# Service difficulty reports: N104HQ

A list on [N104HQ](https://openairdocs.org/aircraft/N104HQ.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 · 102 reports

- [SDR R61A2025112700519](https://openairdocs.org/sdr/R61A2025112700519.md): Sensor · faulted · Nov 27, 2025 · N104HQ · Emb ERJ170200LR · Trailing Flap Position Indicating System
  > FLAP FAIL AT ZERO AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CHANGED THE T3 SKEW SENSOR.
- [SDR R61A2025112600518](https://openairdocs.org/sdr/R61A2025112600518.md): Actuator · faulted · Nov 26, 2025 · N104HQ · Emb ERJ170200LR · Trailing Edge Flap Actuator
  > FLAP FAIL AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3 FLAP ACTUATOR.
- [SDR R61A2025071800313](https://openairdocs.org/sdr/R61A2025071800313.md): Stringer · corroded · Jul 18, 2025 · N104HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY CHECK - AFT CARGO STGR 29R SHOWS SIGNS OF CORROSION. PERFORMED SPLICE REPAIR ON STINGER 29R REF ETD2025-170-924028.
- [SDR R61A2025071800312](https://openairdocs.org/sdr/R61A2025071800312.md): Skin · cracked · Jul 17, 2025 · N104HQ · Emb ERJ170200LR · Wing, Plate/Skin
  > WHILE IN HEAVY CHECK - RH WING CRACK ON LOWER SKIN BETWEEN RIBS 4 & 5 AT SPAR 2. REPAIRED RH WING LOWER SKIN BETWEEN RIBS 4 & 5 AT SPAR 2 REF ETD2025-170-923747.
- [SDR R61A2023010600058](https://openairdocs.org/sdr/R61A2023010600058.md): Floor Support · corroded · Jan 7, 2023 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK - TOOLING MARK FRAME 84 FROM LH FLOOR SILL TO LH INBD SEAT TRACK. REMOVED DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLE, AND SHIMS. REF ETD2022-170-037256 REV. A.
- [SDR R61A2023010600057](https://openairdocs.org/sdr/R61A2023010600057.md): Intercostal · corroded · Jan 7, 2023 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK - "HEATED DRAIN MAST INTERCOSTAL BETWEEN FR86/87 STR27R/28R. REMOVED & REPLACED HEATED DRAIN MAST NTERCOSTAL BETWEEN FR8687 TR27R28R. REF SRM 51-40-08."
- [SDR R61A2023010600056](https://openairdocs.org/sdr/R61A2023010600056.md): Shear Tie · corroded · Jan 7, 2023 · N104HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY CHECK - SHEAR CLIP AT FR88 BETWEEN STR27R/28R. REMOVED AND REPLACED SHEAR CLIP AT FR 88 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08.
- [SDR R61A2023010600055](https://openairdocs.org/sdr/R61A2023010600055.md): Profile · gouged · Jan 7, 2023 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY CHECK - FWD AVIONICS COMPARTMENT ACCESS HATCH AFT FRAME GOUGED BELOW L/H LOCKPIN. REMOVED AND REPLACED FWD AVIONICS COMPARTMENT ACCESS HATCH PROFILE. REF EMB SRM 51-40-08.
- [SDR R61A2021022500192](https://openairdocs.org/sdr/R61A2021022500192.md): Shear Tie · corroded · Feb 21, 2021 · N104HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT CARGO INTERNAL SIDE FUSELAGE SHEAR CLIP IS CORRODED AT FR 82 STRG 28R-29R. REMOVED AND REPLACED AFT CARGO INTERNAL SIDE FUSELAGE SHEAR CLIP AT FR 82 STRG 28R-29R. REF SRM 51-40-02. 51-40-08.
- [SDR R61A2021022500191](https://openairdocs.org/sdr/R61A2021022500191.md): Shear Tie · corroded · Jan 21, 2021 · N104HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY CHECK FOUND AFT CARGO INTERNAL SIDE FUSELAGE SHEAR CLIPS ARE CORRODED AT FR 83 STRG 27R-29R. REMOVED AND REPLACED SHEAR CLIPS IN AFT CARGO INTERNAL SIDE FUSELAGE AT FR 83 STRG 27R-29R. REF SRM 51-40-08.
- [SDR R61A2020070900555](https://openairdocs.org/sdr/R61A2020070900555.md): Power Unit · inoperative · Jul 9, 2020 · N104HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHTS IN AFT CABIN STAY ON WHEN A/C TURNED OFF. R&R AFT OUTBOARD ELPU.
- [SDR R61A2020052800501](https://openairdocs.org/sdr/R61A2020052800501.md): Power Unit · inoperative · May 27, 2020 · N104HQ · Emb ERJ170200LR · Emergency Lighting
  > DURING TEST OF EMERGENCY LIGHTING SYSTEM, SEVERAL LIGHTS IN FORWARD LEFT HAND AREA DID NOT ILLUMINATE. R & R ELPU NR 2 IAW AMM 33-50-01.
- [SDR R61A2019120541351](https://openairdocs.org/sdr/R61A2019120541351.md): Skin · dented · Dec 4, 2019 · N104HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE INSPECTION 2 DENTS WERE DISCOVERED ON RH FORWARD FUSLAGE BETWEEN FRAMES 8 & 9 AND BETWEEN STR 17R & 18R. DAMAGE WAS REPAIRED IAW EMBRAER ETD 2019-170-159946 B. AC RETURNED TO SERVICE.
- [SDR R61A201902221182](https://openairdocs.org/sdr/R61A201902221182.md): Lever · lack of lube · Feb 21, 2019 · N104HQ · Emb ERJ170200LR · Service Doors
  > FA HAS DIFFICULTY DISARMING R1 DOOR. CLEANED AND LUBED R1 ARM AND DISARM LEVER IAW CMM 52-41-22.
- [SDR R61A201806080682](https://openairdocs.org/sdr/R61A201806080682.md): Gasket · damaged · Jun 8, 2018 · N104HQ · Emb ERJ170200LR · Pneumatic Distribution System
  > DURING CLIMB OUT, RECEIVED BLEED 2 LEAK MESSAGE. AT LANDING, RECEIVED BLEED 1 LEAK MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE NR 2 PRECOOLER GASKETS RT ENGINE, 1 PRECOOLER GASKET (AFT) ON LH ENGINE, AND R&R 4 CERAMIC PINS ON FIRE LOOPS.
- [SDR R61A201806050676](https://openairdocs.org/sdr/R61A201806050676.md): Doubler · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION WAS ON THE INNER SURFACE OF PANEL 192CR. REMOVED DAMAGED DOUBLER, REMOVED SURFACE CORROSION ON THE PANEL UNDER DOUBLER, INSPECTED, TREATED AND PAINTED PANEL, INSTALLED NEW DOUBLER.
- [SDR R61A201806050675](https://openairdocs.org/sdr/R61A201806050675.md): Support Bracket · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FRAME 89 AND 90 RT SIDE OF CROSS BEAM HAD CORROSION AT THE PANEL SUPPORT. REMOVED AND REPLACED THE PANEL SUPPORT BRACKET IAW SRM 51-40-08.
- [SDR R61A201806050674](https://openairdocs.org/sdr/R61A201806050674.md): Support · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FRAME 85 RT SIDE OF CROSS BEAM HAD CORROSION AT THE PANEL SUPPORT. REMOVED AND REPLACED THE CROSS BEAM PANEL SUPPORT BRACKET AT FRAME 85 IAW SRM 51-40-08.
- [SDR R61A201806050673](https://openairdocs.org/sdr/R61A201806050673.md): Seat Track · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FRAMES 84 LEFT SEAT TRACK HAD CORROSION. PERFORMED A PERMANENT REPAIR ON THE SEAT TRACK IAW SRM 53-00-10-R-01P.
- [SDR R61A201806050672](https://openairdocs.org/sdr/R61A201806050672.md): Floor Support · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT FRAME 84, LEFT SIDE OF THE CROSSBEAM HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.
- [SDR R61A201806050671](https://openairdocs.org/sdr/R61A201806050671.md): Closeout Panel · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO CLOSE-OUT PANEL WAS CORRODED. REMOVED AND REPLACED THE CLOSEOUT PANEL.
- [SDR R61A201806050670](https://openairdocs.org/sdr/R61A201806050670.md): Closeout Panel · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THE FWD CARGO CLOSE-OUT PANEL WAS CORRODED. REMOVED AND REPLACED THE CLOSE OUT PANEL IAW AMM 20-10-07.
- [SDR R61A201806050669](https://openairdocs.org/sdr/R61A201806050669.md): Floor Support · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD WET AREA RT TRACK SUPPORT BEAM HAD CORROSION, BETWEEN FRAMES 17 AND 18. REPLACEED THE FLOOR SUPPORT.
- [SDR R61A201806050668](https://openairdocs.org/sdr/R61A201806050668.md): Floor Support · corroded · Jun 5, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD WET AREA LEFT FLOOR SUPPORT WAS CORRODED AT FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT.
- [SDR R61A201805250602](https://openairdocs.org/sdr/R61A201805250602.md): Floor Support · corroded · May 17, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR SUPPORT HAD CORROSION BETWEEN FRAMES 13 AND 14. REPLACED THE FLOOR SUPPORT.
- [SDR R61A201806090681](https://openairdocs.org/sdr/R61A201806090681.md): Skin · dented · May 16, 2018 · N104HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, FUSELAGE EXTERNAL SURFACE HAS A DENT BETWEEN FR 29 AND FR 30 STR L3 AND L4 5" X.5". REMOVED DENT BY CUTOUT ON FUSELAGE EXTERNAL SURFACE AT FR 29 AND FR 30 STR L3 AND L4 AND PERFORMED PERMANENT DOUBLER REPAIR, REF SRM 53-21-01 R10, 51-75-17. SEE
- [SDR R61A201806090680](https://openairdocs.org/sdr/R61A201806090680.md): Service Door · corroded · May 16, 2018 · N104HQ · Emb ERJ170200LR · Service Doors
  > CORROSION WASTE SERVICE DOOR FRAME 88/89 STRINGER 25R/28R. REMOVED AND REPLACED WASTE SERVICE DOOR PN: 170-86668-403 REF SRM 51-40-08 & 20-10-01. SEE W/O H6230 SN 111 FOR WORK DETAILS.
- [SDR R61A201803060303](https://openairdocs.org/sdr/R61A201803060303.md): Cabin Pressure · intermittent · Mar 6, 2018 · N104HQ · Emb ERJ170200LR · Cabin Pressure Control System
  > AT 12000 FEET, CABIN ALTITUDE 900 FEET, THEN AT 14000 FEET CABIN ALTITUDE 100 FEET. WENT TO MANUAL TO CONTROL CABIN ALTITUDE. AT 5000 FEET, WENT BACK TO AUTO AND SEEMED TO FUNCTION IN AUTO NORMALLY. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED PRESSU
- [SDR R61A201705050342](https://openairdocs.org/sdr/R61A201705050342.md): Light · unsecure · May 5, 2017 · N104HQ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY EXIT LIGHT STRIP AT ROW 1 SEPARATED FROM FLOOR. RE-INSTALLED AND SECURED LUMINESCENT STRIP IAW AMM 25-24-02.
- [SDR R61A201705040340](https://openairdocs.org/sdr/R61A201705040340.md): Light · detached · May 4, 2017 · N104HQ · Emb ERJ170200LR · Emergency Lighting
  > FWD BULKHEAD, RT EMERGENCY LIGHT DETACHED. SECURED THE LIGHT STRIP IAW AMM 33-50-21.
- [SDR R61A201607230428](https://openairdocs.org/sdr/R61A201607230428.md): Flashlight · missing · Jul 23, 2016 · N104HQ · Emb ERJ170200LR · Emergency Equipment
  > CREW REPORTED THAT THE FIRST OFFICERS FLASHLIGHT WAS MISSING. MAINTENANCE INSTALLED A NEW FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201606020381](https://openairdocs.org/sdr/R61A201606020381.md): Rod · not reported · Jun 2, 2016 · N104HQ · Emb ERJ170200LR · Trailing Edge Flap Control System
  > CREW REPORTED A FLAP FAILURE. AN EMERGENCY WAS DECLARED AND CREW RETURNED TO DEPARTURE, WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE R & R NR 1 UPPER FLAP ROD, NR 2 UPPER FLAP ROD, NR 2 LOWER FLAP ROD AND RT WING NR 3 UPPER FLAP ROD IAW AMM AND OPS CHECKE
- [SDR R61A201603060172](https://openairdocs.org/sdr/R61A201603060172.md): Lock · broken · Mar 6, 2016 · N104HQ · Emb ERJ170200LR · Landing Gear Door Retract Section
  > CREW RECEIVED A LANDING GEAR NOSE DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AN CREW LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN LOCKING DEVICE ON LT AFT NLG DOOR LINKAGE. MAINTENANCE PERFORMED TEMP GEAR DOOR LINKAGE ADJUSTMENT IAW AMM AND PLA
- [SDR R61A201512030913](https://openairdocs.org/sdr/R61A201512030913.md): Rib · cracked · Dec 3, 2015 · N104HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > DURING HEAVY CHECK WAS REPORTED THAT RIB 4 ON RT HORIZONTAL STABILIZER L/E IS CRACKED. MAINTENANCE REPAIRED RIB 4 ON RT HORIZONTAL STABILIZER L/E IAW ETD-2015-170-112427.
- [SDR R61A201511290914](https://openairdocs.org/sdr/R61A201511290914.md): Intercostal · corroded · Nov 29, 2015 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, REPORTED THAT CORROSION ON DRAIN INTERCOSTAL, REAR BETWEEN FRAMES 86-87 BETWEEN STRINGERS 27R-28R. MAINTENANCE REMOVED INTERCOSTAL AND FABRICATED NEW PART AND INSTALLED PART IAW SRM 170/175, SRM 51-41-01, 51-31-01, 51-23-04, 51-23-05, 51-2
- [SDR R61A201511290906](https://openairdocs.org/sdr/R61A201511290906.md): Intercostal · corroded · Nov 29, 2015 · N104HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, DRAIN INTERCOASTALS FWD BETWEEN FRAME 86-87, STRINGERS 27R AND 28R DRAIN IS CORRODED. MAINTENANCE R & R INTERCOASTALS FWD BETWEEN FRAME 86-87, STRINGERS 27R AND 28R IAW SRM 51-41-01, PN 170-87560-001 INTERCOSTAL,
- [SDR R61A201511290887](https://openairdocs.org/sdr/R61A201511290887.md): Shear Tie · corroded · Nov 29, 2015 · N104HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK, SHEAR CLIP AT FRAME 86, STRINGER 27-28R IS CORRODED. MAINTENANCE R & R SHEAR CLIP AT FRAME 86, STRINGER 27-28R IAW SRM 170 51-41-01, PN 170-6603-001, SHEAR CLIP.
- [SDR R61A201511290886](https://openairdocs.org/sdr/R61A201511290886.md): Shear Tie · corroded · Nov 29, 2015 · N104HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING HEAVY CHECK, SHEAR CLIP ON FRAME 87 BETWEEN STRINGERS 27R-28R IS CORRODED. MAINTENANCE R & R SHEAR CLIP ON FRAME 87 BETWEEN STRINGERS 27R-28R IAW SRM 51-41-01, PN 170-66041-002, SHEAR CLIP.
- [SDR R61A201511270907](https://openairdocs.org/sdr/R61A201511270907.md): Nut Plate · corroded · Nov 27, 2015 · N104HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > MAJOR REPAIR, DURING HEAVY CHECK WAS REPORTED THAT L1 DOOR STEP FLOORBOARD CLIP NUT PLATE IS CORRODED. MAINTENANCE R & R L1 DOOR LOWER BEAM IAW SRM 51-40-02, 51-43-02, 51-21-02, 51-23-06, PN 170-031719-005, BEAM.
- [SDR R61A201511270905](https://openairdocs.org/sdr/R61A201511270905.md): Firewall · cracked · Nov 27, 2015 · N104HQ · Emb ERJ170200LR · APU Cowling/Containment
  > DURING HEAVY CHECK, APU FIREWALL 351AZ CRACKED AT TOP AND BOTTOM OF L ANGLE. MAINTENANCE BLENDED OUT CRACKS IN APU FIREWALL, 351AZ CRACKED AT TOP AND BOTTOM IAW SRM 53-31-21.
- [SDR R61A201511270893](https://openairdocs.org/sdr/R61A201511270893.md): Firewall · cracked · Nov 27, 2015 · N104HQ · Emb ERJ170200LR · APU Cowling/Containment
  > DURING HEAVY CHECK, APU FIRE WALL PANEL 351AZ IS CRACKED AT TOP, BOTTOM OF LT ANGLE. MAINTENANCE TRIMMED OUT DAMAGE, NO REINENFORCEMENT ON APU FIRE WALL IAW SRM 53-31-21.
- [SDR R61A201511260888](https://openairdocs.org/sdr/R61A201511260888.md): Bearing · corroded · Nov 26, 2015 · N104HQ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > DURING HEAVY CHECK, NR 1 BEARING ON HORIZONTAL STABILIZER FOR RT ELEVATOR IS PITTED. MAINTENANCE R & R NR 1 BEARING ON HORIZONTAL STABILIZER FOR RT ELEVATOR IAW AMM 20-10-08, PN DSRP-FS464, BEARING.
- [SDR R61A201511250921](https://openairdocs.org/sdr/R61A201511250921.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, WAS REPORTED THAT LT WING NR 3 SPOILER PANEL MOUNTING HARDWARE IS CORRODED. MAINTENANCE R & R LT WING NR 3 SPOILER PANEL MOUNTING HARDWARE IAW AMM 27-64-01.
- [SDR R61A201511250920](https://openairdocs.org/sdr/R61A201511250920.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, LT WING SPOILER NR 3 PCU BOLT, NUT, BUSHING ARE CORRODED. MAINTENANCE R & R LT WING SPOILER NR 3 PCU BOLT, NUT, BUSHING IAW AMM 27-64-01. PN NAS6212-31D, BOLT.
- [SDR R61A201511250919](https://openairdocs.org/sdr/R61A201511250919.md): Bushing · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Ailerons
  > DURING HEAVY CHECK, WAS REPORTED THAT LT WING SPOILER NR 3 MOUNT FITTING ON WING BUSHINGS HAVE PITTING. MAINTENANCE R & R LEFT WING SPOILER NR 3 MOUNT FITTING ON WING BUSHINGS IAW AMM 20-10-08, PN 170-32258-001, BUSHING.
- [SDR R61A201511250912](https://openairdocs.org/sdr/R61A201511250912.md): Bushing · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Wing Main, Frame Structure
  > DURING HEAVY CHECK, LT WING NR 3 PCU MOUNT FITTING ON PANEL BUSHING IS CORRODED. MAINTENANCE R & R LT WING NR 3 PCU MOUNT FITTING ON PANEL IAW AMM 20-10-08. PN 170-34140-003, BUSHING.
- [SDR R61A201511250911](https://openairdocs.org/sdr/R61A201511250911.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, RT WING NR 4 SPOILER PCU BOLT IS CORRODED. MAINTENANCE R & R RT WING NR 4 SPOILER PCU BOLT IAW AMM 27-65-01, PN NAS6212-31D, BOLT.
- [SDR R61A201511250910](https://openairdocs.org/sdr/R61A201511250910.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, WAS REPORTED THAT LT WING NR 4, NR 5 SPOILER PCU BOLTS, NUTS, BUSHINGS ARE WORN AND CORRODED. MAINTENANCE R & R LT WING NR 4, NR 5 SPOILER PCU BOLTS, NUTS, BUSHINGS IAW AMM 27-64-01, P/N NAS62123-13D, BOLT.
- [SDR R61A201511250909](https://openairdocs.org/sdr/R61A201511250909.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, RT SPOILER NR 5 PCU BOLT IS CORRODED. MAINTENANCE R & R RT SPOILER NR 5 PCU BOLT IAW AMM 27-65-01, PN NAS 6212-31D, BOLT.
- [SDR R61A201511250904](https://openairdocs.org/sdr/R61A201511250904.md): Bolt · corroded · Nov 25, 2015 · N104HQ · Emb ERJ170200LR · Drag Control Actuator
  > DURING HEAVY CHECK, NR 3 SPOILER PCU BOLT IS CORRODED. MAINTENANCE R & R NR 3 SPOILER PCU BOLT IAW AMM 27-65-01, PN NAS6212-31D, BOLT.

Next page: https://openairdocs.org/aircraft/N104HQ/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 = 'N104HQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N104HQ/reports

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