# N701AA: 2009 Smith Roland W ZENITH CH 701 - Status: Valid registration - Airframe: [Smith Roland W ZENITH CH 701](https://openairdocs.org/model/smith-roland-w-zenith-ch-701) (registry code 05627RL, 2 seats) - Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572) - Serial number: 7-5599 - Year built: 2009 - Type: Fixed wing single engine - Engine type: Reciprocating - Kit: Zenith Acft Co STOL CH 701 - Airworthiness: Experimental, amateur built - Airworthiness date: December 2, 2009 - Certificate issued: July 3, 2017 - Expires: July 31, 2027 - Mode S code: A95846 - Registered owner: [Turek Air LLC](https://openairdocs.org/faa-owner/TUREK%20AIR%20LLC) - Location: [King Ferry, NY](https://openairdocs.org/faa-place/NY/King%20Ferry) - Owner type: LLC - Owner's area on the map: 42.6736° N, 76.6272° W: Placed by OpenAirDocs at the center of ZIP code 13081, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=701AA - Page: https://openairdocs.org/aircraft/N701AA 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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Smith Roland W ZENITH CH 701) None in force. ### Matched by engine (Rotax 912ULS series) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N701AA. ## NTSB investigations on N701AA 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 FTW85IA168](https://openairdocs.org/ntsb/FTW85IA168), Mar 29, 1985: Boeing 727-200B (N701AA), Mexico City, Mexico, incident, minor damage ## FAA accident and incident reports None matched to N701AA. ## Reports on N701AA not matched to an aircraft (2) They name N701AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19850329026869I](https://openairdocs.org/incident/19850329026869I), Mar 29, 1985: Boeing 727200 (N701AA), Mexico City, Mexico, Substantial damage. Struck light standard after liftoff. Crew did not use all runway, turn off ac packs, did not have performance data. - [Incident 19820310011649I](https://openairdocs.org/incident/19820310011649I), Mar 10, 1982: Boeing 727200 (N701AA), Detroit, MI, Minor damage. Aircraft hit snow ridge on side of taxiway which was closer to taxiway than in most other areas. Ridge was removed. ## 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 N701AA not matched to an aircraft (31) They name N701AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AALA990061](https://openairdocs.org/sdr/AALA990061), Dec 30, 1998: SKIN. CORRODED. TUL - FOUND CORROSION ON SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER (PLENUM) FROM STATION 830 TO STRINGER 850. INSTALLED REPAIRS PER SRM 57-30-3 FIG 8 AND FIG 9. ( - [SDR AALA980291](https://openairdocs.org/sdr/AALA980291), Feb 9, 1998: FRAME. CORRODED. TUL - STA 970 FRAME AND SHEAR TIE CORRODED BETWEEN STR 29R AND STR 36. INSTALLED DOUBLER PER SRM 53-10-4 FIG 12. TST: 46,991 HOURS. CYCLES: 24,531. (X) - [SDR AALA980290](https://openairdocs.org/sdr/AALA980290), Feb 9, 1998: STRINGER. CORRODED. TUL - CORROSION AT STR 29L AT STA 971. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER 51-10-6. ACCOMPLISHED REPAIR PER ECO 11697 DATED 2-2-98. TST: 4 - [SDR AALA970919](https://openairdocs.org/sdr/AALA970919), May 17, 1997: CLAMP. LOOSE. MEX - FLT 2147 - EN ROUTE MIZ/MEX DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WITH NR 1 PO - [SDR AALA970445](https://openairdocs.org/sdr/AALA970445), Mar 3, 1997: CONNECTOR. LOOSE. MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 25D THROUGH 28D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNEC - [SDR AALA961352](https://openairdocs.org/sdr/AALA961352), Sep 13, 1996: CONNECTOR. BROKEN. MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYS - [SDR AALA961120](https://openairdocs.org/sdr/AALA961120), Jul 27, 1996: LIGHT STRIP. DEFECTIVE. RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 29DEF AND 30DEF INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT RO - [SDR AALA960857](https://openairdocs.org/sdr/AALA960857), Jun 2, 1996: LIGHT. DEFECTIVE. RDU - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOORS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOOR. SYSTEM GROUND - [SDR AALA960478](https://openairdocs.org/sdr/AALA960478), Mar 25, 1996: STRINGER. CORRODED. FOUND CORROSION IN STRINGER 27 RT FROM STATION 615 TO STATION 620. REPAIRED STRINGER 27 RT STATION 615 TO STATION 620 PER SRM 53-10-3, FIG 1. (M) - [SDR AALA960477](https://openairdocs.org/sdr/AALA960477), Mar 25, 1996: SKIN. WORN. TUL - UPPER FWD CORNER OF CARGO DOOR OPENING WORN. REPORTED PER ESO 11697, DATED 2-28-96. (M) - [SDR AALA960476](https://openairdocs.org/sdr/AALA960476), Mar 25, 1996: SKIN. CORRODED. FOUND CORROSION ON STRINGER 29L AND SKIN FWD OF 950E AFT CARGO FROM 950D-950E. REMOVED CORROSION FROM SKIN AND STRINGER 29L AT 950D-950E NDT DETERMINED THICKNES - [SDR AALA960475](https://openairdocs.org/sdr/AALA960475), Mar 25, 1996: SKIN. CORRODED. TUL - CORROSION LOWER WING SKIN EXTENSION OUTBOARD OF NR 4 SLAT TRACK. REPAIRED PER B727 AARD 57-30-00-2 PG 1-3. (M) - [SDR AALA960474](https://openairdocs.org/sdr/AALA960474), Mar 25, 1996: BLKHD BEAM. CRACKED. FOUND VERTICAL BEAM CRACKED AT STATION 1183 RBL 36, BOTH SIDES APPROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW BOEING 727 SB NR 727-53-0192. (M) - [SDR AALA960473](https://openairdocs.org/sdr/AALA960473), Mar 25, 1996: SKIN. CORRODED. TUL - FOUND CORROSION INSIDE FUSELAGE SKIN FWD CARGO BILGE. REMOVED CORROSION INSIDE SKIN AND BLENDED OUT SRM 51-10-6 DAMAGED AREA NOT CUT OUT PER ESO 11697 DAT - [SDR AALA960472](https://openairdocs.org/sdr/AALA960472), Mar 25, 1996: WEB. CORRODED. FOUND CORROSION FORWARD CARGO DOOR WEB LANDING AT FWD AND AFT ENDS. REMOVED CORRODED WEB BOTH ENDS AT FWD CARGO DOOR MANUFACTURED NEW WEBS 7075-T6 .071 AND CHOR - [SDR AALA960471](https://openairdocs.org/sdr/AALA960471), Mar 25, 1996: STRINGER. CORRODED. TUL - FOUND CORROSION IN STRINGER SPLICE STRINGER 28L, STATION 680. INSTALLED STRINGER REPAIR STATION 680, STRINGER 28L IAW SRM 53-10-3. (M) - [SDR AALA960470](https://openairdocs.org/sdr/AALA960470), Mar 25, 1996: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 27R STATION 680-706. CUT OUT CORRODED AREA OF STRINGER, FABRICATED AND INSTALLED SPLICE PLACE PER SRM 51-10-1. (M) - [SDR AALA960469](https://openairdocs.org/sdr/AALA960469), Mar 25, 1996: SKIN. CRACKED. FOUND SKIN HAS CRACK AND CORROSION AT STRINGER 27R, STATION 695. CUT OUT CORROSION ON SKIN FROM STATION 695-680 ALONG STRINGER 27R. INSTALLED DOUBLER ON SKIN FR - [SDR AALA960468](https://openairdocs.org/sdr/AALA960468), Mar 25, 1996: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 29RT, STATION 992 TO 102. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-10-3 PGS 11A THROUGH 11E. (M) - [SDR AALA960463](https://openairdocs.org/sdr/AALA960463), Mar 25, 1996: STRINGER. CORRODED. FOUND CORROSION IN STRINGER SPLICE 28R, STATION 680. REPAIRED STRINGER 28R AT STATION 680, IAW SRM 53-10-3. (M) - [SDR AALA960462](https://openairdocs.org/sdr/AALA960462), Mar 25, 1996: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 27L, FS 690. CUT OUT DAMAGED AREA INSTALLED DOUBLER REF 53-10-3. (M) - [SDR AALA960460](https://openairdocs.org/sdr/AALA960460), Mar 25, 1996: FRAME. CORRODED. FOUND CORROSION ON 1148 FRAME IN AFT CARGO BILGE. REPAIRED PER SRM 53-10-4 FIG 12. (M) - [SDR AALA960325](https://openairdocs.org/sdr/AALA960325), Feb 27, 1996: SKIN. CRACKED. TUL - CROWN SKIN CRACKED IN 2 PLACES AT STA 1096 EACH SIDE STR 1 AT INLET DOGHOUSE ATTACH ANGLE. CUT OUT CRACKED AREAS AND INSTALLED DOUBLER PER SB 727-53A-204, - [SDR AALA952065](https://openairdocs.org/sdr/AALA952065), Dec 9, 1995: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT CHECK, R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R1 DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA952061](https://openairdocs.org/sdr/AALA952061), Dec 8, 1995: CONNECTOR. BROKEN. RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GR - [SDR AALA951933](https://openairdocs.org/sdr/AALA951933), Nov 13, 1995: EEL WIRE. BROKEN. RDU - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH TRACK LIGHTING BRIGHT IN FIRST CLASS AND DIMMING TOWARDS THE AFT LAVATORIES. REPAIRED SPLICE I - [SDR AALA951828](https://openairdocs.org/sdr/AALA951828), Oct 19, 1995: EEL CONNECTOR. BROKEN. RDU - FLT NR 0627 - DURING MAINTENANCE CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN INOPERATIVE. AIRCRAFT MAINTENANCE FERRY RDU/MIA. REPLACED BROKEN EMERGENCY FLO - [SDR AALA951761](https://openairdocs.org/sdr/AALA951761), Oct 8, 1995: LOCK ACTUATOR. DEFECTIVE. RDU - FLT NR 1040 - DURING APPROACH WHEN LOWERING GEAR THE LEFT GEAR DOOR, LIGHT AND RED GEAR LIGHT ILLUMINATED. CYCLED GEAR WITH SAME RESULTS. DID FLY BY AND C - [SDR AALA950784](https://openairdocs.org/sdr/AALA950784), May 2, 1995: SWITCH. DEFECTIVE. MIA - FLT 0480 - AFTER TAKEOFF, WHEN LANDING GEAR RETRACTED, RT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME RESULTS. AIRC - [SDR AALA950527](https://openairdocs.org/sdr/AALA950527), Mar 28, 1995: EEL ASSEMBLY. DEFECTIVE. MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKS NORMAL OPERAT - [SDR AALA950353](https://openairdocs.org/sdr/AALA950353), Feb 27, 1995: SPLICE. BROKEN. MIA - FLT 651 - DURING APPROACH WITH LANDING GEAR EXTENDED, NLG UNSAFE LIGHT ILLUMINATED AND AURAL WARNING HORN SOUNDED. ACCOMPLISHED GO-AROUND AND RECYCLED LAN ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Smith Roland W ZENITH CH 701 aircraft: https://openairdocs.org/model/smith-roland-w-zenith-ch-701/aircraft.md - The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.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.