N647QX
Registered owner: HORIZON AIR INDUSTRIES INC, WA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FLIGHT 2175. EMERGENCY LIGHTS TURN WHEN POWERED OFF AND GROUND SERVICE BUTTON PUSHE. REMOVED FROM SERVICE. CYCLED COCKPIT EMERGENCY LIGHT SWITCH SEVERAL TIMES AND FAULT CONDITION IS NO LONGER PRESENT. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00-710-801-A. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2080. RECTED TAKEOFF AT 100-110 KTS, DUE TO CAUTION MSG-ENG TLA NOT TOGA-POSSIBLE CA BUMPED TL. BRAKE TEMPS IN YELLOW BUT NO OVERHEAT MSG RECIEVED. NO BRAKE OVERHEAT EICAS MESSAGE NOTED. ACCOMPLISHED AMM 05-50-12-200-801-A. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.
URING CRUISE AT FL370, GOT AN AMBER ELEVATOR FAULT. RAN CHKLIST IN QRH. ON PUSHING FCM ELEVATORS BUTTON IN AND OUT, THE MESSAGE WENT AWAY. UPON LANDING, WE GOT FLT CTRL NO DISPATCH. AFTER PARKING, GOT ANOTHER ELEVATOR FAULT, WHICH WENT AWAY ON ITS OWN AFTER ABOUT 5 SECONDS. REMOVED FROM SERVICE. ATTEMPTED FCND RTS TES IAW AMM 27-00-00-070-801-A. UNABLE TO INITIALIZE TEST. . REPLACED PACE 1 IAW AMM 27-03-03-000/400-801-A. RIGGING CHECK GOOD. NO MORE EICAS MESSAGES SHOWING. RESET AIRCRAFT. RESET P-BITS. FCND AND RELATED EICAS MESSAGES STILL DONT SHOW. COMPLETED FREEDOM OF MOVEMENT CHK, ENSURED FULL TRAVEL & VERIFIED PROPER DIRECTION OF MOVEMENT. NO DEFECTS PER GPM 9.2. NFDN. AIRCRAFT GOOD FOR SERVICE.
FLIGHT 2014. ELEVATOR FELT STIFF IN FLIGHT. BOTH CA AND FO SIDE. NO NOTICEABLE "SNAP" OF CONTROL COLUMN UPON AP DISCONNECT. HYD PBIT WAS NORMAL AS WAS THE FLGIHT CONTROL CHECK. WAS NOT ABNORMALLY STIFF ON GROUND. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CHECKED CMC FOR FAULTS. NONE FOUND PER REQUEST C/W FHDB AND QAR DOWNLOADS REF AMM 45-45-00-970-801-A AND 31-32-00-470-801-A. COMPLIED WITH E175 FIM TASK 27-30-00-810-806-A STEPS 1-4 P(1). NO DEFECTS FOUND OTHER THAN R/H CONTROL COLUMN DAMPER IS LEAKING FLUID. REMOVED AND REPLACED R/H CONTROL COLUMN DAMPER PER E175 AMM TASKS 27-31-02-000-801-A AND 27-31-02-400-801-A. OPS CHECK IS GOOD. NO LEAKS NOTED. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT FOR FLIGHT CONTROLS. NO DEFECTS NOTED PER GPM 9.2. REF LP 1135514 FOR OPS TEST OF AUTOPILOT ELEVATOR SERVO. REFERENCE LP 1135515 FOR OPERATIONAL CHECK FLIGHT. OPERATIONAL CHECK FLIGHT GOOD. RETURNED TO SERVICE.
FLIGHT 2088. ENG 1, NO DISPATCH AND ENG 1 FADEC FAULT APPEARED UPON EXITING RUNWAY AFTER LANDING. REMOVED FROM SERVICE. FAULT CODE 73216117E1B POSTED IN CMC CIRCUIT BREAKER FADEC 1A PULLED AND RESET. REPLACED LT ENGINE FADEC IAW AMM 73-21-01-000-801-A AND 73-21-01-400-801-A. EICAS MESSAGES EXTINGISHED NO ACTIVE FAULT PRESENT. RETURNED TO SERVICE.
FUEL FEED 2 FAULT ON TAKEOFF. REJECTED TAKEOFF. REMOVED FROM SERVICE. INFO ONLY RESET. FUEL FEED 2 FAULT IAW AOM 1 PG 3.8.25 AND GPM 8.2.2.4 MSG CLRD. RETURNED TO SERVICE. NO PARTS REPLACED.
WHEN MOVING CONTROL COLUMN AFT OR FORWARD FEELING A CLICK IN THE CONTROLS. NO BINDING WAS FELT.. REMOVED FROM SERVICE AND FERRIED FOR REPAIRS. REMOVED AND REPLACED CONTROL DISCONNECT DEVICE REF E175 AMM TASK 27-31-06-000-801-A, 27-31-06-400-801-AOPS CK GOOD NO OTHER DEFECTS NOTED AT THIS TIME COMPLETED FREEDOM OF MOVEMENT CHECK ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO OFHTER DEFECTS NOTED. PER GPM 9.2. RETURNED TO SERVICE.
7AB CEILING LIGHT BURST.. REMOVED FROM SERVICE. REMOVED AND REPLACED CEILING LIGHT LAMP IAW AMM 33-21-05-000-801-A & 33-21-05-400-801-A. OPS CHECK GOOD. RETURNED TO SERVICE.
FLIGHT 2453. MASTER WARNING "LAV SMOKE" AT FL350. NO SMOKE, FUMES OR EVIDENCE OF FIRE FROM FA"S. PAX WAS NOT VAPING BUT WAS QUITE TALL. SUSPECT HAIR RUBBING SMOKE DET. AFT LAV AFFECTED. REMOVED FROM SERVICE. GVI OF AFT LAV SMOKE DETECTOR REVEALS NO DEFECTS. C/W OP'S TEST OF AFT LAV SMOKE DETECTOR. REF E175 AMM TASK 26-14-01-710-801-A. OP'S TEST GOOD. NO DEFECTS NOTED. A/C RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2100. HYD 3 LO QTY EICAS MESSAGE NEAR TOP OF DECENT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. SERVICED #3 HYDRAULIC SYSTEM RESERVOIR REF E175 AMM 12-12-01-600-801-A. RAN 3A AND 3B ACMP'S AND INSPECTED SYS 3 AREA NO LEAKS FOUND. FLUID QTY REMAINS STEADY. NO FURTHER DEFECTS NOTED.RETURNED TO SERVICE. NO PARTS REPLACED.
AFT OVERHEAD AISLE EMERGENCY LIGHT OUT. REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW E175 AMM 33-50-13-000-803-A/-400-802-A. NO HELP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT #4 IAW E175 AMM 33-50-01-000-801-A 33-50-01-400-A OPS CHECK GOOD. RETURNED TO SERVICE.
SLAT FAIL DURING FINAL APPROACH @ 4500 MSL, DID MISSED APPRAOCH. RAN SLAT FAIL CHECKLIST, CYCLED FLAPS, MESSAGE REMAINED. ASSOC EICAS: AP FAIL, SPD BRAKE FAIL, SHAKER ANTICIPATED, AOA LIMIT FAIL, AT FAIL. WEATHER CLEAR, NO TURBULANCE, NO WIND GUSTS. LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W FIM TASK 27-81-00-810-805-A & AMM 27-80-00 FOR OPS CHECK, FAULT RETURNED. FAULT CODE 27811013ACE. FOUND OUTBOARD SLAT SKEW SENSOR DAMAGED. REPLACED OUTBOARD SLAT SKEW SENSOR PER E175 AMM 27-83-01-000/400-801-A. PERFORMED SLAT CONTROL SYSTEM MECHANICAL RIGGING PER AMM 27-80-00-820-801-A. OPS TEST OF SLAT SYSTEM GOOD. NO FAULTS ARE DISPLAYED ON EICAS. RETURNED TO SERVICE.
ECMP REQUEST TO REPLACE THE FADEC.
LH INBOARD SEAT TRACK BEAM AT FR 84 CORROSION. COMPLIED WITH EC ETD2024-170-015406 PERMANENT REPAIR-LH INBOARD SEAT TRACK BEAM AT FR 84 CORROSION REF EAMS H9579
LH IB SEAT TRACK HAS CORROSION AT FR 84. INSTALLED RH IB SEAT TRACK SPICE REPAIR AT FR84 REF ETD2022-170-022163 REV A.
CORROSION IN RH IB SEAT TRACK AT FR 17. REPAIRED RH IB SEAT TRACK AT FR 17 REF ETD2024-170-015417.
LH IB SEAT TRACK HAS CORROSION AT FR 84. REPAIRED LH INBD SEAT TRACK FR 84 BY INSTALLING REPAIR FILLER AND DOUBLER ON LH INBD SEAT TRACK FR 84 REF ETD2024-170-015406.
CORROSION RH IB SEAT TRACK BETWEEN FR20 23. REMOVED AND REPLACE RH IB SEAT TRACK BETWEEN FR20 23 REF SRM 51-40-08.
WHILE ENTERING A/C, FOUND L1 DOOR, FWD GIRT BAR FLOOR FITTING FLAP SLIDE NOT SITTING FLUSH. REMOVED FROM SERVICE. REMOVED AND REPLACED L1 DOOR, FWD GIRT BAR FLLOR FITTING ASSY, REF AMM TASKS 53-10-21-000/400-804-A. NO ADJUSTMENTS MADE. RETURNED TO SERVICE.
AFTER TAKEOFF A SLIGHT BURNING/ FOOD COOKING SMELL NOTED IN FLIGHTDECK. WITHIN A COUPLE MINUTES SMELL WENT AWAY. AFTER LANDING BURNT SMELL NOTED AGAIN, THIS TIME NOT LIKE FOOD COOKING. SMELL PERSISTED WHILE TAXIING IN. OVENS NOT USED DURING ENTIRE FLIGHT. REMOVED FROM SERVICE. PLACED APU ON MEL 49-00-00. 5/22 MEL CLEARED BY: REF FIM TASK 21-20-00-810-801-A STEP 5AC, 5AD. SUSPECT APU BLEED SHUTOFF VALVE. REMOVED VAPU-BLEED SHUTOFF VALVE IAW AMM 36-12-01-000-801-A. INSTALLED SERVICEABLE APU-BLEED SHUTOFF VALVE IAW EMBRAER MM TASK# 36-12-01-400-801-A. OPERATED #1 AND #2 PACKS USING APU BLEED AIR WITH TEMPERATURE SETTINGS FROM FULL HOT TO FULL COLD WITH RECIRCULATION FAN ON MAND OFF. NO ABNORMAL ODORS NOTED. THIS MAINTENANCE ACTION CLEARS MEL 49-00-00 AND PLACARDS DEFECT# 1002502 . RETURNED TO SERVICE.
WHEN SELECTING FLAPS 1 SHAKER ANTICIPATED, AOA LIMIT FAIL AND SLAT FAIL MASTER CAUTION RAN CHECKLIST. WENT AROUND FOR 2ND APPROACH. FLIGHT LANDED SAFELY. LANDED SLATS 0 FLAPS 1. REMOVED FROM SERVICE. INTERROGATED CMC FOUND FAULT CODE 27811013ACE. C/W E175 FIM TASK 27-81-00-810-805-A. FOUND SLAT SKEW SENSOR 3/4 BROKEN. REMOVED AND REPLACED SLAT SKEW SENSOR 3/4 IAW E175 AMM TASKS 27-83-01-000-801-A AND -400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
DURING FUEL QUANTITY HARNESS ROUTING INSPECTION, FOUND INCORRECT ROUTING UNDER PANEL 195AL. REROUTED GROUND SPOILER CONTROL MDL HARNESS SO THAT IT RAN SEPARATE FROM FQIS HARNESS TO COMPLY WITH INSPECTION CRITERIA IN E175 AMM 28-41-00-210-801-A.
FORWARD LENGTH OF PHOTOLUMINESCENT STRIP IS DAMAGED. REMOVED FROM SERVICE. REPLACED DAMAGED PHOTOLUMINESCENT STRIP IAW E175 AMM 33-50-21-000-001-A AND TASK 33-50-21-400-801-A. RETURNED TO SERVICE.
FORWARD LEFT HAND SECTION OF PHOTOLUMINESCENT STRIP FROM BULKHEAD TO SEAT 2A DAMAGED. REPLACED DAMAGED PHOTOLUMINESCENT STRIP IAW E175 AMM 33-50-21-000-001-A AND TASK 33-50-21-400-801-A. RETURNED TO SERVICE.
FORWARD LENGTH OF PHOTOLUMINESCENT STRIP IS DAMAGED. DEFERRED UNDER MEL 33-50-21A. MEL CLEARED BY REPLACING DAMAGED PHOTOLUMINESCENT STRIP IAW E175 AMM 33-50-21-000-001-A AND TASK 33-50-21-400-801-A. CLEAR MEL. RETURNED TO SERVICE.