# Brumit John C JR GALAXY - Type: Aircraft model (FAA registry) - Registry code: 05614UQ - Manufacturer (registry): BRUMIT JOHN C JR - Model: GALAXY - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 ยท Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/brumit-john-c-jr-galaxy Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N2406X](https://openairdocs.org/aircraft/N2406X): [Brumit John E Jr](https://openairdocs.org/faa-owner/BRUMIT%20JOHN%20E%20JR), [Odessa, TX](https://openairdocs.org/faa-place/TX/Odessa), built 2003, S/N 01 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (90, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000741](https://openairdocs.org/sdr/2026FA0000741), Sep 17, 2026: WINDSHIELD. SMOKE. SMOKE WAS OBSERVED EMITTING FROM THE LOWER SECTION OF THE R/H WINDSHIELD IN THE AREA OF THE HEATING ELEMENT. THE CREW TURNED OFF THE WINDSHIELD HEAT, AT WHICH T - [SDR 2026FA0000402](https://openairdocs.org/sdr/2026FA0000402), May 18, 2026: CARBON SEAL. LEAKING. DURING DEPARTURE THE CREW NOTICED SMOKE IN THE CABIN. NOTIFIED TOWER AND RETURNED TO ICT. STANDARDAERO BORESCOPED THE ENGINE AND FOUND THE #5 CARBON SEAL LEAKIN - [SDR 2026FA0000284](https://openairdocs.org/sdr/2026FA0000284), Apr 22, 2026: CARBON SEAL. LEAKING. DURING TAKE OFF FOR A SCHEDULED TEST FLIGHT REQUIRED FOR THE REINSTALLATION OF THE #1 ENGINE. IT WAS NOTICED THERE WAS SMOKE COMING IN THE CABIN AND COCKPIT GAS - [SDR 2025F00275](https://openairdocs.org/sdr/2025F00275), Nov 25, 2025: WINDSHIELD. CRACKED. KVNY TO MMSD. ONE HOUR INTO FLIGHT, RIGHT WINDSHIELD EXTERNAL LAYER CRACKED AT 39,000 FT. CREWS DECLARED PAN PAN PAN AND FOLLOWED QRH. FLIGHT RETURNED TO KVNY A - [SDR 2025FA0000753](https://openairdocs.org/sdr/2025FA0000753), Oct 23, 2025: WINDOW. CRACKED. PILOT REPORTED THEY DEPARTED KSNA AT 1501Z ON 10/23/2025. DESTINATION WAS KADS. WEATHER WAS NOT A FACTOR. FLIGHT WAS UNEVENTFUL UNTIL INITIAL CLIMB. APPROXIMATE - [SDR 2021FA0000195](https://openairdocs.org/sdr/2021FA0000195), Jul 3, 2021: ANTI-SKID SYS. FAILED. ON LANDING IN KASE THE ANTI-SKID SYSTEM FAILED AFTER 3-4 SECOUNDS. ANTI-SKID WAS RESET AND UPON RESET ALL TIRES BLEW AT THE SAME TIME AND LOSS BREAKING. - [SDR 2022FA0000019](https://openairdocs.org/sdr/2022FA0000019), May 20, 2021: NONE. CORRODED. SKIN CORROSION FOUND UNDER ANTENNAS ON AIRCRAFT BELLY - [SDR CWQA201906040001](https://openairdocs.org/sdr/CWQA201906040001), May 31, 2019: SMOKE DETECTOR. FALSE ACTIVATION. DURING CRUISE, CREW RECEIVED BAGGAGE SMOKE EICAS MESSAGE. CHECK LIST FOLLOWED, DESCENDED QUICKLY, EMERGENCY DECLARED, AND UNSCHEDULED LANDING PERFORMED WITHOUT - [SDR CA190329022](https://openairdocs.org/sdr/CA190329022), Mar 15, 2019: REGULATOR VALVE. FAILED. (CAN) CREW REPORTED ENGINE ROLLED BACK DURING FLIGHT AT ABOUT 33000FT. DURING TROUBLESHOOTING THE PRESSURE REGULATING SHUT-OFF VALVE WAS REPLACED AND THE AIRCRA - [SDR K5SR2016T27895](https://openairdocs.org/sdr/K5SR2016T27895), Dec 6, 2016: STARTER GEN. MALFUNCTIONED. DURING NR 2 ENGINE START, THE STARTER GENERATOR AUTOMATIC CUTOUT FEATURE WHICH IS TO OCCUR AT 60 PERCENT N2 DID WORK. PILOT HAD TO MANUALLY DE-SELECT STARTER GE - [SDR W6JA20160914009](https://openairdocs.org/sdr/W6JA20160914009), Sep 8, 2016: FUEL DOOR. DEPARTED. AIRCRAFT RECEIVED FUEL, CREW THEN TAXIED AIRCRAFT TO ACTIVE RUNWAY TO WAIT APPROXIMATELY 15 MINUTES. AT NO POINT DURING THEIR WAIT DID THE REFUEL DOOR ILLUMINAT - [SDR W6JA20160802008](https://openairdocs.org/sdr/W6JA20160802008), Jul 31, 2016: CONTROL UNIT. FAULTED. THE CREW NOTED A RED LEFT "BLEED AIR LEAK" EICAS MESSAGE FOR AN ENGINE BLEED AIR LEAK. MESSAGE ILLUMINATED AT FLIGHT 350. CREW FOLLOWED THE QRH PROCEDURES TO SH - [SDR CWQA20160318001](https://openairdocs.org/sdr/CWQA20160318001), Mar 16, 2016: ROLLER. BROKEN. DURING FLIGHT, CREW HEARD A THUMP & RECEIVED BAGGAGE DOOR OPEN MSG, NO NOTICEABLE PRESSURIZATION ISSUE NOTED. CHECKLIST FOLLOWED & UNSCHEDULED LANDING PERFORMED - [SDR CA150525001](https://openairdocs.org/sdr/CA150525001), May 6, 2015: OIL SYSTEM. LEAKING. (CAN) DURING CLIMB, CREW REPORTED HAZE AND SLIGHT ODOR IN THE CABIN. THERE WERE NO OTHER ISSUES REPORTED. CREW ELECTED TO RETURN TO AIRPORT OF DEPARTURE AND PER - [SDR CA150518008](https://openairdocs.org/sdr/CA150518008), Apr 25, 2015: UNKNOWN. SMOKE. (CAN) A PAX REPORTED SMOKE IN CABIN. THE EVENT WAS NOTED DURING CLIMB FROM AT APPROX 12K FEET. SUSPECTED THE ISSUE TO BE OIL MIST. DECLARED AN EMER & RETURNED T - [SDR CWQA20150223001](https://openairdocs.org/sdr/CWQA20150223001), Feb 18, 2015: ACTUATOR. LEAKING. DURING CRUISE AT FL410, CREW RECEIVED HYD LEVEL LOW RT LIGHT FOLLOWED BY AUX HYD PUMP ON LIGHT. CHECKLIST FOLLOWED, EMER DECLARED & UNSCHEDULED LANDING PERFORME - [SDR DXTR2014082001](https://openairdocs.org/sdr/DXTR2014082001), Aug 20, 2014: BRACKET. CRACKED. ANGLE AT BS 487 ON TOP OF FUEL BLADDER STRUCTURE IS CRACKED IN HALF. R & R BRACKET IAW G-200-53-144 AND ENGINEERING REPAIR ORDER ERO-605951. - [SDR DXTR2014072101](https://openairdocs.org/sdr/DXTR2014072101), Jul 21, 2014: UNKNOWN. VIBRATION. AT FL210, HAD AN AIRFRAME VIBRATION NOTICED AT 300 KIAS AND INCREASED AS AIRSPEED INCREASED. INTENSITY INCREASED IN LT TURNS, CLIMBS, DESCENTS, AUTO-PILOT ON & - [SDR 9JLA2014072106430](https://openairdocs.org/sdr/9JLA2014072106430), Jun 21, 2014: ACTUATOR. DEFECTIVE. THE CREW REPORTED THAT THEY RECEIVED RT THRUST REVERSER FAIL CAS MSG ILLUMINATED DURING LANDING. THE THRUST REVERSER WOULD NOT FULLY DEPLOY. TROUBLESHOOTING FOU - [SDR DXTR2014061001](https://openairdocs.org/sdr/DXTR2014061001), Jun 4, 2014: ATTACH ANGLE. CRACKED. ANGLE AT FS 487 ON TOP OF FUEL BLADDER STRUCTURE IS CRACKED THROUGH. - [SDR 9JLA2014042106437](https://openairdocs.org/sdr/9JLA2014042106437), Apr 16, 2014: DUCT. CRACKED. DURING POST FLIGHT CHECKS, BLUE WATER WAS NOTED DRIPPING FROM ACFT BELLY PANEL. INVESTIGATION FOUND THE LAVATORY WASTE DRAIN DUCT CRACKED INBD OF THE LAVATORY S - [SDR DXTA2013112005574](https://openairdocs.org/sdr/DXTA2013112005574), Nov 19, 2013: ENGINE. DAMAGED. CLIMBING THROUGH 38000' IN MAX CLIMB DETENT 290KTS TWO DISTINCT BANGS, SIMILAR TO COMPRESSOR STALLS, WERE FELT THROUGH FLOOR, RUDDERS & CONTROLS. ALL INSTRUMENT - [SDR 9BPA2012FA0000714](https://openairdocs.org/sdr/9BPA2012FA0000714), Aug 21, 2012: FLEX LINE. FAILED. PAX OXYGEN SYSTEM FAILED TO DEPLOY DURING FUNCTIONAL CHECK. UPON INVESTIGATION, MX FOUND MULTIPLE O2 FLEX LINES HAD FAILED AT MULTIPLE LOCATIONS ON EACH LINE. B - [SDR CA120813008](https://openairdocs.org/sdr/CA120813008), Aug 3, 2012: ENGINE. VIBRATION. (CAN) ON A REVENUE FLIGHT, THE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE VIBRATION GAUGE WAS NOTED TO BE BETWEEN THE GREEN AND YELLOW BAND BUT THE VIBRATION COU - [SDR DXTA2012051104974](https://openairdocs.org/sdr/DXTA2012051104974), May 9, 2012: WARNING LIGHT. ILLUMINATED. ON APPROACH, AT 170KIAS THE LANDING GEAR WAS LOWERED. THE NOSE AND LT MAIN GEAR INDICATIONS WERE NORMAL. THE RT MAIN GEAR SHOWED AMBER FOR ABOUT 10 SECONDS FOLL - [SDR DXTA2012030704907](https://openairdocs.org/sdr/DXTA2012030704907), Mar 6, 2012: SELECTOR VALVE. LEAKING. ON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICATION - [SDR DXTA2011080204680](https://openairdocs.org/sdr/DXTA2011080204680), Jul 31, 2011: ACTUATOR. INOPERATIVE. UPON GEAR EXTENSION, THE RT MAIN GEAR INDICATION TURNED AMBER FOR A SHORT PERIOD OF TIME, THEN TURNED RED. THE RT ANTI-SKID OFF ILLUMINATED AS WELL. RECYCLED TH - [SDR 2011F00095](https://openairdocs.org/sdr/2011F00095), Apr 22, 2011: SENSOR. DAMAGED. EICAS MESSAGE CARGO COMPARTMENT SMOKE MESSAGE. DISCOVERED CARGO COMPARTMENT HEAT BLANKET TEMPERATURE SENSOR DAMAGED CAUSING HEAT BLANKET TO OVERHEAT. PRIA - [SDR 2011FA0000108](https://openairdocs.org/sdr/2011FA0000108), Jan 16, 2011: INLET SCREEN. WORN. ON RECEPTION FOR MX THE LT ENGINE INLET ACOUSTIC MESH WAS FOUND DEPARTED FROM INLET AREA AT 3PM POSITION TO 6PM POSITION. ENGINE DIGESTED THE MESH CAUSING DAMAG - [SDR DXTA200803089](https://openairdocs.org/sdr/DXTA200803089), Jun 1, 2008: WIRE. OUT OF POSITION. UPON FULL POWER APPLICATION AT APPROX 40KTS, RED BLEED PRESS / TEMP HI WARNING LIGHTCAME ON. ABORTED TAKEOFF. FOUND OVERPRESSURE SWITCH WIRES VERY CLOSE TO AN A - [SDR DXTA200802759](https://openairdocs.org/sdr/DXTA200802759), Jan 10, 2008: FLOAT VALVE. FAILED. IN CRUISE FLIGHT AT FL380 WE NOTICED FUEL LEAKING OUT OVER THE LT AILERON. REMOVED DEFECTIVE LEFT WING VENT FLOAT VALVE AND INSTALLED NEW VALVE PER G200 CMP 285 - [SDR DXTA200702431](https://openairdocs.org/sdr/DXTA200702431), Aug 27, 2007: SIGHT GLASS. CRACKED. LT ENG OIL PRESS LOW EICAS MSG ON CLIMB OUT. (OIL PRESS 5 PSI INDICATED ON LT ENG) COMPLIED WITH QRH AND SECURED/SHUTDOWN ENG. REMOVED LT ENGINE UPPER AND LOWER - [SDR 2007FA0000014](https://openairdocs.org/sdr/2007FA0000014), Dec 20, 2006: LIFE RAFT. MISRIGGED. THIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOORING LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO LIFE RAFT FIRST AND - [SDR 2007FA0000013](https://openairdocs.org/sdr/2007FA0000013), Dec 20, 2006: LIFE RAFT. MISRIGGED. THIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOOORING LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO THE RAFT FIRST AND - [SDR 2007FA0000012](https://openairdocs.org/sdr/2007FA0000012), Dec 20, 2006: LIFE RAFT. MISRIGGED. THIS RAFT WAS INSTALLED ON AC BUT MAY BE INSTALLED ON OTHER SIMILAR AC. MOORING THE LINE (FIRING LINE) WAS FOUND RIGGED WRONG. LINE WAS TIED TO LIFE RAFT FIRST - [SDR DXTA200601483](https://openairdocs.org/sdr/DXTA200601483), Jul 5, 2006: ODOR. UNKNOWN. DURING FLIGHT FROM AFW TO EGE, STRONG EXHAUST ODOR IN THE COCKPIT AND DID NOT GO AWAY UNTIL AFTER SHUTDOWN. BORESCOPED LT, RT, APU BLEED AIR DUCTS LEADING TO AC - [SDR DXTA200601317](https://openairdocs.org/sdr/DXTA200601317), Mar 24, 2006: ENGINE. WARNING MESSAGE. UPON APPLICATION OF TAKEOFF POWER, HAD A MASTER WARNING INDICATION. IT APPEARED TO BE THE BLEED PRESS/TEMP HI MESSAGE. MESSAGE WENT OUT IMMEDIATELY WHEN RETARDI - [SDR O2G2006F00001](https://openairdocs.org/sdr/O2G2006F00001), Dec 15, 2005: CONTROLLER. FAILED. AT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. REMOVED AND REPLACED PRESSURE - [SDR O2G2006F00000](https://openairdocs.org/sdr/O2G2006F00000), Dec 15, 2005: CONTROLLER. FAILED. AT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. COULD NOT CONTROL CABIN ALT PR - [SDR DXTA200500980](https://openairdocs.org/sdr/DXTA200500980), Sep 23, 2005: FUEL FILTER. CLOGGED. LEFT FUEL PRESS, LOW CAS MESSAGE ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 75 KNOTS. REPLACED FUEL FILTERS (BOTH ENGINES) AND LEAK CHECKED, NO LEAKS NOTED - [SDR DXTA200500975](https://openairdocs.org/sdr/DXTA200500975), Sep 18, 2005: TRIM SYSTEM. MALFUNCTIONED. IMMEDIATELY AFTER TAKEOFF THE NORMAL PITCH TRIM FROZE AT 2.6 DEG SETTING. AFTER SEVERAL MINUTES AND SEVERAL ATTEMPTS AT NOSE DOWN TRIM, SYSTEM WORKED NORMAL, HO - [SDR 62GX20281](https://openairdocs.org/sdr/62GX20281), Nov 22, 2004: STATIC PORT. CORRODED. AIRCRAFT ADC (AIR DATA COMPUTER) - 200 FT SPLIT ON APPROACH TO LAND IN HEAVY RAIN. FOUND MOISTURE IN STATIC PORTS (4 EA) DURING POST FLIGHT INSPECTION. CLOSER I - [SDR DXTA200400269](https://openairdocs.org/sdr/DXTA200400269), Mar 18, 2004: AMPLIFIER. OVERHEATED. DURING FLIGHT CREW DETECTED SMOKE IN THE COCKPIT, NOTICED SMOKE COMING OUT FROM BEHIND THE BOTTOM FORWARD 2 DRAWS. TURNED THE GALLEY POWER OFF AND AFTER A FEW M - [SDR DXTA200400258](https://openairdocs.org/sdr/DXTA200400258), Mar 8, 2004: ODOR. DETECTED. AFTER 1.5 HOURS INTO FLIGHT, CREW NOTICED EXHAUST ODOR IN COCKPIT, SELECTED DIFFERENT AIR SUPPLY AND PROBLEM REMAINED. PRECAUTIONARY DIVERTED TO ABQ. ITEM IS UN - [SDR DXTA200300164](https://openairdocs.org/sdr/DXTA200300164), Nov 16, 2003: ACTUATOR. MALFUNCTIONED. AFTER TAKEOFF DURING FLAP RETRACTION THE LEFT AND NOSE GEAR UNLOCK LIGHTS ILLUMINATED AND THE RIGHT GEAR WENT TO RED, ACCOMPLISHED AIR TURNBACK TO LAS. ADJUSTED - [SDR V9B2003F00003](https://openairdocs.org/sdr/V9B2003F00003), Jun 20, 2003: ACTUATOR. INOPERATIVE. RUDDER TRIM WOULD NOT MOVE. FOUND LOWER TRIM ACTUATOR RECEIVING POWER BUT IT WOULD NOT MOVE. INSTALLED NEW LOWER ACT PN 4AS5830510-013 BUT COULD NOT TIME ACTUAT - [SDR V9B2003F00002](https://openairdocs.org/sdr/V9B2003F00002), Jun 20, 2003: ACTUATOR. INOPERATIVE. RUDDER TRIM INOPERATIVE. FOUND LOWER RUDDER TRIM ACTUATOR RECEIVING ELECTRICAL POWER BUT THE TRIM ACTUATOR WOULD NOT MOVE. - [SDR DXTA200300028](https://openairdocs.org/sdr/DXTA200300028), May 5, 2003: OIL CAP. LOOSE. ON CLIMBOUT RIGHT ENGINE LOW OIL PRESSURE MESSAGE CAME ON. RETARDED THROTTLE TO IDLE AND ENGINE PRESS DROPPED TO ZERO. SHUTDOWN THE RIGHT ENGINE PER CHECKLIST A - [SDR 2002FA0001223](https://openairdocs.org/sdr/2002FA0001223), Oct 8, 2002: SERVO. FAILED. SERVO CAUSED AUTOPILOT MISTRIM CONDITION AND EVENTUALLY DID NOT PERMIT AUTOPILOT TO ENGAGE. - [SDR UO22002F00012](https://openairdocs.org/sdr/UO22002F00012), May 1, 2002: FASTENER. MISINSTALLED. TWO FASTENERS IN THE FUSELAGE TANK APPEAR TO BE MISINSTALLED WITH NO EDGE DISTANCE. THEY ALSO DUE NO SIT FLUSH. THESE FASTENERS ARE ACCESSED THRU THE UPPPER FUS All 90: https://openairdocs.org/model/brumit-john-c-jr-galaxy/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Israel Aircraft Industries GALAXY](https://openairdocs.org/model/israel-aircraft-industries-galaxy): 19 registered aircraft, registry code 4500307 - [Gulfstream Aerospace LP GALAXY](https://openairdocs.org/model/gulfstream-aerospace-lp-galaxy): 0 registered aircraft, registry code 3980401 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.