N642QX
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
STEERING DISENGAGED MOMENTAIRILY FOR TWICE WHILE WAITING TO CROSS A RUNWAY. CYCLED THE PARKING BRAKE TO REGAIN STEERING. REMOVED FROM SERVICE. INTERROGATED CMC, NO CORRELATED MAINTENANCE MESSAGES/FC. PERFORMED STEERING HYDRAULIC SYSTEM OPS TEST, TEST PASSED. REF W/O 363694, N/R - 00001 FOR WORK PERFORMED. RETURNED TO SERVICE. NO PARTS REPLACED.
INSPECT AUTOTHROTTLE SYSTEM FOR DISCREPANCIES. RECURRING AUTOTHROTTLE SPLIT FAULT MESSAGES. PERFORMED E175 FIM 22-31-00-810-909-A AND FIM 22-31-00-810-922-A TO TRANSITORY CONDITION OF THE AUTO THROTTLE. AS A PRE-CAUTIONARY MEASURE AND FIM RECOMMENDATION, REMOVED AND REPLACED THE TCQ ASSEMBLY IAW E175 AMM 76-11-01-000-801-A AND AMM 76-11-01-400-801-A. PLACED INTO SOS PROGRAM OPERATIONAL TEST OF THE TAKEOFF/GO-AROUND (TOGA) SWITCHES AND THRUST REVERSER FUNCTIONAL TEST â GOOD. IAW E175 AMM 22-11-00-710-801-A AND AMM 78-30-01-720-801-A. ADDITIONALLY, OPERATIONAL TEST OF AUTO THROTTLE/TCQ INTERFACE â GOOD. IAW E175 AMM 22-31-00-710-801-A.
DURING CRUISE AT FL360 ELEVATOR FAULT MASTER CAUTION AND AP FAIL MASTER CAUTION. ACCOMPLISHED ELEVATOR FAULT CHECKLIST AND BOTH MESSAGES EXTINGUISHED. AMBER DASHED BOX ON ELEV RH LINE UNDER RIGHT ACTUATOR ON FLT CTC PAGE REMAINED. RECIEVED FLT CTRL NO DISPATCH ON GROUND. REMOVED FROM SERVICE. INTERROGATED CMC FOUND FAULT CODE 27030522FCS & 270030422FCS. C/W FIM 27-03-00-810-91Y-A STEPS 1-G(I). FAULT CODES NO LONGER ACTIVE. PERFORMED FCND RTS TEST IAW AMM 27-00-00-070-801-A. RTS TEST GOOD. FCND NO LONGER SHOWN ON EICAS. PERFORMED AUTOPILOT OPS TEST IAW AMM 22-11-00-710-802-A. OPS TEST GOOD. NO DEFECTS NOTED. AIRCRAFT REMAINS CAT III, COCKPIT PLACARD READS CAT III, MTX CONTROL ADVSED. NO PARTS REPLACED. RETURNED TO SERVICE.
PHOTOLUMINECENT STRIP DAMAGED BEYOND LIMITS. REMOVED AND REPLACED DAMAGED PHOTOLUMINESCENT STRIP REF. AMM TASK 33-50-21-000/400-801-A.
FLIGHT 2061. AFTER LANDING AND AUTOBRAKE RELEASE, TOE BRAKES PULSATED TO A SKID UNTIL STOP. NO MESSAGES OF ANY KIND. BRAKES WERE LOCKED AND AIRCRAFT UNABLE TO LEAVE THE RUNWAY. PASSENGERS WERE REMOVED VIA BUSSES. REMOVED FROM SERVICE. REF W/O# 350254 N/R'S 00001, 00002, &00003 FOR WORK PERFORMED AND REPLACEMENT OF #2 BCM, BRAKE CONTROL VALVE, AND #3 BRAKE PRESSURE TRANSDUCER. ALL CHECKS ARE GOOD. NO FAULTS NOTED. AIRCRAFT OKAY FOR SERVICE. BRAKE CONTROL VALVE PN 39-871-2. BRAKE PRESSURE TRANSDUCER PN 52-633500-1.
FLIGHT 2064. AFTER STOPPING ACFT AT THE GATE, ENGINES SHUT DOWN, LOST A/C POWER, ASSOCIATED WITH APU FAIL CAUTION. RAMP PERSONNEL HEARD A LOUD BANG FROM THE APU OBSERVED SPARKS AND SMOKE FROM APU TAILPIPE. PLACED APU ON MEL 49-00-00. RETURNED TO SERVICE.
FIRST OFFICER CONTROL COLUMN HAS UNUSUAL FRICTION AND FEEL IN PITCH ACTION ONLY. UNUSUAL FEEL FELT IN FLOOR BOARDS AND PEDALS ON FO SIDE AT THE SAME TIME. REMOVED FROM SERVICE. CHECKED A/C HISTORY - NONE. CMC SHOWED NO ASSOCIATED FAULTS OR HISTORY. INSPECTED FLIGHT CONTROL MECHANISMS BELOW COCKPIT FLOOR. NO DEFECTS NOTED. PERFORMED FIM MCN E270006 ISSUE 1. CONTROL COLUMN MOVES SMOOTHLY WITH NO BINDING. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED PER GPM 9.2 (FREEDOM OF MOVEMENT CHECK). RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.
AFTER TAKING RUNWAY , ADVANCING THROTTLE, RECEIVED EICAS MSG FUEL FEED 2 FAULT. ABOURTED TAKEOFF AT LESS THAN 10 KNOTS. REMOVED FROM SERVICE. INFO ONLY- RESET #2 AC PUMP IAW AOM 1 3.8.25 AS DIRECTED BY M/C. GPM GPM 8.2.2.4 CAUTION CLEAR. RETURNED TO SERVICE.
CORROSION IN LH IB SEAT TRACK AT FR 84. INSTALLED DOUBLER REPAIR LH IB SEAT TRACK AT FR 84 SRM 53-23-10.
CORROSION RH IB SEAT TRACK AT FR 84. APPLIED SPLICE REPAIR TO RH IB SEAT TRACK AT FR84.
TAPE APPLIED TO DAMAGED FASTENER ON UPPER FUSELAGE SKIN PANEL 170-20871-003, STGR 2L, 19.5" AFT OF FR20 AND 13.2" FWD OF FR 23 IS TO BE INSPECTED WEEKLY. IF FOUNDATION WORN, TORN, OR PEELING TAPE IS TO BE REPLACED. REMOVED TAPE AND REMOVED AND REPLACED FASTENER AT FR20-21 STGR 2L, REF 51-40-08.
DAMAGED FASTENER ON UPPER FUSELAGE SKIN PANEL 170-20871-003, STR 2L 19.5" AFT OF FR 20 AND 13.2" FWD OF FR23 REQUIRES A DET INSPECTION TO BE PERFORMED EVERY 150 FC TO ENSURE DAMAGE HAS NOT FURTHER DETERIORATED BEYOND THE LIMITS OF SRM II 53-00-00 AD04. COMPLIED WITH ETASKCARD. REMOVED AND REPLACED FASTENER AT FR20-21 STGR 2L. REF 51-40-08.
LH FWD FUSELAGE SKIN CREASE DAMAGE. COMPLIED WITH ETD2021-170-012403-3 LH FWD FUSELAGE SKIN CREASE DAMAGE PERMANENT REPAIR.
CORROSION RH IB SEAT TRACK AT FR17. INSTALLED REPAIR DOUBLER RH IB SEAT TRACK AT FR17, REF ETD2024-170-003631.
MISDRILLED HOLE AT STR 2L 19.5" AFT OF FR 20 AND 13.2" FWD OF FR23. REPAIRED THE STRINGER AS PER SRM 51-10-07, CASE 2 BY INSTALLING A CYLINDRICAL BUSHING TO THE STRINGER AND A COUNTERSUNK BUSHING TO THE DAMAGED SKIN. INSTALLED FASTENER ONCE BUSHING IS INSTALLED. REF SRM 51-40-08.
FORWARD FUSELAGE-FR22 STRINGER 2L MISDRILLED HOLE PERMANENT REPAIR. COMPLIED WITH EC ETD2024-170-003979 FORWARD FUSELAGE-FR22 STRINGER 2L MISDRILLED HOLE PERMANENT REPAIR.
AFT SERVICE DOOR ESCAPE SLIDE CABLE UPPER END INSULATION SEPARATED. REPAIRED ESCAPE SLIDE CABLE UPPER END INSULATION ON AFT SERVICE DOOR PER HORIZON COC AMM 52-42-40, MCN E520113-01. REF AMM 52-42-40, 52-42-00.
FWD SERVICE DOOR EVACUATION SLIDE MECHANISM CABLE CASING IS SEPARATED AT UPPER END. REPAIRED EVACUATION SLIDE MECHANISM CABLE CASING UPPER END INSULATION ON FWD SERVICE DOOR PER HORIZON COC AMM 52-41-40, MCN E520113-01. REF AMM 52-41-40, 52-41-00.
R1 DOOR GIRT BAR FLOOR FITTINGS BOTH FOUND TO BE STICKING. R&R BOTH R1 DOOR GIRT BAR FLOOR FITTINGS REF E175 AMM TASK 53-10-25-00/400-804-A. NO RIGGING ADJUSTMENTS MADE.
STRONG UNKNOWN SMELL AFTER TAKEOFF. IN FLIGHT DECK AND CABIN. RETURNED TO PDX. REMOVED FROM SERVICE. C/W E175 FIM TASK 21-20-00-810-801-A. RAN A/C FOR 20 MIN WITH NO ADNORMAL SMELLS NOTED. ALSO REF. MCN E210016-3 A/C OK FOR CONTINUED SERVICE. RETURNED TO SERVICE.
GLOW STRIP ON FLOOR AT 1C CAME OFF. REMOVED FROM SERVICE. RE SECURED PHOTOLUMINESCENT STRIP AT 1C IAW E175 AMM TASK 33-50-21-400-801-A. STRIP OPERATES AS NORMAL. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
AT CRUISE (FL280) AMBER "ALT" FLAG APPEARED ON BOTH ALTIMETERS. FO WAS PILOT FLYING AND SRC WAS ON FO SIDE. IN FLIGHT DATA AS FOLLOWS: ADS1 - 28220', ADS2 - 28000', ADS3 - 28080' ALTIMETER 29.92, T=56 C, IESS - 28070. XPDR#1 WAS IN USE. NO CHANGE WHEN SELECTING XPDR#2. UPON DESCENT "ALT" FLAG EXTINGUISHED AND REMAINED SO FOR DURATION OF RETURN FLIGHT AT FL250, APPROACH AND LANDING. PERFORMED ALTITUDE SPLIT EVALUATION REF FIM 34-15-00-810-850-A ADSP 1 SHOWS 100% RESPONSIBLE PERFORMED GVI OF ADS PROBES, NO DEFECTS NOTED. I HAVE PERFORMED ALL INSPECTIONS AND/OR TESTS AS DETAILED IN PARAGRAPH C OF THIS FERRY PERMIT, AND HAVE DETERMINED THAT THE AIRCRAFT IS SAFE FOR FERRY FLIGHT FROM ANC TO PDX. REPLACED THE #1 AIR DATA PROBE.
FWD EMERGENCY LIGHTS (ONLY) REMAINS ILLUMINATED AFTER TERMINATING CHECKLIST. REMOVED FROM SERVICE. PERFORMED EMERGENCY LIGHTS OPS TEST PER E175 AMM 33-50-00-710-801-A, OPS TEST GOOD. COULD NOT DUPLICATE DISCREPANCY. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.
FWD SERVICE DOOR WILL NOT OPEN. REMOVED FROM SERVICE. ACCOMPLISHED FIM TASK FOR FWD SERVICE DOOR HARD TO OPEN, CYCLED DOOR MULTIPLE TIMES, OPS CHECK GOOD. NO SIGNS OF DAMAGE OR FURTHER DEFECTS NOTED. REF FIM TASK 52-41-00-810-806-A. RETURNED TO SERVICE.
FWD SERVICE DOOR WILL NOT OPEN. REMOVED FROM SERVICE. ACCOMPLISHED FIM TASK FOR FWD SERVICE DOOR HARD TO OPEN, CYCLED DOOR MULTIPLE TIMES, OPS CHECK GOOD. NO SIGNS OF DAMAGE OR FURTHER DEFECTS NOTED. REF FIM TASK 52-41-00-810-806-A. RETURNED TO SERVICE.
FA REPORTS AFT LAV SMOKE DETECTOR SHOWS RED LIGHT CONTACTED MAINT, THEY ADVISED TEST WITH FORWARD FA PANEL- DID NOT RESET AND DID NOT TRIGGER MASTER WARNING OR EICAS. REMOVED FROM SERVICE. C/W E175 FIM TASK 26-14-00-810-802-A. NO FAULT CODES. PERFORMED OPERATIONAL TEST OF THE LAVATORY SMOKE DETECTOR IAW AMM TASK 26-14-01-700-801-A. OPS TEST GOOD, NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
AFT SPOILER CNTL MODULE HARNESS FOUND TO BE ROUTED ALONG WITH FUEL QTY HARNESSES. REROUTED AFT SPOILER CNTL MODULE HARNESS AND FUEL QTY HARNESSES TO BE SEPARATE FROM EACH OTHER PER E175 AMM 28-41-06-400-801-A, SWPM 20-45-30, NO DEFECTS NOTED.
WINDSHIELD 2 HTR FAIL CAUTION ILLUMINATED DURING CRUISE. COMPLIED WITH E&A CHECKLIST & MESSAGE EXTINGUISHED. REMOVED FROM SERVICE. REMOVED & REPLACED WINDSHIELD HEATER CONTROL UNIT 2 REF E175 AMM TASK 30-42-01-000-801-A + 30-42-01-400-801-A. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
RAMP REPORTS UNABLE TO OPEN R1 DOOR. REMOVED FROM SERVICE. OPEN & CLOSED DOOR. NO DEFECTS NOTED. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
PHOTOLUMINESCENCE FLOOR STRIP IN FRONT OF FWD GALLEY AND ROW 1 SEAT CD IS WORN OUT ONLY PARTIALLY ILLUMINATE ( PHOTOLUMINESCENT ESCAPE ROUTE MARKING SYSTEM - PART 91 ONLY ). REMOVED FROM SERVICE. REPLACED THE WORN OUT PHOTOLUMINESCENT STRIP LIGHTS REF E175 AMM 33-50-21-960-801-A. OPS TEST GOOD. THIS CLEARS MEL. PLACARD ON FA PANEL AND AML REMOVED. AIRCRAFT RETURNED TO SERVICE.
LH/RH BRAKE FAULT CAS MESSAGE AS WE TOOK THE RUNWAY. AUTO BRAKE KICKED OFF AND A/C SURGED FORWARD MOMENTARILY. ABORTED TAKEOFF RETURNED TO THE GATE. REMOVED FROM SERVICE. NO RELATED CMC FAULTS TO EITHER LH/RH BRAKE FAULT MSGS, ALSO NO AUTO BRAKE FAULTS NOTED. DID FIND FAULT CODE 32533300NWS MAU1 BCM1/MAU2 NWSCM/WRG. REF FIM TASK 32-53-00-810-803-A. DEEMED TO BE A TRANSITORY CONDITION OF NIC+PROCESSOR MODULE 1. NO CURRENT RELATED MSGS OR CMC FAULTS NOTED. NO RECENT RELATED HISTORY IN TRAX. A/C OK FOR CONTINUED SERVICE.
DURING CRUISE HYD 1 LO QTY AND HYD PUMP EDP 1 FAIL ADVISORY MESSAGES ILLUMINATED HYD 1 LO PRESS CAUTION ILLUMINATED SHORTLY AFTER. RAN QRH PROCEDURE TO COMPLETION HYD 1 QTY READS ZERO. REMOVED FROM SERVICE. PERFORMED NR 1 EDP FAIL INSPECTION/CHECK, REF AMM TASK 05-50-23-200-802-A DPI WERE NOT EXTENDED ON FILTER MANIFOLD. ALSO PERFORMED NR 1 EDP RUN DRY INSPECTION, REF TASK 05-50-23-200-801-A. PERFORMED FIM TASK 29-11-00-810-805-A FOR HYD 1 LO QTY MESSAGE. ALL OPERATIONS AND LEAK CHECKS GOOD. REPLACED NR 1 EDP WAS REPLACED. RETURNED TO SERVICE.
FLUORESCENT LIGHTSTRIP BY 2A NOT WORKING OR VERY DIM IF IT IS. REMOVED FROM SERVICE. WATER FOUND IN FLUORESCENT LIGHT STRIP. R AND R FLUORESCENT LIGHT STRIP BY SEAT 2A. REF AMM 33-50-21-000-801-A AND 33-50-21-400-801-A. OPS TEST GOOD. AIRCRAFT RETURNED TO SERVICE.
FORWARD INBOARD COFFEE MAKER OVERHEAT AND OVERFLOWED.REMOVED FROM SERVICE. CLEANED COFFEE GRAINS FROM COFFEE MAKER AREA. BREW COFFEE AND NO OVER HEAT OR OVERFLOW NOTED. NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE. NO PARTS REPLACED.
R2 DOOR WOULD NOT ARM. REMOVED FROM SERVICE. PERFORMED GVI OF R2 DOOR. FOUND FOD (MAGNET) BLOCKING DOOR OPERATION. REMOVED FOD AND PERFORMED GVI OF AFFECTED AREA NO DAMAGE NOTED. FOD APPEARS NOT TO BE AIRCRAFT RELATED. CYCLED DOOR, ARMING, AND VENT LEVERS SEVERAL TIMES. NO DEFECTS NOTED DOOR, ARMING AND VENT LEVERS CYCLE NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.