N334JB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JETBLUE AIRWAYS CORPORATION (YENA) | Operator | 2023-05-13 – 2023-05-13 | Operator named in NTSB report |
| JETBLUE AIRWAYS CORP | Operator | 2023-05-13 – 2023-05-13 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FLT#2254, DCA-BOS. 'DESCENTING THROUGH 13000FT #1 FA REPORTS OF PUNGENT ODOR AND BURNING GAS SMELL AROUND DOOR L1; PERFORMED CABIN ODOR EVENT INSPECTION, NO DEFECTS NOTED REF FIM TASK 21-20-00-810-801-A. A/C OK FOR SVC. ENG RUN, BLEED OP CHECKS GOOD.'
FLT#68, CHS-VOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO CHS) 'AFTER TAKEOFF, BLEED 1 LEAK EICAS MSG DISPLAYED ALONG WITH BLEED 2 FAIL EICAS MSG COMPLETED QRH FOR BOTH. LEAK MSG CLEARED BUT BLEED 2 FAIL STAYED. ( ENGINE BLEED SYSTEMS CROSSBLEED OPERATIVE ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#2534, PBI-DCA. ' LG NO DISPATCH ON LDG; INTERRIGATED CMC AND FOUND NLG DOWNLOCK 2 SHOWS OPEN ALL TIMES. FAULT CODE 32612206PSS. REMOVED AND REPLACED NO 2 NLG DOWNLOCK SENSOR ALL GOOD ALL WORK FIM 32 61 00 810 885 A.'
DURING HEAVY MAINTENANCE: FWD CVFDR REQUIRES REMOVAL DUE TO SIGNIFICANT EVENT REPORTED ON LOG PAGE 3387496-1, SEVERE TURBULENCE ENCOUNTER AND CONVECTIVE HAIL ENCOUNTER. AS PER GMM 6.13.4. P/N 1605-01-00 S/N 335; FWD CVFDR REMOVED IAW E190 AMM 31-31-01-000-801-A. NO DEFECT NOTED ITEM HAS BEEN QUARANTINE. ENCOMPASSED IN TOMX WO 2296 / NR 00002.'
DURING HEAVY MAINTENANCE: DAMAGE ALL OVER A/C EXTERIOR OF AIRCRAFT- RADOME- ENG NARCELLS -WING LEADING EDGE; CHAPTER 05-50-28-210-801A INSPC/W TOMX WO 2296, NR 00068, CH 05-50-60 HAIL STRIKE INSP C/W TOMX WO 2296 NR 00010 RADOME REPL NR00042, ENGINLET REPLACEMENTSON NR 00038, 00039. BELLY FAIRING ON MDDR# , AND ENGINEERING EA'S ON WO# 1255215, 1275034, 1276059, AND 1267779 FOR PERMANENT AND TEMPORARY REPAIRS FOR FUSELAGE, EMPENNAGE, WINGS, SLATS. AIRCRAFT HAS BEEN INSPECTED AND DAMAGE ADDRESSED.
DURING HEAVY MAINTENANCE: ENG#2 SHUTDOWN DUE VECTOR INTO EXTEREM/SERVER WEATHER ITT EXCEEDANCE FIRE BOTTLE /HANDLE PULLED; REF TOMAX WO# 2296 FOR WORK PERFORMED CHAPTER 05-50-18/600 INSPECTION COMPLIED WITH FOR ITT EXCEEDANCE ON #2 ENGINE TOMX NR# 00078 C/W, ENGINE #2 BOROSCOPING ON NR# 0008 C/W, ENGINE #2 FIRE BOTTLE REPLACEMENT NR# 00051 C/W, ENGINE INLET ASSY REPLACEMENT NR# 00035 CW, ENGINE #2 RUNUP NR# 00057 CW, DVDR ANALYSIS FOR OVERTEMP INCIDENT PERFORMED BY AVIONICA. AND JETBLUE WO# 1257676 TASK CARD E23-788-01 TALLY 5026 ENG CF34-10E ESN 424561 -FAN OGV FERRY FLIGHT RELIEF UNDER MDDR 523462 FOR 2 FC. TO ACCOUNT FOR ALL WORK PERFORMED TO #2 ENGINE. AND NACELLES.
DURING HEAVY MAINTENANCE: SEVERE TURBULANCE ENCOUNTER AND SEVERE CONVECTIVE HAIL ENCOUNTER; FUSELAGE REPAIRS PERFORMED UNDER WO 1286900 AND 1279523 & 1279523 AND CAS WO# 334-1286900. ENGINE WORK PERFORMED BY EMBRAER MCN SOW# H9368 JB WO# 1284880. ALL DAMAGES CAUSED BY HAIL EVENT HAVE BEEN ADDRESSED. (DENT AND BUCKLE LOG LISTS ALL REPAIRS BY EA#, NUMBERS LISTED ON FUSELAE)( #2 ENGINE AND AIR INLET COWL REPLACED) (FOUR FWD FUSELAGE SKINS REPLACED).'
DURING HEAVY MAINTENANCE: AFT CVFDR REQUIRES REMOVAL DUE TO SIGNIFICANT EVENT REPORTED ON LOG PAGE 3387496-1, SEVERE TURBULENCE ENCOUNTER AND CONVECTIVE HAIL ENCOUNTER. AS PER GMM 6.13.4. P/N 1605-00-00 S/N 287 / AFT CVFDR REMOVED IAW E190 AMM 31-31-01-000-801-A. NO DEFECT NOTED ITEM HAS BEEN QUARANTINE. ENCOMPASSED IN TOMX WO 2296 / NR 00003.
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / UPPER SKIN ABOVE WINDSHIELD FRAME BTWN STGR 4R-5R / MISDRILLED HOLES - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FWD LOWER SKIN BETWEEN FR1-7 & STGR 24R-25R AND 24L-25L / HAIL DAMAGE - TEMPORARY REPAIR (CONSIDERED A MAJOR REPAIR)
FLT# 8595, FLL-QRO. "DAMAGE ALL OVER A/C EXTERIOR OF AIRCRAFT- RADOME- ENG NARCELLS -WING LEADING EDGE; CHAPTER 05-50-28-210-801A INSPC/W TOMX WO 2296, NR 00068, CH 05-50-60 HAIL STRIKE INSP C/W TOMX WO 2296 NR 00010 RADOME REPL NR00042, ENGINLET REPLACEMENTSON NR 00038, 00039. BELLY FAIRING ON MDDR# , AND ENGINEERING EA'S ON WO# 1255215, 1275034, 1276059, AND 1267779 FOR PERMANENT AND TEMPORARY REPAIRS FOR FUSELAGE, EMPENNAGE, WINGS, SLATS. AIRCRAFT HAS BEEN INSPECTED AND DAMAGE ADDRESSED."
FLT# 8595, FLL-QRO. "A/C OVERSPEED IN THE SEVERE STORM; OVERSPEED INSPECTION FOR EXCEEDANCE REPORTED BY CREW IS COMPLIED WITH PER E190 AMM CHAPTER 05-50-06 SUBTASK 210-005-A DVDR ANALYSIS BY AVIONICA LLC. SHOWS ALL THREE CONDITIONS WERE MET, AND THE AIRCRAFT CAN RETURN TO SERVICE.(CONDITION 1. THE SPEED STAYED BELOW 330KIAS, MACH STAYED BELOW M 0.83 THROUOUT THE FLIGHT, CONDITION 2. THE OVERSPEED EVENT DID NOT LAST MORE THAT 10 SEC. CONDITION 3 THERE WAS ONLY ONE OVERSPEED EVENT IN THE SAME FLIGHT.)"
FLT# 8595, FLL-QRO. "ENG#2 SHUTDOWN DUE VECTOR INTO EXTEREM/SERVER WEATHER ITT EXCEEDANCE FIRE BOTTLE /HANDLE PULLED; REF TOMAX WO# 2296 FOR WORK PERFORMED CHAPTER 05-50-18/600 INSPECTION COMPLIED WITH FOR ITT EXCEEDANCE ON #2 ENGINE TOMX NR# 00078 C/W, ENGINE #2 BOROSCOPING ON NR# 0008 C/W, ENGINE #2 FIRE BOTTLE REPLACEMENT NR# 00051 C/W, ENGINE INLET ASSY REPLACEMENT NR# 00035 CW, ENGINE #2 RUNUP NR# 00057 CW, DVDR ANALYSIS FOR OVERTEMP INCIDENT PERFORMED BY AVIONICA. AND JETBLUE WO# 1257676 TASK CARD E23-788-01 TALLY 5026 ENG CF34-10E ESN 424561 -FAN OGV FERRY FLIGHT RELIEF UNDER MDDR 523462 FOR 2 FC. TO ACCOUNT FOR ALL WORK PERFORMED TO #2 ENGINE. AND NACELLES."
DURING HEAVY MAINTENANCE: FWD CVFDR REQUIRES REMOVAL DUE TO SIGNIFICANT EVENT REPORTED ON LOG PAGE 3387496-1, SEVERE TURBULENCE ENCOUNTER AND CONVECTIVE HAIL ENCOUNTER. AS PER GMM 6.13.4. P/N 1605-01-00 S/N 335; FWD CVFDR REMOVED IAW E190 AMM 31-31-01-000-801-A. NO DEFECT NOTED ITEM HAS BEEN QUARANTINE. ENCOMPASSED IN TOMX WO 2296 / NR 00002.
DURING HEAVY MAINTENANCE: AFT CVFDR REQUIRES REMOVAL DUE TO SIGNIFICANT EVENT REPORTED ON LOG PAGE 3387496-1, SEVERE TURBULENCE ENCOUNTER AND CONVECTIVE HAIL ENCOUNTER. AS PER GMM 6.13.4. P/N 1605-00-00 S/N 287; AFT CVFDR REMOVED IAW E190 AMM 31-31-01-000-801-A. NO DEFECT NOTED ITEM HAS BEEN QUARANTINE. ENCOMPASSED IN TOMX WO 2296 / NR 00003.
FLT#8595, BOS-FLL. (AIRCRAFT DECLARED AN EMERGENCY) ' SEVERE TURBULANCE ENCOUNTER AND SEVERE CONVECTIVE HAIL ENCOUNTER.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#1073, JFK-BNA. 'AIRCRAFT ENCOUNTERED MOD TO SEVERE TURB. AFT GALLEY CART FELL OVER; PERFORMED SEVERE TURBULENCE CHECK IAW AMM 05-50-28-210-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.'
DURING HEAVY MAINTENANCE: CPCP FINDING. CORROSION ON SHEAR CLIP BTW FR 88 & BTW STRG 28-27 RH; ALL WORK ACCOMPLISHED ON TOMEX NR 00274, SHEAR CLIP BTW FR 88 & BTW STRG 28-27 RH WAS REPLACED PER EMB 190 SRM 51-41-01, SRM 51-42-01 AND SRM 51-43-03. (CONSIDERED A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: EXTERNAL EMERGENCY LIGHT AFT LH WAS FOUND INOP REF WEEKLY CHECK; REF TOMX N/R 00016 WO 2078 AFT EXTERNAL EMERGENCY LIGHT LH WAS REPLACED PER EMB 190 AMM 33-50-25-000-802-A AND AMM 33-50-25-400-802-A. OPERATIONAL TEST SATISFACTORY.
DURING HEAVY MAINTENANCE, CRACK FOUND ON HINGE OF RUDDER AT UPPER PCU. RUDDER REPLACED IAW WO 1178489 TASK CARD # E190-27-21-05-400-801.
DURING HEAVY MAINTENANCE: CPCP FINDING: CORROSION ON FLOOR STRUCTURE BEAM, BETWEEN FR 12 AND FR 14 AT Y=250 RH; ALL WORK ACCOMPLISHED ON TOMEX NR 00280, CORROSION ON FLOOR STRUCTURE BEAM, BETWEEN FR 12 AND FR 14 AT Y=250 RH WAS REMOVED, AND EVALUATED, THEREFORE IT IS OUT OF LIMITS. THE FLOOR STRUCTURE BEAM WAS REPLACED FOR ONE NEW PER EMB190 SRM 51-41-01, SRM 51-41-02, SRM 51-43-04, AND SRM 51-43-03. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. (CONSIDERED A MAJOR REPAIR)
FLT#315, SYR-JFK. 'IN DESCENT THE PARKING BRAKE "ON" MSG. FLASHED INTERMITTENTLY. THE "PRKG BRK NOT RELEASED" MSG. DISPLAYED SEVERAL TIMES BUT NEVER REMAINED DISPLAYED. QRH CHECKLIST PERFORMED; T/S TO EMERGENCY/PARKING BRAKE PRESSURE SWITCH OF THE OUTBD (HYDRAULIC SYSTEM 1) BRAKE SYST. REMOVED AND REPLACED SYST 1 PRESSURE SWITCH. REF TO AMM 32-44-09. FUNCTIONAL TEST AND LEAK CHECK GOOD.'
FLT#6102, RIC-MCO (AIRCRAFT DECLARED AN EMERGENCY INTO MCO). ' AVNX MAU1 FAILURE DURING ARRIVAL INTO MCO QRH PROCEDURE ACCOMPLISHED AFTER AVNX MAU1 FAIL MESSAGE. MODERATE VIBRATIONS WERE FELT DIRECTLY BELOW THE FLIGHT DECK IN THE FWD EBAY VIBRATIONS WERE ACCOMPANIED BY MIL PITCH DEVIATIONS AND SMAL SURGES; TS PER E190 FIM 31-41-00-810-88S-A STEP F-6-1. REMOVED AND REPLACED MAU1 PWR SUPPLY 1 CARD PER E190 AMM 31-41-02. OPS CHECK OK, NO FAULTS AT THIS TIME.'
FLT#1734, PBI-DCA. (AIRCRAFT DIVERTED TO RIC).' DURING CRUISE FLT FL370 WE HAD A/P AND A/T FAIL. FMS1 INOP, ACARS INOP. ROOT CAUSE ON EICAS SHOWED BRAKE RH FAULT, BRAKE LH FAULT CAUTION; REPLACED NIC PROC MODULE 1 MAU1 FAULTS REMAIN. ITEM REMAINS OPEN SEE LP 3292103 IAW 31-41-04.' (SUPPLEMENTAL TO FOLLOW).
FLT#2020, FLL-BOS. 'AILERON RH FAIL; FOLLOWED FIM TASK 27-03-00-810-92G-A. RESET A/C POWER. PERFORMED P-BIT SUCCESSFULLY. PERFORMED RETURN TO SERVICE TEST WITH NO DEFECTS. TRANSITORY CONDITION OF FLIGHT CONTROL SYSTEM. A/C OK FOR SERVICE.'
FLT 232, LGA-BOS. DOOR DISARM INDICATION NOT SHOWING FULLY SHOWING DISARMED. VENT FLAP ARMING HANDLES NOT LINING UP; PERFORMED FIM TASK 52-11-00-810-808-A FOUND DRY ARM/DISARM INDICATOR LINKAGE AND ARM/DISARM LINKAGE. CLEANED AND LUBED OPS CHECKS NUMEROUS TIMES. NO DEFECTS NOTED, OK TO CONTINUE
FLT # 625. EWR-CHS(DIVERTED TO JFK). COMPLETE LOSS OF HYD SYS 2 FLUID IN FLIGHT LANDING 96000LB 300FPMOR LESS; FOUND #2 HYD FILTER MANIFOLD TOP RETURN LINE LOOSE. TIGHTEN HYD LINE + LEAKED CHK REF LOG PG 3202515 FOR FILTER CHANGE AND SERVICING. REPLACED RETURN LINE + PRESSURE LINE FILTERS FOR #2 HYD SYS MANIFOLD PRECAUTIONARY AMM 29-11-05/400 LEAK CHECK GOOD.PERFORMED A,MM 05-50-14-200-901-A FOUND NO DEFECTS A/C IS BACK IN NORMAL CONFIGURATION A/C OK FOR CONT SVC
FLT 1318, JFK-BOS. LH AFT WTB FAIRING EXTERNAL EMERGENCY LIGHT ASSY INOP; R & R ELPU #5 IAW AMM 33-50-01.OK FOR SERVICE.
FT # 2752, SJU-TPA. DURING TASK CARD EXTERNAL EMERGENCY LIGHT OPERATIONAL TEST FOUND EXTERNAL LIGHTS LEFT FWD AND AFT INOP. ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT ); RESISTANCE FLUCTUATION BET P0753 TO LIGHT P3324 REF WM: 33-50-50, CLEANED CONNECTOR P0753, RESISTANCE CK GOOD. ELPU #4 & #6 ALSO DEFECTIVE. R & R ELPU #4 & #6 IAW AMM: 33-50-01. EMER LTS OPS GOOD. MEL CLEARED, MX-4 UPDATED, PLACARD REMOVED.
FT # 2752, SJU-TPA. DURING TASK CARD EXTERNAL EMERGENCY LIGHT OPERATIONAL TEST FOUND EXTERNAL LIGHTS LEFT FWD AND AFT INOP. ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT ); RESISTANCE FLUCTUATION BET P0753 TO LIGHT P3324 REF WM: 33-50-50, CLEANED CONNECTOR P0753, RESISTANCE CK GOOD. ELPU #4 & #6 ALSO DEFECTIVE. R & R ELPU #4 & #6 IAW AMM: 33-50-01. EMER LTS OPS GOOD. MEL CLEARED, MX-4 UPDATED, PLACARD REMOVED.
FLT 1479, DCA-FLL. FOUND CEILING EMERGENCY LIGHT AT ROW 17 OUT; REPLACED POSITION #6 BATTERY CHARGER BY R2 DOOR FOUND CHECKS GOOD PER AMM 33-50-01.
FLT 1646, CLT-BOS. CEILING EMERGENCY LIGHT AT ROW 17 INOP; R & R #6 EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECK GOOD.
FLT 1446, CLT-BOS. L1 DOOR UNABLE TO DISARM; REMOVED L1 DOOR SLIDE ADJUSTED GIRT BAR IAW CH 52-11-40. OPS CHECK NORMAL. INSTALLED L1 DOOR SLIDE IAW AMM CH 25-65-01. OPS CHECK NORMAL A/C OK FOR CONT SERVICE.
THE LEFT AFT EMERGENCY LIGHT ON THE EXTERIOR WING TO BODY FAIRING FOUND INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY NR 6 IAW MM 33-50-01. OPS CHECKED GOOD.
CORROSION WAS DISCOVERED ON AFT CARGO DOOR SURROUND LOWER BEAM, THE BEAM WAS REPLACED IAW SRM 51-43-04, AND 51-41-02 REV 3S.
CORROSION WAS DISCOVERED ON THE AFT CARGO DOOR SURROUND LOWER BEAM, UNDERNEATH FWD LATCH FITTING. REPLACED IAW SRM 51-43-04 AND SRM 51-41-02, REV C.
CORROSION WAS DISCOVERED ON THE AFT CARGO DOOR CUTOUT FINGER DOUBLER BETWEEN FRAMES 77 - 78+3, RBL 14. REPLACED THE FINGER DOUBLER IAW SRM 51-41-02, REV 3S, AND SRM 51-43-04, REV 3S.
FLT 316, JFK-SYR, AIR RETURN. SLAT FAILURE WAS REPORTED FOR THE THIRD TIME ON THIS AIRCRAFT. RIGHT WING SLAT ACTUATOR NR 6 TRIPPED. R & R RIGHT SLAT ACTUATOR NR 6 IAW AMM 27-81-01. SLAT CONTROL SYSTEM MECHANICAL & ELECTRICAL RIGGING PERFORMED ON RIGHT WING PER AMM 27-80-00. OPS CHECK PASSED. NO CURRENT FAULTS NOTED. RESECURED SLAT 3 MECHANICAL STOP BOLT PER AMM 27-81-07.
FLT 316, JFK-SYR, AIR RETURN. SLAT FAILURE WAS REPORTED FOR THE THIRD TIME ON THIS AIRCRAFT. RIGHT WING SLAT ACTUATOR NR 6 TRIPPED. R & R RIGHT SLAT ACTUATOR NR 6 IAW AMM 27-81-01. SLAT CONTROL SYSTEM MECHANICAL & ELECTRICAL RIGGING PERFORMED ON RIGHT WING PER AMM 27-80-00. OPS CHECK PASSED. NO CURRENT FAULTS NOTED. RESECURED SLAT 3 MECHANICAL STOP BOLT PER AMM 27-81-07.
AFTER SELECTING FLAPS 1 RECEIVED AMBER SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, COMPLIED WITH QRH AND FAULT/FAIL REMAINED. EMERGENCY DECLARED, ACFT LANDED UNEVENTFULLY. R & R WIRING HARNESSES W611 & W612, R & R BOTH RT OTBD SKEW SENSORS IAW AMM 27-83-01, AND R & R MAU 3 GENERIC I/O CARD SLOT 9/10 IAW AMM 31-41-06. FOLLOWED TSI 15983 FOR THE REPAIR.
AFTER SELECTING FLAPS 1 RECEIVED AMBER SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL,COMPLIED WITH QRH AND FAULT/FAIL REMAINED. EMERGENCY DECLARED, ACFT LANDED UNEVENTFULLY. I R & R WIRING HARNESSES W611 & W612, R & R BOTH RT OTBD SKEW SENSORS IAW AMM 27-83-01, AND R & R MAU 3 GENERIC I/O CARD SLOT 9/10 IAW AMM 31-41-06.
AFTER SELECTING FLAPS 1 RECEIVED AMBER SHAKER ANTICIPATED, SPOILER FAULT, SLAT FAIL, COMPLIED WITH QRH AND FAULT/FAIL REMAINED. EMERGENCY DECLARED, ACFT LANDED UNEVENTFULLY. R & R WIRING HARNESSES W611 & W612, R & R BOTH RT OTBD SKEW SENSORS IAW AMM 27-83-01, AND R & R MAU 3 GENERIC I/O CARD SLOT 9/10 IAW AMM 31-41-06. FOLLOWED TSI 15983 FOR THE REPAIR.
GATE RETURN, STRONG ACRID ODOR PERMEATED THE CABIN ON TAXI OUT. R & R K5 RELAY AND SPDA 2 DC POWER MODULE IAW AMM 24-61-13. OPS CHECK GOOD. THERE WERE 2 FANS THAT WERE REPLACED IN THE PROCESS, 1 DURING TROUBLESHOOTING AND ANOTHER GOT OVERHEATED AND THAT IS HOW IT WAS DISCOVERED THAT THE POWER BEING SUPPLIED TO THE FAN WAS THE ISSUE. THE FAILED DC POWER MODULE WAS CAUSING THE ODOR.
RIGHT FORWARD GALLEY COFFEEMAKER HAS AN ELECTRICAL ODOR, TURNED OFF SYSTEM AND ODOR DISSIPATED. OPERATIONAL CHECKED FORWARD COFFEEMAKER. OPERATIONAL CHECKED GOOD. NO ODORS NOTED.
LEFT FORWARD GALLEY COFFEEMAKER HAS AN ELECTRICAL ODOR. TURNED OFF SYSTEM AND ODOR DISSIPATED; R & R FORWARD COFFEEMAKER IAW AMM 25-35-00. OPS CHECK GOOD.
SLAT FAIL EICAS MESSAGE BEFORE MOVING FLAPS SLAT HANDLE AFTER TAKEOFF SLATS SHOWED 3 AND FLAPS SHOWED 1. EMERGENCY DECLARED, ON LANDING FLAPS WENT FULL,SLATS STAYED AT 3. R & R RT SLAT 2-3 AND RT SLAT 3-4 SKEW SENSORS IAW AMM 27-83-01. ALSO, R & R OF RIGHT SLAT 2-3 AND SLAT 3-4 SENSOR HARNESSES IAW AMM 27-83-07. NO FAULTS.
SLAT FAIL EICAS MESSAGE BEFORE MOVING FLAPS SLAT HANDLE AFTER TAKEOFF. SLATS SHOWED 3 AND FLAPS SHOWED 1. EMERGENCY DECLARED, ON LANDING FLAPS WENT FULL,SLATS STAYED AT 3. R & R RT SLAT 2-3 AND RT SLAT 3-4 SKEW SENSORS IAW AMM 27-83-01. ALSO, R & R OF RT SLAT 2-3 AND SLAT 3-4 SENSOR HARNESSES IAW AMM 27-83-07. NO FAULTS.
DIVERTED, ON APPROACH, SLAT FAIL EICAS MESSAGE WHEN MOVING FLAPS FROM 0 TO 1, SPOILER FAULT AND SHAKER ANTICIPATED EICAS MESSAGE. R & R RT WING 3-4 SKEW SENSOR AND OPS CHECKED IAW MM 27-83-01-04 AND 27-83-01-05. ALL CHECKED NORMAL.
DURING MAINTENANCE WALK AROUND, FOUND RT MLG UPPER SIDE STAY ASSEMBLY SUPPORT MISSING HARDWARE AND NUT BACKED OFF AT TRUNNION. ACCOMPLISHED TORQUE OF SUPPORT ASSY NUT IAW AMM SUB TASK 32-11-05-420-006-A, ITEM 1H, 1I, AND 1J. REPLACED MISSING LOCKING NUT, REF FIG 401, ITEM 4 AND REPLACED MISSING LOCKING RING, REF FIG 401, ITEM 3. NOTE: ACFT WAS SENT ON SPECIAL FLIGHT AND MLG SIDE STAY WAS REMOVED, CLEANED, INSPECTED AND REINSTALLED. ALL OPS CHECKS NORMAL.
FLT 625 JFK-HOU, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO IAD DUE TO SLAT FAIL, SHAKER ANTICIPATED, AOA LIMITER FAIL, AP FAIL, SPOILER FAULT, AT LEVEL 360. LANDED FLAPS 2 AND SPOILERS DID WORK UPON LANDING. SLAT ACTUATOR GEN VISUAL INSPECTION REF AMM 27-81-01-210-801A NO FAULTS NOTED. REMOVED AND REPLACED SLAT/FLAP POSITION SENSOR REF AMM 27-83-06 AND FIM TASK 27-83-00-810-806A. OPS CHECK GOOD.
FLT 462 RSW-BOS, CREW DECLARED EMERGENCY DUE TO SLAT FAIL MESSAGE IN FLIGHT WITH FLAPS/SLATS AT ZERO. PERFORMED SUBTASK 810-058A OF FIM 27-83-00810-814A. CLEARED INHIBITS RIGGED SLATS FLAP SYSTEM, NO FAULTS NOTED. ON 1/30/12 TSI WAS ISSUED DUE TO PREVIOUS REPORTS OF SLAT FAIL REFERENCE FIM 27-83-00-810-814-A FOR FAULT CODE 27831005ACE. TECHNICIAN REMOVED AND REPLACED LEFT WING 2/3 SKEW SENSOR AND 511 HARNESS DUE FOUND SHORTED TO GROUND.