# Service difficulty reports: N14834, cancelled Jun 25, 2019

A list on [N14834, cancelled Jun 25, 2019](https://openairdocs.org/deregistered/N14834-2019-06-25.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 5 · 213 reports

- [SDR HYIA20180403002](https://openairdocs.org/sdr/HYIA20180403002.md): Adc · defective · Mar 31, 2018 · N14834 · Aerosp ATR42320 · Air Data Computer
  > 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 COMPUTER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.
- [SDR HYIA20160411001](https://openairdocs.org/sdr/HYIA20160411001.md): Power Supply · inoperative · Apr 10, 2016 · N14834 · Aerosp ATR42320 · Emergency Lighting
  > 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 33-51-21-RAI-10000-002.
- [SDR HYIA20160314001](https://openairdocs.org/sdr/HYIA20160314001.md): Wire · shorted · Mar 14, 2016 · N14834 · Aerosp ATR42320 · Light System Wiring
  > 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 & AWM 33-21-06. OPERATIONS CHECKED GOOD & NO BURNING SMELL NOTED AT THIS TIME IAW AMM JIC 33-20-00 OP
- [SDR HYIA20160304003](https://openairdocs.org/sdr/HYIA20160304003.md): Fitting · cracked · Feb 28, 2016 · N14834 · Aerosp ATR42320 · Main Landing Gear Attach Section
  > 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.md): Bearing · defective · Oct 27, 2015 · N14834 · Aerosp ATR42320 · Rudder Control System
  > 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 & RELEASED FOR A FUNCTIONAL FLIGHT CHECK. FLIGHT CHECK WAS SUCCESSFUL WITH NO FURTHER DEFECT NOTED.
- [SDR HYIA20150904001](https://openairdocs.org/sdr/HYIA20150904001.md): Ecu · inoperative · Aug 27, 2015 · N14834 · Aerosp ATR42320 · Fuel Control/Turbine Engines
  > 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, PERFORMED ENG RUN-UP & FOUND TO BE OK IAW MM JIC 73-23-61 RAI 10000. AFTER INITIAL DISCREPANCY C
- [SDR HYIA20150604001](https://openairdocs.org/sdr/HYIA20150604001.md): Brake Sys · contaminated · Jun 4, 2015 · N14834 · Aerosp ATR42320 · Landing Gear Brake System
  > 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 IAW ATR 42 AMM & JIC 32-42-00 BUS10010 NO LEAK NOTED AT THIS TIME, OPERATIONAL TESTED GOOD.
- [SDR HYIA20150220001B](https://openairdocs.org/sdr/HYIA20150220001B.md): Bolt · loose · Feb 18, 2015 · N14834 · Aerosp ATR42320 · Aileron Control System
  > 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 2014 HEAVY CHECK. SECURED & RE-TORQUED SHACKLE BOLT NUT IAW AMM JIC 20-21-12. NO FURTHER DEFECTS F
- [SDR HYIA20150220001](https://openairdocs.org/sdr/HYIA20150220001.md): Bolt · loose · Feb 18, 2015 · N14834 · Aerosp ATR42320 · Aileron Control System
  > 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 JIC 20-21-12. NO FURTHER DEFECTS FOUND.
- [SDR HYIA20141017089](https://openairdocs.org/sdr/HYIA20141017089.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Spar
  > 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 FROM RIB 16 TO 30 WITH SPLICES BETWEEN RIBS 16 - 17 & 23 - 24 IAW NEW REPAIR DWG REF 22S572R0331.
- [SDR HYIA20141017088](https://openairdocs.org/sdr/HYIA20141017088.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Spar
  > 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 WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMI
- [SDR HYIA20141017087](https://openairdocs.org/sdr/HYIA20141017087.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOS
- [SDR HYIA20141017086](https://openairdocs.org/sdr/HYIA20141017086.md): Housing · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Miscellaneous Structure
  > 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.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART WAS FREE OF DEFECTS. IAW
- [SDR HYIA20141017084](https://openairdocs.org/sdr/HYIA20141017084.md): Skin Panel · delaminated · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > DURING INSPECTION, DELAMINATION WAS FOUND ON THE RT WING LE PANEL 611. REMOVED DAMAGED AREAS, APPLIED REPAIR PLIES & CURED PER INSTRUCTION. IAW EO ATR-57-25-2014.
- [SDR HYIA20141017083](https://openairdocs.org/sdr/HYIA20141017083.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED T
- [SDR HYIA20141017082](https://openairdocs.org/sdr/HYIA20141017082.md): Skin Panel · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART
- [SDR HYIA20141017081](https://openairdocs.org/sdr/HYIA20141017081.md): Skin Panel · deformed · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 & 4.9” FROM THE AFT EDGE. REMOVED DAMAGED AREAS, POTTED IN DAMAGED AREAS & CURED IAW MANUFACTURER'S
- [SDR HYIA20141017080](https://openairdocs.org/sdr/HYIA20141017080.md): Skin Panel · deformed · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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. ACCOMPLISH REPAIR, TE ASSEMBLY, WING RT PANEL NR 631BB. REPAIRED BY CUTTING BACK & POTTING IN DAMAGED AR
- [SDR HYIA20141017079](https://openairdocs.org/sdr/HYIA20141017079.md): Hinge · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Spoilers
  > 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 PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT
- [SDR HYIA20141017078](https://openairdocs.org/sdr/HYIA20141017078.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Spar
  > 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 PERFORMED AT THE LOCAL DAMAGED AREA, NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED T
- [SDR HYIA20141017077](https://openairdocs.org/sdr/HYIA20141017077.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS. IAW EO ATR-57-18-2014.
- [SDR HYIA20141017076](https://openairdocs.org/sdr/HYIA20141017076.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Spar
  > 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 DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART WAS FREE O
- [SDR HYIA20141017075](https://openairdocs.org/sdr/HYIA20141017075.md): Stringer · gouged · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Longeron/Stringer
  > 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 AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PAR
- [SDR HYIA20171017074](https://openairdocs.org/sdr/HYIA20171017074.md): Attach Fitting · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Control Surface Attach Fittings
  > 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 & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS
- [SDR HYIA20141017073](https://openairdocs.org/sdr/HYIA20141017073.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > RIGHT 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
- [SDR HYIA20141017072](https://openairdocs.org/sdr/HYIA20141017072.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Spar
  > 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. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS. IAW
- [SDR HYIA20141017071](https://openairdocs.org/sdr/HYIA20141017071.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Leading Edge Devices
  > 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 THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART
- [SDR HYIA20141017070](https://openairdocs.org/sdr/HYIA20141017070.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 THE RAM AIR INLET. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA.
- [SDR HYIA20141017069](https://openairdocs.org/sdr/HYIA20141017069.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 & 30. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PE
- [SDR HYIA20141017068](https://openairdocs.org/sdr/HYIA20141017068.md): Splice Plate · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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.md): Skin Panel · damaged · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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. IAW EO ATR-57-08-2014.
- [SDR HYIA20141017066](https://openairdocs.org/sdr/HYIA20141017066.md): Slat · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Leading Edge Devices
  > 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 ISSUE B. IAW EO ATR-57-07-2014.
- [SDR HYIA20141017065](https://openairdocs.org/sdr/HYIA20141017065.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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.md): Angle · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing Miscellaneous Structure
  > 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-57-05-2014.
- [SDR HYIA20141017063](https://openairdocs.org/sdr/HYIA20141017063.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 FOUND. THE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT W
- [SDR HYIA20141017062](https://openairdocs.org/sdr/HYIA20141017062.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Wing, Plate/Skin
  > 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 WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMIN
- [SDR HYIA20141017061](https://openairdocs.org/sdr/HYIA20141017061.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Spar/Rib
  > CORROSION 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 TO
- [SDR HYIA20141017060](https://openairdocs.org/sdr/HYIA20141017060.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Plate/Skin
  > CORROSION 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 P
- [SDR HYIA20141017059](https://openairdocs.org/sdr/HYIA20141017059.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Vertical Stabilizer, Plate/Skin
  > 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 WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS. IAW E
- [SDR HYIA20141017058](https://openairdocs.org/sdr/HYIA20141017058.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator, Plate/Skin
  > 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 SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN
- [SDR HYIA20141017057](https://openairdocs.org/sdr/HYIA20141017057.md): Attach Angle · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator Miscellaneous Structure
  > 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 FIGURES 2 - 12. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED
- [SDR HYIA20141017056](https://openairdocs.org/sdr/HYIA20141017056.md): Fitting · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Elevator Miscellaneous Structure
  > 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. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREA. NDT WAS
- [SDR HYIA20141017055](https://openairdocs.org/sdr/HYIA20141017055.md): Spar · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Horizontal Stabilizer, Spar/Rib
  > 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 AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERI
- [SDR HYIA20141017054](https://openairdocs.org/sdr/HYIA20141017054.md): Fairing · out of alignment · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Aerodynamic Fairings
  > 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 ADJACENT PANELS. IAW EO ATR-53-69-2014.
- [SDR HYIA20141017053](https://openairdocs.org/sdr/HYIA20141017053.md): Frame · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Frame
  > 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 OF SRM REPAIR IAW 53-00-00 FIG 435 FOLLOWING ATR INSTRUCTION. IAW EO ATR-53-68-2014.
- [SDR HYIA20141017052](https://openairdocs.org/sdr/HYIA20141017052.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR HYIA20141017051](https://openairdocs.org/sdr/HYIA20141017051.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > 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 ATR-53-66-2014.
- [SDR HYIA20141017048](https://openairdocs.org/sdr/HYIA20141017048.md): Strap · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Frame
  > FUSELAGE 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.
- [SDR HYIA20141017047](https://openairdocs.org/sdr/HYIA20141017047.md): Skin · corroded · Oct 17, 2014 · N14834 · Aerosp ATR42320 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORROSION AT SERVICE DOOR SURROUND. CORRODED SKIN AREAS BLENDED OUT & INSPECTED FOLLOWING ATR INSTRUCTION.

Next page: https://openairdocs.org/deregistered/N14834-2019-06-25/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 = 'N14834' AND deregistration_id = 'N14834-2019-06-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14834-2019-06-25/reports

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