# Service difficulty reports: N416QS

A list on [N416QS](https://openairdocs.org/aircraft/N416QS.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR JGVR20260718004](https://openairdocs.org/sdr/JGVR20260718004.md): Skin · corroded · Jul 18, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > REMOVED 30 AREAS OF SUSPECTED CORROSION LOCATED ON LT WING UPPER SKIN TRAILING EDGE FWD OF PANELS 551AT, 532BT, 532AT, INBD AND OUTBD SPOILER PANELS, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECH
- [SDR JGVR20260718003](https://openairdocs.org/sdr/JGVR20260718003.md): Skin · corroded · Jul 18, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > REMOVED TOPCOAT ON 9 AREAS OF SUSPECTED CORROSION LOCATED ON RH WING LOWER SKIN TRAILING EDGE FWD OF FLAP PANELS 641TB, 641SB AND 641PB, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICE
- [SDR JGVR20260718001](https://openairdocs.org/sdr/JGVR20260718001.md): Skin · corroded · Jul 18, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > REMOVED TOPCOAT ON 3 AREAS OF SUSPECTED CORROSION LOCATED ON LH WING LOWER SKIN TRAILING EDGE FWD OF PANELS 541PB AND 541QB, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR DXT2026F00000](https://openairdocs.org/sdr/DXT2026F00000.md): Skin · corroded · Jul 18, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > MECHANICALLY REMOVED 12 AREAS OF CORROSION LOCATED ON RT WING TRAILING EDGE, UPPER SKIN FWD OF PANEL 632AT AND 632BT, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR 2026F00154](https://openairdocs.org/sdr/2026F00154.md): Skin · corroded · Jul 17, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > MECHANICALLY REMOVED 15 AREAS OF CORROSION LOCATED ON RH UPPER WING TRAILING EDGE, FWD OF PANELS 641AT, 641BT, AND OUTBD RH SPOILER IAW EMBRAER PHENOM 300 SRM 51-12-01 AND SRM 51-10-03. PER AQRD RFTS-117852 REV. 0. TITLED "N416QS (50500443) RH WING SKIN CORROS
- [SDR 2026F00153](https://openairdocs.org/sdr/2026F00153.md): Skin · corroded · Jul 17, 2026 · N416QS · Emb EMB505 · Wing, Plate/Skin
  > MECHANICALLY REMOVED 15 AREAS OF CORROSION LOCATED ON RH UPPER WING TRAILING EDGE, FWD OF PANELS 641AT, 641BT, AND OUTBD RH SPOILER IAW EMBRAER PHENOM 300 SRM 51-12-01 AND SRM 51-10-03. PER AQRD RFTS-117852 REV. 0. TITLED "N416QS (50500443) RH WING SKIN CORROS
- [SDR 2026F00152](https://openairdocs.org/sdr/2026F00152.md): Skin · corroded · Jul 17, 2026 · N416QS · Emb EMB505 · Nacelle/Pylon, Plate/Skin
  > MOVED 1 AREA OF CORROSION LOCATED AFT OF RH PYLON TRAILING EDGE, INBD AREA ON FUSELAGE SKIN IAW SRM 51-12-01 AND SRM 51-10-03. PER AQRD RFTS-117833 REV. 0. TITLED "N416QS (50500443) RT PYLON T/E FUSELAGE SKIN CORROSION" DATED 14JULY26. DAMAGE TOLERANCE: YES. T
- [SDR DXTA2025081404566](https://openairdocs.org/sdr/DXTA2025081404566.md): Door Seal · torn · Aug 11, 2025 · N416QS · Emb EMB505 · Passenger/Crew Doors
  > DOOR SEAL SQUEAL DURING CLIMB OUT BETWEEN 14,000 AND 20,000 AND DESCENT 8,500 AND 6,000 DELTA P 3.3PSI. SMALL DAMAGE TO SEAL ON FUSELAGE FRAME TOP LEFT CORNER. CORRECTIVE ACTION: REPLACED MED SEAL WORK PERFORMED IAW EMBRAER PHENOM 300 AMM CH. 52-10-20. PERFOR
- [SDR DXTA2025061803929](https://openairdocs.org/sdr/DXTA2025061803929.md): Power Supply · defective · Jun 16, 2025 · N416QS · Emb EMB505 · Emergency Lighting
  > AFTER ENGINE START AND WITH EMERGENCY LIGHT SWITCH IN ARM SOME OF THE CABIN EMERGENCY LIGHTS ILLUMINATED. MOVING SWITCH TO OFF DID NOT EXTINGUISH THE LIGHTS. A COUPLE CEILING LIGHTS WERE ILLUMINATED AND DOOR STEP LIGHTS. EXIT SIGNS WERE NOT ILLUMINATED. CORREC
- [SDR DXTA2024101800870](https://openairdocs.org/sdr/DXTA2024101800870.md): Interface Unit · defective · Oct 15, 2024 · N416QS · Emb EMB505 · Indicating/Recording System
  > GEA 2 FAIL WHITE CAS: DURING CRUISE FLIGHT AT FL410 WE RECEIVED A WHITE GEA 2 FAIL CAS. THIS WAS ACCOMPANIED BY YELLOW E2 FUEL IMP BYPASS, YELLOW A-I E1 FAIL, WHITE FUEL2 FEED FAULT, AND WHITE ENG NO DISPATCH. ALL SYNOPTIC SCREENS SHOWED MULTIPLE FAILED EQUIP
- [SDR DXTA2024052111824](https://openairdocs.org/sdr/DXTA2024052111824.md): Light · malfunctioned · May 20, 2024 · N416QS · Emb EMB505 · Emergency Lighting
  > CABIN EMERG LIGHT: AFTER TURNING OFF EMER LIGHT SWITCH IN COCKPIT, AND TURNING THE BATTERIES OFF, THE CABIN EMER LIGHTS CONTINUED TO STAY ON. PERFORMED,LIGHT CHECK OF THE EMERGENCY OPERATIONAL LIGHTS IAW AMM CHAPTER 33-52-00. NO FAULT DISCREPANCIES NOTED
- [SDR DXTA2024040911444](https://openairdocs.org/sdr/DXTA2024040911444.md): Control Unit · faulted · Apr 8, 2024 · N416QS · Emb EMB505 · Landing Gear Brake System
  > BRK FAIL YELLOW CAS: ON TAXI, YELLOW BRAKE FAIL MESSAGE ILLUMINATED. NEITHER PILOTS BRAKES WERE OPERATIONAL WITH THE CAS ILLUMINATED. HAD TO USE EMERGENCY BRAKE TO STOP AIRCRAFT FROM TAXIING. REMOVED "FAULTY" BRAKE CONTROL MODULE DAP00101-02 SN 019RK AND INS
- [SDR DXTA2023100997490](https://openairdocs.org/sdr/DXTA2023100997490.md): Unknown · unknown · Oct 7, 2023 · N416QS · Emb EMB505 · Passenger/Crew Doors
  > UPPER RIGHT DOOR PIN GREEN FLAG FOR THE CLOSED AND LOCKED INDICATION IS NOT VISIBLE THROUGH THE VIEW WINDOW. VERIFIED DISCREPANCY. GREEN FLAG ON UPPER RIGHT PIN HAS WORN OFF. REMOVED AIRSTAIRS IAW EMB-505 MM, 52-14-00. NOTIFIED NETJETS. GREEN PAINT IS ON ORDE
- [SDR DXTA2023032082860](https://openairdocs.org/sdr/DXTA2023032082860.md): Unknown · unknown · Mar 18, 2023 · N416QS · Emb EMB505 · Passenger/Crew Doors
  > MAIN DOOR HANDLE: DOOR WILL NOT CLOSE FROM EITHER INSIDE OR OUTSIDE DOOR IS STUCK IN THE OPENING POSITION. //SIGNOFF// PERFORMED DVI OF DOOR MECHANISM, HANDLE, LOCKING MECHANISM AND SEAL IAW EMBRAER OUTSIDE DOOR IS STUCK IN TL IE OPENING POSITON. PHENOM 300 AM
- [SDR DXTA2023011678570](https://openairdocs.org/sdr/DXTA2023011678570.md): Door · lack of lube · Jan 15, 2023 · N416QS · Emb EMB505 · Passenger/Crew Doors
  > EXCESSIVE FORCE REQUIRED ON BOTH INTERIOR AND EXTERIOR HANDLES TO LOCK MAIN CABIN DOOR. DOOR SEAL RECENTLY REPLACED AND STIFF SO YOU HAVE TO PULL DOOR IN AND LATCH ON BOTH SIDES.. LUBRICATED ENGAGEMENT PINS, DOOR MECHANISM WORKS WITH NO DEFECTS NOTED AT THIS
- [SDR DXTA2022122176780](https://openairdocs.org/sdr/DXTA2022122176780.md): Battery Pack · inoperative · Dec 20, 2022 · N416QS · Emb EMB505 · Emergency Lighting
  > EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH IN ARM POSITION. REMOVED & REPLACED THE FWD NR 1 BATTERY PACK IAW AMM 33-52-00. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR DXTA2022050961520](https://openairdocs.org/sdr/DXTA2022050961520.md): Light · inoperative · May 8, 2022 · N416QS · Emb EMB505 · Emergency Lighting
  > EMERG EXIT SIGN/LIGHT: ENTRY DOOR LOWER SIDEWALL EMERGENCY EXIT LIGHT IS INOP. REMOVED LOWER EMERGENCY EXIT SIGN LIGHT AND INSTALLED CUSTOMER SUPPLIED "NEW" EXIT IDENTIFIER, OPS CHECK GOOD. ALL WORK DONE IAW AMM 33-52-13.
- [SDR 2021FA0000174](https://openairdocs.org/sdr/2021FA0000174.md): Battery Pack · failed · Jun 15, 2021 · N416QS · Emb EMB505 · Emergency Lighting
  > FORWARD EMERGENCY LIGHT BATTERY FAILED THE FUNCTIONAL TEST IN ACCORDANCE WITH PHENOM 300 AMM 33-52-01, BATTERY FAILED AT 15:35 SECONDS AT 20VDC. PASSING TIME IS 22 MIN AT 20VDC. PERFORMED REPLACEMENT #1 FORWARD EMERGENCY LIGHT BATTERY WITH A NEW BATTERY IN AC
- [SDR DXTA2020101204190](https://openairdocs.org/sdr/DXTA2020101204190.md): Rod · binding · Oct 10, 2020 · N416QS · Emb EMB505 · Passenger/Crew Doors
  > MAIN DOOR MAKES A LOUD "SNUBBING" SOUND UPON OPENING AND CLOSING. STOPS MOVEMENT IN 2 POSITIONS (SEE PHOTOS). CAN BE FORCED OPEN/CLOSED IF YOU MOVE IT HARD ENOUGH AND START THE MOTION OUT FAST, BUT DEFINITELY STRONGER THAN NORMAL FORCES ARE NEEDED AND FROM T
- [SDR DXTA202001133337](https://openairdocs.org/sdr/DXTA202001133337.md): Warning Message · false activation · Jan 13, 2020 · N416QS · Emb EMB505 · Central Warning
  > FLAP FAIL YELLOW CAS ILLUMINATED - WHILE DESCENDING THROUGH FL270 CAS CAUTION ILLUMINATED YELLOW "SWPS FAULT","FLAP FAIL","PTRIM BKP FAIL" AND A WHITE "SPOILER FAULT". THE AUTO PILOT WAS UNAVAILABLE AS WAS EXPECTED. PRIMARY TRIM WAS WORKING, WITH NO TRIM INDIC

## 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 = 'N416QS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N416QS/reports

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