JETBLUE AIRWAYS CORPORATION

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

The “follow me” driver stopping the airplane (flight 551) about 35 feet from the normal stopping point due to a difficulty in seeing the yellow “T”-bar because of the dark night conditions and the presence of de-icing fluid on the ground.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

An inadvertent encounter with convectively induced turbulence during cruise that was not depicted by the airplane’s weather radar system.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

The loss of both Integrated Drive Generators (IDG) due to worn fixed cylinder block bores, which caused the IDGs to be tripped offline and caused the airplane to enter an emergency electrical configuration.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

Electrical sparking caused by a faulty connection between the aircraft and ground power unit resulting in a serious injury to a ground service agent.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

The captain’s rotation of the airplane pitch before the rotation speed on takeoff due to his surprise about encountering head on landing traffic, which resulted in an exceedance of the airplane’s pitch limit and a subsequent tail strike. Contributing to the accident was the flight crew’s expectation bias that the incoming aircraft was landing on the same runway as they were departing from, and the conflicting traffic’s nonstandard use of phraseology when making position calls on the common traffic advisory frequency.

Operated by Jetblue Airways (per NTSB report)

Operated by Jetblue Airways (per NTSB report)

an inadvertent encounter with clear air turbulence.

Operated by Jetblue Airways Corp (per NTSB report)

A buildup of pressure in the coffee filter package resulting in the release of hot coffee and grounds when the pot locking lever was raised.

Operated by jetBlue Airways (per NTSB report)

an inadvertent encounter with convective turbulence.

Operated by JetBlue Airways (per NTSB report)

an inadvertent encounter with convective turbulence, which resulted in a serious injury to a flight attendant.

Operated by JetBlue Airways (per NTSB report)

an inadvertent encounter with convective turbulence while in cruise flight.

Operated by jetBlue Airways (per NTSB report)

Operated by jetBlue Airways (per NTSB report)

The probable cause of the engine failure and subsequent undercowl engine fire was due to the fatigue fracture of a high pressure turbine stage 2 disk blade retaining lug that released two blades which impacted the low pressure turbine case causing a fuel line to fracture spraying fuel on the hot engine cases where it ignited. During a machining operation of the disk lug, a tool mark was introduced that set up the area for fatigue cracks to initiate.

Operated by jetBlue Airways (per NTSB report)

Operated by JETBLUE AIRWAYS CORPORATION (per NTSB report)

the failure of the right main landing gear door retraction flexible hydraulic line in the Green hydraulic system, which led to prolonged operation of the power transfer unit and subsequent overheating and loss of pressure in the Yellow hydraulic system, resulting in the airplane's operation with only one hydraulic system. Contributing to the incident was the lack of incorporation of aircraft manufacturer service bulletins that describe procedures for aircraft modifications intended to prevent this occurrence.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

The airplane's inadvertent encounter with turbulence during the approach, which resulted in serious injury to a flight attendant.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

The first officer’s inadvertent activation of the parking brake in flight, which led to the airplane abruptly stopping and all four of its main landing gear tires deflating, and his use of a nonstandard procedure to cancel the airplane's monitoring alert system.

Operated by JetBlue Airways, Inc. (per NTSB report)

The separation of both halves of the left engine fan cowl assembly due to improper latching and locking of the all the fan cowl latches. The cause of the improper latching and locking of the fan cowls was due to the failure of the mechanic to unstow and properly latch and lock the fan cowl latches after the engine maintenance had been completed, and the failure of the maintenance inspector to detect and identify the unlatched condition. Contributing the incident is the design of the fan cowl latch assembly that can provide a false latch condition when the latch is neither latched or locked. Also contributing incident is the lack of adequate Airbus and Jet Blue fan cowl latch inspection guidance to detect and identify an unlatched condition.

Operated by JetBlue Airways (per NTSB report)

failure of the engine high pressure turbine active clearance control valve fuel rod supply tube coupling seal due to a cross-threaded B-nut as installed during original manufacture.

Operated by JETBLUE AIRWAYS CORP (per NTSB report)

An inadvertent in-flight encounter with turbulence during approach. Contributing to the accident was the passengers' failure to follow the instructions of the illuminated seatbelt sign.

Sanction: $13,200 · case closed 2015-10-22

Sanction: $8,000 · case closed 2015-03-31

Sanction: $11,000 · case closed 2015-05-15

Sanction: $12,500 · case closed 2014-02-26

Sanction: $14,000 · case closed 2014-04-01

Sanction: $14,000 · case closed 2014-04-01

Sanction: $10,000 · case closed 2015-06-16

Sanction: 13500 · case closed 2012-02-23

Sanction: $20,750 · case closed 2014-11-28

Sanction: $8,000 · case closed 2009-07-23

Sanction: $16,000 · case closed 2009-10-27

Sanction: $22,000 · case closed 2005-06-01

Part: FADEC — WARNING MESSAGE · airframe 6,774 hrs · 1,270 cycles

FLT # 841, JFK-DUB. (ETOPS) "ENG 2 CLASS 2 FADEC ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1)FAULT(S) INDICATED BY ENG (1 AND/OR 2) FADEC NO FAULTS REPORTED BY CFFDS REGARDING ADIRUS BUS )." (SUPPLEMENTAL INFORMATION TO FOLLOW).

Part: FUEL SYS — WARNING MESSAGE · airframe 9,221 hrs · 1,381 cycles

FLT 2261, BOS-MAD. (ETOPS) "FUEL AFT 2 ACT HI LVL ( HIGH LEVEL FUEL DETECTION SYSTEM ADDITIONAL CENTER TANK(S) ).

Part: WARNING MESSAGE — ILLUMINATED (AC GENERATOR) · airframe 9,441 hrs · 1,438 cycles

FLT 332, MXP-BOS. (ETOPS) "AC GEN MX MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN).

Part: GENERATOR — WARNING MESSAGE · airframe 9,441 hrs · 1,438 cycles

FLT#332, MXP-BOS. (ETOPS) AC GEN MX MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN ) OPEN

Part: HEATER — FAULTED (AOA PROBE) · airframe 9,180 hrs · 1,375 cycles

FLT 2261, BOS-MAD. (ETOPS) ANTI ICE STBY AOA MESSAGE ON ECAM. ( ANGLE OF ATTACK PROBE HEATERS (STBY).

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 1,627 hrs · 298 cycles

FLT 1034, SFO-BOS. EPSU TEST FAILED (MCDU BITE TEST) BATT PACK 1001WL, FWD LEFT. REFERENECE AMP TASK 335100-13-1 STEP 4 (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: GENERATOR — FAULT MESSAGE · airframe 20,188 hrs · 3,776 cycles

FLT 411, JFK-LAX. (ETOPS) "CLASS II AC GEN MSG AFTER SHUTDOWN ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN ).

Part: HF COMM — FAULTED (NR 1) · airframe 6,741 hrs · 1,264 cycles

FLT # 423, JFK-LAX. (ETOPS) "HF 1 INOP WILL NOT TUNE ( HIGH FREQUENCY (HF) COMMUNICATION SYSTEM (D-LRCS) HF 1 )." (SUPPLEMENTAL INFORMATION TO FOLLOW).

Part: ACTUATOR — FAILED (NR 1 A/C PACK) · airframe 9,417 hrs · 1,435 cycles

FLT 345, BOS-BCN. (ETOPS) "AIR PACK 1 REGUL FAULT ( AIR COND PACK RAM AIR INLET FLAPS ); REMOVED + REPLACED PACK 1 RAM AIR INLET FLAP ACTUATOR REF AMM 21-61-51 + PERFORMED OPS CH REF AMM 21-61-00. REACTIVATED PACK 1 INLET FLAP ACTUATOR + THIS CLEARS MDDR, MX-4 UPDATED."

Part: UNKNOWN — ODOR (CABIN) · airframe 12,739 hrs · 3,604 cycles

FLT # 528, GYE-JFK (AIRTURN BACK TO GYE). LEVEL 3 FUMES EVENT ON TAKE OFF. VERY STRONG FUMES IN THE BACK OF THE A/C. ONE FA HAD A BLEEDING NOSE AND ONE WAS VOMITING. LIGHT FUMES IN THE FRONT. ( BLEED AIR SUPPLY SYSTEMS ); (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — FUMES · airframe 74,064 hrs · 26,873 cycles

FLT 2584, MCO- JFK. FUMES AT ENG START, TAXI, & T/O, APPLIED FUMES PROCEDURES TO DISIPATE WITH PACK 2 OFF.

Part: PUMP — LEAKING (HYD SYS) · airframe 84,438 hrs · 30,879 cycles

FLT 585, JFK-RDU (AIRTURN BACK TO JFK) G RSVR KO LVL ON TAKEOFF-ECAM-HYD PAGE SHOWED B SYS RSVR LO LVL.. R & R GREEN SYS EDP (1030EK) IAW AMM 29-11-51 UP TO SUBTASK 29-11-51-860-001-A. OPS+LEAK CHK IAW AMM 29-11-51-400-010-A FROM SUBTASK 29-11-51-860-040 TO COMPLETION OF AMM TASK. OPS CHKS OK.

Part: PUMP — INTERMITTENT (RT FUEL) · airframe 11,829 hrs · 2,201 cycles

FLT 1548, LAS-JFK. (ETOPS) RIGHT TANK FUEL PUMP 1 INTERMITTENTLY INOP ( WING TANK PUMPS ). OPEN

Part: CABIN PRESS SYS — FAULTED · airframe 6,710 hrs · 1,259 cycles

FLT 842, DUB-JFK. (ETOPS) CABIN PRESSURE 2 FAULT ( AUTOMATIC CABIN PRESSURE CONTROL SYSTEMS SYSTEM 2 (CPC 2) ). OPEN

Part: A/C PACK — ODOR (NR 1) · airframe 67,352 hrs · 24,729 cycles

FLT 1447, HPN-TPA. ODOR OF DIRTY SOCKS AT GATE WITH APU RUNNING, IN COCKPIT. ALSO HAD TRANSIENT SOCK ODOR ON DESCENT, PACK 1 SELECTED OFF, ODOR DIMINISHED. COMPLIED W/ INFO NOTICE 2017-T015 STEPS 1&2. ODOR TYPE 1. DECONTAMINATION LEVEL A, WAS ACCOMPLISHED IAW AMM 21-00-00-615-802-A. ACFT OK FOR SERVICE.

Part: A/C PACK — ODOR (NR 1) · airframe 85,112 hrs · 30,819 cycles

FLT 953, JFK-PBI. DURING TAKEOFF, HAD FUME EVENT, SEEMED ISOLATED TO FWD GALLEY & FLIGHT DECK. FUMES DISAPATED IN FLIGHT DECK AFTER 5 MIN. F/A SMELLED FUMES, PERSISTED IN FWD GALLEY. RAN ISOLATION CHKLST, CONFIGURED WITH PACK 2 OFF & BLEED VALVE SHUT. ACCOMPLISHED INFO NOTICE 2017-T015L. VERIFIED ODOR IS PACK 1 TYPE 5, PACK 1 DEFFERED IAW LOG PG 4719202 ITEM 2. NO FUMES NOTED WITH PACK 1 OFF.

Part: STARTER — LEAKING (ZONE 100) · airframe 66,502 hrs · 23,652 cycles

FLT # 234, BOS-MCO. OIL SMELL FORM 15000FT TO THE GROUND DID ISOLATION CHECKLIST WAITED 3 MIN TURNED ON AND ODOR WAS AT THE SAME LEVEL 2; COMPLIED WITH INFO NOTICE 2017-T015M. ITEM DEFERED PER MEL 49-10-01. M PROCEDURE C/W C/B L41 AND L42 PULLED AND COLLAR. R & R APU STARTER IAW AMM 49-42-00. OPC GOOD/NO LEAKS. OK FOR SVC. )

Part: HF COMM — FAULTED (ZONE 200) · airframe 7,612 hrs · 1,421 cycles

FLT # 1023, JFK-LAX. (ETOPS) "HF RADIO SLOW TO TUNE GOOD RECEPTION BUT MOST TRANSMISSIONS WERE CLICKING AFTER A SECOND OR TWO ( HIGH FREQUENCY (HF) COMMUNICATION SYSTEM (D-LRCS) HF 1 )." (SUPPLEMENTAL INFORMATION TO FOLLOW).

Part: GENERATOR — FAULT MESSAGE · airframe 20,159 hrs · 3,770 cycles

FLT 323, JFK-LAX. (ETOPS) "AC GEN CLASS II MX MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY GPCU OR AC GEN )." (SUPPLEMENTAL INFORMATION TO FOLLOW).

Part: FLUID — LOW (RAIN REPELLANT) · airframe 19,983 hrs · 3,721 cycles

FLT 841, JFK-DUB. (ETOPS) "RAIN REPELLANT LOW ( RAIN REPELLENT SYSTEMS )." (SUPPLEMENTAL INFORMATION TO FOLLOW).

Part: HF COMM — FAULTED · airframe 7,612 hrs · 1,421 cycles

FLT 1023, JFK-LAX. (ETOPS) "HF RADIO SLOW TO TUNE GOOD RECEPTION BUT MOST TRANSMISSIONS WERE CLICKING AFTER A SECOND OR TWO ( HIGH FREQUENCY (HF) COMMUNICATION SYSTEM (D-LRCS) HF1 ). OPEN

Part: RELAY — FAILED · airframe 77,831 hrs · 28,172 cycles

FLT 1439, BOS-AUS (AIRTURN BACK TO BOS). NR 2 ENG EPR MODE FAULT ON CLIMB OUT AT APPROX FL 230. REPLACED P2/T2 PROBE NO HELP IAW 73-22-11. R & R RELAY BOX OPS CHECKED OK IAW 71-51-49-400-010-A.

Part: TRANSCEIVER — FAULTED (NR 1 HF) · airframe 6,678 hrs · 1,254 cycles

FLT 1079, BOS-EDI. (ETOPS) "WHEN ATTEMPTING TO TUNEHF-1, THERE IS NO TUNE WHEN ANTENNA IS TURNING AND AUDIO CUTS OUT FOR 15 SECONDS ( HIGH FREQUENCY (HF) COMMUNICATION SYSTEM (D-LRCS) HF 1 ). OPEN

Part: VALVE — FAULTED (NR 2 ENGINE) · airframe 19,326 hrs · 2,874 cycles

FLT # 1620, BOS-BOS. (ETOPS) ON ENG 2 START , GOT ECAM ENG 2 FUEL VALVE FAULT, FUEL VALVE NOT OPEN. R & R ENGINE NR 2 IFPC IAW AMM 73-11-01. OPS CHK GOOD. LEAK CHECK GOOD. NO FURTHER FAULTS DETECTED. GROUND VERIFICATION SUCCESSFUL.

Part: CONTROLLER — FAILED (NR 2 ENGINE) · airframe 19,326 hrs · 2,874 cycles

FLT 1620, BOS-BOS. (ETOPS) "ON ENG START GOT ECAM ENG 2 FADEC IDENT FAULT , FAULT LIGHT ON ENG 2 PEDESTAL WARNING LIGHT, R & R ENGINE NR 2 IFPC IAW AMM 73-11-01. OPS CHK GOOD. LEAK CHECKED GOOD. NO FURTHER FAULTS DETECTED. GROUND VERIFICATION SUCCESSFUL.

Part: UNKNOWN — ODOR (CABIN) · airframe 71,379 hrs · 25,872 cycles

FLT 404, SJU-RDU. FROM TAKEOFF THRUST TO 1000FT WE ENCOUNTERED A LEVEL 2 FUMES EVENT WE COMPLIED WITH THE FCOM PROCEDURE TURNING OFF PACK 1 AND SHUTTING THE X BLEED VALVE 4 MINS LATER WE TURNED EVERYTHING ON AND THE SMELL WENT AWAY. IN DESCENT ALSO GOT A LEVEL 2 SMELL IN THE FLIGHT DECK AND AFT GALLEY AREA.; C/W NOTICE 2017-T015M PERFORMED OPS TEST OF PACKS 1 AND 2 WITH APU BLEED FOR APPROX 90 MINS WITH NO ODOR PRESENT. TROUBLESHOT ODOR TO TYPE 10 WITH NO 30 DAY HISTORY . A/C OK FOR SVC.

Part: APU — ODOR (ZONE 100) · airframe 66,826 hrs · 24,044 cycles

FLT 1067, HPN-PBI, (DIVERTED TO JAX). COCKPIT ODOR EVENT ( PACKS ); COMPLIED WITH INFO NOTICE 20178-T015 ISOLATED FAULT TO TYPE 10 AMBIENT AIR, NO ODOR, NO 30 DAY HISTORY IAW TSM 05-50-00-810-085-B AS PRECAUTION PLACED PACK 1 ON MEL 21-52-01C, CAT C, MX 4 UPDATED PLACARD INSTALLED. DEACTIVATED AIR CONDITIONING PACK IAW AMM 21-51-00-040-002. PERFORMED APU WASH IAW TASK CARD NOTED. PERFORMED APU BLEED OPS CHK WITH BOTH PACKS IAW AMM 32-12-0. OPS CHKD GOOD. NO ODOR NOTED. THIS CLEARS MDDR 626671, MX-4 UPDATED, PLACARD REMOVED.

Part: A/C PACK — ODOR (ZONE 100) · airframe 66,636 hrs · 23,661 cycles

FLT 1042,MCO-ROC. SA NOTICED STRONG FUMES DIRTY SOCK ODOR DURING CLIMB MID CABIN. SA SMELLED DIRTY SOCK ODOR ON DESCENT. ACFT TO BE REPOSITIONED TO JFK FOR FURTHER T/S. MX-4 UPDATED, PLACARD INSTALLED. PERFORMED LEVEL B REMOVAL OF CONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM, LEAK AND OPS TEST GOOD, MX-4 UPDATED PLACARD REMOVED MCC NOTIFIED IAW AMM 21-00-00-615-803-A. REPLACED BOTH LT AND RT RECIRC FILTERS AS PERCAUTION TO ODOR, IAW AMM 21-21-41.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,148 hrs · 3,768 cycles

SFO-BOS (DIVERTED TO DEN). ODOR AFTER T/O & DURING CRUISE. REACHED A LEVEL 3 STATUS & DIVERTED TO DENVER. ( PACKS ). (OPEN)

Part: A/C PACK — ODOR (NR 1) · airframe 18,811 hrs · 2,844 cycles

FLT 220, SAN-BOS. FROM TAKEOFF ANDDURING CLIMB WE NOTICED A DIRY SOCK / LOCKER ACRID SMELL . THE SMELL WAS ONLY EVIDENT IN FLIGHT DECK WE COMPLETED THE FUME CHECKLIST. AFTER ISOLATING PACK 1 THE ODOR GREATLY SUBSIDED ( PACKS ); DEACTIVATED THE AIR CONDITION PACK (10HM) PER AMM TASK 21-51-00-040-002. COMPLIED WITH INFO NOTICE 2015-T015 STEPS 1 AND 2. IDENTIFIED ODOR TO PACK 1. LEVEL A WAS ACCOMPLISHED PER AMM 21-52-00. PACK 1 PLACED MEL 21-52-01A CAT C. MX-4 UPDATED PLACARD INSTALLED. (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: SEAL — DAMAGED (ZONE 100) · airframe 34,761 hrs · 6,895 cycles

FLT 1707, FLL-LAS. ABNORMAL VIBRATION AND LOUD HUMMING SOUND CONCENTRATED IN MID CABIN AROUND ROW 11- BOTH SIDES OF THE AIRCRAFT REPORTED B Y FA AND DH PILOTS IN CABIN - SUBTLE VIBRATION ROW 10-18; ACCOMPLISHED VIBRATION INSP TSM 05-50-00-810-801 AND IDENTIFIED SOURCE OF VIBRATION TO PANEL 191DT SEAL DAMAGE. PER TSM 53-35-00-810-801 APPLIED SPEED TAPE TO PANEL 191DT PANEL EDGES. AERODYNAMIC SEAL PLACED ON GMM SR320/321-51-001 FOR 50FC MDDR PER MCC SPEED TAPE APPLIED MX4 UPDATED. PEN

Part: A/C PACK — ODOR · airframe 18,811 hrs · 2,844 cycles

FLT 220, SAN-BOS. FROM TAKEOFF ANDDURING CLIMB WE NOTICED A DIRY SOCK, LOCKER ACRID ODOR . THE ODOR WAS ONLY EVIDENT IN FLIGHT DECK, COMPLETED FUME CHECKLIST. AFTER ISOLATING PACK 1 THE ODOR GREATLY SUBSIDED ( PACKS ); DEACTIVATED THE AIR CONDITION PACK (10HM) PER AMM TASK 21-51-00-040-002. COMPLIED WITH INFO NOTICE 2015-T015 STEPS 1 AND 2. IDENTIFIED ODOR TO PACK 1. LEVEL A WAS ACCOMPLISHED IAW AMM 21-52-00. PACK 1 PLACED MEL 21-52-01A CAT C. MX-4 UPDATED PLACARD INSTALLED. OPEN

Part: DOUBLER — CORRODED (ZONE 100) · airframe 7,309 hrs · 3,421 cycles

DURING HEAVY MAINTENANCE, EA AC26-609-01, FUSELAGE / REAR FUSELAGE / WASTE ACCESS DOUBLER FR 75-76 & STGR 32L-35L. CORROSION - TEMPORARY REPAIR (CONSIDERED MAJOR REPAIR)

Part: IGNITER — NOT REPORTED (ENGINE) · airframe 16,080 hrs · 2,393 cycles

FLT 2220, LHR-JFK. (ETOPS) IGNITER PLUGS REQ REPLACEMENT; R & R IGNITER PLUGS IAW AMM 74-21-41, OPS CHKD NORMAL ACFT OK FOR SVC.

Part: SEAL — LEAKING (ZONE 400) · airframe 9,893 hrs · 1,823 cycles

FLT 220, SAN-BOS. (ETOPS) FOUND OIL IN SPINNER OF # 2 ENG; REMOVED & REPLACED FAN SHAFT COVER SEAL IAW AMM 72-15-01, SEE DEFECT 4556649 FOR LEAK AND OPS TEST.

Part: FAN — FAILED (ZONE 200) · airframe 80,377 hrs · 29,218 cycles

FLT 588, MCO-ORH. AT FL 350 VERY HEAVY ELECTRICAL ODOR IN COCKPIT. CIRCUIT BREAKER X-18 POPPED AND ODOR SUBSIDED - LT RECIRC INOP FANS; R & R LT RECIRC FAN IAW AMM 21-21-51. OPS CK GOOD PLACARD REMOVED MX4 UPDATED

Part: FAN — FAILED (ZONE 200) · airframe 9,893 hrs · 1,823 cycles

FLT 220, SAN-BOS. MUSTY ODOR IN COCKPIT AND CABIN DURING DESCENT FROM 4000 FEET UNTIL LANDING PACK 1 OFF AND APU OFF. PACK ON.; (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: CONTROL UNIT — FAILED (WX RADAR) · airframe 19,875 hrs · 3,702 cycles

FLT 1926, LGW-BOS. (ETOPS) WXR/PWS PULL-UP SAFETY LOCK TOGGLE SWITCH IN INOP SWITCH SHOULD REQUIRED PULL TO GO FROM '1' TO 'OFF' BUC CAN BE KNOCKED 'OFF' WITHOUT PULLING; R/R WX RADAR CONTROL UNIT IAW AMM 34-41-12.

Part: WARNING MESSAGE — ILLUMINATED (CPC SYS) · airframe 6,593 hrs · 1,239 cycles

FLT 1548, LAS-JFK. (ETOPS) SHORTLY AFTER T/O K/E GOT THE FOLLOWING ECAM : CPC SYSTEM 2 FAULT THIS IS A HISTORY ITEAM. OPEN

Part: COOLING FAN — FAILED (ZONE 100) · airframe 86,871 hrs · 31,459 cycles

FLT 944, BZN-JFK. OIL FUMES EVENT INITIALLY OCCURED AT FL 250 ON DECENT. ODORS DISSIPATED FUMES AGAIN OCCURED ON FINAL APPROACH AT 3000FT. DID NOT FOLLOW ISOLATION GUIDE; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEPS 1 AND 2. IDENTIFIED ODOR TO BE APU OIL COOLING FAN. PERFORMED REMOVAL AND INSTALLATION OF APU OIL COOLING FAN PER AMM 49-52-51. OPS CHECK GOOD, NO LEAKS NOTED. DECONTAMINATION LEVEL A ACCOMPLISHED PER AMM 21-00-00-615-802-A. AIRCRAFT IS OK FOR SERVICE

Part: FIRE BOTTLE — FAILED (ZONE 100) · airframe 4,665 hrs · 2,216 cycles

FLT # 2324, MCO-DCA. CARGO BTL FAIL MESSAGE ILLUMINATED IN FLIGHT; VERIFIED W/CREW THAT MESSAGE ILLUMINATED AND EXTINGUISHED IN FLIGHT. INTERRIGATED OMS FOR CURRENT FAULTS - NONE FOUND. ACCOMPLISHED SATISFACTORY OPERATIONAL TEST FOR ASSURANCE - ALL GOOD , OK FOR CONT SERVICE. ALL WORK EFIM BD500AJ45450001AAAC21A AND AMP BD500AJ26000001AAA320A.

Part: WARNING MESSAGE — ILLUMINATED (FUEL SYS) · airframe 12,436 hrs · 2,281 cycles

FLT 1333, BOS-SFO. (ETOPS) FUEL, CLASS II MAINTENANCE MESSAGE. OPEN

Part: PRIORITY VALVE — FAILED (ZONE 700) · airframe 7,721 hrs · 3,552 cycles

FLT # 811, BOS-ORD(EMERGENCY DECLARED). HYD 1 LO QTY EICAS AT 36000. HYD 1 LO PRESS EICAS DESCENDING THROUGH 28000; FOR CORRECTIVE ACTION REFERENCE LP 4707576 ITEM 1 & 2 R/R OF PRIORITY HYD VALVE AND R/R OF ENG 1 EDP; FOUND MAJOR LEAK FROM LANDING GEAR PRIORITY VALVE R+R VALVE OPS CHECK GOOD IAW AMM 29-11-12.UPON INSP OF THE #1 HYDRAULIC SYS FOUND THE CASE DRAIN FILTER WITH METAL DEBRISR/R ENG #1 EDP IAW AMP 29-11-01 LEAK AND OPS CHECKS GOOD. NO DEFECTS NOTED ALS OFIF A FLUSH OF THE #1 HYDRAULIC SYS AND R/R ALL FILTES IAW AMP 29-10-00 PRESS AND QTY HOLDING NO DEFECTS NOTED AC GOOD FOR SVC

Part: PUMP — FAILED (ZONE 400) · airframe 7,721 hrs · 3,552 cycles

FLT # 811, BOS-ORD(EMERGENCY DECLARED). HYD 1 LO QTY EICAS AT 36000. HYD 1 LO PRESS EICAS DESCENDING THROUGH 28000; FOR CORRECTIVE ACTION REFERENCE LP 4707576 ITEM 1 & 2 R/R OF PRIORITY HYD VALVE AND R/R OF ENG 1 EDP; FOUND MAJOR LEAK FROM LANDING GEAR PRIORITY VALVE R+R VALVE OPS CHECK GOOD IAW AMM 29-11-12.UPON INSP OF THE #1 HYDRAULIC SYS FOUND THE CASE DRAIN FILTER WITH METAL DEBRISR/R ENG #1 EDP IAW AMP 29-11-01 LEAK AND OPS CHECKS GOOD. NO DEFECTS NOTED ALS OFIF A FLUSH OF THE #1 HYDRAULIC SYS AND R/R ALL FILTES IAW AMP 29-10-00 PRESS AND QTY HOLDING NO DEFECTS NOTED AC GOOD FOR SVC

Part: IDG — NOT REPORTED · airframe 10,286 hrs · 1,911 cycles

FLT 1534, SFO-BOS. (ETOPS) INSUFFICIENT INFO IN TASK CARD A320-24-21-00-920-802-A FOR ENG 1 IDG DRAIN & FILL, OIL FILTERS REPLACEMENT.; C/W AMM 24-21-51-960-801-A, REMOVED & REPLACED IDG 1 FILTERS, SERVICING.LEAK CHECKED GOOD. THIS ALSO C/W W/O 1513120.

Part: A/C PACK — ODOR (ZONE 100) · airframe 73,986 hrs · 26,838 cycles

FLT 545, ISP-PBI. LEVEL 2 FUMES EVENT ON DESCENT START AS A MILD DIRTY SOCK SMELL THEN AS A ALT GOT LOWER AND PACKS WHERE ON HP VALVES IN SWITCH TO A STRONG DIRTY SOCK SMELL BOTH PACKS TRIED TOO ISOLATE WHICH PACK BUT SEEMS TO BE BOTH PACKS O2 MASK WERE USED ; PERFORMED INSPECTION PER TSM 05-50-00-810-831-A. NO ACTIVE HYDRAULIC OR APU OIL LEAKS NOTED. COMPLIED W/ INFO NOTICE 2017-T015, STEPS 1 AND 2. IDENTIFIED ODOR TYPE 5 - PACK 1. DECONTAMINATION LEVEL A WAS C/W PER AMM 21-00-00-615-802. AND REPLACED RECIRC FILTERS IAW AMM 21-21-41.

Part: FUEL FILTER — NOT REPORTED (ZONE 400) · airframe 1,655 hrs · 304 cycles

FLT 842, DUB-JFK. (ETOPS), REF EC A7323031-01 ENG NR 2 FUEL FILTER INSPECTION AND REPLACEMENT NEEDED, R & R ENG NR 2 FUEL FILTER IAW AMM PW1100G-A73-11-0600A-720A-D OPS CHECK GOOD .

Part: A/C PACK — ODOR (ZONE 100) · airframe 74,352 hrs · 26,717 cycles

FLT 914, HPN-PBI. PASSING THRU 10000FT STRONG ODOR COMING FROM PACKS MADE BOTH PILOTS COUGH. COMPLETED MX-270/271 ODOR REPORT, COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10, AMBIENT AIR DURING DESCENT, IAW TSM 05-50-00-810-085-B/TSM 05-50-00-810-085-D. RAN & INSPECTED APU FOR LEAKS ALONG WITH ENGINES WITH NO LEAKS FOUND. UTILIZED BLEED AIR FROM APU AND ENGINES WITH NO ODOR PRESENT. AIRCRAFT IS OK FOR SERVICE. NO 30 DAY HISTORY.

Part: BLEED AIR SYS — FAILED (NR 1 ENGINE) · airframe 2,263 hrs · 1,087 cycles

FLT 372, SLC-JFK, AIR TURNBACK TO SLC. ENG 1 BLEED FAIL FAILED AFTER T/O RAN ECL WHICH LIMITED ALT TO 31000 FT, ENGINE BLEED PRESSURE REGULATING SHUTOFF VALVE (PRSOV) LEFT SIDE ENGINE BLEED OFF, ITEM PLACED ON MEL 36-12-01A CAT C DEACTIVATED AFFECTED LT PRSOV IAW AMP BD500-A-J36-11-01-00AAA-560A-A, ACCOMPLISHED METHOD ONE. VERIFIED NO EVIDENCE OF EXCESSIVE HPV LEAKAGE, A DAMAGED HPV SEALING RING, A MISSING OR BROKEN RETAINING CLIP, OR ANY OTHER CONDITION REQUIRING HPV REPLACEMENT IAW AMP BD500-A-J36 -11-02- 00AAA- 369A-A, HIGH PRESSURE VALVE (HPV) CLIP & SEALING RING. AIRCRAFT OK TO CONTINUE UNDER MEL. PER MCC STEPHEN MX4 UPDATED PLACARD INSTALLED. OPEN.

Part: A/C PACK — CONTAMINATED (NR 1) · airframe 9,877 hrs · 1,820 cycles

FLT 1833, BOS-SFO. STRONG MUSTY ODOR UPON TAKEOFF ODOR ISOLATION DISTINGUISHED PACK 1 ODOR IMPROVED WITH PACK 1 OFF YET DID NOT COMPLETELY GO AWAY 2 FLT ATTENDANTS HAD MILD IRRITATION AIRWAY LEVEL 2 EVENT.ODOR RETURNED ON DESCENT AND CABIN WITH PACK 1 OFF APU OFF NOT AS STRONG BUT DEFINITE MUSTY SMELL. ; CW INFO NOTICE 2017-T015M AND PERFORMED A LEVEL 2 ACS DECONTAMINATION. IDENTIFIED ODOR COMING FROM PACK 1 DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER AMM 21-00-00-615-803-A PACK 1 AND APU DEFERRED ON LOGPAGE 4556640 ITEM 1 AND 2.REFERENCE LOGPAGE 4556637 ITEN 1 PACK 1 AND APU DEFERRED ON LP 4556640 ITEM 1 AND 2. ITEM PLACED ON MEL 49-10-01B CAT C MCC ROLAND NOTIFIED, DISPATCH NOTIFIED, MX-4 UPDATED, PLACARD INSTALLED, ACT FUEL TRANSFER TO CENTER TANK ACCOMPLISHED PER MEL 49-10-01B. OPEN