# N575ML: Malcolm D Muir WITTMAN TAILWIND - Status: Valid registration - Airframe: [Malcolm D Muir WITTMAN TAILWIND](https://openairdocs.org/model/malcolm-d-muir-wittman-tailwind) (registry code 05632YO, 2 seats) - Serial number: 96-1025 - Type: Fixed wing single engine - Engine type: Reciprocating - Certificate issued: August 23, 2013 - Expires: August 31, 2029 - Mode S code: A7621A - Registered owner: [Muir Malcolm D](https://openairdocs.org/faa-owner/MUIR%20MALCOLM%20D) - Location: [Quincy, CA](https://openairdocs.org/faa-place/CA/Quincy) - Owner type: Individual - Owner's area on the map: 39.9292° N, 120.9244° W: Placed by OpenAirDocs at the center of ZIP code 95971, 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=575ML - Page: https://openairdocs.org/aircraft/N575ML 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 (Malcolm D Muir WITTMAN TAILWIND) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N575ML. ## FAA accident and incident reports None matched to N575ML. ## Reports on N575ML not matched to an aircraft (1) They name N575ML, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19990119039529I](https://openairdocs.org/incident/19990119039529I), Jan 19, 1999: Cndair CL6002B19 (N575ML), Atlanta, GA, Minor damage. Surveillance ASI noted midway airline CL-65, N575ML had struck an midwest express belt loader with the left wing leading edge, damage minor. Midwest express… ## 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 N575ML not matched to an aircraft (14) They name N575ML, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR WVE2003F00002](https://openairdocs.org/sdr/WVE2003F00002), Dec 20, 2002: ANGLE. CRACKED. DURING C CHECK THE INTERCOSTAL ATTACH ANGLE AT FS 484, LBL 27, WL 73.5 WAS FOUND TO BE CRACKED. (2003B0322) - [SDR MDR02046](https://openairdocs.org/sdr/MDR02046), Nov 11, 2002: FLOOR SUPPORT. CRACKED. DURING BRIDGING INSPECTION FOUND FS 621 FLOOR SUPPORT ANGLE RIGHT SIDE CRACKED. - [SDR MDR02045](https://openairdocs.org/sdr/MDR02045), Nov 11, 2002: FLOOR SUPPORT. CRACKED. DURING BRIDIGING INSPECTION FOUND FS 621 FLOOR SUPPORT ANGLE LEFT SIDE CRACKED. - [SDR MDR02044](https://openairdocs.org/sdr/MDR02044), Nov 9, 2002: PANEL. CHAFED. DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE COWL PANEL 432 AT TRAILING EDGE CHAFED 1 INCH BY .5 INCH BY .003 INCH DEEP. - [SDR MDR02043](https://openairdocs.org/sdr/MDR02043), Nov 9, 2002: TRACK. CHAFED. DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE TORQUE BOX MAIN BOX MAIN TRACK AT 6 O'CLOCK POSITION AFT END FITTING CHAFED. - [SDR MDR02042](https://openairdocs.org/sdr/MDR02042), Nov 9, 2002: TRACK. CHAFED. DURING BRIDGING INSPECTION DISCOVERED LEFT ENGINE TORQUE BOX MAIN TRACK AT 4 O'CLOCK POSITION AFT END FITTING CHAFED. - [SDR MDR02041](https://openairdocs.org/sdr/MDR02041), Nov 8, 2002: DOUBLER. CRACKED. DURING BRIDGING INSPECTION DISCOVERED LEFT DOUBLER CRACKED IN RADIUS 3 INCHES AT FS 718 BETWEEN STRINGERS 10 AND 12. - [SDR MDR02040](https://openairdocs.org/sdr/MDR02040), Nov 8, 2002: ANGLE. CRACKED. DURING BRIDGING INSPECTION DISCOVERED RIGHT OBLIQUE ANGLE CRACKED IN RADIUS 1.2500 AT FS 621-630. - [SDR MDR02039](https://openairdocs.org/sdr/MDR02039), Nov 8, 2002: ANGLE. CRACKED. DURING BRIDGING INSPECTION DISCOVERED LEFT OBLIQUE ANGLE CRACKED IN RADIUS 1.2500 INCHES AT FS 621-630. - [SDR JBXA000307](https://openairdocs.org/sdr/JBXA000307), Jul 12, 2001: HYDRAULIC SYSTEM. FAILED. Discrepancy : Lost #2 engine driven hydraulic pump and all fluid. Corrective Action : Removed and replaced #2 ED hydraulic pump I-A-W AMM 29-11-01 Ops check and - [SDR JBXA000289](https://openairdocs.org/sdr/JBXA000289), Jun 7, 2001: SWITCH. INOPERATIVE. ANTI-ICE DUCT MESSAGE DURING CLIMBOUT OF RDU. MSG AND AURAL ON THRU FL180 WITH ANTI-ICE IN OFF MSG AND AURAL INTERMITTENT BACK TO RDU. AUTO-ICE SYNOPTIC PAGE SH - [SDR JBXA000263](https://openairdocs.org/sdr/JBXA000263), Apr 6, 2001: PUMP. FAILED. NR 1 HYDRAULIC SYSTEM LOST ALL PRESSURE AND FLUID AT 26,000 FEET. RETURNED TO RDU. REMOVED AND REPLACED ALL NR 1 SYSTEM HYDRAULIC FILTERS IAW CRJ AMM 29-11-09, - [SDR JBXA000243](https://openairdocs.org/sdr/JBXA000243), Feb 11, 2001: HYDRAULIC LINE. CRACKED. NR 1 HYDRAULIC SYSTEM INDICATED ZERO PERCENT AT FL290 EN ROUTE TO BUF. RAN QRH AND DIVERTED TO PHL. FOUND PRESSURE LINE FROM EDP NR 1 TO PRESSURE FILTER CRACKED - [SDR JBXA0000159](https://openairdocs.org/sdr/JBXA0000159), Mar 27, 2000: ACTUATOR. BINDING. FLAPS FAIL MESSAGE AT 0 DEGREES. RESET AND FAILED AT 13 DEGREES ON APPROACH. REMOVED AND REPLACED LEFT WING OUTBOARD FLAP ACTUATORS NR 3 AND NR 4 IAW CL-65 AMM ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Malcolm D Muir WITTMAN TAILWIND aircraft: https://openairdocs.org/model/malcolm-d-muir-wittman-tailwind/aircraft.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.