# Service difficulty reports: N103HQ

A list on [N103HQ](https://openairdocs.org/aircraft/N103HQ.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 · 108 reports

- [SDR R61A2026022600056](https://openairdocs.org/sdr/R61A2026022600056.md): Warning Message · false activation · Feb 26, 2026 · N103HQ · Emb ERJ170200LR · Door Warning System
  > L1 DOOR OPEN EICAS MSG IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED PRESSURE CHECKS. NO FAULTS FOUND. L1 DOOR EICAS MESSAGES PLACED ON DEFERRAL.
- [SDR R61A2025042300210](https://openairdocs.org/sdr/R61A2025042300210.md): Stringer Splice · corroded · Apr 10, 2025 · N103HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION BETWEEN FRAMES 88/89 ON STRINGER 20R AS MARKED. REMOVED AND INSTALLED NEW FABRICATED STRINGER 20R BETWEEN FR 86-89. REF ETD2025-170-905860
- [SDR R61A2025042300209](https://openairdocs.org/sdr/R61A2025042300209.md): Stringer Splice · corroded · Apr 5, 2025 · N103HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION BETWEEN FRAMES 88/89 ON STRINGER 19R AS MARKED.REMOVED AND INSTALLED STGR 19R AND SPLICE BETWEEN FR 88-90. REF ETD2025-170-905863
- [SDR R61A2025042300208](https://openairdocs.org/sdr/R61A2025042300208.md): Stringer Splice · corroded · Apr 5, 2025 · N103HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION BETWEEN FR88-89 ON STRINGER 21L.REMOVED AND REPLACED STRINGER 21L AFT OF FR 88 IN ACCORDANCE WITH ETD REPAIR, REF ETD-2025-170-905548 REV.: A.
- [SDR R61A2025042300207](https://openairdocs.org/sdr/R61A2025042300207.md): Crossbeam · corroded · Apr 2, 2025 · N103HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > COCKPIT FLOOR CENTER CROSS FRAME CORRODED AS MARKED FR 11.REMOVED DAMAGE AND REPAIRED COCKPIT FLOOR CENTER CROSS FRAME AT FR 11 IN ACCORDANCE WITH REF ETD2025-170-905344 REV A
- [SDR R61A2025042300206](https://openairdocs.org/sdr/R61A2025042300206.md): Crossbeam · corroded · Mar 31, 2025 · N103HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION FOUND ON RH CROSSBEAM AT FR 84-85 UNDERNEATH CABIN FLOOR PANEL 252CRF AND 252DRF.REMOVED AND INSTALLED PARTS FOR CROSSBEAM REPAIR IN ACCORDANCE WITH ETD2025-170-905198
- [SDR R61A2025022800119](https://openairdocs.org/sdr/R61A2025022800119.md): Spoiler Sys · faulted · Feb 28, 2025 · N103HQ · Emb ERJ170200LR · Drag Control System
  > SPOILER FAULT MSG AT CRUISE. A/C DECLARED EMERGENCY LANDED WITHOUT INCIDENT. FAULT CLEARED ON ARRIVAL. REMOVED AND REPLACED RH PCU.
- [SDR R61A2024062600293](https://openairdocs.org/sdr/R61A2024062600293.md): Actuator · failed · Jun 19, 2024 · N103HQ · Emb ERJ170200LR · Trailing Edge Flap Actuator
  > FLAP FAIL MESSAGE INDICATING FLAPS ZERO AND SLATS 3 ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND RH #2 FLAP ACTUATOR JAMMED. R&R RH #2 FLAP ACTUATOR.
- [SDR R61A2024061700270](https://openairdocs.org/sdr/R61A2024061700270.md): Flap System · failed · Jun 14, 2024 · N103HQ · Emb ERJ170200LR · Trailing Edge Flap Control System
  > FLAP FAIL EICAS MESSAGE DURING RETRACTION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PLACED ON DEFERRAL.
- [SDR R61A2024051500212](https://openairdocs.org/sdr/R61A2024051500212.md): Skin · cracked · May 11, 2024 · N103HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > RH WING LOWER SKIN CRACKEDAFT OF FWD SPAR BETWEEN RIBS 16 AND 17, LENGTH 66MM.REPAIRED SKIN IAW ETD2024-170-013274,INSTALLED FILLER,DOUBLER AND TRIPLER. ALSO REF VP-019530-2024 N/R #1 FOR WORK ACCOMPLISHED.
- [SDR R61A2023020800105](https://openairdocs.org/sdr/R61A2023020800105.md): Not Reported · not reported · Feb 3, 2023 · N103HQ · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > DEPARTING ON CLIMBOUT, LANDING GEAR WOULD NOT RETRACT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEANED DEBRIS FROM LANDING GEAR PROXIMITY SENSORS.
- [SDR R61A2022090400537](https://openairdocs.org/sdr/R61A2022090400537.md): Support · corroded · Sep 4, 2022 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE ACFT IN HEAVY CHECK MAINT FOUND BAGGAGE COMPT SUPPORT CORRODED IN AFT CARGO AT FR 75 AND FR76 STR 29L-29R. REMOVED AND REPLACED BAGGAGE COMPT SUPPORT IN AFT CARGO AREA AT FR 75 AND FR 76 STR 29L-29R. REF EMB SRM 51-40-08.
- [SDR R61A2022090400535](https://openairdocs.org/sdr/R61A2022090400535.md): Frame · corroded · Sep 4, 2022 · N103HQ · Emb ERJ170200LR · Fuselage Main, Frame
  > WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON FRAME 80. REMOVED AND REPLACED FRAME 80 REF EMB SRM 51-40-08.
- [SDR R61A2022091000551](https://openairdocs.org/sdr/R61A2022091000551.md): Doubler · corroded · Aug 15, 2022 · N103HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION - WASTE SERVICE BOX CUTOUT FWD I/B CORNER.: REMOVED AND REPLACED WASTE BOX INTERNAL SKIN DOUBLER BETWEEN FRAMES 88-89 REF SRM 51-40-08.
- [SDR R61A2021092800767](https://openairdocs.org/sdr/R61A2021092800767.md): None · none · Sep 25, 2021 · N103HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY EXIT LIGHT BESIDE FWD LAV INOP. R&R FWD EMERGENCY EXIT LOCATOR SIGN IAW AMM 33-50-19.
- [SDR R61A2022091000550](https://openairdocs.org/sdr/R61A2022091000550.md): None · corroded · Aug 18, 2021 · N103HQ · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION SHEAR CLIP FRAME 88, STRINGER 25R-26R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STGR 25R-26R REFER SRM 51-40-08. RESTORED SURFACE PROTECTION TO FASTENERS PER SRM 51-23-06.
- [SDR R61A2021051400422](https://openairdocs.org/sdr/R61A2021051400422.md): Arming Lever · lack of lube · May 11, 2021 · N103HQ · Emb ERJ170200LR · Service Doors
  > R2 DOOR VERY HARD TO ARM/DISARM. FELT LIKE GRINDING METAL. LUBRICATED ARM/DISARM MECHANISM ON R2 DOOR.
- [SDR R61A2020070600551](https://openairdocs.org/sdr/R61A2020070600551.md): Power Unit · inoperative · Jul 3, 2020 · N103HQ · Emb ERJ170200LR · Emergency Lighting
  > EICAS MESSAGE EMERGENCY LIGHT BATTERY FAULT. R&R EMERGENCY LIGHT POWER UNITS 1 AND 2.
- [SDR R61A201911231324](https://openairdocs.org/sdr/R61A201911231324.md): Seat Track · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORROSION ON FR 84 (BY SEAT TRACK RH) REMOVED CORROSION BY BLENDING PER SRM 51-10-03 ON AFT WET AREA ON FR 84 MAX MATERIAL LOSS.012 REMAINING.088 COMPLIED WITH ETD2019-170-157186
- [SDR R61A201911231323](https://openairdocs.org/sdr/R61A201911231323.md): Seat Track · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORROSION ON RH INBD SEAT TRACK FR 85 REMOVED CORROSION BY BLENDING ON AFT WET AREA CORROSION ON RH INBD SEAT TRACK FR 85 MATERIAL LOSS.030, REMAINING.070. OUT OF LIMITS PER SRM 53-23-10. TOOL HG3-61455, CAL 5-1-20. CO
- [SDR R61A201911231322](https://openairdocs.org/sdr/R61A201911231322.md): Upper Sheet · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORROSION ON LH UPPER SHEET AT FR 86 REMOVED AND REPLACED LH UPPER SHEET FR 86 IN REF TO SRM 51-40-08
- [SDR R61A201911231321](https://openairdocs.org/sdr/R61A201911231321.md): Shear Panel · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORRODED SHEAR PANEL RH FR 88/89 REPLACED RH SHEAR PANEL FR 88-89 IN REF TO SRM 51-40-08
- [SDR R61A201911231320](https://openairdocs.org/sdr/R61A201911231320.md): Gusset · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORRODED GUSSET RH INBD FR 90. REMOVED AND REPLACED RH INBD GUSSET FR90 IN REF TO SRM 51-40-08
- [SDR R61A201911231319](https://openairdocs.org/sdr/R61A201911231319.md): Gusset · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORRODED GUSSET RH OTBD FR 90. REMOVED CORRODED AFT WET AREA GUSSET RH OTBD FR 90. LOCATED, DRILLED, AND APPLIED ALODINE TO THE NEW AFT WET AREA. GUSSET RH OTBD FR 90 PER REF SRM 51-40-02, 51-23-04 PO# 243626. INSTALLED
- [SDR R61A201911231318](https://openairdocs.org/sdr/R61A201911231318.md): Splice Plate · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA CORRODED SPLICE PLATE BETWEEN FR 87/88 RH. REMOVED AND REPLACED RH SPLICE PLATE FR87/88 IN REF. TO SRM 51-40-08
- [SDR R61A201911231317](https://openairdocs.org/sdr/R61A201911231317.md): Splice Plate · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA. CORRODED SPLICE PLATE BETWEEN FR87/88 LH REMOVED AND REPLACED LH SPLICE PLATE BETWEEN FR87/88 IN REF TO SRM 51-40-08
- [SDR R61A201911231316](https://openairdocs.org/sdr/R61A201911231316.md): Door Sill · corroded · Nov 23, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK FOUND AFT WET AREA. AFT SILL RH FR89 CORROSION. REMOVED AND REPLACED RH SILL AT FR89 IN REF. TO SRM 51-40-08
- [SDR R61A201911261337](https://openairdocs.org/sdr/R61A201911261337.md): Crossbeam · gouged · Nov 21, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > MAJOR: INCOMING PREVIOUS GOUGE DAMAGE L= 0.4 W= 0.1 H= 0.080 FOUND AT CROSSBEAM 57 WEB AREA. FABRICATED, DRILLED AND INSTALLED REPAIR '' L'' ANGLE FOR CROSSBEAM 57 PER ETD2019-170-158123 AND SRM 51-40-08. RESTORED SURFACE TREATMENT PER SRM 51-23-06, CPM 51-25
- [SDR R61A201911261335](https://openairdocs.org/sdr/R61A201911261335.md): Seal Rest · corroded · Nov 18, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION-AFT SERVICE DOOR LOWER CENTER SEAL REST AS MARKED. REMOVED AND REPLACED AFT SERVICE DOOR LOWER CENTER SEAL REST REF E175 SRM 51-40-08 APPLIED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H7026 SN 164 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY
- [SDR R61A201911261336](https://openairdocs.org/sdr/R61A201911261336.md): Frame · corroded · Nov 17, 2019 · N103HQ · Emb ERJ170200LR · Fuselage Main, Frame
  > MAJOR: AFT WET AREA CORROSION ON FR 84 (BY SEAT TRACK RH) AS MARKED. REMOVED CORROSION BY BLENDING PER SRM 51-10-03 ON AFT WET AREA ON FR 84 (BY SEAT TRACK RH. MAX MATERIAL LOSS.012. REMAINING.088. COMPLY WITH ETD2019-170-157186. SEE EAMS W/O H7026 SN 47
- [SDR R61A201911261334](https://openairdocs.org/sdr/R61A201911261334.md): Seat Track · corroded · Nov 17, 2019 · N103HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH INBD SEAT TRACK INBD FLANGE CORRODED @ RIVETS AS MARKED FRAMES 46 AND 55. COMPLIED WITH PERMINANT REPAIR OF RH INBD SEAT TRACK FLANGE AND FASTENER HOLES PER ETD2019-170-156903 REV.B SEE EAMS W/O H7026 SN 368 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHE
- [SDR R61A201911261333](https://openairdocs.org/sdr/R61A201911261333.md): Seat Track · corroded · Nov 17, 2019 · N103HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH INBD SEAT TRACK INBD FLANGE CORRODED @ RIVETS AS MARKED FRAME 46 TO 55. REMOVED AND REPLACED RIVETS AT LH INBD SEAT TRACK AT FR 46-55 AND TRANSFER ADDITIONAL WORK TO WO 7026 TC S/N 575,629. SEE EAMS W/O H7026 SN 367 FOR WORK DETAILS. AIRCRAFT REMAINS IN HE
- [SDR R61A201903200304](https://openairdocs.org/sdr/R61A201903200304.md): Bracket · out of adjust · Mar 20, 2019 · N103HQ · Emb ERJ170200LR · Emergency Equipment
  > L1 DOOR WOULDN'T DISARM THE SLIDE. ADJUSTED C1 DOOR GIRT BRACKET X DIMENSIONS AND FWD COMMAND RAMPS IAW AMM 52-11-00.
- [SDR R61A201903200303](https://openairdocs.org/sdr/R61A201903200303.md): Girt Bar · out of adjust · Mar 20, 2019 · N103HQ · Emb ERJ170200LR · Emergency Equipment
  > L1 DOOR ARMING LEVER WON'T OPEN. REMOVED BUSTLE AND MANUALLY MOVED FWD GIRT BAR SPRING CLIP TO UNARM DOOR. CLEANED AND ADJUSTED DOOR GIRT BAR IAW AMM 52-11-40. OPS CHECK GOOD. REINSTALLED BUSTLE.
- [SDR R61A201903170289](https://openairdocs.org/sdr/R61A201903170289.md): Seal · debonded · Mar 17, 2019 · N103HQ · Emb ERJ170200LR · Passenger/Crew Doors
  > INABILITY TO DISARM L1 DOOR. FERRIED TO CMH. PERFORMED INSPECTION OF L1 DOOR AND FOUND AFT P-SEAL OF ACCESS PANEL 811 DLW JAMMING IN EMERGENCY EVAC SLIDE GIRT BAR. REBONDED P-SEAL TO ACCESS PANEL IAW AMM 25-00-23.
- [SDR R61A201808217903](https://openairdocs.org/sdr/R61A201808217903.md): Bustle · broken · Aug 17, 2018 · N103HQ · Emb ERJ170200LR · Passenger/Crew Doors
  > L2 DOOR IS UNABLE TO BE OPENED FROM OUTSIDE. R & R BROKEN BUSTLE IAW AMM 25-23-07.
- [SDR R61A2018071300781](https://openairdocs.org/sdr/R61A2018071300781.md): Connector · loose · Jul 10, 2018 · N103HQ · Emb ERJ170200LR · Door System Wiring
  > L1 DOOR LOCK INDICATION OPEN ON EICAS AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND CONNECTOR FOR L1 DOOR MICROSWITCH LOOSE. TIGHTENED CONNECTOR PER AMM 52-11-00.
- [SDR R61A201712080923](https://openairdocs.org/sdr/R61A201712080923.md): Lever · dirty · Dec 8, 2017 · N103HQ · Emb ERJ170200LR · Service Doors
  > R2 ARMING LEVER STIFF. CLEANED DEBRIS ON R2 ARMING LEVER IAW CMM 52-42-22. OPS CHECK GOOD.
- [SDR R61A201712010904](https://openairdocs.org/sdr/R61A201712010904.md): Shear Panel · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX CHECK, FRAME88 AFT WET AREA CENTER FLOOR PLATE HAS CORROSION AS MARKED. REMOVED AND REPLACED CENTER SHEAR PANEL AT FRAME 87-88 REF 51-42-01.
- [SDR R61A201712010903](https://openairdocs.org/sdr/R61A201712010903.md): Plate · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX CHECK, RT FRAME88 AFT WET AREA FLOOR PLATE HAS CORROSION AS MARKED. REMOVED AND REPLACED AFT WET AREA RT FLOOR PLATE BETWEEN FRAMES 87 -88.
- [SDR R61A201712010902](https://openairdocs.org/sdr/R61A201712010902.md): Crossbeam · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX CHECK, CORROSION FR16 JUST INBOARD OF L1. REMOVED AND INSTALLED NEW FR 16 CROSSBEAM REF SRM 51-41-01 REF SRM 51-41-02, 51-43-03 PN 170-98018-003.
- [SDR R61A201712010901](https://openairdocs.org/sdr/R61A201712010901.md): Seat Track · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN HEAVY MX CHECK, CORROSION RT SEAT TRACK BETWEEN FR20/21. REMOVED AND REPLACED RT SEAT TRACK BETWEEN FR20/21 REF SRM 51-40-02 AND 51-23-04 PN 170-27305-003.
- [SDR R61A201712010899](https://openairdocs.org/sdr/R61A201712010899.md): Door Sill · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX CHECK, CORROSION FOUND AT 3 AREAS ON RIGHT SILL FRAME 14. REMOVED AND REPLACED RT DOUBLER PANEL AT FRAME 14 IAW SRM 51-43-04.
- [SDR R61A201712010898](https://openairdocs.org/sdr/R61A201712010898.md): Beam · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION FOUND AT 2 AREAS ON BEAM AT FRAME 12. REMOVED AND REPLACED THE BEAM IAW SRM 51-41-02, 51-43-03, AND 51-43-04.
- [SDR R61A201712010897](https://openairdocs.org/sdr/R61A201712010897.md): Attach Fitting · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > FWD LAVATORY OUTBOARD AFT ATTACHMENT FITTING AT FRAME 16 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT FITTING.
- [SDR R61A201712010896](https://openairdocs.org/sdr/R61A201712010896.md): Floor Support · corroded · Dec 1, 2017 · N103HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT THE LT SILL FRAMES 12-13AND. REMOVED AND REPLACED THE SILL IAW SRM 51-41-02, AND 51-43-04.
- [SDR R61A201703150222](https://openairdocs.org/sdr/R61A201703150222.md): Glowstrip · missing · Mar 15, 2017 · N103HQ · Emb ERJ170100LR · Emergency Equipment
  > GLOWSTRIP NEAR L1 DOOR MISSING. ADJUSTED IN PLACE THE GLOWSTRIP IAW AMM 33-50-21.
- [SDR R61A201601070054](https://openairdocs.org/sdr/R61A201601070054.md): Flashlight · missing · Jan 7, 2016 · N103HQ · Emb ERJ170200LR · Emergency Equipment
  > DURING HEAVY CHECK, MAINTENANCE REPORTED THAT THE L1 DOOR EMERGENCY FLASHLIGHT WAS MISSING. MAINTENANCE INSTALLED NEW FLASHLIGHT IAW AMM AND OPS CHECKED GOOD. ACFT REMAINS OUT OF SERVICE IN HEAVY CHECK.
- [SDR R61A201601050044](https://openairdocs.org/sdr/R61A201601050044.md): Floorboard · corroded · Jan 5, 2016 · N103HQ · Emb ERJ170200LR · Fuselage Floor Panel
  > DURING HEAVY CHECK, FWD CARGO DOOR NET PUCKS AND CUPS ON FLOORBOARDS ARE 131CLF ARE BENT AND CORRODED. MAINTENANCE R & R FWD CARGO DOOR NET PUCKS AND CUPS ON FLOORBOARDS ARE 131CLF IAW AMM 50-22-01, PN 170-40537-403, CUP.
- [SDR R61A201601010047](https://openairdocs.org/sdr/R61A201601010047.md): Bracket · cracked · Jan 1, 2016 · N103HQ · Emb ERJ170200LR · Cabin Cooling System
  > DURING HEAVY CHECK, BRACKET FWD OF LT PACK VALVE IS CRACKED. MAINTENANCE R & R BRACKET FWD OF LT PACK VALVE IAW SRM 51-41-01, 51-43-01, 51-40-02, 51-23-04. PN 170-86944-001, SUPPORT.

Next page: https://openairdocs.org/aircraft/N103HQ/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 = 'N103HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N103HQ/reports

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