N606JB
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 | 2009-07-10 – 2009-07-10 | Operator named in NTSB report |
| JETBLUE AIRWAYS CORP | Operator | 2009-07-10 – 2009-07-10 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FLT # 1245 ISP-PBI. " ODOR/SMELL DURING DESCENT THRU 9000' IDLE POWER.ONLY IN THE COCKPIT PREVIOSLY WRITTEN UP.DEFECT#4620792.; ACCOMPLISHED INFO NOTICE 2017-T015 M VERIFIED ODOR TO BE A MISCELLANIOUS TYPE 10 A LIGHT CHLORINE ODOR.AS PER TABLE 2.INSPECTED APU COMPT.FOUND NO LEAKS AND CLEAN.ACCOMPLISHED DECONTAMINATION OF BOTH PACKS,IAW TSM 05-50-00-810-085-D.A/C IS OK FOR SERVICE."
FLT #217 PHL-FLL." DIRTY SOCK/OILY SMELL DURING DESCENT @ 10,000' IDLE POWER, VMC,COCKPIT ONLY.; COMPLY INFO NOTICE 2017-T015M. ISOLATE FOR TYPE 1 APU OIL OVERSERVICED. REMOVED EXTR APU OIL IAW AMM 12-13-49. PER TSM 05-50-00-810-085 A/C IS OK FOR SVC "
FLT 995, MCO- SJO. AIRCRAFT DIVERTED TO FLL. PASSENGER RECORDED A VIDEO OF OPEN LOWER PANEL ON IMBOARD SIDE OF #1 ENGINE DURING FLIGHT. N606-FLT-MCO-SJO-DIVERSION THE A/C DIVERTED TO FLL, THE CREW REPORTED A PANEL WAS OPEN ON THE NBR 1 ENG AND SEEMED TO BE FLAPPING IN THE AIR. CREW DIVERTED INTO FLL TO HAVE THE PANEL ADDRESSED BY MAINTENANCE. FLL MX WAS ADVISED.; RESOLUTION: MX FOUND ENG #1 STARTER ACCESS DOOR OPENED. NO DAMAGE FOUND. CLOSED ACCESS DOOR IAW AMM 52-40-00. AC OK FOR SERVICE.
FLT 503, JFK-SJU. ODOR DETECTED DURING DESCENT BELOW 10,000. CONFIRMED WITH CABIN CREW. LOCATION OVERWING EXITS STRONGEST, AND FWD. LASTED A MINUTE THEN DISSAPATED. FOUL HEATED PLASTIC TYPE ODOR, FOLLOWED INFO NOTICE 2017-T015L WITH MX-270 PROVIDED. TSM 05-50-00-810-085-B FAULT ISOLATION FOR TYPE 1 LEVEL A. NO LEAKS FOUND DURING ULTRA VIOLET LIGHT INSP. APU WORKING PROPERLY. IAW AMM 49-00-00-200-812-A ACFT OK TO CONT SVC. NO ODOR PRESENT AT THIS TIME.
DURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325667. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 4 ); (RESOLVED ON W/O: 1388014 TASKCARD: NR-00016) FUR-A320-53-02297. REF AEROMAN WO# 2025 181/1 NR# 2025-325667. PERFORMED PERMANENT REPAIR LOCATED ON FRAME 68, R/H SIDE AT LEVEL OF DOOR STOP #1 I.A.W. A320 SRM 53-41-12-300-011 AND DWG D53480505. THIS REPAIR IS CATEGORY B, FOR AREA 4 INSPECTION THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT 19700FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS OF 19700 FC (FH NOT RELEVANT), INSPECTION METHOD HFEC I.A.W. A320 SRI 53-41-12-205-010, TABLE 6.
DURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325635. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 1 & 3 ); (RESOLVED ON W/O: 1388014 TASKCARD: NR-00014) FUR-A320-53-02292. REF AEROMAN WO# 2025 181/1 NR# 2025-325635. PERFORMED PERMANENT REPAIR LOCATED ON FRAME 68, R/H SIDE AT LEVEL OF DOOR STOP #1 I.A.W. A320 SRM 53-41-12-300-011 AND DWG D53480505. THIS REPAIR IS CATEGORY B, FOR AREA 1 AND 3 INSPECTION THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT 60000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION INTERVALS TBD, INSPECTION METHOD TBD, IAW A320 SRM 53-41-12-205-010, TABLE 6.
DURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325666. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 2 ); (RESOLVED ON W/O: 1388014 TASKCARD: NR-00015) FUR-A320-53-02295. REF AEROMAN WO# 2025 181/1 NR# 2025-325666. PERFORMED PERMANENT REPAIR LOCATED ON FRAME 68, R/H SIDE AT LEVEL OF DOOR STOP #1 I.A.W. A320 SRM 53-41-12-300-011 AND DWG D53480505. THIS REPAIR IS CATEGORY B, FOR AREA 2 INSPECTION THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT 37900 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS OF 5300 FC (FH NOT RELEVANT), INSPECTION METHOD HFEC I.A.W. A320 SRI 53-41-12-205-010, TABLE 6.
DURING HEAVY MAINTENANCE: BROKEN HINGE FITTING HINGE 3 ELEVATOR LH; REF: ARM W/O 2025-181/1 N/R # 2025-325674. PERFORMED PERMANENT REPAIR ON HINGE FITTING HINGE 3 ELEVATOR LH IAW A320 SRM 55-26-41-300-001, REPAIR IS CATEGORY A.
FLT#1603, JFK-SJU. 'DURING FINAL DESCENT, SLIGHT ODOR OF OIL IN VENTS IN CLEAR AIR. PACK 1 SET TO OFF, XBLEED SHUT AND ODOR CEASED; C/W INFO NOTICE 2017-T015K SECTION A.ISOLATED FAULT TO TYPE 10 AMBIENT AIR. PERFORMED DECONTAMINATION OF THE ECS LEVEL A PER AMM 21-00-00-615-802. ACFT OK FOR SVC.
FLT#266, RSW-BOS. 'RED ECAM L/G GEAR NOT DOWNLOCKED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#5, AIRCRAFT PERFORMED AN AIR TURN BACK. O2 MASKS OVER FLIGHT ATTENDANT JUMPSEAT 1 AND 2 DEPLOYED UNCOMMANDED; REMOVED AND REPLACED O2 MASK CONTAINER (28WR) IAW AMM 35-21-41 ALL OPS OK AT THIS TIME.'
FLT#1584, MCO-JFK. 'UNCOMMANDED REDUCTION IN THURST AT 9500 IN CLIMB FROM 1.3 TO 1.2 EPR IN ENGINE #1 FOR APPROX 25SEC CAUSING SIGNIFICANT YAWING MOTION AT THE SAME TIME FUEL IN THE CENTER WENT TO 0 AND GOT A CTR TANK 1 PUMP 1 FAULT; #1 ENG REMOVED AND REPLACED REF LP 3494378, ITEM #1 (A FTTO WAS ACCOMPLISHED ON 10/5/22 & FLT. #1464.) FOR COMPLIANCE ALL CHECKS ARE OK. ' (SUPPLEMENTAL INFORMATION TO FOLLOW)
FLT#1636, LAX- SFO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX). ' ENGINE ONE STALL CLIMBING OUT OF LAX 10,500 FT #1 ENG WENT TO IDLE AND RELIT. NO ECAM. APPLIED QRH ENG 1 STALL PG 6-31. ENG 1 PARAMETERS ARE NORMAL. RETURNED TO LAX; ACCOMPLISHED TSM 77-00-00-810-801-A. REMOVED AND REPLACED #1 ENG EEC IAW AMM 73-22-34. OPS CHECK NORMAL. ACCOMPLISHED ENG 1 HIGH PWR ASSURANCE TEST IAW AMM 71-00-00 TEST 11. OPS CHECK NORMAL. A/C OK FOR SERVICE.'
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH LOWER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ã7; REF AEROMAN N/R 2022-355591, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #7 AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, R53113118 AND DWG D53114223.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH UPPER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ã7; REF AEROMAN N/R 2022-355593, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP 7 AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, R53113118 AND DWG D53114223.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 L/H UPPER I/B SIDE POSITION OPEN FASTENER HOLE DOOR STOP FITTING Ã7; REF AEROMAN N/R 2022-355592, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #7 AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, R53113118 AND DWG D53114223.
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH UPPER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ã7; REF AEROMAN N/R 2022-355590, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP 7 AS PER A320 SRM 51-42-11,A320 SRM 51-72-11, R53113118 AND DWG D53114223.
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR41R TO STR42R AT FR32 IN FWD CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355543. REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR41R AND STR42R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. COMPLETED BY M. CARRILLO EMP # 8673420. AND RII BYQC R. MURILLO EMP # 222. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR40R AND STR41R AT FR33 IN FWD CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355551. REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR40R AND STR41R AT FR33 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. COMPLETED BY M. CARRILLO EMP # 8673420. AND RII BYQC L. MARTINEZ EMP # 285. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR42R AND STR43R AT FR32 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR43R AND STR43R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355544. COMPLETED BY O. GARCIA EMP # 8672920. AND RII BY QC E. LOPEZ EMP # 244. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR41R TO SRT42R AT FR33 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR41R AND STR42R AT FR33 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355552. COMPLETED BY M. CARRILLO EMP # 8673420. AND RII BY QC R. MURILLO EMP # 222. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION ON SHEAR TIE LOC. BTW STR40R TO STR41R AT FR32 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR40R AND STR41R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355541. COMPLETED BY O. GARCIA EMP # 8672920. AND RII BY QC Y. CALDERON EMP # 238. (CONSIDERED AS A MAJOR REPAIR)
DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FR 60 AND 62 AT LEVEL STR 38R IN AFT CARGO; REF AEROMAN N/R 2022-355522, REMOVED AND REPLACED LOWER SILL, FASTENERS. LOC BTW FR 60 AND FR62 AT LEVEL STR 38R I.A.W. A320 SRM 53-41-49-300-002, A320 SRM 51-72-11, A320 SRM 51-42-11.'
DURING HEAVY MAINTENANCE: CORROSION STRINGER 32L LOCATED BTW FR 53 AND FR 64 IN AFT CARGO COMPA RTMENT; (RESOLVED ON W/O: 1159479 TASKCARD: NR-00010 ) FUR-A320-53-00421, REF AEROMAN N/R 2022-355537, REMOVED CORROSION LOCATED P1. STR32L FR56 PLUS 6.521IN, P2. STR32L FR57 PLUS 8.387IN. P3 STR32L FR59 PLUS 6.434IN. P4 STR32L FR61 PLUS 5.998IN. ON AFT CARGO COMPARTMENT IAW A320 SRM 51-74-00 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS P1: STR 32L AT FR 56 PLUS 6.521IN, P2: STR 32L AT FR57 PLUS 8.387IN, P3: STR 32L AT FR59 PLUS 6.434IN AND P4: STR 32L AT FR 61 PLUS 5.998IN IAW A320 SRM 53-44-13-283-002 STEP 2.A. FIGURE 001. THIS REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT 60000 FC/120000 FH WHICHEVER VALUE FC/FH OCCURS FIRST, SUBSEQUENT INSPECTION AT INTERVALS OF TBD. I.A.W. A320 SRI 53-41-13-205-002 TABLE 001. TOOL USED DIGITAL CALIPER PN: 500-197-30, SN: A21303945, DUE DATE: MAY-06-2023, P/N: 45MG S/N: 130061901 DUE DATE: APR-08-2023. ACCOMPLISHED BY #8617115, CHECKED BY # 8619800.
DURING HMV, LANDING GEAR -MAIN GEAR - INSPECTION SLIDING TUBE / SLAVE LINK LUG CRACK (CLASSIFIED MAJOR)
FLT 563, ORD-FLL. INFLT REPORTED BURING SMELL IN BACK OF A/C AND LIVE TV IN ACFT CABIN INOPERABLE. PERFORMED CABIN ORDER INSPECTION, PER TSM 05-50-00-810-831-A. NO 'BURNING SMELL' COULD BE DUPLICATED. TSM 05-50-00-810-831-A WAS FOLLOWED BY CAPTAINS CABIN ODOR REPORT SHEET. AC OK TO CONTINUE SERVICE, IAW CAPTAINS ODOR REPORT SHEET, TYPE 9 OF TSM 05-50-00-810-831-A WAS PERFORMED, AFTER CONCLUSION OF TYPE 9 INSPECTION, TYPE 10 INSPECTION WAS PERORMED DUE TO NO "BURNING" SMELL FINDINGS ON TYPE 9 INSPECTION OF THE ABOVE MENTIONED TSM. COFFEE MAKERS WERE OPERATED AND PULLED TO CHECK FOR ANY LOSE WIRING, NO COFFEE MAKER WAS FOUND DEFECTIVE. ALL TOILETS WERE OPERATED SEVERAL TIMES. NO "BURNING" SMELL OCCURANCE. ALL CEILING & SIDE WALL LIGHTS ARE OPERATING, NO FLICKERING OF ANY SORT IS PRESENT OR CREATING A "BURNING" SMELL. OPERATED ALL READING LIGHTS FROM ROWS 16ABC, DEF AFT. NO "BURNING" SMELL WAS PRESENT, AFT GALLEY WAS CHECKED FOR TRASH COMPACTOR & LAV WASTE BOX WERE INSPECTED WITH NO "BURNING" SMELL. NO "BURNING" SMELL WAS NOTED ON AFT CARPETING OR SEATS COVERS. AFT CABIN CEILING PANELS. AFT CEILING PANELS WERE REMOVED TO CHECK FOR ANY LOSE WIRINGS OR ANY "BURNING" SMELL PRESENCE, NO "BURNING" SMELL WAS FOUND PRESENT. GALLEY CEILING PANELS WERE REMOVED IN AFT CABIN FOR PRESENCE OF "BURNING" SMELL, NO "BURNING" SMELL WAS FOUND PRESENT. A/C IS OK TO RETURN TO SERVICE AFTER THOROUGH INSPECTION, PER TSM 05-50-00-810-831-A TYPE 9 & TYPE 10 INSPECTIONS.
FLT 2633, BDL-TPA. AFT EMERGENCY LIGHT TEST FAILED FIN 13WL BATTERY. REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT FIN 13WL PER AMM 33-51-38.
FLT 88, FLL-ALB. COMM 1 & 2 ONLY TRANSMIT ON 119.3 RECEIVE ON ALL FREQ. T/S AND FOUND F/O'S BOOMSET DEFECTIVE, REPLACED F/O'S BOOMSET AS REQUIRED. ALSO REMOVED & REPLACED AUDIO MANAGEMENT UNIT (1RN) PER AMM 23-51-34, ALL BITE TEST AND OPS TEST OK. A/C NOW OK FOR SERVICE.
DURING DESCENT THROUGH 8000 FEET, SMELLED A STRONG ODOR OF DIRTY SOCKS THROUGH THE PACKS FOR ABOUT 12 MINUTES. DONNED OXYGEN MASKS ALL THE WAY TO LANDING. FLIGHT ATTENDANT ALSO COMPLAINED ABOUT THE ODOR. PERFORMED INFO NOTICE 2017-T015, FOLLOWED PERFORMANCE OF THE NR 1 & 2 PACK DECONTAMINATION IAW AMM 21-00-00-615-001. R & R THE NR 1 & 2 OZONE FILTERS IAW AMM 21-51-41. PERFORMED HIGH POWER ENGINE RUNS IAW 71-00-00. NO ODOR PRESENT. ACFT OK FOR SERVICE.
DURING DESCENT THROUGH 8000 FEET, SMELLED A STRONG ODOR OF DIRTY SOCKS THROUGH THE PACKS FOR ABOUT 12 MINUTES. DONNED OXYGEN MASKS ALL THE WAY TO LANDING. FLIGHT ATTENDANT ALSO COMPLAINED ABOUT THE ODOR. PERFORMED INFO NOTICE 2017-T015, FOLLOWED PERFORMANCE OF NR 1 & 2 PACK DECONTAMINATION IAW AMM 21-00-00-615-001. R & R THE NR 1 & 2 OZONE FILTERS IAW AMM 21-51-41. PERFORMED HIGH POWER ENGINE RUN IAW 71-00-00. NO ODOR PRESENT. ACFT OK FOR SERVICE.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 68, STR 23R AT AFT GALLEY AREA. R & R LOWER SILL.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, +Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA. REPLACED FLOORBEAM +Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATION AT RIB 15, TOP SKIN PANEL 2 LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 15, TOP SKIN PANEL 2 ON LT WING.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATION AT RIB 16 TOP SKIN PANEL 2, LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, ON LT WING.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E AT RIB 15 + 8", TOP SKIN PANEL 2, LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E AT RIB 15 + 8", TOP SKIN PANEL 2 ON LT WING.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATED AT RIB 17 TOP SKIN PANEL 2 LOWER SURFACE ON RT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, LOWER SURFACE ON RT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, LOWER SURFACE ON RT WING.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA. R & R FLOORBEAM AT FWD GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, -Y765 BETWEEN FRAME 20 TO FRAME 24 AT FWD GALLEY AREA. R & R FLOORBEAM -Y765 BETWEEN FRAME 20 TO FRAME 24 AT FWD GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, LOCATION: -Y254, FRAME 20 AT FWD GALLEY AREA; R & R FLOORBEAM -Y254, FRAME 20 AT FWD GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM, LOCATION: +Y1162, FRAME 67+18" AT AFT GALLEY AREA. R & R FLOORBEAM Y1162 FRAME 67 + 18" AT AFT GALLEY AREA IAW SRM 51-72-11.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1162, LOCATION FRAME 67 + 18" AT AFT GALLEY AREA; R & R FLOORBEAM -Y1162, FR 67 +18" AT AFT GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1162, FR 67 +15" AT AFT GALLEY AREA. R & R FLOORBEAM -Y1162, FRAME 67 + 15" AT AFT GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 66, STR 23R AT AFT GALLEY AREA. R & R NEW LOWER SILL.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL, LOCATION: FRAME 66, STR 23L AT AFT GALLEY AREA; INSTALLED NEW LOWER SILL LOCATION, FRAME 66 AT LEVEL STR 23L AT AFT GALLEY AREA.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON TOP SKIN ON UPPER SURFACE LEVEL STR 11, BETWEEN RIB 11 AND RIB 12, LEFT WING. REPAIRED AREA ON TOP SKIN UPPER SURFACE LEVEL STR 11, BETWEEN RIB 11 AND RIB 12 LT WING.
DURING MAINTENANCE, CORROSION WAS DISCOVERED ON TOP SKIN ON UPPER SURFACE ON LT WING ON RIB 1 AND STR 11. REPAIRED AREA ON TOP SKIN UPPER SURFACE ON LT WING ON RIB 1 AND STR 11.
IN-FLIGHT CREW SMELLED ELECTRICAL ODOR IN-FLIGHT ON DESCENT, NO VISIBLE SMOKE OR MALFUNCTIONING EQUIPMENT. NO COCKPIT INDICATIONS; PERFORMED INSPECTION IAW 05-50-00-810-831-A & TSM 24-00-00-810-823-A. NO FINDINGS BOTH APU ENG BLEED INCLUDED. AS A PRECAUTION PLACED LTV, CSS, & WADL ON MEL. NO C/B'S COCKPIT OR CABIN TRIPPED. INSPECTED ALL CABIN SYS. LAVS, EMERGENCY LIGHTS, READING LIGHTS AND GALLEY EQUIPMENT WITH NO FINDINGS. INSPECTED EMERGENCY EQUIPMENT NO FINDINGS.
ACFT DIVERTED. CREW REPORTED ON INITIAL CLIMB WITH POWER REDUCTION, ACFT RECEIVED AIR ENG 2 BLEED ABNORMAL PRESSURE ECAM. COMPLIED WITH QRH. PERFORMED TSM TASK 36-11-00-810-810A. FOUND BLEED PRESSURE REGULATOR VALVE 4001HA2 INTERMITTENTLY OPENING WITH 20 PSI. ALSO FOUND SENSE LINE LEAKING REPLACED VALVE AND LINE. OPS CHECK IAW 36-11-52, ALL CHECKS GOOD.
FLT 844 SJU-BOS FWD OVERHEAD DOOR EXIT SIGNS NOT ILLUMINATED. REMOVED AND REPLACED EPSU PER AMM 33-51-38. OPS CHECKED OK.
FLT 505 EWR-FLL, FWD GALLEY OVERHEAD EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EPSU (10WL) PER AMM 33-51-38, OPS CHECK GOOD.
FLT 705, JFK-LGB, ON CLIMB, LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER PER AMM 32-31-11-04. OPS CHECK OK. PERFORMED GEAR SWING PER AMM 32-30-00-02. NO DEFECTS NOTED. A/C OK FOR SERVICE.
10 MIN INTO FLT, AFT AVIONICS COMPARTMENT, RACK POWER WARNING , LIGHT IN BUTTON AND HORN . TURNED POWER OFF, NO FURTHER WARNING. LEFT IN OFF POSITION FOR REST OF FLT. REMOVED AND REPLACED COOLING FAN ASSY IAW MM 23-39-00. LTV OPS CK GOOD IAW LTV MM 23-39-00.