# Service difficulty reports: N116HQ

A list on [N116HQ](https://openairdocs.org/aircraft/N116HQ.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 · 116 reports

- [SDR R61A2026032800070](https://openairdocs.org/sdr/R61A2026032800070.md): Skin · damaged · Mar 28, 2026 · N116HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING AAI INSP. FOUND - AAI DISCREPANCY ITEM NR 2 REPAIR NR 38 - FR 27-28, STGR 22R-23R, PROVIDES A REPAIR DISPOSITION OF SRM 51-75-11 FOR DAMAGE BETWEEN STGR 22R AND 23R; HOWEVER, SRM 51-75-11 IS NOT APPLICABLE BECAUSE THE DOUBLER CROSSES A RIVET ROW (STGR
- [SDR R61A2026032800069](https://openairdocs.org/sdr/R61A2026032800069.md): Skin · chafed · Mar 28, 2026 · N116HQ · Emb ERJ170200LR · Passenger/Crew Doors
  > DURING HEAVY CHECK FOUND, SKIN UNDER AFT PAX DOOR 3 ISOLATORS, 2 ON TOP AND 1 ON BOTTOM AFT HAS CHAFING DAMAGE.
- [SDR R61A2026032800068](https://openairdocs.org/sdr/R61A2026032800068.md): Plate · chafed · Mar 28, 2026 · N116HQ · Emb ERJ170200LR · Engine Thrust Reverser
  > RIGHT ENGINE OTBD THRUST REVERSER MIDDLE THERMAL INSULATION BLANKET WEAR PLATE IS GOUGED.
- [SDR R61A2026032800067](https://openairdocs.org/sdr/R61A2026032800067.md): Plate · chafed · Mar 28, 2026 · N116HQ · Emb ERJ170200LR · Engine Thrust Reverser
  > LEFT ENG INBD THRUST REVERSER MID. THERMAL INSULATION BLANKET WEAR PLATE IS GOUGED
- [SDR R61A2026030200055](https://openairdocs.org/sdr/R61A2026030200055.md): Skin · cracked · Feb 26, 2026 · N116HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > DURING OVERNIGHT INSPECTION FOUND RH WING LOWER SKIN CRACKED BETWEEN RIB 16 AND RIB 17 JUST AFT OF FWD SPAR APROX 27.94 MM LONG.REPAIRED IAW EMB ETD2026-170-003614,INSTALLED FILLER,DOUBLER AND TRIPLER. ALSO REF VP-005555-2026 FOR WORK ACCOMPLISHED.
- [SDR R61A2025022000100](https://openairdocs.org/sdr/R61A2025022000100.md): Warning Light · illuminated · Feb 20, 2025 · N116HQ · Emb ERJ170200LR · Landing Gear Brake System
  > BRAKE RH FAULT AND BRAKE LH FAULT ILLUMINATED ON OR DISPLAYED ON EICAS INFLIGHT FOR APPROXIMATELY 10 SECONDS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. C/W FIM TASK 32-41-00-810-844A, MESSAGES CLEARED.
- [SDR R61A2024120700572](https://openairdocs.org/sdr/R61A2024120700572.md): Beam · damaged · Nov 20, 2024 · N116HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DAMAGED FWD PRESSURE BULKHEAD AT RH VERTICAL BEAM. REMOVED AND REPLACED FWD PRESSURE BULKHEAD AT RH VERTICAL BEAM, IAW EMB SRM 51-40-02
- [SDR R61A2024120700571](https://openairdocs.org/sdr/R61A2024120700571.md): Frame · damaged · Nov 20, 2024 · N116HQ · Emb ERJ170200LR · Fuselage Main, Frame
  > DAMAGE FR 1 LWR SIDE. BLENDED AFFECTED AREA, RESTORED SURFACE PROTECTION, FABRICATED AND INSTALLED REPAIR BUSHING PER ETD2024-170-0314419 AND EMB SRM 51-75-16.
- [SDR R61A2024120700570](https://openairdocs.org/sdr/R61A2024120700570.md): Skin · damaged · Nov 20, 2024 · N116HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DAMAGE RH RADOME AND RVSM SKIN AREA ON RH SIDE. REMOVED AND REPLACED RADOME AND LWR SKIN FR1-6 STGR 20R-20L. IAW EMB SRM 51-40-08
- [SDR R61A2023102800590](https://openairdocs.org/sdr/R61A2023102800590.md): Seat Track · corroded · Oct 14, 2023 · N116HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FF FWD RH IB SEAT TRACK FROM FR 12-20 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-03
- [SDR R61A2023102800586](https://openairdocs.org/sdr/R61A2023102800586.md): Seal · corroded · Oct 14, 2023 · N116HQ · Emb ERJ170200LR · Cargo/Baggage Doors
  > FWD CARGO DOOR AFT LWR SEAL DEPRESSOR CORRODED. REPLACED SEAL RETAINER IAW SRM 51-40-02
- [SDR R61A2023102800589](https://openairdocs.org/sdr/R61A2023102800589.md): Floor Support · corroded · Oct 13, 2023 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CF3 RH FLOOR SUPPORT CORRODED BTWN FR 88-90. REPLACED SUPPORT IAW SRM 51-42-01
- [SDR R61A2023102800588](https://openairdocs.org/sdr/R61A2023102800588.md): Shear Panel · corroded · Oct 13, 2023 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CF3 LH SHEAR WEB BTWN FR87-88 CORRODED. REPLACED SHEAR WEB IAW SRM 51-42-01
- [SDR R61A2023102800587](https://openairdocs.org/sdr/R61A2023102800587.md): Shear Panel · corroded · Oct 13, 2023 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CF3 MIDDLE SHEAR WEB BTWN FR 87-88 FOUND CORRODED. REPLACED SHEAR PANEL IAW SRM 51-42-01
- [SDR R61A2021090900721](https://openairdocs.org/sdr/R61A2021090900721.md): Intercostal · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORRODED L BRACKET AT FRAME 86- 87 STRINGER 27R. REMOVED AND REPLACED ''L'' INTERCOASTAL BRACKET AT FRAME 86- 87 STRINGER 27R REFER SRM 51-40-08.
- [SDR R61A2021090900720](https://openairdocs.org/sdr/R61A2021090900720.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FRAME 88 STRINGER 27R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 STRINGER 27R REF SRM 51-40-08
- [SDR R61A2021090900719](https://openairdocs.org/sdr/R61A2021090900719.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FRAME 86 STRINGER 27L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 86 STRINGER 27L PER SRM 51-40-08.
- [SDR R61A2021090900718](https://openairdocs.org/sdr/R61A2021090900718.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FRAME 86 STRINGER 27R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 86 STRINGER 27R REFER SRM 51-40-08.
- [SDR R61A2021090900717](https://openairdocs.org/sdr/R61A2021090900717.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FRAME 85 STRINGER 27R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 85 STRINGER 27R REFER SRM 51-40-08.
- [SDR R61A2021090900716](https://openairdocs.org/sdr/R61A2021090900716.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP AT FRAME 84 STRINGER 27R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 84 STRINGER 27R REFER SRM 51-40-08.
- [SDR R61A2021090900715](https://openairdocs.org/sdr/R61A2021090900715.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FRAME 84 STRINGER 28R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 84 STRINGER 28R REFER SRM 51-40-08.
- [SDR R61A2021090970714](https://openairdocs.org/sdr/R61A2021090970714.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO INTERNAL FUSELAGE SKIN HAS CORRODED SHEAR CLIP AT FRAME 84 STRINGER 27L. REMOVED AND REPLACED AFT CARGO INTERNAL FUSELAGE SKIN SHEAR CLIP AT FRAME 84 STRINGER 27L REFER SRM 51-40-08.
- [SDR R61A2021090970713](https://openairdocs.org/sdr/R61A2021090970713.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO INTERNAL FUSELAGE SKIN HAS CORRODED SHEAR CLIP AT FRAME 83 STRINGER 27R. REMOVED AND REPLACED CORRODED SHEAR CLIP, AT FRAME 83 STRINGER 27R REF: EMB SRM 51-40-02, EMB SRM 51-40-08. 51-40-08.
- [SDR R61A2021090970712](https://openairdocs.org/sdr/R61A2021090970712.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO INTERNAL FUSELAGE SKIN HAS CORRODED SHEAR CLIP AT FRAME 82 STRINGER 28R. REMOVED AND REPLACED AFT CARGO INTERNAL SHEAR CLIP AT FRAME 82 STRINGER 28R REFER SRM 51--40-08.
- [SDR R61A2021090970711](https://openairdocs.org/sdr/R61A2021090970711.md): Shear Tie · corroded · Aug 14, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO INTERNAL FUSELAGE SKIN HAS CORRODED SHEAR CLIP AT FRAME 75 STRINGER 29R. REMOVED AND REPLACED INTERNAL FUSELAGE SKIN SHEAR CLIP AT FRAME 75 STRINGER 29R REFER SRM 51-40-08. RESTORED SURFACE PROTECTION PER SRM 51--23-05, 51-23-06.
- [SDR R61A2021090700710](https://openairdocs.org/sdr/R61A2021090700710.md): Beam · corroded · Aug 12, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT PAX DOOR CUTOUT LOWER BEAM GOUGED AND CORRODED AS MARKED FR 85-87. REMOVED AND REPLACED AFT PAX DOOR LOWER BEAM REF: EMB SRM 51-40-08.
- [SDR R61A2021090870709](https://openairdocs.org/sdr/R61A2021090870709.md): Crossbeam · corroded · Aug 11, 2021 · N116HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > R/H CROSS BEAM AT FR 17 HAS CORROSION AS MARKED. REMOVED AND DAMAGE AREA BY CUTTING ON RH CROSS BEAM FRAME 17, FABRICATED AND INSTALLED ''L'' ANGLE AND FILLER REFER SRM 51-40-08 AND SRM 53-00-10 REP.03 FIG.203. RESTORED SURFACE PROTECTION PER SRM 51-23-05, 51
- [SDR R61A2021040600318](https://openairdocs.org/sdr/R61A2021040600318.md): Slide · partial deploy · Apr 1, 2021 · N116HQ · Emb ERJ170200LR · Escape Slide
  > R2 DOOR SLIDE PARTIALLY DEPLOYED DUE TO BROKEN FLEXBALL CABLE. R&R R2 DOOR SLIDE IAW AMM 25-65-01.
- [SDR R61A2020012410054](https://openairdocs.org/sdr/R61A2020012410054.md): Windshield · scratched · Jan 22, 2020 · N116HQ · Emb ERJ170200LR · Flight Compartment Windows
  > NOTICED SMALL CRACK FORMING ACROSS FO'S WINDSHIELD. DECLARED EMERGENCY, DIVERTED TO LGA, LANDED WITHOUT INCIDENT. NO CRACKS, FOUND SCRATCHES INSTEAD. PLACED ON DMI. LATER THAT NIGHT, R&R FO'S WINDSHIELD IAW AMM 56-11-00.
- [SDR R61A2019040960363](https://openairdocs.org/sdr/R61A2019040960363.md): Girt Bar · dirty · Apr 6, 2019 · N116HQ · Emb ERJ170200LR · Emergency Equipment
  > R1 DOOR ARMING HANDLE HARD TO MOVE. CLEANED GIRT BAR LATCH AND LUBED, OPS CHECK GOOD IAW AMM 52-41-00.
- [SDR R61A201902120237](https://openairdocs.org/sdr/R61A201902120237.md): Frame · cracked · Feb 12, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Main, Frame
  > WHILE AC WAS IN FOR HVY CK FOUND LT MAIN LANDING GEAR BAY FWD BULKHEAD FR 52 CRACKED QTY 2 FOUND AT BOTTOM AND MIDDLE AREA. MX REMOVED 2 EACH CRACKS.5" LONG AT LT MAIN LANDING GEAR BAY FWD BULKHEAD FR 52. IAW SRM 53-22-04REPAIR 5. SEE NRC # 4000319-1000-0070.
- [SDR R61A201902110225](https://openairdocs.org/sdr/R61A201902110225.md): Shear Panel · corroded · Feb 11, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND CENTER FUSELAGE 3 PAX CABIN FLOOR STRUCTURE SUPPORT UNDER RT SHEAR PANEL BTW FR 87-88 AND RBL 32" AREA. MX REMOVED AND REPLACED RT SHEAR PANEL PN 170-86131-001 IAW SRM 51-42-01. FOR DETAILS OF WORK PERFORMED SEE NRC 400031
- [SDR R61A201902110224](https://openairdocs.org/sdr/R61A201902110224.md): Upper Sheet · corroded · Feb 11, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND CENTER FUSELAGE 3 PAX CABIN FLOOR STRUCTURE CORROSION FOUND AT UPPER SHEET BTW FR 85-86 AND LBL 12" AREA. MX REMOVED AND REPLACED UPPER SHEET BTW FR 85-86 AND LBL 12" AREA PN 170-86101-001 IAW SRM 51-43-04 SEE NRC 4000319-
- [SDR R61A201902110223](https://openairdocs.org/sdr/R61A201902110223.md): Shear Panel · corroded · Feb 11, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND CENTER FUSELAGE 3 PAX CABIN FLOOR STRUCTURE CORROSION FOUND AT RT SHEAR PANEL BTW FR 87-88 AND BTW RBL 12" TO RBL 36" AREA. MX REMOVED AND REPLACED RT SHEAR PANEL PN 170-91919-001 BTW FR 87-88 AND BTW RBL 12" TO RBL 36" AR
- [SDR R61A201902110222](https://openairdocs.org/sdr/R61A201902110222.md): Attach Angle · corroded · Feb 11, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND FWD FUSELAGE PAX CABIN FLOOR STRUCTUE, CORROSION FOUND AT ANGLE ATTACH TO CROSSBEAM FR 17 LBL 24" AREA. MX REMOVED AND REPLACED FLOORBEAM ANGLE PN 170-04075-001 AT FR 17 LBL 24" ON CROSS BEAM IAW SRM 51-43-01. SEE NRC # 40
- [SDR R61A201902090247](https://openairdocs.org/sdr/R61A201902090247.md): Door Sill · corroded · Feb 9, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION ON FWD PAX DOOR CUTOUT LOWER MAIN SILL BEAM (L1)AT LOWER BEAM AREA OF BOTH ESCAPE SLIDE FITTINGS UNDER SERRATED PLATRES. MX CUT OUT LOWER MAIN SILL BEAM PN 170-03719-005 AND REPLACED IAW SRM 51-43-02. FOR DETAILS
- [SDR R61A201902080221](https://openairdocs.org/sdr/R61A201902080221.md): Door Sill · corroded · Feb 8, 2019 · N116HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE AC WAS IN FOR HEAVY CHECK FOUND AFT PAX DOOR CUTOUT LOWER MAIN SILL BEAM, CORROSION FOUND AT ESCAPE SLIDE ATTACHMENT FASTNER AREA. MX REMOVED AND REPLACED AFT PAX DOOR CUTOUT LOWER MAIN SILL BEAM ATTACHMENT FASTNER AREA PN 170-65703-005 REMOVED IAW SRM 5
- [SDR R61A201902060236](https://openairdocs.org/sdr/R61A201902060236.md): Skin · cracked · Feb 6, 2019 · N116HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > *** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED A CRACK ON THE RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 4 CUTOUT. MAINTENANCE CUTOUT AND REPAIRED CRACK ON THE RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 4 CUTOUT IAW SRM 51-10-03
- [SDR R61A201902060235](https://openairdocs.org/sdr/R61A201902060235.md): Skin · cracked · Feb 6, 2019 · N116HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > *** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED A CRACK ON THE LT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 5 CUTOUT. MAINTENANCE CUTOUT AND REPAIRED CRACK ON THE LT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 5 CUTOUT IAW SRM 51-10-03
- [SDR R61A201902060234](https://openairdocs.org/sdr/R61A201902060234.md): Skin · cracked · Feb 6, 2019 · N116HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > *** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED A CRACK ON THE RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 5 CUTOUT. MAINTENANCE CUTOUT AND REPAIRED CRACK ON THE RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 5 CUTOUT IAW SRM 51-10-03
- [SDR R61A2018081080850](https://openairdocs.org/sdr/R61A2018081080850.md): Battery Pack · inoperative · Aug 8, 2018 · N116HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-50-01.
- [SDR R61A201806130690](https://openairdocs.org/sdr/R61A201806130690.md): Unknown · malfunctioned · Jun 13, 2018 · N116HQ · Emb ERJ170200LR · Drag Control System
  > GROUND SPOILERS FAIL IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RESET A/C AND PERFORMED RTS TEST. MESSAGE CLEARED.
- [SDR R61A201804250512](https://openairdocs.org/sdr/R61A201804250512.md): Sign · inoperative · Apr 25, 2018 · N116HQ · Emb ERJ170200LR · Emergency Lighting
  > L2 EXIT ID SIGN INOP. R&R L2 DOOR EXIT ID SIGN IAW AMM 33-50-15. OPS CHECK GOOD.
- [SDR R61A201711280907](https://openairdocs.org/sdr/R61A201711280907.md): Door · lack of lube · Nov 28, 2017 · N116HQ · Emb ERJ170200LR · Service Doors
  > FA R1 DOOR HANDLE DIFFICULT TO MOVE. LUBE AND CLEAN R1 DOOR IAW AMM 52-11-00. OPS CHECK GOOD.
- [SDR R61A201705110347](https://openairdocs.org/sdr/R61A201705110347.md): Sign · cracked · May 11, 2017 · N116HQ · Emb ERJ170200LR · Emergency Lighting
  > L2 DOOR EXIT IDENTIFIER SIGN IS CRACKED. R&R EXIT SIGN IAW AMM 33-50-11. OPS CHECK GOOD.
- [SDR R61A201701050012](https://openairdocs.org/sdr/R61A201701050012.md): Battery Pack · faulted · Jan 5, 2017 · N116HQ · Emb ERJ170200LR · Emergency Lighting
  > CREW RECEIVED AN EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201612280763](https://openairdocs.org/sdr/R61A201612280763.md): Light · unsecure · Dec 28, 2016 · N116HQ · Emb ERJ170200LR · Emergency Lighting
  > CREW REPORTED THAT THE L2 DOOR WOULD NOT CLOSE. MAINTENANCE FOUND TRIM SCREW LOOSE, SECURED IAW AMM AND L2 DOOR OPS CHECKED GOOD.
- [SDR R61A201612150731](https://openairdocs.org/sdr/R61A201612150731.md): Closeout Panel · corroded · Dec 15, 2016 · N116HQ · Emb ERJ170200LR · Cargo/Baggage Doors
  > WHILE IN HEAVY CHECK, FOUND CORROSION ON AFT CARGO CLOSE OUT PANEL. REMOVED AND REPLACED THE CLOSEOUT PANEL IAW AMM 201-10-01.
- [SDR R61A201612120720](https://openairdocs.org/sdr/R61A201612120720.md): Doubler · corroded · Dec 2, 2016 · N116HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DOUBLER AROUND PANEL 192CR CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02.
- [SDR R61A201612120717](https://openairdocs.org/sdr/R61A201612120717.md): Stringer Clip · corroded · Dec 2, 2016 · N116HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > CORROSION AT ATTACHING CLIP AT FRAME 88 STRINGER 19R REMOVED, FABRICATED, AND INSTALLED NEW CLIP PN: 170-65210-002 AT FR88 REF EMBRAER SRM 51-41-02 & 51-43-03. SEE EAMS W/O H5305 SEQ 1567 SN 432 FOR WORK DETAILS. AIRCRAFT REMAINS IN HVY CHECK BNA

Next page: https://openairdocs.org/aircraft/N116HQ/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 = 'N116HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N116HQ/reports

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