N999QS

Part: FAIRING — DAMAGED (LEFT) · airframe 14,848 hrs · 9,036 cycles

OVER-WING FAIRING (LEFT SIDE) DAMAGE (FASTENER HOLES OVERSIZED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ21615M1 DATED MAY 21, 2019; 750-0203 (N999QS) OVER-WING FAIRING (LEFT SIDE) DAMAGE (FASTENER HOLES OVERSIZED).

Part: SKIN — GOUGED (PAX DOOR) · airframe 14,848 hrs · 9,036 cycles

GOUGE DAMAGE, FUSELAGE, MAIN CABIN DOOR SKIN, FS 190.2 AND WL 143.5. ACCOMPLISHED REPAIR DEFINITION NO. FR-750-0203-6643 REV-, FIELD REPAIR - GOUGE DAMAGE, FUSELAGE, MAIN CABIN DOOR SKIN, FS 190.2 AND WL 143.5 - REPAIR DATED MAY 21, 2019- AND FAA FORM 8100-9 DATED MAY 21, 2019 WEIGHT AND BALANCE WAS NOT AFFECTED. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION UNDER REVISION# 106889.

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 14,848 hrs · 9,036 cycles

LEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER. DQ21738M1REVA (CORRECTED DQ NUMBER, TT AND TL); 750-0203 (N999QS) LEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK.

Part: SKIN — CORRODED (RT WING) · airframe 14,848 hrs · 9,036 cycles

REPAIR OF RT UPPER WING SKIN CORROSION. ENGINEERING LETTER DQ19545M1 DATED MAY 16, 2019.

Part: FITTING — GOUGED (CARGO DOOR) · airframe 14,848 hrs · 9,036 cycles

REPAIR TO BAGGAGE DOOR LINTEL GOUGE. REPAIR DEFINITION S-750-ATA53/07RD, 8110-3 DATED FEB. 5, 2007.

Part: DIFFUSER — CHAFED (ZONE 500) · airframe 14,848 hrs · 9,036 cycles

REPAIR TO LT AND RT INBOARD LEADING EDGE DIFFUSERS CHAFED (FROM ANTI-ICE VALVE). ENGINEERING LETTER DQ19428M1 REV A, DATED MAY 9, 2019.

Part: DOWNLOCK SWITCH — DEFECTIVE (MLG) · airframe 14,655 hrs · 8,920 cycles

RIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - ON DEPARTURE RIGHT MAIN LANDING GEAR DID NOT RETRACT. WHEN GEAR HANDLE SELECTED UP RIGHT MAIN DID NOT APPEAR TO MOVE AT ALL. RIGHT GREEN GEAR LIGHT REMAINED STEADY GREEN. RED UNLOCKED LIGHT CYCLED NORMALLY. // SIGNOFF // GATHERED EQUIPMENT FROM TECHNIC AIR. OBTAINED HANGAR SPACE FOR AIRCRAFT. JACKED AIRCRAFT TO SWING GEAR. FIRST 3 GEAR SWINGS OPERATIONAL CHECKS WERE SATISFACTORY. ALL GEAR LIGHTS OPERATED CORRECTLY. APPLIED FREEZE SPRAY TO R/H DOWNLOCK SWITCH AND ACCOMPLISHED GEAR SWINGS. R/H "GREEN" DOWNLOCK LIGHT NOW STAYS ON THROUGH GEAR RETRACTION AND EXTENSION. NETJETS MAINTENANCE CONTROL ORDERED DOWN LOCK SWITCH P/N 6-0407-1. DOWN JACKED AIRCRAFT WHILE AWAITING PARTS DELIVERY DUE TO HANGAR AVAILABILITY. 02/07/2019 08:26:00 STANLEY REEDER ( C38338 ) JACKED AIRCRAFT. REMOVED R/H MAIN GEAR ACTUATOR DOWNLOCK SWITCH P/N 6-0407-1 S/N NSN AND INSTALLED NETJETS PROVIDED SWITCH P/N 6-0407-1S/N NSN AND ADJUSTED SWITCH IN REFERENCE TO CE750 MM CHAPTER 32-30-04. OPERATIONAL CHECK SATISFACTORY. DOWN JACKED AIRCRAFT.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 14,412 hrs · 8,781 cycles

EXHAUST FUMES IN CABIN NOTICED DURING CLIMB AND AT CRUISE ALTITUDE. (FL400) SEEMED TO GET WORSE WHEN TEMPERATURE CONTROL CALLED FOR HEAT. THEN SMELL SEEMED TO DECREASE WHEN TEMPERATURE SETTING WAS REDUCED. AT LOWER ALTITUDES AND ON GROUND AFTER LANDING EVENTUALLY BECAME FAR LESS NOTICEABLE. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED COALESCERS PN: 746451-3

Part: CONVERTER — DIRTY (OZONE) · airframe 13,785 hrs · 8,393 cycles

PASSENGERS AND CREW SMELLED A STRONG SMOKY ODOR COMING INTO CABIN. CLEANED FWD & AFT WATER SEPARATOR AND DRAIN LINE. CLEANED OZONE CONVERTER. RAN SYSTEM, NO DEFECTS NOTED. WORK PERFORMED IAW MM 21-11-00, 21-21-00, 21-22-00, 21-51-00, AND 21-71-00.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 13,741 hrs · 8,367 cycles

LEFT GEAR GREEN INDICATOR IS NOT ILLUMINATED. DECLARED EMERGENCY FOR UNSAFE LANDING GEAR INDICATION. DETERMINED LIGHT BULBS INOPERABLE. REMOVED AND REPLACED LEFT LANDING GEAR INDICATION LIGHT BULBS IAW AMM 32-60-00. OPS CHECK GOOD.

Part: DOOR FRAME — DENTED (PAX DOOR) · airframe 13,476 hrs · 8,195 cycles

REPAIR OF DENTED CABIN DOOR OPENING STRUCTURE.

Part: DIFFUSER — CRACKED (LT INBD) · airframe 13,476 hrs · 8,195 cycles

LEFT INBOARD LEADING EDGE DIFFUSER CRACKED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,251 hrs · 8,060 cycles

ACRID ODOR IN COCKPIT, NOT CABIN. INTERMITTENT BUT VERY STRONG

Part: LINE — FAILED (HYD SYSTEM) · airframe 13,176 hrs · 8,021 cycles

DURING TAKE OFF, THE AIRCRAFT LOST ALL HYDROLIC FLUID FROM THE A SYSTEM. EMERGENCY BREAKING AND EMERGENCY GEAR BLOW DOWN WAS USED. INSPECTED AIRCRAFT AND FOUND R/H LANDING ACTUATOR RETRACT HOSE RUPTURED. REMOVED AND REPLACED THE HOSE. JACKED AIRCRAFT, SERVICED HYDRAULICS, CYCLED AND BLEED LANDING GEAR. OPS AND LEAK CHECKED GOOD. ALSO BLEED BRAKES AND SLATS. SERVICES HYD A SYSTEM ONCE MORE. OPENED SEVERAL BELLY AND WHEEL WELL PANELS AND CLEANED AS MUCH HYD FLUID AS POSSIBLE. WORKED IAW MM 32-30-00.

Part: APU — ODOR · airframe 13,018 hrs · 7,940 cycles

ON GROUND AND DURING FLIGHT ACFT HAS STRONG ODOR OF FUMES. THIS IS VERY NOTICEABLE WHILE RUNNING APU. FUMES SEEM TO DISPARATE SOME AFTER APU SHUTDOWN HOWEVER ODOR IS STILL PRESENT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED THE APU.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 9,506 hrs · 5,751 cycles

DURING GEAR EXTENSION DID NOT RECEIVE A GREEN LIGHT FOR THE LT MAIN GEAR. CONFIRMED WITH TOWER THAT IT WAS DOWN. BLEW GEAR DOWN BOTTLE. RAN ROTORY TEST WHEEL TO LANDING GEAR AND RECEIVED NO HORN. LANDED WITHOUT INCIDENT. FOUND BOTH LT GEAR INDICATOR LIGHT BULBS BURNED OUT. R & R LT INDICATOR WITH NEW BULBS. COMPLIED WITH LEAKING GEAR EMERGENCY PNEUMATIC STORAGE BOTTLE SERVICING PROCEDURES AND HYD BLEEDING PROCEDURES. PERFORMED SEVERAL SATISFACTORY GEAR SWINGS. OPS CHECK GOOD. SERVICED HYD TO CORRECT LEVEL. WORK DONE IAW MM CH 12-10-36.

Part: HINGE BRACKET — CRACKED (LT ELEVATOR) · airframe 9,426 hrs · 5,709 cycles

LT INBD ELEVATOR HINGE FITTING BRACKET DUE TO CRACK. REMOVE EXISTING ANGLES AND BRACKETS FOR ACCESS, FABRICATE LOCATING TEMPLATE, REMOVE EXISTING HINGE BRACKET, LOCATE DRILL AND INSTALL NEW HINGE ASSY. R & R LT ELEVATOR INBD HINGE FITTING BRACKET INBD HALF PN 6732030-207 AND BEARING PN MS27641-6 ON LT HORIZONTAL. SEE SUPPLEMENT FORM FOR DETAILS. WORK PERFORMED IAW SRM 51-40-03, 51-40-06 AND 51-70-03.1. REMOVED LT ELEVATOR INBD HINGE FITTING BRACKET INBD HALF ON LT HORIZONTAL DUE TO CRACK 2 LOCATED AND DRILLED NEW INBD HINGE FITTING BRACKET INBD HALF PN 6732030-207-3 CLEANED SURFACE AND INSTALLED NEW LT INBD ELEVATOR HINGE FITTING PN 6732030-207 AND BEARING PN MS27641-6 USING EA9309.3NA LOT JH2DAA3570 AND AN470AD4 AND 5 RIVETS AND NAS1097AD4 RIVETS

Part: OIL SYSTEM — LEAKING (APU) · airframe 9,036 hrs · 5,477 cycles

BAD, FOUL ODOR COMING OUT OF COCKPIT AND CABIN VENTS BOTH ON THE GROUND AND IN FLIGHT. REMOVED APU INLET DUCT ASSY AND INSPECTED AREA. FOUND OIL SEEPING AT COMMPRESSOR INLET HOUSING AND OIL RUNNING DOWN THE BOTTOM OF SAME HOUSING. R & R THE APU IAW MM 49-10-00. APU OPERATES NORNALLY. OPS AND LEAK CHECKED GOOD. NO ABNORMAL ODOR NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,543 hrs · 4,545 cycles

DURING DESCENT WHEN THRUST WAS REDUCED WE HEARD A BUMP NOISE FROM REAR OF AIRCRAFT. IMMEDIATELY WE BEGAN TO DETECT A BURNED OIL ODOR THAT LASTED APPROX 3 MIN. COCKPIT PAC TEMP WAS UNCONTROLLABLE FOR REST OF FLIGHT.

Part: WARNING LIGHT — ILLUMINATED · airframe 8,590 hrs · 5,271 cycles

DURING 2 ABORTED TAKEOFFS AT 70_80KTS, THE FOLLOWING AMBER CAS MESSAGES APPEARED; YD OFF LOWER, FGC-A FAIL, FGC-ADC MISCOMP, FOLLOWED BY A RED NO TAKEOFF.

Part: SWITCH — MALFUNCTIONED (RUDDER SYS) · airframe 6,532 hrs · 3,917 cycles

IN FLIGHT AT FL430 AMBER "RUD STBY SYS FAIL" ILLUMINATED. RESET WAS UNSUCCESSFUL. REMOVED AND REPLACED RUDDER STANDBY SWITCH IAW MM 29-20-05. SYSTEM OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 6,342 hrs · 3,802 cycles

FUEL FILTER BYPASS L CAS MESSAGE ILLUMINATED IN FLIGHT.

Part: CONNECTOR — LOOSE (BYPASS SWITCH) · airframe 6,342 hrs · 3,802 cycles

FUEL FILTER BYPASS L CAS MESSAGE ILLUMINATED IN FLIGHT. MESSAGE ONLY STAYED ON APPROX 1 MINUTE, SECOND EACH OCCURENCE, BUT WOULD REAPPEAR EVERY FEW MINUTES. THIS CONTINUED LANDING. FOUND FUEL FILTER BYPASS SWITCH ELECTRICAL CONNECTOR TO BE LOOSE AND DIRTY. CLEANED CONNECTOR AND SWITCH. PERFORMED MM FUNCTIONAL TEST OF THE FILTER BYPASS INDICATING SYS. NO DEFECTS NOTED. IAW MCC NO FURTHER ACTION NEEDED. WORK DONE IAW MM 73-30-00-700-801.

Part: PROXIMITY SWITCH — INOPERATIVE (AILERONS) · airframe 6,188 hrs · 3,709 cycles

AFTER LEVELING OFF AT 10,000, ACFT WAS SEVERELY OUT OF TRIM. IMMEDIATELY AFTER TRIMMING, AILERON RATIO LOW MESSAGE APPEARED. MESSAGE REMAINED ON UNTIL APU SHUTDOWN PRIOR TO LANDING. CONFIRMED DISCREPANCY, AILERON LOW RATIO ON W/ HYD POWER APPLIED TO ACFT. REMOVED PANEL 166AB TO ACCESS AILERON RATIO PROX SWITCH SY019. CHECKED GAP WAS GOOD. VERIFIED PROPER OPERATION OF AILERON SYS. VERIFIED GOOD WIRES TO PROXIMITY SWITCH GROUNDS 28PL005 AND MESSAGE EXTINGUISHED. GAINED ACCESS TO PROXIMITY SWITCH AND REPLACED WITH NEW SWITCH IAW MM, CH. 27-10-01, REV 35. FOUND PROXIMITY SWITCH TARGET DOES NOT PASS STRAIGHT OVER PROXIMITY SWITCH. CONTACTED TEAM X PRODUCT SUPPORT, WHO CONTACTED ENGINEERING TO CONFIRM THAT TARGET LOCATION IS ACCEPTABLE. POWERED HYD SYS (A AND B) AND CONFIRMED THAT AILERON RATIO LOW CAS MESSAGE EXTINGUISHED. TIGHTENED AND SAFETIED SWITCH MOUNTING NUT MM CH 27-10-01 REV 35. AILERON RATIO PROX SWITCH OPS CHECK GOOD IN REF MM CHP 27-10-01 REV 37.

Part: UNKNOWN — OUT OF TRIM · airframe 6,188 hrs · 3,709 cycles

AFTER LEVELING OFF AT 10,000FT, AIRCRAFT WAS SEVERLY OUT OF TRIM.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 5,615 hrs · 3,340 cycles

UPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00.

Part: PDU — INOPERATIVE (TE FLAPS) · airframe 5,615 hrs · 3,340 cycles

UPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00.

Part: DIODE — BURNED · airframe 5,605 hrs · 3,334 cycles

REMOTE CB TRIPPED CYAN CAS MESSAGE. ILLUMINATED DURING DESCENT. MESSAGE WAS ACCOMPANIED BY ODOR OF ELECTRICAL SMOKE. OPENED AFT "J" BOX & FOUND CB HK005 TRIPPED. RESET BREAKER, POWERED AIRCRAFT. POWERED PASSENGER SAFETY SYSTEM. AFTER APPROX 10 MIN. CB HK005 TRIPPED. INSPECTED WIRING & FOUND DIODE BURNED ON RELAY BEHIND SWITCH PANEL FOR PASSENGER SAFETY SWITCH. REMOVED & REPLACED BAD DIODE. C/W SATISFACTORY OPERATIONAL CHECK OF THE PASSENGER WARNING SYSTEM. ALL EICAS INDICATIONS NORMAL. IAE MM 33-20-01.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 5,303 hrs · 3,152 cycles

IN CRUISE FLIGHT AT FL390 RECEIVED (WINDSHIELD HEAT L FAIL) CAS MSG FOLLOWED BY THE FRACTURING OF THE OUTER PLY OF THE LT WINDSHIELD. PERFORMED ELECTRICAL HEATED WINDSHIELD FUNCTIONAL TEST IAW CESSNA 750 M/M 30-41-00, REMOVED LT WINDSHIELD. INSTALLED NEW L/H WINDSHIELD. PERFORMED ELECTRICAL HEATED WINDSHIELD FUNCTIONAL TEST IAW CESSNA 750 MM 30-41-00. NO DISCREPANCIES AT THIS TIME. INSTALATION OF WINDSHIELD WAS PERFORMED IAW CESSNA 750 M/M 56-11-00.

Part: STRUT — DISCHARGED (NLG) · airframe 4,465 hrs · 2,635 cycles

VIOLENT NOSE WHEEL SHIMMY DURING T/O ROLL (VERBAL FROM CREW STARTED AT 80KTS AND CONTINUED DOWN TO ABOUT 40 KTS). UPON ARRIVING AT AIRCRAFT FOUND NOSE STRUT FLAT. REMOVED LOWER & UPPER BARREL ASSY AND FOUND INTERNAL DAMAGE. RMVD AND REPLACED UPPER & LOWER BARREL ASSY. NO HYD LINES WERE REMOVED. RE-SECURED ALL ACCESS ITEMS. GEAR SWINGS/TAXI SWINGS/TAXI CHECK GOOD I/A/W CE750 C/M/M 32-20-02

Part: FLOAT VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 3,796 hrs · 2,246 cycles

AT FL 320 AND 3100 LBS IN RIGHT TANK AND 0 LBS IN CENTER WING TANK O FULL, RT EICAS MESSAGE APPEARED RIGHT WING WAS VENTING FUEL MOVED CENTER WING X-FER SWITCH TO OFF ABOUT 30-40 SECONDS LATER EICAS MESSAGE DISAPPEARED AND FUEL STOPPED VENTING. REMOVED AND REPLACED RT O/B TRANSFER FLOAT VALVE IAW 750 MM 28-20-06. LEAK CHECKED PANELS WITH FUEL CAPACITY AT MAXIMUM FOR 40 MINUTES. NO LEAKS NOTED.

Part: VENT — LEAKING (FUEL SYSTEM) · airframe 2,997 hrs · 1,791 cycles

AMBER CAUTION, WING TANK OVER FILL RT, INFLIGHT AND DID NOT EXTINGUISH WHILE VENTING FUEL UNTIL DESENT WAS INITIATED. INSPECTED FLOAT VALVE ON PANEL 642DB, FLAPPER VALVE ON 641DB, FUEL TRANSFER FLOAT VALVE, AND CENTER TANK FLOAT VALVE, CLIMB VENT LINE FLAPPER VALVE, WING FUEL TANK PRESSURE/VACUUM RELIEF VALVE, FUEL FLAPPER CHECK VALVE AND OUTBOARD FUEL TRANSFER FLOAT VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM FLOW TEST AND FUEL TRANSFER SYSTEM SHUTOFF TEST. BOTH TEST WITHIN LIMITS.

Part: WHEEL — VIBRATES (NLG) · airframe 2,810 hrs · 1,666 cycles

DURING T/O ROLL, NOSE STRUT VIBRATES EXCESSIVELY. REMOVED AND REPLACED LT AND RT NOSE GEAR TIRE ASSYS IAW 750 MM 32-41-01.

Part: BRAKE — STICKING (LEFT) · airframe 2,771 hrs · 1,639 cycles

WHILE TAXIING, DURING BRAKE TEST, THE LEFT MAIN BRAKES SEEMED TO BE STICKING, AN ABRUPT PULLING TO THE LEFT, COULD NOT HOLD A/C STRAIGHT EVEN WITH DIFFERENTIAL BRAKING . HYDRAULIC PRESSURE NORMAL.

Part: LIMIT SWITCH — INOPERATIVE (FUEL TANK) · airframe 2,547 hrs · 1,368 cycles

DURING A 52 MINUTE FLIGHT IN CRUISE, "WING TANK O'FULL R" AMBER CAS MESSAGE ILLUMINATED 3 DIFFERENT TIMES. EACH TIME LOST APPROX 100-200 LBS OF FUEL. REMOVED AND REPLACED FLOAT SWITCH IAW CE 750 MM 28-20-07.

Part: WHEEL — OUT OF BALANCE (MLG) · airframe 2,530 hrs · 1,497 cycles

EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL CAUSED YD OFF MESSAGE ABORTED TAKE OFF. REMOVED LT AND RT NOSE WHEELS, INSTALLED OVERHAULED NOSE WHEEL ASSEMBLIES IAW M/M CHAPTER 32-41-01.

Part: O-RING — CUT (FUEL TANK) · airframe 2,432 hrs · 1,438 cycles

WING TANK OVERFULL R AMBER CAS MESSAGE CAME ON IN FLIGHT. DID NOT STOP OVERVENTING FUEL UNTIL DESCENDING THRU +/- 17000 FEET AND RIGHT FUEL GAUGE 3010 LBS, LEFT GAUGE 3290 LBS. - (M2B) FOUND FUEL COMING FROM RT AILERON BELCRANK DRY BAY. FOUND ONE CROSS OVER TUBE IN THIS DRY BAY TO HAVE A CUT O-RING. REPLACED 4 EA O-RINGS P/N MS29513-117 AND 4 EA O-RINGS P/N MS29415-218 AT THE ENGINES FITTINGS IN THE DRY BAY TUBES. FOUND FLAPPER VALVE AT INBOARD END OF FWD TUBE TO HAVE EXCESSAVE PLAY. REPLACED FLAPPER VALVE WITH NEW VALVE IAW CE750 M/M CH 28-10-0. OPS CHECKED AND LEAK CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (FUEL SYS) · airframe 1,834 hrs · 1,107 cycles

"WING O FILL R" AMBER LIGHT CAME ON IN FLIGHT, LOST ABOUT 400 LBS OF FUEL. INSPECTED RIGHT WING OUTBOARD TRANSFER VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM SHUTOFF TEST. FOUND ALL OPERATION NORMAL. NO FURTHER ACTION TAKEN. WORK PERFORMED IAW CHAPTER 28-20-00 OF THE CITATION 750 MM.

Part: AUDIO VIDEO UNIT — FAILED (CABIN) · airframe 770 hrs · 478 cycles

WHILE ON GROUND AT ASE PRIOR TO BOARDING PASSENGERS, CREW NOTICED SMOKE COMING OUT FROM THE AFT CLOSET AREA, CREW DISCHARGED FIRE BOTTLE INTO AREA. TROUBLESHOT AND FOUND AIRSHOW SYSTEM INOPERATIVE AND AUDIO VIDEO AMP BREAKER POPPED, INSPECTED MONITORS AND FOUND FOIL FROM RIGHT AFT MONITOR PINS. INSPECTED AFT CLOSET AND FOUND THE PASSENGER ENTERTAINMENT AUDIO AMPLIFIER WAS THE SOURCE OF THE SMOKE AND ODOR. REPLACED AMPLIFIER. SYSTEM NOW OPERATIONAL BUT NO AUDIO OR VIDEO. DEACTIVATED PASSENGER ENTERTAINMENT SYSTEM AND SECURED AV AMP BREAKER.