# TCDS A9SO: Piper Aircraft Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Piper Aircraft Inc.
- Revision: 10
- Revised: August 7, 2006
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheet PDF: https://openairdocs.org/files/sha256/4a/83/4a83fea645ff53968768d9860de56558f6e8ca90ac1b1193a2c394f1e0eeffaa
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A2851E78D87B4E28625720A0054A474.0001
- Page: https://openairdocs.org/tcds/A9SO

## Models (3)

As the data sheet lists them.

- PA-36-300
- PA-36-375
- PA-36-285

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
A9SO 
Revision 10 
Piper Aircraft, Inc 
 
PA-36-285 
PA-36-300 
PA-36-375 
 
August 7, 2006 
TYPE CERTIFICATE DATA SHEET A9SO 
 
This data sheet which is a part of Type Certificate No. A9SO, prescribes conditions and limitations under which the product for 
which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. 
 
Type Certificate Holder Piper Aircraft, Inc. 
 2926 Piper Drive 
 Vero Beach, Florida  32960 
 
Type Certificate Holder Record The new Piper Aircraft, Inc transferred TC A9SO to Piper Aircraft, Inc on August 7, 
2006. 
 
I. - Model PA-36-285,   1 PCLM (Normal Category),   Approved May 31, 1972. 
Engine 1 Teledyne Continental 6-285-B or 6-285-C with CMC injector with fuel flow schedule 
per curve No. 71-12, or 
 1 Teledyne Continental 6-285-BA or 6-285-CA    (See NOTE 9 for -BA and -CA engines) 
with CMC injector with fuel flow schedule per curve No. 77041.  Propeller drive ratio to 
crankshaft 0.500:1. 
 
Fuel 100/130 minimum grade aviation gasoline 
 
Engine Limits For all operations, 4000 r.p.m.    (2000 propeller r.p.m.)     (285 hp) 
 
Propeller and Propeller Limits 1 Hartzell, Hub Model HC-C2YF-1 ( )F, Blade Model F9587A 
 Pitch Setting: High 27° to 29°, Low 18° ± 0.2° at 30" station. 
 Diameter: Not over 95", not under 93". 
    No further reduction permitted. 
 Spinner:  Hartzell A4203 Spinner Assembly is required. 
 Propeller Governor:  Hartzell Model F-4-6A 
      OR 
 1 Hartzell, Hub Model HC-C3YF-1 ( )F, Blade Model F9684-1 
 Pitch Setting: High 29° to 31 °, Low 16.3° to 16.5° at 30" station. 
 Diameter: Not over 95", not under 93". 
    No further reduction permitted. 
 Spinner:  Hartzell A4203-1    (See NOTE 5 for data on spinner.) 
 Propeller Governor:  Hartzell Model F-4-6A 
 
Propeller Limitations Hartzell Model HC-C2YF-1 ( )F only. 
 Avoid continuous operation on the ground between 950 and 1150 propeller r.p.m. in 
wind above 15 mph. 
 
Airspeed Limits (CAS) Vne Never exceed 182 mph (158 knots) 
 Vno Maximum structural cruising 150 mph (130 knots) 
 Vp Maneuvering 136 mph (118 knots) 
 Vfe Flaps Extended 115 mph (100 knots) 
Page No. 1 2 3 4 5 6 7 
Rev. No. 9 9 9 9 9 9 9

A9SO Page 2 of 7 
 
 
Center of Gravity Range (+137.25)   at 3000 lb. or less 
 (+139.00) to (+143.20) at 3900 lb. 
 (+146.35)  at 2600 lb. or less 
 Straight line variation between points given. 
 
3900
3600
3200
2800
2400
LB.
136 140 144 148
FUSELAGE STATION - INCH
NORMAL
CATEGORY
137. 25 139.00 143. 20 146. 35
 
Empty Weight C.G. Range None 
 
Maximum Weight  3900 lb. 
 
No. of Seats 1 (+196.0) 
 
Maximum Baggage None 
 
Fuel Capacity 89 gallons at (+138.4) (2 wing tanks) (87 gallons usable) 
 See NOTE 1 for data on unusable fuel. 
 
Oil Capacity 9 quarts (5 quarts usable) 
 See NOTE 1 for data on system oil. 
 
Manufacturer's Serial Numbers 36-7360001 through 36-7660135    (See NOTE 6 for airworthiness certification 
eligibility in the United States) 
 
 
II. - Model PA-36-300,   1 PCLM (Normal Category),   Approved November 22, 1974. 
 Same as Model PA-36-285 except engine installation. 
 
Engine 1 Lycoming IO-540-K1G5 with one 5th order and one 6th order pendulum damper. 
 
Fuel 100/130 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2700 r.p.m.    (300 hp)

Page 3 of 7 A9SO 
 
 
Propeller and Propeller Limits 1 Hartzell, Hub Model HC-C2YF-1 ( )F, Blade Model F8475R 
 Pitch Setting: High 29° ± 1°, Low 12.0° ± 0.2° at 30" station. 
 Diameter: Not over 84", not under 82.3". 
    No further reduction permitted. 
 Spinner:  Piper Drawing 99374  (See NOTE 5 for data on spinner.) 
 Propeller Governor:  Hartzell Model F-4-11A 
     OR 
 1 Hartzell, Hub Model HC-C3YR-1 ( )F, Blade Model F8468A-6 
 Pitch Setting:  High 26° ± 1°, Low 11.8° ± 0.2° at 30" station. 
 Diameter: Not over 80", not under 78". 
    No further reduction permitted. 
 Spinner:  Hartzell 835-36  (See NOTE 5 for data on spinner.) 
 Propeller Governor:  Hartzell Model F-4-11A 
 
Airspeed Limits Vne Never exceed 182 mph CAS,   177 m.p.h. IAS 
 Vno Maximum structural cruising 150 mph CAS,   146 m.p.h. IAS 
 Vp Maneuvering 136 mph CAS,   132 m.p.h. IAS 
 Vfe Flaps Extended 115 mph CAS,   116 m.p.h. IAS 
 
Center of Gravity Range (+137.25)  at 3000 lb. or less 
 (+139.00) to (+143.20) at 3900 lb. 
 (+146.35)   at 2600 lb. or less 
 Straight line variation between points given. 
 
3900
3600
3200
2800
2400
LB.
136 140 144 148
FUSELAGE STATION - INCH
NORMAL
CATEGORY
137. 25 139. 00 143. 20 146. 35
 
 
Empty Weight C.G. Range None 
 
Maximum Weight 3900 lb. 
 
No. of Seats 1 (+196.0) 
 
Maximum Baggage None 
 
Fuel Capacity 89 gallons at (+138.4) (2 wing tanks) (87 gallons usable) 
 See NOTE 1 for data on unusable fuel. 
 
Oil Capacity 12 quarts  (9¼ quarts usable) 
 See NOTE 1 for data on system oil.

A9SO Page 4 of 7 
 
 
Manufacturer's Serial Numbers 36-7560001 through 36-8160023  (See NOTE 6 for airworthiness certification eligibility 
in the United States). 
 
 
III. - Model PA-36-375,   1 PCLM (Normal Category),   Approved October 4, 1977. 
 
Engine 1 Lycoming IO-720-D1CD or IO-720-D1C with one 3.5 order, six 4th order and one 5th 
order pendulum damper. 
 
Fuel 100/130 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2500 r.p.m.  (375 hp) 
 
Propeller and Propeller Limits 1 Hartzell , Hub Model HC-C3YR-1 ( )F, Blade Model F8475R 
 Pitch Setting: High 27° ± 1°, Low 13.3° ± 0.2° at 30" station. 
 Diameter: Not over 86", not under 84". 
    No further reduction permitted. 
 Spinner:  Hartzell 835-36    (See NOTE 5 for data on spinner.) 
 Propeller Governor:  Hartzell Model F-4-23 
 
Airspeed Limits Vne Never exceed 189 mph CAS, 184 mph IAS 
 Vno Maximum structural cruising 150 mph CAS, 147 mph IAS 
 Vp Maneuvering 136 mph CAS, 134 mph IAS 
 Vfe Flaps Extended 120 mph CAS, 121 mph IAS 
 
Center of Gravity Range (+139.00)  at 3900 lb. or less 
 (+139.00) to (+143.20) at 3900 lb. 
 (+146.00)  at 2740 lb. or less 
 Straight line variation between points given. 
 
 
3900
3600
3200
2800
2400
LB.
136 140 144 148
FUSELAGE STATION - INCH
NORMAL
CATEGORY
139. 00 143 .20 146. 35
 
Empty Weight C.G . Range None 
 
Maximum Weight 3900 lb. 
 
No. of Seats 1 (+196.0) 
 
Maximum Baggage None

Page 5 of 7 A9SO 
 
Fuel Capacity 89 gallons at (+138.4) (2 wing tanks) (87 gallons usable)   
 See NOTE 1 for data on unusable fuel. 
 
Oil Capacity 17 quarts  (14 quarts usable) 
 See NOTE 1 for data on system oil. 
 
Manufacturer's Serial Numbers 36-7802001 through 36-8302025  (See NOTE 6 for airworthiness certification eligibility in 
the United States). 
 
 
DATA PERTINENT TO ALL MODELS 
Datum 126.0 inches forward of the wing leading edge at the intersection of the straight and 
tapered section. 
 
Leveling Means Two screws right side fuselage, inside below window. 
 
Control Surface Movements Aileron (± 1°) Up 20° Down 17° 
 Elevator (± 1°) Up 30° Down 20° 
 Elevator Tabs (+3°, -1°) Up 15.5° Down 22.5°    Elevator Neutral 
 Rudder (± 1°) Left 25° Right 25° 
 Flaps (± 1°) Up 0° Down 30°    for PA-36-285 and PA-36-300
  (± 1°) Up 0° Down 20°    for PA-36-375 
 
 See NOTE 7 for flap travel restriction. 
 
Certification Basis FAR Part 23, effective February 1, 1965;  and including Amendments 23-1 through 23-6 
 dated August 1, 1967. 
 
 Application for Type Certificate dated April 30, 1969. 
 Type Certificate issued May 31, 1972.  Obtained by the manufacturer under delegation option 
procedures. 
 
Production Basis Approved for manufacture of spare part s only under Production Certificate No. 206. 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see 
certification basis) must be installed in the aircraft for certification.  In addition, the following 
items of equipment are required: 
 
 1. VB-645 approved August 19, 1974, for Model PA-36-285, S/N 36-7360001 through 
   36-7460041. 
 
 2. VB-682 approved January 31, 1975, for Model PA-36-285, S/N 36-7560001 through 
   36-7660135. 
 
 3. Piper Report 2032 issued November 22, 1974, and Piper Report 2035 issued November 20, 
   1974, for Model PA-36-300, S/N 36-7560001 through 36-8160023. 
 
 4. Piper Report 2114 issued October 11, 1977,  and Piper Report 2115 issued October 11,  
   1977, for Model PA-36-375, S/N 36-7802001 through 36-8302025.

A9SO Page 6 of 7 
 
NOTE 1 Current Weight and Balance Report, including list of  equipment included in certificated empty weight and 
loading instructions when necessary, must be provided for each aircraft at the time of original certification. 
 
 The certificated empty weight and corresponding center of gravity locations must include undrainable system 
oil (not included in oil capacity) and unusable fuel as noted below: 
 
 PA-36-285:
  Fuel:   12.0 lb.   at   +138.4 
  Oil:     7.5 lb.    at   +87.0 
 PA-36-300:
  Fuel:    18.0 lb.  at   +138.4 
  Oil:     3.5 lb.    at   +88.5 
 PA-36-375:
  Fuel:    18.0 lb.  at   +138.4 
  Oil:     3.5 lb.    at   +90.5 
 
NOTE 2 All placards required in the approved Airplane Flight Manual and approved Airplane Flight Manual 
Supplements must be installed in the appropriate locations. 
 
NOTE 3 The PA-36-285 engine installation consists of th e basic Teledyne Continental Motors Model 6-285-B,  
 6-285-BA, 6-285-C, or 6-285-CA engine with Teledyne Continental Customer Specifications No. 2. 
 
NOTE 4 Model PA-36-285, S/N 36-7360001 through 36-7460041 are e ligible for multiple airworthiness certification 
in the Restricted and Normal Categories in accordance with FAR 21.187.  Conversion between categories 
may be accomplished in accordance with Piper Report VB-592. 
 
NOTE 5 PA-36-285 aircraft may be operated with Hartze ll A4201-1 spinner dome removed.  Spinner backup plate 
must remain installed. 
 
 PA-36-300 two-blade propeller aircraft may be operated with spinner dome and forward bulkhead removed.  
Piper aft bulkhead P/N 67791 is required for flight. 
 
 PA-36-300 three-blade propeller aircraft may be operated with spinner dome and filler plates removed.  
Hartzell aft bulkhead P/N C-885-3 is required for flight. 
 
 PA-36-375 three-blade propeller aircraft may be operated with spinner dome and filler plate removed.  
Hartzell aft bulkhead P/N C-885-3 or P/N C-4549 is required for flight. 
 
NOTE 6 The following serial numbered aircraft are not  eligible for import certification to the U.S.: 
 
 Model PA-36-285:
 36-7360050, 36-7460011, 36-7460012, 36-7460013, 36-7460014, 36-7460015, 36-7560088, 36-7660085,  
 36-7660088, 36-7660091, and 36-7660094. 
 
 Model PA-36-300:
 36-7760018, 36-7760034, 36-7760047, 36-7760051, 36-7760055, 36-7760120, 36-7760121, 36-7760123,  
 36-7760125, 36-7760129, 36-7760132, 36-7860010, 36-7860011, 36-7860012, 36-7860043, 36-7860045,  
 36-7860047, 36-7860049, 36-7860050, 36-7860051, 36-7860069, 36-7860071, 36-7860073, 36-7860089,  
 36-7860090, 36-7860091, 36-7860092, 36-7860093, 36-7860094, 36-7860095, 36-7860096, 36-7860097,  
 36-7860098, 36-7860102, 36-7860103, 36-7860104, 36-7860105, 36-7860109, 36-7860111, 36-7860112,  
 36-7860122, 36-7860123, 36-7960001, 36-7960007, 36-7960008, 36-7960009, 36-7960010, 36-7960011,  
 36-7960012, 36-7960013, 36-7960014, 36-7960015, 36-7960016, 36-7960017, 36-7960018, 36-7960019,  
 36-8060002, 36-8060003, 36-8060007, 36-8060010, 36-8060015, 36-8060020, 36-8060021, 36-8060022, 
and 36-8060023. 
 
 Model PA-36-375:
 36-7802034, 36-7802050, 36-7802061, 36-7802062, 36-7802063, 36-7802074, 36-7902001, 36-7902002,  
 36-7902003, 36-7902020, 36-7902022, 36-7902024, 36-7902033, 36-7902035, 36-7902037, 36-7902048,  
 36-7902049, 36-7902050, 36-7902051, 36-8002005, 36-8002006, 36-8002011, 36-8002013, 36-8002016,  
 36-8002018, and 36-8002025.

Page 7 of 7 A9SO 
 
NOTE 7 Wing flap travel on Models PA-36-285 and PA-36-300, S/N 36-7360001 through 36-7460041, is  
 0° (± 1°) Up, and 20° (± 1°) Down. 
 
NOTE 8 The following life limits are required: 
 
 For all PA-36 models:
 The wing main spar lower attachment bolts, Piper P/N 77245-00, must be replaced upon the accumulation of 
 2000 hours time-in-service (TIS) and every 2000 hours TIS thereafter (Ref. Piper Service Bulletin No. 501). 
 The wing main spar upper attachment bolts, Piper P/N 77245-00, must be replaced upon the accumulation of 
4100 hours TIS and every 4100 hours TIS thereafter (Reference Piper Service Bulletin 744). 
 The wing carry-through spar fittings, Piper P/N 97713-00, 97713-02 or 97713-03, must be replaced upon the 
accumulation of 4100 hours TIS and every 4100 hours TIS thereafter with P/N 97713-03 (Reference Piper 
Service Bulletin 744). 
 The wing spar fittings, Piper P/N 97712-00, must be replaced upon the accumulation of 4100 hours TIS and 
every 4100 hours TIS thereafter (Reference Piper Service Bulletin 744). 
 
 For Models PA-36-285 and PA-36-300, S/N 36-7360001 through 36-7560003 and 36-7660123 through  
 36-8160023, and Model PA-36-375, S/N 36-7802001 through 36-8302025:
 The spar carry-through assembly, Piper P/N 97370-00 or P/N 76824-02, as applicable, must be replaced 
upon the accumulation of 4100 hours TIS and every 4100 hours TIS thereafter with P/N 76824-02 
(Reference Piper Service Bulletins 552 and 744). 
 
 For Models PA-36-285 and PA-36-300, S/N 36-7560056 through 36-8160023 and Model PA-36-375, S/N 
 36-7802001 through 36-8302025:
 The spar assembly, Piper P/N 97701-00 (Rev. P) and P/N 97701-01 (Rev. P) must be replaced with Piper Kit 
764 393, left spar assembly, and Kit 764 394, right spar assembly, upon the accumulation of 4100 hours TIS 
and every 4100 hours TIS thereafter (Reference Piper Service Bulletin 744). 
 
 For Models PA-36-285 and PA-36-300, S/N 36-7560004 through 36-7660122:
 The spar carry-through assembly, Piper P/N 76767-00 must be replaced upon the accumulation of 4000 hours 
TIS with Piper P/N 76824-02;  and P/N 76824-02 must be repalced every 4100 hours TIS thereafter 
(Reference Piper Service Bulletin 744). 
 
 For Models PA-36-285 and PA-36-300, S/N 36-7360001 through 36-7560055:
 The spar assemblies, Piper P/N 97701-00 (Rev. N or earlier) and P/N 97701-01 (Rev. N or earlier) must be 
replaced upon the accumulation of 3100 hours TIS with Piper Kit 764 393 (left spar assembly) and Kit 764 
394 (right spar assembly), as applicable;  and Kits 764 393 and 764 394 must be replaced every 4100 hours 
TIS thereafter (Reference Piper Service Bulletin 744). 
 
NOTE 9 Field installation of Teledyne Continental engines 6-285-BA and 6-285-CA require the following: 
 (a) Engine installed in accordance with instruction per Teledyne Continental Kit EQ6534, EQ6535, 
EQ6539 or EQ6540 (Ref. Teledyne Continental Newsletter dated April 4, 1977). 
 (b) Engine cowl modified in accordance with Piper Service Letter No. 774 (Applicable to S/N  
  36-7360001 through 36-7660102). 
 (c) The following Airplane F light Manual (AFM) required: 
 
 Aircraft Serial Numbers AFM 
      36-7360001 through 36-7460041 VB-645 
      36-7560001 through 36-7660102 VB-682 
 
 
 
 
....END....
```

## ADs

None name its models.

## STCs approved under this data sheet (64, first 50)

- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes.. Concorde Battery Corporation
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.. Michelin North America Inc.
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes.. Aero-Mach Wilco LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA1151NW](https://openairdocs.org/stc/SA1151NW): Installation of the Flight Grip Model 135 Control Stick Grip. Air Products & Parts LLC
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [STC SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks  Starting Vibrator Booster Systems. Continental Motors, Inc.
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc.
- [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc.
- [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc.
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc.
- [STC SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc.
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC ST00961LA](https://openairdocs.org/stc/ST00961LA): Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions.  These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated
June 26, 2000, or later FAA approved revisions.. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [STC SA4847SW](https://openairdocs.org/stc/SA4847SW): Installation of freon air conditioner, engine-driven or wind-driven compressor. Collins Aircraft Dynamics Inc
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc.
- [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc.
- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC
- [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC
- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc.
- [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc.
- [STC SA2167NM](https://openairdocs.org/stc/SA2167NM): Installation of the Precise Flight stand-by vacuum system (SVS).. Precise Flight Inc
- [STC SA10126SC](https://openairdocs.org/stc/SA10126SC): Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.. Aero Holdings Ltd. a Texas limited partnership
- [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC
- [STC SA277NW](https://openairdocs.org/stc/SA277NW): Installation of Automatic Flagman Model No. 4. R-S Sales Inc.
- [STC SA09470SC](https://openairdocs.org/stc/SA09470SC): Installation of Starter Indicator light system.. Texas Skyways Inc
- [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.. Avalaska Inc
- [STC SA2687NM](https://openairdocs.org/stc/SA2687NM): Installation of Truboplus/ Electronics Int'l gauges and switches.. Aero Manufacturing Inc.
- [STC SA01280CH](https://openairdocs.org/stc/SA01280CH): Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404). D & K Aviation
- [STC SA693CE](https://openairdocs.org/stc/SA693CE): Replace existing engine induction air filter with AC Spark Plug filter.. Brackett Aero Filters Inc.
- [STC SA5925NM](https://openairdocs.org/stc/SA5925NM): Installation of oil pressure/temperature instrument.. Electronics International

All 64: https://openairdocs.org/tcds/A9SO/stcs.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.