# N42836: Aerospatiale/Aeritalia ATR 42-320, registration cancelled 2019-06-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 26, 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: 200
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 15, 1990
- Certificate issued: January 21, 2015
- Last registry action: November 1, 2017
- Mode S code: A51C37
- Owner when cancelled: [Pcalg Aircraft LLC](https://openairdocs.org/faa-owner/PCALG%20AIRCRAFT%20LLC)
- Location: [Pearce, AZ](https://openairdocs.org/faa-place/AZ/Pearce)
- Physical address: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: LLC
- Owner's area on the map: 31.8760° N, 109.6642° W: Placed by OpenAirDocs at the center of ZIP code 85625, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N42836
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=42836
- Page: https://openairdocs.org/deregistered/N42836-2019-06-26

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 (146, newest 50)

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

- [SDR HYIA20180222001](https://openairdocs.org/sdr/HYIA20180222001), Feb 22, 2018: HUB. DAMAGED. DURING ROUTINE BLADE CHANGE DISCOVERED DAMAGE AT BLADE ROOT AND PROPELLER HUB, REMOVED PROPELLER ASSEMBLY FOR FURTHER INVESTIGATION. ADDITIONAL RESULTS TO BE SU
- [SDR HYIA20160624001](https://openairdocs.org/sdr/HYIA20160624001), Jun 16, 2016: BULB. FAILED. ON CLIMBOUT, CREW SMELLED BURNING ODOR, APPEARED TO BE COMING FROM WEMAC VENTS. MAINTENANCE INSPECTED THE ACFT LIGHTING SYSTEM AND FOUND THE LIGHT SOCKET ON ROW
- [SDR HYIA20160108002](https://openairdocs.org/sdr/HYIA20160108002), Jan 6, 2016: FITTING. FAILED. PILOT REPORTED WHEN THE GEAR WAS RETRACTED ON DEPARTURE THERE WAS AN UNUSUAL NOISE, GEAR WAS EXTENDED, THE WHOLE PLANE SHOOK & A LOUD NOISE CAME FROM THE RT SID
- [SDR HYIA20160108001](https://openairdocs.org/sdr/HYIA20160108001), Jan 5, 2016: FAN. DEFECTIVE. PILOT REPORTED ON APPROACH TO LAND, RECIRCULATION FAN NR 2 FAULTED, BEFORE FAULT THERE WAS A UNIQUE SMELL. REMOVED & INSTALLED NR 2 RECIRCULATION FAN IAW 42 AMM
- [SDR HYIA20141217003](https://openairdocs.org/sdr/HYIA20141217003), Nov 27, 2014: SPAR. CORRODED. TEMPORARY REPAIR PERFORMED TO RT WING FWD SPAR LOWER CHORD IAW ENGINEERING STRUCTURAL REPAIR INSTRUCTION DT S-6990 14-23433 DATED NOV 18, 2014. ACFT WILL BE FER
- [SDR HYIA20141114001](https://openairdocs.org/sdr/HYIA20141114001), Nov 9, 2014: CONTROLLER. DIRTY. EXCESS CABIN ALTITUDE, REPORTED THEY EXPERIENCED A CABIN DEPRESSURIZATION APPROXIMATELY 45 MILES AWAY FROM DESTINATION ON INITIAL DESCENT. THE CREW THEN DONNED 
- [SDR HYIA20141006001](https://openairdocs.org/sdr/HYIA20141006001), Oct 4, 2014: BATTERY. MALFUNCTIONED. PILOT REPORTED MAIN BATTERY OFF LIGHT ILLUMINATED IN FLIGHT & NOTICED A BURNING SMELL IN COCKPIT. INSPECTED ALL ELEC POWER SYS. REMOVED & INSTALLED MAIN BATTERY
- [SDR HYIA20141002001](https://openairdocs.org/sdr/HYIA20141002001), Oct 2, 2014: SYMBOL GENERATOR. FAULTED. FIRST OFFICER`S SIDE EFIS & SGU FAIL FOLLOWED BY INTERMITTENT AHRS FAILURE. AHRS FAIL INCLUDED RADIO ATT GOING TO ZERO WITH GEAR NOT DOWN WARNING. BURNING SMELL
- [SDR HYIA20140725001](https://openairdocs.org/sdr/HYIA20140725001), Jul 24, 2014: BATTERY. DEFECTIVE. MAIN BATTERY CHARGE OFF LIGHT ILLUMINATED. MX PANEL MAIN BATTERY VOLTS SHOWED 18 VOLTS THEN READ 29. HOWEVER, LIGHT REMAINED ILLUMINATED UNTIL DESCENT 10000 FEE
- [SDR HYIA20130928001](https://openairdocs.org/sdr/HYIA20130928001), Sep 28, 2013: POWER SUPPLY. DISCHARGED. EMERGENCY EXIT LIGHTS DO NOT ALL ILLUMINATE DURING TEST. REPLACED POWER SUPPLY UNITS 3WL, 10WL, 15WL, 18WL, 29WL.
- [SDR HYIA201307290001](https://openairdocs.org/sdr/HYIA201307290001), Jul 27, 2013: WIRE. BROKEN. LANDING GEAR WOULD NOT EXTEND NORMALLY. THREE RED UNLOCKED INDICATORS REMAINED ILLUMINATED AFTER SELECTING GEAR DOWN. PERFORMED EMERGENCY LANDING GEAR EXTENSION
- [SDR HYIA201305280001](https://openairdocs.org/sdr/HYIA201305280001), May 27, 2013: VENT LINE. CLOGGED. ON TAXI TO GATE, COCKPIT STARTED TO FILL WITH SMOKE. SELECTED BOTH BLEEDS AND BOTH PACKS TO OFF. INSPECTED NR 1 ENGINE NR 5 BEARING VENT TUBE. CLEANED CLOGGED V
- [SDR HYIA20121205002](https://openairdocs.org/sdr/HYIA20121205002), Dec 1, 2012: ACCESS DOOR. DEPARTED. PILOT REPORTED THAT WHILE CONDUCTING A POST FLIGHT REVIEW OF THE ACFT, THEY NOTED THAT THE HYD BAY ACCESS DOOR 195CL HAD DEPARTED THE ACFT IN FLIGHT. UPON MX IN
- [SDR HYIA20111031001](https://openairdocs.org/sdr/HYIA20111031001), Oct 31, 2011: SPAR CAP. CORRODED. DURING HEAVY CHECK CORROSION ZL-532-GVI-10000, 572220-DVI-10000, SPOTS WERE FOUND ON LT WING AT AFT SPAR UPPER CAP VERTICAL FLANGE BETWEEN RIBS 24-26. CORROSION
- [SDR HYIA836HC201121](https://openairdocs.org/sdr/HYIA836HC201121), Oct 31, 2011: FLOORBEAM. DAMAGED. DURING HEAVY CHECK FLOORBEAM FR13 WAS BEING REPLACED. DURING THE INSTALLATION THE OEM DESIGNED CONTROL CABLE GUIDE THROUGH-HLOES WERE ACCIDENTALLY DRILLED ON TH
- [SDR HYIA836HC201120](https://openairdocs.org/sdr/HYIA836HC201120), Oct 31, 2011: BEAM. CRACKED. DURING HEAVY CHECK OVERSIZED HOLES FOUND IN NR1 ENGINE LOWER COWL BEAM AT OIL LINE SUPPORT BRACKET ATTACH POINT. IN ADDITION TO OVERSIZED AND ELONGATED HOLES, T
- [SDR HYIA836HC201113A](https://openairdocs.org/sdr/HYIA836HC201113A), Oct 27, 2011: FRAME. CRACKED. DURING HEAVY CHECK A CRACK WAS FOUND ON THE LT SIDE OF UPPER FRAME 28. REPAIRED IAW EA 12-2011-010. REPAIR PERFORMED BY TECH SERVICES (MRO) UNDER W/O 17010. DTA
- [SDR HYIA20111027004](https://openairdocs.org/sdr/HYIA20111027004), Oct 27, 2011: SKIN. CORRODED. CORROSION WAS FOUND ON LOWER SKIN AT FRAME 31. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA 12-2011-018. REPAIR PERFORM
- [SDR HYIA836HC201119](https://openairdocs.org/sdr/HYIA836HC201119), Oct 27, 2011: FRAME. DAMAGED. DURING HEAVY CHECK, RT SPONSON FRAME WAS DAMAGED. SPONSON FRAME WAS REPAIRED IAW EA 09/2011-184. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17077.
- [SDR HYIA836HC201118](https://openairdocs.org/sdr/HYIA836HC201118), Oct 27, 2011: STRUCTURE. DEBONDED. DURING HEAVY CHECK THE TRANSVERSE LAVATORY WALL WAS FOUND WITH A LARGE AREA OF DISBOND. WALL REPAIRED IAW EA 14-2011-003. REPAIRS PERFORMED BY TECH SERVICE (MRO
- [SDR HYIA836HC201117](https://openairdocs.org/sdr/HYIA836HC201117), Oct 27, 2011: PANEL. DEBONDED. DURING HEAVY CHECK THE LONGITUDINAL LAVATORY WALL WAS FOUND WITH A LARGE AREA OF DISBOND. WALL REPAIRED IAW STS ENGINEERING SOLUTIONS EA 14-2011-003. REPAIRS PE
- [SDR HYIA836HC201116](https://openairdocs.org/sdr/HYIA836HC201116), Oct 27, 2011: COWLING. CRACKED. DURING HEAVY CHECK A CRACK WAS FOUND ON A BEAM IN THE LT LOWER ENGINE COWLING. THE DAMAGE CONSISTS OF A SINGLE CRACK 1.8" LONG THAT RUNS BETWEEN 2 LIGHTNING HOL
- [SDR HYIA836HC201115](https://openairdocs.org/sdr/HYIA836HC201115), Oct 27, 2011: SINK. CRACKED. DURING HEAVY CHECK LAVATORY WASH BASIN WAS FOUND TO BE CRACKED. THE DAMAGE CONSISTS OF 4 CRACKS. DAMAGE REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-022. R
- [SDR HYIA836HC201114](https://openairdocs.org/sdr/HYIA836HC201114), Oct 27, 2011: SKIN. CORRODED. DURING HEAVY CHECK CORROSION WAS FOUND ON LOWER SKIN AT FRAME 31. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW STS ENGINEE
- [SDR HYIA836HC201113](https://openairdocs.org/sdr/HYIA836HC201113), Oct 27, 2011: FRAME. CRACKED. DURING HEAVY CHECK A CRACK WAS FOUND ON THE LT SIDE OF THE UPPER FRAME 28. THE DAMAGE CONSISTS OF A SINGLE CRACK THAT STARTS MIDWAY DOWN THE WEB RUNNING 1.6" TH
- [SDR HYIA836HC201112](https://openairdocs.org/sdr/HYIA836HC201112), Oct 27, 2011: PANEL. DELAMINATED. DURING HEAVY CHECK NR1 OTBD LATERAL PANEL WAS FOUND TO HAVE A LARGE DELAMINATION OVER THE CORE. PANEL REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-023. REP
- [SDR HYIA836HC201111](https://openairdocs.org/sdr/HYIA836HC201111), Oct 27, 2011: PANEL. CRACKED. DURING HEAVY CHECK, TOILET COMPARTMENT PANEL NR261EW FOUND CRACKED IN 3 PLACES. PANEL REPAIRED IAW STS EA 12-2011-020. REPAIR PERFORMED BY COMPOSITE SHOP UNDER 
- [SDR HYIA836HC201110](https://openairdocs.org/sdr/HYIA836HC201110), Oct 27, 2011: PANEL. CRACKED. DURING HEAVY CHECK SEVERAL CRACKS FOUND ON THE FACE OF INTERIOR PANEL NR261DW. PANEL WAS REPAIRED IAW STS EA 12-2011-019. REPAIR PERFORMED BY ACFT TECH SERVICES
- [SDR HYIA836HC201109](https://openairdocs.org/sdr/HYIA836HC201109), Oct 27, 2011: TUBE. CHAFED. DURING HEAVY CHECK, NR1 ENGINE NR7 MOUNT TUBE FOUND CHAFED. BLENDED IAW ATR 42-320, SRM 54-21-00. ORIGNAL THICKNESS OF TUBE IS .0632", THICKNESS AFTER BLENDING 
- [SDR HYIA836HC201108](https://openairdocs.org/sdr/HYIA836HC201108), Oct 27, 2011: SKIN. CORRODED. DURING HEAVY CHECK CORROSION FOUND ON EXTERIOR SURFACE OF FORWARD KEEL SKIN AT RT ECS CUTOUT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIR PR
- [SDR HYIA836HC201107](https://openairdocs.org/sdr/HYIA836HC201107), Oct 27, 2011: SKIN. CORRODED. DURING HEAVY CHECK CORROSION FOUND ON EXTERIOR SURFACE OF LT FWD KEEL SKIN AT THE LT ECS CUT OUT. REMOVED CORROSION IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMI
- [SDR HYIA20111026005](https://openairdocs.org/sdr/HYIA20111026005), Oct 26, 2011: SKIN. CORRODED. DURING HEAVY CHECK, CORROSION WAS FOUND ON LOWER SKIN AT FRAME 45. REPAIRED IAW STS EA 12-2011-017, REV A. REPAIR PERFORMED BY TECH SERVICES UNDER W/O 17010. DT
- [SDR HYIA20111026003](https://openairdocs.org/sdr/HYIA20111026003), Oct 26, 2011: SKIN. CORRODED. DURING HEAVY CHECK COROSION WAS FOUND ON THE LOWER SKIN AT VHF2 ANTENNA LOCATION. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPA
- [SDR HYIA836HC201106](https://openairdocs.org/sdr/HYIA836HC201106), Oct 26, 2011: SKIN. CORRODED. DURING HEAVY CHECK, CORROSION WAS FOUND ON LOWER SKIN AT FRAME 45 BETWEEN STRINGERS 20R AND 20L. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF L
- [SDR HYIA836HC201105](https://openairdocs.org/sdr/HYIA836HC201105), Oct 26, 2011: SKIN. CORRODED. DURING HEAVY CHECK CORROSION WAS FOUND ON THE LOWER SKIN AT VHF2 ANTENNA LOCATION. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REP
- [SDR HYIA20111025001](https://openairdocs.org/sdr/HYIA20111025001), Oct 25, 2011: SKIN. DAMAGED. DURING HEAVY CHECK INSP, LT AND RT FUSELAGE SKIN WAS DAMAGED BY DRILL MARKS BETWEEN FRAMES 39 TO 42 BELOW STRINGER 14. DAMAGE EXCEED LIMITATIONS. SUBMITTED INFO
- [SDR HYIA20111024001](https://openairdocs.org/sdr/HYIA20111024001), Oct 24, 2011: FRAME. CORRODED. DURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON MLG FAIRING RT WEB SEGMENT AT FRAME 29. CORROSION WAS OUT OF LIMITS PER THE SRM 51-21-58. CORRODED FRAME W
- [SDR HYIA201110200002](https://openairdocs.org/sdr/HYIA201110200002), Oct 20, 2011: SPAR. CORRODED. LT WING-AFT SPAR LOWER CAP HORIZ FLANGE CORROSION BETWEEN RIBS 18-19. DAMAGE BEYOND THE LIMITS IAW THE SRM. DAMAGED SPAR CAP REPLACED IAW REPAIR.
- [SDR HYIA20111020001](https://openairdocs.org/sdr/HYIA20111020001), Oct 20, 2011: FLOOR PANEL. PUNCTURED. DURING HEAVY CHECK, FLOOR PANEL 222CZ REMOVED FOR MX. FOUND IMPACT DAMAGE AND 2 PUNCTURES IN THE FLOOR PANEL. 1 WAS 0.5 " IN LENGTH AND SECOND 1.0" IN LENGTH. R
- [SDR HYIA2011101900001](https://openairdocs.org/sdr/HYIA2011101900001), Oct 19, 2011: SKIN. CRACKED. DURING MX, PASSENGER DOOR INTERIOR SKIN WAS FOUND CRACKED, APPROX 2.25" IN LENGTH RUNNING IN THE UP/DOWN DIRECTION. CRACK THRU INNER SKIN ONLY. REPAIRED IAW STS
- [SDR HYIA20111019001](https://openairdocs.org/sdr/HYIA20111019001), Oct 19, 2011: SKIN. CORRODED. DURING HEAVY CHECK, CORROSION WAS FOUND ON THE EMERGENCY HATCH INNER SKIN AFT OF FRAME 9 AT STA 5136, INBD OF STRINGER 2R. CORROSION REMOVED IAW SRM 51-21-58 AN
- [SDR HYIA20111013007](https://openairdocs.org/sdr/HYIA20111013007), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 241DW WERE FOUND TO HAVE SMALL CRACKS ALONG THE BOTTOM AND MISSING MATERIAL THAT WERE BEYOND SRM LIMITS. REPAI
- [SDR HYIA20111013006](https://openairdocs.org/sdr/HYIA20111013006), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 252CW, 252AW, AND 242EW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REPAIRS W
- [SDR HYIA20111013005](https://openairdocs.org/sdr/HYIA20111013005), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 231FW, AND 2231JW WERE FOUND TO HAVE SMALL CRACKS ALONG THE BOTTOM AND UPPER ANGLE THAT WERE BEYOND SRM LIMITS
- [SDR HYIA20111013004](https://openairdocs.org/sdr/HYIA20111013004), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 232FW,232JW, AND 242AW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REPAIRS WE
- [SDR HYIA20111013003](https://openairdocs.org/sdr/HYIA20111013003), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 251AW, 251CW, AND 251EW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM AND MISSING THAT WERE BEYOND SRM LIMIT
- [SDR HYIA20111013002](https://openairdocs.org/sdr/HYIA20111013002), Oct 13, 2011: PANEL. CRACKED. DURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 242DW AND 242AW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REQUEST FOR REPAI
- [SDR HYIA20110927002](https://openairdocs.org/sdr/HYIA20110927002), Sep 27, 2011: SPAR CAP. CORRODED. DURING HEAVY CHECK INSP RT WING AFT SPAR UPPER CAP WAS CORRODED REF:ZL-632-GVI-10000/572220-DVI-10000 BEYOND LIMITS IAW THE SRM 57-22-00. DAMAGE WAS SUBMITTED T
- [SDR HYIA20110923001](https://openairdocs.org/sdr/HYIA20110923001), Sep 23, 2011: SKIN. CORRODED. DURING HEAVY CHECK INSP, CORROSION WAS FOUND ON LT WING LOWER SKIN AT AFT SPAR NEAR RIBS 6-7. CORROSION WAS REMOVED AND BLENDED IAW SRI REF: DP/TS-3-3/11-15470 
- [SDR HYIA20110922001](https://openairdocs.org/sdr/HYIA20110922001), Sep 22, 2011: SKIN. CORRODED. DURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON LT WING LOWER SKIN AT AFT SPAR NEAR RIBS 4 AND 7. CORROSION WAS REMOVED AND BLENDED IAW SRI REF: DP/TS-3-3

All 146: https://openairdocs.org/deregistered/N42836-2019-06-26/reports.md

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