# N459MC: Morsecorp TREK - Status: Valid registration - Airframe: [Morsecorp TREK](https://openairdocs.org/model/morsecorp-trek) (registry code 06102J4) - Serial number: TRK02 - Type: Powered parachute - Engine type: Reciprocating - Certificate issued: September 2, 2026 - Expires: September 30, 2033 - Mode S code: A594A1 - Registered owner: [Morsecorp Inc](https://openairdocs.org/faa-owner/MORSECORP%20INC) - Location: [Cambridge, MA](https://openairdocs.org/faa-place/MA/Cambridge) - Owner type: Corporation - Owner's area on the map: 42.3625° N, 71.0810° W: Placed by OpenAirDocs at the center of ZIP code 02142, 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=459MC - Page: https://openairdocs.org/aircraft/N459MC 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 (Morsecorp TREK) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N459MC. ## FAA accident and incident reports None matched to N459MC. ## 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 N459MC not matched to an aircraft (25) They name N459MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR UIEA2013112500570](https://openairdocs.org/sdr/UIEA2013112500570), Nov 25, 2013: SHUTOFF VALVE. INOPERATIVE. EICAS MESSAGE BLEED 4, NACELLE ANTI-ICE INOPERATIVE. REPLACED NR 4 HPSOV, OPS CHECKS NORMAL. - [SDR UIEA2013100700511](https://openairdocs.org/sdr/UIEA2013100700511), Oct 7, 2013: BATTERY PACK. INOPERATIVE. EMERGENCY BATTERY PACK, AT BS 717 INOPERATIVE. R & R BATTERY. OPS CHECKED GOOD IAW AMM 33-51-04-902-001-001. - [SDR UIEA2012101300470](https://openairdocs.org/sdr/UIEA2012101300470), Oct 13, 2012: SMOKE DETECTOR. MALFUNCTIONED. 16X STATUS MESSAGES; ALL MAIN DECK SMOKE DETECTORS. MESSAGES CLEARED FROM CMC IAW WD 26-16-02-103. OPS CHECKED OK. - [SDR UIEA2012091200413](https://openairdocs.org/sdr/UIEA2012091200413), Sep 12, 2012: SKIN. DAMAGED. DAMAGE ON THE OUTER SKIN LOCATED 1 FOOT FROM THE FWD EDGE APPROX 10 O'CLOCK POSITION ARE .2500" BY .6250" AND 1.5". IN ADDITION, THE LT THRUST REVERSER OUTER SK - [SDR UIEA2012091200414](https://openairdocs.org/sdr/UIEA2012091200414), Sep 12, 2012: THRUST REVERSER. MISSING. NR 1 ENGINE LT THRUST REVERSER IS MISSING APPROXIMATELY 2 FT OF THE FORWARD WEAR STRIP ON THE FORWARD OTBD FRAME. DISPOSITION IS TO PERFORM A TIME LIMITED REPAI - [SDR UIEA2012071900325](https://openairdocs.org/sdr/UIEA2012071900325), Jul 16, 2012: LAMP. INOPERATIVE. UPPER DECK CEILING, BS 644 HAS EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED GOOD IAW MM 33-51-00. - [SDR UIEA2012052100247](https://openairdocs.org/sdr/UIEA2012052100247), May 21, 2012: SKIN. DAMAGED. CARGO DOOR SKIN FORWARD LOWER CORNER DAMAGED. REPAIRED IAW SRM 52-30-01, FIG 201, REPAIR 2. - [SDR UIEA2012012000020](https://openairdocs.org/sdr/UIEA2012012000020), Jan 14, 2012: FRAME. DENTED. DURING A D2/C1/A3 INSPECTION, DETECTED A MAJOR DENT ON THE FUSELAGE FRAME AT BS 1840, S-11R; CUT OUT THE DAMAGED PORTION OF THE FRAME, PERFORMED HFEC INSPECTION - [SDR UIEA2012011900015](https://openairdocs.org/sdr/UIEA2012011900015), Jan 9, 2012: PANEL. BROKEN. PANEL OF FWD CARGO BAY BROKEN AT STA 970, LBL 42. REPAIR IAW EI NR T2012A53B-099, REV 00. AND REV 01. - [SDR UIEA2012011900014](https://openairdocs.org/sdr/UIEA2012011900014), Jan 9, 2012: RIB. CRACKED. FOUND CRACK ON RIB AND CLIP OF THE LT HST L/E AT L/E STA 145. REPAIRED IAW EI NR T2012A55B-091, REV 00. - [SDR UIEA2012011900016](https://openairdocs.org/sdr/UIEA2012011900016), Jan 8, 2012: SKIN. DENTED. DENT ON THE LT WING INBD L/E NOSE CAP SKIN AT ILES 277. REPAIRED IAW EI NR T2012A57B-047 REV 00 AND REV 01. - [SDR UIEA2012011900017](https://openairdocs.org/sdr/UIEA2012011900017), Jan 6, 2012: RIB. CRACKED. CRACK ON THE RIB AND CLIP OF LT HST L/E AT STA 138. REPAIR IAW EI NR T2012A55B-091, REV 00. - [SDR UIEA2012011900013](https://openairdocs.org/sdr/UIEA2012011900013), Jan 6, 2012: RIB. CRACKED. CRACK ON THE RIB AND UPPER CLIP OF THE LT HORIZONTAL STABILIZER, NOSE L/E FAIRING INTERNAL STRUCTURE L/E STA 131. REPAIRED IAW EI NO T2012A55B-091, REV 00. - [SDR UIEA2012011900018](https://openairdocs.org/sdr/UIEA2012011900018), Jan 2, 2012: CYLINDER. DISCHARGED. PERFORMED J/C 250230101 UPPER DECK DOOR SLIDE DEPLOY. FOUND LT UPPER DECK ENTRY DOOR WASN'T LIFT. UNABLE TO DEPLOY SLIDE. REPLACE UPPER DECK LT EMERGENCY POWER - [SDR UIEA2012011900019](https://openairdocs.org/sdr/UIEA2012011900019), Jan 1, 2012: FRAME. DAMAGED. DISTORTED ON THE FRAME OF MAIN DECK CARGO COMP AT STA 1840 S11R. REPAIR IAW EO NR T2012A53B-087 REV 00. AND REV 01. - [SDR UIEA2011122300727](https://openairdocs.org/sdr/UIEA2011122300727), Dec 21, 2011: SKIN. DENTED. DURING WALKAROUND INSPECTION, MX REPORTED DAMAGE FOUND TO LT WING L/E INBD OF LANDING LIGHT DENT/DAMAGE, MEASURING 4.0" X 4.5" AND IS 0.250" DEEP (REF FIG 1). D - [SDR UIEA2011110400634](https://openairdocs.org/sdr/UIEA2011110400634), Nov 4, 2011: PDU. INOPERATIVE. FLAP DRIVE EICAS MESSAGE DISPLAYED. LT OTBD L/E DID NOT RETRACT AFTER TAKEOFF. R & R THE LT OTBD L/E FLAP PDU IAW MM 27-81-03 AND OPERATES NORMAL IAW MM. - [SDR UIEA2011102400626](https://openairdocs.org/sdr/UIEA2011102400626), Oct 22, 2011: DOOR. MALFUNCTIONED. RT UPPER DECK DOOR ASSIST BOTTLE DISCHARGED UNCOMMANDED WITH DOOR IN MANUAL MODE. - [SDR UIEA2011100400562](https://openairdocs.org/sdr/UIEA2011100400562), Oct 4, 2011: FLOORBOARD. DAMAGED. DURING WALKAROUND INSPECTION, DAMAGE FOUND TO MAIN DECK FLOORBOARD PANEL BS 2020 - LBL7.0. THE DAMAGED AREA MEASURES APPROX 3" X 3". DAMAGE IS BEYOND THE SRM 53 - [SDR UIEA2011092900529](https://openairdocs.org/sdr/UIEA2011092900529), Sep 25, 2011: THRUST REVERSER. DAMAGED. DURING WALKAROUND, MX FOUND THE NR 2 RT THRUST REVERSER INSULATION DAMAGED. DAMAGE IS SUSPECTED TO BE DUE TO DAMAGE FROM THE IDG AIR/OIL COOLER PARTIAL VANE LIB - [SDR UIEA2011062300324](https://openairdocs.org/sdr/UIEA2011062300324), Jun 23, 2011: STRUCTURE. DAMAGED. DURING MX WALKAROUND, FOUND LIGHTNING STRIKE DAMAGE TO THE RT THRUST REVERSER TRANSLATING COWL . THE DAMAGE IS 1.0 IN. DIAMETER. PERFORMED A TIME LIMITED REPAIR - [SDR UIEA2011061700323](https://openairdocs.org/sdr/UIEA2011061700323), Jun 17, 2011: DEPRESSOR. DAMAGED. DURING WALK-AROUND INSPECTION, DAMAGE TO THE LOWER LOBE - FWD CARGO DOOR - BS670 SEAL DEPRESSOR FOUND (REF. FIGURE 1), MEASURING 1 INCH WIDE FROM THE EDGE AND 5 - [SDR UIEA2011052200266](https://openairdocs.org/sdr/UIEA2011052200266), May 22, 2011: FAIRING. DAMAGED. DURING LOADING OPERATIONS; A CARGO DOLLY STRUCK ACFT CAUSING DAMAGE TO WING TO BODY FAIRINGS FROM BS800 TO BS1000. UPON INSPECTION OF THE DAMAGED AREAS FOUND 3 - [SDR UIEA2011042800254](https://openairdocs.org/sdr/UIEA2011042800254), Apr 28, 2011: HEAT SHIELD. DAMAGED. DURING INSP, THE NR 4 ENGINE INB CORE COWL HEATSHIELD WAS FOUND DAMAGED. REF TO FIG 1 & AMP; 2 FOR DETAILS. A REPAIR SRM 54-45-01, REPAIR 3 WILL BE PERFORMED BU - [SDR UIEA2011041100257](https://openairdocs.org/sdr/UIEA2011041100257), Apr 11, 2011: SLIDE. FAILED. U/DECK FLOOR MOUNTED ESCAPE SLIDE BURST DURING CABIN DOOR EVACUATION SLIDE DEPLOYMENT FUNCTIONAL TEST. (ZONE: 222, RT SIDE) IAW MJC 52-023-01-02. PN 7A1323-114, ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Morsecorp TREK aircraft: https://openairdocs.org/model/morsecorp-trek/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.