FAA SDR: IXXA fumes or odor report on 2025-01-18

CREW REPORTED AT TOP OF CLIMB, AUDIBLE METALLIC SCRAPING SOUND FOLLOWED BY LEFT FMC CDU BLANK AND STRONG ODOR OF ELECTRICAL SMOKE. CREW ELECTED AIR TURN BACK TO DEPARTURE STATION KAWF WITH AN EMERGENCY DECLARATION. VISABILITY WAS NOT IMPARIED. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. LINE MAINTENANCE REPORTED, SUBSEQUENT TO CIRCUIT BREAKER RESET METALLIC SCRAPING NOISE WITH CIRCUIT BREAKER TRI

FAA SDR: AALA fumes or odor report on 2025-01-17

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A DIRTY MUSTY ODOR DURING DESCENT THRU ENGINE SHUTDOWN WITH THE PACKS AND BLEEDS ON. MAINTENANCE FOUND THE APU GEARBOX VENT LINE TO HAVE SIGNIFICANT COKING AND REPLACED IT PER TASK CARD 26L00021002. MAINTENANCE ACCOMPLISHED THE DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM PER TASK CARD 26L00021014 WITH NO LEAKS OR ODORS NOTED.

FAA SDR: AALA fumes or odor report on 2025-01-17

AIRCRAFT WAS GROUNDED: AFTER FIRST ENGINE START EXCESSIVE FUME SMELL IN CABIN, LINGEREDAND GOT PROGRESSIVELY WORSE AS TAXI PROCEEDED. ACCOMPLISHED J/C 08L0021001. FOUND WHEEL WELL AND BELLY EXTREMELY DIRTY. FOUND EVIDENCE OF DEICING FLUID IN TAIL AREA. WASHED AND CLEANED WHEEL WELL, BELLY, APU INTAKE AND TAIL AREA, PER AMM 12-40-00. RAN PACKS APU, NO FUMES. RAN PACKS WITH ENGINES, NO FUMES.

FAA SDR: N753JS fumes or odor report on 2025-01-17

WILLIAMS INTERNATIONAL ENGINE MODEL FJ44-3A, SERIAL NUMBER 141208, FROM AIRCRAFT 525B-0100 (N753JS), WAS RETURNED TO THE REPAIR STATION FOR UNSCHEDULED REPAIR. AIRCRAFT OPERATOR SQUAWKED AN OIL CONSUMPTION ISSUE AND BLEED ODOR ISSUE ISOLATED TO THIS ENGINE. ENGINE OEM PRODUCT SUPPORT TROUBLESHOT THE ISSUE WITH AN AIRCRAFT OEM MOBILE SERVICE TECHNICIAN, WHICH DETERMINED AN OIL CONSUMPTION RATE ABOVE LIMITS ALLOWED BY THE ENGINE MANUAL. ENGINE OEM DIRECTED THE TECHNICIAN TO REM

FAA SDR: DALA fumes or odor report on 2025-01-16

SHIP 6812 AFTER ENGINE START DIRTY SOCK VINEGAR SMELL THAT DISSIPATED DURING FIRST 30 MIN OF FLIGHT, INTERMITTENT SMELL AT CRUISE SEEMED TO CLEAR UPNO SMOKE VISIBLE AT ANY TIME. CORRECTIVE ACTION: #2 ENGINE WAS REPLACED SEE LOGS 0761629 AND 0762022. (6924590)

FAA SDR: CALA fumes or odor report on 2025-01-16

AFTER PUSH HAD A SMOKY ODOR IN CABIN MAKERS IN USE AND OVENS OFF. NO VISABLE SMOKE REPORTED, ODOR OF SMELL DISSAPATED WHEN CABIN DOOR OPENED. DEBRIEFING FROM FLIGHT CREW. ODOR OF ELECTRICAL BURNING OCCURED IN ALL AREAS OF PASSENGER CABIN DURING PUSH BACK OFF GATE. BOTH ENGINES OFF, APU ON, BLEED ON, PACKS ON. COULD NOT SMELL ODOR IN COCKPIT UNTIL DOOR OPENED. FLIGHT ATTENDANTS REPORT COFFEE COMPLIED WITH AMM 05-51-58-910-801-C1 SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDI

FAA SDR: DXTA smoke report on 2025-01-15

LEFT ENGINE ENGINE OVERTEMP: FOLLOWING LEFT ENGINE START ITT ROSE RAPIDLY ACCOMPANIED BY A RED HOT MESSAGE ON THE ITT GAUGE. TEMP CONTINUED TO RISE AND CREW TERMINATED THE START AT 804°. CREW FOLLOWED THE HOT START QRH PROVEDURE. ALSO, THE MARSHALER HAD A CONCERNED LOOK AT THE SAME TIME THE HOT MESSAGE WAS DISPLAYED. FOLLOWIMG SHUTDOWN, THE MARHALLER INFORMED ME THAT HE SAW A LARGE PUFF OF WHITE SMOKE. CORRECTIVE ACTION: PERFORMED GVI OF ENGINE INLET AND EXHAUST. OPS CHECK GO

FAA SDR: GTIA fumes or odor report on 2025-01-15

FUME WET SOCK ODOR ON PACK 1 DURING CLIMB ODOR DISSIPATES WITH PACK 1 OFF. REFER TO LOG PAGES 3384151 3384152 3610150 3610149 3610147 3610146 PACK 2 ON DESCENT-COMPLIED WITH TI 2100-2002-NEO AND AMM 21-00-00-615-804-A LEVEL C DECONTAMINATION OF ECS WITH BOTH PACKS. ALL OPS TESTS/LEAK CHECKS GOOD. NO FUMES OR ODOR. A/C OK FOR CONT. SVC. DESCRIPTION OF FUMES/ODOR: OIL/OIL BURNING, MUSTY DRY. SOURCE: CABIN AIR SUPPLY VENTS. AFFECTED AREA: FLIGHT DECK, FWD CABIN, MID CABIN, AFT C

FAA SDR: DXTA fumes or odor report on 2025-01-14

ON CLOMB OUT AT 7-8K FT, A BURNING SMELL STARTED . THE ENTIRE FLIGHT THE BURNING SMELL CAME IN STRONG WAVES. THE STRONGEST WAS DURING THE DECENT OUT OF 18K FT AND BELOW . REPLACED ENGINE HP VALVE SEALS. OPS CHECK GOOD. IAW CE-680A AMM 36-10-05