N648QX
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
ENG 2 REV DEPLOYED DURING TAXI / ENGINE SHUTDOWN. ENG 2 REV PROT FAULT REMOVED FROM SERVICE. MANNALLY STOWED ENG 2 TR REF E175 AMM TASK 78-30-01-980-802-A. PERFORMWED TR FUNCTIONAL TEST REF E175 AMM TASK 78-30-01-720-801-A. OPS CHECK GOOD, FAULT CLEARED. RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.
FWD GALLEY OVEN 204 NOT HEATING FOOD. TIMER WORKS. MILD ELECTRICAL ODOR, NEGATIVE SMOKE. ODOR WENT AWAY WHEN OVEN TURNED OFF. CB DID NOT TRIP.REMOVED FROM SERVICE AND PLACED ON DMI. RETURNED TO SERVICE.
FLIGHT 2119. A/T FAULT ADVISORY AT TAKEOFF. TAKEOFF REJECTED AND RETURNED TO GATE. REMOVED FROM SERVICE AND PLACED ON MEL 22-33-00A. MEL CLEARED BY INTERROGATED CMC. FOUND NO CORRELATED FAULT CODES. PERFORMED A/T OPS TEST IAW AMM 22-31-00-710-801-A. OPS CHECK GOOD. ACFT REMAINS CAT 3. PLACARD REMAINS CAT 3. THIS CLEARS MEL. MTX CONTROL NOTIFIED. RETURNED TO SERVICCE. NO PARTS REPLACED.
FLIGHT 2186. ON TAKEOFF ROLL AT APPROX 30-40 KNOTS, EICAS PAX AFT DOOR OPEN. TAKEOFF REJECTED. CLEARED DURING TAXI TO GATE. REMOVED FROM SERVICE & PLACED ON MEL 52-70-00A. AFT PAX DOOR & NOTICED IND WENT FROM GREEN TO YELLOW BOX WITH BLACK X. INSPD & FOUND BREAK IN WIRE OF AFT PAX DOOR LOCK HARNESS AT DOOR SIDE OF HINGE FOR PINS C OF CONNECTERS P1 & P2. REPLACED AFT PAX DOOR LOCKED SENSOR HARNESS IAW MM 52-72-21-000-801-A, PARAGS 8I - 8L, & 52-72-21-400-801-A PARAGS 8A - 8G IAW FIM 52-72-00-810-804-A. AFT PAX DOOR NOW INDICATES NORMAL WHEN CLOSED & LOCKED OR FULLY OPEN. THIS MAINT ACTION CLEARS MEL 52-70-00(A) & PLACARDS REMOVED FROM CENTER CONSOLE IN FLIGHT DECK & ACFT MAINT LOG BOOK. RETURNED TO SERVICE.
FLIGHT 2358. ON T/O AT FAULT CYAN MSG ON EICAS. MANUALLY MATCHED THROTTLE LH THAT LAGGED RH. SHORTLY AFTER L/O FL250 AT FAIL MASTER CAUTION. BEFORE CALLING VLIST COMPLETE MSG DISAPPEARED. FIVE MINUTES LATER MASTERCAUTION AT FAIL. FLOW MANUAL THRUST LEVERS REMAINDER OF FLIGHT. REMOVED FROM SERVICE. PLACED ON MEL 22-30-00B. MEL CLEARED 1/30/25 BY REPLACING AUTO THROTTLE/THRUST QUADRANT IAW E175 FIM 22-31-00-810-909-A & AMM 76-11-01-000/400-801-A. OPS CHECK GOOD. PERFORMED AUTO THROTTLE/THRUST QUADRANT INTERFACE LLM RTS OPS TEST IAW E15 AMM 22-31-00-710-801-A. RETURNED TO SERVICE.
FLIGHT 2041. EAGLE, BIRD STRIKE ON TAKEOFF. LG NOSE DOOR OPEN CAUTION MSG. RETURN TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W BIRD STRIKE INSPECTION REF. E175 AMM 05-50-02-200-801-A. NO EVIDENCE OF ENGINE INGESTION NOTED. FOUND BROKEN RH NLG AFT DOOR LINKAGE TO BE CAUSE OF LG NOSE DOOR OPEN CAUTION MSG. REMOVED RH NLG AFT DOOR LINKAGE REF E175 AMM TASK 32-22-03-000-801-A. INSTALLED RH NLG AFT DOOR LINKAGE PER E175 AMM 32-22-03-400-801-A. ADJUSTMENT OF NEW PART REQUIRED. ADJUSTMENT MADE PER E175 AMM 32-22-03-820-802-A. A/C OKAY FOR SERVICE.
FLIGHT 2166. CA REPORTS COCKPIT, COCKPIT ENTRY, AND R1 DOOR EMER LIGHTS WILL NOT EXTINGUISH. REMOVED FROM SERVICE.CHARGED ELPU'S IAW E175 AMM 33-50-01-800-801-A. NO HELP LIGHTS REMAIN ON. SUSPECT FAULTED FWD RH BATTERY PACK. REMOVED FWD RH BATTERY PACK S/N:059735 IAW E175 AMM 33-50-01-000-802-A. INSTALLED NEW BATTERY PACK (FWD RH) IAW E175 AMM 33-50-01-400-802-A. OPS TEST PASSED. ALL EMERGENCY LIGHTS TURN ON AND EXTINGUISH PROPERLY. NO INAPPROPRIATE EICAS MESSAGES OR FAULTS. AIRCRAFT OK FOR SERVICE.
COCKPIT DOOR ISNT OPENING PROPERLY. IT GETS STUCK CLOSED AND IS DIFFICULT TO OPEN. REMOVED FROM SERVICE. GRIME BUILDUP ON DOOR LATCH STRIKER. CLEANED STRIKER AND DOOR OPERATES NORMALLY, MANUALLY AND AUTOMATICALLY. OPS TEST GOOD. RETURNED TO SERVICE.
CORROSION RH IB SEAT TRACK BETWEEN FR 84 FR 85 AT Y =+10.748. REPAIRED IAW HORIZON REF ETD2022-170-022163 REV A.
CORROSION RH BEAM BETWEEN FR 86-FR 88. REMOVED AND REPLACED RH BEAM BETWEEN FR 86-FR 88 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06.
DURING PRE DEPARTURE CHECK FOUND FWD CABIN EMERGENCY LIGHTS COME ON AFTER POWER DOWN. ELPU 2. REMOVED FROM SERVICE. PERFORMED E175 FIM TASK 33-50-00-810-816-A THROUGH 6.W.REPLACED ELPU 2 PER E175 AMM 33-50-01-000/400-802-A OPS TEST GOOD. ALL EMERGENCY LIGHTS WORK NORMALLY.NO FURTHER DEFECTS. RETURNED TO SERVICE.
BURNING SMELL NOTED DURING CLIMB THROUGHT CABIN LASTING APPROX 5MINS. CABIN TEMP ADJUSTMENT (LOWERING) ELIMINATED ODOR NO ODOR IN FLIGHTDECK, FLIGHT CONDUCTED 16,000 FT. REMOVED FROM SERVICE. COMPIED WITH FIM TASK 21-20-00-810-801-A. OPERATED BOTH PACKS AND APU INDIVIDUALLY NO DEFECTS NOTED WHILE ADJUSTING CABIN TEMP. DETERMINED TO BE TRANSITORY CONDITION. RETURNED TO SERVICE.
#1 ENGINE STARTER CONTROL VALVE HAS A HOLE IN IT. REPLACED THE STARTER CONTROL VALVE.
DURING CLIMBOUT HAD BURNING RUBBER SMELL FOR ABOUT 5 MIN. WENT AWAY. CAME BACK DURING APPROACH AT ABOUT 190KTS . SLIGTLY NOTICED THE SMELL WITH THE APU BLEED AS THE ONLY BLEED SOURCE. REMOVED FROM SERVICE. RAN APU FOR 15 MINS, DID NOT SMELL BURNING RUBBER SMELL. PERFORMED GVI OF APU. NO DEFECTS NOTED. RAN PACKS 1&2 ON HOT AND COLD. NO DEFECTS OR SMELLS. PERFORMED E175 FIM TASK 21-20-00-810-801-A SUBTASK 21-20-00-810-011-A AND 21-20-00-813-019-A. NO DEFECTS NOTED. FOUND TO BE TRANSITORY. RETURNED TO SERVICE.
SMELL IN CABIN SMELLS LIKE EXHAUST & ELECTRICAL. APU BLEED VALVE FLUCTUATING ON ECS PAGE. REMOVED FROM SERVICE. C/W E175 FIM TASK 21-20-00-810-803. PERFORMED GVI OF PACK AIR DUCTS, APU INLET, AND EXHAUST MANIFOLDS. FOUND AND REMOVED SNOW/ICE ACCUMULATION IN THE APU INLET. THE SMELL OF AN ODD ODOR IN THE FLIGHT DECK/CABIN HAS DISSIPATED, AND NO EXHAUST, ELECTRICAL SMELL/ODOR WAS NOTED. PERFORMED OPS TEST OF THE APU IAW AMM TASK 49-10-00-700-801-A, NO APU BLEED VALVE FLUCTUATIONS. OPS TEST GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
THE PHOTOLUMINESCENT INDICATOR STRIP AT SEAT 1A HAS MIGRATED AFT IN THE TRACK. REMOVED AND REPOSITION PHOTO LUMINESCENT INDICATOR STRIP LIGHT REF. E-175 AMM TASK #33-50-21-000-801-A, AND 33-50-21-400-801-A.
DURING ARRIVAL CHECK THE MCD GIRT BAR WOULD NOT REMAIN UPRIGHT. REPLACED THE FORWARD PASSENGER DOOR SLIDE FITTING ASSEMBLY IAW E175 AMM 53-10-21-00-804-1 AND 53-10-21-400-004A. CHECKS GOOD.
FOUND #1 ENGINE HYDRAULIC SUCTION LINE DAMAGED. REMOVED FROM SERVICE. REPLACED #1 ENGINE HYDRAULIC PUMP SUCTION LINE IAW E175 AMM TASK 29-11-32-000-802-A AND TASK 29-11-32-400-802-A. OPS/LEAK CHECK GOOD. NO DEFECTS NOTED. CLEAR DMI. RETURNED TO SERVICE.
EMERGENCY LIGHTS POWER SUPPLY AT POSITION 2 FAILED FUNCTIONAL CHECK. REPLACED BATTERY.
EMERGENCY LIGHTS OVER AISLE ROWS 3+5 NOT ILLUMINATING. REMOVED FROM SERVICE. R+R FWD LH EMERGENCY LIGHT POWER UNIT BATTERY REF. E175 AMM TASK 33-50-01-000-802-A & 33-50-01-400-802-A. OPS TEST GOOD. NO FURTHER DEFECT. AIRCRAFT RETURNED TO SERVICE.
AFTER COMPLETING TERMINATING CHECKLIST, AND SELECTING GSU PANEL IN USE, EMERGENCY LIGHTS ILLUMINATED FOR TWO MINUTES WITH FLIGHT DECK EMERGENCY LIGHT SELECTED OFF AND CABIN EMERGENCY LIGHT SELECTED OFF. REMOVED FROM SERVICE. INTERROGATED CMC NO FAULTS FOUND. PERFORMED EMERGENCY LIGHTING OPS TEST IAW E175 AMM 33-50-710-801-A. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.
R2 DOOR INDICATION DOES NOT DISPLAY "ARMED". MFD PAGE SHOWS DOOR CLOSED (GREEN). ARMING LEVER APPEARED TO NOT BE FLUSH. REMOVED FROM SERVICE. ADJUSTMENT AND RII OF EMERGENCY EVAC SLIDE MECHANISM, AND EVAC SLIDE ASSY REMOVE AND REINSTALL. AIRCRAFT RETURNED TO SERVICE.
EXITING RUNWAY AT 40KTS EICAS DISPLAYED LEFT + RIGHT BRAKE FAULT. LOST BRAKING FOR 2 SECONDS. EXITING RUNWAY EICAS LEFT + RIGHT BRAKE FAULT DISPLAYED AGAIN WITH A LOSS OF BRAKES FOR 2 SECONDS. REMOVED FROM SERVICE. CMC POSTED FAULT CODE 32533301NWS. PERFORMED FIM TASK 32-53-00-810-813-A. COULD NOT DUPLICATE FAULT. REPLACED BRAKE CONTROL MODULE 2 AS PRECAUTIONARY MEASURE. REF AMM TASK 32-41-07-000-801-A AND 32-41-07-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS OR FAULT CODES NOTED. RETURNED TO SERVICE.
DURING POST FLIGHT WALK AROUND FOUND POSSIBLE TAIL STRIKE ON ANTENNA. REMOVED FROM SERVICE. INSP. OF HARD LANDING PHASE I AND DMI FOR HARD LANDING PHASE II, TAIL STRIKE INSP. PHASE I AND II, DMI FOR PAINT AFT COLD WATER DRAIN FAIRING, FINDINGS OF THE WIFI ANT. CLIP AND FUSELAGE DENT. AFT L/H CLIP BROKEN FOR AFT WIFI ANTENNA. FUSELAGE DENT FROM AFT END OF BASE OF WIFI ANTENNA EXTENDING 53/4" AFT & 51/2" WIDE MAX DEPTH .1080. FERRIED FOR REPAIRS.
FURRING FUEL QUANTITY HARNESS ROUTING INSPECTION FOUND INCORRECT ROUTING UNDER PANEL 195AL. REROUTED GROUND SPOILER CNT MDL HARNESS SO THAT IT RAN SEPARATE FROM FQIS HARNESS TO COMPLY WITH INSPECTION CRITERIA IN E175 AMM 28-41-00-210-801-A.
UPON RECEIVING TAKEOFF CLEARANCE RELEASED EMER PARK BRAKE AND APPLIED POWER. AIRPLANE WOULD NOT MOVE. BRAKES APPEAR STUCK. NO LIGHTS ILLUMINATED AND NO MESSAGES. BRAKES FELT TOUCHY ON WAY BACK TO THE GATE. REMOVED FROM SERVICE. DURING RECOVERY FROM TAXIWAY, NOTED THAT ALL BRAKES APPEARED TO BE SETTING AND RELEASING AS PARK BRAKE WAS APPLIED AND RELEASED. ONCE A/C WAS PARKED BACK AT GATE, NOTED THAT L/H BRAKE TEMPS WERE 145 AND 151, R/H WAS 35 AND 38. TROUBLESHOT PER E175 DRAGGING BRAKE FIM TASK 32-40-00-810-804-A AND OVERTEMP BRAKE FIM TASK 32-40-00-810-801-A. WHEELS TURN, BRAKES DO NOT DRAG, PRESSURE TRANSDUCER READINGS W/IN RANGE, NO STUCK PEDALS, WHEEL SPEED TRANSDUCERS OPERATING NORMAL, BRAKE TEMPS INDICATING NORMAL AND HARNESS WIRING SERVICEABLE. TAXIED A/C W/ MODERATE BRAKING. BRAKES OPERATED SMOOTHLY W/ NO TEMPERATURE ISSUES. NO FURTHER DEFECTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
DURING EMERGENCY LIGHT TEST, CAS MESSAGE FOR BATTERY FAULT ILLUMINATED WHEN BATTERY SELECTED TO ON. REPLACED BATTERY.
ON POST FLIGHT WALK GROUND NOTICED RIGHT MAIN GEAR SMOKING BRAKE INDICATION IN YELLOW W/NO BRAKE OVERHEAT CAUTION. NO EXCESSIVE BRAKING DONE. REMOVED FROM SERVICE. PERFORMED OVERHEAT WHEELS INSPECTION, PER AMM TASK 05-50-16-200-801-A AND 05-50-12-200-801-A (N/A STEPS DUE TO THE BRAKE OVERHEAT MESSAGE NOT BEING PRESENT) NO DEFECTS NOTED DURING THE INSPECTION. BRAKE TEMPERATURES WITHIN ALLOWABLE LIMITS. RETURNED TO SERVICE.
PAX SEAT 3C BROKEN, IMPEDING EGRESS ROUTE FOR ROW 4CD. DEFERRED SEAT. ADJUSTED SEAT RECLINE CABLE AT SEAT 3C IAW E175 AMM 25-21-11-820-801-A. OPS CHECK GOOD. SEAT REMAINS UPRIGHT AND RECLINES PROPERLY. RETURNED TO SERVICE.
MAIN CABIN DOOR ABNORMALLY DIFFICULT TO OPEN EXTERNALLY. HANDLE STICKS AND HAS TO BE PULLED HARD. REMOVED FROM SERVICE. OPERATED DOOR MULTIPLE TIMES DOOR IS IN SERVICEABLE CONDITION. COULD NOT DUPLICATE PROBLEM. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.
DURING CRUISE LOST INDICATIONS FOR N1, N2, FUEL FLOW ON NUMBER ONE ENGINE. ALSO ELEV THR COMP FAIL ON ICAS. ALSO AUTOBRAKE FAIL ON ICAS. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED #1 ENGINE FADEC PER EMB 175 AMM TASKS 73-21-01-000-801-A AND 73-21-01-400-801-A. GROUND RAN #1 ENGINE. ALL INDICATIONS ARE NORMAL. NO FAULTS OR MESSAGES INDICATED. ALL CHECKS ARE GOOD. FOR AUTOBRAKE MESSAGE, CMC INDICATES NO FAULT MESSAGES AND NO FAULT DISPLAYED ON EICAS. REF EMB175 FIM TASK 32-41-00-810-809-A. CONSIDERED AS TRANSITORY CONDITION. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
MTX CONTROL REQUESTS REMOVAL OF #1 L/H OUT BOARD MAIN WHEEL TO PERFORM GVI OF #1 L/H OUTBOARD BRAKE DUE TO POSSIBLE "SMOKE" SIG. REMOVED FROM SERVICE. REMOVED #1 (LEFT OUTBOARD) WHEEL IAW E175 32-49-05-000-801-A. PERFORMED GVI OF BRAKE AXLE AND WHEEL. FOUND NO DAMAGE OR EXCESS GREASE. BARRINGS ALL APPEAR NORMAL, NO DISCOLORATION. NO DAMAGE FOUND. REINSTALLED TIRE IAW E175 AMM 32-49-05-400-801-A. AIRCRAFT RETURNED TO SERVICE.
"ON TAXI TO GATE, AIRCRAFT BEHIND US REPORTED DARK ABNORMAL EXHAUST OUT OF APU, APU WAS SHUT DOWN WITH NO ABNORMAL INDICATIONS." REMOVED FROM SERVICE. OPERATIONAL CHECK OF APU IAW E175 AMM 49-10-00-700-801-A. NO SMOKE NOTED, ALL OTHER PARAMETERS NOMINAL. COULD NOT DUPLICATE. MO PARTS REPLACED.
CREW REPORTS NO T/O TRIM WARNING PRIOR TO T/O. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED FROM SERVICE. CYCLED A/C PWR PITCH TRIM IND. RETURNED ON PWR UP. C/W OPS TEST OF HORIZ. STAB IAW AMM TASK 27-40-00-710-801-A. OPS CK GOOD. PITCH TRIM IND. FUNCTIONS NORMALLY. RETURNED TO SERVICE.
BURNING SMELL OBSERVED AFTER TAKEOFF DUMPED CABIN AND SMELL DISSIPATED A BIT. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W FIM INITIAL EVALUATION PER TASK 21-20-00-810-012-A. FOUND NO DETECTED SMELL. BEFORE FLIGHT ENGINE COMPRESSOR WASH WAS DONE. C/W FIM TASK 21-20-00-810-009-A. GROUND RAN ENGINES ABOVE 65% N1 FOR 15 MINUTES. NO FURTHER ABNORMALITIES NOTED. A/C IS OK FOR CONTINUED SERVICE. ALSO C/W FORM M-749, INITIAL MILD ODOR NOTED IN CABIN. NO ODOR IN COCKPIT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
FRONT LEFT MAIN DOOR DOES NOT OPEN FULLY. REMOVED FROM SERVICE. FOUND DEBRIS BUILD UP ON GUST LOCK PREVENTING THE GUST LOCK TO ENGAGE WHEN CLOSING MCD. CLEANED DEBRIS OFF GUST LOCK AND MCD OPENS & LATCHES NORMALLY. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
SHORT FINAL AT APPROX 300 AGL, FUEL FEED 2 FAULT DISPLAYED ALONG WITH A CLICKING SOUND (PRESENT EVERY 1 SEC). SOUND WAS LOCATED JUST FORWARD AND UNDERNEATH OF THE T/O CONFIG BUTTON, FORWARD FROM THE THRUST LEVERS. ON ROLLOUT/WOW, ENG1 NO DIPATCH AND ENG22 NO DISPATCH DISPLAYED ON EICAS. EXITING RUNWAY & HOLDING ON TAXIWAY, FUEL FEED 2 FAULT EXTINGUISHED AND CRG FIRE PROT FAULT DISPLAYED ALONG WITH OTHER NO DISPATCH LISTED EARLIER. MONITORED SYSTEM ELEC PAGE ON MFD AND EVERY 10 SECONDS AMBER DASHES POPULATE ACROSS MULTIPLE BUSSES. BOTH ENGINES POWERED & NO APU AT TIME HOLDING ON TAXIWAY. ANOTHER AIRCRAFT ON GROUND REPORTED OUR TAXI LIGHT FLASHING WHEN ON. NO FLASH IN OFF POSITION. WAS ABLE TO TAXI IN UNDER OWN POWER AND USED GPU AS DID NOT KNOW WHICH SYSTEMS WERE ALL AFFECTED. AT GATE WITH ONLY GPU, STILL AMBER DASHES INTERMITANTLY DISPLAYING EVERY 5-10 SECONDS BUT NO MORE CLICKING SOUND (WENT AWAY WITH ENGINE SHUTDOWN. REMOVED FROM SERVICE. REMOVED AND REPLACED MICRO COMM CARDS IN SPDA1 CARD 8 AND 12 IAW 24-61-07-000-801-A AND 24-61-07-400-801-A. NO HELP. RETURNED TO ORIGINAL CONFIGURATION. REPLACED POWER SUPPLY MODULES IN SPDA1 CARD SLOT 1 AND 20 IAW 24-61-11-000-801-A AND 24-61-11-400-801-A NO HELP. RETURNED TO ORIGINAL CONFIGURATION. REPLACED ASCB COMMS MODULE SPDA1 SLOT 10 IAW 24-61-09-000-801-A AND 24-61-09-400-801-A. OPS CK GOOD. RETURNED TO SERVICE.