# N767NA: 2022 Kaman Aerospace K-1200 - Status: Valid registration - Airframe: [Kaman Aerospace K-1200](https://openairdocs.org/model/kaman-aerospace-k-1200) (registry code 13027LS, 1 seats) - Engine: [Honeywell T5317A-1](https://openairdocs.org/engine/honeywell-t5317a-1) (registry code 33859) - Data sheets: [TCDS TR7BO](https://openairdocs.org/tcds/TR7BO) (Kaman Aerospace Corporation), [TCDS E17EA](https://openairdocs.org/tcds/E17EA) (Ozark Aeroworks LLC) (OpenAirDocs) - Serial number: A94-0049 - Year built: 2022 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: November 17, 2022 - Certificate issued: November 23, 2022 - Expires: November 30, 2029 - Mode S code: AA5CB6 - Registered owner: [Dh Helicopter Inc](https://openairdocs.org/faa-owner/DH%20HELICOPTER%20INC) - Location: [Whitefield, ME](https://openairdocs.org/faa-place/ME/Whitefield) - Owner type: Corporation - Owner's area on the map: 44.1980° N, 69.6197° W: Placed by OpenAirDocs at the center of ZIP code 04353, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=767NA - Page: https://openairdocs.org/aircraft/N767NA 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): 16 in force ### Matched by airframe (Kaman Aerospace K-1200) - [AD 2016-08-21](https://openairdocs.org/ad/2016-08-21): Main Rotor Control · Kaman Aerospace K-1200. Effective May 31, 2016 - [AD 2015-14-04](https://openairdocs.org/ad/2015-14-04): Main Rotor MRB · Kaman Aerospace K-1200. Effective Aug 17, 2015 - [AD 2010-26-11](https://openairdocs.org/ad/2010-26-11): Main Rotor Blades · Kaman Aerospace K-1200. Effective Jan 5, 2011 - [AD 2004-13-26](https://openairdocs.org/ad/2004-13-26): Main rotor blade (blade) grips · Kaman Aerospace K-1200. Effective Jul 22, 2004 - [AD 2001-13-03 R1](https://openairdocs.org/ad/2001-13-03-R1): Flap clevis · Kaman Aerospace K-1200. Effective May 27, 2003 - [AD 2000-18-10](https://openairdocs.org/ad/2000-18-10): Sprag Clutches · Kaman Aerospace K-1200. Effective Sep 26, 2000 - [AD 99-26-04](https://openairdocs.org/ad/99-26-04): Clutch Assembly · Kaman Aerospace K-1200. Effective Feb 8, 2000 ### Matched by engine (Honeywell T5317A-1) - [AD 2022-10-02](https://openairdocs.org/ad/2022-10-02): Engine Controls · Honeywell International T53-L-703, T53-L-13B S/SB, T53-L-13B S/SA and 14 more. Effective Jun 28, 2022 - [AD 2009-15-13](https://openairdocs.org/ad/2009-15-13): Combustion chamber housings (CCHs) · Honeywell International T5313B, T5317A, T5317A-1 and 2 more. Effective Aug 25, 2009 - [AD 2006-11-16](https://openairdocs.org/ad/2006-11-16): Fuel control regulator assemblies · Honeywell International T53-L-703, T53-L-13B/D, T53-L-13B and 8 more. Effective Jul 5, 2006 - [AD 2006-01-05](https://openairdocs.org/ad/2006-01-05): Turboshaft engine · Honeywell International T53-L-703, T53-L-13B/D, T53-L-13B S/SB and 12 more. Effective Feb 16, 2006 - [AD 2002-15-04](https://openairdocs.org/ad/2002-15-04): Compressor impellers · Honeywell International T53-L-703, T53-L-13B/D, T53-L-13B and 4 more. Effective Sep 10, 2002 - [AD 2002-09-09](https://openairdocs.org/ad/2002-09-09): Centrifugal Compressor Impeller · Honeywell International T53-L-703, T53-L-13B/D, T53-L-13B and 10 more. Effective Jun 13, 2002 - [AD 97-21-07 R1](https://openairdocs.org/ad/97-21-07-R1): Accessory Drive Carrier Assembly · Honeywell International T53-L-703, T5313B, T5317A and 1 more. Effective Jul 6, 1998 - [AD 97-07-05](https://openairdocs.org/ad/97-07-05): Accessory Drive Assembly · Honeywell International T53-L-703, T5311A, T5311B and 4 more. Effective Jun 24, 1997 - [AD 95-10-04](https://openairdocs.org/ad/95-10-04): Centrifugal Compressor Impeller · Honeywell International T5313B, T5317A, T5317A-1 and 1 more. Effective May 25, 1995 ### Historical (superseded or no longer in force) - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [AD 2001-13-03](https://openairdocs.org/ad/2001-13-03) (historical): Rotor Shaft and Teeter Pin Assembly · Kaman Aerospace K-1200. Effective Aug 1, 2001 - [AD 98-22-11](https://openairdocs.org/ad/98-22-11) (historical): Fuel Pumps · Honeywell International T5317A-1. Effective Dec 18, 1998 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N767NA. ## FAA accident and incident reports None matched to N767NA. ## 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 N767NA not matched to an aircraft (134, newest 50) They name N767NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR NOCA2014010623](https://openairdocs.org/sdr/NOCA2014010623), Jan 6, 2014: BATTERY PACK. DISCHARGED. IN CABIN EMERGENCY LIGHTS OVERHEAD AFT LT SIDE AISLE WILL NOT ILLUMINATE. R & R BATTERY PACK AT M739 IAW AMM 33-51-01 AND OPS CHECKED OK. - [SDR NOCA2013112317](https://openairdocs.org/sdr/NOCA2013112317), Nov 23, 2013: BATTERY PACK. INOPERATIVE. F/A EMERGENCY FLASHLIGHT IN AFT GALLEY RED LIGHT NOT BLINKING. R & R FLASHLIGHT BATTERY PACK IN AFT GALLEY CENTER FLT ATTEND STATION. OPS CHECKED NORMAL IAW AMM - [SDR NOCA201309165](https://openairdocs.org/sdr/NOCA201309165), Sep 16, 2013: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHT AT DOORS L4 & R4 DO NOT ILLUMINATE. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. - [SDR NOCA09812](https://openairdocs.org/sdr/NOCA09812), Nov 11, 2012: BATTERY PACK. DISCHARGED. LEFT FWD ENTRY DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1028 AS PER MM 33-51-07, OPS CHECK GOOD. - [SDR NOCA20121111097](https://openairdocs.org/sdr/NOCA20121111097), Nov 11, 2012: BATTERY PACK. DISCHARGED. LEFT FWD ENTRY DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1028 AS PER MM 33-51-07, OPS CHECK GOOD. - [SDR NOCA09713](https://openairdocs.org/sdr/NOCA09713), Oct 17, 2012: LIGHT. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT INOP AT SEATS 11FG. REMOVED AND REPLACED LIGHT ASSY AT FLOOR SEAT 11FG PER AMM 33-51-10 P/N OFF - S417N509-14, P/N ON - 81000-22601. - [SDR NOCA06812](https://openairdocs.org/sdr/NOCA06812), Jul 17, 2012: CYLINDER. DISCHARGED. WHILE PERFORMING ARMFIRE SWITCH CHECK, OUTER OVERWING SLIDE DOOR ACTUATED. REPLACED CYLINDER AND 3 DOOR LATCH ACTUATORS. - [SDR NOCA07212](https://openairdocs.org/sdr/NOCA07212), Jul 13, 2012: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOP THROUGHOUT PASS CABIN ENTIRE FRONT SECTION AND AT ROW 15, 24, 35, AND 27 THROUGH 31. REPAIRED BROKEN WIRES AT SEAT AND DOOR EMERGENCY LIGH - [SDR NOCA07112](https://openairdocs.org/sdr/NOCA07112), Jul 10, 2012: BATTERY PACK. DISCHARGED. ALL EMERGENCY LIGHT BATTERY PACKS FAILED TO TURN ON EXCEPT FOR THE 2 OVERWING LIGHT CHECK. RESET BREAKERS AND CHARGED BATTERIES. REMOVED AND REPLACED M738 BATTE - [SDR NOCA201207090001](https://openairdocs.org/sdr/NOCA201207090001), Jul 7, 2012: SLIDE. UNWANTED DEPLOY. L3 DOOR SLIDE DEPLOYED DURING COURSE OF TROUBLESHOOTING CREW COMPLAINT. L3 DOOR OPENED WHEN DOOR WAS ARMED. SLIDE DEPLOYED BUT DID NOT INFLATE. REPLACED THE L3 - [SDR NOCA06112](https://openairdocs.org/sdr/NOCA06112), Jun 30, 2012: ATTACH BRACKET. CRACKED. NR 1 PYLON EDP SHUTOFF VALVE ATTACH BRACKET IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED WITH NEW PYLON EDP SHUTOFF VALVE ATTACH BRACKET IAW EO 767-54-022, - [SDR NOCA06612](https://openairdocs.org/sdr/NOCA06612), Jun 29, 2012: WINDOW FRAME. CORRODED. LEFT WINDOW FRAME STA 1175-1197 HAS PITTING CORROSION IN PREVIOUS BLENDOUT ON LWR AFT SIDE. REMOVED AND REPLACED WINDOW FRAME (P/N 140T240104) PER SRM 51-40-02 - [SDR NOCA07612](https://openairdocs.org/sdr/NOCA07612), Jun 28, 2012: MOUNT. DAMAGED. NR 1 ENGINE FORWARD LOWER MOUNT UPPER MATING SURFACE HAS SEVERAL AREAS OF MECH DAMAGE, PITTING & CHIPPING AROUND FASTENER HOLES. REMOVED AND REPLACED NR 1 ENGIN - [SDR NOCA07512](https://openairdocs.org/sdr/NOCA07512), Jun 28, 2012: MOUNT. DAMAGED. NR 1 ENGINE AFT LWR MOUNT UPPER MATING SURFICE HAS SEVERAL AREAS OF MECHANICAL DAMAGE. REMOVED AND REPLACED NR 1 UPPER FITTING ON NR 1 AFT LWR MOUNT IAW AMM 71- - [SDR NOCA2012071100001](https://openairdocs.org/sdr/NOCA2012071100001), Jun 28, 2012: MOUNT. CORRODED. NR 2 FORWARD LOWER ENGINE MOUNT UPPER SURFACE IS FRETTING AT THE AFT I/B FASTENER HOLE. REMOVED AND REPLACED NR 2 FWD MOUNT LOWER MOUNT PLATFORM PER MM 71-21-01 - [SDR NOCA07012](https://openairdocs.org/sdr/NOCA07012), Jun 21, 2012: SKIN. GOUGED. LEFT WING LOWER SKIN SURFACE IS GOUGED AT NR 1 PYLON SIDE LINK FITTING FWD I/B FASTENER HOLE AREA. REPAIRED DAMAGE PER ATS ER 12-02353 DATED 7-10-12. - [SDR NOCA06512](https://openairdocs.org/sdr/NOCA06512), Jun 16, 2012: SPAR. CRACKED. NR 1 PYLON UPPER SPAR FITTING I/B AFT FASTENER HOLE HAS CRACK INDICATION ON THE WEB LAYER. REMOVED AND REPLACED NR 1 PYLON UPPER SPAR WEB (P/N 311T1130-70) PER - [SDR NOCA07712](https://openairdocs.org/sdr/NOCA07712), Jun 15, 2012: DEPRESSOR. DAMAGED. NR 1 PYLON I/B MID T/R FIRE SEAL DERESSOR IS GOUGED & CHAFED. REPAIRED PER ATS ER 12-02288 DATED 7-13012 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA06412](https://openairdocs.org/sdr/NOCA06412), Jun 13, 2012: FLOOR SUPPORT. CORRODED. CORROSION ON BULK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT AROUND NUT PLATE HOLES BS 1461, LBL 12. FABRICATED SUPPORT & INSTALLED PER DRAWING 452T3264, REV B-1 - [SDR NOCA06912](https://openairdocs.org/sdr/NOCA06912), Jun 12, 2012: SKIN. CRACKED. SKIN CRACKED ON LEFT NACELLE STRUT CUTOUT FOR PANEL 432AL, UPPER AFT FASTENER. REPAIRED CRACK PER ATS ER 12-02257 DATED 7-11-12 & NAA EO 767-54-042. - [SDR NOCA08412](https://openairdocs.org/sdr/NOCA08412), Jun 12, 2012: SPAR. CRACKED. CRACK IN LEFT NACELLE STRUT FORWARD UPPER SPAR WEB O/B SIDE AT CUTOUT WEB NAC STA 231. REPAIRED CRACK PER ATS ER 12-02265 & SB 767-54-0090 REV 2. - [SDR NOCA08312](https://openairdocs.org/sdr/NOCA08312), Jun 12, 2012: FIRESEAL. WORN. NR 2 PYLON MID O/B T/R FIRE SEAL WORN. REPAIRED SEAL PER ATS ER 12=02288 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA08212](https://openairdocs.org/sdr/NOCA08212), Jun 12, 2012: FIRESEAL. CHAFED. CHAFING DAMAGE ON FORWARD I/B SECTION OF METAL FIRE SEAL, LEFT NACELLE STRUT. REPAIRED SEAL PER ATS ER 12=02288 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL D - [SDR NOCA08112](https://openairdocs.org/sdr/NOCA08112), Jun 12, 2012: FIRESEAL. WORN. NR 2 PYLON FORWARD O/B T/R FIRE SEAL WORN. REPAIRED SEAL PER ATS ER 12-02288 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA08012](https://openairdocs.org/sdr/NOCA08012), Jun 12, 2012: FIRESEAL. WORN. NR 2 PYLON FORWARD I/B T/R FIRE SEAL WORN. REPAIRED SEAL PER ATS ER 12-02288 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA07912](https://openairdocs.org/sdr/NOCA07912), Jun 12, 2012: FIRESEAL. WORN. NR 2 PYLON AFT I/B T/R FIRE SEAL WORN. REPAIRED SEAL PER ATS ER 12-02288 DATED 7-13-12 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA07812](https://openairdocs.org/sdr/NOCA07812), Jun 12, 2012: FIRESEAL. TORN. NR 2 PYLON AFT O/B T/R FIRE SEAL TORN. REPAIRED SEAL PER ATS ER 12-02288 DATED 7-13-12 & NAA EO 767-54-0043 REV INITIAL DATED 7-13-12. - [SDR NOCA201207100002](https://openairdocs.org/sdr/NOCA201207100002), Jun 12, 2012: HINGE. CRACKED. LEFT WING I/B MAIN FLAP CENTER AFT FLAP HINGE I/B FLANGE ON THE MAIN FLAP IS CRACKED. REPAIRED LEFT WING I/B MAIN FLAP HINGE I/B FLANGE IAW SRM 57-53-02. - [SDR NOCA06712](https://openairdocs.org/sdr/NOCA06712), Jun 12, 2012: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK AT BS 1480, LBL 57 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 1361 - BS 1482, LBL 54-57, WL 200 (P/N HFAB53-SEA-016) IAW DWG 146T52 - [SDR NOCA06312](https://openairdocs.org/sdr/NOCA06312), Jun 12, 2012: HINGE. CRACKED. RIGHT WING I/B MAIN FLAP CENTERAFT FLAP HINGE I/B FLANGE ON MAIN FLAP IS CRACKED. REPAIRED RIGHT WING I/B MAIN FLAP I/B HINGE I/B FLANGE IAW SRM 57-53-02. - [SDR NOCA07412](https://openairdocs.org/sdr/NOCA07412), Jun 10, 2012: SKIN. CORRODED. CORROSION ON SKIN AT L-4 DOOR CUTOUT THRESHOLD AREA. REMOVED CORROSION AND REPAIRED BLENDED AREA IAW EO 767-53-047 DATED JULY 7 2012. - [SDR NOCA07312](https://openairdocs.org/sdr/NOCA07312), Jun 10, 2012: SKIN. GOUGED. GOUGE ON FUSELAGE SKIN AT L-4 DOOR LWR AFT CORNER THRESHOLD AREA. REPAIRED SKIN IAW EO 767-53-048 DATED JULY 10, 2012. - [SDR NOCA201207110002](https://openairdocs.org/sdr/NOCA201207110002), Jun 10, 2012: ATTACH FITTING. CHAFED. RIGHT PYLON STRAP UPPER AFT ATTACH POINT FASTENER PLUG CHAFING THRU SKIN. FABRICATED AND INSTALLED FILLER AND SPLICE PER DWG 313T3310 REV G & SRM 54-52-70/201. - [SDR NOCA06012](https://openairdocs.org/sdr/NOCA06012), Jun 8, 2012: LATCH. DEFECTIVE. LEFT OVERWING ESCAPE SLIDE DOOR WILL NOT OPEN WHILE PERFORMING OPS CHECK. REMOVED AND REPLACED ALL (4 EA) LEFT OFFWING SLIDE COMPARTMENT DOOR LATCHES IAW MM 25- - [SDR NOCA2012007100001](https://openairdocs.org/sdr/NOCA2012007100001), Jun 7, 2012: SKIN SPLICE. CRACKED. LEFT WING LE INNER SPLICE IS CRACKED AT LES 504. REMOVED AND REPLACED LE INNER SPLICE PER SRM 51-40-05, 51-40-02 & 5124-13. - [SDR NOCA03812](https://openairdocs.org/sdr/NOCA03812), Apr 29, 2012: SENSOR. INOPERATIVE. ACFT HAD AN AIR-TURNBACK DUE TO RIGHT ENGINE N1 ERRATIC JUMPIMG BETWEEN 88.2 - 82.0 N2 JUMPING BETWEEN 94.3 - 94.9 STBY ENGINE INDICATOR MATCHED EICAS DISPLAY. - [SDR NOCA02712](https://openairdocs.org/sdr/NOCA02712), Mar 10, 2012: INDICATOR. INOPERATIVE. F/O'S AIRSPEED INDICATION FAILED DURING T/O ROLL. REPLACED THE F/O'S AIRSPEED INDICATOR PER AMM 34-12-02. OPS CHECK NORMAL. - [SDR NOCA2012022202412](https://openairdocs.org/sdr/NOCA2012022202412), Feb 22, 2012: BATTERY. INOPERATIVE. AFT GALLEY FLASHLIGHT INOPEATIVE, CENTER POSITION. REMOVED AND REPLACED FLASHLIGHT BATTERY AND OPS CHECKED NORMAL. - [SDR NOCA201202170001](https://openairdocs.org/sdr/NOCA201202170001), Feb 16, 2012: BATTERY. DISCHARGED. EMERGENCY FLASHLIGHT AT L3 DOOR NOT BLINKING. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY ASSY, AT 3L REF AMM 25-64-00, OPS CHECK NORMAL. - [SDR NOCA00912](https://openairdocs.org/sdr/NOCA00912), Jan 15, 2012: CONNECTOR. LOOSE. SEAT 2FG EMERGENCY LIGHT INOP. RESET CONNECTOR AS PER MM 33-51-05, OPS CHECK GOOD. - [SDR NOCA00712](https://openairdocs.org/sdr/NOCA00712), Jan 12, 2012: WIRE. BROKEN. SEAT ROWS 1F AND 31F EMERGENCY LIGHTS INOP. FOUND BROKEN WIRES AT FLOOR LEVEL SEAT BASE. RE-SPLICED WIRES PER SWPM 20-30-12, LIGHT OPERATION CHECKS OK. - [SDR NOCA11411](https://openairdocs.org/sdr/NOCA11411), Nov 16, 2011: FSEU. INOPERATIVE. L/E SLAT ASYM DISPLAY L/E LIGHT ILLUM WITH FLAP LEVER IN 25 BOTH POINTERS WERE CORRECT. REPLACED FSEU PER MM 27-81-02 TS PER FIM 27-81-00 SLAT SENSOR S285 FAULT - [SDR NOCA201110200511](https://openairdocs.org/sdr/NOCA201110200511), Oct 20, 2011: SEAT BELT. INOPERATIVE. PRIMARY OBSERVER'S SEAT INOPERATIVE DUE TO SEAT BELT SYSTEM INOPERATIVE. REMOVED AND REPLACED FIRST OBSERVER RESTRAINT SYSTEM REFERENCE AMM 25-11-04. OPS NORMAL - [SDR NOCA09811](https://openairdocs.org/sdr/NOCA09811), Sep 26, 2011: LAMP. INOPERATIVE. ESCAPE PATH LIGHTS INOP AT 8B AND 33F. RELAMPED EMERGENCY LIGHTS IAW AMM 33-51-11 . OPS CHECKED OK. - [SDR NOCA05711](https://openairdocs.org/sdr/NOCA05711), May 19, 2011: FLOORBEAM. CORRODED. TOP OF FLANGE ON FLOORBEAM FS 303 CORRODED AT LOCATION LBL 66. INSTALLED BEAM CAP PLATE AS PER SRM 53-00-51. - [SDR NOCA04411](https://openairdocs.org/sdr/NOCA04411), Apr 13, 2011: LIGHT. MISSING. FOUND ON DAILY CHECK EMERGENCY LIGHT ASSY AT 29G-F MISSING. REPLACED EMERGENCY LIGHT ASSY 29G-F PER MM 33-51-05. - [SDR NOCA04111](https://openairdocs.org/sdr/NOCA04111), Apr 8, 2011: UNKNOWN. NO INDICATION. AFTER TAKEOFF LOUD NOISE AT THE LT WINDOW EMERGENCY EXIT WITH VIBRATION IN THE FLOOR GOING ALL THE WAY BACK TO L4. R & R LT OVERWING DOOR SEAL PER MM 52-09-03. - [SDR NOCA03911](https://openairdocs.org/sdr/NOCA03911), Apr 6, 2011: ANGLE. CRACKED. A FRAME SUPPORT CRACKED NR 2 PYLON SAIL BOAT FAIRING FWD FRAME AFT SIDE. REMOVED DAMAGED PARTS DRILLED AND INSTALLED NEW ANGLE AS PER SRM 54-52-70. - [SDR NOCA03811](https://openairdocs.org/sdr/NOCA03811), Apr 6, 2011: ANGLE. CRACKED. A FRAME SUPPORT CRACKED SAIL-BOAT FAIRING FED INBD ANGLE AND LOWER AFT SIDE. REMOVED DAMAGED PARTS DRILLED AND INSTALLED NEW ANGLES PER SRM 54-52-70. - [SDR NOCA03711](https://openairdocs.org/sdr/NOCA03711), Apr 6, 2011: FLANGE. WORN. FLANGE WORN NR 1 ENGINE INBD SIDE OF PYLON ACCESS PLATE 416BR CUT OUT FLANGE 5 O'CLOCK POSITION WORN GOUGED. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT TO CHECK F All 134: https://openairdocs.org/aircraft/N767NA/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (13) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Kaman Aerospace K-1200) - [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc - [STC SR01767SE](https://openairdocs.org/stc/SR01767SE): Manufacture of Isolair Eliminator Model 4600-K1200 Fire Fighting System. Isolair Inc - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SR00103SE](https://openairdocs.org/stc/SR00103SE): Installation of Aviation Development Corporation oil filter. Aviation Development Corporation - [STC SR01561SE](https://openairdocs.org/stc/SR01561SE): Installation of the Model 36300 Auxiliary Hydraulic System. Kawak Aviation Technologies Inc - [STC SR01587SE](https://openairdocs.org/stc/SR01587SE): Installation of the Model 36400 Fire Tank System. Kawak Aviation Technologies Inc - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited - [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System. Atlantic Avionics Inc ### Approved for the engine (Honeywell T5317A-1) - [STC SE00585AT](https://openairdocs.org/stc/SE00585AT): Installation of Aeronautical Accessories, Inc. PC Safety Valve Kit. Bell Helicopter Textron Inc - [STC SE00029EN](https://openairdocs.org/stc/SE00029EN): Installation of Pratt & Whitney Engine Services Inc. SmartCycle Plus Engine Monitoring System, P/N EMU-K-010-1 on specific T53 engine models. Pratt & Whitney Engine Services Inc ## Related - Other Kaman Aerospace K-1200 aircraft: https://openairdocs.org/model/kaman-aerospace-k-1200/aircraft.md - The Honeywell T5317A-1 engine: https://openairdocs.org/engine/honeywell-t5317a-1.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.