# Service difficulty reports: N131HQ

A list on [N131HQ](https://openairdocs.org/aircraft/N131HQ.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 R61A2025121600546](https://openairdocs.org/sdr/R61A2025121600546.md): Power Supply · faulted · Dec 20, 2025 · N131HQ · Emb ERJ170200LR · Navigation System
  > DURING DECENT INTO JFK THEY HAD A MAU2B FAIL, RECEIVED MULTIPLE FAULT MESSAGES ELE L AND R FAIL, GND PROX FAIL, ADS 2 FAIL, TERRAIN FAIL, WINDSHEAR FAIL, ADSP 3 FAIL, TAT 2 FAIL EMERGENCY DECLARED, LANDED WITHOUT INCIDENT, REMOVED AND REPLACED POWER SUPPLY ON
- [SDR R61A2025121600545](https://openairdocs.org/sdr/R61A2025121600545.md): Fire Loop · faulted · Dec 16, 2025 · N131HQ · Emb ERJ170200LR · Fire Detection
  > ENGINE 1 FIRE ABOVE 10K DIRECT EBAKE. QRC THEN QRH, BLEW BOTH BOTTLES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED ALL E1 FIRE DETECTOR LOOPS, E1 W8, W9, W519 HARNESSES AND ENGINE FIRE BOTTLES A AND B.
- [SDR R61A2024093000439](https://openairdocs.org/sdr/R61A2024093000439.md): Slide · unwanted deploy · Sep 30, 2024 · N131HQ · Emb ERJ170200LR · Escape Slide
  > INADVERTENT SLIDE DEPLOYMENT FROM THE L1 DOOR WHEN CHECKING DOOR CLOSURE. SLIDE DETACHED FROM AIRCRAFT. R&R L1 DOOR SLIDE.
- [SDR R61A2024091900412](https://openairdocs.org/sdr/R61A2024091900412.md): Shear Tie · corroded · Sep 4, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP CORRODED AT FRAME 88 STGR 28R-27R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STGRS 27R-28R REFER SRM 51-40-08.
- [SDR R61A2024091900411](https://openairdocs.org/sdr/R61A2024091900411.md): Shear Tie · corroded · Sep 4, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP CORRODED AT FRAME 88 STGR 29R-28R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STGRS 28R-29R REFER SRM 51-40-08.
- [SDR R61A2024091900410](https://openairdocs.org/sdr/R61A2024091900410.md): Shear Tie · corroded · Aug 29, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP LOCATED AT FR83 AND BETWEEN STR. 27R AND 28R. REMOVED AND REPLACED SHEAR CLIP LOCATED AT FR83 AND BETWEEN STR. 27R AND 28R. REF SRM 51-40-08
- [SDR R61A2024091900409](https://openairdocs.org/sdr/R61A2024091900409.md): Shear Tie · corroded · Aug 29, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP LOCATED AT FR82 AND BETWEEN STR. 27R AND 28R. REMOVED AND REPLACED SHEAR CLIP LOCATED AT FR82 AND BETWEEN STR. 27R AND 28R. REF SRM 51-40-08
- [SDR R61A2024091900408](https://openairdocs.org/sdr/R61A2024091900408.md): Doubler · corroded · Aug 28, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WATER/WASTE DOOR EXTERNAL CUTOUT INNER FLANGE IS CORRODED AS MARKED NEAR BONDING WIRE. REMOVED AND REPLACED WASTE/WATER INNER FLANGE INTERNAL WASTE BOX DOUBLER AND REINSTALLED WASTE BOX AND SHEAR CLIPS REFER SRM 51-40-08
- [SDR R61A2024091900407](https://openairdocs.org/sdr/R61A2024091900407.md): Doubler · dented · Aug 28, 2024 · N131HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REAR FUSELAGE LOWER SKIN PANEL EXTERNAL SIDE HAS 1EA PROTRUDING DENT AT FR 98-99, STGR 29L-29R. PERFORMED REPAIR DOUBLER ON REAR FUSELAGE FR98-99 STGR 29L-29R LOWER SKIN PANEL EXTERNAL SIDE REF SRM 53-30-01/REPAIR 12P
- [SDR R61A2024040500156](https://openairdocs.org/sdr/R61A2024040500156.md): Unknown · odor · Apr 3, 2024 · N131HQ · Emb ERJ170200LR · Air Distribution System
  > SMOKE/BURNING SMELL AFTER TAKEOFF. RAN PACKS 1 AND 2, NO NOTICEABLE SMOKE OR SMELL.
- [SDR R61A2023031400184](https://openairdocs.org/sdr/R61A2023031400184.md): Unknown · unknown · Mar 11, 2023 · N131HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT IN THE COCKPIT DOES NOT WORK. R&R EMERGENCY LIGHT POWER UNIT 1.
- [SDR R61A2022040500236](https://openairdocs.org/sdr/R61A2022040500236.md): None · damaged · Apr 5, 2022 · N131HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > RH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. REPAIRED DAMAGE TO RH HORIZONTAL STABILIZER BEARING FITTING ON O/B SIDE BY BLEND OUT AND SPOT FACE PER ETD2022-170-009919.
- [SDR R61A2022040500235](https://openairdocs.org/sdr/R61A2022040500235.md): Skin Panel · burned · Apr 5, 2022 · N131HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > FIVE LIGHTNING STRIKE WELD MARKS ON LOWER FUSELAGE SKIN FR 3-4, STGR 28L-28R. COMPLIED WITH 3 THROUGH DAMAGE REPAIRS, 1 FREEZE PLUG REPAIR, AND 1 DOUBLER REPAIR ON LOWER FUSELAGE SKIN FR3-4 STGR 28L-28R. REF ETD2022-170-010248 REV: C. SDR WRITTEN FOR DOUBLER R
- [SDR R61A2022040500234](https://openairdocs.org/sdr/R61A2022040500234.md): None · damaged · Apr 5, 2022 · N131HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > LH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. REPAIRED DAMAGE TO LH HORIZONTAL STABILIZER BEARING FITTING ON O/B SIDE BY BLEND OUT AND SPOT FACE PER ETD2022-170-009927
- [SDR R61A2021100800797](https://openairdocs.org/sdr/R61A2021100800797.md): None · none · Oct 6, 2021 · N131HQ · Emb ERJ170200LR · Emergency Lighting
  > MULTIPLE PHOTOLUMINESCENT FLOOR PATH MARKINGS CRACKED OR BUSTED. R&R PHOTOLUMINESCENT FLOOR PATCH.
- [SDR R61A2020022490252](https://openairdocs.org/sdr/R61A2020022490252.md): Light · damaged · Feb 19, 2020 · N131HQ · Emb ERJ170200LR · Emergency Lighting
  > PHOTOLUMINESCENT STRIP AT ROW 19, AIRCRAFT RIGHT, IS DAMAGED. R&R TWO FEET OF DAMAGED PHOTOLUMINESCENT STRIP IAW AMM 33-50-21.
- [SDR R61A2019101631093](https://openairdocs.org/sdr/R61A2019101631093.md): Connector · not seated · Oct 13, 2019 · N131HQ · Emb ERJ170200LR · Light System Wiring
  > EMERGENCY LIGHT BATTERY FAULT ON EICAS. RESEATED CONNECTOR PLUG ON ELPU #2 (FWD LH), OPS CHECK NORMAL.
- [SDR R61A201910011044](https://openairdocs.org/sdr/R61A201910011044.md): Skin · dented · Sep 28, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DENT ON LH FWD FUSELAGE STARTING AT EDGE OF FRAME 10 TO SKIN SPLICE BETWEEN FRAMES 9 &10, STRINGERS 17L-18L. PERFORMED PERMANENT REPAIR BY CUT OUT AND SKIN DOUBLER AT FWD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9L-10L STGR 17L-18L IN ACCORDANCE WITH REFERENCE E
- [SDR R61A201910011038](https://openairdocs.org/sdr/R61A201910011038.md): Skin · dented · Sep 28, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DENT ON LT FWD FUSELAGE STARTING AT EDGE OF FRAME 10 TO SKIN SPLICE BETWEEN FRAMES 9 - 10, STRINGERS 17L-18L. PERFORMED PERMANENT REPAIR BY CUT OUT AND SKIN DOUBLER AT FWD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9L-10L STGR 17L-18L IN ACCORDANCE WITH REFERENCE E
- [SDR R61A201909281013](https://openairdocs.org/sdr/R61A201909281013.md): Support Bracket · corroded · Sep 21, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF RH SHEAR PANEL FRAME 87-88 FOUND GALLEY SUPPORT BRACKET CORRODED. REMOVED AND REPLACED RH SHEAR PANEL FRAME 87-88 GALLEY SUPPORT BRACKET REF SRM 51-40-08. SEE EAMS W/O H6968 SN 426 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909301033](https://openairdocs.org/sdr/R61A201909301033.md): Rib · cracked · Sep 19, 2019 · N131HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: CRACK ON RIB 11A INTERNALLY RH HORIZONTAL STAB BETWEEN MID SPAR AND FRONT SPAR, UPPER RIVET ROW AFT OF 5TH RIVET FROM FRONT SPAR. REFER H6968 TASK CARD #3100:170EO- 55-10-0004_1 AND SEQ #3100 FOR LEFT AND RIGHT HSTAB RIB 10A, 11A & 12A REPLACEMENT. SEE
- [SDR R61A201909301032](https://openairdocs.org/sdr/R61A201909301032.md): Rib · cracked · Sep 19, 2019 · N131HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: CRACK ON RIB 11A INTERNALLY LH HORIZONTAL STAB BETWEEN MID SPAR AND FRONT SPAR, UPPER RIVET ROW AFT OF 5TH RIVET FROM FRONT SPAR. REFER H6968 TASK CARD #3100:170EO-55-10-0004_1 AND SEQ #3100 FOR LEFT AND RIGHT HSTAB RIB 10A, 11A & 12A REPLACEMENT. SEE E
- [SDR R61A201909301031](https://openairdocs.org/sdr/R61A201909301031.md): Rib · cracked · Sep 19, 2019 · N131HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR:CRACK ON RIB 12A INTERNALLY RH HORIZONTAL STAB BETWEEN MID SPAR AND FRONT SPAR, LOWER RIVET ROW AFT OF 6TH RIVET FROM FRONT SPAR. REFER H6968 TASK CARD #3100:170EO-55-10-0004_1 AND SEQ #3100 FOR LEFT AND RIGHT HSTAB RIB 10A, 11A & 12A REPLACEMENT. SEE E
- [SDR R61A201910011045](https://openairdocs.org/sdr/R61A201910011045.md): Stringer · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 19R FROM FRAMES 86-90. PERFORMED STRINGER SPLICE REPAIR ON THE STRINGER PER ETD-170-129275 REV.A AND SRM 53-23-03 Z3.
- [SDR R61A201910011037](https://openairdocs.org/sdr/R61A201910011037.md): Stringer · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 19R APROX FROM FRAMES 86-90. PERFORMED STRINGER SPLICE REPAIR ON STGR 19R BETWEEN FRAMES 86-90 PER ETD-170-129275 REV.A AND SRM 53-23-03 Z3. SEE EAMS W/O H6968 SN 143 FOR WORK DETAILS.
- [SDR R61A201909281012](https://openairdocs.org/sdr/R61A201909281012.md): Seat Track · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION STRUCTURAL CENTER FUSELAGE III DRY AREA 53-23 RH INBD SEAT TRACK FRAME 84 FLANGE. REMOVED DAMAGED SECTION LH INBD SEAT TRACK FRAME 84 REF ETD2019-170-129362 INSTALLED REPAIR PARTS RH INBD SEAT TRACK FRAME 84 REF ETD2019-170-129362 APPLIED SURFACE
- [SDR R61A201909281011](https://openairdocs.org/sdr/R61A201909281011.md): Seat Track · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION STRUCTURAL CENTER FUSELAGE III DRY AREA 53-23 LH INBD SEAT TRACK FRAME 84 FLANGE. REMOVED DAMAGED SECTION BY CUT-OUT LH INBD SEAT TRACK FRAME 84 REF SRM 53-00-10/REPAIR 01 LOCATED AND DRILLED REPAIR PARTS REF ETD2019-170-129362 INSTALLED REPAIR PART
- [SDR R61A201909281010](https://openairdocs.org/sdr/R61A201909281010.md): Splice · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 LH SPLICE FRAME 90. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 LH SPLICE FRAME 90 REF: SRM 51-40-08. SEE EAMS W/O H6968 SN 147 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909281009](https://openairdocs.org/sdr/R61A201909281009.md): Gusset · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH GUSSET PLATE FRAME 90. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH GUSSET PLATE FRAME 90 REF: SRM 51-40-08. SEE EAMS W/O H6968 SN 144 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK
- [SDR R61A201909281008](https://openairdocs.org/sdr/R61A201909281008.md): Splice · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SPLICE FR89. REMOVED AND REPLACED RH SPLICE AT FRAME 89 REF. SRM 51-40-08 RESORED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H6968 SN 142 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909271007](https://openairdocs.org/sdr/R61A201909271007.md): Splice · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 CENTER SPLICE FRAME 89. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 CENTER SPLICE FRAME 89 REF SRM 51-40-08 SEE EAMS W/O H6968 SN 141 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA..
- [SDR R61A201909271006](https://openairdocs.org/sdr/R61A201909271006.md): Upper Sheet · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH UPPERSHEET FR85-86. REMOVED AND REPLACED RH UPPER SHEET AT FRAME 85-86 REF. SRM 51-40-08 RESTORED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H6968 SN 138 FOR WORK DETAILS. AIRCRAFT REMAINS IN
- [SDR R61A201909271005](https://openairdocs.org/sdr/R61A201909271005.md): Upper Sheet · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 LH UPPERSHEET FR85-86. REMOVED AND REPLACED LH UPPER SHEET AT FRAME 85-86 REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H6968 SN 137 FOR WORK DETAILS. AIRCRAFT REMAINS IN
- [SDR R61A201909271004](https://openairdocs.org/sdr/R61A201909271004.md): Beam · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89 PER SRM 51-40-08. SEE EAMS W/O H6968 SN 136 FOR WORK DETAILS. AIRCRAFT REMAINS IN HE
- [SDR R61A201909271003](https://openairdocs.org/sdr/R61A201909271003.md): Panel Support · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT FR 88/90. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT FR 88/90 REF: SRM 51-40-08. SEE EAMS W/O H6968 SN 134 FOR WORK DETAILS. AIRCRAFT REMAINS IN HE
- [SDR R61A201909271002](https://openairdocs.org/sdr/R61A201909271002.md): Shear Panel · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PANEL FRAME 87-88. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PANEL FRAME 87-88 REF: SRM 51-40-08. SEE EAMS W/O H6968 SN 131 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHE
- [SDR R61A201909271001](https://openairdocs.org/sdr/R61A201909271001.md): Shear Panel · corroded · Sep 17, 2019 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL FRAME 87-88. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL FRAME 87-88 REF: SRM 51-40-08. SEE EAMS W/O H6968 SN 130 FOR WORK DETAILS. AIRCRAFT REMAINS IN
- [SDR R61A201806120689](https://openairdocs.org/sdr/R61A201806120689.md): Acm · damaged · Jun 12, 2018 · N131HQ · Emb ERJ170200LR · Cabin Cooling System
  > PACK 1 FAIL ON LANDING, PACK MAKING GRINDING SOUND FOLLOWED BY BURNING SMELL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R NR 1 PACK ACM IAW AMM 21-51-05.
- [SDR R61A201803190380](https://openairdocs.org/sdr/R61A201803190380.md): Light · missing · Mar 19, 2018 · N131HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT STRIP MISSING IN THE FWD CABIN NEAR SEAT 1D. REPLACED THE EMERGENCY LIGHT IAW CMM 33-51-07.
- [SDR R61A201709180709](https://openairdocs.org/sdr/R61A201709180709.md): Skin · damaged · Sep 3, 2017 · N131HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > DAMAGED HOLES FOUND IN THE WING STUB LOWER SKIN AND SPAR II. UNDER THE LT AILERON TUBE SUPPORT FITTING. REPAIRED IAW ETD2017-170-075978. MAJOR REPAIR.
- [SDR R61A201709170702](https://openairdocs.org/sdr/R61A201709170702.md): Doubler · corroded · Sep 3, 2017 · N131HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL WASTE CUTOUT DOUBLER. PERFORMED COMPOSITE REPAIR ON THE WASTE SERVICING BOX IAW SRM 53-23-60.
- [SDR R61A201709170708](https://openairdocs.org/sdr/R61A201709170708.md): Attach Angle · corroded · Sep 1, 2017 · N131HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > PANEL 1431DL HAS TWO BARREL NUT ATTACH ANGLES WITH CORROSION. FOUND CORROSION HAD NO ALLOWABLE LIMITS. REMOVED AND REPLACED THE ATTACH ANGLES IAW AMM 20-10-01.
- [SDR R61A201709170707](https://openairdocs.org/sdr/R61A201709170707.md): Attach Angle · corroded · Sep 1, 2017 · N131HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > PANEL 1441FR ALL BARREL NUT ATTACH ANGLES HAVE CORROSION. FOUND TO BE CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE ATTACH ANGLES IAW AMM 20-10-01.
- [SDR R61A201709170706](https://openairdocs.org/sdr/R61A201709170706.md): Doubler · corroded · Sep 1, 2017 · N131HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION ON THE CROSS BEAM DOUBLER AT FRAME 19, LEFT SIDE. BLENDED THE CORROSION AND FOUND BE OUT OF ALLOWABLE LIMITS IAW SRM 51-75-16. REPAIRED IAW ETD2017-170-074721.
- [SDR R61A201709170705](https://openairdocs.org/sdr/R61A201709170705.md): Seat Track · corroded · Sep 1, 2017 · N131HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION BETWEEN FRAMES 17 - 18 ON THE RT SEAT TRACK. BLENDED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW ETD2017-170-074659.
- [SDR R61A201709170704](https://openairdocs.org/sdr/R61A201709170704.md): Seat Track · corroded · Sep 1, 2017 · N131HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT SEAT TRACK AT FRAME 19. BLENDED THE CORROSION ON THE SEAT TRACK AND FOUND OUT OF ALLOWABLE LIMITS. REMOVED THECORRODED SECTION OF THE SEAT TRACK FILLER AND DOUBLER AND INSTALLED A NEW FILLER AND DOUBLER IAW SRM 53-10-10, REPAIR A.
- [SDR R61A201709170703](https://openairdocs.org/sdr/R61A201709170703.md): Closeout Panel · corroded · Aug 31, 2017 · N131HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT CARGO CUTOUT CLOSE-OUT PANEL HAS CORROSION. FOUND CLOSEOUT BEAM CORRODED OUT OF LIMITS. REMOVED AND REPLACED CLOSEOUT BEAM IAW AMM 20-10-01.
- [SDR R61A201709180710](https://openairdocs.org/sdr/R61A201709180710.md): Hinge · corroded · Aug 30, 2017 · N131HQ · Emb ERJ170200LR · Fuselage, Door Hinge
  > WASTE SERVICE DOOR AND HINGE CORRODED. NO DAMAGE ALLOWED TO DOOR OR HINGE. REMOVED AND REPLACED THE DOOR IAW AMM 53-03-63.
- [SDR R61A201612140734](https://openairdocs.org/sdr/R61A201612140734.md): Actuator · failed · Dec 14, 2016 · N131HQ · Emb ERJ170200LR · Trailing Edge Flap Actuator
  > CREW RECEIVED A FLAP FAIL MESSAGE. CREW RAN QRH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT NR 4 FLAP ACTUATOR IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201603110305](https://openairdocs.org/sdr/R61A201603110305.md): Seal Rest · corroded · Mar 11, 2016 · N131HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, NUT PLATES ALONG INTERNAL EDGE OF FWD CARGO DOOR AFT LOWER SEAL REST ARE CORRODED. MAINTENANCE R & R FWD CARGO DOOR AFT LOWER SEAL REST IAW SRM 175 51-40-02, 51-23-04, PN 170-66803-402 SEAL REST.

Next page: https://openairdocs.org/aircraft/N131HQ/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 = 'N131HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N131HQ/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.