N726AE
Registered owner: AIR EVAC EMS INC, MO (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AIR EVAC EMS, INC. (EVCA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
CORROSION FOUND INSIDE MAST DURING 12 MONTH INSPECTION
DURING ROUTINE INSPECTION, MAIN ROTOR BLADE SN:A-4318 EROSION STRIP HAS DELAMINATION EXTENDING 1.75 INCHES BY 1.3 INCHES FROM OUTBOARD TIP OF BLADE.
FIRST OFFICER WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD IAW EMB AMM. PRESSURIZATION AND LEAKED CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
FOUND LEFT OUTBOARD SEAT TRACK CORRODED. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
FOUND LEFT OUTBOARD SEAT TRACK CORRODED. RAI SEAT TRACK, AIW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
SAW - FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 17-23. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 17-23. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
SAW - FOUND RIGHT INBOARD SEAT TRACK CORRODED FROM FRAME 36-47. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
SAW - FOUND RIGHT INBOARD SEAT TRACK CORRODED FROM FRAME 36-47. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 36-47. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 36-47. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)
SAW - FOUND FORWARD CABIN FLOOR U-SHAPE NEAR MAIN DOOR HAS CORROSION. REPLACED U-SHAPE IAW SRM 51-20-03 AND I/C 2006-145/6840. AIRCRAFT RETURNED TO SERVICE. (M)
FOUND FORWARD CABIN FLOOR U SHAPE NEAR MAIN DOOR HAS CORROSION. REPLACED U SHAPE IAW SRM 51-20-03 AND I/C 2006-145/6840. AIRCRAFT RETURNED TO SERVICE. (M)
ON APPROACH, RECEIVED (FLAP FAIL) ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBRICATED THE LT AND RT FLAP FLEX SHAFTS AND REPLACED NR 2 AND NR 3 FLAP ACTUATORS AND THE FLAP ELECTRONIC CONTROL UNIT IAW MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE.(K)
DURING APPROACH TO LGA WHEN CREW SELECTED FLAPS THE FLAPS FROZE WOULD NOT MOVE FROM 0 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FLAP TRANSMISSION BRAKES IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE.
FORWARD FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED FORWARD PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE.
DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUTOUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND BOTTOM PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 51-40-02. (M)
DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 53-22-10 FIGURE 203 AND EMB REPAIR STATEMENT IC2003-145/3835 DATED AUGUST 18, 2004. (M)
DURING AN IMBV INSPECTION, THE AFT DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT SECTION OF EXISTING DIGITAL STARTING 5.1 IN INBOARD OF THE LEFT SEAT TRACK AT FRAME 18 AND TREATED EDGES. AN ADDITIONAL AREA OF THE DIGITAL AT FRAME 18 OUTBOARD LEFT SEAT TRACK WAS CORRODED BEYOND SRM LIMITS. INSTALLED NEW DIGITAL IAW EMB REPAIR STATEMENT IC2003-145/3806 PARA 3 DATED AUGUST 16, 2004. (M) SIMA
DURING IMBV INSPECTOIN, THE FORWARD DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE EXISTING FORWARD DIGITAL AND INSTALLED A NEW DIGITAL. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTERS 51-40-02 AND 51-20-01. (M)
ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/3835 DATED AUGUST 18, 2004. (M)
DURNG AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CARGO DOOR CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-023 DATED APRIL 4, 2002. (M)
ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVICE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM 145/1142 REV 26, 51-40-02 EMB REPAIR STATEMENT IC2003-145/0818 DATED MAR 6, 2003 AND ETN EB 53-009 DATED 8/28/2001. (M) SIMA
DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMGAED AREA. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. RPAIR DONE IAW EMB 145 SRM, SRM 145/1142, REV 26, CHAPTER 53-21-10. (M)
ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24-25. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 26, 53-22-10. (M)
ABI - DURING AN IMBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-022R1. (M)
ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS, AT AFT BELLY FAIRING. BLENDED THE CHAFE ON STRINGER 19R AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIF DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-24-02 AND EMB REPAIR STATEMENT IC 2003-145/3093A. (M)
CLT - FLT 4430 - DURNG TAKEOFF ROLL AT ABOUT 60 KNTS CREW NOTED YOKES BEING SLAMMED TOWARDS THEM. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. DURING POST FLIGHT NOTED LEFT ELEVATOR TRIM STUCK DOWN IN THE 90 DEGREE POSITION. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR ASSEMBLY IAW EMB MM. GORUND FUNCTINAL CHECK WAS GOOD AND A FUNCTIONAL CHECK FLIGHT WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE.(M)
DURING AN MBV INSPECTION, FOUND DAMAGE TO STRINGER 16L FORWARD OF FRAME 20, AT JOINT DRILL MARKS AND OVERSIZE HOLE. REMOVED DRILL MARKS BY BLENDING. REAMED HOLES, INSTALLED NEW FASTENERS IAW STANDARD SRM PRACTICES.
DURING AN MBV INSPECTION, FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGER 15 AND 17L, RIVETS IMPROPERLY INSTALLED. REMOVED PREVIOUS REPAIR DOUBLER, INSTALLED IAW STANDARD SRM PRACTICES.
DURING AN MBV INSPECTION FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGERS 15 AND 17L, RIVETS IMPROPERLY INSTALLED. REMOVED C PREV. REPAIR FAB A REPAIR DOUBLER, REPAIR DONE IAW STANDARD SRM PRACTICES.
ORD - FLT 9754 - AFTER TAKEOFF, WITH PITCH TRIM SET AT +8, THE PILOT ATTEMPTED TO RETRIM. PITCH TRIM MOVED FROM +8 TO +6 AND THEN FAILED. BACKUP TRIM WORKED NORMAL. MAINTENANCE REMOVED AND REPLACED THE HSCU. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS SATISFACTORY AND WAS RETURNED TO SERVICE. (M)
ABORTED TAKEOFF FOR CARGO DOOR WARNING HOWEVER CARGO DOOR WAS ALREADY ON MEL AND DOOR WAS CLOSED. THIS WAS SUBMITTED FOR THE ABORTED TAKEOFF ONLY. (M)
CLE - FLT 4465 - DURING LANDING NR 2 PITOT HEAT OVERTEMP FOLLOWED BY SMOKE IN COCKPIT. REPLACED NR 2 PITOT CURRENT SENSOR IAW AMM. OPS CHECK GOOD. (M)