# N14834: Aerospatiale/Aeritalia ATR 42-320, registration cancelled 2019-06-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 25, 2019
- Status when cancelled: Valid registration
- Airframe: [Aerospatiale/Aeritalia ATR 42-320](https://openairdocs.org/model/aerospatiale-aeritalia-atr-42-320) (registry code 8680930)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 193
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 6, 1990
- Certificate issued: December 23, 2014
- Last registry action: November 7, 2017
- Mode S code: A0C346
- Owner when cancelled: [Pcalg Aircraft LLC](https://openairdocs.org/faa-owner/PCALG%20AIRCRAFT%20LLC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: LLC
- Owner's area on the map: 36.0953° N, 115.3717° W: Placed by OpenAirDocs at the center of ZIP code 89135, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14834
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14834
- Page: https://openairdocs.org/deregistered/N14834-2019-06-25

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Aerospatiale/Aeritalia ATR 42-320: https://openairdocs.org/model/aerospatiale-aeritalia-atr-42-320.md

## Service difficulty reports (213, newest 50)

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

- [SDR HYIA20180403002](https://openairdocs.org/sdr/HYIA20180403002), Mar 31, 2018: ADC. DEFECTIVE. PILOT REPORTED CA/FO/STBY AIRSPEED INDICATOR ALL VARIED BY 20+ KNOTS. MAINTENANCE INSPECTED AND FOUND THE NR 2 AIR DATA COMPUTER TO HAVE A BURNED ODOR. THE COMP
- [SDR HYIA20160411001](https://openairdocs.org/sdr/HYIA20160411001), Apr 10, 2016: POWER SUPPLY. INOPERATIVE. PILOT REPORTED EMER AISLE LIGHTS INOPERATIVE AT SEATS 10B, 11B, & 12B. R & R EMER POWER SUPPLY UNIT 30WL & OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM JIC 33-5
- [SDR HYIA20160314001](https://openairdocs.org/sdr/HYIA20160314001), Mar 14, 2016: WIRE. SHORTED. PILOT REPORTED BURNING SMELL SHORTLY AFTER TAKEOFF. MX INSPECTED & FOUND WIRE 216, BETWEEN 771VT & 71VC SHORTING TO GND. REPAIRED WIRE 216 IAW SPM 20-52-00 & AW
- [SDR HYIA20160304003](https://openairdocs.org/sdr/HYIA20160304003), Feb 28, 2016: FITTING. CRACKED. DURING INSPECTION FCD ATR-2016-32-001, RT MLG ACTUATOR FITTING WAS FOUND CRACKED AT LEVEL OF THE TWO LOWER ATTACHMENT HOLES.
- [SDR HYIA20151030001](https://openairdocs.org/sdr/HYIA20151030001), Oct 27, 2015: BEARING. DEFECTIVE. PILOT REPORTED THE RUDDER WAS STIFF & HARD TO MOVE IN FLIGHT. R & R TWO AFTER RUDDER QUADRANT BEARINGS PN MS27645-10 & MS27648-16 IAW AMM JIC 22-18-32 & RELEASE
- [SDR HYIA20150904001](https://openairdocs.org/sdr/HYIA20150904001), Aug 27, 2015: ECU. INOPERATIVE. AFTER GO AROUND, ECU 1 FAULTED. ECU 1 WAS TURNED OFF IAW QRH. ON BASE TO FINAL, LT TORQUE WENT TO 100% & LT NP WENT INTO CAUTION, NR 1 ECU. CLEANED CONNECTOR, P
- [SDR HYIA20150604001](https://openairdocs.org/sdr/HYIA20150604001), Jun 4, 2015: BRAKE SYS. CONTAMINATED. PILOT REPORTED UPON PARKING, BRAKES WERE APPLIED TO THE STOP. ALMOST NEEDED TO USE THE EMER BRAKE. PCE PERFORMED FOUR BRAKE ASSEMBLY HIGH PRESSURE LINE BLEEDING
- [SDR HYIA20150220001B](https://openairdocs.org/sdr/HYIA20150220001B), Feb 18, 2015: BOLT. LOOSE. LEFT AILERON OTBD SHACKLE BOLT WAS FOUND LOOSE AFTER REPORTS OF SLIGHT VIBRATION IN FLIGHT FROM THE FLIGHT CREW. AILERON WAS R & R AT AN OUTSIDE VENDOR DURING 2
- [SDR HYIA20150220001](https://openairdocs.org/sdr/HYIA20150220001), Feb 18, 2015: BOLT. LOOSE. LEFT AILERON OTBD SHACKLE BOLT WAS FOUND LOOSE AFTER REPORTS OF SLIGHT VIBRATION IN FLIGHT FROM THE FLIGHT CREW. SECURED & RE-TORQUED SHACKLE BOLT NUT IAW AMM J
- [SDR HYIA20141017089](https://openairdocs.org/sdr/HYIA20141017089), Oct 17, 2014: SPAR. CORRODED. RIGHT WING AFT SPAR UPPER CHORD CORROSION BETWEEN RIBS 23 - 30. CORROSION REMOVED & DAMAGES BLENDED IAW SRI REF DO TS-136 11-14754. AFT SPAR UPPER CAP REPLACED 
- [SDR HYIA20141017088](https://openairdocs.org/sdr/HYIA20141017088), Oct 17, 2014: SPAR. CORRODED. CORROSION FOUND ON RT WING REAR LOWER SPAR. UPON REMOVAL OF PAINT, MAJOR CORROSION WAS FOUND IN AREAS SHOWN IN FIGURE 5. CORROSION WAS CLEANED AWAY & BLENDING W
- [SDR HYIA20141017087](https://openairdocs.org/sdr/HYIA20141017087), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, THE TECHNICIAN FOUND CORROSION ON RT OTBD WING LOWER SURFACE AT MULTIPLE LOCATIONS, BETWEEN RIBS 13 - 23. THE CORROSION WAS CLEANED AWAY 
- [SDR HYIA20141017086](https://openairdocs.org/sdr/HYIA20141017086), Oct 17, 2014: HOUSING. CORRODED. WING ACCESS DOORS 521 DT & 522 CT HOUSINGS CORROSION. CORROSION REMOVED & DAMAGE BLENDED IAW SRI REF DT S-2398 14-21886. IAW EO ATR-57-27-2014.
- [SDR HYIA20141017085](https://openairdocs.org/sdr/HYIA20141017085), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, CORROSION WAS FOUND AT LT WING LOWER SKIN INBD CUT OUTS. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. N
- [SDR HYIA20141017084](https://openairdocs.org/sdr/HYIA20141017084), Oct 17, 2014: SKIN PANEL. DELAMINATED. DURING INSPECTION, DELAMINATION WAS FOUND ON THE RT WING LE PANEL 611. REMOVED DAMAGED AREAS, APPLIED REPAIR PLIES & CURED PER INSTRUCTION. IAW EO ATR-57-25-201
- [SDR HYIA20141017083](https://openairdocs.org/sdr/HYIA20141017083), Oct 17, 2014: SKIN. CORRODED. CORROSION FOUND ON RT WING SKIN, BETWEEN ENG NACELLE RIB 12 & 16. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND. CORROSION WAS CLEANED AWAY & BLENDING WAS PE
- [SDR HYIA20141017082](https://openairdocs.org/sdr/HYIA20141017082), Oct 17, 2014: SKIN PANEL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AROUND THE HOLES ON LOWER SURFACE OF THE RT WING PANEL. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED A
- [SDR HYIA20141017081](https://openairdocs.org/sdr/HYIA20141017081), Oct 17, 2014: SKIN PANEL. DEFORMED. RIGHT WING TE ASSEMBLY LOWER PANEL WAS FOUND TO HAVE A 7.75” X 7.4” X 0.2” AREA OF LAMINATE DEFLECTION. THE DISCREPANT AREA IS LOCATED 6.1” FROM THE INBD EDGE &
- [SDR HYIA20141017080](https://openairdocs.org/sdr/HYIA20141017080), Oct 17, 2014: SKIN PANEL. DEFORMED. RIGHT WING TE ASSEMBLY LOWER PANEL WAS FOUND TO HAVE AN AREA OF LAMINATE DEFLECTION FROM THE ORIGINAL CONTOUR OF UP TO .37” OVER THE LENGTH OF THE PANEL. ACCOMP
- [SDR HYIA20141017079](https://openairdocs.org/sdr/HYIA20141017079), Oct 17, 2014: HINGE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT SPOILER HINGE FASTENER HOLES SHOWN IN FIGURES 5 - 7. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERF
- [SDR HYIA20141017078](https://openairdocs.org/sdr/HYIA20141017078), Oct 17, 2014: SPAR. CORRODED. UPON REMOVAL OF PAINT, CORROSION WAS FOUND AT THE RT WING, UPPER SLAT REAR SPAR AT RIB 13. THIS PART IS A SHIM. AFTER CORROSION WAS CLEANED AWAY & BLENDING WAS 
- [SDR HYIA20141017077](https://openairdocs.org/sdr/HYIA20141017077), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND ON THE LT WING LOWER SKIN SURFACE TE BETWEEN RIBS 4 & 10. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED A
- [SDR HYIA20141017076](https://openairdocs.org/sdr/HYIA20141017076), Oct 17, 2014: SPAR. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT WING LOWER SPAR FLANGE AT RIB 10. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL 
- [SDR HYIA20141017075](https://openairdocs.org/sdr/HYIA20141017075), Oct 17, 2014: STRINGER. GOUGED. RIGHT WING INNER LOWER STRINGER 7 INBD OF RIB 6, GOUGE DAMAGE. UPON INSPECTION, GOUGE SCRAPES WERE FOUND IN THE AREA SHOWN IN FIGURE 3. THE DAMAGE WAS BLENDED A
- [SDR HYIA20171017074](https://openairdocs.org/sdr/HYIA20171017074), Oct 17, 2014: ATTACH FITTING. CORRODED. REPAIR FOR THE RT INBD WING FLAP, CTR ATTACH FITTING SURFACE CORROSION. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND IN AREA. CORROSION WAS CLEANED AWAY & B
- [SDR HYIA20141017073](https://openairdocs.org/sdr/HYIA20141017073), Oct 17, 2014: SKIN. CORRODED. RIGHT WING LOWER SKIN, BETWEEN RIB 5 & 10, SURFACE CORROSION. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFOR
- [SDR HYIA20141017072](https://openairdocs.org/sdr/HYIA20141017072), Oct 17, 2014: SPAR. CORRODED. LEFT HAND SPAR FRONT SLAT, BETWEEN RIB 5 & 10, SURFACE CORROSION. UPON INSPECTION CORROSION & CHAFE DAMAGE WAS DISCOVERED AT THE LT LOWER SLAT AT RIB 5 & 10. ND
- [SDR HYIA20141017071](https://openairdocs.org/sdr/HYIA20141017071), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND ON THE LT WING UPPER SLAT FRONT SPAR BETWEEN RIBS 5 & 6. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT
- [SDR HYIA20141017070](https://openairdocs.org/sdr/HYIA20141017070), Oct 17, 2014: SKIN. CORRODED. SURFACE CORROSION ON THE LT WING LOWER SKIN NACA AREA. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND AROUND PERIMETER OF LT WING LOWER SKIN NACA AREA FWD OF 
- [SDR HYIA20141017069](https://openairdocs.org/sdr/HYIA20141017069), Oct 17, 2014: SKIN. CORRODED. MINOR SURFACE CORROSION FOUND ON LT WING LOWER SKIN. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND ON THE LE SURFACE OF THE LT LOWER SKIN BETWEEN RIBS 28 & 3
- [SDR HYIA20141017068](https://openairdocs.org/sdr/HYIA20141017068), Oct 17, 2014: SPLICE PLATE. CORRODED. WING UPPER SKIN REMOVABLE PANELS EXT SPLICE PLATE CORROSION AT RIB 0. CORROSION BLENDED IAW SRI DT S-2286-14-21888. IAW EO ATR-57-09-2014.
- [SDR HYIA20141017067](https://openairdocs.org/sdr/HYIA20141017067), Oct 17, 2014: SKIN PANEL. DAMAGED. RIGHT WING UPPER SKIN REMOVABLE PANEL OVERSIZED HOLE BETWEEN RIBS 7 & 8 ST FWD LONGERON JUNCTION. HOLE ENLARGED & BUSHING INSTALLED IAW SRI DT S-2606 14-22016. 
- [SDR HYIA20141017066](https://openairdocs.org/sdr/HYIA20141017066), Oct 17, 2014: SLAT. CORRODED. LEFT WING FWD SPAR UPPER STRIP SLAT CORROSION AT RIB 19 PLUS BETWEEN RIBS 23 - 24 & 29 - 30. CORROSION REMOVED & DAMAGES BLENDED IAW SRI REF DT S-1559 14-21618 
- [SDR HYIA20141017065](https://openairdocs.org/sdr/HYIA20141017065), Oct 17, 2014: SKIN. CORRODED. LANDING GEAR WING LOWER SKIN EXT CORROSION AT LE BETWEEN RIBS 19 & 20. CORROSION BLENDED IAW SRI DT S-1551 14-21619. IAW EO ATR-57-06-2014.
- [SDR HYIA20141017064](https://openairdocs.org/sdr/HYIA20141017064), Oct 17, 2014: ANGLE. CORRODED. RIGHT WING UNDERWING BOX ANGLE AT RIB 10 MID AREA VERTICAL FLANGE CORROSION. CORROSION REMOVED & DAMAGE BLENDED IAW SRI RF DT S-1538 14-21620. IAW EO ATR-57-05-
- [SDR HYIA20141017063](https://openairdocs.org/sdr/HYIA20141017063), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND ON RT WING FRONT, LOWER CHORD, BETWEEN RIB 5 & 6, SURFACE CORROSION. UPON REMOVAL OF PAINT, MINOR CORROSION WAS
- [SDR HYIA20141017062](https://openairdocs.org/sdr/HYIA20141017062), Oct 17, 2014: SKIN. CORRODED. WING SKIN SURFACE CORROSION. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND AT LT WING LOWER SKIN BETWEEN RIBS 13 & 30. CORROSION WAS CLEANED AWAY & BLENDING 
- [SDR HYIA20141017061](https://openairdocs.org/sdr/HYIA20141017061), Oct 17, 2014: SPAR. CORRODED. CORROSION RT & LT HORIZONTAL REAR SPAR, LOWER CHORD. DURING INSPECTION CORROSION WAS FOUND ON THE RT & LT HORIZONTAL REAR SPAR, LOWER CHORD. THE SURFACE CORROSI
- [SDR HYIA20141017060](https://openairdocs.org/sdr/HYIA20141017060), Oct 17, 2014: SKIN. CORRODED. CORROSION ON THE RT SIDE HORIZONTAL STABILIZER, UPPER & LOWER SKIN. DURING INSPECTION, CORROSION WAS FOUND AT MULTIPLE PLACES ALONG THE TRAILING SKIN. THE SURFA
- [SDR HYIA20141017059](https://openairdocs.org/sdr/HYIA20141017059), Oct 17, 2014: SKIN. CORRODED. UPON REMOVAL OF PAINT, SURFACE CORROSION LT SIDE OF THE VERTICAL STABILIZER. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT
- [SDR HYIA20141017058](https://openairdocs.org/sdr/HYIA20141017058), Oct 17, 2014: SKIN. CORRODED. CORROSION ON THE LT ELEVATOR TRAILING INBD EDGE UPPER TIP FITTING LOCATION. DURING INSPECTION CORROSION WAS FOUND ON THE LT ELEVATOR TRAILING INBD EDGE. THE SUR
- [SDR HYIA20141017057](https://openairdocs.org/sdr/HYIA20141017057), Oct 17, 2014: ATTACH ANGLE. CORRODED. CORROSION ON AN ATTACH ANGLE ON THE OTBD LT SIDE OF THE ELEVATOR. DURING INSPECTION CORROSION WAS FOUND AT MULTIPLE PLACES ALONG THE ATTACH ANGLE AS SHOWN IN FI
- [SDR HYIA20141017056](https://openairdocs.org/sdr/HYIA20141017056), Oct 17, 2014: FITTING. CORRODED. SURFACE CORROSION ON RT ELEVATOR TE UPPER TIP FITTING. DURING INSPECTION CORROSION WAS FOUND ON THE RT ELEVATOR TE UPPER TIP FITTING & OTBD STATIC WICK BASE. TH
- [SDR HYIA20141017055](https://openairdocs.org/sdr/HYIA20141017055), Oct 17, 2014: SPAR. CORRODED. CORROSION ON RT HORIZONTAL REAR SPAR UPPER CHORD. UPON REMOVAL OF PAINT MINOR CORROSION WAS FOUND IN RT HORIZONTAL REAR SPAR UPPER CHORD. CORROSION WAS CLEANED 
- [SDR HYIA20141017054](https://openairdocs.org/sdr/HYIA20141017054), Oct 17, 2014: FAIRING. OUT OF ALIGNMENT. REPAIR REQUIRED FOR THE MLG BELLY FAIRING PANEL 192FR PN S5247121200900. THE REPAIR IS NECESSARY DUE TO NUMEROUS AREAS OF GAPS & AERODYNAMIC MISMATCH WITH THE A
- [SDR HYIA20141017053](https://openairdocs.org/sdr/HYIA20141017053), Oct 17, 2014: FRAME. CORRODED. FUSELAGE FRAME 24 CORROSION BETWEEN STRINGERS 19 - 20 RHS. CORRODED FRAME PORTION CUT AWAY & NEW PORTION SPLICED AT LEVEL OF STRINGERS 17 LT & RT IAW ADAPTATION
- [SDR HYIA20141017052](https://openairdocs.org/sdr/HYIA20141017052), Oct 17, 2014: SKIN. CORRODED. FUSELAGE SKIN INTERNAL & EXTERNAL CORROSION AT LEVEL OF FRAME 24 BETWEEN STRINGERS 19 - 20 RHS. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRU
- [SDR HYIA20141017051](https://openairdocs.org/sdr/HYIA20141017051), Oct 17, 2014: SKIN. CORRODED. FUSELAGE SKIN INTERNAL CORROSION BETWEEN FRAMES 03 - 04 AT LEVEL OF LT STATIC PORT. CORRODED SKIN AREA BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION IAW EO 
- [SDR HYIA20141017048](https://openairdocs.org/sdr/HYIA20141017048), Oct 17, 2014: STRAP. CORRODED. FUSELAGE FRAME 25 INTERNAL STRAP CORROSION AT STRINGER. CORRODED INTERNAL STRAP PORTION BLENDED OUT & INSPECTED WITHOUT ADDITIONAL FINDINGS FOLLOWING ATR INSTRU
- [SDR HYIA20141017047](https://openairdocs.org/sdr/HYIA20141017047), Oct 17, 2014: SKIN. CORRODED. FUSELAGE SKIN CORROSION AT SERVICE DOOR SURROUND. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION.

All 213: https://openairdocs.org/deregistered/N14834-2019-06-25/reports.md

## 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 19970815027959I](https://openairdocs.org/incident/19970815027959I), Aug 15, 1997: Aerosp ATR42320 (N14834), Newark, NJ. Flew thru aircraft wake. Pitch disconnected. Flew to airport manually. Prior problems with pitch disconnect type.
- [Incident 19920608032039I](https://openairdocs.org/incident/19920608032039I), Jun 8, 1992: Aerosp ATR42320 (N14834), Newark, NJ. Encountered turbulence while maneuvering around cummulus clouds. Flight attendant slightly injured.

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