N586QS

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 7,597 hrs · 5,033 cycles

ARM LIGHT TEST FAIL MULTIPLE TIMES, TRIED UNSUCCESSFUL RECHARGE PROCEDURE. REPLACED BATTERY PACKS. OPS CHECK GOOD. IAW CESSNA CE-680A AMM 33-50-06

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 7,148 hrs · 4,704 cycles

CLIMBING OUT OF KHPN ABOUT TO LEVEL AT 5000 FT WE RECIEVED A RIGHT RED ENGINE FIRE WARNING. BEFORE I COULD RUN THE CHECKLIST THE LIGHT AND WARNING EXTINGUISHED. I BELIEVE IT WAS FROM THE THEOTTLE RETARDING AT LEVEL OFF. NOTICED THE ITT ON THE RIGHT ENGINE WOULD FLUTUATE WITH THROTTLE POSITION, IT DID NOT MATCH THE LEFT SIDE. I SAW THE ITT IN THE AMBER, IM NOT SURE IT MADE IT INTO THE RED. WE RETURNED TO HPN UNEVENTFULLY. UPON INSPECT ON GROUND A BIG HOLE ON TOP OF COWLING BY THE OIL DOOR. REMOVED THE UNSERVICEABLE RT ENG AND INSTALLED A REPAIRED SERVICEABLE RT ENG. PERFORMED ALL REQUIRED OPS CHECKS WITH ENGINE WITHIN EMM PARAMETERS, NO LEAKS NOTED. MAINTENANCE ACCOMPLISHED IAW AMM 71-00-05 AND EMM 71-00-00.

Part: STEERING UNIT — DEFECTIVE (ZONE 700) · airframe 6,926 hrs · 4,570 cycles

UPON LANDING WHILE ATTEMPTING TO EXIT THE RUNWAY LEFT AND RIGHT TILLER STEERING APPEARED TO BE INOP. REPLACED NWS UNIT. OPS CHECK/LEAK CHECK GOOD. IAW CE-680A AMM 32-50-50

Part: LIGHT — DEFECTIVE · airframe 6,773 hrs · 4,477 cycles

ON POST FLIGHT WALK NOTICED THE SMALLER EMER LIGHT ON THE RIGHT SIDE OVER WING LIGHT IS VERY DIM AND FLICKERING. CORRECTIVE ACTION; REMOVED OVER WING EMER LIGHT INSTALLED NEW OVER WING EMER LIGHT OPS CHECK GOOD. NO DEFECTS NOTED. REF. CE 680A AMM 33-50-20.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,525 hrs · 3,651 cycles

MAIN DOOR: MAIN CABIN DOES NOT OPEN NORMALLY. REQUIRES PUSH TO OPEN. //SIGNOFF// COULD NOT DUPUCATE DISCREPANCY. DOOR OPENS AND CLOSES AS INTENDED. CHECKED RIG OF DOOR PER CE-680A MM 52-10-00 FOUND DOOR RUBBING SUGHTLY ON AFT RUB BLOCK REMOVED SHIMS FROM RUB BLOCK TO BRING GAP WITHIN UMITS. NO OTHER DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF DOOR. NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,525 hrs · 3,651 cycles

MAIN DOOR: MAIN CABIN DOOR DIFFICULT TO OPEN. // SIGNOFF// INSPECTED MAIN CABIN DOOR FOR ANY DAMAGE AND NO DEFECTS NOTED, PERFORMED SERVERAL SATISFACORY OPS CHECKS OF MAIN CABIN DOOR, NO DIFFICULTY NOTED OPENING AND CLOSING FROM INSIDE AND OUTSIDE I/A/W CE·680A AMM 52·10-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,385 hrs · 3,554 cycles

AT FL400 , LOUDRUSH OF AIR NOISE SIMILAR TO THE NOISE MADE WHEN DOING PRESSURIZATION SYSTEM CHECKS CAME ON CONTINUOUSLY. NOISE CONTINUES NON STOP WHILE ON GROUND, AND A BURNING ODOR NEAR LAVATORY & REAR CABIN. RAN APU & ENGINES WITH BLEED ON, NO DEFECTS OR BURNING ODOR NOTED. WITH ENGINES RUNNING ACCOMPLISHED EMER SYS TEST IAW AMM 21-12-00. TESTED OK, NO BURNING ODOR. ADVISED MCC ON FINDINGS. MCC ADDED DUCT BURN PROCEDURE IAW TC-68A-21-101006M. HEPA FILTER. COMPLIED WITH ENVIRON CONTROL SYS BLEED & TRIM AIR DUCT BURN PROCEDURE.TC-68A-21-181006MR3. R & R HEPA FILTER IAW AMM 21-70-10. OPS CHKD GOOD, AFTER ENGINE RUNS NO BURNING ODOR IN CABIN, UNABLE TO DUPLICATE DISCREPANCY.

Part: UNKNOWN — UNKNOWN · airframe 4,531 hrs · 2,993 cycles

A VIBRATION OF UNDETERMINED LOCATION. COULD BE FELT THROUGH OUT THE ENTIRE AIRCRAFT. SEEMS TO LESSEN WITH SPEED BUT NEVER GOES AWAY. VIBRATION OCCURRED CLIMBING OUT OF 3000 WITH THE FLAPS & GEAR UP. REMAINED THROUGHOUT THE ENTIRE FLIGHT UNTIL LANDING. BUT IT DID GET LESS WITH SPEED. CHECKED ALL DOORS & FOUND ALL SECURE, LANDING GEAR DOOR FOUND SECURE. ALL PANELS SECURE. RAN ENGS & NOTICED A DIFFERENT SOUND WHEN THE RT PRESSURE SOURCES SELECTED & WENT AWAY WHEN ON LT SELECTED. ASKED TO RUN AT HIGH POWER & TO TURN ON WING ANTI ICE . AFTER RUNNING SECOND TIME, ALL NOISES WENT AWAY WHEN SELECTED RT OR LT SOURCE & ENG BLEEDS, ASKED TO DOWNLOAD ARES. READ ARES DOWNLOAD & SAW NO DISCREPANCY. RAN A/C AGAIN WITH MANY DIFFERNT BLEEDS ON & OFF & POWER SETTLNGS, ONLY HEARD A LOW RUMBLE FIRST TIME & NEVER HEARD IT AGAIN. LOOKED AT ALL DUCTS IN AFT BAY ALL LOOKED SECURE.

Part: NOT REPORTED — NOT REPORTED · airframe 11,562 hrs · 8,845 cycles

CABIN EMERG LIGHT: WITH THE EMER LTS SWITCH IN THE ARM POSITION AND PAX SAFETY SWITCH IN OFF OR SEAT BELT ON POSITION, THE FWD HALF OF THE EMER LIGHTS IN THE CABIN WERE STILL ON. THE AFT LIGHTS WORKED AS ADVERTISED.///SIGN-OFF///RESET FWD EMERGENCY LIGHTING BATTERY PACK IMPACT SWITCH AND PERFORMED OPS CHECK. IAW CE-560XL AMM 33-50-01. OPS CHECK GOOD.

Part: NOT REPORTED — NOT REPORTED · airframe 3,708 hrs · 2,465 cycles

FLOOR EMERG EXIT LIGHT: THE TOE KICK LIGHTING UNDER THE LAV SEAT IS INOPERATIVE. THE LIGHTS DO NOT OPERATE WITH EMERGENCY BATTERY POWER OR WITH MAIN SHIPS POWER.///SIGN-OFF///FOUND TOE KICK LIGHTING CONNECTOR DISCONNECTED. RECONNECTED TOE KICK CONNECTOR. OPS CHECK GOOD. IAW CE-680A AMM 30-50-00.

Part: SKIN — CORRODED (LT WING) · airframe 3,111 hrs · 2,071 cycles

REPAIR TO LH WING LOWER SKIN CORROSION. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ30944M1 DATED 8/4/2021, LEFT WING EXTENSION DAMAGE (CORROSION).

Part: SKIN — CHAFED (ZONE 100) · airframe 3,111 hrs · 2,071 cycles

LWR SKIN CHAFE FROM ANTI - ICE CROSSFLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/15/2019, STANDARD REPAIR - 680A ALL S/N LWR SKIN CHAFE FROM ANTI - ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 DATED 07/19/2019. COMPLETED STEPS 1 THOUGH 5.

Part: SKIN — CORRODED (LT WING) · airframe 3,111 hrs · 2,071 cycles

REPAIR TO LH WING LOWER SKIN CORROSION. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ30944M1 REV. A DATED: 8/11/2021, LEFT WING EXTENSION DAMAGE (CORROSION).

Part: ACM — CONTAMINATED · airframe 2,923 hrs · 1,946 cycles

ODORS IN COCKPIT / CABIN: CLEAR ACM INTAKE AND INTAKE DUCTS OF CICADAS. CLEAN CICADA DEBRIS FROM APU INTAKE DUCT AND ASSOCIATED AREAS. ALL INSECT DEBRIS HAS BEEN REMOVED AND RESTORED AIRCRAFT TO ORIGINAL CONDITION CLEAR ACM INTAKE AND INTAKE DUCTS OF CICADAS. PERFORMED BOROSCOPE OF ACM INTAKE AND INTAKE DUCKS NO NOTICABLE DEBRIS FOUND.

Part: UNKNOWN — ODOR (COCPIT) · airframe 2,346 hrs · 1,582 cycles

DURING CLIMB OUT NOTICED AN UNIDENTIFIED ODOR IN THE COCKPIT. THERE WAS NO SIGN OF SMOKE. ANTI ICE WAS OFF AND CLIMB POWER WAS SET. ALL ELECTRICAL INDICATIONS WERE NORMAL AND AIR CONDITIONING SUPPLY TEMPERATURES WERE NORMAL. SIGNOFF. PERFORMED ENGINE RUNS AT DIFFERENT THROTTLE SETTINGS AND VARIED BLEED SOURCES, NO SMELLS WERE NOTED. INSPECTED BLEED LINES AND FOUND NO DEFECTS.

Part: DOUBLER — CRACKED (NLG WW) · airframe 1,989 hrs · 1,347 cycles

CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75.