N706JB
Registered owner: JETBLUE AIRWAYS CORP, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| JETBLUE AIRWAYS CORPORATION (YENA) | Operator | 2011-02-19 – 2011-02-19 | Operator named in NTSB report |
| JETBLUE AIRWAYS CORP | Operator | 2011-02-19 – 2011-02-19 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FLT 65, JFK-ABQ(DIVERTED TO ICT). PAX AND FA'S REPORTED STRONG ODOR OF GASOLINE IN THE AFT CABINN AND AFT GALLEY AFTER LANDING CUSTOMERS SAID IT WAS MORE OF A ROTTEN EGG ODOR THAN GASOLINE ( PACKS ); PERFORMED LEVEL C DECONTAMINIATION APG 1 IAW AMM 05-50-00-808-831-A, FOUND BY NORMAL OF ECS IAW REF AMM 21-00-00-615-804-A, DECONTAMINATION OF BLEED AIR DUCTS IAW AMM 36-10-00-615-802-A. OPS CHKD GOOD NO ODOR NOTED.
FLT 141, BDI--PBI. LEVEL 3 FUME ON DECENT. APPLIED ODOR/ FUME ISOL/ PROCEDURE PACK 1 / FLIGHT DECK; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEPS 1 AND 2. IDENTIFIED ODOR TYPE 1 (APU) DEACTIVATED DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00-810 AC OK FOR SERV."
DURING MAINTENANCE: "EMERG BATT 10WL FAILED TEST; REMOVED NAD REPLACED 10WL EMERG BATT IAW AMM 33-51-00 OPS CHK GOOD. A/C OK CONT SVC."
FLT#1461, LGA-PBI. 'FLIGHT ATTENDANT REPORTED SMELL A FLUID BURNING SMELL AT 1800F DECENT TO APPROXIMATELY 1000 FT SMELL CAME BACK JUST BEFORE LANDING FA SMELL 8 OF 10 REPORTS; PER INFO NOTICE 2017-T015L PERFORMED TSM 05-50-00-810-831-A ODOR VERIFIED TO BE MISCELLANEOUS TYPE 10 PER TABLE 2 RAN BOTH ENGS IAW 71-00-00 NO ODOR NOTED, SECTION A COMPLIED WITH , A/C OK FOR SERVICE. '
FLT#1962, PBI-LGA. '2 AFT F/A'S REPORTED FUME EVENT AT GATE ARRIVAL. IT BEGAN AT TOP OF DESCENT AND DISSIPATED DURING THE DESCENT. NO APU WAS OPERATING; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, AMBIENT AIR HIGH HUMIDITY PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085-D. AIRCRAFT OK FOR SERVICE.'
FLT#977, BOS-LAS. (AIRCRAFT DIVERTED TO ORD) 'AFT CABIN INDICATED 54* IN FLIGHT; PERFORMED OPERATIONAL TEST OF THE PACK TEMP CONTROL SYSTEM IAW AMM 21-61-00-710-001. TEST REVEALED TRIM AIR VALVE 12HK AND 13HK FAILED. WHEN TWO TRIM AIR VALVES FAIL THE HOT AIR VALVE WILL AUTOMATICALLY CLOSE. RESET ACSC 2 (57HH) AND RAN PACK TEMP CONTROL SYSTEM TEST AGAIN. ALL FAULTS CLEARED. OPERATED BH PACKS IN ALL RANGES COLD TO HOT AND AFT CABIN.
DURING HEAVY MAINTENANCE: DENT ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00052) PERFORMED PERMANENT REPAIR LOC. ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L IAW A320 SRM 53-21-11-300-093, THIS REPAIR IS CLASSIFIED AS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT AT 60,000FC/120,000 FH, SUBSEQUENT INSPECTION UNTIL 60,000FC/120,000 FH AT INTERVALS OF TBD, INSPECTION METHOD TBD IAW SRI 53-21-11-205-073 TABLE 1.
DURING HEAVY MAINTENANCE, TAIL CONE, FR 80-84 BOTH RT & LT SIDES, APU AIR INTAKE DUCT, THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /3/RDAF AND IS CLASSIFIED AS MAJOR.(E/C: A24-1107-01)
DURING HEAVY MAINTENANCE: DENT ON PASSENGER (R1) CREW DOOR 841 LOWER AFT CORNER AT FWD GALLEY AREA; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00055) 52PERFORMED REPAIR ON PASSENGER CREW DOOR 841 LOWER AFT CORNER AT FWD GALLERY AREA IAW A320 SRM 52-10-00-300-003 ITEM 2 A.1 STEP (K),(L) THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT 60000FC (FH NOT RELEVANT) INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT WITH SUBSEQUENT INSPECTION AT INTERVALS OF TBD AND METHOD TBD IAW A320 SRI 52-10-00-205-022 TABLE 1.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( AFT RH EEH DOOR 844 ) CRACK L=0.135 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404155 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460556 AND EC# A320-52-1144 FOR REPLACEMENT OF FRAME SEGMENTS AT OVERWING EMERGENCY EXIT DOOR 844. WORKE BY AEROAMN TECH # 8619911 & RII # AE 360 QC.
DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833 ) CRACK L=0.130 INCH APRPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460553 AND EC# A320-52-1144 FOR REPLACEMENT OF FRAME SEGMENTS AT OVERWING EMERGENCY EXIT DOOR 833. WORKED BY AEROMAN TECH # 8619911 & RII # AE 360 QC.
DURING HEAVY MAINTENANCE: CRACK INDICATION WAS FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( FWD RH EEH DOOR 843 ) CRACK L=0.200 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460554 AND EC# A320-52-1144 FOR REPLACEMENT OF FRAME SEGMENTS AT OVERWING EMERGENCY EXIT DOOR 843. WORKED BY AEROMAN TECH # 8619911 & RII # AE 360 QC.
DURING HEAVY MAINTENANCE: CRACK INDICATION WASA FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834 ) CRACK L=0.220 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460555 AND EC# A320-52-1144 FOR REPLACEMENT OF FRAME SEGMENTS AT OVERWING EMERGENCY EXIT DOOR 834. WORKED BY AEROMAN TECH # 8619911 & RII # AE 360 QC.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL FITTING I/B LOWER HOLE COMMON TO DOOR STOP FITTING Ã7 AT FR16 RH. CRACK DIRECTION AT 9 O CLOCK VIEW LO OKING FORWARD; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00050) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. DOOR STOP FITTING #7 AT FR16 RH IAW A 320 SRM 53-11-12-300-010. INSTALLED DOOR STOP FITTING #7 AT FR16 RH IAW A320 SRM 51-42-11.
FLT#1077, MCO-PUJ. DUE TO ODOR EVENT AND GROUND TIME ODOR IN ALL PHASE OF FLIGHT; INSPECTED A/C AND FOUND ODOR TO BE LEVEL B IAW AMM 49-00-00-200-811-A. PERFORMED ECS DECON WITH ENGINES IAW AMM 21-00-00-615-803-A. FOUND FUEL, HYDRAULIC LEAKS AND APU COOLING FANS AND TRANSFER TUBE LEAKING .INFO NOTICE 2017-T015K ACCOMPLISHED.
FLT#987, ORH-MCO. 'DIRTY SOCKS SMELLED BY ALL 4 FLIGHT ATTENDANTS AND FLIGHT DECK APU WAS ON, BLEEDS ON APU SMELL EQUAL THROUGHOUT THE CABIN; COMPLITED WITH INFORMATIONAL NOTICE 2017-T015, SECTION B1. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-710-080-A-2. A/C OK FOR SERVICE.'
FLT#1141, BDL-PBI. 'DIRTY SOCK/TAL SMELL DESCENDING THRU 9000' DISSIPATED SLIGHTLY WHEN PACK 1 SELECTED OFF.CABIN ODOR REPORTING FORM COMPLETE; ACCOMPLISHED TASKS IAW INFO NOTICE 2017-T015J,ACCOMPLISHED TSM 05-50-00-810-831-A. DETERMINED THAT ODOR EVENT IS A CATEGORY IS LEVEL 1. A/C IS OK FOR SERVICE. NO ODOR AFTER DECONTAMINATION NOTED.'
FLT#737, BDL-MCO. 'ON SHORT FINAL WE SMELLED THE "DIRTY SOCK SMELL" ON THE FLIGHT DECK. DURING DEPLANING THE FLIGHT ATTENDANTS COMPLAINED OF THE SAME SMELL OCCURRING RIGHT BEFORE LANDING; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00.-810-831. AIRCRAFT IS OK FOR SERVICE.'
FLT#626, FLL-RDU. 'ODOR/ FUME EVENT: LEVEL 2 AFT FLIGHT ATTENDANTS REPORTED SMELLING DIRTY SOCKS " SMELL SHORTLY AFTER THE 10000 CHIME ON DESCENT INTO RDU. CLEAR SKIES, NO CLOUDS, FIRST OFFICER REPORTED ODOR SMELL AROUND 3000FT ODOR DISSIPATED ON LANDING. ( PACKS ); REF LOG PAGE 3665682 ITEM 1 (REMOVED AND REPLACED L/H OZONE FILTER REF AMM 21-51-41) AND 2 (REMOVED AND REPLACED R/H OZONE FILTER REF AMM 21-51-41) LP 3665682 ITEM 1 FOR CORRECTIVE ACTION. COMPIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. DECONTAMINATION/ PACK BURN WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. ODOR REMOVED. MDDR 521887 CLEARED. MX-4 UPDATED. PLACARD REMOVED. MCC INFORMED. IDENTIFIED ODOR COMING FROM APU. NO ODOR WAS NOTICED DURING ENG 1&2 IDLE ODOR TEST.'
FLT#1433, MCO-SJU. 'DURING CRUISE AND DESCENT, THE INFLIGHT CREW DETECTED A CHEMICAL-TYPE ODOR IN THE FLIGHT ATTENDANT REPORTED A SCRATCHY SORE THROAT AND ONE FELT NAUSEATED. NO ODORS WERE DETECTED ON THE FLIGHT DECK; EXECUTED T/S AS PER INFO NOTICE 2017-7015J. NO 30-DAY HISTORY WAS FOUND. FOLLOWED TSM 05-50-00-810-831-A. PERFORMED PACK BURN PROCEDURES. OP'S CHECK WAS ACCOMPLISHED. NO FURTHER ODOR WAS NOTICED. A/C FOR CONTINUED SERVICE.'
FLT#113, MCO - CUN. '(AIRCRAFT PREFORMED AN AIR TURN BACK TO MCO).' "PREVIOUS WRITE-UP" ON CLIMB OUT, CRUISE, AND DESCENT CONSTANT VIBRATION IN COCKPIT / CABIN FILLED OUT ACFT VIB FORM MCC REQUESTED RTB ALL PARAMETER, ON VIB FORM; REF LP # 3482684, ITEM 2 (RIGGED BOTH RH ELEVATOR SERVOS TO .5NU POSITION REF AMM 27-34-00-820-003 SERVOS TORQUEDREF LP 3482685 FOR SAFETY AND CLOSE UP AND TOOL REMOVAL), 3482685, ITEM 2 (ADJUSTED LH ELEVATOR OUTBOARD 9BLUE) SERVO 1MM DOWN. INBD SERVO GOOD REF AMM 27-34-00-820-003B), AND 3482686, ITEM 1 (FOUND LAV A TOILET PLUMBING HAD 1 BROKEN CLAMP AND 2 LOOSE CLAMPS GIVING EXCESSIVE PLAY. REPLACED BROKEN CLAMP AND TIGHTENED 2 LOOSE CLAMPS REF AMM 38-31-01). RIGGED ELEVATOR AND SECURED FWD LAV PLUMBING.'
FLT#2457, LGA-DEN. (AIRCRAFT DIVERTED TO JFK) 'ENG 1 VIBRATION IN CLIMB ABOVE 10,000 THROUGH FL200 HIGH VIB NOTED 1.7 FLUCTUATE BETWEEN0.1-1.6 ON DECENT. VIBRATION FELT BY PAX AND FA DURING CLIMB; SYSTEM CHECKED AND PERFORMED FAN TRIM BALANCE WITH EVMU ONE-SHOT METHOD. REMOVED WEIGHT 5A0136 FROM BOLT 27 AND INSTALLED WEIGHT 5A0138 IN BOLTS 11 AND 34.PERFORMED TEST # 8 VIBRATION SURVEY IAW AMM 71-00-00-700-022-B AND TEST # 11 HIGH POWER ASSURANCE TEST IAE AMM 71-00-00-710-013-C. ALL PARAMETERS NORMAL.'
FLT#942, LAX-RNO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX) 'ENG 2 COMPRESSOR VANE ECAM; CLM REPORTS B25TK FOR ENGINE 2 REF TSM 75-30-00-810-850. BLEED 2.5ACT FAIL ON BOTH FADEC CHANNELS. REMOVED AND REPLACED 2.5 BLEED MASTER ACTUATOR PER AMM 75-31-42 PB 401.'
FLT#1475, BDL-SJU. 'SMOKE FWD AND AFT CARGO SMOKE ECAM MESSAGES; PERFORMED T/S PER TSM 26-16-00-810-805-A. FOUND NO EVIDENCE OF SMOKE OR FIRE ON FWD OR AFT CARGO. CLEANED AND INSPECTED FWD AND AFT CARGO SMOKE DETECTORS. NO DEFECTS WERE NOTED. ACCOMPLISHED CONDITIONING WITH APU. NO FUMES WERE NOTED. ACCOMPLISHED CIDS SDF BITE AND GROUND SCAN. NO FAULTS NOTED. ACCOMPLISHED CIDS INTERFACE AND POWER-UP TEST. NO FAULTS NOTED. COULD NOT DUPLICATE THE FAULT AT THIS TIME. A/C OK FOR SERVICE.'
DURING HEAVY MAINTENANCE, SAFETY PIN CANNOT BE INSERTED ON EMERGENCY EVACUATION SLIDE/RAFT VALVE REGULATOR DOOR 832 AT AFT GALLEY AREA. PERFORMED CONTROLLED DEPLOYMENT OF ESCAPE SLIDE DOOR 832 IAW AMM 25-62-00-710-001-A AND PERFORMED OPERATIONAL TEST IS OK.
ON BATTERY CAPACITY CHECK (12WL) THE BATTERY FAIL, REPLACED THE BATTERY (12WL) IAW AMM 33-51-00.
FLT 225, JFK-TPA. EPSU BATTERY 11WL FAILS EMERGENCY LIGHT SYSTEM TEST. R&R EPSU 11WL BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKS GOOD.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT FRAME FROM FR 69 TO 70 AND STR 23L AT AFT GALLEY AREA; REPLACED SUPPORT FRAME LOC FR 69 TO FR 70 AND STR AT AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11 AND DRAWING D53474180. ALL WORK ACCOMPLISHED ON NR 2018-261166.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK =Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA; REPLACED SEAT TRACK =Y1292 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261210.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 AT FRAME 16 AT FWD GALLEY AREA; REPLACED DUMMY RAIL IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261158.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261214.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-621214.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED OM NR 2018-261214.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM Y765 BETWEEN FR 67 TO FR 69 AT AFT GALLEY AREA; REPLACED FLOORBEAM Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261211.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM Y765 BETWEEN FR 67 TO FR 69 AT AFT GALLEY AREA; REPLACED FLOORBEAM Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261211.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FLOOR STRUCTURE LOCATED AT +Y1175 + AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM LOCATED AT +Y1175 IAW SRM 51-72-11. REF NR 2018-261213.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FLOOR STRUCTURE LOCATED AT +Y1175 AND FR68 AT AFT GALLEY AREA; REPLACED FLOORBEAM LOCATED +Y1175 AND BTW FR 67+18" TO FR 69 IN AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472780.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEATTRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA; REPLACED SEAT TRACK IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261210.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 53-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 53-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM +Y254 AT FRAME 18 +3 INCHES AT FWD GALLEY AREA; PERFORMED PERMANENT REPAIR LOCATED ON FLOORBEAM +254 AT FRAME 18 +3 IAW SRM 53-11-14-300-002. WORK ACCOMPLISHED ON NR 2018-261162.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y254 BTW FR 12 TO 18 AT FWD GALLEY AREA; REPLACED FLOORBEAM -Y254 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261159.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL AT LEVEL FR 66 AND S-23R AT AFT GALLEY AREA; REPLACED LOWER SILL AND FASTENERS LOC AT LEVEL STR 23R AND BTW FR 66 TO 68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DRAWING D53480505 SRM 51-72-11. ALL WORK ACCOMPLISHED ON NR 2018-261204.
SUPPLEMETAL INFORMATION (DIFFICULTY DATE CHANGE): DURING HEAVY MAINTENANCE, WAS FOUND WITH CORROSION TO THE UPPER AND LOWER SURFACES OF TOP SKIN PANEL 2 BETWEEN WX3622 â WX4490.52 AT THE TRAILING EDGE OVERHANG ON THE LEFT HAND WING. NDT INSPECTION REPORTS INDICATED CORROSION HAD EXTENDED BETWEEN THE TOP SKIN AND FALSE REAR SPAR FLANGE. THEREFORE WAS CONTACTED PROVIDED REPAIR INSTRUCTIONS AS PER REF /3/. THE REF /3/ REPAIR WAS PERFORMED PER REF /1/ EA. EC A18-704-01 INCORPORATES REF /1/ WITHOUT DEVIATION. EC A18-704-02 ACCOMPLISHES POST-REPAIR INSPECTIONS REQUIRED PER REF /2/ WHICH CONSIST OF EXTERNAL DET WITH A THRESHOLD OF 20000 FC/33000 FH AND INTERVAL 10000 FC/20000 FH; REF /2/ APPROVES THIS REPAIR AND REQUIRES POST-REPAIR INSPECTIONS. THIS IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REAR SPAR T/E LOWER SURFACE BTW RIB 7 TO RIB 8 ON LT WING 1EA; PERFORMED PERMANENT REPAIR ON REAR SPAR T/E UPPER AND LOWER SURFACE BTW RIB 7 TO RIB 9 ON LT WING IAW EA 57-0223 -18 REV 0 AND EC A18-704-01 THIS REPAIR IS CATEGORY B. ALL WORK ACCOMPLISHED ON NR 2018-261126.
DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REAR SPAR T/E LOWER SURFACE BTW RIB 7 TO RIB 8 ON LT WING; PERFORMED PERMANENT REPAIR ON REAR SPAR T/E UPPER AND LOWER SURFACE BTW RIB 7 TO RIB 9 ON LT WING IAW EA 57-0223 -18 REV 0 AND EC A18-704-01 THIS REPAIR IS CATEGORY B. ALL WORK ACCOMPLISHED ON NR 2018-261126.
FT # 41, FLL-MDE. RETURNED TO FIELD (FLL); ENG 2 BEARING 4 OIL SYS "HI-PRESS" MESSAGE ON ECAM/RETURN TO KFLL AS PER COMPANY MX/DISP. R & R ENG #2 XCDR NO4 BEARING PRESS IAW AMM 79-33-16. LEAK CK & OPS CK GOOD. NO FAULTS AT THIS TIME.
FLAP HANDLE STUCK AT 2. RETURNED TO FIELD. NO OVERWEIGHT LANDING. R & R FLAP HANDLE IAW AMM 27-51-43, ALL OPS CK OK.
RETURN TO DEPARTURE. NAV GPWS FAULT. R & R GPWC IAW AMM 34-48-34, PERFORMED UPLOAD OF ENHANCED GPWC DATABASE. BITE TEST ALL NORMAL.
DURING HEAVY MAINTENANCE L2 DOOR SILL WAS FOUND WITH CORROSION AT FRAME 66 FRAME 68 STR 23L, R & R L2 DOOR SILL FRAME 66, FRAME 68, STRINGER 23L. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
DURING FINAL APPROACH , FIX AND ACFT FULLY CONFIGURED AT APPROACH SPEED, ENG 2 COMPRESSOR VANE FAULT AT APPROXIMATELY 2000 FT MSL. ENG 2 STALL FAULT WITH AUDIBLE ENGINE STALLS IN COCKPIT FOLLOWED BY ENG 2 FAIL. SHUTDOWN ENGINE 2 IAW ECAM AND WITH ENGINE 2 SECURED, N1 AND N2 WERE BOTH WINDMILLING. ENG 2 EGT OVERLIMIT WITH ENGINE 2 SHUTDOWN, 700 DEGREES NOTED ON EGT GAUGE. ACCOMPLISHED T/S IAW TSM 71-00-00-810-809-A & TSM 75-30-00-810-846-A. R & R ENG NR 2 VSV ACTUATOR AMM 75-32-41. HIGH POWER ASSURANCE TEST C/W ALL PARAMETERS NORMAL. ENGINE WAS ALSO REPLACED ON 11/28/14.
FLT 191 JFK-LAS, ECAM A/I R WINDSHIELD WITH A SULPHUR SMELL AT THE SAME TIME (WINDSHIELD HEATING SYSTEMS). ACCOMPLISHED TSM 24-00-00-810-823 CONFIRMED SULPHUR SMELL ASSOCIATED TO WINDSHIELD HEAT SYS. REMOVED AND REPLACED WINDSHIELD AS PER AMM 56-11-11-04. OPS CHECK GOOD.