N819LF

ATA 5321

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 4,497 hrs · 10,475 cycles

DAMAGE WAS FOUND ON THE COCKPIT FLOOR PANEL IN THE FORM OF IMPACT DAMAGE AND CORROSION. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2026-24444A DATED 16 JUL 2026, AIR METHODS ENGINEERING AUTHORIZATION 23-5321-EA-5737 INITIAL REVISION DATED 22 JUL 2026, AND AIR METHODS ENGINEERING AUTHORIZATION 23-5321-EA-5741 REV. 1 DATED 27 JUL 2026. FOR ALL OTHER INFORMATION PLEASE REFER TO WORK ORDER MG #759 ON FILE AT CRS#2A6R933B.

ATA 6300

Part: WARNING MESSAGE — ILLUMINATED · airframe 4,405 hrs · 10,280 cycles

TRANSMISSION CHIP CAUTION ILLUMINATED MULTIPLE TIMES WHILE IN CRUISE FLIGHT. CAUTION REMAINED ON FOR LAST 3 MINUTES OF FLIGHT.

ATA 2120

Part: UNKNOWN — ODOR (ZONE 400) · airframe 4,337 hrs · 10,144 cycles

AFTER SHUTTING DOWN, CREW INDICATED A BURNING ODOR COMING FROM THE AFT NR 2 ENGINE AREA. CREW DESCRIBED THE ODOR AS ACRID AND ELECTRICAL IN NATURE. PILOT NOTED UNBURNT JET FUEL ODOR BUT COULD NOT IDENTIFY AN ELECTRICAL ODOR OR SEE ANY EVIDENCE OF FIRE OR BURNING.

ATA 2120

Part: UNKNOWN — ODOR (ECS) · airframe 3,679 hrs · 8,552 cycles

CREW REPORTED ABNORMAL SMELL IN THE REAR CABIN DURING OPERATING OF THE BLEED HEATING. TURNED THE HEATING OFF AND CONTINUED ON RTB LEG. LANDED WITHOUT INCIDENT, CALLED MAINTENANCE TO INVESTIGATE.

ATA 7200

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 2,815 hrs · 6,577 cycles

CORRECTION TO PREVIOUS SUBMISSION. THIS WAS INCORRECTLY SUBMITTED UNDER CONTROL NUMBER QMLA202305050031. (THIS CONTROL # WAS PREVIOUSLY USED) NEW SDR SUBMITTED AS QMLA2023050520036 N819LF 0781

ATA 7200

Part: WARNING UNIT — UNSERVICEABLE (INSTRUMENT PANEL) · airframe 2,815 hrs · 6,577 cycles

INFLIGHT ON AN AIR AMBULANCE FLIGHT. RECEIVED A #2 FUEL VALVE CL CAUTION FOLLOWED BY #2 FUEL PRESSURE AND THEN AND ENGINE FAIL LIGHT. I MADE AN EMERGENCY LANDING AT THE NEAREST AIRPORT. AFTER LANDING AND COMPLETE SHUTDOWN FOR TEN MINUTES. SDR SUBMITTED LATE FROM THE FIELD

ATA 7200

Part: WARNING UNIT — UNSERVICEABLE (INSTRUMENT PANEL) · airframe 2,815 hrs · 6,577 cycles

INFLIGHT ON AN AIR AMBULANCE FLIGHT. RECEIVED A #2 FUEL VALVE CL CAUTION FOLLOWED BY #2 FUEL PRESSURE AND THEN AND ENGINE FAIL LIGHT. I MADE AN EMERGENCY LANDING AT THE NEAREST AIRPORT. AFTER LANDING AND COMPLETE SHUTDOWN FOR TEN MINUTES. THIS WAS INCORRECTLY SUBMITTED UNDER SDR # QMLA2023050520031 THIS # WAS PREVIOUSLY USED.

ATA 5300

Part: NONE — DAMAGED · airframe 2,497 hrs · 5,805 cycles

COMPLETION OF 23-5300-EO-3820 PART 1. REPAIRED FRAME 5 IAW REFERENCED EA BY INSTALLING DOUBLERS AS DIRECTED. ISSUED 337 FOR REPAIR. EO CONTAINS FIGURES OF REPAIRS. MORE DETAILS FOUND ON UNIFLIGHT AVIATION WORK ORDER. AIRCRAFT OOS AT HEAVY MAINTENANCE EVENT STARTING 03/30/2022, EXPECTED RTS 08/31/2022

ATA 7110

Part: WIRE — UNSECURE (COWLING) · airframe 1,551 hrs · 3,495 cycles

AC EQUIPPED WITH AN FDC IBF SYSTEM, WHICH INVOLVES AN ADDITIONAL COWLING ACROSS THE FORWARD PART OF THE TRANSMISSION DECK. THIS COWLING INCLUDES, ON EACH SIDE, TWO PIECES OF HARD PLASTIC DUCTING CONNECTED BY A PIECE OF FLEXIBLE ORANGE DUCTING WITH A METAL WIRE WOUND THROUGH THE INTERIOR FOR STIFFENING (SCAT TUBING), WHICH COMPRISE THE INTAKE PATH FOR THE NR 1 AND NR 2 OIL COOLER IMPELLER FANS. THE AIRCRAFT WAS OUT OF SERVICE FOR AN UNRELATED ISSUE. ONE OF THE LOCAL MECHANICS WAS TURNING THE MR SYSTEM THROUGH AS PART OF AN INSPECTION, AND HEARD AN UNUSUAL NOISE. UPON INVESTIGATION, IT APPEARED THAT THE STIFFENING WIRE FROM THE INTERIOR OF THE FLEXIBLE DUCTING HAD COME LOOSE AND BEEN INGESTED INTO THE IMPELLER FAN. AIRCRAFT STILL REMAINS OUT OF SERVICE AT THIS TIME DUE TO OTHER MAINTENANCE.