# N113DA: 1972 Slingsby T59D KESTREL 19 - Status: Valid registration - Airframe: [Slingsby T59D KESTREL 19](https://openairdocs.org/model/slingsby-t59d-kestrel-19) (registry code 8321510, 2 seats) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Serial number: 1799 - Year built: 1972 - Type: Glider - Engine type: None - Airworthiness: Standard, normal, glider - Airworthiness date: April 6, 1973 - Certificate issued: June 30, 2015 - Expires: June 30, 2028 - Mode S code: A037A4 - Registered owner: [Del Mar College](https://openairdocs.org/faa-owner/DEL%20MAR%20COLLEGE) - Location: [Corpus Christi, TX](https://openairdocs.org/faa-place/TX/Corpus%20Christi) - Owner type: Government - Owner's area on the map: 27.7679° N, 97.3994° W: Placed by OpenAirDocs at the center of ZIP code 78404, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=113DA - Page: https://openairdocs.org/aircraft/N113DA 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 (Slingsby T59D KESTREL 19) None in force. ### Matched by engine (NONE) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N113DA. ## NTSB investigations on N113DA not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA05MA083](https://openairdocs.org/ntsb/DCA05MA083), Jul 11, 2005: Boeing 767-232 (N113DA), Raleigh-Durham, NC, no damage. Probable cause: An inadvertent in-flight encounter with clear air turbulence. ## FAA accident and incident reports None matched to N113DA. ## Reports on N113DA not matched to an aircraft (2) They name N113DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 20050711017559A](https://openairdocs.org/incident/20050711017559A), Jul 11, 2005: Boeing 767232 (N113DA), Huntersville, NC. (-23) Delta flight 952, 757-200, 37,000FT, 20 miles northeast of clt in route from atl to lga, encountered turbulence while navigating cells. During turbulence… - [Incident 19870730046572I](https://openairdocs.org/incident/19870730046572I), Jul 30, 1987: Boeing 767232 (N113DA), Los Angeles, CA, Minor damage. After pushback, a taxiing metroliners rudder struck the underside of the Boeing 767 wing outer panel. ## 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 N113DA not matched to an aircraft (24) They name N113DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DL767041130](https://openairdocs.org/sdr/DL767041130), Dec 22, 2004: ODOR. DETECTED. DURING CLIMBOUT, SMELL NOTICED IN COCKPIT, LIKE BURNING PLASTIC. RAN ENGINES AND PACKS, UNABLE TO DUPLICATE. SUSPECT RECENT FAN LUBE. - [SDR DL767030437](https://openairdocs.org/sdr/DL767030437), May 5, 2003: SUPPORT FITTING. CORRODED. THE HOLE BORES FOR THE FLAP ATTACMENTS ON THE INBD SUPPORT FITTING ON THE LT INBD FLAP ON THE LT WING WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZI - [SDR DL767030438](https://openairdocs.org/sdr/DL767030438), May 4, 2003: SUPPORT FITTING. CORRODED. THE ATTACH HOLE BORES FOR THE INBD FLAP, OUTBD SUPPORT FITTING ON THE LT WING WERE FOUND CORRODED WITH ADDITIONAL CORROSION ON THE FACES OF THE LUGS. THE HOLE B - [SDR DL767030043](https://openairdocs.org/sdr/DL767030043), Jan 10, 2003: MODULE. LEAKING. A/C 113 LOST C-SYS HYDRAULIC QUANTITY INFLIGHT. A/C WAS INBOARD TO ATL. FOUND RAT TEST MODULE IN RT W/W LEAKING. REPLACED SAME. - [SDR DL767020502](https://openairdocs.org/sdr/DL767020502), May 4, 2002: FAN. FAILED. EICAS MSG INFLT - RT RECIR FAN, ALONG WITH INOP LIGHT IN RT RECIR FAN SWITCH. REPLACED RT RECIRC FAN, OP CKS GOOD. - [SDR DL767020442](https://openairdocs.org/sdr/DL767020442), Apr 16, 2002: MONITOR. FAULTY. AFTER T/O, RIGHT HYD QTY WENT TO ZERO, ATB. FOUND RIGHT HYD QTY IND INOP. NO ASSOCIATED LOW PRESS LIGHTS REPLACED MONITOR AND TRANSMITTER PER M/M, OP CHECKED NO - [SDR DL767011467](https://openairdocs.org/sdr/DL767011467), Sep 3, 2001: PANEL. FAULTY. DURING TROUBLESHOOTING OF OVERWING SLIDE DOOR SQUIB TEST, SQUIBS WERE INADVERTANTLY FIRED. REPLACED SQUIB PANEL - [SDR DL767011455](https://openairdocs.org/sdr/DL767011455), Sep 1, 2001: MEC. DEFECTIVE. NR 2 ENGINE SHUT DOWN BY CREW ON APPROACH TO PBI. DURING CRUISE NOTICED RT THROTTLE/ENGINE WAS NOT RESPONDING TO MOVEMENT, COMMAND BAR WAS PRESENT. DURING DESCE - [SDR DL767002501](https://openairdocs.org/sdr/DL767002501), Dec 22, 2000: CONTROLLER. INOPERATIVE. CABIN WILL NOT PRESSURIZE IN AUTO 1 OR AUTO 2. REPLACED NR 2 CABIN PRESS CONTROLLER AND CONTROL PANEL. RAN SELF TEST ALL NORMAL. FWD NBR 1 SYS TO MCO AND PLAC P - [SDR DL767002470](https://openairdocs.org/sdr/DL767002470), Dec 14, 2000: SKIN. DENTED. FUSELAGE SKIN REPAIR AT STA 566-573 AND STR 35L-36L, ERA 396471-14 ISSUED TO REPAIR DENT DAMAGE (DUE TO GROUND DAMAGE) - [SDR DL767002469](https://openairdocs.org/sdr/DL767002469), Dec 14, 2000: SKIN. DENTED. FUSELAGE SKIN AT STA 1480-1502, STR 24R TO 29R, PERMANENT REPAIR WAS ACCOMPLISHED FOR EXISTING SKIN REPAIR. REFERENCEERA 396597-14. - [SDR DL767992213](https://openairdocs.org/sdr/DL767992213), Oct 4, 1999: BULKHEAD CHORD. CRACKED. FUSELAGE BULKHEAD FS 1809.5, LBL 45 OUTER CHORD, CRACK REPAIR. THE FS 1809.5 BULKHEAD OUTER CAP WAS FOUND WITH A TYPICAL CRACK AT LBL 45. THE CRACK IS TYPICAL O - [SDR DL767991297](https://openairdocs.org/sdr/DL767991297), Jun 8, 1999: HOSE. FAILED. RIGHT MAIN GEAR TRUCK TILT HYD HOSE BURST. A/C DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC HOSE TO TRUCK TILT ACTUATOR BURST. REPLACED HOSE. - [SDR DL767982222](https://openairdocs.org/sdr/DL767982222), Oct 26, 1998: AIR DIST. SMOKE. F/A REPORTED SMOKE IN AFT CABIN. UPON DISCONNECTING UTILITY BUSES ODOR/SMELL WENT AWAY. RESET UTILITY BUSES OPERATED ALL GALLEY EQUIPMENT, NO ODOR PRESENT. RAN - [SDR DL767981885](https://openairdocs.org/sdr/DL767981885), Sep 10, 1998: SKIN. CORRODED. CORROSION DAMAGE WAS FOUND DURING ROUTINE INSPECTION OF THE CENTER WING UPPER SKIN OVERLYING THE REAR SPAR. CORROSION WAS LOCATED AT LBL 68 NEAR THE DRAIN AT LB - [SDR DL767981886](https://openairdocs.org/sdr/DL767981886), Sep 9, 1998: FLOORBEAM. CORRODED. CORROSION WAS FOUND ON THE UPPER CAP OF THE RBL 33 LONGITUDINAL OVERWING FLOORBEAM BETWEEN FS 835 AND 910. A SECTION OF UPPER CAP WILL BE REPLACED WITH A SPLICE - [SDR DL767980421](https://openairdocs.org/sdr/DL767980421), Feb 18, 1998: WEDGE. DELAMINATED. THE UPPER SKIN OF THE RT WING NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 4 X 2.5 AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER THE B767 SRM 57-43-02 AND - [SDR DL767980420](https://openairdocs.org/sdr/DL767980420), Feb 18, 1998: WEDGE. DELAMINATION. THE UPPER SKIN OF THE LT WING NR 5 SLAT WAS FOUND WITH A 1 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER - [SDR DL767980813](https://openairdocs.org/sdr/DL767980813), Jan 15, 1998: BATTERY. DISCHARGED. JUMPSEAT TWO CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY AND BULB ASSY. - [SDR DL767971526](https://openairdocs.org/sdr/DL767971526), Jul 30, 1997: SKIN. DELAMINATED. TWO AREAS OF DELAMINATION WERE FOUND ON THE UPPER SKIN OF THE NR 11 SLAT T/E WEDGE. ONE AREA OF DELAMINATION WAS FOUND ON THE UPPER SKIN OF THE NR 12 SLAT T/E W - [SDR DL767961466](https://openairdocs.org/sdr/DL767961466), Jun 18, 1996: IDG. MALFUNCTIONED. FORTY-FIVE MINUTES OUT OF SAN JUAN, GOT LEFT GENERATOR DRIVE LIGHT WITH 'L' IDG OIL TEMP STATUS MSG. DISCONNECTED CSD. STARTED APU, BUT APU GENERATOR BREAKER WO - [SDR DL767954642](https://openairdocs.org/sdr/DL767954642), Dec 7, 1995: BATTERY. DISCHARGED. SQUIB TEST 1 THE LEFT LIGHT DOES NOT COME ON FOR SLIDE. SQUIB TEST 2 THE RIGHT LIGHT DOES NOT COME ON FOR SPOLILER. REPLACED RIGHT HAND OVER WING SLIDE BATTERY - [SDR DL767954432](https://openairdocs.org/sdr/DL767954432), Nov 19, 1995: EEL POWER SUPPLY. INOPERATIVE. POWER SUPPLY FOR ESCAPE PATH LIGHTING FAILED TEST DURING LAYOVER AT TOC. REPLACED POWER SUPPLY UNIT (P/N 333780100), CLEARED BY LOG BOOK ITEM. - [SDR DL767954527](https://openairdocs.org/sdr/DL767954527), Nov 18, 1995: SKIN. DELAMINATED. THE NR 8 L/E SLAT T/E WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. REPAIRED PER DL ERA 272443-14AD. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Slingsby T59D KESTREL 19 aircraft: https://openairdocs.org/model/slingsby-t59d-kestrel-19/aircraft.md - The NONE engine: https://openairdocs.org/engine/none.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.