# Service difficulty reports: N118HQ

A list on [N118HQ](https://openairdocs.org/aircraft/N118HQ.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 · 134 reports

- [SDR R61A2026100300295](https://openairdocs.org/sdr/R61A2026100300295.md): Fitting · corroded · Sep 16, 2026 · N118HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > RH HORIZONTAL STABILIZER PIVOT FITTING HAS CORROSION ON OB SIDE.REPAIRED HORIZONTAL STABILIZER RH PIVOT FITTING REF. ETD2026-170-016046 REV.: A
- [SDR R61A2026100300294](https://openairdocs.org/sdr/R61A2026100300294.md): Bushing · loose · Sep 6, 2026 · N118HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER FAILED ROLL BACKLASH. INSTALLED BUSHING REPAIR PER ETD2026-170-016037
- [SDR R61A2026100300293](https://openairdocs.org/sdr/R61A2026100300293.md): Rib · cracked · Sep 5, 2026 · N118HQ · Emb ERJ170200LR · Wing, Rib/Bulkhead
  > CRACK AS MARKED RH WING RIB 4.REPAIRED CRACK IN RH WING RIB 4 IAW ETD2026-170-015445.
- [SDR R61A2026100300292](https://openairdocs.org/sdr/R61A2026100300292.md): Rib · cracked · Sep 5, 2026 · N118HQ · Emb ERJ170200LR · Wing, Rib/Bulkhead
  > CRACK LT WING AT FWD WHEEL WELL RIB 3A. REPAIRED CRACK LT WING AT FWD WHEEL WELL RIB 3A IAW ETD2026-170-015448
- [SDR R61A2024072900334](https://openairdocs.org/sdr/R61A2024072900334.md): Shear Angle · corroded · Jul 23, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > SHEAR CLIP BETWEEN STRINGERS 29R AND 29L AT FR77 FOUND TO BE CORRODED AFTER REMOVAL. REMOVED AND REPLACED SHEAR CLIP BETWEEN STRINGERS 29R AND 29L AT FR77 REF: EMB SRM 51-40-08.
- [SDR R61A2024072600333](https://openairdocs.org/sdr/R61A2024072600333.md): Shear Tie · corroded · Jul 23, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP BETWEEN STRINGERS 29R AND 29L AT FR78 FOUND TO BE CORRODED AFTER REMOVAL. REMOVED AND REPLACED SHEAR CLIP AT FRAME 78 BETWEEN STRINGERS 29R AND 29L REF: EMB SRM 51-40-08.
- [SDR R61A2024072900342](https://openairdocs.org/sdr/R61A2024072900342.md): Shear Angle · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DUE TO AFT LAV SPILL,CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 83 BETWEEN STRINGERS 27R-28R CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 83 BETWEEN STRINGERS 27R-28R REF EMB SRM 51-40-08
- [SDR R61A2024072900335](https://openairdocs.org/sdr/R61A2024072900335.md): Stringer Splice · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > DUE TO AFT LAV SPILL, CENTER FUSELAGE III AFT CARGO, STRINGER 28L CORRODED BETWEEN FRAMES 78 AND 79. PERFORMED PERMANENT STRINGER SPLICE REPAIR ON STGR 28L IN AFT CARGO BETWEEN FR 78-79. REF EMB ETD2024-170-019268. "
- [SDR R61A2024072600332](https://openairdocs.org/sdr/R61A2024072600332.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 82 BETWEEN STRINGERS 28L-29L CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 82 STGR 28L-29L. REF EMB SRM 51-40-08.
- [SDR R61A2024072600331](https://openairdocs.org/sdr/R61A2024072600331.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORRODED SHEAR CLIP FR87, STR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 87 STGR 27R-28R. REF EMB SRM 51-40-08.
- [SDR R61A2024072600330](https://openairdocs.org/sdr/R61A2024072600330.md): Stringer · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CENTER FUSELAGE III AFT CARGO, STRINGER 23L CORRODED BETWEEN FRAMES 75 AND 82. PERFORMED STGR SPLICE REPAIR TO CENTER FUSELAGE III AFT CARGO STRINGER 23L BETWEEN FRAMES 75 AND 82 REF ETD 2024-170-019331 AND REF SRM SRM 53-23-03 REPAIR 06.
- [SDR R61A2024072500327](https://openairdocs.org/sdr/R61A2024072500327.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 76 BETWEEN STRINGERS 24L-25L CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 76 STGR 24L-25L. REF SRM 51-40-08
- [SDR R61A2024072500326](https://openairdocs.org/sdr/R61A2024072500326.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 82 BETWEEN STRINGERS 28R-29R CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 82 BETWEEN STRINGERS 28R-29R REF EMB SRM 51-40-08.
- [SDR R61A2024072500325](https://openairdocs.org/sdr/R61A2024072500325.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 78 BETWEEN STRINGERS 22L-23L CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 78 BETWEEN STRINGERS 22L-23L REF EMB SRM 51-40-08.
- [SDR R61A2024072500324](https://openairdocs.org/sdr/R61A2024072500324.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 78 BETWEEN STRINGERS 21L-22L CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 78 BETWEEN STRINGERS 21L-22L REF EMB SRM 51-40-08.
- [SDR R61A2024072500323](https://openairdocs.org/sdr/R61A2024072500323.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 84 BETWEEN STRINGERS 27R-28R CORRODED. REMOVE AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 84 BETWEEN STRINGERS 27R-28R REF EMB SRM 51-40-08.
- [SDR R61A2024072500322](https://openairdocs.org/sdr/R61A2024072500322.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 84 BETWEEN STRINGERS 27L-28L CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 84 BETWEEN STRINGERS 27L-28L REFER SRM 51-40-08.
- [SDR R61A2024072500321](https://openairdocs.org/sdr/R61A2024072500321.md): Shear Tie · corroded · Jul 12, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 83 BETWEEN STRINGERS 28R-29R CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 83 BETWEEN STRINGERS 28R-29R REF EMB SRM 51-40-08
- [SDR R61A2024072300319](https://openairdocs.org/sdr/R61A2024072300319.md): Crossbeam · corroded · Jul 11, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > FR.11 CENTER OF COCKPIT HAS SCORE MARKS. PERFORMED PERMANENT REPAIR BY FABRICATING NEW DOUBLER AND FILLER FOR FR 11 CROSSBEAM CENTER OF COCKPIT. REF: ETD2024-170-019089.
- [SDR R61A2024072300318](https://openairdocs.org/sdr/R61A2024072300318.md): Crossbeam · corroded · Jul 8, 2024 · N118HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION CENTER FUSELAGE III WET AREA 53-23 LONGITUDINAL CROSSBEAM FRAME 90. COMPLIED WITH REPAIR OF CFIII WET AREA 53-23 CROSSBEAM FR 90 BY REMOVING CORROSION ON CENTER LOCATION AND INSTALL OF REPAIR DOULBER ON LH SIDE REF ETD 2024-170-019214
- [SDR R61A2024010500779](https://openairdocs.org/sdr/R61A2024010500779.md): Unknown · pilot error · Dec 19, 2023 · N118HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TAIL STRIKE DURING LANDING BETWEEN FRA 99 AND FRA 100 AND STR 29L TO STR 29R. REPAIRED IAW ETD2023-170-032292 REV A AND TI-170-23-249. ALSO REF VP-054105-2023 N/R #5 & #6 FOR REPAIRS. INSTALLED DOUBLER AT FRAME 100.
- [SDR R61A2022111400702](https://openairdocs.org/sdr/R61A2022111400702.md): Battery Pack · inoperative · Nov 10, 2022 · N118HQ · Emb ERJ170200LR · Emergency Lighting
  > #1 EMERGENCY LIGHT INOP. R&R AFT OUTBOARD EMERGENCY LIGHT POWER BATTERY UNIT.
- [SDR R61A2022030200213](https://openairdocs.org/sdr/R61A2022030200213.md): Frame · corroded · Mar 2, 2022 · N118HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > FR 84 CROSSBEAM IS CORRODED IN SEVERAL LOCATIONS. PERFORMED DOUBLER REPAIR REF: ETD2022-170-008948
- [SDR R61A2022030200212](https://openairdocs.org/sdr/R61A2022030200212.md): Shear Tie · corroded · Mar 2, 2022 · N118HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > CORRODED SHEAR CLIP AT FR 85, STGR 27R - 28R. REMOVED AND REPLACED SHEAR CLIP AT FR 85, STGR 27R - 28R. REF EMB SRM 51-40-08.
- [SDR R61A2021061100482](https://openairdocs.org/sdr/R61A2021061100482.md): Fitting · underserviced · Jun 8, 2021 · N118HQ · Emb ERJ170200LR · Passenger/Crew Doors
  > MAIN CABIN DOOR IS DIFFICULT TO CLOSE AND ESPECIALLY TO OPEN. SERVICED L1 DOOR COMMAND RAMPS FITTINGS IAW AMM 53-10-21.
- [SDR R61A2020020740160](https://openairdocs.org/sdr/R61A2020020740160.md): Module · faulty · Feb 4, 2020 · N118HQ · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. TROUBLESHOT PER FIM 32-33-00-810-802A AND FOUND SPDA 1 LRM 13 AT FAULT. R&R SPDA 1 POWER MODULE SLOT 13 IAW AMM 24-61-13.
- [SDR R61A201909130959](https://openairdocs.org/sdr/R61A201909130959.md): Rib · cracked · Sep 6, 2019 · N118HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: FOUND LT HORIZONTAL RIB 12A CRACK. REMOVED AND REPLACED LT HORIZONTAL STAB RIB 12A PER SRM 51-40-08. APPLIED SURFACE PROTECTION PER SRM 51-23-05, 51-03-06. SEE WIPS FOR WORK PERFORMED. SEE W/O H6951 SN 691 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CH
- [SDR R61A201909150960](https://openairdocs.org/sdr/R61A201909150960.md): Rib · cracked · Aug 28, 2019 · N118HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > PERFORMED PERMANENT REPAIR OF RIB 11A ON LT HORIZONTAL BY MEANS OF FABRICATION AND INSTALLATION OF REPAIR DOUBLERS IAW ETD2019-170-122890. SEE WIPS, TASK AND ATTACH ETD2019-170-122890 FOR WORK PERFORMED. SEE W/O H6951 SN 644 FOR WORK DETAILS.
- [SDR R61A201909130958](https://openairdocs.org/sdr/R61A201909130958.md): Rib · cracked · Aug 28, 2019 · N118HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: CRACK ON RIB 12A INTERNALLY ON RT HORIZONTAL BETWEEN MID SPAR AND FRONT SPAR FWD/AFT OF 6TH RIVET FROM FRONT SPAR LOWER RIVET ROW. REMOVED AND REPLACED RT HORIZONTAL STABRIB 12A PER SRM 51-40-08. APPLIED SURFACE PROTECTION TO FASTENERS PER SRM 51-23-05,
- [SDR R61A201909130957](https://openairdocs.org/sdr/R61A201909130957.md): Rib · cracked · Aug 28, 2019 · N118HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: CRACK ON RIB 11A INTERNALLY ON RT HORIZONTAL BETWEEN MID SPARAND FRONT SPAR 5TH RIVET FROM FRONT SPAR UPPER RIVET ROW REMOVED AND RE-INSTALLED RT HORIZONTAL STABILIZER RIB 11A PER SRM 51-40-08. REF TO W/O H6951 SN# 00688 FOR FABRICATION AND INSTALLATION
- [SDR R61A201909130956](https://openairdocs.org/sdr/R61A201909130956.md): Crossbeam · corroded · Aug 27, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FLANGE OF CROSSBEAM BETWEEN FRAME 11 AND 12 AS SEEN UNDER COCKPIT FLOOR 221ELF AND 221DLF. BLENDED OUT CORROSION AND INSTALLED REPAIR ANGLES ON UPPER FLANGE OF CROSSBEAM BETWEEN FR 11 AND 12 REF ETD2019-170-118438. SEE W/O H6951 SN 614 FOR
- [SDR R61A201909130955](https://openairdocs.org/sdr/R61A201909130955.md): Threshold · corroded · Aug 27, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE PERFORMING L1 DOOR LOWER BEAM REWORK, CORROSION FOUND ON FWD AND AFT LOWER GIRT BAR CUT OUT AREAS. REMOVED AND INSTALLED NEW L1 DOOR THRESHOLD REF: SRM 51-40-08. SEE W/O H6951 SN 610 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909130954](https://openairdocs.org/sdr/R61A201909130954.md): Door Sill · corroded · Aug 27, 2019 · N118HQ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > WHILE PERFORMING L2 DOOR LOWER BEAM REWORK, CORROSION FOUND ON TOP OF SILL AT AFT GIRT BAR FITTING. REMOVED AND INSTALLED NEW L2 DOOR LOWER BEAM REF: SRM 51-40-08. SEE W/O H6951 SN 606 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110951](https://openairdocs.org/sdr/R61A201909110951.md): Floor Support · corroded · Aug 26, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FR16 LAV FLOOR SUPPORT MONUMENT. REMOVED REPLACED LAV FLOOR SUPPORT MONUMENT AT FR16 SRM 51-40-02 APPLIED SURFACE PROTECTION REF SRM 51-23-04,51-23-05, 51-23-06 SEE W/O H6951 SN 570 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909130953](https://openairdocs.org/sdr/R61A201909130953.md): Panel · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON INNER FLANGE OF PANEL 192BL. REMOVED AND REPLACED INNER FLANGE OF PANEL 192BL. REF SRM 51-40-08. SEE EAMS W/O H6951 SN 420 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909130952](https://openairdocs.org/sdr/R61A201909130952.md): Shear Tie · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO SHEAR CLIP CORRODED AT FR 82 STRG 26-27R. AFT CARGO SHEAR CLIP CORRODED AT FR 82 STRG 26-27R. RESTORED SURFACE PROTECTION REF SRM 51-23-04,51-23-05, 51-23-06. SEE W/O H6951 SN 410 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110950](https://openairdocs.org/sdr/R61A201909110950.md): Seat Track · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LT INBD BEAM AT FR 84 HAS AREAS OF CORROSION AS MARKED. CUT, FABRICATED AND INSTALLED REPAIR PARTS LT INBD SEAT TRACK AT FR 84 REFER ETD2019-170-118216 AND SRM 53-00-10/REPAIR01. APPLIED SURFACE PROTECTION TO PARTS AND FASTENERS PER SRM 51-23-- 05, 51-23-06. P
- [SDR R61A201909110949](https://openairdocs.org/sdr/R61A201909110949.md): Splice Plate · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FR 87-88 LT OB SPLICE PLATE HAS AREA OF CORROSION. REMOVED AND REPLACED SPLICE PLATE AT FR 87-88 LT OB REF SRM 51-40-08. SEE W/O H6951 SN 488 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110948](https://openairdocs.org/sdr/R61A201909110948.md): Beam · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > RT INBD BEAM HAS AREAS OF CORROSION FR 84. COMPLIED WITH CUTOUT AND SPLICE REPAIR OF RT INBD BEAM HAS AREAS OF CORROSION FR 84 REF ETD2019-170-118217. SEE W/O H6951 SN 486 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110947](https://openairdocs.org/sdr/R61A201909110947.md): Floorbeam · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > LT INBD FLOOR BEAM HAS CORRODED FASTENERS AS MARKED. REMOVED AND REPLACED LT FLOORBEAM AT FR 84 TO 88 PER SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04,51-23-05, 51-23-06. SEE W/O H6951 SN 485 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110946](https://openairdocs.org/sdr/R61A201909110946.md): Shear Panel · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT SHEAR PANEL FR 87-88 AREAS OF CORROSION AND CORRODED FASTENERS. REMOVED AND REPLACED RT SHEAR PANEL FR 87-88 REF 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04,51-23-05,51-23-06. SEE W/O H6951 SN 482 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY C
- [SDR R61A201909110945](https://openairdocs.org/sdr/R61A201909110945.md): Door Sill · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT OB SILL REST FR 89 MOUNT HOLE CORRODED. REMOVED AND REPLACED RT OB SILL REST AT FR 89 REF SRM 51-23-04, RESTORED SURFACE PROTECTION REF SRM 51-23-04,51-23-05, 51-23-06. SEE W/O H6951 SN 481 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110944](https://openairdocs.org/sdr/R61A201909110944.md): Gusset · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT FR 90 GUSSET CORRODED AS MARKED. REMOVED AND REPLACED RT FR 90 GUSSET REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-04 51-23-05, 51-23-06. SEE W/O H6951 SN 480 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110943](https://openairdocs.org/sdr/R61A201909110943.md): Panel Support · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > LT OB PANEL SUPPORT AT FR 90 MOUNT HOLE CORRODED AS MARKED. REMOVED AND INSTALLED NEW LT OB PANEL SUPPORT AT FR 90 REF SRM 51-40-08. SEE W/O H6951 SN 477 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110942](https://openairdocs.org/sdr/R61A201909110942.md): Door Sill · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOOR SILL RT FR 17-20 CORRODED AS MARKED. REMOVED AND REPLACED RT OB SILL AT FR 17-20 REF SRM 51-40-08. SEE W/O H6951 SN 448 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
- [SDR R61A201909110941](https://openairdocs.org/sdr/R61A201909110941.md): Angle · corroded · Aug 24, 2019 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON 3 EA LOWER ANGLE AND 2 MISSING RECEPTACLE ON PANEL 1441FR. 2 EACH LOWER ANGLES OUT OF LIMITS REMOVED AND REPLACED 2 EACH LOWER ANGLES ON PANEL 1441FR REF SRM 51-40-08 AND AMM 20-10-01 170-10064-002, 170-10065-002 SEE EAMS W/O H6951 SN 430 FOR WO
- [SDR R61A2018060400667](https://openairdocs.org/sdr/R61A2018060400667.md): Module · faulty · May 29, 2018 · N118HQ · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT. DECLARED AN EMERGENCY, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. R & R THE DC POWER MODULE IN SPDA 1, SLOT 13 IAW AMM 24-61-13. PERFORMED AN OPERATIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW AMM 32-33-0
- [SDR R61A201708120617](https://openairdocs.org/sdr/R61A201708120617.md): Doubler · corroded · Aug 12, 2017 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOOR DOUBLER AT FRAME 19 CORRODED. REMOVED AND REPLACED THE FLOOR DOUBLER IAW SRM 51-41-02, 51-42-02, 51-23-04, 51-23-05, AND 51-23-06.
- [SDR R61A201708120616](https://openairdocs.org/sdr/R61A201708120616.md): Floor Support · corroded · Aug 12, 2017 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT FWD FLOOR SUPPORT BETWEEN FRAMES 12 AND 14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-04, & 51-41-02. ALODINED, PRIMED, AND TOPCOATED IAW SRM 51-23-04, 51-23-05, AND 51-23-06.
- [SDR R61A201708120615](https://openairdocs.org/sdr/R61A201708120615.md): Floor Support · corroded · Aug 12, 2017 · N118HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > LEFT FWD FLOOR SUPPORT AT FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. ALODINED, PRIMED, AND TOPCOATED IAW SRM 51-23-04, 51-23-05,AND 51-23-06.

Next page: https://openairdocs.org/aircraft/N118HQ/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 = 'N118HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N118HQ/reports

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