N223QS

ATA 4900

Part: APU — ODOR · airframe 7,325 hrs · 4,248 cycles

UPON ARRIVING AT THE AIRPORT, NOTICED A MUSTY & OILY ODOR IN THE CABIN & COCKPIT. THIS SMELL PERSISTED & BECAME STRONGER WITH APU USAGE & WHILE INFLIGHT. UPON LANDING WE BOTH FELT A BURNING SENSATION IN BOTH OUR EYES. THE OILY ODOR IS MUCH STRONGER IN THE COCKPIT THAN THE CABIN. R & R APU IAW AMM 49-10-01-900-802. OPERATIONAL & LEAK CHECKS WERE SATISFACTORY. ALSO COMPLIED WITH CHECK & DECONTAMINATION OF THE AIR CONDITIONING SYS AFTER POLLUTION, WORK DONE IAW AMM 05-50-00-700-801.

ATA 2120

Part: DUCT — CONTAMINATED (CABIN AIR) · airframe 3,329 hrs · 1,946 cycles

BURNING ODOR WITH STRONG FUMES IN CABIN WITH APU RUNNING. TRACES OF OIL FOUND ON ECS FLOORBOARD. FOUND AIR DUCT CONTAMINATED. REMOVED CONTAMINATED DUCT AND INSTALLED NEW ASSY IAW MM 20-125 20-000 20-001.

ATA 7200

Part: ENGINE — VIBRATION (LEFT) · airframe 3,010 hrs · 1,751 cycles

LT ENGINE ROLLED BACK TO IDLE AT FL430. ITT ROSE TO A YELLOW INDICATION ABOUT 875. SOME VIBRATION, ABOUT 24 ON VIB INDICATION. LANDED WITH ENGINE AT IDLE. R & R NR 1 ENGINE.

ATA 2130

Part: CIRCUIT BOARD — DEFECTIVE (CABIN PRESSURE) · airframe 2,539 hrs · 1,476 cycles

CABIN DID NOT PRESSURIZE AFTER TAKEOFF. WHITE CAS MESSAGE "CABIN RATE" CAME ON DURING EACH CLIMB SEGMENT. REPLACED DEFECTIVE PRINTED CIRCUIT BOAD IAW MM 45-60-21. 32-600 AND 21-302. OPS CHECK GOOD.

ATA 3240

Part: SERVO VALVE — MALFUNCTIONED (MLG) · airframe 2,410 hrs · 1,377 cycles

BRAKE APPLICATION CAUSES ACFT TO YAW RT W/ NO NWS APPLICATION, (BRAKE PRESS) AMBER CAS MESSAGE COMES ON TEMPORARILY AFTER APPLICATION RELEASE. NO FAULT CODES, NO MAINT MESSAGE. REPLACED (DEFECTIVE) RT BRAKE SERVO VALVE WITH UNIT REPAIRED IN ACCORDANCE WITH MM 29-004. OPERATIONAL AND LEAK CHECKS GOOD.

ATA 2613

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 3,897 hrs · 2,389 cycles

BLEED OVERHEAT LIGHT CAME ON 2 MIN AFTER TAKEOFF. CHECKLIST ACCOMPLISHED AND CREW WAS UNABLE TO ISOLATE THE MALFUNCTION. FAULT CODE 404 AND 428. BLEED OVERHEAT COMES ON WITH APU BLEED ON AND ENGINE OFF. REMOVED & REINSTALLED TEMP SENSOR L70HU. OPS & LEAK CHECKS GOOD IAW MM 36-70-00

ATA 3240

Part: ISOLATION VALVE — MALFUNCTIONED (BRAKE) · airframe 966 hrs · 589 cycles

WHEN BRAKES ARE APPLIED DURING LOW SPEED TAXI, BRAKES WILL RELEASE INTERMITTENTLY. 10-29-07 REPLACED DEFECTIVE BRAKE ISOLATION VALVE WITH UNIT INSPECTED BY EATON FH3R501L. REPLACED DEFECTIVE BRAKE SERVO VAVE WITH UNIT REPAIRED BY APRO XPER689K IN ACCORDANCE WITH F2000 EXEASY M/M 29-004 AND 32-412. OPERATIONAL AND LEAK CHECKS GOOD

ATA 3240

Part: BRAKE ASSY — INTERMITTENT (MLG) · airframe 951 hrs · 581 cycles

AIRPLANE BRAKES WORKING INTERMITENTLY. POWERED UP AIRCRAFT AND INTERROGATED CMC. NO FAULTS FOUND FOR BRAKE SYSTEM OR CAS MESSAGE PRESENT. PERFORMED BRAKE PRESSURE CHECKS ON SYSTEM 1 AND 2. NO DEFECTS NOTED. BLED BOTH BRAKE SYSTEM. BRAKE SYSTEM OPS CHECK GOOD. WORK PERFORMED PER F2000 EX M/M 34-412, 32-414, 32-415, 32-419 & 32-446

ATA 2910

Part: FILTER — UNKNOWN (HYD SYSTEM) · airframe 128 hrs · 74 cycles

ON TAXI OUT, LT BRAKE WAS BINDING AND PULLING TO THE LT USED EMERGENCY BRAKE TO STOP EMERGENCY BRAKE WORKED FINE. LT BRAKE TEMP 170/150, RT BRAKE TEMP NORMAL 60/50. TROUBLESHOT LT BRAKES VISUALLY INSPECTED IB AND OB LT BRAKE AND TIRE ASSY SATISFACTORY AT THIS TIME. CHECKED FOR FAULT CODES. NO BRAKE FAULTS AT THIS TIME. REMOVED AND REPLACED LT AND RT HYD MANIFOLD RETURN FILTERS (LT) CD11, CD12, AND GENERAL RETURN (RT) CD2 W/NEW. LEAK CHECKS GOOD. NJA FLT CREW C/W TAXI/HIGH SPEED TAXI CKS GOOD AT THIS TIME IAW MM CH (32-429), (29-008), (45-308), (32-446) AND F2000EX AFM.