N14834, cancelled Jun 25, 2019

Service difficulty reports · 213

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

Query with SQL
duckdb -csv -c "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 = 'N14834' AND deregistration_id = 'N14834-2019-06-25'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR HYIA20180403002Adc · defectivePILOT 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 COMPUTER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Mar 31, 2018 · N14834 · Aerosp ATR42320 · Air Data ComputerSDR HYIA20160411001Power Supply · inoperativePILOT 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 33-51-21-RAI-10000-002.Apr 10, 2016 · N14834 · Aerosp ATR42320 · Emergency LightingSDR HYIA20160314001Wire · shortedPILOT 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 & AWM 33-21-06. OPERATIONS CHECKED GOOD & NO BURNING SMELL NOTED AT THIS TIME IAW AMM JIC 33-20-00 OPMar 14, 2016 · N14834 · Aerosp ATR42320 · Light System WiringSDR HYIA20160304003Fitting · crackedDURING INSPECTION FCD ATR-2016-32-001, RT MLG ACTUATOR FITTING WAS FOUND CRACKED AT LEVEL OF THE TWO LOWER ATTACHMENT HOLES.Feb 28, 2016 · N14834 · Aerosp ATR42320 · Main Landing Gear Attach SectionSDR HYIA20151030001Bearing · defectivePILOT 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 & RELEASED FOR A FUNCTIONAL FLIGHT CHECK. FLIGHT CHECK WAS SUCCESSFUL WITH NO FURTHER DEFECT NOTED.Oct 27, 2015 · N14834 · Aerosp ATR42320 · Rudder Control SystemSDR HYIA20150904001Ecu · inoperativeAFTER 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, PERFORMED ENG RUN-UP & FOUND TO BE OK IAW MM JIC 73-23-61 RAI 10000. AFTER INITIAL DISCREPANCY CAug 27, 2015 · N14834 · Aerosp ATR42320 · Fuel Control/Turbine EnginesSDR HYIA20150604001Brake Sys · contaminatedPILOT 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 IAW ATR 42 AMM & JIC 32-42-00 BUS10010 NO LEAK NOTED AT THIS TIME, OPERATIONAL TESTED GOOD.Jun 4, 2015 · N14834 · Aerosp ATR42320 · Landing Gear Brake SystemSDR HYIA20150220001BBolt · looseLEFT 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 2014 HEAVY CHECK. SECURED & RE-TORQUED SHACKLE BOLT NUT IAW AMM JIC 20-21-12. NO FURTHER DEFECTS FFeb 18, 2015 · N14834 · Aerosp ATR42320 · Aileron Control SystemSDR HYIA20150220001Bolt · looseLEFT 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 JIC 20-21-12. NO FURTHER DEFECTS FOUND.Feb 18, 2015 · N14834 · Aerosp ATR42320 · Aileron Control SystemSDR HYIA20141017089Spar · corrodedRIGHT 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 FROM RIB 16 TO 30 WITH SPLICES BETWEEN RIBS 16 - 17 & 23 - 24 IAW NEW REPAIR DWG REF 22S572R0331. Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing SparSDR HYIA20141017088Spar · corrodedCORROSION 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 WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMIOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing SparSDR HYIA20141017087Skin · corrodedUPON 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 & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017086Housing · corrodedWING 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.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Miscellaneous StructureSDR HYIA20141017085Skin · corrodedUPON 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. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART WAS FREE OF DEFECTS. IAW Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017084Skin Panel · delaminatedDURING INSPECTION, DELAMINATION WAS FOUND ON THE RT WING LE PANEL 611. REMOVED DAMAGED AREAS, APPLIED REPAIR PLIES & CURED PER INSTRUCTION. IAW EO ATR-57-25-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017083Skin · corrodedCORROSION 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 PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED TOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017082Skin Panel · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE HOLES ON LOWER SURFACE OF THE RT WING PANEL. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PARTOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017081Skin Panel · deformedRIGHT 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 & 4.9” FROM THE AFT EDGE. REMOVED DAMAGED AREAS, POTTED IN DAMAGED AREAS & CURED IAW MANUFACTURER'S Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017080Skin Panel · deformedRIGHT 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. ACCOMPLISH REPAIR, TE ASSEMBLY, WING RT PANEL NR 631BB. REPAIRED BY CUTTING BACK & POTTING IN DAMAGED AROct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017079Hinge · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RT SPOILER HINGE FASTENER HOLES SHOWN IN FIGURES 5 - 7. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THATOct 17, 2014 · N14834 · Aerosp ATR42320 · SpoilersSDR HYIA20141017078Spar · corrodedUPON 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 PERFORMED AT THE LOCAL DAMAGED AREA, NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED TOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing SparSDR HYIA20141017077Skin · corrodedUPON 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 AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS. IAW EO ATR-57-18-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017076Spar · corrodedDURING 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 DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART WAS FREE OOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing SparSDR HYIA20141017075Stringer · gougedRIGHT 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 AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PAROct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Longeron/StringerSDR HYIA20171017074Attach Fitting · corrodedREPAIR 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 & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Control Surface Attach FittingsSDR HYIA20141017073Skin · corrodedRIGHT WING LOWER SKIN, BETWEEN RIB 5 & 10, SURFACE CORROSION. UPON REMOVAL OF PAINT, MINOR CORROSION WAS FOUND. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017072Spar · corrodedLEFT 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. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS. IAW Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing SparSDR HYIA20141017071Skin · corrodedUPON 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 THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART Oct 17, 2014 · N14834 · Aerosp ATR42320 · Leading Edge DevicesSDR HYIA20141017070Skin · corrodedSURFACE 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 THE RAM AIR INLET. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017069Skin · corrodedMINOR 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 & 30. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PEOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017068Splice Plate · corrodedWING 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.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017067Skin Panel · damagedRIGHT 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. IAW EO ATR-57-08-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017066Slat · corrodedLEFT 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 ISSUE B. IAW EO ATR-57-07-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Leading Edge DevicesSDR HYIA20141017065Skin · corrodedLANDING 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.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017064Angle · corrodedRIGHT 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-57-05-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Miscellaneous StructureSDR HYIA20141017063Skin · corrodedUPON 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 FOUND. THE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017062Skin · corrodedWING 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 WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINOct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/SkinSDR HYIA20141017061Spar · corrodedCORROSION RT & LT HORIZONTAL REAR SPAR, LOWER CHORD. DURING INSPECTION CORROSION WAS FOUND ON THE RT & LT HORIZONTAL REAR SPAR, LOWER CHORD. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TOOct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Spar/RibSDR HYIA20141017060Skin · corrodedCORROSION ON THE RT SIDE HORIZONTAL STABILIZER, UPPER & LOWER SKIN. DURING INSPECTION, CORROSION WAS FOUND AT MULTIPLE PLACES ALONG THE TRAILING SKIN. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN POct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Plate/SkinSDR HYIA20141017059Skin · corrodedUPON REMOVAL OF PAINT, SURFACE CORROSION LT SIDE OF THE VERTICAL STABILIZER. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS. IAW EOct 17, 2014 · N14834 · Aerosp ATR42320 · Vertical Stabilizer, Plate/SkinSDR HYIA20141017058Skin · corrodedCORROSION ON THE LT ELEVATOR TRAILING INBD EDGE UPPER TIP FITTING LOCATION. DURING INSPECTION CORROSION WAS FOUND ON THE LT ELEVATOR TRAILING INBD EDGE. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THENOct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator, Plate/SkinSDR HYIA20141017057Attach Angle · corrodedCORROSION 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 FIGURES 2 - 12. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGEDOct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator Miscellaneous StructureSDR HYIA20141017056Fitting · corrodedSURFACE 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. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS Oct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator Miscellaneous StructureSDR HYIA20141017055Spar · corrodedCORROSION 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 AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIOct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Spar/RibSDR HYIA20141017054Fairing · out of alignmentREPAIR REQUIRED FOR THE MLG BELLY FAIRING PANEL 192FR PN S5247121200900. THE REPAIR IS NECESSARY DUE TO NUMEROUS AREAS OF GAPS & AERODYNAMIC MISMATCH WITH THE ADJACENT PANELS. IAW EO ATR-53-69-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Aerodynamic FairingsSDR HYIA20141017053Frame · corrodedFUSELAGE 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 OF SRM REPAIR IAW 53-00-00 FIG 435 FOLLOWING ATR INSTRUCTION. IAW EO ATR-53-68-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, FrameSDR HYIA20141017052Skin · corrodedFUSELAGE SKIN INTERNAL & EXTERNAL CORROSION AT LEVEL OF FRAME 24 BETWEEN STRINGERS 19 - 20 RHS. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION IAW EO ATR-53-67-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/SkinSDR HYIA20141017051Skin · corrodedFUSELAGE SKIN INTERNAL CORROSION BETWEEN FRAMES 03 - 04 AT LEVEL OF LT STATIC PORT. CORRODED SKIN AREA BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION IAW EO ATR-53-66-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/SkinSDR HYIA20141017048Strap · corrodedFUSELAGE FRAME 25 INTERNAL STRAP CORROSION AT STRINGER. CORRODED INTERNAL STRAP PORTION BLENDED OUT & INSPECTED WITHOUT ADDITIONAL FINDINGS FOLLOWING ATR INSTRUCTION IAW EO ATR-53-63-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, FrameSDR HYIA20141017047Skin · corrodedFUSELAGE SKIN CORROSION AT SERVICE DOOR SURROUND. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION.Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
Back to N14834, cancelled Jun 25, 2019