# Partenavia P68B

- Type: Aircraft model (FAA registry)
- Registry code: 6780104
- Manufacturer (registry): PARTENAVIA S.P.A.
- Model: P68B
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Cruise speed: 143 mph
- Certification: Type certificated
- Data sheet: [TCDS A31EU](https://openairdocs.org/tcds/A31EU) (OpenAirDocs)
- Holder: Vulcanair S.p.A.
- Registered aircraft: 5
- Page: https://openairdocs.org/model/partenavia-p68b

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2022-20-10](https://openairdocs.org/ad/2022-20-10): Rudder Structure · Vulcanair P.68, P.68B, P.68C and 5 more. Effective Nov 28, 2022
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2014-10-01](https://openairdocs.org/ad/2014-10-01): Wings · Vulcanair P 68, P 68 Observer, P 68B and 4 more. Effective Jun 18, 2014
- [AD 2009-24-03](https://openairdocs.org/ad/2009-24-03): Wing spar · Vulcanair P 68, P 68 Observer, P 68B and 2 more. Effective Jan 4, 2010
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-19-08](https://openairdocs.org/ad/2002-19-08): Engine control system · Vulcanair AP68 TP Series 300 Spartacus, P 68, P 68 Observer and 5 more. Effective Nov 8, 2002
- [AD 91-22-06](https://openairdocs.org/ad/91-22-06): Placard Operating Limitations · Vulcanair P 68, P 68 Observer, P 68B and 3 more. Effective Nov 12, 1991
- [AD 89-03-03](https://openairdocs.org/ad/89-03-03): Engine Mounting System · Vulcanair P 68, P 68 Observer, P 68B and 3 more. Effective Feb 16, 1989
- [AD 88-21-04](https://openairdocs.org/ad/88-21-04): Stabilator Trim Tabs · Vulcanair P 68, P 68 Observer, P 68B and 3 more. Effective Oct 27, 1988
- [AD 88-13-08](https://openairdocs.org/ad/88-13-08): Engine Mount · Vulcanair P 68, P 68 Observer, P 68B and 3 more. Effective Jul 13, 1988
- [AD 87-10-12](https://openairdocs.org/ad/87-10-12): Leading Edge Wing Ribs · Vulcanair P 68, P 68B, P 68C and 1 more. Effective Jun 1, 1987
- [AD 87-04-20](https://openairdocs.org/ad/87-04-20): Aileron Control Cable · Vulcanair P 68, P 68 Observer, P 68B and 3 more. Effective Mar 16, 1987
- [AD 85-08-06](https://openairdocs.org/ad/85-08-06): Aileron Control · Vulcanair P 68, P 68 Observer, P 68B and 2 more. Effective May 28, 1985
- [AD 83-14-03](https://openairdocs.org/ad/83-14-03): Fin Rear Spar · Vulcanair P 68 and P 68B. Effective Aug 19, 1983
- [AD 83-07-22 R1](https://openairdocs.org/ad/83-07-22-R1): Flap Selector Switch Replacement · Vulcanair P 68B, P 68C and P 68C-TC. Effective Aug 9, 1983
- [AD 83-15-04](https://openairdocs.org/ad/83-15-04): Torque Support Brackets · Vulcanair P 68, P 68 Observer, P 68B and 2 more. Effective Aug 4, 1983
- [AD 83-12-04](https://openairdocs.org/ad/83-12-04): Flap Bellcrank Attach Mountings · Vulcanair P 68, P 68 Observer, P 68B and 2 more. Effective Jun 23, 1983
- [AD 83-07-17](https://openairdocs.org/ad/83-07-17): Fuel Selector Control · Vulcanair P 68B and P 68C. Effective Apr 14, 1983
- [AD 83-05-07](https://openairdocs.org/ad/83-05-07): Oil Cooler Fittings and Hoses · Vulcanair P 68 and P 68B. Effective Mar 17, 1983
- [AD 82-18-11](https://openairdocs.org/ad/82-18-11): Wheel Shaft Universal Joints · Vulcanair P 68 and P 68B. Effective Sep 13, 1982
- [AD 81-07-08](https://openairdocs.org/ad/81-07-08): Longitudinal Trim Tab · Vulcanair P 68 and P 68B. Effective Apr 6, 1981
- [AD 81-07-03](https://openairdocs.org/ad/81-07-03): Propeller Pitch Control System · Vulcanair P 68 and P 68B. Effective Apr 2, 1981
- [AD 80-15-02](https://openairdocs.org/ad/80-15-02): Rudder Control System · Vulcanair P 68 and P 68B. Effective Jul 21, 1980
- [AD 80-01-01](https://openairdocs.org/ad/80-01-01): Stabilator Balance Weight · Vulcanair P 68 and P 68B. Effective Jan 2, 1980

Historical (superseded or no longer in force):

- [AD 2008-24-11](https://openairdocs.org/ad/2008-24-11) (historical): Safe Fatigue Limits (SFL) of the Wing Structure · Vulcanair AP68 TP Series 300 Spartacus, AP68TP 600 Viator, P 68 and 6 more. Effective Jan 2, 2009
- [AD 85-08-04](https://openairdocs.org/ad/85-08-04) (historical): Wing Spars · Vulcanair P 68, P 68 Observer, P 68B and 4 more. Effective May 17, 1985

## Information bulletins (advisory) (1)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018

## Registered aircraft (5)

- [N321RT](https://openairdocs.org/aircraft/N321RT): [Barr Air Patrol LLC](https://openairdocs.org/faa-owner/BARR%20AIR%20PATROL%20LLC), [Mesquite, TX](https://openairdocs.org/faa-place/TX/Mesquite), built 1979, S/N 189
- [N53695](https://openairdocs.org/aircraft/N53695): [N53695 LLC](https://openairdocs.org/faa-owner/N53695%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1979, S/N 126
- [N590WA](https://openairdocs.org/aircraft/N590WA): [Schellhorn Frederick Jr](https://openairdocs.org/faa-owner/SCHELLHORN%20FREDERICK%20JR), Harxheim Mainz, S/N 61
- [N7668B](https://openairdocs.org/aircraft/N7668B): [Pacific Flight Academy LLC](https://openairdocs.org/faa-owner/PACIFIC%20FLIGHT%20ACADEMY%20LLC), [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu), S/N 28
- [N920AA](https://openairdocs.org/aircraft/N920AA): [Goins Clay Jefferson](https://openairdocs.org/faa-owner/GOINS%20CLAY%20JEFFERSON), [West Park, FL](https://openairdocs.org/faa-place/FL/West%20Park), built 1978, S/N 198

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19900108004109I](https://openairdocs.org/incident/19900108004109I), Jan 8, 1990: Parten P68B (N53695), Kailua-Kona, HI, Minor damage. Upon touchdown the aircraft experienced airframe vibration due to right main tire being flat.
- [Incident 19881231070789I](https://openairdocs.org/incident/19881231070789I), Dec 31, 1988: Parten P68B (N53695), Honolulu, HI. Using loran to navigate pilot flew out of radio range. Was off course. Did not advise ATC of problem.

## Service difficulty reports (80, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR AU510002124](https://openairdocs.org/sdr/AU510002124), Nov 11, 2005: DOOR. SEPARATED. RT SIDE EMERGENCY EXIT POPPED OUT ON TAKEOFF. INVESTIGATION COULD FIND NO FAULTS. SUSPECT CAUSED BY PREVIOUS PASSENGER INTERFERENCE WITH LOCKING LEVER.
- [SDR AU510001994](https://openairdocs.org/sdr/AU510001994), Jun 1, 2005: FITTING. CORRODED. TORQUE TUBE ATTACHMENT FITTING CORRODED. LIMITED INFORMATION PROVIDED.
- [SDR AUS20040321](https://openairdocs.org/sdr/AUS20040321), May 1, 2004: SUPPORT ANGLE. CRACKED. (AUS) WING SPAR STRAP SUPPORT FORWARD AND AFT ANGLES CRACKED ALONG RIVET LINE.
- [SDR AUS20040276](https://openairdocs.org/sdr/AUS20040276), Apr 16, 2004: INJECTOR. FAULTY. (AUS) RT ENGINE FUEL INJECTOR FLOW ERRATIC.
- [SDR AUS20040267](https://openairdocs.org/sdr/AUS20040267), Mar 26, 2004: INJECTOR. CONTAMINATED. (AUS) RT ENGINE FUEL INJECTORS CONTAMINATED BY SMALL FERROUS (RUST) PARTICLES.
- [SDR AUS20040118](https://openairdocs.org/sdr/AUS20040118), Feb 20, 2004: NOZZLE. BLOCKED. (AUS) NR 4 CYLINDER FUEL INJECTOR NOZZLE BLOCKED.
- [SDR AUS20040133](https://openairdocs.org/sdr/AUS20040133), Feb 6, 2004: SPAR CAP. CRACKED. (AUS) REAR WING SPAR BOTTOM SPAR CAP CRACKED IN AREA OF LT SIDE WING ATTACHMENT. CRACK LENGTH 6MM (0.236IN). FOUND DURING EDDY CURRENT INSPECTION.
- [SDR AUS20040067](https://openairdocs.org/sdr/AUS20040067), Feb 2, 2004: HOSE. DISTORTED. (AUS) VACUUM HOSE KINKED. DISTORTION WAS LOCATED ON FRAME F AT THE TOP FRONT LT DOOR FRAME AND WAS CAUSED BY THE BEND RADIUS BEING TOO SMALL AFTER PASSING OVER 
- [SDR AUS20031334](https://openairdocs.org/sdr/AUS20031334), Dec 15, 2003: DOUBLER. CORRODED. (AUS) WING SPAR DOUBLERS PN 68-1.4009-3 AND PN 68-1.4009-4 CONTAINED A SMALL AMOUNT OF CORROSION. DOUBLERS ARE LOCATED IN AREA BEHIND ENGINES AND ENGINE FIREWAL
- [SDR AUS20031333](https://openairdocs.org/sdr/AUS20031333), Dec 15, 2003: FITTING. CRACKED. (AUS) ENGINE MOUNT FITTINGS PN 68-1.2025-1 AND PN 68-1.2025-2 CRACKED AROUND RIVET HOLES.
- [SDR AUS20031107](https://openairdocs.org/sdr/AUS20031107), Oct 4, 2003: GENERATOR. FAILED. (AUS) LT AND RT GENERATORS FAILED.
- [SDR AUS20021303](https://openairdocs.org/sdr/AUS20021303), Nov 6, 2002: SPAR CAP. CRACKED. (AUS) LH WING SPAR CAP CRACKED. PREVIOUS CRACK HAD BEEN REPAIRED USINGSTAINLESS STEEL LAMINATIONS. DURING EDDY CURRENT INSPECTION IAW AD/P68/43 AMDT1 IT WAS FOU
- [SDR AUS20020860](https://openairdocs.org/sdr/AUS20020860), Jul 25, 2002: BRACKET. CRACKED. (AUS) TOP RUDDER HINGE BRACKET CRACKED.
- [SDR AUS20020778](https://openairdocs.org/sdr/AUS20020778), Jul 20, 2002: CYLINDER. MISINSTALLED. (AUS) RT ENGINE NR 2 CYLINDER INLET VALVE PUSHROD BROKEN. SHROUD TUBE SEVERELY DISTORTED. METAL IN OIL FILTER. INVESTIGATION FOUND THE FOLLOWING DEFECTS: NR 1 C
- [SDR AUS20020350](https://openairdocs.org/sdr/AUS20020350), Apr 16, 2002: KEY. UNAPPROVED PART. (AUS) STABILATOR KEYS (2OFF) WERE UNAPPROVED HANDMADE PARTS. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20020349](https://openairdocs.org/sdr/AUS20020349), Apr 15, 2002: BOLT. MISINSTALLED. (AUS) STABILATOR FORWARD CONTROL ROD BOLT INSTALLED IN INCORRECT DIRECTION.
- [SDR AUS20011281](https://openairdocs.org/sdr/AUS20011281), Nov 27, 2001: BRAKE. MISSING. (AUS) AIRCRAFT NOSE SPAT AND PITOT TUBE DAMAGE WHEN AIRCRAFT RAN INTO THE SIDE OF THE HANGAR WHILE BEING TAXIED FOR REFUELLING. INVESTIGATION FOUND THAT THE PIL
- [SDR AUS20010960](https://openairdocs.org/sdr/AUS20010960), Aug 20, 2001: BRACKET. CORRODED. (AUS) LH WING LEADING EDGE TOP FORWARD ATTACHMENT BRACKET CORRODED.
- [SDR AUS20010430](https://openairdocs.org/sdr/AUS20010430), May 4, 2001: FLANGE. CRACKED. (AUS) AFT WING SPAR WEB FLANGE CRACKED ON THE LH SIDE IN THE AREA OUTBOARD OF THE ATTACHMENT FITTING. FOUND DURING INSPECTION IAW AD/P68/22, AD/P68/45 AND SB 65
- [SDR AU001049](https://openairdocs.org/sdr/AU001049), Nov 6, 2000: SPAR. CRACKED. (AUS) LEFT AND RIGHT WING REAR SPAR WEBS CRACKED AT RELIEF HOLE FOR NR 3 FLAP HINGE BRACKET. (X)
- [SDR AU000774](https://openairdocs.org/sdr/AU000774), Aug 12, 2000: PIPE. WORN. (AUS) ENGINE OIL PRESSURE LINE LOCATED BEHIND INSTRUMENT PANEL WORN BY OPILOT ASHTRAY. OIL LEAKING. (X)
- [SDR AU000543](https://openairdocs.org/sdr/AU000543), Jul 9, 2000: RIVET. MISALIGNED. (AUS) LEFT OUTBOARD ENGINE NACELLE COWL RIVET MISALIGNED TO SPAR CAP RIVETS BY APPROXIMATELY 3.175 MM (0.125 INCH). FOUND DURING INSPECTION IAW AD/P68/46. (X)
- [SDR AU000357](https://openairdocs.org/sdr/AU000357), Apr 1, 2000: LINK. CORRODED. (AUS) LEFT AND RIGHT INBOARD FLAP HANGERS CORRODED IN AREA OF BONDING WIRE ATTACHMENT. FOUND DURING INSPECTION IAW AD/P68/40.
- [SDR AU000087](https://openairdocs.org/sdr/AU000087), Jan 28, 2000: RIVET. MISALIGNED. (AUS) LEFT AND RIGHT WING INBOARD ENGINE COWL RIVETS MISALIGNED. THE RIVETS DID NOT IMPINGE ON THE SPAR. FOUND DURING INSPECTION IAWAD/P68/46.
- [SDR AU000111](https://openairdocs.org/sdr/AU000111), Jan 25, 2000: MOUNT. CRACKED. (AUS) LEFT AND RIGHT ENGINE MOUNTS CRACKED AND CORRODED.
- [SDR AU990726](https://openairdocs.org/sdr/AU990726), Jul 22, 1999: CONTROL CABLE. WORN. (AUS) RIGHT FORWARD RUDDER CABLE EXCESSIVELY WORN IN THE AREA OF THE FORWARD PULLEY LOCATED AT FRAME NR 3.
- [SDR AU990722](https://openairdocs.org/sdr/AU990722), Jul 22, 1999: FITTING. CRACKED. (AUS) LEFT ENGINE MOUNT UPPER INBOARD ATTACHMENT FITTING CRACKED IN THE VERTICAL FLANGE.
- [SDR AU990678](https://openairdocs.org/sdr/AU990678), Jun 23, 1999: ROD END. WRONG PART. (AUS) LEFT ENGINE MIXTURE CONTROL TO FCU CONTROL ROD ROD END AND ATTACHING HARDWARE SUSPECT UNAPPROVED PARTS.
- [SDR AU990516](https://openairdocs.org/sdr/AU990516), May 10, 1999: BRACKET. CORRODED. (AUS) RT WING FLAP BRACKET CORRODED.
- [SDR AU990569](https://openairdocs.org/sdr/AU990569), May 8, 1999: ENGINE. OVERSERVICED. (AUS) SMOKE IN COCKPIT. INVESTIGATION FOUND A SMALL QUANTITY OF OIL AROUND THE MUFFLER SHROUD. SUSPECT OIL HAD BEEN SPILT DURING ENGINE OIL TOP UP.
- [SDR AU990027](https://openairdocs.org/sdr/AU990027), Jan 21, 1999: ANGLE. CRACKED. (AUS) FORWARD WING SPAR RIGHT AFT SPAR CAP ANGLE FOUND TO BE CRACKED IN THE AREA OUTBOARD OF THE RIGHT WING ATTACHMENT. FOUND DURING INSPECTION IAW AD/P68/45 (S
- [SDR AU990002](https://openairdocs.org/sdr/AU990002), Jan 3, 1999: CONTROL CABLE. FAILED. (AUS) PILOT REPORTED RUDDER CABLE SLIPPAGE. INVESTIGATION FOUND THAT THE RT RUDDER (FORWARD) CABLE HAD FAILED AT THE FORWARD MOST PULLEY. THE LT CABLE WAS THEN 
- [SDR AU981040](https://openairdocs.org/sdr/AU981040), Aug 25, 1998: ANGLE. CRACKED. (AUS) SPAR CAP ANGLE CRACKED BEYOND THE STOP DRILL HOLE. PART TC: 7,384.
- [SDR AU980847](https://openairdocs.org/sdr/AU980847), Jul 21, 1998: MOUNT. CRACKED. (AUS) RIGHT LOWER ENGINE MOUNT TUBE CRACKED.
- [SDR AU981187](https://openairdocs.org/sdr/AU981187), Jun 23, 1998: VALVE. WORN. (AUS) LEFT ENGINE FUEL SELECTOR VALVE WOULD NOT COMPLETELY OPEN. PART TC: 7,649.
- [SDR AU980317](https://openairdocs.org/sdr/AU980317), Mar 27, 1998: HOSE. DETERIORATED. (AUS) PITOT/STATIC SYSTEM HOSE DETERIORATED. SILICON HOSE APPEARS TO BE BREAKING DOWN AND EXUDING AN OILY FILM WHICH IS PARTIALLY BLOCKING THE STATIC AIR DISTRI
- [SDR AU980318](https://openairdocs.org/sdr/AU980318), Mar 24, 1998: SKIN. CORRODED. (AUS) RT ENGINE LOWER NACELLE SKIN SEVERELY CORRODED INTERNALLY. SKIN IS LOCATED ABOVE THE EXHAUST GAS STREAM. PART OF THE NACELLE LATERAL BEAM WAS ALSO CORRODE
- [SDR AU980225](https://openairdocs.org/sdr/AU980225), Feb 26, 1998: BATTERY. LEAKING. (AUS) ELT BATTERY ACID SPILLAGE. ACID ATE THROUGH THE BATTERY CASE AND BATTERY MOUNTING PLATE.
- [SDR AU980182](https://openairdocs.org/sdr/AU980182), Feb 12, 1998: PUMP. FAILED. (AUS) ENGINE FUEL PUMP DRIVE LEVER FAILED ACROSS PIVOT PIN HOLES. LEVER SECTION WITHIN THE PUMP HAS SECONDARY CRACKING AND IS SLIGHTLY BOWED OUTWARDS. BROKEN PO
- [SDR AU980653](https://openairdocs.org/sdr/AU980653), Jan 15, 1998: PIPE. LOOSE. (AUS) RT FUEL SELECTOR PIPE TO TANK LOOSE.
- [SDR AU980215](https://openairdocs.org/sdr/AU980215), Jan 8, 1998: FITTING. LOOSE. (AUS) RT ENGINE SURGED AND FAILED. LT ENGINE SURGED AND THEN FAILED DURING TAXI FOLLOWING LANDING. INVESTIGATION FOUND THAT THE RT FUEL SELECTOR FITTING WAS LOO
- [SDR AU971570](https://openairdocs.org/sdr/AU971570), Dec 18, 1997: BRACKET. CRACKED. (AUS) ENGINE MOUNT TO WING ATTACHMENT BRACKETS (3OFF) WERE FOUND CRACKED:1. LH LOWER INBOARD PNO 68-1.2027,2. RH UPPER INBOARD PNO 68-1.2025-1 AND 3. RH UPPER O
- [SDR AU971623](https://openairdocs.org/sdr/AU971623), Nov 18, 1997: BULKHEAD. CRACKED. (AUS) FRONT BULKHEAD CRACKED THROUGH TWO BOLT HOLES. FOUND FOLLOWING REMOVAL OF THE UPPER NOSE LEG MOUNT PLATE DUE TO TOWING DAMAGE. DAMAGE CAUSED BY INCORRECT 
- [SDR AU971410](https://openairdocs.org/sdr/AU971410), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) RH FLAP CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU971409](https://openairdocs.org/sdr/AU971409), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) RH FORWARD ELEVATOR CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU971408](https://openairdocs.org/sdr/AU971408), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) RH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU971407](https://openairdocs.org/sdr/AU971407), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) LH AILERON BALANCE CABLE STRANDS BROKEN. FOUND DURING INSPECTIONIAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU971406](https://openairdocs.org/sdr/AU971406), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) RH AILERON OUTBOARD CONTROL CABLE STRANDS BROKEN. FOUND DURINGINSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU971403](https://openairdocs.org/sdr/AU971403), Nov 3, 1997: CONTROL CABLE. FRAYED. (AUS) LH OUTBOARD AILERON CABLE STRANDS BROKEN. FOUND DURING INSPECTION IAW AD/P68/44 (PARTENAVIA SB 75 REV3).
- [SDR AU970948](https://openairdocs.org/sdr/AU970948), Jun 30, 1997: CAPACITOR. BURNT. (AUS) MAGNETO CAPACITOR AND POINTS BURNT - FOUND DURING INSPECTION IAWAD/ELECT/46 AMDT 6

All 80: https://openairdocs.org/model/partenavia-p68b/reports.md

## STCs that may be installed (OpenAirDocs) (133, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA03420AT](https://openairdocs.org/stc/SA03420AT): Propeller model MTV-12-B-C-F/CF183-59b propeller installed. MT-Propeller Entwicklung GmbH
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists P68 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [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 SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc

All 133: https://openairdocs.org/model/partenavia-p68b/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.