# Service difficulty reports: N75

A list on [N75](https://openairdocs.org/aircraft/N75.md).

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

- [SDR RU3A2021052100011](https://openairdocs.org/sdr/RU3A2021052100011.md): Actuator · faulted · Jun 14, 2021 · N75 · Beech 300BEECH · Landing Gear Actuator
  > JUST OUTSIDE FAF ON ILS 27L TO KPHL, WE COMPLETED A BEFORE LANDING CHECK. OBSERVED THE RIGHT MAIN LANDING GEAR WAS NOT DOWN AND LOCKED, AND THAT THE GEAR HANDLE RED LIGHT WAS ILLUMINATED. NOSE GEAR AND LEFT MAIN LANDING GEAR HAD GREEN CAPSULE LIGHTS ILLUMINAT
- [SDR RU3A2020080500029](https://openairdocs.org/sdr/RU3A2020080500029.md): Unknown · odor · Aug 5, 2020 · N75 · Beech 300BEECH · Air Distribution System
  > UNKNOWN ELECTRICAL ODOR SPREAD FROM CABIN TO COCKPIT.
- [SDR RU3A201908197040](https://openairdocs.org/sdr/RU3A201908197040.md): Proximity Switch · failed · Aug 16, 2019 · N75 · Beech 300BEECH · Propeller Indication System
  > RT PROP PITCH LIGHT FAST FLICKERS AND COMES ON BEFORE LEFT. FLICKERS ON SHUTDOWN AS WELL. R/H ENGINE PROXIMITY SWITCH WAS FOUND TO HAVE FAILED. REPLACED SWITCH. NO FURTHER ACTION REQUIRED.
- [SDR RU3A20181102100](https://openairdocs.org/sdr/RU3A20181102100.md): Wire · disconnected · Nov 2, 2018 · N75 · Beech 300BEECH · Landing Gear System Wiring
  > FLIGHT CREW UNABLE TO EXTEND THE GEAR. THE GEAR WAS MANUALLY PUMPED DOWN. THREE GREEN LANDING LIGHTS INDICATED AFTER MANUAL EXTENSION. WIRE P221C14 DISCOVERED DISCONNECTED FROM CIRCUIT BREAKER CB107. CONNECTED THE WIRE, SUCCESSFULLY OPS-CHECKED WITH 5 N
- [SDR RU3A20180228006](https://openairdocs.org/sdr/RU3A20180228006.md): Not Reported · malfunctioned · Feb 28, 2018 · N75 · Beech 300BEECH · Trailing Edge Flap Control System
  > FLAPS DID NOT MOVE WHEN COMMANDED TO FLAP APPROACH.
- [SDR RU3A20180222005](https://openairdocs.org/sdr/RU3A20180222005.md): Relay · failed · Feb 22, 2018 · N75 · Beech 300BEECH · Trailing Edge Flap Control System
  > FLAPS FAILED TO EXTEND FOR LANDING. FLAP POWER BRAKE RELAY FOUND TO BE SOURCE OF PROBLEM. FLAPS OPERATED NORMALLY AFTER RELAY REPLACEMENT. NO FURTHER ACTION IS REQUIRED.
- [SDR RU3A20171221050](https://openairdocs.org/sdr/RU3A20171221050.md): Hook · out of tolerance · Dec 21, 2017 · N75 · Beech 300BEECH · Door Warning System
  > CABIN DOOR WARNING LIGHT ILLUMINATED AT 5000 FT. AFTER EMERGENCY CHECKLIST ITEMS COMPLETED, EXTINGUISHED AT APPROXIMATELY 1000 FT ON FINAL APPROACH. FOUND FORWARD J-HOOK WAS FOUND TO BE TIGHT. J-HOOKS RE-RIGGED. OPERATIONAL CHECK OF DOOR WAS GOOD. NO FURTHER
- [SDR RU3A20150505011](https://openairdocs.org/sdr/RU3A20150505011.md): Tube · loose · May 5, 2015 · N75 · Beech 300BEECH · Pneumatic Distribution System
  > RIGHT BLEED AIR FAIL LIGHT ILLUMINATED IN FLIGHT. EVA TUBING COMING LOOSE, CONNECTED SUPPLY LINE AT DISTRIBUTION MANIFOLD & REPLACED CLAMP.
- [SDR RU3A20150302010](https://openairdocs.org/sdr/RU3A20150302010.md): Tube · damaged · Feb 25, 2015 · N75 · Beech 300BEECH · APU Bleed Air System
  > LEFT BLEED AIR FAIL ILLUMINATED. REPAIRED HOLE IN EVA TUBING.
- [SDR RU3A20141112040](https://openairdocs.org/sdr/RU3A20141112040.md): Solenoid · dirty · Oct 30, 2014 · N75 · Beech 300BEECH · Propeller Controlling System
  > WITH FLAPS IN APPROACH MODE, ACFT EXPERIENCED SLIGHT YAW TO THE RT. AS POWER WAS FURTHER REDUCED FOR LANDING, THE YAW INCREASED. PILOT WAS UNABLE TO CORRECT WITH RUDDER & AILERON. AFTER GO AROUND AT SAFE ALTITUDE, FLIGHT CREW ATTEMPTED TO DUPLICATE THE PROB
- [SDR RU3A20140204003](https://openairdocs.org/sdr/RU3A20140204003.md): Light · inoperative · Feb 4, 2014 · N75 · Beech 300BEECH · Landing Gear Position and Warning
  > LEFT & RT MLG LIMITS DID NOT ILLUMINATE WITH GEAR SELECTED DOWN. PRESS TO TEST GEAR MODULE, CONFIRMED LT & RT MLG LIGHTS INOPERATIVE.
- [SDR RU3A20121212003](https://openairdocs.org/sdr/RU3A20121212003.md): Warning System · activated · Dec 12, 2012 · N75 · Beech 300BEECH · Pneumatic Indicating System
  > RIGHT BLEED AIR ANNUNCIATOR ILLUMINATED IN FLIGHT. CREW ACCOMPLISHED BLEED AIR FAIL EMERGENCY CHECKLIST. UNEVENTFUL LANDING FOLLOWED.
- [SDR RU3A1116](https://openairdocs.org/sdr/RU3A1116.md): Adapter · misaligned · Jun 30, 2011 · N75 · Beech 300BEECH · Autopilot Main Servo
  > DURING INSPECTION FOUND RUDDER SERVO BRIDAL TOP CABLE MISALIGNED COMING OFF RUDDER SERVO CAPSTAN PULLEY. THIS PROLONGED CONDITION WILL CAUSE THE PULLEY AND CABLE TO WEAR PREMATURELY. PRELIMINARY EO IS IN DRAFT PROVIDING INSTRUCTIONS FOR REMOVING EXISTING SERV
- [SDR RU3A1106](https://openairdocs.org/sdr/RU3A1106.md): Trim Tab · detached · Feb 3, 2011 · N75 · Beech 300BEECH · Aileron Tabs
  > LEFT AILERON TRIM TAB PARTIALLY DETACHED ABOUT ONE HOUR INTO FLIGHT ACCOMPANIED BY INTERMITTENT AILERON MISTRIM (YELLOW) ANNUNCIATION.
- [SDR RU3A1104](https://openairdocs.org/sdr/RU3A1104.md): Tube · damaged · Jan 28, 2011 · N75 · Beech 300BEECH · Pneumatic Distribution System
  > LEFT BLEED AIR FAIL LIGHT ILLUMINATED 4-5 MINUTES AFTER TAKEOFF. THE IMMEDIATE ACTION STEP WAS TAKEN TO TURN THE LEFT BLEED AIR OFF. THE AFM EMERGENCY CHECKLIST WAS REFERENCED. INSTRUMENT AND VISUAL INDICATION OF THE LEFT ENGINE WERE NORMAL. SUBSEQUENT APP
- [SDR RU3A0903](https://openairdocs.org/sdr/RU3A0903.md): Cap · loose · Feb 9, 2009 · N75 · Beech 300BEECH · Hydraulic Reservoir, Main
  > DURING CLIMB TO 14000FT, HYD LOW LIGHT ILLUMINATED. CREW MADE A TURNBACK TO BASE, AFTER INFORMING ATC. ABOUT 3 MINUTES AFTER THE TURN THE WARNING LT EXTINGUISHED. CREW BACKED UP SITUATION WITH THE ABNORMAL CHECKLIST. ON EXTENDED FINAL, USING THE BEFORE LAN
- [SDR RU3A0705](https://openairdocs.org/sdr/RU3A0705.md): Motor · failed · Jul 2, 2007 · N75 · Beech 300BEECH · Cabin Cooling System
  > WHILE OUTBOUND IN A "FLIGHT INSPECTION HOLDING PATTERN" THE MISSION SPECIALIST REPORTED SOMETHING WAS ON FIRE IN THE REAR CABIN, BOTH PILOTS VISUALLY CONFIRMED SMOKE IN THE AFT CABIN AREA. DECLARED AN EMERGENCY WITH INTENTION TO LAND AT WILEY POST, CREW DONNE
- [SDR 2004F00058](https://openairdocs.org/sdr/2004F00058.md): Actuator · inoperative · Jan 15, 2004 · N75 · Beech 300BEECH · Landing Gear Actuator
  > NO NOSE WHEEL GEAR GREEN LIGHT INDICATION WAS OBSERVED WHEN LANDING GEAR WAS EXTENDED. GEAR WAS CYCLED WITH SAME RESULTS, BUT 'RED' GEAR HANDLE LIGHT ILLUMINATED. A/C RETURNED TO BASE. UPON ARRIVAL, GEAR WAS EXTENDED WITH ALL PROPER INDICATIONS, THREE GREEN
- [SDR RU3A99005](https://openairdocs.org/sdr/RU3A99005.md): Retract Mech · malfunctioned · Jun 2, 1999 · N75 · Beech 300BEECH · Landing Gear Retraction/Extension System
  > OKC - LANDING GEAR FAILED TO EXTEND NORMALLY ON APPROACH TO LANDING AND EMERGENCY EXTENSION PROCEDURE SUCCESSFULLY EMPLOYED. (M)
- [SDR RU3A97006](https://openairdocs.org/sdr/RU3A97006.md): Power Supply · failed · Aug 14, 1997 · N75 · Beech 300BEECH · Dependent Position Determining System
  > STRONG ELECTRICAL SMELL, SMOKE IN REAR OF CABIN. CONTROL DISPLAY UNIT FAILED AND TECHNICAN PANEL FAILED. REQUESTED PRIORITY HANDLING. CLEARED TO LAND. SHORTED POWER SUPPLY IN THE NAVIGATIONAL COMPUTER UNIT WAS THE SOURCE OF SMELL AND SMOKE. NCU REPLACED A

## 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 = 'N75' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N75/reports

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