# Service difficulty reports: N115HQ

A list on [N115HQ](https://openairdocs.org/aircraft/N115HQ.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 · 112 reports

- [SDR R61A2026090200247](https://openairdocs.org/sdr/R61A2026090200247.md): Control Lever · inoperative · Sep 2, 2026 · N115HQ · Emb ERJ170200LR · Landing Gear Selector
  > LANDING GEAR DID NOT RETRACT DURING TAKE OFF AND LG LEVER DISAG MESSAGE POPULATED. RAN QRH PROCEDURE, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. R&R LANDING GEAR CONTROL LEVER.
- [SDR R61A2026012800031](https://openairdocs.org/sdr/R61A2026012800031.md): Rib · cracked · Jan 29, 2026 · N115HQ · Emb ERJ170200LR · Wing, Rib/Bulkhead
  > WHILE IN HEAVY CHECK, A CRACK WAS FOUND ON LT WING WHEEL WELL OPENING ON THE FWD EDGE, BETWEEN RIB 3 AND 4.
- [SDR R61A2026020200017](https://openairdocs.org/sdr/R61A2026020200017.md): Skin · cracked · Jan 16, 2026 · N115HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > HEAVY CHECK - CRACK ON RH WING LEADING EDGE AT SLAT TRACK #4. PERFORMED CUTOUT AND INSTALLED DOUBLER REPAIR PER ETD 2026-170-000933 REV A
- [SDR R61A2026020200018](https://openairdocs.org/sdr/R61A2026020200018.md): Skin · cracked · Jan 13, 2026 · N115HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > WHILE ON HEAVY CHECK, A CRACK WAS FOUND ON LT WING LEADING EDGE AT SLAT TRACK NR 4.
- [SDR R61A2026020200016](https://openairdocs.org/sdr/R61A2026020200016.md): Skin · cracked · Jan 13, 2026 · N115HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > HEAVY CHECK - CRACK ON LT WING LEADING EDGE AT SLAT TRACK #5. PERFORMED CUTOUT AND INSTALLED DOUBLER REPAIR PER ETD2026-170-000858 REV A
- [SDR R61A2024072600328](https://openairdocs.org/sdr/R61A2024072600328.md): Hydraulic Line · failed · Jul 23, 2024 · N115HQ · Emb ERJ170200LR · Hydraulic System, Main
  > HYD 2 LO QTY. LOST ALL HYD FLUID IN #2. HYD 2 FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R MLG HYDRAULIC LINE. NO LEAKS PRESENT.
- [SDR R61A2023101300580](https://openairdocs.org/sdr/R61A2023101300580.md): Slide · partial deploy · Oct 10, 2023 · N115HQ · Emb ERJ170200LR · Escape Slide
  > L1 SLIDE PARTIAL DEPLOYED. R&R L1 DOOR SLIDE ASSEMBLY
- [SDR R61A2023090800490](https://openairdocs.org/sdr/R61A2023090800490.md): Shear Tie · corroded · Aug 27, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > LOW SKIN PNL SHEAR CLIP AT FR 83, BETW STR 27R-28R CORRODED OFF LIMITS. R&R IAW SRM 51-41-01 & 51-41-02.
- [SDR R61A2023090800487](https://openairdocs.org/sdr/R61A2023090800487.md): Support Angle · corroded · Aug 24, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO SUPPORT ANGL BRKT AT FR 80 STR 25R-26R CORRODED. R&R IAW 51-41-02 &51-43-03.
- [SDR R61A2023090800486](https://openairdocs.org/sdr/R61A2023090800486.md): Skin · cracked · Aug 24, 2023 · N115HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > RH WING FIXED L/E SKIN AT BTWN RIB 14-15 CRACKED. REPAIRED IAW SRM 57-49-01 & ETD2023-170-021301 REV:A
- [SDR R61A2023090800491](https://openairdocs.org/sdr/R61A2023090800491.md): Seat Track · corroded · Aug 21, 2023 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSG R/H I/B SEAT TRACK BETW FR12-20 CORRODED. R&R IAW SRM 51-41-02, 51-43-03 & 51-43-04.
- [SDR R61A2023090800489](https://openairdocs.org/sdr/R61A2023090800489.md): Shear Tie · corroded · Aug 21, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > LOW SKIN PNL SHEAR CLIP AT FR 81, BETW STR 28-29 CORRODED OFF LIMITS. R&R IAW SRM 51-41-01 & 51-41-02.
- [SDR R61A2023090800488](https://openairdocs.org/sdr/R61A2023090800488.md): Shear Tie · corroded · Aug 21, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > LOWER SKIN PNL SHEAR CLIP AT FR 88 BETW STR 27R-28R CORRODED OFF LIMITS. R&R IAW SRM 51-41-02 & 51-43-03.
- [SDR R61A2023090800492](https://openairdocs.org/sdr/R61A2023090800492.md): Gusset · corroded · Aug 20, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > PAX FLOOR STRUCTURE GUSSET PLATE AT FR 90, RBL 18-27 CORRODED. R&R IAW SRM 51-41-02.
- [SDR R61A2023090800494](https://openairdocs.org/sdr/R61A2023090800494.md): Shear Tie · corroded · Aug 20, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > LOW SKIN PNL SHEAR CLIP AT FR 82, BETW STR 27R-28R CORRODED OFF LIMITS. R&R IAW SRM 51-41-01 & 51-41-02.
- [SDR R61A2023090800493](https://openairdocs.org/sdr/R61A2023090800493.md): Gusset · corroded · Aug 20, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > PAX FLOOR STRUCTURE GUSSET PLATE AT FR 90, RBL 9-12 CORRODED. R&R IAW SRM 51-41-02.
- [SDR R61A2023090800495](https://openairdocs.org/sdr/R61A2023090800495.md): Shear Plate · corroded · Aug 20, 2023 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > PAX FLOOR STRUC SHEAR PLATE CORRODED BTWN FR 87-88, RBL 9 - LBL 9. R&R IAW SRM 51-42-01.
- [SDR R61A2022113000762](https://openairdocs.org/sdr/R61A2022113000762.md): Stringer · corroded · Nov 25, 2022 · N115HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > DURING A BI-WEEKLY INSPECTION, FOUND 5TH RIVET AFT OF FRAME 90 ON STRINGER 28L HEAD WAS POPPED OFF AND SKIN SLIGHTLY BULDGED OUT. UPON FURTHER INVESTAGATION FOUND CORRISION UNDER STR 28L. REMOVED AND REPLACED STR 28L IAW ETD2022-170-035434.
- [SDR R61A2022071300429](https://openairdocs.org/sdr/R61A2022071300429.md): Control Valve · leaking · Jul 8, 2022 · N115HQ · Emb ERJ170200LR · Hydraulic System, Main
  > INFLIGHT, HYDRAULIC 1 LOW QUANTITY. IT STAYED ABOUT 16%-14% FOR THE REMAINER OF THE FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND OUTBOARD BRAKE CONTROL VALVE BODY LEAKING. R&R OUTBOARD BRAKE CONTROL VALVE.
- [SDR R61A2021072800611](https://openairdocs.org/sdr/R61A2021072800611.md): Skin · dented · Jul 22, 2021 · N115HQ · Emb ERJ170200LR · Horizontal Stabilizer, Plate/Skin
  > L/H HORIZONTAL STAB LOWER SKIN DENTED BETWEEN RIBS 8 AND 9 PERFORMED TEMPORARY REPAIR BY CUTOUT, FILLER AND DOUBLER REPAIR ON L/H HORIZONTAL STAB LOWER SKIN BETWEEN RIBS 8 AND 9 IN ACCORDANCE WITH,REF ETD2021-170-024022, AERNNOVA TI-170-21-113.
- [SDR R61A2021072800607](https://openairdocs.org/sdr/R61A2021072800607.md): Attach Angle · elongated · Jul 20, 2021 · N115HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > THIS CARD CREATED FOR 1EA. STUCK FASTENER AT FR 52 SUPPORT RIB UPPER ATTACHMENT ANGLE. REMOVED DAMAGE BY REAMING HOLE DIAMETER TO (.547"). REF: ETD2021-170-023727 REV-.:/ SRM 51-40-02.PERFORMED HFEC ROTO PROBE HOLE INSPECTION, NO DEFECTS NOTED I/A/W NDT MANUA
- [SDR R61A2021072800609](https://openairdocs.org/sdr/R61A2021072800609.md): Door Frame · damaged · Jul 12, 2021 · N115HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > R2 DOOR AFT FRAME HAS MISS DRILLED HOLE FOR LOWER ISOLATOR MOUNT. REPAIRED DAMAGED HOLE ON R2 DOOR AFT FRAME LOWER ISOLATOR MOUNT BY INSTALLING BUSHING REF ETD2021-170-022616 REV B
- [SDR R61A2021072800610](https://openairdocs.org/sdr/R61A2021072800610.md): Doubler · corroded · Jul 6, 2021 · N115HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > L/H SIDE OF CAPT'S CONTROL COLUMN FLOOR SKIN SILL HAS CORROSION PERFORMED SPLICE REPAIR ON L/H SIDE OF CAPT'S CONTROL COLUMN FLOOR SKIN REF ETD2021-170--022251.
- [SDR R61A2021020200138](https://openairdocs.org/sdr/R61A2021020200138.md): Door · lack of lube · Jan 30, 2021 · N115HQ · Emb ERJ170200LR · Passenger/Crew Doors
  > L1 DOOR HARD TO OPEN AND CLOSE. CLEANED AND LUBED L1 DOOR MECHANISMS, OPS CHECK GOOD.
- [SDR R61A2020090300605](https://openairdocs.org/sdr/R61A2020090300605.md): Oxygen System · false indication · Aug 30, 2020 · N115HQ · Emb ERJ170200LR · Oxygen System
  > CREW OXYGEN LOW PRESSURE EICCAS MESSAGE APPEARED FOR 2 SECONDS WITH OBSERVER OXYGEN LOW PRESSURE IN BLUE. NO O2 CHANGES OBSERVED, NO CRE ALTITUDE FLUCTUATIONS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. OXYGEN PRESSURE HAS NOT DROPPED AFTER 50 MINUTES, RE
- [SDR R61A2020071400564](https://openairdocs.org/sdr/R61A2020071400564.md): Power Unit · discharged · Jul 11, 2020 · N115HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY BATTERY FAULT ON EICAS. PERFORMED FIM TASK 33-50-00-810-802-1. CHARGED ELPU REF AMM 33-50-01.
- [SDR R61A201909040938](https://openairdocs.org/sdr/R61A201909040938.md): Battery · failed · Sep 4, 2019 · N115HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY BACK UP BATTERY FAILED FUNCTIONAL TEST. R&R EMERGENCY BATTERY PER AMM 22-03-09.
- [SDR R61A201901080034](https://openairdocs.org/sdr/R61A201901080034.md): Floor Support · corroded · Dec 16, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON RT AFT FLOOR SUPPORT AT FR84. REMOVED AND REPLACED RT AFT FLOOR SUPPORT PANEL PN: 170-92908-001 REF SRM 51-40-08. SEE W/O H6589 SN 404 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901080036](https://openairdocs.org/sdr/R61A201901080036.md): Threshold · corroded · Dec 15, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > R2 THRESHOLD HAS SURFACE CORROSION AROUND FWD. AND AFT. GIRT BAR FITTINGS AS MARKED. REPLACED R2 THRESHOLD WITH NEW REF. SRM 53-23-11/AD03, 51-40-08, 51-40-02, 51-23-04, 51-23-05, 51-23-06 AND CPM 51-25-00. P/N 170-65639-005. TOP COATED. SEE W/O H6589 SN 332 F
- [SDR R61A201901080035](https://openairdocs.org/sdr/R61A201901080035.md): Threshold · corroded · Dec 14, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > L2 THRESHOLD HAS SURFACE CORROSION AROUND FWD. AND AFT. GIRT BAR FITTINGS AS MARKED. REPLACED L2 THRESHOLD WIT H NEW AND TOP COATED REF. SRM 53-23-11/AD03, 51-40-08, 51-40-02, 51-23-06 AND CPM 51-25-00. P/N 170-65703-005. SEE W/O H6589 SN 275 FOR WORK DETAIL
- [SDR R61A201901080033](https://openairdocs.org/sdr/R61A201901080033.md): Threshold · corroded · Dec 14, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > L1 THRESHOLD HAS SURFACE CORROSION AROUND AFT. GIRT BAR FITTINGS AS MARKED. REPLACED THRESHOLD WITH NEW REF. SRM 53-10-11/AD02, 51-40-08, 51-40-02, 51-23-04, AMM 20-10-01 AND TOP COATED SRM 51-23-06. P/N 170-03719-005. SEE W/O H6589 SN 296 FOR WORK DETAILS.
- [SDR R61A201901080032](https://openairdocs.org/sdr/R61A201901080032.md): Floor Support · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN FWD. WET AREA FLOOR PANEL SUPPORT (PT166) AT FR.17 AS MARKED. REPLACED FLOOR PANEL SUPPORT WITH NEW, REF. SRM 51-10-03, 51-40-08, 51-40-02, 51-23-04, 51-23-06 AND CPM 51-25-00. P/N 170-13939-001. SEE W/O H6589 SN 235 FOR WORK DETAILS. AIRCRAFT R
- [SDR R61A201901080031](https://openairdocs.org/sdr/R61A201901080031.md): Floorbeam · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION IN FWD WET AREA RT TRACK FLOORBEAM IN 2 LOCATIONS BETWEEN FR15 AND FR18 AS MARKED. REMOVED CORROSION FROM THE FWD WET AREA RT TRACK FLOORBEAM IN 2 LOCATIONS BETWEEN FR15 AND FR18 REF EMB SRM 51-10-03. MATERIAL LOSS IS.013" WHICH IS OUT OF LIMITS.
- [SDR R61A201901080030](https://openairdocs.org/sdr/R61A201901080030.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN FWD WET AREA LT TRACK FLOOR BEAM IN 3 LOCATIONS FROM FR16 TO FR20 AS MARKED. REMOVED AND INSTALLED NEW LT I/B SEAT TRACK FROM FRAMES 12-20 REF SRM 51--40-08 APPLIED TOPCOAT AND C.I.C TO L/H I/B SEAT TRACK FROM FRAMES 12-20 REF: SRM 51-23-06 SEE W
- [SDR R61A201901080029](https://openairdocs.org/sdr/R61A201901080029.md): Splice · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT. WET AREA SPLICE P/N 170-86119-005 HAS CORROSION FR 90. REPLACED SPLICE WITH NEW AND TOP COATED REF. SRM 51-75-16, 51-40-08, 51-40-03 AND 51-23-06. SEE W/O H6589 SN 220 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070018](https://openairdocs.org/sdr/R61A201901070018.md): Beam · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA RT BEAM P/N 170-65669-002 IS CORRODED FR86-89 REMOVED AND REPLACED RT BEAM PN: 170-65669-004 REF SRM 51-43-01. SEE W/O H6589 SN 219 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070017](https://openairdocs.org/sdr/R61A201901070017.md): Upper Sheet · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA UPPER SHEET P/N 170-86101-001 IS CORRODED FR85-86. REMOVED AND REPLACED UPPER SHEET PN: 170-86101-001 REF EMB SRM 51-43-01. SEE W/O H6589 SN 217 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070016](https://openairdocs.org/sdr/R61A201901070016.md): Panel Support · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA CENTER PANEL SUPPORT IS CORRODED FR87-88. REMOVED AND REPLACED CENTER PANEL SUPPORT PN: 170-65928-001 REF SRM 51-43-01.
- [SDR R61A201901070015](https://openairdocs.org/sdr/R61A201901070015.md): Shear Panel · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA RT SHEAR PANEL IS CORRODED FR87-88. REMOVED AND REPLACED RT SHEAR PLATE PN: 17091919-001 REF SRM 51-42-01. SEE W/O H6589 SN 215 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070014](https://openairdocs.org/sdr/R61A201901070014.md): Panel Support · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA RT PANEL SUPPORT IS CORRODED FR88-90. REMOVED AND REPLACED RT PANEL SUPPORT PN: 170-86181-005 REF SRM 51-40-08. RESTORE FINISH REF SRM 51-23-04, 51-23-05 AND 51-23-06. SEE W/O H6589 SN 214 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070013](https://openairdocs.org/sdr/R61A201901070013.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > NICKS AND CORROSION ON RT CENTER SET TRACK FR 74 THRU 84. REMOVED AND REPLACED SECTION OF SEAT TRACK PN: 170-86082-005 AT FRAME 82 THRU 84 REF ETD2018-170-133078. REMAINING TRACK FROM 74 TO 82 FOUND WITHIN LIMITS REF SRM 53-23-10 AD01 RESTORE FINISH REF SRM 51
- [SDR R61A201901070012](https://openairdocs.org/sdr/R61A201901070012.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > NICKS AND CORROSION ON LT CENTER SET TRACK FR 74 THRU 84. REMOVED AND REPLACED SECTION OF SEAT TRACK PN: 170-86081-005 AT FRAME 81 THRU 84 REF EMB ETD2018-170-133071. REMAINING TRACK FROM 74 TO 81 FOUND WITHIN LIMITS REF SRM 53-23-10 AD01 RESTORE FINISH REF S
- [SDR R61A201901070011](https://openairdocs.org/sdr/R61A201901070011.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > NICKS AND CORROSION ON RH CENTER SET TRACK FR 23 THRU 34/43. REMOVED AND REPLACED SECTION OF SEAT TRACK BETWEEN FRAME 31 AND 34 PN: 170-67660-431 REF. ETD2018-170-133197 REMAINING AREA FOUND TO BE WITHIN LIMITS REF SRM 53-21-10 AD01. SEE W/O H6589 SN 203 FOR
- [SDR R61A201901070010](https://openairdocs.org/sdr/R61A201901070010.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES/CORROSION ON RT WALL SEAT TRACK FR 74 THRU 84. REMOVED AND REPLACED RT WALL SEAT TRACK AT FR 74 THRU 84. REF: SRM 51-40-08. SEE W/O H6589 SN 201 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201901070009](https://openairdocs.org/sdr/R61A201901070009.md): Seat Track · corroded · Dec 13, 2018 · N115HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT WALL SEAT TRACK AT FR 73. REMOVED AND REPLACED LT O/B SEAT TRACK AT FR 60-73, APPLIED TOPCOAT TO INSTALL FASTENERS ON LT O/B SEAT TRACK AT FR 60-73 REF SRM 51-23-06. SEE W/O H6589 SN 195 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A2018112641175](https://openairdocs.org/sdr/R61A2018112641175.md): Warning Message · false activation · Nov 24, 2018 · N115HQ · Emb ERJ170200LR · Trailing Edge Flap Control System
  > FLAP FAIL EICAS IN FLIGHT. DECLARED EMERGENCY, DIVERTED TO IAD, LANDED WITHOUT INCIDENT. PERFORMED FIM IAW 25-51-00. OPS CHECK GOOD.
- [SDR R61A201712130933](https://openairdocs.org/sdr/R61A201712130933.md): Skin · dented · Dec 12, 2017 · N115HQ · Emb ERJ170200LR · Horizontal Stabilizer, Plate/Skin
  > R/H LWR SKIN OF HORIZONTAL STAB @ RIBS 12-13 BETWEEN REAR SPAR TO MID SPAR WAS REPAIRED I.A.W. ETD2017-170-061843 REV.A AND AERONOVA TI-170-17-078. NO ADDITIONAL INSPECTION REQUIRED DURING 12 MONTH VALIDITY OF TEMPORARY REPAIR.
- [SDR R61A201612190745](https://openairdocs.org/sdr/R61A201612190745.md): Warning Message · false activation · Dec 19, 2016 · N115HQ · Emb ERJ170200LR · Leading Edge Slat Control System
  > DURING FLT, CREW RECEIVED A SLAT FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENACE RAN FIM TASK 27-81-00-810-0802-A IAW AMM AND CLEARED INHIBITS. AIRCRAFT IS GOOD FOR SERVICE.
- [SDR R61A201609130677](https://openairdocs.org/sdr/R61A201609130677.md): Closeout Panel · corroded · Nov 20, 2016 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINT FOUND CORROSION ON AFT CARGO DOOR THRESHOLD CLOSE OUT. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD CLOSEOUT PANEL. REF AMM 20-10-07, 51-21-02
- [SDR R61A201609130676](https://openairdocs.org/sdr/R61A201609130676.md): Door Sill · corroded · Nov 20, 2016 · N115HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINT FOUND CORROSION ON SILL PANEL AT FR19 ALONG EDGE OF PANEL AS MARKED. REMOVED AND REPLACED SILL PN: 170-07311-001 REF EMBRAER SRM 51-23-05. APPLIED PRIMER AND RESTORE TO ORIGINAL FINISH REF SRM 51-23-05 & 51-23-06.

Next page: https://openairdocs.org/aircraft/N115HQ/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 = 'N115HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N115HQ/reports

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