# Service difficulty reports: N135HQ

A list on [N135HQ](https://openairdocs.org/aircraft/N135HQ.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 2 · 73 reports

- [SDR R61A2026010500002](https://openairdocs.org/sdr/R61A2026010500002.md): Floorbeam · corroded · Jan 5, 2026 · N135HQ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > EVALUATED 14EA SPOT OF CORROSION ON COCKPIT COPILOT'S FLOOR DOUBLER AS MARKED AND REMOVED DAMAGE BY BLENDING. DEEPEST MEASURED(LOCATED BETWEEN FR 9-8): L=6.1", W=1", MATERIAL LOSS= 0.015", ORIGINAL THICKNESS= 0.040", MAX. ALLOWABLE MATERIAL LOSS= 0.008"(20%),
- [SDR R61A2026010500001](https://openairdocs.org/sdr/R61A2026010500001.md): Skin · damaged · Jan 5, 2026 · N135HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY CHECK. FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FR 1-2 AND STGR 2L-2R
- [SDR R61A2024092600432](https://openairdocs.org/sdr/R61A2024092600432.md): Skin · cracked · Sep 21, 2024 · N135HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > ON OVERNIGHT INSPECTION FOUND LH WING LOWER SKIN CRACKED INBD OF RIB 17 AFT OF FWD SPAR APROX 2 IN LONG. REPAIRED CRACK IAW ETD2024-170-025696 REV A. ALSO REF VP-036497-2024 N/R # 3 FOR WORK ACCOMPLISHED.
- [SDR R61A2023071300126](https://openairdocs.org/sdr/R61A2023071300126.md): Doubler · burned · Jul 18, 2023 · N135HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY CHECK VISIT MAINT FOUND BEHIND LH COCKPIT CB PANEL FRAME 10 BETWEEN STRINGER 12L AND 13L HAS BURN HOLE FROM BREAKER. PERFORMED A PERMANENT DOUBLER REPAIR ON FR 10 BETWEEN STRG 12L-13L BEHIND LH COCKPIT CB PANEL. REF ETD2023-170-017966
- [SDR R61A2023071300125](https://openairdocs.org/sdr/R61A2023071300125.md): Beam · corroded · Jul 13, 2023 · N135HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY CHECK VISIT MAINT FOUND FWD CARGO DOOR CUTOUT HORIZONTAL BEAM EDGE HAS CORROSION ABOVE 2ND FROM FOWARD C LATCH FITTING AT FR 25. REMOVED AND REPLACED FWD CARGO DOOR CUTOUT LOWER BEAM REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETI
- [SDR R61A2023071300124](https://openairdocs.org/sdr/R61A2023071300124.md): Shear Angle · corroded · Jul 13, 2023 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK VISIT MAINT FOUND A L/H SHEAR CLIP CORRODED AT FRAME 22 STGR 28L-28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
- [SDR R61A2022091900553](https://openairdocs.org/sdr/R61A2022091900553.md): Skin · cracked · Sep 15, 2022 · N135HQ · Emb ERJ170200LR · Wing Structure
  > RH WING UPPER SKIN HAS 3 CRACKS OUTBD OF RIB 10, INBD OF # 3 SPOILER INBD HINGE AND AFT OF REAR SPAR FASTNER LINE ON TOP OF WING. REPAIRED IAW ETD2022-170-029017. ALSO REF VP-040130-2022 N/R 1&4 AND LP R1018658/1 & 3 FOR WORK PERFORMED.
- [SDR R61A2020010320004](https://openairdocs.org/sdr/R61A2020010320004.md): Battery · inoperative · Jan 2, 2020 · N135HQ · Emb ERJ170200LR · Emergency Lighting
  > 1ST AND 3RD FORWARD CEILING EMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN EMER LT SET TO ON. R&R #2 ELPU IAW AMM 33-50-01, OPS CHECK GOOD.
- [SDR R61A201902260206](https://openairdocs.org/sdr/R61A201902260206.md): Fan · odor · Feb 26, 2019 · N135HQ · Emb ERJ170200LR · Air Distribution Fan
  > BURNING METAL SMELL FROM CENTER OF AIRCRAFT. ONCE RECIRC FANS TURNED OFF, SMELL BEGAN TO DISSIPATE. NO EICAS MESSAGES DURING EVENT, SMELL SUDDENLY CAME TO THE ATTENTION OF BOTH FLIGHT ATTENDANTS AND THEN PASSENGERS. DECLARED EMERGENCY, DIVERTED TO LGA, LANDED
- [SDR R61A2019020130140](https://openairdocs.org/sdr/R61A2019020130140.md): Power Supply · inoperative · Jan 30, 2019 · N135HQ · Emb ERJ170200LR · Emergency Lighting
  > FORWARD 3 EMERGENCY LIGHTS NOT WORKING, BUT NO EICAS MESSAGE. CA FOUND LIGHTS ON WHEN HE BOARDED THE AIRCRAFT. CA IS REPOWERING VIA APU. R&R #2 EMERGENCY BATTERY SUPPLY IAW AMM 33-50-01.
- [SDR R61A201611140653](https://openairdocs.org/sdr/R61A201611140653.md): Switch · out of position · Nov 14, 2016 · N135HQ · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > DURING FLIGHT, CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. AN EMERGENCY WAS NOT DECLARED AND RETURNED TO DEPARTURE WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EMERGENCY EXTENSION OVERRIDE SWITCH IN THE GEAR DOWN POSITION. MAINTENANC
- [SDR R61A201605160359](https://openairdocs.org/sdr/R61A201605160359.md): Shear Tie · damaged · May 16, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK WAS REPORTED THAT SHEAR CLIP AT SKIN DENT LOCATED AT FRAME 10 BETWEEN STRINGERS 17L-18L IS DAMAGED. MAINTENANCE R & R SHEAR CLIP AT SKIN DENT LOCATED AT FRAME 10 BETWEEN STRINGERS 17L-18L IAW SRM 51-23-06, PN 170-03216-001, SHEAR TIE.
- [SDR R61A201605160358](https://openairdocs.org/sdr/R61A201605160358.md): Shear Tie · damaged · May 16, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK, WAS REPORTED THAT SHEAR CLIP AT SKIN DENT AT FRAME 11 BETWEEN STRINGERS 17-18L IS DAMAGED. MX R & R SHEAR CLIP AT SKIN DENT AT FRAME 11 BETWEEN STR 17-18L IAW SRM 51-23-06, PN 170-03224-003, SHEAR TIE.
- [SDR R61A201605050332](https://openairdocs.org/sdr/R61A201605050332.md): Shear Plate · gouged · May 5, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK WAS REPORTED THAT FWD CARGO DOOR LOWER AFT SHEAR PLATE HAD TWO GOUGES ON PLATE. MX R & R FWD CARGO DOOR LOWER AFT SHEAR PLATE IAW SRM 51-41-02, 51-43-02. PN 170-67115-002, DOUBLER.
- [SDR R61A201605040351](https://openairdocs.org/sdr/R61A201605040351.md): Bracket · corroded · May 4, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, WAS REPORTED WASTE SERVICE BOX BRACKET ON INTERNAL SIDE OF BOX IS CORRODED. MAINTENANCE R & R WASTE SERVICE BOX BRACKET ON INTERNAL SIDE OF BOX, PN 170-87889-401, BRACKET.
- [SDR R61A201605040323](https://openairdocs.org/sdr/R61A201605040323.md): Bracket · corroded · May 4, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, WASTE SERVICE BOX BONDING BRACKET IS CORRODED. MAINTENANCE ACCOMPLISHED S/B 170-53-0095.
- [SDR R61A201605030328](https://openairdocs.org/sdr/R61A201605030328.md): Shear Plate · corroded · May 3, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, SHEAR PLATE AT FRAME 89 BETWEEN STRINGERS 25-26R IS CORRODED. MAINTENANCE R & R SHEAR PLATE IAW SRM 51-41-02.
- [SDR R61A201605030327](https://openairdocs.org/sdr/R61A201605030327.md): Shear Plate · corroded · May 3, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, SHEAR PLATE AT FRAME 89 BETWEEN STR 27-28R IS CORRODED. MAINTENANCE R & R SHEAR PLATE AT FRAME 89 BETWEEN STR 27-28, RT IAW SRM 51-41-02, PN 170-60257-001, SHEAR PLATE.
- [SDR R61A201605030322](https://openairdocs.org/sdr/R61A201605030322.md): Gusset · corroded · May 3, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY CHECK, GUSSET PLATE AT FRAME 89 AND FRAME 88 BETWEEN STR 23-24R. MAINTENANCE R & R THE GUSSET PLATE IAW SRM 51-42-01, 51-43-03, 51-40-02.
- [SDR R61A201605010350](https://openairdocs.org/sdr/R61A201605010350.md): Bolt · corroded · May 1, 2016 · N135HQ · Emb ERJ170200LR · Drag Control System
  > DURING HEAVY CHECK, LT WING, NR 4 SPOILER PCU TOP BOLT IS CORRODED. MAINTENANCE R & R LT WING NR 4 SPOILER PCU TOP BOLT IAW AMM 27-65-01, PN NAS6212-31D.
- [SDR R61A201605010333](https://openairdocs.org/sdr/R61A201605010333.md): Doubler · gouged · May 1, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY CHECK WAS REPORTED THAT FWD CARGO DOOR LOWER HORIZONTAL BEAM FWD TOP PLATE IS GOUGED. MAINTENANCE R & R FWD CARGO DOOR LOWER HORIZONTAL BEAM FWD TOP PLATE IAW SRM 51-40-02, 51-43-02, 51-41-02, PN 170-67115-001, DOUBLER.
- [SDR R61A201605010330](https://openairdocs.org/sdr/R61A201605010330.md): Bolt · corroded · May 1, 2016 · N135HQ · Emb ERJ170200LR · Wing Main, Frame Structure
  > DURING HEAVY CHECK, LT WING NR 5 MFS PCV TOP BOLT ATTACHING HARDWARE IS CORRODED. MX R & R LT WING NR 5 MFS PCV TOP BOLT ATTACHING HARDWARE IAW AMM 27-65-01, NAS6212-31D, BOLT.
- [SDR R61A201605010329](https://openairdocs.org/sdr/R61A201605010329.md): Bushing · corroded · May 1, 2016 · N135HQ · Emb ERJ170200LR · Spoilers
  > HEAVY CHECK WAS REPORTED THAT LT WING SPOILER 1 PCU ATTACH FITTING BUSHING ARE CORRODED. MAINTENANCE R & R LT WING SPOILER 1 PCU ATTACH FITTING BUSHING IAW AMM 20-10-08, PN 170-34140-003 BUSHING.
- [SDR R61A201605010326](https://openairdocs.org/sdr/R61A201605010326.md): Seat Track · corroded · May 1, 2016 · N135HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK, CABIN FLOORBEAM INBD OF FWD LAV AFT MOUNT HOLE IS CORRODED. MAINTENANCE R & R CABIN FLOORBEAM INBD OF FWD LAV AFT MOUNT HOLE IAW SRM 51-43-01, 51-43-02, AND 51-41-01.
- [SDR R61A201604300338](https://openairdocs.org/sdr/R61A201604300338.md): Seal Rest · corroded · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, FWD CARGO DOOR, ALL 3 LOWER SEAL REST HAVE CORROSION. MAINTENANCE R & R FWD CARGO DOOR ALL 3 LOWER SEAL REST IAW SRM 51-44-01, AMM 20-10-01.
- [SDR R61A201604300337](https://openairdocs.org/sdr/R61A201604300337.md): Nut · corroded · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Trailing Edge Flap Control System
  > DURING HEAVY CHECK, NR 2 FLAP TRACK SUPPORT FWD MOUNTING HARDWARE IS CORRODED. MAINTENANCE R & R NR 2 FLAP TRACK SUPPORT, FWD MOUNTING HARDWARE IAW AMM 57-54-21. PN MS14145L8, NUT.
- [SDR R61A201604300331](https://openairdocs.org/sdr/R61A201604300331.md): Rib · cracked · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > DURING HEAVY CHECK, RT HORIZONTAL STABILIZER, RIB 4 RIVETS BACK FROM FWD SPAR AT UPPER SKIN ATTACH POINT RIB 12 IS CRACKED MAINTENANCE R & R RT HORIZONTAL STABILIZER, RIB 4 RIVETS BACK FROM FWD SPAR AT UPPER SKIN ATTACH POINT RIB 12 IAW SRM 51-40-02, 51-41-02.
- [SDR R61A201604300325](https://openairdocs.org/sdr/R61A201604300325.md): Fitting · corroded · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Emergency Equipment
  > DURING HEAVY CHECK, AFT SIDE OF AFT GIRT BAR FITTING ON L2 DOOR CUTOUT LOWER BEAM IS CORRODED. MAINTENANCE BLENDED OUT CORROSION AFT SIDE OF AFT GIRT BAR FITTING ON L2 DOOR CUTOUT LOWER BEAM IAW SRM 53-23-11.
- [SDR R61A201604300324](https://openairdocs.org/sdr/R61A201604300324.md): Fitting · broken · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Emergency Equipment
  > DURING HEAVY CHECK, NUT PLATE AT L2 DOOR GIRT BAR FITTING AFT OTBD HOLE OF AFT GIRT BAR FITTING IS BROKEN. MAINTENANCE R & R NUT PLATE L2 DOOR GIRT BAR FITTING AFT OTBD HOLE OF AFT GIRT BAR FITTING IAW SRM 51-42-02.
- [SDR R61A201604300320](https://openairdocs.org/sdr/R61A201604300320.md): Spar · cracked · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Wing Spar
  > DURING HEAVY CHECK, RT SPAR 3 HAS CRACK LIKE INDICATIONS. MAINTENANCE REAMED HOLE IAW ETD2016170-041851.
- [SDR R61A201604300319](https://openairdocs.org/sdr/R61A201604300319.md): Spar · cracked · Apr 30, 2016 · N135HQ · Emb ERJ170200LR · Wing Spar
  > DURING HEAVY CHECK, LT SPAR 3 WING STUB HAS CRACK LIKE INDICATIONS IN FASTENER HOLE. MAINTENANCE REAMED HOLE IAW ETD2016-170-041851.
- [SDR R61A201604280342](https://openairdocs.org/sdr/R61A201604280342.md): Case · loose · Apr 28, 2016 · N135HQ · Emb ERJ170200LR · Escape Slide
  > DURING HEAVY CHECK, MAINTENANCE FOUND THE L2 DOOR SLIDE CASING WAS UNRAVELING. MAINTENANCE R & R L2 DOOR SLIDE IAW AMM AND OPS CHECKED GOOD. ACFT REMAINS OUT OF SERVICE IN HEAVY CHECK.
- [SDR R61A201604250287](https://openairdocs.org/sdr/R61A201604250287.md): Handset · intermittent · Apr 25, 2016 · N135HQ · Emb ERJ170200LR · Lighting System
  > CREW REPORTED THAT THE AFT F/T RAINBOW LIGHT WAS FLICKERING.
- [SDR R61A201604200258](https://openairdocs.org/sdr/R61A201604200258.md): Warning Message · unknown · Apr 20, 2016 · N135HQ · Emb ERJ170200LR · Central Warning
  > CREW REPORTED ADS 1, 2, 3 & 4 FAILURE ALONG WITH WINDSHEAR FAIL, STALL PROT FAIL, AOA LIMIT FAIL AND A/T FAIL AFTER FLYING THRU WAKE TURBULANCE. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE RESET ACFT POWER IAW AMM AND ALL FAULTS CLEARED.
- [SDR R61A201509140635](https://openairdocs.org/sdr/R61A201509140635.md): Engine · power loss · Sep 14, 2015 · N135HQ · Emb ERJ170200LR · Engine (Turbine/Turboprop)
  > CREW REPORTED A LOUD BANG FOLLOWED BY LOSS OF ALL POWER FROM THE NR 1 ENGINE. CREW DECLARED AN EMERGENCY, RAN QRH AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT.
- [SDR R61A201506160372](https://openairdocs.org/sdr/R61A201506160372.md): Wire Harness · damaged · Jun 16, 2015 · N135HQ · Emb ERJ170200LR · Flight Control System Wiring
  > ON GEAR RETRACTION, CREW RECEIVED A SLAT FAIL MESSAGE. RAN QRH, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND R & R THE RT OTBD SLAT HARNESS AND SKEW SENSOR IAW AMM AND OPS CHECKED
- [SDR R61A201412201254](https://openairdocs.org/sdr/R61A201412201254.md): Flashlight · inoperative · Dec 20, 2014 · N135HQ · Emb ERJ170200LR · Emergency Equipment
  > CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201412061224](https://openairdocs.org/sdr/R61A201412061224.md): Flashlight · inoperative · Dec 6, 2014 · N135HQ · Emb ERJ170200LR · Emergency Equipment
  > CREW REPORTED THAT THE AFT FLASHLIGHT WAS NOT CHARGING. MAINTENANCE R & R AFT FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201406190778](https://openairdocs.org/sdr/R61A201406190778.md): Bolt · corroded · Jun 19, 2014 · N135HQ · Emb ERJ170200LR · Main Landing Gear
  > DURING HEAVY CHECK, RT MLG SIDE STAY ATTACH BOLT PIN CORRODED. MX R & R RT MLG SIDE STAY ATTACH BOLT PIN IAW AMM 32-11-05.
- [SDR R61A201406140779](https://openairdocs.org/sdr/R61A201406140779.md): Bushing · corroded · Jun 14, 2014 · N135HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > DURING HEAVY CHECK, HORIZONTAL STAB RT HINGE FITTING BEARING BORE IS CORRODED. MX REPAIRED HORIZONTAL STABILIZER RT FITTING IAW ETD 2014-170-050071 REV A AND B AND TECHNICAL INSTRUCTION TI-170-14-043 REV A, B. TASK 55-10-020-00001.
- [SDR R61A201406140777](https://openairdocs.org/sdr/R61A201406140777.md): Pin · corroded · Jun 14, 2014 · N135HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > DURING HEAVY CHECK, EXTERNAL HINGE PIN AT FRAME 100 ON RT SIDE ALONG WITH 2 FLOATING HAT BUSHINGS ARE CORRODED. MX R & R 2 FLOATING HAT BUSHINGS, EXTERNAL HINGE PIN AT FRAME 100 RT SIDE, PN 170-62007-001, EXTERNAL PIN, 170-61254-001, BUSHING, 170-61250-001
- [SDR R61A201406130776](https://openairdocs.org/sdr/R61A201406130776.md): Rod End · corroded · Jun 13, 2014 · N135HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > DURING HEAVY CHECK, HORIZONTAL STAB RT ROD END ON HINGE PIN ADJUSTABLE ROD IS CORRODED. MX R & R HORIZONTAL STAB, RT ROD END ON HINGE PIN ADJUSTABLE ROD IAW AMM 27-41-03.
- [SDR R61A201406120781](https://openairdocs.org/sdr/R61A201406120781.md): Isolator · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · APU Cowling/Containment
  > DURING HEAVY CHECK, RT APU MOUNT ISOLATOR BOLTS CORRODED. MX R & R RT APU MOUNT ISOLATOR BOLTS IAW AMM 170/175 AMM 53-31-35, PN 960073-14 ISOLATOR.
- [SDR R61A201406120780](https://openairdocs.org/sdr/R61A201406120780.md): Isolator · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · APU Cowling/Containment
  > DURING HEAVY CHECK WAS REPORTED THAT LT APU MOUNT ISOLATOR BOLTS CORRODED. MX R & R LT APU MOUNT ISOLATOR ASSY INSTALLED IAW AMM 53-31-35, PN 96073-15 ISOLATOR.
- [SDR R61A201406120766](https://openairdocs.org/sdr/R61A201406120766.md): Doubler · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Aerodynamic Fairings
  > DURING HEAVY CHECK, PANEL 192CR ON INTERNAL DOUBLER OF PANEL HAS HEAVY CORROSION. MX R & R INTERNAL DOULBER IAW SRM 51-41-02.
- [SDR R61A201406120763](https://openairdocs.org/sdr/R61A201406120763.md): Shear Plate · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, AFT WET AREA ON LT SHEAR PLATE AT FRAME 88 IS CORRODED. R & R SHEAR PLATE IAW SRM 51-40-02,51-42-01, 51-42-02.
- [SDR R61A201406120762](https://openairdocs.org/sdr/R61A201406120762.md): Shear Plate · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, AFT WET AREA ON MIDDLE SHEAR PLATE AT FRAME 88 IS CORRODED. MX R & R SHEAR PLATE IAW SRM 51-40-02.
- [SDR R61A201406120761](https://openairdocs.org/sdr/R61A201406120761.md): Shear Plate · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, AFT WET AREA RT SHEAR PLATE AT FRAME 88 IS CORRODED. MX R & R SHEAR PLATE IAW SRM 51-40-02.
- [SDR R61A201406120760](https://openairdocs.org/sdr/R61A201406120760.md): Seat Track · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK, AFT WET AREA ON RT INBD SEAT TRACK EXTENSION, BETWEEN FRAMES 86-87 IS CORRODED. MX R & R SEAT TRACK IAW SRM 51-40-02.
- [SDR R61A201406120759](https://openairdocs.org/sdr/R61A201406120759.md): Seat Track · corroded · Jun 12, 2014 · N135HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK, RT INBD SEAT TRACK EXTENSION AT FRAME 86 RIVET HEADS ARE CORRODED. MX R & R RT INBD SEAT TRACK IAW SRM 51-40-02, 51-41-01,51-43-01.

Next page: https://openairdocs.org/aircraft/N135HQ/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 = 'N135HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N135HQ/reports

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