N335QS

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 10,305 hrs · 8,147 cycles

ALL EMER LIGHTS IN CABIN FLICKERING. REPEAT WRITE UP. REMOVED AND REPLACED NR 1 & 2 EMERGENCY BATTERY PACK AND PERFORMED OPS CHKD IAW AMM 33-52-01. OPS CHKD GOOD.

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 10,288 hrs · 8,132 cycles

OBSERVED ALL EMER LIGHTS INTERMITTENTLY FLICKERING. OBSERVED ALL EMER LIGHTS REMAINING ON FOR 20+ MINUTES WHEN SWITCH IN ARM POSITION. POWERED THE PLANE AND CHARGED THE EMERGENCY LIGHTS AND OPS CHECKED THE EMERGENCY LIGHTS IAW EMB-505 AMM 33-52-01. OPS CHECK GOOD, NOTED NO DISCREPANCIES WITH THE SYSTEM. DISCONNECTED AND RECONNECTED BOTH EMERGENCY BATTERIES IAW EMB-505 AMM 33-52-01/400. / NO DEFECTS NOTED.

Part: BATTERY — DEFECTIVE (ZONE 200) · airframe 9,723 hrs · 7,673 cycles

CABIN EMERG LIGHT: EMERGENCY LIGHTS STAYING ON IN THE ARM POSITION. EVEN WITH ENGINES RUNNING. CORRECTIVE ACTION: REPLACED BOTH THE FWD AND AFT EMERGENCY BATTERIES IAW EMB-505 AMM 33-52-01. OPS CHECK GOOD AT THIS TIME

Part: DRAIN — BROKEN (ZONE 100) · airframe 9,701 hrs · 7,655 cycles

HAD A NOTICABLE VIBRATION IN FLIGHT IN COCKPIT. WAS MORE NOTICABLE ON LEFT SIDE OF COCKPIT. SPEED OF AIRCRAFT SEEMED TO CHANGE THE SOUND AS WE GOT FASTER. SOUND SEEMED HARMONIC. FOUND THE FWD CHIN FARING FILET SEAL MISSING RTV UNDERNEATH THE SEAL APPLIED RTV AS NEEDED UNDER FWD CHIN FARING FILET SEAL WORK PERFORMED IAW SRM CH.51-21-00 . PERFORMED REPAIR ON FWD FILLET FAIRING CENTER, LH & RH SEAL, ALL WORK DONE IAW E50-20-0001_1.REPLACED BROKEN FWD FUSELAGE DRAIN. WORK PERFORMED IAW PHENOM 300 AMM CH.53-05-00.OPS CHECK GOOD

Part: BATTERY — FAILED (ZONE 200) · airframe 9,097 hrs · 7,173 cycles

ABOUT 45 MIN INTO FLIGHT CABIN EMERGENCY LIGHTS STARTED FLASHING, FLASHING BECAME FASTER AS FLIGHT WENT ON. ON GROUND AFTER SHUTDOWN AND TURNING OFF AND BACK ON EMER LIGHTS DID NOT FLASH. CORRECTIVE ACTION: REMOVED AND REPLACED FWD AND AFT E BATTERY. REMOVED FWD PN 7450LS-00 S/N 001052M AFT PN 7450LS-00 S/N 001475M

Part: MOTOR — DEFECTIVE (ZONE 300) · airframe 8,312 hrs · 6,541 cycles

VENTRAL RUD FAIL WHITE CAS: DURING ENROUTE CLIMB AT ABOUT FL350 WE GOT AN INTERMITTENT VENTRAL RUD FAIL WHITE CAS WHICH THEN STAYED ON PERMANENTLY UNTIL LANDING. WE LEVELED OFF AT FL380 AND MAINTAINED APPROXIMATEY 210KTS INDICATED FOR THE REST OF THE FLIGHT. REMOVED AND REPLACED WITH C/P REPAIRED SERVO MOTOR IAW AMM 22-11-11. OPS CHECK COMPLETED OK PERFORMED SERVO LOG DOWNLOADS AND SENT TO CONTACT CENTER FOR REVIEW. REF AMM 31-41-05 CONTACT CENTER RESPONDED BACK THE FOLLOWING "PERFORM THE ELECTRICAL CHECKS GIVEN ON THE SUBTASK 810-110-A & SUBTASK 813-138-A, IF NO DISCREPANCY IS NOTED ON THE CHECKS, REPLACE AUTOPILOT VENTRAL-RUDDER SERVO ACTUATOR". REMOVED CONNECTOR J1415 AND CHECK POWER AT PINS N AND P. 28VDC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,540 hrs · 8,310 cycles

FLAP FAIL YELLOW CAS: DURING FLIGHT RECEIVED SWPS FAULT FLAP FAIL PTRIM BKP FAIL SPOILER FAULT VENTRAL RUDER FAIL PERFORMED APPROPRIATE CHECK LIST AND LANDED IN PBE. SUGGESTED TO SWAP FCE 1 AND FCE 2. REMOVED SERVICEABLE FCE 1 (LH) AND INSTALLED IN POSON 2. REMOVED SERVICEABLE FCE 2 (RH) AND INSTALLED IN POSITION 1 IAW AMM 27-03-01. COMPLETED RIGGING OF FLAP SYSTEM AFTER SWAPPING FCE'S AND COMPLETED OPS CHECK. IAW MM 27-50-00. NO DEFECTS NOTED AND NO CASS MESSAGES DURING OPS CHECKS IAW 27-50-00.

Part: BATTERY PACK — DEFECTIVE (ZONE 100) · airframe 7,851 hrs · 6,169 cycles

CABIN EMERG LIGHT: C CAME ON STEADY AND THEN STARTED FLASHING. REMOVED FAULTY #1 EMERGENCY BATTERY AND REPLACE WITH "MODIFIED" EMERGENCY BATTERY. PERFORMED SATIFACTORY OPERATION CHECK. REF AMM 33-52-01.

Part: NONE — NONE · airframe 7,602 hrs · 5,977 cycles

EMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ON WITH THE EMER LT SWITCH IN THE ARM POSITION.

Part: BATTERY — DISCHARGED (ZONE 900) · airframe 7,602 hrs · 5,977 cycles

EMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ON WITH THE EMER LT SWITCH IN THE ARM POSITION. *** CORRECTIVE ACTION *** TROUBLESHOT AND REMOVED DEFECTIVE #2 EMERGENCY BATTERY AND REPLACED WITH CUSTOMER SUPPLIED MODIFIED EMERGENCY BATTERY IAW EMB-505 AMM 33-52-01. OPS CHECKED GOOD NO DEFECTS NOTED AT THIS TIME.

Part: NONE — DEFECTIVE (ZONE 800) · airframe 7,123 hrs · 5,583 cycles

MAIN DOOR LOCK: MAIN CABIN DOOR LOCK STUCK IN THE LOCKED POSITION. CANNOT OPEN THE MAIN CABIN DOOR FROM OUTSIDE AIRCRAFT. // SIGNOFF// REMOVED MAIN ENTRY DOOR LOCK KIT P/N: 505-09737-901, S/N: N/A. INSTALLED "NEW" MAIN ENTRY DOOR LOCK KIT P/N: 505-09737-901, S/N: N/A. OPERATIONAL CHECK GOOD. WORK PERFORMED IAW EMBRAER PHENOM 300 AMM CHAPTER 52-11-26.

Part: LENS — DEFECTIVE · airframe 6,626 hrs · 5,188 cycles

MAIN DOOR VISUAL INDICATOR: MAIN CABIN DOOR LOCK INDICATION VISOR (LENS) IS MISSING.//CORRECTIVE ACTION// CLEANED AREA OF MISSING VISOR AND INSTALLED NEW VISOR.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 5,931 hrs · 4,661 cycles

CABIN EMERG LIGHT: ON DESCENT INTO KEGE WE NOTICED THAT THE CABIN EMER LIGHTS WERE FLASHING.WE RECYCLED THE EMER LIGHT SWITCH BUT IT CONTINUED TO FLASH WITH THE SWITCH IN THE ARM POSITION. // SIGNOFF// TRIED SWITCHING- EMER LIGHTS TO ARM AND THEY WERE FLASHING . GAINED ACCESSED TO FRONT AND BACK EMER BATTERY'S. PARTS ON ORDER. 7/24/2021 OS REMOVED #1 FWD ERNER BATTERV. INSTALLED NEW #1 FWD ERNER BATTERV IAW EMB-505 AMM CH 33-52-01 REMOVED #2 AFT BATTERV. INSTALLED NEW #2 AFT ERNER BATTERY IAW EMB-505 AMM CH 33-52-01. OPS CHECK GOOD IAW EMB-505 AMM CH 33-52-00

Part: BALANCE WEIGHT — CORRODED · airframe 4,762 hrs · 3,754 cycles

LEVEL 1 CORROSION FOUND ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS. REMOVED LEVEL 1 CORROSION ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS IN ACCORDANCE WITH EMBRAER SB 505-55-A004 REV 5 "MASS BALANCE AND ATTACHMENT PARTS -(INSPECTION)"PARTS I,II,III,IV,V,VI". NO FLIGHT CONTROL WEIGHT CHANGES AT THIS TIME.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 3,554 hrs · 2,783 cycles

RECEIVED A FLAP FAIL, SWPS FAULT, PTRIM BKP FAIL, AND SPOILER FAULT CAS MESSAGES ALONG WITH MAX SPD ABOVE THE AIRSPEED TAPE AND A DATA PATH HAS FAILED MESSAGE ON THE GTC. HAD AN X OVER THE FLAP INDICATION ON THE MFD. ALL THIS CAME ON AT THE INSTANT THE VS MODE SELECTOR WAS PUSHED TO DESCEND FROM ALTITUDE. PERFORMED FIM 27-03-00-810-811A WITH NO DEFECTS NOTED. CONSIDERED TO BE A TRANSITORY CONDITION.

Part: UNKNOWN — ODOR (CABIN) · airframe 3,374 hrs · 2,643 cycles

DETECTED A BURNING ODOR IN THE COCKPIT, SHORTLY AFTER TAKEOFF WITH THE COCKPIT TEMP CONTROL ABOUT 10 O'CLOCK. NOTICED A BURNING RUBBER ODOR. WE PUT THE TEMP CONTROL TO FULL COLD AND THE ODOR STARTED TO DISSIPATE. WENT TO FULL COLD AND THE ODOR EVENTUALLY WENT AWAY. AT CRUISE, PUT THE TEMP CONTROL TO 8 O'CLOCK AND THE ODOR CAME BACK THROUGH APPROXIMATELY 18,000 FT WITH CLIMB POWER SET. AT ALTITUDE THE ODOR EVENTUALLY WENT AWAY. PERFORMED SMOKE & ABNORMAL ODOR IN THE CABIN & COCKPIT, FIM 21-20-00-810-801-A, IAW FIM 21-20-00. ALL CHECKED GOOD WITH NO DEFECTS NOTED.

Part: VALVE — BROKEN (RAM AIR) · airframe 3,149 hrs · 2,472 cycles

IN CRUISE AT FL410 WHEN DUCT 2 OVERTEMP CAS ILLUMINATED. FOLLOWED CHECKLIST PROCEDURES BUT DUCT TEMP CONTINUED TO RISE, ULTIMATELY REACHING 232F. AFTER APPROXIMATELY 2 MINUTES, DUCT 1 OVERTEMP ALSO ILLUMINATED. AS WE DESCENDED THROUGH FL 240, TEMPS BRIEFLY STABILIZED, BUT DUCT 1 TEMP THEN STARTED CLIMBING AGAIN. MADE PRECAUTIONARY LANDING. FOUND RAM AIR VALVE BROKEN. REMOVED AND REPLACED RAM AIR VALVE ASSY WITH REPAIRED UNIT IAW AMM 21-23-03-400-801-A.

Part: GENERATOR — FAILED (RIGHT) · airframe 367 hrs · 276 cycles

AFTER LEFT ENGINE START WITH NO GPU ASSIST, RIGHT GEN FAIL CAS CAME ON. ELECTRIC SYNOPTIC SHOWED RIGHT GEN OFF. ALSO HAD ELECTRIC OZONE ODOR IN CABIN. REMOVED AND REPLACED THE RT GENERATOR WITH AN OVERHAULED UNIT IAW AMM 24-31-01. OPS CHECKED GOOD IAW AMM 24-31-00. PERFORMED FIM TASK 21-20-00-810-801-A. NO SMOKE OR ABNORMAL ODORS AT THIS TIME.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 11,060 hrs · 8,888 cycles

ACFT DID NOT PRESSURIZE ON DEPARTURE. GROUND RAN AIRCRAFT CK LEFT AND RIGHT ENGINE SEPARATELY FOR PRESSURIZATION. OPS CK GOOD. CHECK PRE PRESS. OP'S CK GOOD. INSPECTED AND OP'S CK WOW SWITCH OP'S CK GOOD. NO DEFECTS NOTED ON GROUND IAW CESSNA 560 MM CH 21-31-00.

Part: LINE — CONTAMINATED (DOOR SEAL) · airframe 11,059 hrs · 8,886 cycles

EMERGENCY DECLARED, LOST PRESSURIZATION WHILE IN CRUISE AT FL390. HEARD AUDIBLE "POP" FOLLOWED BY AIR "HISSING" AND CABIN CLIMBING AT >4000 FPM. CABIN ALT REACHED 10000 FEET. DEPLOYED MASKS MANUALLY FOR ELDERLY PAX. PERFORMED EMER DESCENT CABIN REMAINED NEAR 10000 FT TILL PASSING FL240 IN THE DESCENT. INSPECTED CABIN PRESS SYSTEM FOUND SMALL AMOUNT OF WATER IN DOOR SEAL LINES ALONG WITH TORN DOOR GROMMET. PURGED SYSTEM WITH NITROGEN AND REPLACED GROMMET. COMPLIED WITH PRESSURE CHECK INSIDE. OPS CK GOOD. GROUND RUN AIRCRAFT OPS CK GOOD.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 11,039 hrs · 8,871 cycles

WINDSHIELD OVERHEAT ANNUNCIATOR ILLUMINATED WITH WINDSHIELD HEAT SELECTED ON IN THE LOW POSITION. RAN CHECKLIST AND SELECTED OFF. CONDITION OCCURED ABOUT 30 TO 60 SECONDS AFTER SELECTING ON. HOT BURNING ODOR WAS PRESENT.KSPI-KLAL. TROUBLESHOT PROBLEM DOWN TO A BLOWN FUSE INSIDE OF WINDSHIELD TEMP CONTROLLER. REMOVED CONTROLLER P/N 9912085-6 S/N 9AV134 AND INSTALLED NEW CONTROLLER PIN 9912085-6 S/N 8BC167 IAW CESSNA CITATION 560 AMM SECTION 30-41-02. OPS CHECK SATISFACTORY.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,766 hrs · 8,647 cycles

STRONG BURNING ODOR ENCOUNTERED IN FLIGHT. TURNED OFF AIR CONDITIONER AND ODOR DISSIPATED. INSPECTED FWD AND AFT AIR CONDITIONING EVAPORATOR UNITS FOR BURNING SMALL AND SIGNS OF DAMAGE. CHECKED RESISTANCE OF FAN SPEED RESISTORS, BOTH READ 1.8 OHM NO SIGNS OF BORING ODOR OR DAMAGE NOTED. INSPECTED TAIL CONE ACM AND FREON COMPRESSOR UNITS AND DRIVE BELT. NO SIGNS OF DAMAGE NOTED. APPLIED ELECTRICAL LOADS TO AVIONICS SYSTEMS, RADIOS, LIGHTS, MFD, PFD'S, AIR CONDITIONING SYSTEMS, ETC. WITH ENGINES RUNNING FOR MORE THEN 20 MINUTES. NO SIGNS OF BURNING ODOR WAS NOTED.

Part: MASTER CYLINDER — LEAKING (BRAKES) · airframe 10,734 hrs · 8,623 cycles

DURING AIRCRAFT TAXI, CAPTAINS AND F/O RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE F/O PEDAL WENT TO THE FLOOR CAPTAINS SIDE WENT DOWN 2-3 INCHES. T/S AND FOUND RT CO-PILOTS MASTER CYLINDER LEAKING INTERNALLY REMOVED AND REPLACED CO-PILOTS LT AND RT MASTER CYLINDER TO BLED AND LEAK CHECKS WERE GOOD IAW MM 32-42-02.

Part: BRAKE ASSY — WEAK (MLG) · airframe 10,732 hrs · 8,618 cycles

DURING AIRCRAFT TAXI, CAPTAINS SIDE RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE, PEDAL GOES IN ABOUT 2 INCHES FARTHER, THEN SEEMS TO PRESSURIZE AND EXTEND BRAKE TO NORMAL POSITION. [07-13-07] INSPECTED RUDDER TORQUE TUBE, RUDDER PEDAL ATTACHMENTS AND CONNECTED HARDWARE FOR SECURITY AS REQUESTED. NO DEFECTS. PERFORMED AN ANTISKID BRAKE SYSTEM BLEEDING. OPERATIONAL CHECKS NORMAL. NO LEAKS NOTED. PERFORMED IAW THE CE560 M/M CHAPTER 32-42-00.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 10,523 hrs · 8,444 cycles

RT ENG SPOOLED DOWN TO 10-15 PERCENT N1 APPROX 2 MIN AFTER START WITH NO THROTTLE MOVEMENT, RAPID INCREASE IN ITT AT THE SAME TIME BUT NOT ABOVE LIMITATIONS. ALSO, ENG STARTED ON THIRD ATTEMPT, NO FUEL SPILL. REMOVED FUEL INLET LINE TO FLOW DIVIDER & MOTORED ENG OVER. FUEL SPRAYED OUT AT HIGH VOLUME. PERFORMED 2 NORMAL ENG STARTS AND TOOK ENG TO N1 OF THE DAY. ALL READINGS NORMAL. WAITED A HOUR & TOOK ENG TO N1 OF THE DAY AGAIN WITH NORMAL RESULTS. VISUALLY INSPECTED ALL ADJUSTMENT POINTS FOR SECURITY. RECOWLED NR 2 ENG & PERFORMED 1 MORE START & VERIFIED BOTH ENG STARTED NORMALLY, NO ERRATIC READINGS. COULD NOT DUPLICATE SQUAWK. WORK DONE IAW CITATION 560 AMM SECTION 73-10-00, PWA JT15-5D EMM 3040342.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 10,282 hrs · 8,273 cycles

PILOTS (LT) O2 MASK WILL NOT WORK IN EMERG NR O2 FLOW. REMOVED AND REPLACED O2 MASK. OPS CHECK GOOD IAW MM CH 35-10-01.

Part: ACTUATOR — INTERMITTENT (RT MLG) · airframe 10,165 hrs · 8,186 cycles

ON APPROACH TO KLUK, RT MAIN GEAR LIGHT WAS INOP. WENT AROUND AT ALT. DID EMERG CHECKLIST AND TROUBLESHOT. SPEED BRAKES, FLAPS PAST 35*, NO LIGHT ROTARY TEST DID NOT COME ON. CALL CMH CONFIRMED ALL STEPS COMPLETED, WENT AHEAD AND FINISHED CHECKLIST. INCLUDING GEAR BLOW DOWN. DECLARED EMERG AND LANDED ON 2IL, NO PROBLEM STOPPING PLANE, HAD A/C TOWED TO HANGER. T/S AND FOUND RT MLG ACTUATOR DOWN AND LOCK SWITCH INTERMITTENT. REMOVED AND REPLACED WITH A REPAIRED ACTUATOR ASSY. PERFORMED OPERATIONAL CHECKS AND LEAK CHECKS. OPERATIONAL CHECK GOOD. NO LEAKS NOTED. PERFORMED CONTOUR CHECK CAMBER CHECK GOOD IAW 560 M/M 32-11-01 IAW CE560 M/M 32-31-04

Part: POTENTIOMETER — MALFUNCTIONED (INDICATOR LIGHTS) · airframe 10,122 hrs · 8,149 cycles

PUT GEAR DOWN NO RIGHT GEAR LIGHT, NO RED LIGHT. NO SECONDARY GEAR UNSAFE INDICATIONS. TROUBLESHOT, TURN DAY/NIGHT DIMMER SWITCH ON/OFF GOT ALL THREE GREEN INDICATION ON GEAR. RECYCLED GEAR AND NO MAIN LIGHT. PROBLEM APPEARS TO BE WITH DIMMER. BLEW DOWN USING EMERGENCY PROCEDURES IN CHECKS. JACKED AIRCRAFT. CYCLED GEAR 15 TIMES BLED SYSTEM AND OPERATED LIGHTING DIMMER. SERVICED EMERGENCY BOTTLE, OPS CHECKED GOOD IAW CESSNA M/M CH 32-01-00.

Part: INDICATOR — UNKNOWN (COCKPIT) · airframe 10,052 hrs · 8,090 cycles

DURING TAKEOFF, LEFT SIDE AIRSPEED LAG BEHIND RIGHT AIRSPEED, SUBSEQUENT "INASP" IN YELLOW ILLUMINATED, ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. SUSPECT WATER WAS IN PITOT LINES. NO WATER WAS DETECTED. RAN AIRSPEED UP AND DOWN RAPIDLY WITH NO SPLIT IN INDICATION. SYSTEM OPS CHECKS GOOD. REFERENCE CESSNA 560 MAINTENANCE MANUAL 34-11-10.

Part: SEAL — LEAKING (PAX DOOR) · airframe 9,940 hrs · 7,988 cycles

LOST CABIN PRESSURE AT FL 400. REMOVED & REPLACED SECONDARY DOOR SEAL. DOOR SUPPLY GROMMET & CHECK VALVE IAW CESSNA 560 M/M CHPT. 52-10-01, 52-10-00 & 21-30-00. SYSTEM OPS & LEAK CHECKS GOOD.

Part: BATTERY — OVERTEMP (MASTER) · airframe 9,326 hrs · 7,452 cycles

BATTERY OVERTEMP AT 145 DEGREES STEADY, ANNUNCIATOR LIGHT ILLUMINATED, DELARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.

Part: PRESSURE SYSTEM — FLUCTUATES (CABIN) · airframe 9,030 hrs · 7,210 cycles

WILD PRESSURIZATION FLUCTUATIONS ON TAKEOFF SHORTLY FOLLOWED BY A PECULIAR ODOR. PRESSURE FLUCTUATIONS APPEARED TO BE ASSOCIATED WITH POWER CHANGES. ITEM IS UNDER INVESTIGATION.

Part: BULB — BURNED OUT (MLG INDICTOR) · airframe 8,672 hrs · 6,918 cycles

RIGHT MAIN GEAR INDICATOR LIGHT INOP, EMERGENCY/ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTING AND RAN LANDING GEAR WILL NOT EXTEND CHECKLIST, FOUND THE MLG LIGHT BULBS BURNED OUT. REMOVED AND REPLACED RIGHT MAIN GEAR INDICTING LIGHT IAW CESSNA CE-560 MM 33-11-01.

Part: IGNITER — FAILED (ENGINE) · airframe 8,245 hrs · 6,559 cycles

ON FIRST ATTEMPT RT ENGINE WOULD NOT LIGHT, ON SECOND ATTEMPT ENGINE LIGHT OFF AND STARTED. AFTER ENGINE START, WHILE AT IDLE THE RT ENGINE FLAMED OUT PRIOR TO TAXI. FOUND IGNITER FIRES INTERMITTENTLY REPLACED INBOARD IGNITER AND FOUND THROTTLE NOT RIGGED CORRECTLY, RE-RIGGED THROTTLE AND ALL OPS CHECK GOOD. ALL WORK DONE IAW JT15D-5D MM CHAPTER 74-20-02 AND CESSNA 560MM CH 76-11-00.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 8,152 hrs · 6,480 cycles

DURING EMERGENCY EGRESS TRAINING, FOUND EMERGENCY EXIT DOOR WOULD NOT OPEN. FOUND SEALANT BONDED TO EXIT STRUCTURE. REMOVED EXIT AND CLEANED SEAL, REMOVED AND REINSTALLED EMERGENCY EXIT SEVERAL TIMES, OPS CHECK GOOD IAW CESSNA 560 MM CHAPTER 52-20-01.

Part: BULB — INOPERATIVE (MLG INDICATOR) · airframe 7,842 hrs · 6,243 cycles

DURING APPROACH AT TEB LT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED, EXTENDED GEAR WITH PNEUMATIC BLOW DOWN SYSTEM. REMOVED 4 INOPERATIVE LIGHT BULBS AND INSTALLED 4 NEW BULBS IAW CE560 MM CHAPTER 33-13-01. BLED GEAR HYDRAULIC SYSTEM, PERFORMED OPS CHECK IAW CE-560 MM CHAPTER 32-01-00. OPS CHECKED GOOD.

Part: PANEL — MALFUNCTIONED (EMERG EXIT)

DURING INSPECTION, ATTEMPTED TO REMOVE THE EMERGENCY EXIT DOOR. FOUND NUMEROUS PROBLEMS. EXTERIOR HANDLE ROTATION DIFFICULT. HATCH HAD TO BE HIT HARD AT TOP TO MAKE IT RELEASE FROM OPENING. DETERMINED RUBBER SEAL THAT IS GLUED TO DOOR WITH 1300L, WAS ADHERED TO 890 THAT IS UTILIZED TO CREATE A BETTER PRESSURIZATION SEAL. CAUSED SITUATION WHEREAS DEALING WITH THE SEAL BECAME A PART OF THE OPERATION TO REMOVE THE EMERG EXIT. ALSO, INTERIOR TRIM PIECE THAT IS VELCROED INTO PLACE WAS TRAPPED IN PLACE WITH SEAT IN OTBD POSITION. THIS TRIM PIECE BLOCKED 6-8 INCHES OF THE LOWER PORTION OF THE EXIT OPENING.