# N5007Y: 2002 Hall Daniel M QCKSLVR MXL II SPORT - Status: Valid registration - Airframe: [Hall Daniel M QCKSLVR MXL II SPORT](https://openairdocs.org/model/hall-daniel-m-qckslvr-mxl-ii-sport) (registry code 056194C, 2 seats) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Serial number: 865 - Year built: 2002 - Type: Fixed wing single engine - Engine type: Reciprocating - Kit: Quicksilver Aircraft QUICKSILVER MXL II - Airworthiness: Experimental, amateur built - Airworthiness date: October 9, 2005 - Certificate issued: September 14, 2005 - Expires: April 30, 2028 - Mode S code: A63D54 - Registered owner: [Hall Daniel M](https://openairdocs.org/faa-owner/HALL%20DANIEL%20M) - Location: [Coldwater, MI](https://openairdocs.org/faa-place/MI/Coldwater) - Owner type: Individual - Owner's area on the map: 41.9055° N, 85.0313° W: Placed by OpenAirDocs at the center of ZIP code 49036, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5007Y - Page: https://openairdocs.org/aircraft/N5007Y From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Hall Daniel M QCKSLVR MXL II SPORT) None in force. ### Matched by engine (Amateur-built UNKNOWN ENG) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N5007Y. ## FAA accident and incident reports None matched to N5007Y. ## Reports on N5007Y not matched to an aircraft (2) They name N5007Y, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19900724048369I](https://openairdocs.org/incident/19900724048369I), Jul 24, 1990: Bell 206L1 (N5007Y), Houma, LA, Minor damage. Main rotor overspeed condition. Autorotated to water. Replaced bendix fuel control governor and engine. - [Incident 19880902053749I](https://openairdocs.org/incident/19880902053749I), Sep 2, 1988: Bell 206L1 (N5007Y), Houma, LA, Minor damage. Landed due to weather and low fuel. Unable to fuel,departed,ran out of fuel over alternate. Chopped tailboom landing ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N5007Y not matched to an aircraft (35) They name N5007Y, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR HEEA072532](https://openairdocs.org/sdr/HEEA072532), Apr 11, 2001: GPS. FAILED. WILL NOT COME ON LINE FOR 20-40 MINUTES. - [SDR HEEA072093](https://openairdocs.org/sdr/HEEA072093), Apr 5, 2001: TRANSCEIVER. MALFUNCTIONED. WILL NOT CHANGE FROM STANDBY TO IN USE AND VERY HARD TO CHANGE FREQUENCY FOR FIRST 20 TO 30 MINUTES OF FLIGHT. PERFORMED PRELIMINARY INSPECTION AND TESTED. ADJU - [SDR HEEA063854](https://openairdocs.org/sdr/HEEA063854), Aug 31, 1999: NOZZLE. CRACKED. ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED VANES ON NR 1 NOZZLE. INSTALLED NEW PART. - [SDR HEEA060930](https://openairdocs.org/sdr/HEEA060930), Feb 23, 1999: POWER SUPPLY. INOPERATIVE. POWER SUPPLY HAS NO POWER OUT AND TRIPS CIRCUIT BREAKER. - [SDR HEEA0015641](https://openairdocs.org/sdr/HEEA0015641), Aug 17, 1998: SHAFT. WORN. DRIVE SHAFT WORN. - [SDR HEEA0014735](https://openairdocs.org/sdr/HEEA0014735), Jun 11, 1998: INDICATOR. STICKING. OIL PRESSURE NEEDLE STICKS DURING START. - [SDR HEEA0014733](https://openairdocs.org/sdr/HEEA0014733), Jun 11, 1998: GYRO. INOPERATIVE. DG ROTOR WILL NOT SPIN. TIME SINCE REPAIR 0:00. - [SDR HEEA0014624](https://openairdocs.org/sdr/HEEA0014624), Jun 8, 1998: INDICATOR. STICKS. INDICATOR INTERMITTENTLY STICKS AT 200 DEGREES. - [SDR HEEA0014619](https://openairdocs.org/sdr/HEEA0014619), Jun 8, 1998: INDICATOR. MALFUNCTIONED. AIRSPEED NEEDLE RISES 45-50 DEGREES WHEN VHF IS KEYED. - [SDR HEEA0014574](https://openairdocs.org/sdr/HEEA0014574), Jun 4, 1998: TRANSDUCER. DEFECTIVE. FUEL SYSTEM TRANSDUCER GIVES INTERMITTENT READINGS. - [SDR HEEA0013958](https://openairdocs.org/sdr/HEEA0013958), Apr 16, 1998: FIRE EXTINGUISHE. DEFECTIVE. PRESSURE AND WEIGHT ARE LOW. - [SDR HEEA0013730](https://openairdocs.org/sdr/HEEA0013730), Apr 2, 1998: TACH GEN. WORN. TACH GEN WORN SPLINE. - [SDR HEEA0013496](https://openairdocs.org/sdr/HEEA0013496), Mar 19, 1998: PANEL. MISMANUFACTURED. INSERTS FOR FUEL CROSSOVER MISLOCATED FROM BELL. - [SDR HEEA0012310](https://openairdocs.org/sdr/HEEA0012310), Dec 8, 1997: FLOAT ASSY. DEFECTIVE. UNBONDED O-RINGS IN INLET VALVE. - [SDR HEEA0011733](https://openairdocs.org/sdr/HEEA0011733), Oct 31, 1997: LONGERON. DEFECTIVE. ANGLE OF BEND ON LONGERON AFT END NOT CORRECT. ORIGINAL PART 55 DEGREES. NEW PART 69 DEGREES. - [SDR HEEA0011556](https://openairdocs.org/sdr/HEEA0011556), Oct 16, 1997: DOOR ASSY. CORRODED. DOOR ASSY CORRODED BEYOND LIMITS. - [SDR HEEA0011130](https://openairdocs.org/sdr/HEEA0011130), Oct 1, 1997: CHANNEL. MIS MFG. CENTER OF CHANNEL IS BOWED TOO MUCH KICKING THE AFT END UPWARD CAUSING NO EDGE DISTANCE FOR THE RIVETS IN THE CENTER AREA APPROXIMATELY 10" FROM AFT EDGE TO APP - [SDR HEEA0011129](https://openairdocs.org/sdr/HEEA0011129), Oct 1, 1997: SUPPORT. MALFORMED. SUPPORT MALFORMED IN MANUFACTURING PROCESS. TWISTED AND INCONSISTENT PARALLELS. UPPER RADIAL LEG BENT TOO MUCH AT CENTER SECTION. - [SDR HEEA0010581](https://openairdocs.org/sdr/HEEA0010581), Aug 6, 1997: CELL. SEEPAGE. FUEL CELL FUEL SEEPAGE. - [SDR HEEA0010577](https://openairdocs.org/sdr/HEEA0010577), Aug 6, 1997: FLUX DETECTOR. FAILED. FLUX DETECTOR UNIT HAS NO OUTPUT. - [SDR HEEA0010443](https://openairdocs.org/sdr/HEEA0010443), Jul 10, 1997: LINK ASSY. BEARING FAILED. LINK ASSY BEARING SEPARATED. - [SDR HEEA0010442](https://openairdocs.org/sdr/HEEA0010442), Jul 10, 1997: LINK ASSY. BEARING FAILED. LINK ASSY BEARING SEPARATED. - [SDR HEEA0010258](https://openairdocs.org/sdr/HEEA0010258), Jun 25, 1997: LINK ASSY. DELAMINATED. LINK ASSY BEARINGS TORN AND DELAMINATED. - [SDR HEEA0010256](https://openairdocs.org/sdr/HEEA0010256), Jun 25, 1997: LINK ASSY. DELAMINATED. LINK ASSY BEARINGS TORN AND DELAMINATED. - [SDR HAIHEEA9666](https://openairdocs.org/sdr/HAIHEEA9666), Apr 29, 1997: ACTUATOR. FAILED. ACTUATOR WILL NOT OPERATE. - [SDR HAIHEEA9465](https://openairdocs.org/sdr/HAIHEEA9465), Apr 23, 1997: SKID TUBE. CRACKED. FOUND THREE CRACKS ON RH SKID TUBE RADIATING FROM SKID PLATE AND FLOAT MOUNTING HOLES. HAVE FOUND THREE SKID TUBES CRACKED IN THS MANNER ALL MANUFACTURED AUGUST - [SDR HAIHEEA9464](https://openairdocs.org/sdr/HAIHEEA9464), Apr 23, 1997: SKID TUBE. CRACKED. FOUND EIGHT CRACKS ON RH SKID TUBE RADIATING FROM SKID PLATE MOUNTING HOLES. THIS TUBE WAS MANUFACTURED AUGUST 14, 1995. HAVE FOUND THREE SKID TUBES CRACKED IN - [SDR 97ZZZX1676](https://openairdocs.org/sdr/97ZZZX1676), Mar 12, 1997: SKID TUBE. CRACKED. FOUND 3 CRACKS ON RT SKID TUBE RADIATING FROM SKID PLATE AND FRONT MOUNTING HOLES. HAVE FOUND 3 SKID TUBES CRACKED IN THIS MANNER. ALL MFG AUG '95. REPLACED TUB - [SDR 97ZZZX1675](https://openairdocs.org/sdr/97ZZZX1675), Mar 12, 1997: SKID TUBE. CRACKED. FOUND 8 CRACKS ON RT SKID TUBE RADIATING FROM SKIP-PLATE MOUNTING HOLES. THIS TUBE WAS MFG 8-14-95. HAVE FOUND 3 SKID TUBES CRACKED IN THIS MANNER. ALL TUBES WE - [SDR HEEA967614](https://openairdocs.org/sdr/HEEA967614), Jul 31, 1996: TRANSCEIVER. FAILED. TRANSCEIVER UNIT WILL NOT LIGHT UP OR TRANSMIT. - [SDR HEEA967281](https://openairdocs.org/sdr/HEEA967281), May 30, 1996: EXHAUST ASSY. CRACKED. EXHAUST ASSY IS CRACKED. (CRACK 3/4" LONG AT BASE MOUNTING FLANGE AND 1 1/4" LONG VERTICAL CRACK AT WELDED SEAM INTERSECTING EACH OTHER IN FORM OF REVERSED "T". - [SDR HEEA966783](https://openairdocs.org/sdr/HEEA966783), Feb 28, 1996: FLEXURE. DETERIORATED. FLEXURE HAS DETERIORATED ELASTOMER. - [SDR HEEA966329](https://openairdocs.org/sdr/HEEA966329), Jan 2, 1996: COUPLING. STEP WEAR. ENGINE REMOVED DUE TO TURBINE 3RD STAGE WHEEL REPLACEMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND LIMITS ON N1 COUPLING I.D. SPL - [SDR HEEA956231](https://openairdocs.org/sdr/HEEA956231), Dec 12, 1995: WHEEL. CRACKED. ENGINE REMOVED DUE TO 3RD STAGE TURBINE WHEEL INSPECTION. 3RD STAGE WHEEL RETURNED TO ALLISON FOR INSPECTION PER LETTER C1245F-RMG-1195. ZYGLO INSPECTION REVEAL - [SDR HEEA955988](https://openairdocs.org/sdr/HEEA955988), Nov 8, 1995: TRANSCEIVER. FAILED. NOT RECEIVED BY TOWER. FOUND POWER SLIGHTLY LOW AT ABOUT 150W. ADJUSTED POWER UP, FREQUENCY AND PULSE SHAPE. REPLACED DETERIORATED RESISTOR R477 AND DEFECTIVE P ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N5007Y The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5007Y before. - [Cancelled 1967-12-12](https://openairdocs.org/deregistered/N5007Y-1967-12-12): Piper PA-23-250, S/N 27-2007. Exported to Australia. Owner: [Capitol Aviation Inc](https://openairdocs.org/faa-owner/CAPITOL%20AVIATION%20INC), [Springfield, IL](https://openairdocs.org/faa-place/IL/Springfield) ## Related - Other Hall Daniel M QCKSLVR MXL II SPORT aircraft: https://openairdocs.org/model/hall-daniel-m-qckslvr-mxl-ii-sport/aircraft.md - The Amateur-built UNKNOWN ENG engine: https://openairdocs.org/engine/amateur-built-unknown-eng.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.