N387QS

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 16,743 hrs · 11,235 cycles

EMERGENCY LTS FAILED FIRST FLIGHT TEST. CORRECTIVE ACTION: TECHS FOUND THE EMERGENCY LIGHTS LIGHTS ASSOCIATED TO BATTERY PACKS #1 & #3 INOP. MCC REQUEST TECHS CHANGE ALL 4 BATTERY PACKS PACKS. TECHS REMOVED AND REPLACED ALL 4 EMERGENCY LIGHT BATTERY PACKS PER CE-680 AMM 33-50-10. NO FURTHER DEFECTS NOTED. ALL EMERGENCY LIGHTS ARE NOW OPERABLE AS DESIGNED. TECHS ALLOW THE BATTERY PACKS TO RECHARGE VIA APU POWER DUE TO FBO CONSTRAINTS NOT HAVING A GPU AVAILABLE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 16,743 hrs · 11,235 cycles

EMERGENCY LIGHTS FAILED FIRST FLIGHT CHECK. BATTERIES OFF, EMER LTS IN ARM; NO EMERGENCY LIGHTE TURNED ON. WHEN SELECTOR PLACED TO ON HALF OF THE REQUIRED LIGHTS CAME ON. CORRECTIVE ACTION: TECHS ARRIVED TO AIRCRAFT AND FOUND THE OUTSIDE WING LIGHT INOP AND THE CABIN INTERIOR PATH LIGHTS INOP MCC REQUEST TECHS TO COMPLY WITH TC-FLT-33-1001 TO PERFORM A RECHARGE OF OUR EMERGENCY BATTERY PACKS. NO CHANGE AFTER COMPLING WITH TASK CARD. TECHS REMOVED THE #3 EMERGENCY BATTERY PACK AND INSTALLED AN OPERATOR SUPPLIED REPAIRED UNIT PER CE-680 AMM 33-50-10. NO FUTHER DEFECTS NOTED

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 16,563 hrs · 11,108 cycles

DURING POWER-ON CHECK DISCOVERED EMERGENCY EXIT SIGN ABOVE SEAT 9 INOP. FOUND BROKEN WIRE AT SPLICE CRIMPED NEW PIN AND INSTALLED NEW SPLICE. OPS CHECK GOOD PER AMM 33-50-00.

Part: SPAR — CORRODED (ZONE 600) · airframe 16,497 hrs · 11,059 cycles

CORROSION ON RH WING AFT SPAR WEB AROUND THE INBD SPOILER HYD LINE CARRY THRU FITTINGS

Part: TRUNNION — CORRODED (ZONE 700) · airframe 16,497 hrs · 11,059 cycles

LH MLG TRUNNION HAS AREA OF CORROSION AROUND ADEL CLAMP FOR BRAKE LINES.

Part: SPAR — CORRODED (ZONE 500) · airframe 16,497 hrs · 11,059 cycles

LH MLG WHEEL WELL AFT SPAR LOWER CLIP HAS EXFOLIATED CORROSION.

Part: SKIN — CORRODED (ZONE 100) · airframe 16,042 hrs · 10,751 cycles

CORROSION FOUND AT BL 0.00 AFT OF AFT FUSELAGE FARING WHERE BELLY FAIRINGS JOIN TOGETHER.

Part: DOOR — CORRODED (ZONE 800) · airframe 16,042 hrs · 10,751 cycles

CORROSION FOUND ON LH MLG DOOR ON LOWER FWD CORNER AND ALONG FWD EDGE OF DOOR. REMOVED AND REINSTALLED FASTENERS TO ACCESS CORROSION SURROUNDING RIVET TAILS. BLENDED AND REMOVED CORROSION FROM 5 EACH LOCATION ON INNER SURFACE OF LH MLG DOOR AT LOWER FWD AND AFT LOCATIONS. NDT CORROSION REMOVAL CHECK AND REMAINING THICKNESS CHECK AT BLEND LOCATIONS. COMPLIED WITH RFTS-112279 REV O, N387QS(680-0119) LH AND RH MLG DOOR CORROSION DATED 22NOV24. THIS IS A PERMANENT MINOR REPAIR.

Part: DOOR — CORRODED (ZONE 800) · airframe 16,042 hrs · 10,751 cycles

CORROSION FOUND ON RH MLG DOOR ON LOWER FWD CORNER AND ALONG THE FWD EDGE OF THE DOOR. REMOVED AND REINSTALLED FASTENERS TO ACCESS THE CORROSION SURROUNDING RIVET TAILS. BLENDED AND REMOVED CORROSION FROM 5 EACH LOCATION ON INNER SURFACE OF RH MLG DOOR AT LOWER FWD AND AFT LOCATIONS. NDT CORROSION REMOVAL CHECK AND REMAINING THICKNESS CHECK AT BLEND LOCATIONS . COMPLIED WITH RFTS-112279 REV 0, N387QS(680-0119) LH AND RH MLG DOOR CORROSION DATED 22NOV24. THIS IS A PERMANENT MINER REPAIR.

Part: SKIN — CORRODED (ZONE 300) · airframe 16,042 hrs · 10,751 cycles

LH AND RH HORIZONTAL STABILIZER CORROSION.

Part: SKIN — CORRODED (ZONE 300) · airframe 16,042 hrs · 10,751 cycles

CORROSION FOUND ON VERTICAL STAB AT RH TOP. BLENDED AND REMOVED CORROSION FROM VERTICAL STAB AT RH TOP LOCATION TILL VISUALLY REMOVED, VERIFIED WITH 10X MAGNIFYING GLASS. COMPLIED WITH ERO-982547 REV. IR, DATED NOV. 25, 2024. N387QS VERTICAL STABILIZER RH SKIN CORROSION. THIS IS A MAJOR REPAIR.

Part: COUNTERBALANCE — OUT OF RIG (PAX DOOR) · airframe 15,328 hrs · 10,220 cycles

THE MAIN DOOR IS EXCESSIVELY HARD TO OPEN AND SLAMS CLOSED ONCE PAST THE 2/3 POSITION IN CLOSING. PERFORMED THE COUTERBALANCE SYSTEM RIGGING OF THE MAIN CABIN DOOR. ADJUSTED THE TENSION UNTIL SATISFACTORY AND WITHIN LIMITS. OPS CHECK GOOD. NO DEFECTS NOTED. ALL WORK DONE IAW CE-680 AMM 52-10-50.

Part: SKIN — CORRODED (ZONE 200) · airframe 15,293 hrs · 10,194 cycles

REPAIR OF UPPER FUSELAGE SKIN CORROSION. REPORT NO. ERO-978708 DATED JAN. 27, 2024 WITH FAA FORM 8110-3.

Part: WEB — CRACKED (ZONE 100) · airframe 15,293 hrs · 10,194 cycles

NOSE WHEEL WELL PANEL CRACK. REMOVED DAMAGED AREA AND ACCOMPLISHED NDI TO CONFIRM DAMAGE HAS BEEN REMOVED. FABRICATED DOUBLER AND FILLER SHIM AND ATTACHED USING OEM BLUEPRINT FASTENERS. ALL WORK ACCOMPLISHED IAW NETJETS RFTS-109815 DATED: 08JAN2024.

Part: STRUT — BROKEN (ZONE 800) · airframe 15,208 hrs · 10,131 cycles

AFT MAIN TELESCOPIC ROD IS UNSEATED AND NOT SUPPORTING THE DOOR. /INSPECTED MAIN ENTRY DOOR AFT TELESCOPIC SUPPORT STRUT AND FOUND THE LOWER END OF THE UPPER BARREL PORTION PULLED THROUGH. ATTEMPTED TO REPLACE DOOR STRUT AND FOUND SUPPORT STRUT PIN SEIZED INTO SUPPORT BRACKET. PLACED ADDITIONAL PARTS ON ORDER. RETURNED NEXT DAY DUE TO PARTS ETA. REMOVED AND REPLACED MAIN ENTRY DOOR SUPPORT STRUT, SUPPORT BRACKET, DOOR SUPPORT PIN AND ASSOCIATED HARDWARE. COMPLIED WITH ADJUSTMENT/TEST OF AFT DOOR SUPPORT. NO OTHER DEFECTS NOTED. CLOSED ALL ACCESS AND PERFORMED NUMEROUS OPSCHECKS OF DOOR WITHOUT ISSUE. WORK PERFORMED IAW AMM 52-10-30.

Part: DOOR — CORRODED (ZONE 800) · airframe 14,973 hrs · 9,971 cycles

THREE AREA OF CORROSION FOUND ON THE EMERGENCY EXIT DOOR. TEXTRON AVIATION CE-680 FIELD REPAIR SR-680-ATA52-18636 STANDARD REPAIR-CORROSION, ESCAPE HATCH DOOR, SKIN WAS ACCOMPLISHED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,319 hrs · 9,530 cycles

POST-FLIGHT - EXTERIOR EMERGENCY LIGHT THAT IS LOCATED INSIDE THE RH LANDING LIGHT HOUSING ("SHARK LIGHT") IS INOP. GAINED ACCESS TO SHARK UGHT. REMOVED DEFECTIVE SHARK LIGHT BULB P/N: 1495 NSN, INSTALLED NEW CUSTOMER SUPPUED SHARK LIGHT BULB P/N: 1495X NSN. PERFORMED OPS CHECKS, OPS CHECK GOOD,NO DEFECTS NOTED. CLOSED UP ALL PREVIOULSY GAINED ACCESS. WORK DONE IAW CE680 AMM 33-50-04. ORIG SUB DATE: 10/28/2022

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,318 hrs · 9,529 cycles

THE EMERGENCY EXTERIOR LIGHT AND INTERIOR LIGHTS ASSOCIATED WITH THIS BATTERY PACK ARE NOT ILLUMINATING WITH THE EMERGENCY LIGHT SWITCH SELECTED ON. THE EMERGENCY EXTERIOR LIGHTS ARE CONSIDERED INOPERATIVE. PERFORMED FUNCTIONAL CHECK. UNABLE TO DUPLUCATE SQK. PERFORMED EMERGENCY BATTERY CAPACITY CHECK. ALL BATTERIES CAPACITY CHECK GOOD. WORK DONE IAW MAINTENANCE MANUAL (REV 31) 33-50-10.

Part: ROD END — BROKEN (ZONE 700) · airframe 14,248 hrs · 9,483 cycles

CLIMB PAST FL340, MLG UNLOCK LIGHT ILLUMINATED. NLG BEGAN TO REPEATEDLY CYCLE, ATTEMPTED UPLOCK. RESULTED IN A BANGING FROM NLG, MEASURABLE VIBRATION, & RESULTED IN INABILITY TO UTILIZE AUTOPILOT. DESCENDING THROUGH FL180, ISSUE CLEARED. ON GEAR EXTENSION, THREE GREEN, NO, LT, & RT, UNLOCK REMAINED EXTINGUISHED. APPROACH & LANDING NORMAL. FOUND A BROKEN BOLT ON LT LOWER ROD END ASSY. REMOVED & INSTALLED NEW ROD END ASSY. MEASURED DISTANCE BETWEEN FLATS OF UPPER & LOWER BARRELS ON NLG & FOUND IT TO BE 9.95" IAW MM 32-00-00, STEP 7. PERFORMED REPACK OF NLG, SWUNG GEAR, LEAK & OPS CHECKED GOOD. WORK DONE IAW CMM 32-20-01, AMM 32-00-00 & 32-20-00.

Part: NOT REPORTED — NOT REPORTED · airframe 13,375 hrs · 8,885 cycles

EMERGENCY LIGHT ON RIGHT WING INBOARD LEADING EDGE (SHARK LIGHT) IN-OP.///SIGN-OFF///REMOVED AND REPLACED BULB. IAW CE680 AMM 33-50-00. OPS CHECK GOOD.

Part: SEAL — DEFECTIVE (NLG) · airframe 12,938 hrs · 8,565 cycles

NLG LANDING GEAR EXTENSION: CLIMBING THROUGH FL230 AT 280 KTS WE HEARD A LOUD BANG, FOLLOWED BY A MODERATE VIBRATION AND THE RED NOSE GEAR UNLOCK WAS FLICKERING ON AND OFF. ON DESCENT BACK TO DEPARTURE POINT THE THE GEAR SEEMED TO RETRACT BACK UP INTO THE WELL AND THE UNLOCK EXTINGUISHED. LANDING GEAR EXTENDED NORMALLY FOR LANDING. // SIGNOFF // JACKED THE AIRCRAFT AND MEASURED THE NLG STRUT EXTENSION TO BE 10.18". THIS IS OVER THE SPECIFICATION OF 9.75+/-.078". THE NOSE STRUT NEEDS TO BE RESEALED. (TALKED TO IAN JENKINS AT NETJETS AND NETJETS WILL LET US KNOW IF THEY DESIRE COMPLIANCE WITH SL680-32-08-- NLG STRUT SEAL IMPROVEMENT.) PERFORMED GEAR SWING AND NOTED THAT ROLLER IS ON EDGE OF UPLOCK HOOK. THE UPLOCK SWITCH MAY HAVE BEEN ADJUSTED TO MATCH THE GEAR AT PRESENT LENGTH AND SO WILL NEED TO BE READJUSTED ONCE THE NLG IS RESEALED. REMOVED LH NOSE WHEEL P/N 3-1538-1 S/N 0630 AND RH NOSE WHEEL P/N 3-1538-1 S/N 1036. WHILE REMOVING NOSE GEAR LOWER BARREL, FOUND ORFICE COMPLETELY UNSCREWED FROM LOWER END OF UPPER BARREL. REMOVED LOWER BARREL P/N 6742170-6 S/N 367 AND DISSEMBLED. REMOVED OLD SEALS AND CLEANED PARTS. IAW CE680CMM 32-20-01. REPLACED ALL SEALS AND REASSEMBLED NOSE STRUT. C/W SL680-32-08 NOSE LANDING GEAR STRUT SEAL IMPROVEMENT. REPLACED RETAINER NUT P/N 6742172-6 DUE TO PITTING AND WEAR(INCLUDED IN SEAL MOD KIT P/N 6742160-200). INSTALLED LOWER BARREL ASSEMBLY P/N 6742170-6 S/N 367 IAW CMM 32-20-01.SERVICED STRUT WITH NITROGEN AND 5606 HYDRAULIC FLUID IAW MM 12-20-32. CLEANED AND LUBED WHEEL BEARINGS. INSTALLED LH WHEEL P/N 3-1538-1 S/N 0630 AND RH WHEEL P/N 3-1538-1 S/N 1036. TORQUED AND SAFETIED AXLE NUTS. INSTALLED HUB CAPS. IAW MM 32-41-10. COMPLIED WITH STEPS 1 THROUGH 15 OF THE NLG UPLOCK SWITCH ADJUSTMENT IAW MM 32-60-00. NEED TO PERFORM THE MLG SYSTEM UPLOCK SWITCHES OPERATION AL CHECKCOMPLIED WITH.

Part: STIFFENER — GOUGED (VERTICAL STAB) · airframe 12,176 hrs · 8,089 cycles

FOUND UPPER RT BOLT HOLE ON THE VERTICAL STABILIZER AFT SPAR STIFFENER GOUGED, BLENDED DAMAGED. REPLACED THE STIFFENER.

Part: SKIN — CORRODED (LT WING) · airframe 12,176 hrs · 8,089 cycles

REPAIRED CORRODED AREAS OF THE UPPER LT & RT WING SKINS LOCATED UNDER AND ADJACENT TO THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING AREA) BY REMOVING THE FORWARD, MIDDLE, AND AFT DRAG ANGLES ON BOTH WINGS FOR ACCESS, BENDING CORRODED AREAS, PERFORMING NDT, REPLACING FASTENERS AS REQUIRED, TREATING, PRIMING BLENDED AREAS AND REINSTALLING DRAG ANGLES IAW FIELD REPAIR. REPLACED THE EXISTING CORRODED RT UPPER INBOARD TRAILING EDGE WING SKIN WITH NEW P/N 6922681-70 PER SRM.

Part: SKIN — CORRODED (ENTRY DOOR) · airframe 12,176 hrs · 8,089 cycles

BLENDED CORRODED AREA OF THE MAIN ENTRY DOOR LOCATED NEAR THE DOOR HINGES ON THE INTERIOR SIDE OF THE DOOR SKIN, PERFORMED EDDY CURRENT AN ULTRASONIC INSPECTIONS AND REPORTED FOR REPAIR DISPOSITION. CLEANED AREA, TREATED PRIMED AND TOP COATED BLENDED AREAS PER REPAIR MEMO.

Part: TIP CAP — CORRODED (LT HORIZ STAB) · airframe 12,176 hrs · 8,089 cycles

BLENDED AREAS OF CORROSION ON THE LT UPPER HORIZONTAL STABILIZER TIP CAP AND THE RT LOWER HORIZONTAL STABILIZER TIP CAP, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIRED CLEANED TREATED PRIMED AND TOP COATED BLENDED AREAS PER REPAIR MEMO.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 11,470 hrs · 7,584 cycles

VERTICAL FIN LEADING EDGE DAMAGE. ACCOMPLISHED MANUFACTURER ENGINEERING LETTER DQ21778M1; 680-0119 VERTICAL FIN LEADING EDGE DAMAGE.

Part: LENS — DAMAGED (RT WING LIGHT) · airframe 11,470 hrs · 7,584 cycles

RIGHT WING INBOARD LEADING LIGHT COVER ATTACH HOLE DAMAGE (OVERSIZED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DATED JUNE 6, 2019 DQ21802M1; 680-0119 (N387QS) RIGHT WING INBOARD LEADING EDGE CUFF AND LIGHT COVER ATTACH HOLE DAMAGE (OVERSIZED).

Part: ANGLE — CRACKED (ROLL SPOILER) · airframe 10,779 hrs · 7,104 cycles

FOUND ROLL SPOILER MIXER SUPPORT STRUT ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 51-40-03.

Part: APU — FAILED (APU BAY) · airframe 6,698 hrs · 4,381 cycles

DURING START OF APU WITH BLEEDS ON, COCKPIT FILLED UP WITH THICK SMOKE. ISOLATED APU AND DETERMINED TO BE SOUCE OF SMOKE IN AIR CONDITIONING. REMOVED AND REPLACED APU, SERVICED AS REQUIRED AND OPS CHECKED. OPS AND LEAK CHECKED GOOD. ACCOMPLISHED IAW MM 49-10-00, 49-20-00 AND 12-11-03.

Part: STEERING UNIT — DEFECTIVE (NLG) · airframe 5,432 hrs · 3,565 cycles

RIGHT SIDE GEAR SLOW TO RETRACT. RT SIDE GEAR LIGHT REMAINED ILLUMINATED ABOUT 4-5 SECONDS LONGER THAN NORMAL AFTER GEAR HANDLE SELECTED UP. R & R THE STEERING UNIT IAW MM 32-50-00. OPS, LEAK, TRAVEL AND TAXI CHECKS GOOD.

Part: STEERING UNIT — FAILED (NLG) · airframe 5,432 hrs · 3,565 cycles

AFTER TAKEOFF, GEAR SELCETED UP AND RED UNLOCK LIGHT CAME ON - RT GEAR GREEN LIGHT REMAINED ON - LT GEAR AND NOSE LIGHTS WENT OFF. LIGHT CONDITION REMAINED UNTIL GEAR APPEARED UP AND UPLOCK LIGHT THEN UNLOCK AND ALL GREEN LIGHTS WENT OUT. APPROXIMATELY TEN SECONDS. REMOVED AND REPLACED THE STEERING UNIT IAW CE-680 MM 32-25-00. OPERATIONAL CHECK, LEAK CHECK, TRAVEL AND TAXI CHECKS GOOD.

Part: PCB — INOPERATIVE · airframe 5,191 hrs · 3,422 cycles

ALL LIGHTS FLICKERED, FOLLOWED BY MASTER CAUTION, SIMULTANEOUSLY WITH DC GEN OFF RT, PIT/ROLL DISCONNECT, DC EMER BUS RT, HYD VOL LOW, T/R UNLOCK RT, RT PFD BLANK, NAV/COM2, FMS 2 INOP, CYAN- GUST LOCK ON, WINDSHEAR FAIL, TERRAIN FAIL, GROUND PROX FAIL, MASTER CAUTION CYCLED WITH HYP VOL LOW CAS MESSAGE. WE HAND FLEW BECAUSE A/P AND Y/D DID NOT WORK AND NOSE WHEEL STEERING INOP. ACCESSED RT START/GEN GROUND LUG GT024, REMOVED TERMINAL INSPECTED GOOD, REINSTALLED AND TORQUED BOLT. DIODE CHECKED GOOD RT ELEC CONT RELAY DIODES DZ124 AND DZ122. INSPECTED GOOD LT, RT, EMER J-BOX COMPONENTS, AND ALL CONNECTIONS. IAW TEAM SOVEREIGN REQUEST, REPOSITIONED LT & RT START/GEN'S FOR MX CONVENIENCE, AND REPLACED RT PWR DIST PCB NZ203 WITH NEW. GROUND ENGINE RUN OPS CHECKS GOOD. WORK ACCOMPLISHED IAW THE MM CH 24-60-10 AND 80-10-00.

Part: RELAY — MALFUNCTIONED (APU) · airframe 5,180 hrs · 3,415 cycles

DC EMER R (AMBER) ILLUMINATED IN-FLIGHT AT FL330. COMPLETED THE EMERGENCY/ABNORMAL PROCEDURES CHECKLIST; "DC EMER BUSS L/R (TAB G3). WHEN REACHED THE "IF DISCHARGE LESS THAN 30 AMPS (FAULT ON MAIN BUS) TURN GEN SWITCH AFFECTED SIDE OFF". WHEN THE RT GEN SWITCH WAS TURNED OFF THE FOLLOWING LIGHTS ILLUMINATED ON THE EICAS. AMBER HYD CONTROL FAULT R, ENGINE CONTROL, PITCH ROLL DISCONNECT, DC GEN OFF R, DC EMER BUS R, THE CYAN GUST LOCK ON, WINDSHEAR FAIL, TERRAIN FAIL, GROUND PROX FAIL. THE MASTER CAUTION RESET WOULD CONTINUOUSLY RESET INFLIGHT BECAUSE OF THE HYD PRESS/VOL INDICATOR ON DU2 SCREEN FLICKERING ON AND OFF. THE FOLLOWING NR WERE DISPLAYED ON THE EICAS. DC VOLTS L 28, R 28, DC AMPS L 50, R 0, BATT VOLTS L 28, R 24, AMPS L 0, R -20, BATT TEMP L 11C, R 18C. HYD PRESS -VOL UNREADABLE; IT WAS FLUCTUATING. AND RT T/R "UNLK" LIGHT WAS ILLUMINATED INFLIGHT. WE HAND FLEW AS A/P AND Y/D NO LONGER WORKED. WE NO LONGER HAD NOSE WHEEL STEERING AFTER LANDING. SWAPPED KZ003 APU RELAY, WITH RT MAIN ELECTRICAL RELAY, PN K400B3C-05, SN CP-54013 IN REF TO MM 24-62-03 AND 49-00-01. OPS CHECKED GOOD.

Part: STEERING UNIT — INOPERATIVE (NLG) · airframe 4,674 hrs · 3,102 cycles

AFTER TAKEOFF NOSE GEAR REMAINED DOWN AND WOULD NOT RETRACT. EMERGENCY/ABNORMAL CHECKLIST COMPLIED WITH AND A NORMAL LANDING. FOUND NOSE GEAR WOULD NOT CENTER WHEN TURNED TO THE LT. TROUBLESHOT TO BAD NOSE WHEEL STEERING UNIT. REMOVED NOSE WHEEL STEERING UNIT FROM ACFT IAW MM 32-50-00. INSTALLED NOSE WHEEL STEERING UNIT IAW MM 32-50-00. ACCOMPLISHED GEAR SWING, NOSE OPS CHECK GOOD. TAXI CHECK GOOD IAW MM 32-50-00.

Part: TORQUE TUBE — BINDING (CONTROL COLUMN) · airframe 4,650 hrs

DURING INSPECTION, IT WAS DISCOVERED THAT THE ELEVATOR TORQUE TUBE, CONNECTED TO THE CONTROL COLUMNS, IS IMPACTING AND BINDING AGAINST A STRINGER AT FS 125.80, LOCATED BELOW THE PEDESTAL IN THE COCKPIT.

Part: ENGINE — LEAKING (RIGHT) · airframe 4,412 hrs · 2,922 cycles

UPON CLIMBOUT THROUGH 5000 FT CABIN AND COCKPIT STARTED TO FILL UP WITH FUMES AND SMOKE IRRITATING THE EYES AND THE BACK OF THE THROAT OF BOTH PILOTS. OXYGEN MASKS WERE DONNED AND BOTH ENGINE BLEED AIRS WERE TURNED TO THE OFF POSITION. AN EMERGENCY WAS DECLARED AND A SUCCESSFUL LANDING WAS ACCOMPLISHED AT TJSJ. REMOVED AND REPLACED RT ENGINE. WORK PERFORMED IAW AMM .71-00-30. ENGINE GROUND RUNS & LEAK CHECKS PERFORMED WITH NO DEFECTS NOTED. NO SMOKE OR OIL ODOR IN CABIN.

Part: ENGINE — SMOKE (RIGHT) · airframe 4,412 hrs · 2,921 cycles

AFTER TAKEOFF AND CLIMBING THROUGH ROUGHLY 10,000 FT, PASSENGER INFORMED US OF A BAD ODOR AND HAZE IN CABIN. BOTH CREW MEMBERS LOOKED BACK AND SAW A WHITE/BLUEISH HAZE ALONG WITH A STRONG PUNGENT ODOR THAT WAS DIFFICULT TO IDENTIFY. PASSENGER COMPLAINED OF BURNING TO EYES. COPILOT WENT BACK TO TRY TO IDENTIFY THE SOURCE. RAN ABNORMAL CHECKLIST FOR ENVIRONMENTAL SYS SMOKE AND ODOR OF UNKNOWN SOURCE. APU WAS OFF, PRESS SOURCE SELECTOR WAS SWITCHED TO LAND DIVERTED. R & R RT ENGINE IAW MM 71-00-30. OPS & LEAK CHECKED GOOD. NO ODOR IN CABIN.

Part: BLADE — BENT (RT ENGINE) · airframe 4,131 hrs · 2,756 cycles

AT THE MOMENT OF GEAR RETRACTION ON TAKEOFF, HEARD A LOUD POP AND A HUMMING NOISE BEGAN, GOT A MASTER WARNING AND AN ENGINE VIBRATION R CAS MESSAGE. PULLED THE POWER BACK AND THE CAS MESSAGE EXTINGUISHED. FOUND BENT FAN BLADE ON RT ENGINE. SUSPECT BIRD INGESTION INTO ENGINE CORE. BORESCOPE INSPECTION INDICATED BIRD WENT THRU BYPASS AND NOT CORE. MX CHANGED 3 FAN BLADES IAW 72-30-00. PERFORM RUNS IAW 72-00-00 AND FOUND SATISFACTORY.

Part: STRUT — DISCHARGED (NLG) · airframe 2,724 hrs · 1,788 cycles

DURING MLG RETRACTION, GEAR SLOW TO RETRACT. IN TRANSIT, UNLOCK LIGHT IS ON & GREEN LIGHTS EXTINGUISH. GREEN LT MLG LIGHT CAME BACK ON & NOISE HEARD FROM NOSE WHILE MLG REMAINED UNRETRACTED. UPON INITIAL MLG HANDLE RETRACTION, SOLENOID BRIEFLY PREVENTED MOVEMENT BEFORE ALLOWING MOVEMENT TO RETRACT POSITION DESPITE BEING IN WOW CONDITION. FOUND NLG STRUT LOW, UPPER CHAMBER AT 245 PSI SPEC IS 240 PSI. LOWER CHAMBER AT 0 PSI, SPEC IS 40 PSI. R & R LOWER CHAMBER SERVICE VALVE IAW MM 32-20-01, SERVICED NLG STRUT IAW MM 32-20-00. FOUND NLG SQUAT SWITCH OUT OF ADJUST. SWITCH 3/4 TURN PAST ENGAGEMENT, SPEC IS 3, RIGGED NLG SQUAT SWITCH IAW MM, GEAR SWINGS, OPS GOOD IAW MM 32-00-00.

Part: SWITCH — OUT OF RIG (NLG) · airframe 547 hrs · 383 cycles

WHEN RETRACTING THE LANDING GEAR, A LOUD RATTLING SOUND AND VIBRATION OCCURED AND THE LANDING GEAR WOULD NOT RETRACT. IT APPEARED TO COME FROM THE NOSE GEAR. ALL GREEN LIGHTS WENT OUT AND THE RED UNLOCK LIGHT REMAINED. ADDITIONALLY, THE AMBER WOW MISCOMPARE EICAS MSG ILLUMINATED. WHEN THE GEAR HANDLE WAS LOWERED TO THE EXTEND POSITION, ALL INDICATIONS WERE NORMAL AND ALL SYSTEMS WORKED NORMALLY ON LANDING. FOUND NOSE WOW SWITCH OUT OF RIG. ADJUSTED NOSE WOW SWITCH IAW CESSNA 680 MM 32-60-00. VERIFIED NO WOW MISCOMPARE EICAS MESSAGE. INTERROGATED CMC WOW PCB BOARDS WITH NO DISCREPANCIES NOTED.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 452 hrs · 309 cycles

LANDING GEAR DID NOT EXTEND NORMALLY, USING CHECKLIST TO EXTEND GEAR (EMERGENCY EXTENSION) 3 GREEN LIGHTS ILLUMINATED RED INTRANSIT LIGHT REMAINED ILLUMINATED. ON ROLLOUT, RUDDER PEDALS INEFFECTIVE FOR NOSE WHEEL STEERING. STEERING TILL OPERATED NORMALLY. FOUND LANDING GEAR CONTROL HANDLE INOP. REMOVED & REPLACED LANDING GEAR CONTROL HANDLE. IAW CE680MM 32-30-40