N289JB

Part: SIGN — INOPERATIVE (CABIN) · airframe 6,108 hrs · 3,934 cycles

AFTER FLT 402 MYS-BOS DURING ROUTINE MAINTENANCE MX FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT SIGN INOP. REMOVED AND REPLACED RT EMERGENCY EXIT SIGN LIGHT IAW AMM 33-50-17, OPS CHECK GOOD.

Part: MODULE — FAILED (NR 1) · airframe 5,429 hrs · 3,112 cycles

FLT 1206 - RSW-HPN DIVERTED TO JFK DO TO EICAS MESSAGE "SPDA FAIL". MX PERFORMED AMM FIM TASK 24-61-00-810-830-A00 AND -855-A00 REPLACED SPDA NR 1 MICRO COMM MODULE SLOT 8 IAW 24-61-07. ALL OPS CHECKS NORMAL. RETURNED TO SERVICE.

Part: SHEAR PIN — CRACKED (ZONE 400) · airframe 5,531 hrs · 3,599 cycles

DURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT INBOARD PYLON TO WING ATTACH FITTING SHEAR PIN CRACKED. REMOVED AND REPLACED THE INBOARD SHEAR PIN ASSEMBLY IAW EMBRAER IC 2009-190/0733A.

Part: SHEAR PIN — CRACKED (ZONE 400) · airframe 5,531 hrs · 3,599 cycles

PLEASE DISREGARD SDR YENA20090909116 FOR AIRCRAFT N289JB MSN 19000002 DATE 09/18/09. DURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT OUTBOARD PYLON TO WING ATTACH FITTING SHEAR PIN WAS FOUND CRACKED. REMOVED AND REPLACED THE OUTBOARD SHEAR PIN IAW IC 2009-190/07333A.

Part: SHEAR PIN — CRACKED (ZONE 400) · airframe 5,531 hrs · 3,599 cycles

DURING 6000 HR CHECK AT EMBRAER AIRCRAFT MAINTENANCE SERVICES BNA, A VISUAL INSPECTION OF THE RT PYLON AFT INBOARD PYLON TO WING FITTING ATTACH SHEAR PIN FOUND CRACKED. REMOVED AND REPLACED THE INBOARD SHEAR PIN IAW EMBRAER IC 2009-190/07333A.

Part: SHEAR PIN — CRACKED (ZONE 400) · airframe 5,531 hrs · 3,599 cycles

DURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT OUTBOARD PYLON TO WING ATTACH PIN CRACKED. REMOVED AND REPLACED THE OUTBOARD AFT SHEAR PIN IAW EMBRAER IC 2009-190/07333A.

Part: SHEAR PIN — BROKEN (NR 2 ENGINE) · airframe 5,531 hrs · 3,499 cycles

DURING HEAVY MX, A SHEAR PIN ON THE NR 2 ENG WAS OBSERVED TO BE BROKEN INTO 2 PIECES. THIS OBSERVATION MADE FOLLOWING THE DETECTION OF 2 BROKEN SHEAR PINS ON THE NR 1 ENG.

Part: SHEAR PIN — BROKEN (ENGINE) · airframe 5,531 hrs · 3,599 cycles

DURING VISUAL INSPECTION OF ENGINE, TWO SHEAR PINS WERE OBSERVED TO BE BROKEN.

Part: SHEAR PIN — UNSERVICEABLE (ENGINE)

SHEAR PIN WAS FOUND BROKEN DURING ENGINE MX. (K)

Part: SENSOR — FAILED (SLAT SKEW) · airframe 4,608 hrs · 3,053 cycles

FLT NR1310, ON APPROACH SLAT FAIL AT POSITION 3, REMOVED AND REPLACED RT WING SKEW SENSOR AT THE 2/3 POSITION. OPERATED SLATS SEVERAL TIMES. NO FAULTS NOTED.

Part: FITTING — LACK OF LUBE (MLG) · airframe 3,963 hrs · 2,686 cycles

DURING GEAR EXTENSION BRAKE CONTROL FAULT MESSAGE DISPLAYED. RT MLG SLOW TO EXTEND WITH SLIGHT YAW FELT - TRANSIENT LANDING LEVER DISAGREE APPEARED ONCE ALL GEAR DOWN - BRAKE CONTROL FAULT ALSO DISAPPEARED. CREW ELECTED TO GO AROUND. A SECOND GEAR EXTENSION WAS ATTEMPTED AND WAS SUCCESSFUL WITH NO FURTHER FAULT. A/C LANDED UNEVENTFULLY IN JFK. PER FIM TASK 32-41-00-810-860A BRAKE CTL FLT IS A TRANSITORY CONDITION. T/S PER FIM 32-61-00-810-913A PERFORMED 5 LG SWINGS PER AMM 32-33-00-710-801-A WERE ABLE TO DUPLICATE MAIN GEAR FAULT. LUBED MLG IAW 32-00-03 REF LP 481138 NR 1 FOR LUBE OF UPLOCK ROLLER FITTINGS. PERFORMED EMERGENCY GEAR EXT SELECT VALVE ROD PER AMM 32-34-00-820-801-A, NO DEFECTS NOTED. RAN SIX MORE SWINGS PER AMM LISTED ABOVE (21 TOTAL) NO FURTHER PROBLEMS, MESSAGES NOTED.

Part: LANDING GEAR — MALFUNCTIONED (RT MLG) · airframe 3,702 hrs · 1,499 cycles

FLT NR 434, MCO-BOS, DURING INITIAL GEAR EXTENSION THE LT MAIN AND NOSE WHEEL EXTENDED NORMALLY AND THE RT MAIN STAYED UP. AFTER A GO AROUND WAS INITIATED THE RT MAIN CAME DOWN. QRH WAS REFERENCED AND GEAR OPERATED NORMALLY, NORMAL LANDING. PERFORMED FIM TASK 32-61-00-810-913-A00. JACKED A/C PERFORMED EMERGENCY EXTENSION FUNCTIONAL TEST 32-34-00. PERFORMED EXTENSION AND RETRACTION. SYSTEM IAW AMM 32-33-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: DUCT — CRACKED (NR 2 PACK) · airframe 3,091 hrs · 2,229 cycles

FL 662, MCO-BUF, AIR RETURN TO MCO. CLIMBING THROUGH 32,000 CABIN ALT WAS 8400 AND CLIMBING. CREW EXECUTED CABIN ALT HIGH PROCEDURE. CABIN ALT HIT 10,000 WITH A CABIN ALT EICAS. OUTFLOW VALVE WAS CLOSED. NO NOISES. PACK INDICATION NORMAL. ON DESCENT CABIN ALT STAYED BELOW 10,000 THROUGH THE REMAINDER OF THE FLIGHT. THE CABIN ALT AND CABIN RATE FLUCTUATED. PERFORMED FIM TASK 21-31-00-810-818-A. FOUND NR 2 PACK OUTLET DUCT CRACKED AND CONDITIONER AIR CHECK VALVE BELLOWS RUPTURED. REMOVED AND REPLACED NR 2 PACK OUTLET DUCT AND CHECK VALVE BELLOWS PER AMM 21-51. OPS CHECKS AND LEAK CHECKS OK. PRESSURIZATION CHECKS GOOD. REF 21-31-00.

Part: SUPPORT — BROKEN (NR 2 PACK) · airframe 3,090 hrs · 2,228 cycles

FLT 1114, MCO-RIC, AIR RETURN TO MCO AT FL 390, HEARD LOUD NOISE SIMILAR TO NOISE REDUCTION HEADSETS TURNING ON AND OFF. FLIGHT ATTENDANTS REPORTED LOUD BANG COMING FROM AFT OF AIRPLANE. CABIN ALT WAS RISING RAPIDLY WITH A HIGH CABIN RATE OF CLIMB. SHORTLY EICAS SHOWED CABIN ALT HIGH WITH MASTER WARNING. OFC WAS FULL CLOSED AND PACK (PSI) WAS NORMAL WITH GREEN LINES ON MFD ECS PAGE. PERFORMED QRH CABIN ALTITUDE HI PROCEDURES. CABIN ALT REACHED APRX 13,500 FT. REACHING 10,000 MSL, FLIGHT ALT CABIN PRESSURIZATION STABILIZED AND STARTED TO PRESSURIZE TO APRX 500 FT. FOUND NR 2 PACK OUTLET DUCT BELLOWS SLIPPED OFF AND A BROKEN PACK OUTLET DUCT SUPPORT ROD ASSY. RESECURED NR 2 PACK BELLOWS AND REMOVED AND REPLACED SUPPORT ROD ASSY IAW 21-51-21. PACK OPS CHECK GOOD AND A/C PRESSURIZATION CHECKS GOOD IAW 21-31-00.