# N945CA: 2020 Costruzioni Aeronautiche Tecna P2012 TRAVELLER

- Status: Valid registration
- Airframe: [Costruzioni Aeronautiche Tecna P2012 TRAVELLER](https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2012-traveller) (registry code 0330521, 11 seats)
- Engine: [Lycoming TEO-540-C1A](https://openairdocs.org/engine/lycoming-teo-540-c1a) (registry code 42715)
- Data sheets: [TCDS A00076CE](https://openairdocs.org/tcds/A00076CE) (Costruzioni Aeronautiche Tecnam S.P.A.), [TCDS E00009NY](https://openairdocs.org/tcds/E00009NY) (Lycoming Engines) (OpenAirDocs)
- Serial number: 024/US
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: November 10, 2020
- Certificate issued: November 24, 2020
- Expires: November 30, 2027
- Mode S code: AD1FEE
- Registered owner: [Hyannis Air Service Inc](https://openairdocs.org/faa-owner/HYANNIS%20AIR%20SERVICE%20INC)
- Location: [Hyannis, MA](https://openairdocs.org/faa-place/MA/Hyannis)
- Owner type: Corporation
- Owner's area on the map: 41.6612° N, 70.2932° W: Placed by OpenAirDocs at the center of ZIP code 02601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=945CA
- Page: https://openairdocs.org/aircraft/N945CA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 3 in force

### Matched by airframe (Costruzioni Aeronautiche Tecna P2012 TRAVELLER)

- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-12-06](https://openairdocs.org/ad/2022-12-06): Elevator Tab Control System · Costruzioni Aeronautiche Tecnam P2012 Traveller. Effective Jul 19, 2022

### Matched by engine (Lycoming TEO-540-C1A)

- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026

### Historical (superseded or no longer in force)

- [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024

## Information bulletins (advisory) (1 in force)

- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019

## NTSB investigations

None matched to N945CA.

## FAA accident and incident reports

None matched to N945CA.

## Service difficulty reports (2)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR HYIA20250106001](https://openairdocs.org/sdr/HYIA20250106001), Jan 1, 2025: FIRE DETECTOR. FAILED. PILOT REPORTED ON APPROACH THE LEFT FIRE CAS MESSAGE APPEARED, THERE WERE NO OTHER FIRE INDICATIONS AND UPON LANDING THE MESSAGE EXTINGUISHED. MAINTENANCE INSPE
- [SDR HYIA20230912005](https://openairdocs.org/sdr/HYIA20230912005), Sep 7, 2023: CYLINDER. FAILED. PILOT REPORTED BLACK AND GREY SMOKE FROM RIGHT ENGINE EXHAUST. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE #5 CYLINDER OIL SOAKED. CYLINDER WAS REPLACED.

## Service difficulty reports on N945CA not matched to an aircraft (60, newest 50)

They name N945CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR COMA0160892](https://openairdocs.org/sdr/COMA0160892), Nov 14, 2001: SKIN. DENTED. FUSELAGE SKIN AT FS310.0 NEAR PAX DOOR HAS TEMPORARY REPAIR THAT REQUIRES PERMANENT REPAIR.PERFORMED A PERMANENT MAJOR REPAIR TO FUSELAGE SKIN AT FS 310.0 I/A/W
- [SDR COMA0160887](https://openairdocs.org/sdr/COMA0160887), Nov 13, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM UPPER PLATE AT RBL3 HAS A CRACK GOING FROM THE AFT EDGE INTO A RIVET HOLE.PERFORMED A TEMPORARY MAJOR REPAIR TO CENTER ENGINE SUPPORT BEAM I
- [SDR COMA0160535](https://openairdocs.org/sdr/COMA0160535), Jul 29, 2001: LIGHT. EMERG LIGHTS ILLUMINATED WITH SWITCH IN AUTO POSITION.FOUND CANNON PLUG JB-6 DISCONNECTED. SECURED CONNECTOR AND SYSTEM TEST NORMAL.
- [SDR COMA0160396](https://openairdocs.org/sdr/COMA0160396), Jun 20, 2001: BUSHING. SCORED. FOUND 3 EACH VERTICAL TO HORIZONTAL PIVOT POINT BUSHINGS TO BE SCORED.REMOVED HORIZONTAL STAB ASSY. REMOVED THE DAMAGED BUSHINGS. INSTALLED 3 EACH NEW BUSHINGS 
- [SDR COMA0160389](https://openairdocs.org/sdr/COMA0160389), Jun 15, 2001: ANGLE. CRACKED. LEFT AND RIGHT FS 484 ANGLES ARE CRACKED. REPAIRED LEFT AND RIGHT FS 484 ANGLES IAW WVAC EO 601R-53-2507.
- [SDR COMA0160390](https://openairdocs.org/sdr/COMA0160390), Jun 14, 2001: VANE. CHAFED. RT INBOARD FLAP VANE CHAFED BEYOND LIMITS. REPAIRED RIGHT INBOARD FLAP VANE IAW AERODESIGN REPORT 1286.
- [SDR COMA0160033](https://openairdocs.org/sdr/COMA0160033), Dec 29, 2000: LIGHT. INOPERATIVE. FLOOR PATH EMERGENCY LIGHTS ROW 5 FORWARD ARE INOPERABLE.REPLACED THE LAMP.
- [SDR COMA0060895](https://openairdocs.org/sdr/COMA0060895), Nov 8, 2000: WARNING LIGHT. ILLUMINATED. LEFT ENGINE T/R UNLOCKED CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM, NO DEFECTS FOUND.
- [SDR COMA0060775](https://openairdocs.org/sdr/COMA0060775), Sep 25, 2000: WARNING SYSTEM. FALSE ACTIVATION. STALL FAIL AND CONFIG SPOILERS WARNING DURING TAKEOFF. CYCLED CIRCUIT BREAKER, COULD NOT DUPLCIATE. SYSTEM TEST NORMAL.
- [SDR COMA0060688](https://openairdocs.org/sdr/COMA0060688), Aug 22, 2000: ANGLE. CORRODED. PASSENGER DOOR SUPPORT ANGLE (P/N 601R-31527-221) CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR BY REPLACING PASSENGER DOOR SUPPORT ANGLE IAW WVAC EO 601R-53
- [SDR COMA0060660](https://openairdocs.org/sdr/COMA0060660), Aug 20, 2000: ANGLE. CORRODED. PAX DOOR SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED ANGLE AND FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R0-53-1597.
- [SDR COMA0060658](https://openairdocs.org/sdr/COMA0060658), Aug 20, 2000: SKIN. DENTED. THE RIGHT HAND FUSELAGE SKIN WAS SCRATCHED AND WAS SLIGHTLY DENTED AT FS 409+16 STR 25. PERFORMED A MAJOR REPAIR BY RE-CONTOURING TO NEAR ORIGINAL CONTOUR FUSEL
- [SDR COMA0060657](https://openairdocs.org/sdr/COMA0060657), Aug 20, 2000: SKIN. DENTED. THE RIGHT HAND SIDE FUSELAGE SKIN WAS SCRATCHED AND WAS SLIGHTLY DENTED AT FS 409+16 STR 20. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 409+16 STR 20 BY RE
- [SDR COMA0060656](https://openairdocs.org/sdr/COMA0060656), Aug 20, 2000: PLATE. MISMANUFACTURED. WHILE PERFORMING S/B 601R-53-037 TITANIUM FLOORBEAM MOD, FOUND STRAPS 2 EA P/N 601R-31030-7715 ARE MANUFACTURED INCORRECTLY. FABRICATED NEW DOUBLER PLATES FROM 
- [SDR COMA0060703](https://openairdocs.org/sdr/COMA0060703), Aug 19, 2000: O-RING. LEAKING. RIGHT HAND ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED THE O-RING ON A SUMP LUB SCAVANGE PUMP.
- [SDR COMA0060661](https://openairdocs.org/sdr/COMA0060661), Aug 19, 2000: ANGLE. CORRODED. FS 280 FORWARD J ANGLE CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW SERVICEABLE J ANGLE IAW WVAC EO 601R-53-1596.
- [SDR COMA0060676](https://openairdocs.org/sdr/COMA0060676), Aug 17, 2000: ANGLE. CORRODED. THE FWD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 
- [SDR COMA0060665](https://openairdocs.org/sdr/COMA0060665), Aug 17, 2000: BEAM. CUT. TRANSVERSE BEAM AT FS 295 AT RBL 9 WAS GROUND INTO WHEN REMOVING FLOORBEAM RBL 9 DURING ACCOMPLISHMENT OF SB 601R-53-027. REPAIRED BEAM IAW WVAC EO 601R-53-1591
- [SDR COMA0060664](https://openairdocs.org/sdr/COMA0060664), Aug 17, 2000: BEAM. CUT. THE TRANSVERSE BEAM WAS CUT AT THE LOWER FLANGE AT FS 379 LBL 9 DURING INCORPORATION OF SB 601R-53-037 REV A. PERFORMED A MAJOR REPAIR TO TRANSVERSE BEAM AT FS 
- [SDR COMA0060663](https://openairdocs.org/sdr/COMA0060663), Aug 17, 2000: FLOORBEAM. CRACKED. THE FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 HAS A 2 INCH CRACK, APPROXIMATELY 1 - 2 INCHES TO THE RIGHT OF FLOOR SUPPORT AT RBL 9.0. PERFORMED A MAJOR REPAI
- [SDR COMA0060662](https://openairdocs.org/sdr/COMA0060662), Aug 17, 2000: CHANNEL. CORRODED. THE AFT J-CHANNEL AT FS 280.0 IS CORRODED AT BL 0. PERFORMED A MAJOR REPAIR TO CORRODED AFT J-CHANNEL AT FS 280.0 BL 0.0 IAW WVAC EO 601R-53-1588.
- [SDR COMA0060687](https://openairdocs.org/sdr/COMA0060687), Aug 15, 2000: SKIN. DENTED. FUSELAGE DAMAGED AT FS 310 AT PAX DOOR. REPAIRED DAMAGED FUSELAGE SKIN AT LOWER LEFT PAX DOOR IAW REO 601R-53-21-180 REV NC.
- [SDR COMA0060582](https://openairdocs.org/sdr/COMA0060582), Jul 18, 2000: SIGN. BROKEN. EXIT SIGN AT SERVICE DOOR IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA0060415](https://openairdocs.org/sdr/COMA0060415), May 11, 2000: CONTROL UNIT. INOPERATIVE. STABILIZER AND MACH TRIM INOP. CYCLED AIRCRAFT POWER, SYSTEM TEST SATISFACTORY. COULD NOT DUPLICATE.
- [SDR COMA0060336](https://openairdocs.org/sdr/COMA0060336), Apr 13, 2000: FLANGE. BENT. PASSENGER DOOR SEAL STRIKER AT FS 310.0 LT, STR 15 - 16 DAMAGED BY IMPACT WITH PASSENGER DOOR LOCK PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR SEAL STRIKER 
- [SDR COMA9960717](https://openairdocs.org/sdr/COMA9960717), Nov 29, 1999: BRACKET. DAMAGED. NLG DID NOT RETRACT. REPLACED THE NLG WOW AND CENTERED PROXIMITY BRACKET.
- [SDR COMA9960642](https://openairdocs.org/sdr/COMA9960642), Oct 20, 1999: ACTUATOR. FAILED. FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTBOARD OUTER FLAP ACTUATOR.
- [SDR COMA9960641](https://openairdocs.org/sdr/COMA9960641), Oct 20, 1999: ACTUATOR. FAILED. FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTER FLAP INBOARD ACTUATOR.
- [SDR COMA9960549](https://openairdocs.org/sdr/COMA9960549), Sep 26, 1999: FRAME. CRACKED. FRAME AT FS 718.00 HAD A TEMPORARY REPAIR PER WVAC EO 601R-53-0056B ON THE FRAME PREVIOUSLY INSTALLED. PERFORMED A PERMANENT MAJOR REPAIR TO CRACKED FRAME FLANG
- [SDR COMA9960538](https://openairdocs.org/sdr/COMA9960538), Sep 19, 1999: ENGINE. FAILED. ON CLIMBOUT, RIGHT ENGINE OIL PSI MESSAGE ON ED-1 SHUT DOWN NR 2 ENGINE. DROPPED TO 22 PSI. FOUND SKYDROL IN ACCESSORY GEARBOX. REMOVED AND REPLACED RIGHT ENGIN
- [SDR COMA9960537](https://openairdocs.org/sdr/COMA9960537), Sep 18, 1999: ENGINE. FAILED. IDG NR 2 CAUTION MESSAGE, FOLLOWED BY GEN NR 2 CAUTION MESSAGE ON TAKEOFF. IDG NR 2 CAUTION MESSAGE WENT OUT DURING ABORT. NR 2 GEN WAS RESET. FOUND SKYDROL IN 
- [SDR COMA9960270](https://openairdocs.org/sdr/COMA9960270), Jun 8, 1999: SHIELD. CRACKED. APU EXHAUST SHIELD HAS A CRACK AT THE 7 O'CLOCK POSITION. REPAIRED PER CANADAIR REO 601R-49-81-003.
- [SDR COMA9960259](https://openairdocs.org/sdr/COMA9960259), Jun 8, 1999: FRAME. CRACKED. FRAME FLANGE AT FS 718 RT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES. REPAIRED PER WVAC EO 601R-53-0057.
- [SDR COMA9960258](https://openairdocs.org/sdr/COMA9960258), Jun 8, 1999: FRAME. CRACKED. FRAME FLANGE AT FS 718 LT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES JUST BELOW STRINGER 11. TEMPORARILY REPAIRED IAW WVAC EO 601R-53-00560. MUST BE PERMANEN
- [SDR COMA9960257](https://openairdocs.org/sdr/COMA9960257), Jun 8, 1999: STRINGER. CRACKED. DOUBLER AFT OF FS 718 HAS APPROX 4 INCH CRACK IN RADIUS AT STRINGER 11. REPAIRED PER WVAC EO NR 601R-53-0058.
- [SDR COMA9960272](https://openairdocs.org/sdr/COMA9960272), Jun 7, 1999: PCU. LEAKING. RIGHT AILERON OUTBOARD PCU LEAKING BEYOND LIMITS. REPLACED PCU.
- [SDR COMA9960271](https://openairdocs.org/sdr/COMA9960271), Jun 7, 1999: DUCT. BROKEN. APU EXHAUST DUCT HAS SEVERAL BROKEN FINGER CLAMP STOPS. REPLACED EXHAUST DUCT.
- [SDR COMA9960269](https://openairdocs.org/sdr/COMA9960269), Jun 6, 1999: BRACKET. MISSING. CARGO DOOR STOP BRACKET IS MISSING. INSTALLED CARGO DOOR STOP BRACKET.
- [SDR COMA9960268](https://openairdocs.org/sdr/COMA9960268), Jun 6, 1999: STRIKER. CRACKED. PAX DOOR SEAL STRIKER AT FS 349 IS DAMAGED. REPAIRED PER REO 601R-52-11-00 REPAIR A.
- [SDR COMA9960267](https://openairdocs.org/sdr/COMA9960267), Jun 6, 1999: STRIKER. CRACKED. PAX DOOR SEAL STRIKER AT FS 3100 PREVIOUS REPAIR IS DAMAGED. REPAIRED PER REO 601R-52-11-008, REPAIR C.
- [SDR COMA9960274](https://openairdocs.org/sdr/COMA9960274), Jun 5, 1999: CAP. CHAFED. LEFT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS.
- [SDR COMA9960273](https://openairdocs.org/sdr/COMA9960273), Jun 5, 1999: CAP. CHAFED. RIGHT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS.
- [SDR COMA9960117](https://openairdocs.org/sdr/COMA9960117), Mar 10, 1999: FUEL. LEAKING. FLUID LEAKING FROM LEFT AND RIGHT WINGS AT THE FUEL VENT AREA. INSPECTED AIRCRAFT FOR FUEL LEAKS AND NONE FOUND.
- [SDR COMA9860408](https://openairdocs.org/sdr/COMA9860408), Dec 23, 1998: RETRACT SYST. MALFUNCTIONED. FLAPS FAILED AT 8 DEGREES. RESET FLAPS PER AD 98-20-01. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9860329](https://openairdocs.org/sdr/COMA9860329), Oct 28, 1998: SKIN. DAMAGED. DAMAGE FOUND BY CREW ON POST FLIGHT INSPECTION. DENT BELOW CARGO DOOR AREA AT FS 599.00 AND STRINGER 22L AND 23 DENT WAS .098 DEEP, WITH A GOUGE OF .015. DAMAGE
- [SDR COMA9860032](https://openairdocs.org/sdr/COMA9860032), Feb 1, 1998: LIGHT. DIM. EMERGENCY FLOOR LIGHTING IS DIM, AFT CABIN AREA. REPLACED AFT TRACK LIGHT ASSY.
- [SDR COMA9760223](https://openairdocs.org/sdr/COMA9760223), Nov 11, 1997: PCU. MALFUNCTIONED. CONFIG SPOILERS WARNING DURING TAKEOFF. REPLACED LEFT HAND OUTBOARD SPOILERON PCU.
- [SDR COMA9760193](https://openairdocs.org/sdr/COMA9760193), Oct 7, 1997: ACTUATOR. MALFUNCTIONED. CONFIG TRIM WARNING DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE AILERON TRIM ACTUATOR FOR TROUBLESHOOTING.
- [SDR COMA9760055](https://openairdocs.org/sdr/COMA9760055), Mar 5, 1997: LIGHT. OVERHEATED. STRONG ELECTRICAL ODOR DETECTED BY CREW DURING TAXI. REPLACED THE GALLEY WORK LIGHT ASSY.
- [SDR COMA9760056](https://openairdocs.org/sdr/COMA9760056), Mar 4, 1997: ELECTRICAL. ODOR. BURNING ELECTRICAL SMELL IN COCKPIT. COULD NOT DUPLICATE DISCREPANCY. POWERED ALL SYSTEMS ON AIRCRAFT AND COULD DETECT BURNING ODOR.

All 60: https://openairdocs.org/aircraft/N945CA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (4)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Costruzioni Aeronautiche Tecna P2012 TRAVELLER)

- [STC SA12478AK](https://openairdocs.org/stc/SA12478AK): Installation of Hartzell Engine Technologies (HET) ALT-FLX Alternators i. Momentum Aeronautics Holdings, LLC
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA11842CH](https://openairdocs.org/stc/SA11842CH): Installation of Preheat Kit, p/n TA3370-1 for 115 volt application in accordance with Preheat Kit drawing TA3370-1. Hartzell Propeller LLC

### Approved for the engine (Lycoming TEO-540-C1A)

- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc

## Related

- Other Costruzioni Aeronautiche Tecna P2012 TRAVELLER aircraft: https://openairdocs.org/model/costruzioni-aeronautiche-tecna-p2012-traveller/aircraft.md
- The Lycoming TEO-540-C1A engine: https://openairdocs.org/engine/lycoming-teo-540-c1a.md

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