N906ER
Registered owner: HEAVY METAL AIR LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Academy of Aviation | Operator | on 2021-08-09 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
4 reports on file, 2010-07-15 – 2011-01-20.
Part: RETAINING RING — MISSING (NLG ACTUATOR) · airframe 1,598 hrs
DURING A ROUTINE ANNUAL INSPECTION, THE TECHNICIAN NOTICED THAT THE AFT NLG ACTUATOR ATTACH PIN(IPC P/N: D60-3223-00-33) HAD MIGRATED TO THE RIGHT, APPROXIMATELY 1/2 INCH THE RETAINING RING (IPC P/N: DIN471-10-ZP) HAD COME LOOSE AND FALLEN FROM THE ASSEMBLY, LEAVING THE PIN UNSECURED. THIS CLIP IS ITEM NR 030 FIGURE 32-30 HYDRAULIC ACTUATOR.
Part: FUEL CELL — CRACKED (RT AUX) · airframe 1,504 hrs
DURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE RT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.
Part: CABLE — FAILED (ZONE 100) · airframe 1,329 hrs
(N3XR) ON OR ABOUT 15 JULY 2010, THIS REPAIR STATION RECEIVED INFORMATION FROM ANOTHER ACFT OPERATOR THAT SIGNIFICANT RUDDER CABLE WEAR THAT WAS FOUND WHERE THE RUDDER CABLE EXITS THE PROTECTIVE NYLON TUBING JUST BELOW THE RUDDER HINGE LINE. BASED ON THE TIME IN SERVICE (TIS) SUPPLIED BY THAT DA42 OPERATOR, A FLEET ACFT WITH EQUIVALENT TIME IN SERVICE WAS INSPECTED AND DID IN FACT HAVE SIMILAR CABLE WEAR AT THAT LOCATION. THE LT AND RT RUDDER CABLES WERE SCHEDULED TO BE REPLACED. DUE TO THE INSTALLATION, THE RUDDER CABLES MUST BE INSTALLED WITHOUT A FINISHED END AT THE AFT END OF THE CABLE. A SWAGED FITTING INSTALLATION MUST BE ACCOMPLISHED IAW AC 43.13-2B. THERE IS NO WAY TO TEST THE STRENGTH OF THE FINISHED SWAGED FITTING. THE FITTING AND SLEEVE WERE ASSEMBLED AND FABRICATED IAW INSTRUCTIONS OUTLINED IN THE ACFT MM AS WELL AS AC43.13-2B. THE FINISHED FITTING WAS COMPARED TO THE ORIGINAL FITTING AND FOUND TO BE VERY CLOSE IN APPEARANCE AND DIMENSION. AFTER APPROX 15.9 HOURS OF OPERATION, THE RT RUDDER CABLE FAILED AT THE AFT SWAGE. AN INVESTIGATION REVEALED THAT ALTHOUGH VERY SIMILAR IN DIMENSION AND APPEARANCE, THE REPLACEMENT SWAGE WAS SLIGHTLY LARGER IN SIZE. A GAUGE FOR MEASURING THE COMPLETED SWAGE HAD BEEN USED ON BOTH THE FACTORY SWAGE AS WELL AS THE REPLACEMENT SWAGE WITH THE SAME RESULTS. DUE TO THE CIRCUMSTANCES WHICH RESULTED IN A FAILED CABLE, SEVERAL PRECAUTIONS SHOULD BE CONSIDERED: A TEST CABLE SHOULD BE FABRICATED USING THE CORRECT CABLE MATERIAL, HARDWARE, TOOL AND GAUGE. THIS CABLE SHOULD BE TESTED BY A CERTIFIED AGENCY TO VERIFY THAT IT MEETS THE TENSION REQUIREMENTS FOR THAT INSTALLATION. SINCE THE TOLERANCE BETWEEN AN ACCEPTABLE AND UNACCEPTABLE SWAGE IS EXTREMELY PRECISE, ONLY A GAUGE OF EXACT TOLERANCE SHOULD BE USED. ALSO, A NUMERIC DIMENSION SHOULD BE OBTAINED FOR A PROPERLY COMPLETED SWAGE AND THAT DIMENSION SHOULD BE OBTAINED AFTER CRIMPING. ONLY A CALIBRATED ACCURATE VERNIER CALIPER SHOULD BE USED TO MEASURE THAT DIMENSION. SOME FORM OF SLIPPAGE INDICATOR SHOULD BE APPLIED TO THE FINISHED SWAGE SUCH AS TORQUE SEAL OR PAINT SO THAT ANY MOVEMENT CAN BE DETECTED DURING PREFLIGHT.
Part: PEDAL — CRACKED (RUDDER) · airframe 1,313 hrs
DURING A ROUNTINE INSPECTION, THE RUDDER CABLE WAS FOUND WORN WITH BROKEN STRANDS WHERE IT EXITS THE TUBE ABOUT 2 INCHES FORWARD OF THE RUDDER BELLCRANK. THIS IS APPROXIMATELY ON THE RUDDER HINGE LINE. ONCE THE CABLE AS REMOVED ADDITION WEAR WAS FOUND 33 INCHES INSIDE THE TUBE. SINCE BOTH ENDS OF THE CABLE ARE SWAGED, THIS CABLE WOULD NEVER BE REMOVED TO INSPECT FOR THAT WAER MIDWAY IN THE PROTECTIVE TUBE.