N802QS

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 5,919 hrs · 3,511 cycles

WHEN EMER LTS ARE IN ARM AND PAX SAFETY SWITCH IS IN ON POSITION, THE WHITE EXIT LIGHT ABOVE THE FORWARD AIRSHOW SCREEN ON THE CABIN DIVIDER IS NOT ILLUMINATED. THE LIGHT WILL ILLUMINATE NORMALLY WHEN EMER LTS ARE PLACED IN THE ON POSITION. NO OTHER EMER LIGHTS ARE AFFECTED. CORRECTIVE ACTION: NO DEFECTS NOTED DURING OPS CHECK. IAW CE 700 AMM 33-50-00

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 5,744 hrs · 3,403 cycles

EMERGENCY EXIT LIGHT ON RIGHT SIDE OF AIRSTAIRS NOT ILLUMINATING. FOUND LIGHT DISCONNECTED FROM CONNECTOR, CHECK WIRES FOR DAMAGAE, RECONNECTED EMERGENCY LIGHT TO WIRE CONNECTOR. OPS TESTED EMERGENCY LIGHTS. OPS TEST GOOD. NO DEFECTS NOTED AT THIS TIME. REF AMM 33-50-00

Part: STEERING UNIT — DEFECTIVE (NLG) · airframe 5,562 hrs · 3,279 cycles

AFTER TAKEOFF AND DURING GEAR RETRACTION WE RECIEVED THE FOLLOWING AMBER INDICATIONS: GEAR CONTROL FAULT, GEAR DOOR OPEN, ADC SSEC MISCOMPARE, AND GEAR DISAGREE N. STARTED WITH GEAR CONTROL FAULT IN THE QRH WHICH REFERRED US TO "LANDING GEAR WILL NOT RETRACT" IN THE QRH. WENT TO THE SECOND STEP AND SELECTED LANDING GEAR DOWN. GEAR INDICATED THREE GREEN AND PROCEDURE COMPLETE. AFTER GEAR HANDLE WAS SELECTED DOWN NO OTHER CAUTION OR ADVISORY LIGHTS REMAINED. REPLACED POWER STEERING CONTROL UNIT IAW AMM 32-50-10. OPS/LEAK CHECK GOOD.

Part: SKIN — DENTED (ZONE 600) · airframe 5,550 hrs · 3,273 cycles

ACCOMPLISHED FR-700-0025-15113 - REV- DATED: 20MAY2025: FIELD REPAIR - DENT AND GOUGE, RH WING, LOWER SKIN, INBOARD OF RIB 2 AT STRINGER 03WL. PERFORM THE FOLLOWING INSPECTION AT 8000 HOURS AND THEN EVERY 4000 HOURS THEREAFTER. REMOVE ACCESS PANELS 612AB AND 612BB PER THE MODEL 700 MM CHAPTER 6-40-27. REMOVE SEALANT FROM AROUND COLLARS SHOWN IN FIGURE 7. SURFACE EDDY CURRENT INSPECT PERIPHERY OF EACH COLLAR SHOWN IN FIGURE 7 PER THE MODEL 700 NONDESTRUCTIVE TESTING MANUAL, PART 6, CHAPTER 20-00-02. LOOK FOR CRACKS IN THE SKIN EMANATING FROM THE FASTENER HOLES. CONTACT TEAM STRUCTURES IF CRACKS OR OTHER ANOMALIES ARE DETECTED. RESTORE COLLAR DAUB SEALS USING TYPE XIV SEALANT PER CSPM, CHAPTER 20-40-20. REINSTALL PREVIOUSLY REMOVED ACCESS PANELS PER THE MODEL 700 MM CHAPTER 6-40-27. AFTER ALL INSPECTIONS HAVE BEEN COMPLETED, CHECK FOR FUEL LEAKS PER THE MODEL 700 MM, CHAPTER 28-10-00.

Part: SQUAT SWITCH — DEFECTIVE (ZONE 700) · airframe 5,394 hrs · 3,186 cycles

NLG: NOSE GEAR WOULD NOT RETRACT. GEAR DISAGREE N AMBER CAS MESSAGE DISPLAYED. CORRECTIVE ACTION: REPLACED SQUAT SWITCH. OPS CHECK GOOD. IAW CE-700 AMM 32-60-10.

Part: THRUST REVERSER — CORRODED (ZONE 400) · airframe 4,799 hrs · 2,821 cycles

LH & RH UPPER AND LOWER TR BUCKETS HAVE EXCESSIVE CORROSION REMOVED AND REPLACED LEFT & RH HAND THRUST REVERSER REF. CE700 MM 78-30-00 THRU STEP 5.(7)(A). STEP 6 THRU COMPLETION STILL REQUIRED. ACCOMPLISHMENT OF STC #ST04560AT AND SQUAWK FOR ACCOMPLISHMENT OF NJA EO WC FLT-78-0002_2 REV 1 DATED 9/5/2024 (QTA TR INSTALLATION).

Part: CIRCUIT BOARD — MALFUNCTIONED (DOOR) · airframe 2,883 hrs · 1,682 cycles

APPROX 3 SECONDS AFTER DOOR IS RAISED FROM INSIDE, DOOR OPENS. DOOR RAISE BUTTON IS THEN UNRESPONSIVE UNTIL CANCEL BUTTON IS PUSHED. WHEN HANDLE IS ATTEMPTED TO BE PULLED DOWN IT IS STUCK AND DOOR COMES OPEN AGAIN. DUE TO HISTORY, AND OVERCURRENT NOTED, MANUFACTURER RECOMENDS TO REPLACE PCB NC101, TO LATEST P/N. ETA 1030 AM. REMOVED AND REPLACED PCBNC101 IAW CE700 MM 24-60-25. OPS CHECKED GOOD. PERFORMED VARIOUS CYCLE WITH NO ISSUES. OK TO CONTINUE.

Part: LIGHT — SHORTED (CABIN) · airframe 2,770 hrs · 1,625 cycles

THE INTERIOR AND EXTERIOR EMERGENCY LIGHT SYSTEM IS NOT OPERSTING PROPERLY. DIFFERENT LIGHTS ARE COMING OFF/ON AT TIMES. CONFIRMED BOTH FUSES FOR SEAT 5 EMERGENCY LIGHT WERE BLOWN. R & R BLOWN FUSE. R & R AFT FUSE. POWERED ON EMERGENCY LIGHTS AND SEAT 5 EMERGENCY PATH LIGHT WORKED FOR A BRIEF TIME BEFORE THE FORWARD AND AFT FUSES BLEW. DISCONNECTED #5 SEAT LIGHT SUSPECTING A SHORTED. REPLACED BOTH FUSES AND POWERED THE EMERGENCY LIGHTS ON FOR SEVERAL MINUTES AND CYCLED THE EMERGENCY LIGHTS MULTIPLE TIMES. RE CHECKED THE FUSES FOR THE SEAT 5 EMERGENCY PATH LIGHT AND THEY ARE STILL GOOD, CONFIRMING A FAULTY EMERGENCY PATH LIGHT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,720 hrs · 1,595 cycles

EMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO ON. ACCOMPLISHED A POWER CYCLE TO INCLUDE DISCONNETING THE MAIN BATTERIES, WHICH HAD NO EFFECT. // SIGNOFF// T/S TO FAILED BATTERY PACK. REMOVED FAILED ASSY AND INSTALLED A REPAIRED ASSY IAW CE-700 AMM 33-50-07 ALL OPS CHECKS GOOD

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 2,667 hrs · 1,564 cycles

EMERGENCY LIGHTING SYSTEM BATTERIES COMPLETELY DISCHARGE OVERNIGHT. THE SYSTEM WORKS FINE AFTER A FIVE MINUTE OF CHARGING ON APU POWER. CHARGED EMERGENCY BATTERY. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00. OPS CHECK GOOD.

Part: MONITOR — DEFECTIVE (ZONE 800) · airframe 2,114 hrs · 1,211 cycles

MAIN DOOR LOCK: CABIN DOOR OPEN CAS MESSAGE REMAINS ON AFTER DOOR IS CLOSED AND LATCHED. THERE IS NO SOUND OF THE DOOR LOCK SOLENOID CLOSING. TRIED THE DOOR RESET PROCEDURE. // SIGNOFF// TROUBLESHOT ISSUE TO NC103 PCB. GAINED ACCESS AND REMOVED NC103 CED MONITOR PN: 7468194-1 SN: 0137 DUE TO PCB POSTING CABIN DOOR WARNING CAS MESSAGES. INSTALLED CUSTOMER SUPPLIED NEW NC103 CED MONITOR PCB PN: 7468194-1 SN: 0177. OPS CHECK OF PCB GOOD. WORK PERFORMED REF CE700 AMM 24-60-25.

Part: NONE — NONE · airframe 1,564 hrs · 911 cycles

MAIN DOOR MOTOR SWITCH: MAIN CABIN WILL NOT CLOSE. DOOR GOES UP 1/4 OF THE WAY BEFORE STOPPING AND THE "CHECK DOOR HANDLE" LIGHT COMES ON. DOOR HANDLE SWITCHES APPEAR TO BE NORMAL.

Part: WIRE — BROKEN (MAIN DOOR) · airframe 1,166 hrs · 673 cycles

MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE. RED BUTTON HAS NO EFFECT. TROUBLESHOT RED PUSHBUTTON RELEASE AND FOUND THAT THE PUSHBUTTON SWITCH WAS GOOD BUT THAT THE CONNECTOR AO0L7 WAS EITHER NOT PROPERLY CRIMPED OR THAT THE WIRE HAD BROKEN OFF INSIDE THE SPLICE. NEW SPLICE ON ORDER. AWAITING PARTS. REMOVED OLD SPLICE AT A0017 AND INSTALLED NEW PIN AND SPLICE. OPERATIONAL CHECKS GOOD. NO FURTHER ACTION REQUIRED AT THIS TIME. ALL MAINTENANCE PERFORMED IAW CE-700 WIRING ?MANUAL 52-00-01.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 820 hrs · 472 cycles

RRL LH IN-BOARD FLAP DAMAGE REF ENGINEERING MEMO DQ29618M1 RRL

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 340 hrs · 209 cycles

MAIN CABIN DOOR EXTREMELY HARD TO OPEN AFTER FLIGHT. INSPECTED AND OPS CHECKED MAIN CABIN DOOR, IAW AMM 52-10-00-10. OPS CHECK GOOD AND NO DEFECTS NOTED, A/C OK FOR SERVICE.

Part: STRUCTURE — BENT (PAX DOOR) · airframe 8,327 hrs · 6,656 cycles

SHEETMETAL DAMAGE ON MAIN CABIN DOOR LOWER FOWARD CORNER ON EXTERIOR EDGE. ACCOMPLISHED REPAIR BY AQRD ENGINEERING ERO-900686 INSTRUCTIONS

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE) · airframe 6,302 hrs · 5,057 cycles

DESCENDING OUT OF CRUISE ALTITUDE, RT THROTTLE LEVER HAD NO EFFECT ON ENGINE POWER SETTING. RT ENGINE MAINTAINED CRUISE POWER, EVEN WHEN RT THROTTLE WAS BROUGHT TO IDLE. CREW SECURED RT ENGINE AS N2 WAS GOING TO EXCEED TOLERANCE, DECLARED AN EMERGENCY, & LANDED UNEVENTFULLY. PERFORMED A FCU CONTAMINATION CHECK IAW MM 73-20-01, NO DEFECTS NOTED. REPLACED FILTER IAW MM 73-20-01. R & R FCU WITH AN OVERHAULED UNIT, OPS & LEAK CHECKED GOOD IAW MM 71-00-00.

Part: MOTOR — UNSERVICEABLE (BRAKE SYSTEM) · airframe 6,102 hrs · 4,883 cycles

AFTER LANDING THE LOW RAKE PRESS & ANTI-SKID INOPERATIVE, ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE, USED EMER BRAKES TO STOP THE ACFT. THE POWER BRAKE CIRCUIT BREAKER IS OUT. REMOVED AND REPLACED THE POWER BRAKE MOTOR IAW CE-560 MM 32-42-01. OPS CHECKS GOOD.

Part: RELAY — UNSERVICEABLE (ANTI-SKID SYS) · airframe 6,083 hrs · 4,864 cycles

AFTER TOUCHDOWN DURING ROLL OUT THE LOW BRAKE PRESS ANNUNCIATOR ILLUMINATED. THE FIRST OFFICER THEN SAID HE HAD LOST BRAKES. USED EMER BRAKES TO STOP ACFT. POWER BRAKE CB POPPED. PUDDLE OF BRAKE FLUID UNDER NOSE GEAR RT SIDE. R & R THE SKID CONTROL RELAY & SKID CONTROL CB. PERFORMED BRAKE BLEEDING PROCEDURE & PURGED AUXILIARY BRAKE LINE OF ALL RESIDUAL FLUID. WORK DONE IAW MM 32-42-06, 24-50-02 & 32-42-00. OPERATIONAL & TAXI CHECKED GOOD.

Part: MOTOR — UNSERVICEABLE (HYDRAULIC SYS) · airframe 6,071 hrs · 4,853 cycles

AFTER NORMAL LANDING THE LOW BRAKE PRESS ANTI-SKID INOPERATIVE ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE DURING TAXI, HAD TO USE EMER BRAKES TO STOP ACFT. PUSHED IN CB, RAN POWER BRAKES 24X, COULDN'T DUPLICATE. IAW AMCC REPLACED MOTOR WITH AN OVERHAULED UNIT. REPLACED PUMP ASSEMBLY WITH NEW. BLED, SERVICED & PERFORMED OPERATIONS CHECK ANTI-SKID SYS IAW MM. OPERATIONS CHECK & LEAK CHECKS GOOD. SERVICED EMER AIR BOTTLE, LEAK CHECKED GOOD. PARTS CHANGED, BRAKE PRESS PUMP ASSEMBLY PN 9912166-3, SN 6992. HYD MOTOR PN MP50B1, SN 4191, COUPLING 6517108-4, NSN, RETAINER MS28774-129, NSN, RETAINER MS28774-130, NSN, O RING NAS1611-129, NSN, O RING NAS1611-130, NSN.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 6,051 hrs · 4,834 cycles

DURING CRUISE FLIGHT AT FL410, MFD BLANKED OUT. ONE MINUTE LATER LARGE RED X APPEARED ON THE SCREEN COUPLED WITH AN ELEC BURNING SMELL. THE MFD CAME BACK ON & ELEC SMELL DISSIPATED A SHORT TIME LATER. REMOVED AND REPLACED MFD IAW CE-560 MM 34-23-01. OPS CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,894 hrs · 4,695 cycles

AFTER PLYING TAKEOFF POWER A FAINT ODOR BEGAN COMING INTO THE CABIN. AROUND 2000' AGL BURNING SMELL BECAME VERY STRONG. RETURNED TO APA FOR LANDING. FREON AIR WAS OFF. DURING ENG RUNS, OPERATED PRESSURIZATION & AIR CONDITIONING SYS AT BOTH HIGH & LOW ENG POWER SETTINGS. CHECKED COALESCE SOCK IAW MM 21-70-00. CHECKED ALL LIGHTING, DISPLAYS & AC GENERATOR, OPERATIONS CHECKS ALL GOOD, NO DISCREPANCIES NOTED.

Part: MOTOR — BURNED · airframe 2,872 hrs · 2,290 cycles

ACFT CAUGHT FIRE. SPRAYED WITH FIRE EXTINGUISHER. MOTOR BURNED. DESERVICED SYS & REMOVED A/C PALLET ASSY IAW MM, CH 21-52-00 8/13/10. INSTALLED NEW MOTOR, PULLEYS AND BELT IAW THE ENVIRO MM GM06103 CH 21-00-07. 8/14 TENSIONED BELT & TORQUED HARDWARE. INSTALLED NEW RECEIVER/DRYER IAW ENVIRO MM GM06-103, CH 21-00-07 8/14/10 INSTALLED A/C PALELY ASSY IAW MM, CH 21-52-00 8/14/10. VACUUMED A/C SYS FOR 15 MINUTS A/C SYS LEAK CHECK GOOD. 8/15/10 CHARGED FREON A/C IAW MM 12-19-02, REV 20, 8/15/10 INSTALLED ACFT BATTERY IAW MM 24-32-00, REV 8.

Part: FLEX DUCT — CHAFED (ZONE 100) · airframe 2,350 hrs

DURING PHASE 1-5 INSPECTION, FOUND FLEX DUCT HAD CHAFED THROUGH THE INSULATION ON SEVERAL WIRE AND MAKE CONTACT WITH THE BARE WIRE SPINE OF THE FLEX DUCT. INDICATIONS OF ARCHING WERE NOTED. THE WIRE BUNDLE THAT WAS CHAFED IS THE R/H MAIN WIRE BUNDLE FROM THE AFT BULKHEAD J-BOX COMING FROM THE BOTTOM AND PASSING THROUGH THE AFT BULKHEAD VERTICAL SUPPORT BEAM LIGHTING HOLE. THE CHAFED WIRES ARE OUTBOARD OF THE VERTICAL BEAM.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 2,309 hrs · 1,840 cycles

IN FLIGHT, THE RADAR WHILE IN STBY WOULD FLASH "WAIT" ON THE MFD LOWER LEFT. IN WX MODE ON THE CONTROL HEAD AND SUBPANEL IT WOULD CYCLE BETWEEN A YELLOW "WX" AND WAIT. YOU COULD NOT ADJUST THE PITCH OR RANGE. THE RADAR WOULD NOT PAINT IN WX OR GMAP MODE.

Part: INVERTER — FAILED (NR 1) · airframe 2,240 hrs · 1,774 cycles

INVERTER NR 1 FAILED IN FLIGHT.

Part: LANDING GEAR — VIBRATION (NLG) · airframe 1,784 hrs · 1,414 cycles

EXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TAKEOFF ROLL. ABORTED TAKEOFF.

Part: COMPUTER — INOPERATIVE (FWD E/E BAY) · airframe 1,436 hrs · 1,101 cycles

AUTOPILOT DISENGAGED TWICE ON CLIMB-OUT ON PFD1. REMOVED AND REPLACED 1IC-615 AND C/W SYS. OPS CHECK IAW MM 34-23-10

Part: UNKNOWN — SMOKE (CABIN) · airframe 691 hrs · 524 cycles

SMOKE DISCOVERED IN CABIN AFTER TAKEOFF. REMOVED AND INSTALLED ACM IAW R70.3G CMM CHAPTER 21-50-03. OPERATIONAL AND LEAK CHECK NORMAL.