (ft)
·
820
Accelerate stop distance (ft)
·
2,220
Normal cruise fuel burn (gph)
·
34
Landing distance over 50ft (ft)
·
1,620
Takeoff distance over 50ft (ft)
·
1,250
Single engine rate of climb (fpm)
·
240

V-speeds

VA_MPH
·
149
VX_MPH
·
107
VY_MPH
·
120
VNE_MPH
·
249
VNO_MPH
·
198
VYSE_MPH
·
102
VLO_LE_MPH
·
150
VFE_FULL_FLAPS_MPH
·
125

Weight & balance

Useful load (lb)
·
2,158
Fuel capacity (gal)
·
144
Max gross weight (lb)
·
5,200
Max landing weight (lb)
·
4,940
Max zero fuel weight (lb)
·
4,400
Standard empty weight (lb)
·
3,042
About this document
What is the useful load of the PIPER Aztec PA-23-250?

For the PIPER Aztec PA-23-250 Model E, the standard useful load is 2158 lbs normally aspirated and 1971 lbs turbocharged. Gross weight is 5200 lbs. Your airplane's own weight and balance report governs.

How fast and how far does the PIPER Aztec PA-23-250 go?

The PIPER Aztec PA-23-250 normally aspirated cruises at up to 210 mph at 4,000 ft and 34.0 gph, with a published no-reserve range of 830 miles. The turbocharged version cruises at up to 245 mph at 22,000 ft with a range of 1050 miles.

What known inspections apply to the PIPER Aztec PA-23-250?

For the PIPER Aztec PA-23-250, SB 540B requires stabilator tip tube inspections on Aztec F serials 27-7654001 to 27-7954121, repeated every 100 hours. SB 1022 covers the induction air filter on serials 27-01 through 27-2504.

What is the PIPER Aztec PA-23-250 Model Guide?

The PIPER Aztec PA-23-250 Model Guide is a model guide for the PIPER Aztec PA-23-250, dated 2026.

What year was the PIPER Aztec PA-23-250 Model Guide published?

The PIPER Aztec PA-23-250 Model Guide — the PIPER Aztec PA-23-250 model guide on file — is dated 2026.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the PIPER Aztec PA-23-250.

More PIPER Aztec PA-23-250manuals & documents

In this document

Performance (Aztec E, gross weight, sea level)

Takeoff run is 820 ft and distance over a 50-ft barrier is 1250 ft. Accelerate-stop is 2220 ft. Landing roll is 850 ft and landing over 50 ft is 1620 ft. Best rate of climb is 1490 fpm normally aspirated and 1530 fpm turbocharged. Single-engine rate of climb is 240 fpm normally aspirated and 265 fpm turbocharged.

Weights, fuel and engines

Maximum gross weight is 5200 lbs and maximum landing weight is 4940 lbs. Standard empty weight is 3042 lbs normally aspirated and 3229 lbs turbocharged. The normally aspirated engine uses 91/96 minimum octane fuel; the turbocharged engine uses 100/130. Each engine holds 12 qts of oil. Normal cruise burns 34.0 gph normally aspirated and 32.6 gph turbocharged.

What to check when buying

Piper built several six-place Aztec series (B, C, D, E, F), and the service manual lists the serial ranges. Confirm the exact model and serial number, then match it to the manual. The Piper service bulletin index and FAA airworthiness directive listings should be reviewed for open items. Avionics and autopilot parts are not listed in the parts catalog for later serial numbers.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Safety notes

  • SB 540B: stabilator tip tube and weight cracks on Aztec F serials 27-7654001 to 27-7954121. Recurring inspection at no more than 100 hours. Cracks must be repaired before the next flight.
  • SB 1022: inspect the FACET induction air filter (Piper P/N 460-632) before the next flight. Replace within 25 hours if required, and look for debris if plastic has crumbled.
  • Minimum controllable single-engine speed is 80 mph. Best single-engine rate of climb speed is 102 mph (IAS).

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

PIPER Aztec PA-23-250 Model Guide The PIPER Aztec PA-23-250 is a six-place, twin-engine piston airplane with two 250 hp Lycoming engines. The figures here come mainly from the Aztec "E" operating manual and checklist. They cover a normally aspirated version and a turbocharged version. Check any airplane against its own flight manual and weight and balance report. • The Aztec E comes normally aspirated (IO-540-C4B5) or turbocharged (TIO-540-C1A). Both are rated 250 hp per engine, with a 5200 lb gross weight. • Standard useful load is 2158 lbs normally aspirated and 1971 lbs turbocharged. Fuel capacity is 144 gal, of which 140 gal is usable. • Published cruise is up to 210 mph at 4,000 ft normally aspirated, or up to 245 mph at 22,000 ft turbocharged. • Check the records for SB 540B (stabilator tip tubes, Aztec F) and SB 1022 (induction air filter). Performance (Aztec E, gross weight, sea level) Takeoff run is 820 ft and distance over a 50-ft barrier is 1250 ft. Accelerate-stop is 2220 ft. Landing roll is 850 ft and landing over 50 ft is 1620 ft. Best rate of climb is 1490 fpm normally aspirated and 1530 fpm turbocharged. Single-engine rate of climb is 240 fpm normally aspirated and 265 fpm turbocharged. Weights, fuel and engines Maximum gross weight is 5200 lbs and maximum landing weight is 4940 lbs. Standard empty weight is 3042 lbs normally aspirated and 3229 lbs turbocharged. The normally aspirated engine uses 91/96 minimum octane fuel; the turbocharged engine uses 100/130. Each engine holds 12 qts of oil. Normal cruise burns 34.0 gph normally aspirated and 32.6 gph turbocharged. What to check when buying Piper built several six-place Aztec series (B, C, D, E, F), and the service manual lists the serial ranges. Confirm the exact model and serial number, then match it to the manual. The Piper service bulletin index and FAA airworthiness directive listings should be reviewed for open items. Avionics and autopilot parts are not listed in the parts catalog for later serial numbers. Safety notes: • SB 540B: stabilator tip tube and weight cracks on Aztec F serials 27-7654001 to 27-7954121. Recurring inspection at no more than 100 hours. Cracks must be repaired before the next flight. • SB 1022: inspect the FACET induction air filter (Piper P/N 460-632) before the next flight. Replace within 25 hours if required, and look for debris if plastic has crumbled. • Minimum controllable single-engine speed is 80 mph. Best single-engine rate of climb speed is 102 mph (IAS).