ARKUSZ DANYCH TECHNICZNYCH do Świadectwa Uznania Zdatności Nr UZ-BB-14/01 z dnia 06 września 2001
Piper PA-22 Tri-Pacer · Type Certificate
Overview
This document is a Type Certificate Data Sheet (TCDS) for the Piper PA-22-160, commonly known as the Tri-Pacer. Issued by the General Inspectorate of Civil Aviation in Poland, it outlines the airworthiness approval conditions and limitations for the aircraft. The TCDS serves as an official record of the aircraft's compliance with safety and operational standards as set by the Federal Aviation Administration (FAA). It includes critical specifications such as engine type, fuel requirements, weight limits, and seating capacity, which are essential for pilots and operators to ensure safe operation of the aircraft.
- Aircraft Model: Piper PA-22-160 (Tri-Pacer)
- Maximum Takeoff Weight: 2000 lbs
- Baggage Weight Limit: 100 lbs
- Engine: Lycoming O-320-B2A or O-320-B2B
- Fuel Requirement: Aviation gasoline min. 91/96 octane
- Maximum Engine Speed: 2700 RPM
- Seating Capacity: 4 persons
Document
Source
Originally published by www.ulc.gov.pl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Year
- 2001
- Pages
- 3
- File size
- 135 KB
- Publisher
- www.ulc.gov.pl
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the Piper PA-22 Tri-Pacer.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the PA-22 to your watchlist and track it in one place.
More Piper PA-22 Tri-Pacermanuals & documents
- FAA/PMA EXHAUST COMPONENTSSystems Description
- SERVICE BULLETIN NO. 1379AMaintenance Manual
- AAIB Bulletin: 2/2006 G-BTLM EW/G2005/11/01Other Documents
- Piper Aircraft Corporation Inspection ReportOther Documents
- SERVICE BULLETIN No. 924Service Bulletins
- Weight & Balance for the Piper PA-22 Tri-PacerWeight And Balance
- PIPER PA-22 Radio control modelAvionics Manual
- Pilot's Operating Handbook for the Piper PA-22 Tri-PacerPilot's Operating Handbook
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In this document
Aircraft Type and Manufacturer
The document specifies that the aircraft type is the Piper Model PA-22-160, also known as the Tri-Pacer. It is manufactured by Piper Aircraft Inc, located in Vero Beach, Florida.
Certification Basis
The certification is based on the American regulations CAR Part 3, effective from November 1, 1949, with amendments. The Type Certificate No 1A6 was issued by the FAA, confirming the aircraft's compliance with airworthiness standards.
Engine Specifications
The PA-22-160 is equipped with a Lycoming O-320-B2A or O-320-B2B engine. It requires aviation gasoline with a minimum octane rating of 91/96 and has a maximum engine speed limitation of 2700 RPM across all operational ranges.
Weight and Capacity
The maximum takeoff weight for the PA-22-160 is 2000 pounds, with a baggage weight limit of 100 pounds. The aircraft can accommodate up to four occupants.
Safety notes
- Ensure compliance with the specified fuel requirements to maintain engine performance.
- Adhere to weight limits to ensure safe operation of the aircraft.
Full document text
R ZEC ZPO SPO LIT A POLSKA REPUBLIC of PO L A N D Główny Inspektorat Lotnictwa Cywilnego General Inspectorate o f Civil Aviation Inspektorat Kontroli Cywilnych Statków Powietrznych Civil Aircraft Inspection Board CERTYFIKAT UZNANIA ZDATNOŚCI CERTIFICATE OF AIRWORTHINESS APPROVAL NUMER , , 7 BB-14/01 N u m b er Data zgłoszenia: Date o f Application: Data wydania: Date o f Issue: Uwagi: R em arks: 03.09.2001 GILC03 Główny Inspektor IKCSP Chief Inspector CAIB GŁÓWNY INSPEKTORAT LOTNICTWA CYWILNEGO INSPEKTORAT KONTROLI CYWILNYCH STATKÓW POWIETRZNYCH Piper Aircraft Model PA-22-160 Wydanie 1 06 września 2001 ARKUSZ DANYCH TECHNICZNYCH do Świadectwa Uznania Zdatności Nr UZ-BB-14/01 z dnia 06 września 2001 Niniejszy Arkusz Danych Technicznych jest częścią składową Świadectwa Uznania Zdatno ści Nr UZ-BB-14/01 z dnia 06 września 2001 i podaje warunki oraz ograniczenia, przy jakich sprzęt lotniczy, dla którego wydano ten dokument, spełnia wymagania zdatności do lotu. 1. Typ samolotu: Piper Model PA-22-160 ( Tri Pacer ) 2. Wytwórca: Piper Aircraft Inc, 2926 Piper Drive; Vero Beach; Florida 32960, USA 3. Podstawa certyfikacji: Przepisy amerykańskie CAR Part 3 wydanie z 01 listopada 1949 z Po prawkami od 3 -Ido 3-6 4. Podstawa wydania świadectwa: Świadectwo Typu Nr 1A6 (Type Certificate 1A6) wydane przez Federal Aviation Administration i Arkusz Danych do Świadectwa Typu Nr 1A6 (Type Certificate Data Sheet No 1A6), Wydanie 33 z 12 lutego 1999. 5. Kategoria: Normalna ARKUSZ DANYCH TECHNICZNYCH do Orzeczenia Uznania Zdatności UZ-BB-14/01 z dnia 06 września 2001 Strona 2 ó.Silnik: Paliwo Lycoming 0-320-B2A lub 0-320-B2B2 benzyna lotnicza min. 91/96 Ograniczenia 2700 obr./min. dla całego zakresu użytkowania 7.Śmigło Sensenich M74DM metalowe o stałym skoku 8.Ciężar maks. 2000 fantów 9.Ciężar bagażu 100 funtów lO.Ilość miejsc 4 Uwaga:Pozostałe ograniczenia i inne dane eksploatacyjne zawiera TCDS No 1A6 oraz Inst rukcja Użytkowania w Locie samolotu KONIEC
What's in the Piper PA-22 Tri-Pacer TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.