# Service difficulty reports: Embraer Executive EMB-505

A list on [Embraer Executive EMB-505](https://openairdocs.org/model/embraer-executive-emb-505.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 39 · 1,936 reports

- [SDR 2026FA0000883](https://openairdocs.org/sdr/2026FA0000883.md): Bracket · cracked · Oct 21, 2026 · N5A · Emb EMB505 · Fuselage Miscellaneous Structure
  > WE HAVE FOUND CRACKED BRACKETS ON BOTH SIDES OF THE NOSE CENTER UPPER CHANNEL WHERE IT ATTACHES TO FRAME 1 DURING THE 60 MONTH INSPECTIONS. THE BRACKETS ARE CRACKED THE SAME WAY ON BOTH SIDES.
- [SDR 2026FA0000881](https://openairdocs.org/sdr/2026FA0000881.md): Bracket · cracked · Oct 21, 2026 · N92WL · Emb EMB505 · Fuselage Miscellaneous Structure
  > FOUND CRACKED BRACKETS ON BOTH SIDES OF THE NOSE CENTER UPPER CHANNEL WHERE IT ATTACHES TO FRAME 1, FOUND DURING THE 60 MONTH INSPECTIONS. THE BRACKETS ARE CRACKED THE SAME WAY ON BOTH SIDES.
- [SDR DXTA2026101910225](https://openairdocs.org/sdr/DXTA2026101910225.md): Elec Connector · pinched · Oct 17, 2026 · N487QS · Emb EMB505 · Door System Wiring
  > CLIMBING THROUGH FL250 WE GOT DOOR PAX OPEN CAS. RAN QRH AND DIVERTED BACK TO DEPARTURE AIRPORT. NO ABNORMAL PRESSURIZATION INDICATIONS. DURING TROUBLESHOOTING OF THE MICROSWITCH, THE PLANE WAS PRESSURIZED AND THE UPPER FWD MICROSWITCH CONNECTOR WAS FOUND
- [SDR DXTA2026101910206](https://openairdocs.org/sdr/DXTA2026101910206.md): Light · inoperative · Oct 16, 2026 · N438QS · Emb EMB505 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ADJACENT TO MAIN ENTRY STAIRWELL INOP. REMOVED SUSPECTED FAULTY EMERGENCY EXIT LIGHT ASSEMBLY AND INSTALLED NEW EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECKS GOOD NO RELATED DEFECTS NOTED AT THIS TIME ALL WORK PERFORMED I.A.W. AMM 33-52-13-
- [SDR DXTA2026101910207](https://openairdocs.org/sdr/DXTA2026101910207.md): Engine · failed · Oct 16, 2026 · N492QS · Emb EMB505 · Engine (Turbine/Turboprop)
  > ON APP FOR RUNWAY 27L INTO PHL, RECEIVED A CAS MSG WITH E1 FUEL FEED FAULT. THEN FOLLOWED WITH E1 FAIL. LOST THE LEFT ENGINE ON THE APPROACH RAN QRC AND LANDED UNEVENTFULLY. ONCE LANDED, SMELLED SMOKE, PERFORMED EVACUATION IAW QRC. CREW AND PAX ARE SAFE. CA
- [SDR DXTA2026101910218](https://openairdocs.org/sdr/DXTA2026101910218.md): Brake Assy · weak · Oct 16, 2026 · N331QS · Emb EMB505 · Landing Gear Brake System
  > BRAKES NOTICEABLY LESS RESPONSIVE AS NORMAL. FELT VERY SPONGEY AND WEAK BRAKE ACTION. UPON ARRIVAL TO AIRCRAFT, INSPECTED LT & RT MLG BRAKE ASSEMBLIES AND NOTED NO DISCREPANCIES, VERIFIED HYDRAULIC RESERVIOR WAS SERVICED TO WITHIN LIMITS. PERFORMED CMC / DOW
- [SDR DXTA2026101610183](https://openairdocs.org/sdr/DXTA2026101610183.md): Brake · vibration · Oct 14, 2026 · N433QS · Emb EMB505 · Landing Gear Brake System
  > DURING TAXI-OUT, APPLICATION OF THE RIGHT BRAKE CAUSED SEVERE, ERRATIC SHAKING AND VIBRATION THROUGHOUT THE AIRCRAFT. CONDITION WAS PARTICULARLY NOTICEABLE DURING RIGHT TURNS WHEN DIFFERENTIAL BRAKING WAS APPLIED TO ASSIST WITH TURNING. SHAKING WAS ABRUPT AND
- [SDR DXTA2026101610157](https://openairdocs.org/sdr/DXTA2026101610157.md): Control Module · faulted · Oct 12, 2026 · N330QS · Emb EMB505 · Landing Gear Brake System
  > RECEIVED BRAKE FAIL CAS MESSAGE ON FINAL INTO KAPF, EXECUTED GO AROUND, RAN QRH AND DIVERTED TO KRSW. LANDED SAFELY AND UTILIZED EMERGENCY BRAKE TO STOP AIRCRAFT ON RUNWAY. FBO TOWED AIRCRAFT INTO PARKING. REMOVED FAILED BRAKE CONTROL MODULE AND INSTALLED I
- [SDR DXTA2026101410165](https://openairdocs.org/sdr/DXTA2026101410165.md): Battery Pack · defective · Oct 12, 2026 · N333QS · Emb EMB505 · Emergency Lighting
  > IN CRUISE FLIGHT WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION THE EMER LIGHTS WERE ON IN THE CABIN. ON LANDING THE EMERGENCY LIGHTS BEGAN TO FLASH. REPLACED BATTERIES. OPS CHECK GOOD. IAW AMM 33-52-01.
- [SDR DXTA2026101510131](https://openairdocs.org/sdr/DXTA2026101510131.md): Wire Harness · defective · Oct 11, 2026 · N404QS · Emb EMB505 · Landing Gear System Wiring
  > ANTI-SKID FAIL CAS ILLUMINATED DURING GEAR EXTENSION ON APPROACH INTO LAS. CHECKLIST WAS COMPLETED AND LANDING WAS UNEVENTFUL, WITH SLOW, LIGHT BRAKE APPLICATION UNTIL ABOUT 100 YARDS BEFORE OUR EXIT TAXIWAY WHEN THE TIRE BLEW. I TAXIED THE AIRCRAFT VERY SLOWL
- [SDR DXTA2026101210105](https://openairdocs.org/sdr/DXTA2026101210105.md): Priority Valve · defective · Oct 9, 2026 · N484QS · Emb EMB505 · Landing Gear Retraction/Extension System
  > REPEAT WRITE UP. ON APPROACH WE SELECTED LANDING GEAR DOWN AND A LOUD BANG NOISE HEARD & FELT FROM NLG. THE MLG INDICATORS TURNED GREEN WHILE NLG INDICATOR REMAINED YELLOW FOR A PERIOD LONGER THAN USUAL. EVENTUALLY IT TURNED GREEN. ABORTED APPROACH & EXECUTED
- [SDR DXTA2026101210101](https://openairdocs.org/sdr/DXTA2026101210101.md): Priority Valve · defective · Oct 9, 2026 · N413QS · Emb EMB505 · Landing Gear Retraction/Extension System
  > REPEAT WRITE UP. ON APPROACH SELECTED MLG DOWN & A LOUD BANG HEARD & FELT FROM THE NLG. MLG INDICATORS TURNED GREEN WHILE NLG INDICATOR REMAINED YELLOW FOR A PERIOD LONGER THAN USUAL. EVENTUALLY IT TURNED GREEN. ABORTED APPROACH & EXECUTED A GO AROUND & SEL
- [SDR DXTA2026101210086](https://openairdocs.org/sdr/DXTA2026101210086.md): Brake · locked · Oct 8, 2026 · N491QS · Emb EMB505 · Landing Gear Brake System
  > UPON LANDING AND TAXI-IN THE RIGHT BRAKE IS CATCHING AND FEELS LIKE THE RIGHT TIRE IS LOCKED. NO FAULTS FOUND. OPS CHECK GOOD. IAW AMM MPP 09-20-01-500-801-A
- [SDR DXTA2026100910075](https://openairdocs.org/sdr/DXTA2026100910075.md): Wire · shorted · Oct 6, 2026 · N492QS · Emb EMB505 · Pneumatic System Wiring
  > DURING CRUISE AT FL400, AMBER BLEED 2 LEAK CAS MSG ILLUMINATED. ACCOMPLISHED INITIAL PORTION OF QRH TO ISOLATE THE FAULTY SYS & CAS MSG EXTINGUISHED. SHORTLY, CAS MSG FLICKERED ON & OFF A COUPLE OF TIMES, DIVERTED & ACCOMP REST OF QRH SHORT OF SHUTTING NR 2
- [SDR DXTA2026100810063](https://openairdocs.org/sdr/DXTA2026100810063.md): Brake Assy · worn · Oct 6, 2026 · N442QS · Emb EMB505 · Landing Gear Brake System
  > DURING TAXI WHEN APPLYING BRAKES STUTTERING & GRINDING COULD BE FELT. AS SPEED DECREASED STUTTERING BECAME MORE PRONOUNCED. TAXIED BACK TO RAMP STUTTERING & GRINDING CONTINUED. PARKED & SPEED DECREASED STUTTERING BECAME MORE PRONOUNCED. THIS COULD BE FELT IN B
- [SDR DXTA2026100810064](https://openairdocs.org/sdr/DXTA2026100810064.md): Battery · faulty · Oct 6, 2026 · N475QS · Emb EMB505 · Emergency Lighting
  > DURING PRE FLIGHT, THE EMERGENCY LIGHTS WERE TESTED. THE LIGHTS REMAINED ON IN THE ARM POSITION. VERIFIED EMER LIGHTS STAY ON WITH EMER LT SWITCH IN ARM POSITION. AFTER TROUBLSHOOTING FOUND AFT EMERGENCY BATTERY IS INOP. REMOVED AFT EMERGENCY BATTERY PN#7450
- [SDR 2026F00221](https://openairdocs.org/sdr/2026F00221.md): Support Bracket · cracked · Oct 6, 2026 · N346AS · Emb EMB505 · Fuselage Miscellaneous Structure
  > FOUND CRACKS ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKET.
- [SDR 2026FA0000816](https://openairdocs.org/sdr/2026FA0000816.md): Receptacle · melted · Oct 6, 2026 · N337AS · Emb EMB505 · Electrical Power System
  > GPU PLUG CAUGHT ON FIRE WHILE PLUGGED INTO THE AIRCRAFT. GPU WAS SHUT DOWN AND CABIN PORTABLE FIRE EXTINGUISHER WAS USED TO EXTINGUISH THE FIRE.
- [SDR 2026F00222](https://openairdocs.org/sdr/2026F00222.md): Support Bracket · cracked · Oct 6, 2026 · N362AS · Emb EMB505 · Fuselage Miscellaneous Structure
  > FOUND CRACKS ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKET
- [SDR CVGA20261003001](https://openairdocs.org/sdr/CVGA20261003001.md): Warning Message · false activation · Oct 3, 2026 · N655UP · Emb EMB505 · Central Warning
  > BLEED 1 AND BLEED 2 FAIL ON CLIMBOUT ( EMERGENCY DECLARED) PERFORMED OPS CHECK IAW AMM 36-00-00-710-801-A. OPS CHECK GOOD AT THIS TIME. REF SL 505-36-0003 AND EMB CASE # EEJ-55-1008, DEEMED TRANSITORY CONDITION. AIRCRAFT GOOD FOR SERVICE.
- [SDR DXTA2026100609998](https://openairdocs.org/sdr/DXTA2026100609998.md): Dcu · defective · Oct 2, 2026 · N452QS · Emb EMB505 · Auto Flight System
  > WHILE IN CRUISE AT FL410 WE REVIEWED MULTIPLE CAS MESSAGES AND AN AURAL AUTO PILOT. THE MESSAGES WERE AP FAIL, SWPS FAULT, YD FAIL, BLEED 2 OFF, STBY BARO NOCOMP, SWPS ICE SPEED, GSD 1 FAIL(HIGHLIGHTED), AND HSDB FAULT. IN ADDITION, THE LT MLG INDICATED TRANS
- [SDR DXTA2026100509999](https://openairdocs.org/sdr/DXTA2026100509999.md): Brake Assy · faulted · Oct 2, 2026 · N479QS · Emb EMB505 · Landing Gear Brake System
  > ON TAXI IN, NOTICED RT BRAKE CAUSES A NOTICEABLE SHUDDER AND SHAKES THE ENTIRE AIRCRAFT. ONLY RH BRAKE CAUSED IT, TESTED THEM INDEPENDENTLY AND ONLY FELT THE SHAKE,SHUDDER WHEN RT BRAKING WAS APPLIED. REMOVED FAULTY RT MLG BRAKE ASSEMBLY & INSTALLED A CUSTOME
- [SDR DXTA2026100509998](https://openairdocs.org/sdr/DXTA2026100509998.md): Multiple · malfunctioned · Oct 2, 2026 · N452QS · Emb EMB505 · Central Warning
  > WHILE IN CRUISE AT FL410 WE REVIEWED MULTIPLE CAS MESSAGES AND AN AURAL AUTO PILOT. THE MESSAGES WERE AP FAIL, SWPS FAULT, YD FAIL, BLEED 2 OFF, STBY BARO NOCOMP, SWPS ICE SPEED, GSD 1 FAIL (HIGHLIGHTED), AND HSDB FAULT. IN ADDITION, THE LT MLG INDICATED TRAN
- [SDR DXTA2026100509949](https://openairdocs.org/sdr/DXTA2026100509949.md): Control Module · faulted · Sep 30, 2026 · N374QS · Emb EMB505 · Landing Gear Brake System
  > GOT A BRK FAIL CAS MESSAGE WHILE TAXIING OUT. HAD TO APPLY MAX PEDAL PRESSURE TO GET ANY BRAKES AT ALL AND IT SEEMED AS IF THE LEFT BRAKE WOULD GRAB WHEN I FINALLY GOT ANY BRAKES. R & R RT WHEEL SPEED XDUCER IAW AMM 32-41-06. OPS CHKD GOOD. PERFORMED PEDAL
- [SDR J7SA2026100200526](https://openairdocs.org/sdr/J7SA2026100200526.md): Fce · unserviceable · Sep 28, 2026 · N308FX · Emb EMB505 · Flight Control System
  > REPEAT FLAP FAIL. REPLACED FCE #1 IAW EMB 505 AMM 27-03-01. OPS AND RIGGING CHECK GOOD.
- [SDR DXTA2026100109928](https://openairdocs.org/sdr/DXTA2026100109928.md): Module · defective · Sep 28, 2026 · N383QS · Emb EMB505 · Indicating/Recording System
  > DURING DESCENT, ENG 1 ANTI ICE FAILED, GEA 2 FAILED, ENG NO DISPATCH CAS ILLUMINATED. GTC SHOWED DATA PATH FAIL, NUMEROUS ENGINE, FLIGHT CONTROL AND LANDING GEAR INDICATIONS, FAILED: ROLL TRIM, YAW TRIM, NR 2 OIL PRESS, NR 2 OIL TEMP, NR 2 FUEL FLOW, NR 2
- [SDR DXTA2026092909904](https://openairdocs.org/sdr/DXTA2026092909904.md): Battery Pack · defective · Sep 26, 2026 · N412QS · Emb EMB505 · Emergency Lighting
  > WITH EMER LIGHTS SWITCH ON, EMERGENCY OVERHEARD LIGHTS FLICKER ON AND OFF, AS WELL AS EXIT SIGN, AND PATHWAY LIGHTS CORRECTIVE ACTION: T/S AND FOUND EMERGENCY BATTERIES DEPLETED. REMOVED AND REPLACED EMERGENCY BATTERIES WITH REPAIRED ASSEMBLIES AND OPERATIONAL
- [SDR DXTA2026092909885](https://openairdocs.org/sdr/DXTA2026092909885.md): Landing Gear · malfunctioned · Sep 25, 2026 · N407QS · Emb EMB505 · Landing Gear Position and Warning
  > ON TAKEOFF WE GOT A RED CAS LG LEVER DISAG. WE RAN THE CHECKLIST. EXTENDED THE GEAR. GOT NORMAL EXTENSION. THEN RETRACTED THE GEAR AND RECEIVED THE SAME CAS MESSAGE. ON RETRACTION, IT SEEMED TO MAKE A LOUDER CLUNK INTO THE NOSE WHEEL WELL THAN NORMAL. ON THE F
- [SDR DXTA2026092909888](https://openairdocs.org/sdr/DXTA2026092909888.md): Wire · shorted · Sep 25, 2026 · N325QS · Emb EMB505 · Landing Gear System Wiring
  > AFTER TAKEOFF, THE LANDING GEAR LEVER WAS SELECTED UP BUT NONE OF THE GEAR CAME UP. WE GOT THE LANDING GEAR SWITCH DISAGREE CAS AND THE QRH HAD US CYCLE THE HANDLE. UPON THE SECOND ATTEMPT TO RAISE THE LANDING GEAR, THE GEAR HANDLE PHYSICALLY WOULD NOT COME UP
- [SDR J7SA2026092900525](https://openairdocs.org/sdr/J7SA2026092900525.md): Spoiler Sys · faulted · Sep 25, 2026 · N363FX · Emb EMB505 · Drag Control System
  > SPOILERS AUTO RETRACTED AFTER DEPLOYMENT ON APPROACH. CREW RECEIVED GND SPLR FAIL, AND SPOILER FAULT CAS MESSAGES. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE #2 IAW EMB-505 AMM 27-03-01. RIGGING AND OPS CHECKS GOOD.
- [SDR J7SA2026092900524](https://openairdocs.org/sdr/J7SA2026092900524.md): Fce · malfunctioned · Sep 22, 2026 · N355FX · Emb EMB505 · Flight Control System
  > CREW REPORTS FCE1 CB POPS WITH BATTERIES ON. REPLACED FCE # 1 IAW EMB-505 CH 27-03-01. OPS CHECK GOOD.
- [SDR DXTA2026092409846](https://openairdocs.org/sdr/DXTA2026092409846.md): Brake Sys · faulted · Sep 22, 2026 · N463QS · Emb EMB505 · Landing Gear Brake System
  > DURING TAXI OUT FOR DEPARTURE, WE EXPERIENCE SOME BRIEF BRAKE CHATTER DURING OUR LAST TURN PRIOR TO THE RUNWAY. WHILE AWAITING TAKEOFF CLEARANCE, WE SET THE PARKING BRAKE AND RECEIVED AN AMBER BRK FAIL CAUTION. WE CALLED OPS AND MCC, THEN SHUT THE AIRCRAFT DOW
- [SDR DXTA2026092309847](https://openairdocs.org/sdr/DXTA2026092309847.md): Light · unsecure · Sep 22, 2026 · N468QS · Emb EMB505 · Emergency Lighting
  > CABIN INTERIOR LIGHT BY LOWER ENTRANCE OF COCKPIT (EMERGENCY LIGHT) RESECURED LOOSE HARDWARE. OPS CHECK GOOD. IAW EMB505 AMM 33-26-03
- [SDR DXTA2026092509835](https://openairdocs.org/sdr/DXTA2026092509835.md): Strut · discharged · Sep 21, 2026 · N402QS · Emb EMB505 · Main Landing Gear Strut/Axle/Truck
  > DURING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR INDICATED IN TRANSIT AND NEVER FULLY RETRACTED. LG LEVER DISAG CAS MESSAGE DISPLAYED. HYDRAULIC PRESSURE WAS NORMAL. ALL GEAR EXTENDED NORMALLY WHEN SELECTED DN. SERVICED NLG STRUT. OPS CHECK GOOD. IAW PHENO
- [SDR DXTA2026092409817](https://openairdocs.org/sdr/DXTA2026092409817.md): Warning Message · illuminated · Sep 20, 2026 · N310QS · Emb EMB505 · Landing Gear Position and Warning
  > ON TAKEOFF FROM KSLK, DURING MLG RETRACT, THE MLG LEVER DISAG RED CASS ILLUM, ALONG WITH THE RED & WHITE HASHMARK IND OVER NLG. PREFORMED QRH & RECYCLED GEAR. THE CASS CLEARED & GEAR IND UP. CONTACTED THE FODM AND CONTINUED TO OUR DESTINATION AND LANDED NORMAL
- [SDR DXTA2026092309808](https://openairdocs.org/sdr/DXTA2026092309808.md): Battery · defective · Sep 20, 2026 · N453QS · Emb EMB505 · Emergency Lighting
  > WHILE ESTABLISHED IN CRUISE AT 41,000 FT, THE CABIN ENERGENCY LIGHTS ILLUMINATED. AFTER THEY TIMED OUT, THEY ILLUMINATED AGAIN. THIS PROCESS REPEATED THROUGHOUT THE FLIGHT. CORRECTIVE ACTION: REPLACED BATTERIES. OPS CHECK GOOD. IAW EMB505 MM 33-52-01
- [SDR JGVR20260918002](https://openairdocs.org/sdr/JGVR20260918002.md): Skin · corroded · Sep 18, 2026 · N318QS · Emb EMB505 · Passenger/Crew Doors
  > R & R THE CENTER HINGE COVER AND BLENDED MULTIPLE AREAS OF CORROSION ON THE MAIN ENTRY DOOR OUTER SKIN, NEAR THE CENTER HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED PER TECHNICAL DISPOSITION.
- [SDR JGVR20260918001](https://openairdocs.org/sdr/JGVR20260918001.md): Door Frame · corroded · Sep 18, 2026 · N318QS · Emb EMB505 · Fuselage Main, Structure
  > REMOVED MULTIPLE AREAS OF CORROSION ON THE MAIN ENTRY DOOR INNER FRAME, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED BLENDED AREAS PER TECHNICAL DISPOSITION.
- [SDR DXTA2026092109759](https://openairdocs.org/sdr/DXTA2026092109759.md): Battery Pack · defective · Sep 17, 2026 · N310QS · Emb EMB505 · Emergency Lighting
  > EMER LIGHTS STAYING ON WITH EMER LT SWITCH IN ARM POSITION. CORRECTIVE ACTION: REPLACED BATTERY PACK. OPS CHECK GOOD. IAW PHENOM 300 AMM 33-52-01-400-801-A
- [SDR DXTA2026092109742](https://openairdocs.org/sdr/DXTA2026092109742.md): Relief Valve · defective · Sep 16, 2026 · N328QS · Emb EMB505 · Landing Gear Brake System
  > DURING CRUISE RECEIVED AN EMER BRK LOW PRESSURE CAS. PRESSURE WAS APPROXIMATLEY 150PSI AND CONTINUED TO DROP. SOMETIME BETWEEN TOUCHDOWN AND ENGINE SHUTDOWN PRESSURE CAME BACK UP TO 2900 THEN DROPPED TO 2400PSI WITHIN 10 MINUTES. TWO MORNINGS IN A ROW AIRCRAFT
- [SDR DXTA2026092109748](https://openairdocs.org/sdr/DXTA2026092109748.md): Brake Sys · malfunctioned · Sep 16, 2026 · N444QS · Emb EMB505 · Landing Gear Brake System
  > DURING TAXI IN RIGHT BRAKE HAD UNCOMMANDED ACTIVATION. WHEN RIGHT BRAKE PEDAL PRESSED THE THE BRAKES FELT LIKE THEY WERE SLIPPING CAUSING THE ENTIRE PLANE TO SHAKE. LEFT BRAKE PEDAL SIMILAR CONDITION BUT LESS PRONOUNCED. PERFORMED BRAKE CHECK. NO FAULTS FOUND
- [SDR DXTA2026091709744](https://openairdocs.org/sdr/DXTA2026091709744.md): Flap System · fault message · Sep 16, 2026 · N443QS · Emb EMB505 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAIL CAS WHEN SELECTING FLAPS 2 WHILE ON APPROACH TO WST. PERFORMED FLAP FAIL QRC WITH NO SUCCESS IN CLEARING FLAP FAIL. DIVERTED TO BDL AND LANDED ACCORDING TO QRC GUIDANCE. UNEVENTFUL LANDING. FLAPS REMAINED STUCK BETWEEN POSITION 1 & 2. SENT C
- [SDR CVGA20260921004](https://openairdocs.org/sdr/CVGA20260921004.md): Uplock Box · failed · Sep 15, 2026 · N670UP · Emb EMB505 · Landing Gear Position and Warning
  > WE DID NOT GET A DOWN AND LOCKED NOSE GEAR INDICATIONWHEN MOVING THE GEAR HANDLE TO THE DOWN POSITION. FOLLOWING THE QRH, WE USED THE EMERGENCY GEAR DOWN HANDLE AND IT CAME DOWN ( EMERGENCY DECLARED) REMOVED NLG UPLOCK BOX AND PROX SWITCH, INSTALLED SERVICEA
- [SDR CVGA20260917002](https://openairdocs.org/sdr/CVGA20260917002.md): Selector · failed · Sep 14, 2026 · N668UP · Emb EMB505 · Trailing Edge Flap Control System
  > FLAP FAILURE ON TAKEOFF, FLAPS STUCK AT FLAPS 1- THIRD OCCURENCE, WILL DOWNLOAD CMC ( EMERGENCY DECLARED) DOWNLOADED CMC FAULT CODES AND AFTER TROUBLESHOOTING DETERMINED FLAP SELECTOR NEEDS REPLACEMENT. REMOVED FLAP SELECTOR LEVER UNIT, INSTALLED SERVICEABEL
- [SDR CVGA20260917003](https://openairdocs.org/sdr/CVGA20260917003.md): Gcu · failed · Sep 13, 2026 · N897JH · Emb EMB505 · DC Generating System
  > RECEIVED A BATT EXCEEDANCE CAS MESSAGE DURING CLIMB, MOMENTARARY A FEW TIMES, THEN STEADY. GENERATOR AND BATTERY 1 VOLTAGE 28.6 +-0.2, GENERATOR AND BATTERY 2 VOLTAGE 29.0 ( EMERGENCY DECLARED) REMOVED AND REPLACED NR 2 GCU WITH AN INSPECTED GCU IAW AMM 24-31
- [SDR DXTA2026091509690](https://openairdocs.org/sdr/DXTA2026091509690.md): Sealant · misinstalled · Sep 13, 2026 · N444QS · Emb EMB505 · Aerodynamic Fairings
  > DURING DESCENT FROM AROUND FL200 A LOW LOUD HUM STARTED. WE WERE AROUND 295-300KTS VIBRATION FELT IN FEET FROM LEFT AND RIGHT PILOT. WORSE VIBRATION FELT FROM THE FLOOR INLINE WITH THE MAIN CABIN DOOR. VIBRATION AND SOUND STOPPED AT 11,000FT IN LEVEL OFF AFTER
- [SDR J7SA2026092900523](https://openairdocs.org/sdr/J7SA2026092900523.md): Fce · malfunctioned · Sep 12, 2026 · N391FX · Emb EMB505 · Flight Control System
  > CREW RECEIVED GND SPOILER FAIL ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT CRE. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. OPS CHECKS GOOD.
- [SDR DXTA2026091509684](https://openairdocs.org/sdr/DXTA2026091509684.md): Battery · inoperative · Sep 12, 2026 · N439QS · Emb EMB505 · Emergency Lighting
  > EMERGENCY LIGHTS ARE REMAINING ILLUMINATED WITH SWITCH IN THE ARM POSITION. CONFIRMED. TROUBLESHOT IAW FIM 33-50-00-810-801-A. REMOVED CREW SEATS IAW AMM 25-11-01 FOR ACCESS. REMOVED FLOOR PANEL 223CLF FOR ACCESS TO NR 1 BATTERY. REMOVED LAV PANEL242AZ TO ACCE
- [SDR J7SA2026092900522](https://openairdocs.org/sdr/J7SA2026092900522.md): Fce · unserviceable · Sep 11, 2026 · N375FX · Emb EMB505 · Flight Control System
  > AFTER ENGINE START "SWPS FAULT", "GND SPLR FAIL", "PTRIM NML FAIL", "SPOILER FAULT" CAS MESSAGES ILLUMINATED. CAS MESSAGES WOULD NOT CLEAR AFTER SHUTDOWN AND POWER RESETS. REPLACED # 2 FCE IAW EMB-505 300 AMM 27-03-01.
- [SDR DXTA2026091409664](https://openairdocs.org/sdr/DXTA2026091409664.md): Brake · abnormal · Sep 11, 2026 · N431QS · Emb EMB505 · Landing Gear Brake System
  > RIGHT MLG BRAKE: RIGHT BRAKE PULSATES NOTICEABLY AT ALL SPEEDS (MOST NOTICEABLE AT TAXI SPEED) WHEN BRAKE PEDAL PRESSURE APPLIED. DURING TAXI BRAKE APPLICATION, THE BRAKES CONSTANTLY GRABBED AND RELEASED. THIS PROCEEDED TO GET WORSE AS AIRCRAFT SLOW SPEED CAUS

Next page: https://openairdocs.org/model/embraer-executive-emb-505/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 aircraft_model_key = 'EMB505'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-executive-emb-505/reports

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