# Service difficulty reports: N42836, cancelled Jun 26, 2019

A list on [N42836, cancelled Jun 26, 2019](https://openairdocs.org/deregistered/N42836-2019-06-26.md).

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

Page 1 of 3 · 146 reports

- [SDR HYIA20180222001](https://openairdocs.org/sdr/HYIA20180222001.md): Hub · damaged · Feb 22, 2018 · N42836 · Aerosp ATR42320 · Propeller Hub Section
  > DURING ROUTINE BLADE CHANGE DISCOVERED DAMAGE AT BLADE ROOT AND PROPELLER HUB, REMOVED PROPELLER ASSEMBLY FOR FURTHER INVESTIGATION. ADDITIONAL RESULTS TO BE SUPPLIED AS AVAILABLE.
- [SDR HYIA20160624001](https://openairdocs.org/sdr/HYIA20160624001.md): Bulb · failed · Jun 16, 2016 · N42836 · Aerosp ATR42320 · Passenger Compartment Lighting
  > 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 5-AB LATERAL LIGHT BULB PINS TO BE ARCED TO SOCKET. MAINTENANCE R & R THE SOCKET AND LAMP IAW SPM
- [SDR HYIA20160108002](https://openairdocs.org/sdr/HYIA20160108002.md): Fitting · failed · Jan 6, 2016 · N42836 · Aerosp ATR42320 · Landing Gear Actuator
  > PILOT REPORTED WHEN THE GEAR WAS RETRACTED ON DEPARTURE THERE WAS AN UNUSUAL NOISE, GEAR WAS EXTENDED, THE WHOLE PLANE SHOOK & A LOUD NOISE CAME FROM THE RT SIDE. THE RT GEAR TOOK EXTREMELY LONG TO EXTEND. INSPECTED & FOUND THE EXTEND & RETRACT ACTUATOR TO F
- [SDR HYIA20160108001](https://openairdocs.org/sdr/HYIA20160108001.md): Fan · defective · Jan 5, 2016 · N42836 · Aerosp ATR42320 · Air Distribution Fan
  > 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 JIC 21-22-21 RAI 10000. OPERATIONALLY TESTED GOOD IAW 21-22-21-OPT-00100. NO DISTINCTIVE SMELL N
- [SDR HYIA20141217003](https://openairdocs.org/sdr/HYIA20141217003.md): Spar · corroded · Nov 27, 2014 · N42836 · Aerosp ATR42320 · Wing Spar
  > 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 FERRIED WHERE IT WILL UNDERGO HEAVY CHECK & THE PERMANENT REPAIR WILL BE ACCOMPLISHED. SEE ATTACHED D
- [SDR HYIA20141114001](https://openairdocs.org/sdr/HYIA20141114001.md): Controller · dirty · Nov 9, 2014 · N42836 · Aerosp ATR42320 · Cabin Pressure Controller
  > EXCESS CABIN ALTITUDE, REPORTED THEY EXPERIENCED A CABIN DEPRESSURIZATION APPROXIMATELY 45 MILES AWAY FROM DESTINATION ON INITIAL DESCENT. THE CREW THEN DONNED O2 MASKS & FOLLOWED THE QRH & DECLARED AN EMER. LANDING WAS UNEVENTFUL. THE TOWER REPORTED THE C
- [SDR HYIA20141006001](https://openairdocs.org/sdr/HYIA20141006001.md): Battery · malfunctioned · Oct 4, 2014 · N42836 · Aerosp ATR42320 · Battery/Charger System
  > PILOT REPORTED MAIN BATTERY OFF LIGHT ILLUMINATED IN FLIGHT & NOTICED A BURNING SMELL IN COCKPIT. INSPECTED ALL ELEC POWER SYS. REMOVED & INSTALLED MAIN BATTERY, BATTERY CHARGE CONTACTOR, BATTERY PROTECTION UNIT & MAIN BATTERY CHARGE PUSH BUTTON SWITCH IAW A
- [SDR HYIA20141002001](https://openairdocs.org/sdr/HYIA20141002001.md): Symbol Generator · faulted · Oct 2, 2014 · N42836 · Aerosp ATR42320 · Attitude and Direction Data System
  > 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 BRIEFLY ACCOMPANIED ABNORMALITY. SMELL WAS BRIEF, 30 SEC & APPROX HALFWAY THROUGH ABNORMALITY.
- [SDR HYIA20140725001](https://openairdocs.org/sdr/HYIA20140725001.md): Battery · defective · Jul 24, 2014 · N42836 · Aerosp ATR42320 · Battery/Charger System
  > MAIN BATTERY CHARGE OFF LIGHT ILLUMINATED. MX PANEL MAIN BATTERY VOLTS SHOWED 18 VOLTS THEN READ 29. HOWEVER, LIGHT REMAINED ILLUMINATED UNTIL DESCENT 10000 FEET. STRONG BURNING SMELL IN FLIGHT DECK. MX REPLACED MAIN BATTERY. OPERATIONS TEST MAIN BATTERY P
- [SDR HYIA20130928001](https://openairdocs.org/sdr/HYIA20130928001.md): Power Supply · discharged · Sep 28, 2013 · N42836 · Aerosp ATR42* · Emergency Lighting
  > 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.md): Wire · broken · Jul 27, 2013 · N42836 · Aerosp ATR42320 · Landing Gear System Wiring
  > LANDING GEAR WOULD NOT EXTEND NORMALLY. THREE RED UNLOCKED INDICATORS REMAINED ILLUMINATED AFTER SELECTING GEAR DOWN. PERFORMED EMERGENCY LANDING GEAR EXTENSION. GEAR CAME DOWN NORMALLY AND 3 GREEN DOWN AND LOCKED INDICATION WITH NO RED UNLOCK LIGHTS ILLUMI
- [SDR HYIA201305280001](https://openairdocs.org/sdr/HYIA201305280001.md): Vent Line · clogged · May 27, 2013 · N42836 · Aerosp ATR42* · Turbine Engine Oil System
  > 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 VENT TUBE. PERFORMED ENGINE RUNUP AND FOUND TO OPERATE NORMALLY.
- [SDR HYIA20121205002](https://openairdocs.org/sdr/HYIA20121205002.md): Access Door · departed · Dec 1, 2012 · N42836 · Aerosp ATR42320 · Fluid Service Doors
  > 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 INSPECTION, THE DOOR WAS REPLACED.
- [SDR HYIA20111031001](https://openairdocs.org/sdr/HYIA20111031001.md): Spar Cap · corroded · Oct 31, 2011 · N42836 · Aerosp ATR42320 · Wing Spar
  > 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 WAS REMOVED AND DAMAGES BLENDED IAW PREVIOUS SRI. REVIEWED REPAIRS AND ISSUED STRUCTURAL REPAIR A
- [SDR HYIA836HC201121](https://openairdocs.org/sdr/HYIA836HC201121.md): Floorbeam · damaged · Oct 31, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK FLOORBEAM FR13 WAS BEING REPLACED. DURING THE INSTALLATION THE OEM DESIGNED CONTROL CABLE GUIDE THROUGH-HLOES WERE ACCIDENTALLY DRILLED ON THE WRONG (OPPOSITE) SIDE OF THE BL0. REPAIRED IAW STS EA 09-2011-227. REPAIR PERFORMED BY TECH SER
- [SDR HYIA836HC201120](https://openairdocs.org/sdr/HYIA836HC201120.md): Beam · cracked · Oct 31, 2011 · N42836 · Aerosp ATR42320 · Nacelle/Pylon, Main Frame
  > 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, THE MATERAL BETWEEN HOLES WAS FOUND TO BE CRACKED, WITH CRACKS TERMINATING AT EACH HOLE. REPAIRED I
- [SDR HYIA836HC201113A](https://openairdocs.org/sdr/HYIA836HC201113A.md): Frame · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Frame
  > 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 EVALUATION TO BE ACCOMPLISHED WITHIN 12 MONTHS IAW AC120-93.
- [SDR HYIA20111027004](https://openairdocs.org/sdr/HYIA20111027004.md): Skin · corroded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 PERFORMED BY TECH SERVICES UNDER W/O 17010. DTA EVALUATION TO BE ACCOMPLISHED WITH IN 12 MONTHS IAW AC 12
- [SDR HYIA836HC201119](https://openairdocs.org/sdr/HYIA836HC201119.md): Frame · damaged · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Frame
  > 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.md): Structure · debonded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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) COMPOSITE SHOP UNDER W/O 17010.
- [SDR HYIA836HC201117](https://openairdocs.org/sdr/HYIA836HC201117.md): Panel · debonded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 PERFORMED BY TECH SERVICE (MRO)COMPOSITE SHOP UNDER W/O 17010.
- [SDR HYIA836HC201116](https://openairdocs.org/sdr/HYIA836HC201116.md): Cowling · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Powerplant System
  > 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 HOLES IN THE BEAM. THE CRACK WAS REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-013. REPAIR PERFOR
- [SDR HYIA836HC201115](https://openairdocs.org/sdr/HYIA836HC201115.md): Sink · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Lavatories
  > 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. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17010.
- [SDR HYIA836HC201114](https://openairdocs.org/sdr/HYIA836HC201114.md): Skin · corroded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 ENGINEERING SOLUTIONS EA 12-2011-018. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17010.
- [SDR HYIA836HC201113](https://openairdocs.org/sdr/HYIA836HC201113.md): Frame · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Frame
  > 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" THROUGH A.098" HOLE AND INTO THE AFT FACING FLANGE 0.6". REPAIRED IAW STS ENGINEERING SOLUTIONS EA 1
- [SDR HYIA836HC201112](https://openairdocs.org/sdr/HYIA836HC201112.md): Panel · delaminated · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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. REPAIR PERFORMED BY COMPOSITE SHOP UNDER W/O 17010.
- [SDR HYIA836HC201111](https://openairdocs.org/sdr/HYIA836HC201111.md): Panel · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 W/O 17010.
- [SDR HYIA836HC201110](https://openairdocs.org/sdr/HYIA836HC201110.md): Panel · cracked · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 (MRO) COMPOSITE SHOP UNDER W/O 17010.
- [SDR HYIA836HC201109](https://openairdocs.org/sdr/HYIA836HC201109.md): Tube · chafed · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Nacelle/Pylon Miscellaneous Structure
  > 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 IS.0551" AND WITH IN LIMITS. WORK PERFORMED BY ACFT TECH SERVICE UNDER W/O 17010.
- [SDR HYIA836HC201108](https://openairdocs.org/sdr/HYIA836HC201108.md): Skin · corroded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 PREFORMED IAW STS ENGINEERING SOULTIONS EA 12-2011-43. REPAIR PERFORMED BY TECH SERVICES UNDER W/O 17
- [SDR HYIA836HC201107](https://openairdocs.org/sdr/HYIA836HC201107.md): Skin · corroded · Oct 27, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 LIMITS. REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-041. REPAIR PERFORMED UNDER W/O 17010.
- [SDR HYIA20111026005](https://openairdocs.org/sdr/HYIA20111026005.md): Skin · corroded · Oct 26, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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. DTA TO BE ACCOMPLISHED WITHIN 12 MONTHS IAW AC 120-93.
- [SDR HYIA20111026003](https://openairdocs.org/sdr/HYIA20111026003.md): Skin · corroded · Oct 26, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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. REPAIR DOUBLER FABRICATED AND INSP IAW STS ENGINEERING SOLUTIONS EA 12-2011-012. REPAIRS PERFORMED BY
- [SDR HYIA836HC201106](https://openairdocs.org/sdr/HYIA836HC201106.md): Skin · corroded · Oct 26, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 LIMITS. DOUBLER FABRICATED AND INSTALLED IAW STS ENGINEERING SOLUTIONS EA 12-2011-017. REPAIR PERFOR
- [SDR HYIA836HC201105](https://openairdocs.org/sdr/HYIA836HC201105.md): Skin · corroded · Oct 26, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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. REPAIR DOUBLER FABRICATED AND INSTALLED IAW STS ENGINEERING SOLUTIONS EA 12-2011-012. REPAIR PERFORM
- [SDR HYIA20111025001](https://openairdocs.org/sdr/HYIA20111025001.md): Skin · damaged · Oct 25, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 INFORMATION WHICH ISSUED S.R.I. DO/TS-5488/11-16116 FOR REPAIR SPECIFICATIONS. DAMAGED SKIN WAS CUT OU
- [SDR HYIA20111024001](https://openairdocs.org/sdr/HYIA20111024001.md): Frame · corroded · Oct 24, 2011 · N42836 · Aerosp ATR42320 · Fuselage Main, Frame
  > 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 WAS CUT OUT AND NEW PORTION SPLICED IN.
- [SDR HYIA201110200002](https://openairdocs.org/sdr/HYIA201110200002.md): Spar · corroded · Oct 20, 2011 · N42836 · Aerosp ATR42320 · Wing Spar
  > 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.md): Floor Panel · punctured · Oct 20, 2011 · N42836 · Aerosp ATR42320 · Fuselage Floor Panel
  > 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. REPAIRED IAW EA 12-2011-021.
- [SDR HYIA2011101900001](https://openairdocs.org/sdr/HYIA2011101900001.md): Skin · cracked · Oct 19, 2011 · N42836 · Aerosp ATR42320 · Passenger/Crew Doors
  > 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 EA 10-2011-088.
- [SDR HYIA20111019001](https://openairdocs.org/sdr/HYIA20111019001.md): Skin · corroded · Oct 19, 2011 · N42836 · Aerosp ATR42320 · Emergency Exits
  > 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 AND EXCEEDED THE LIMITS OF THE SRM. THE DAMAGE CONSISTS OF A.50" DIA HOLE IN THE INNER SKIN. REPAIR
- [SDR HYIA20111013007](https://openairdocs.org/sdr/HYIA20111013007.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-257.
- [SDR HYIA20111013006](https://openairdocs.org/sdr/HYIA20111013006.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 WERE MADE TO THE PANELS UNDER EA 09-2011-260.
- [SDR HYIA20111013005](https://openairdocs.org/sdr/HYIA20111013005.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-259.
- [SDR HYIA20111013004](https://openairdocs.org/sdr/HYIA20111013004.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 WERE MADE TO THE PANELS UNDER EA 09-2011-258.
- [SDR HYIA20111013003](https://openairdocs.org/sdr/HYIA20111013003.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 LIMITS. REQUEST FOR REPAIRS WERE SUBMITTED TO STS ENGINEERING SOLUTIONS. REPAIRS WERE MADE TO THE PANELS
- [SDR HYIA20111013002](https://openairdocs.org/sdr/HYIA20111013002.md): Panel · cracked · Oct 13, 2011 · N42836 · Aerosp ATR42320 · Fuselage Miscellaneous Structure
  > 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 REPAIRS WERE SUBMITTED TO STS ENGINEERING SOLUTIONS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-2
- [SDR HYIA20110927002](https://openairdocs.org/sdr/HYIA20110927002.md): Spar Cap · corroded · Sep 27, 2011 · N42836 · Aerosp ATR42320 · Wing Spar
  > 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 THEN ISSUED S.R.I. DO/TS-3027/11-15459. REPAIR WAS PERFORMED BY TECH SERVICES UNDER W/O 17010, TASK
- [SDR HYIA20110923001](https://openairdocs.org/sdr/HYIA20110923001.md): Skin · corroded · Sep 23, 2011 · N42836 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 BY TECH SERVICES UNDER W/O 17010. APPROVED UNDER STRUCTURAL REPAIR APPROVAL SHEET (SRAS) DO/TS-303
- [SDR HYIA20110922001](https://openairdocs.org/sdr/HYIA20110922001.md): Skin · corroded · Sep 22, 2011 · N42836 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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-3-3/11-15470 BY TECH SERVICES UNDER W/O 17010. APPROVED UNDER STRUCTURAL REPAIR APPROVAL SHEET (SRAS)

Next page: https://openairdocs.org/deregistered/N42836-2019-06-26/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N42836' AND deregistration_id = 'N42836-2019-06-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N42836-2019-06-26/reports

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