# N16927: 1996 Embraer EMB-145EP, registration cancelled 2019-09-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 6, 2019 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Embraer EMB-145EP](https://openairdocs.org/model/embraer-emb-145ep) (registry code 3260221) - Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145.006 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: April 6, 2016 - Last registry action: August 10, 2016 - Mode S code: A115DB - Owner when cancelled: [Avi Sales & Leasing Services LLC](https://openairdocs.org/faa-owner/AVI%20SALES%20%26%20LEASING%20SERVICES%20LLC) - Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon) - Owner type: LLC - Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16927 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16927 - Page: https://openairdocs.org/deregistered/N16927-2019-09-06 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-145EP: https://openairdocs.org/model/embraer-emb-145ep.md ## Service difficulty reports (118, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR V0XD2014062192732](https://openairdocs.org/sdr/V0XD2014062192732), Jun 20, 2014: SEAL. DETERIORATED. AFT MAINTENANCE DOOR PANEL 312AR SEAL DETERIORATED. R & R WITH SERVICEABLE SEAL IAW AMM 52-44-02, - [SDR V0XD2014062192731](https://openairdocs.org/sdr/V0XD2014062192731), Jun 20, 2014: TUBE. DAMAGED. TUBE ASSY FORWARD OF RT PACK VALVE MISSING PART IF INSULATION. REPLACED DAMAGED TUBE ASSY WITH INSULATION WITH SERVICEABLE TUBE ASSY WITH INSULATION PN: 145-275 - [SDR V0XD2014062192730](https://openairdocs.org/sdr/V0XD2014062192730), Jun 20, 2014: GASKET. DAMAGED. RT UNDERWING FUEL PANEL 631CB HAS DAMAGED MESH GASKET. REPLACED MESH GASKET WITH SERVICEABLE GASKET PN:15-20060 IAW AMM28-11-01, WO 80232, WC 6018. - [SDR V0XD2014062192729](https://openairdocs.org/sdr/V0XD2014062192729), Jun 20, 2014: TANK. CRACKED. FUEL PROBE HAS CRACKED HOUSING. R & R TANK UNITS - [SDR V0XD2014062192733](https://openairdocs.org/sdr/V0XD2014062192733), Jun 19, 2014: ATTACH BRACKET. WORN. LOWER RT APU COWLING MOUNTING ATTACH POINT WILL NOT ACCEPT FASTENER. R & R APU COWLING MOUNTING, BRACKET, ATTACH POINTS IAW SRM 51-40-00. - [SDR V0XD2014062192728](https://openairdocs.org/sdr/V0XD2014062192728), Jun 19, 2014: PUSHROD. CORRODED. SPRING TAB PUSH ROD CORRODED. R & R PUSH ROD IAW AMM27-31-08. - [SDR V0XD2014061492727](https://openairdocs.org/sdr/V0XD2014061492727), Jun 12, 2014: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM AT FRAME 54 UNDERNEATH CENTER AISLE CROSSBEAM HAS A CORROSION HOLE. REPAIRED OMEGA BEAM IAW SRM 53-00-10. - [SDR V0XD2014061492726](https://openairdocs.org/sdr/V0XD2014061492726), Jun 12, 2014: FLOORBEAM. CRACKED. FLOORBEAM TEE CRACKED AT RT SIDE JUST AFT OF LAV. R & R FLOORBEAM TEE IAW SRM 51-40-02. - [SDR V0XD2014061492725](https://openairdocs.org/sdr/V0XD2014061492725), Jun 12, 2014: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT AT FRAME 24 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02. - [SDR V0XD2014061092724](https://openairdocs.org/sdr/V0XD2014061092724), Jun 6, 2014: FLOOR SUPPORT. CORRODED. LT OMEGA BEAM AT FRAME 20 UNDERNEATH CENTER AISLE CROSSBEAM HAS HEAVY CORROSION. REPAIRED OMEGA BEAM IAW SRM 53-00-10 & CPM 51-21-04. - [SDR V0XD2014061092723](https://openairdocs.org/sdr/V0XD2014061092723), Jun 6, 2014: FLOOR SUPPORT. CORRODED. RT FLOOR SUPPORT CORRODED OUT OF LIMIT AT FRAMES 35 TO 38. R & R FLOOR SUPPORT IAW SRM 51-40-02. - [SDR ASOA20140401055](https://openairdocs.org/sdr/ASOA20140401055), Apr 1, 2014: SIGN. INOPERATIVE. DURING 4A INSPECTION THE EMERGENCY EXIT SIGN AT SEAT 18A WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECT, - [SDR ASOA20140330052](https://openairdocs.org/sdr/ASOA20140330052), Mar 30, 2014: SKIN. CRACKED. DURING MAINTENANCE INSPECTION, THE TEE POST BETWEEN THE F/O'S WINDSHIELD AND DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A D - [SDR ASOA20130701095](https://openairdocs.org/sdr/ASOA20130701095), Jul 1, 2013: SIGN. INOPERATIVE. DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT (SIGN) WAS NOT ILLUMINATING. MX INSPECTED THE ACFT, R & R THE EMERGENCY EXIT SIGN AT R - [SDR ASOA20130518079](https://openairdocs.org/sdr/ASOA20130518079), May 18, 2013: SKIN. CRACKED. DURING 5A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED BELOW STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPA - [SDR ASOA20130518078](https://openairdocs.org/sdr/ASOA20130518078), May 18, 2013: SKIN. CRACKED. DURING 5A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED ABOVE STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER RE - [SDR ASOA20130327044](https://openairdocs.org/sdr/ASOA20130327044), Mar 27, 2013: LIGHT. UNKNOWN. DURING `A` CHECK INSPECTION, EMERGENCY LIGHT AT 12C WAS FOUND TO BE INOPERATIVE. MX PERFORMED OPS CHECKS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RE - [SDR ASOA20130327043](https://openairdocs.org/sdr/ASOA20130327043), Mar 27, 2013: LIGHT. INOPERATIVE. DURING `A` CHECK INSPECTION, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FO - [SDR ASOA20130211014H](https://openairdocs.org/sdr/ASOA20130211014H), Feb 11, 2013: LAMP. BURNED. THE CREW REPORTED THAT DURING LANDING, A BURNING ODOR AND LIGHT LAYER OF SMOKE WAS NOTED IN THE CABIN. THE SMOKE DISSIPATED AFTER LANDING, HOWEVER THE ODOR REMA - [SDR ASOA201212226001](https://openairdocs.org/sdr/ASOA201212226001), Dec 26, 2012: PRESSURE SWITCH. INOPERATIVE. THE CREW REPORTED BRAKE DEGRADE ON LANDING WITH VERY LITTLE BRAKE PRESSURE, ALSO HAD CMC MESSAGE BRAKE WHEEL SPEED TRANSDUCER 3 FAIL OCCURRED 3 TIMES. THE ACFT - [SDR ASOA20120921124](https://openairdocs.org/sdr/ASOA20120921124), Sep 21, 2012: INVERTER. INOPERATIVE. DURING MX INSPECTION THE AISLE PATH LIGHT AT ROWS 3 THRU 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH N - [SDR ASOA20120914121H](https://openairdocs.org/sdr/ASOA20120914121H), Sep 14, 2012: WIRE. BROKEN. DURING MX INSPECTION, THE AISLE PATH LIGHT STRIP AT ROW 10-11 WAS FOUND INOPERATIVE. MX INSPECTED THE ACFT AND REPAIRED THE WIRE ON THE LIGHT STRIP, OPERATIONAL - [SDR ASOA20120809107](https://openairdocs.org/sdr/ASOA20120809107), Aug 9, 2012: LIGHT. BROKEN. DURING MX INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO HAVE THE BULB OUT OF ITS SOCKET. MX R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE - [SDR ASOA20120406057](https://openairdocs.org/sdr/ASOA20120406057), Apr 6, 2012: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED - [SDR ASOA20120401052](https://openairdocs.org/sdr/ASOA20120401052), Apr 1, 2012: SOLENOID VALVE. INOPERATIVE. AFTER TAKEOFF, CREW REPORTED THAT AFTER RETRACTING THE LANDING GEAR, HEARD SEVERAL LOUD BANGS FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. ACFT RETURNED T - [SDR ASOA20120318039](https://openairdocs.org/sdr/ASOA20120318039), Mar 18, 2012: CONTROL LEVER. INOPERATIVE. THE CREW REPORTED THAT THE NLG DOOR OPENED IN FLIGHT. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE LANDING GEAR CONTROL LEVER, - [SDR ASOA20111214015](https://openairdocs.org/sdr/ASOA20111214015), Dec 14, 2011: RELAY. FAULTED. CREW REPORTED DURING CLIMB OUT AT 3000 FT, THERE WAS A TEMPORARY LOSS OF POWER ON NR 1 ENGINE, N1 APPROX 70 PERCENT. A FEW MINUTES LATER, A SECOND LOSS OF POWER - [SDR ASOA201112141001](https://openairdocs.org/sdr/ASOA201112141001), Dec 14, 2011: RELAY. FAULTED. THE CREW REPORTED THAT DURING CLIMB OUT AT 3000 FEET THERE WAS A TEMPORARY LOSS OF POWER ON ENG NR 1, N1 APPROX 70%. A FEW MINUTES LATER, A SECOND LOSS OF POWER - [SDR ASOA201111231005](https://openairdocs.org/sdr/ASOA201111231005), Nov 23, 2011: FADEC. FAILED. THE CREW REPORTED THAT AFTER ROTATION THE ACFT YAWED AND THE F/O CALLED POWER LOSS. THE POWER LEVERS WERE PUSHED FULL FORWARD AND THE N1 ON THE LT ENGINE WAS AR - [SDR C2XA11IA081](https://openairdocs.org/sdr/C2XA11IA081), May 3, 2011: ACM. SEIZED. XNA - FLIGHT 3099, THE CREW REPORTED A BURNING SMELL AND SMOKE FROM THE LEFT COCKPIT VENT AT THE WINDOW WITH A PACK 1 OVERHEAT MESSAGE. THE AIRCRAFT RETURNED TO - [SDR C2XA10IA341](https://openairdocs.org/sdr/C2XA10IA341), Dec 22, 2010: POWER SUPPLY. INOPERATIVE. IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED TH - [SDR C2XA10IA340](https://openairdocs.org/sdr/C2XA10IA340), Dec 22, 2010: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED TH - [SDR C2XA10IA323](https://openairdocs.org/sdr/C2XA10IA323), Dec 6, 2010: BALLAST. OVERHEATED. FLIGHT 2634, A PASSENGER AND F/A NOTICED AN ELECTRICAL BURNING ODOR IN MID CABIN DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE IN - [SDR C2XA10IA322](https://openairdocs.org/sdr/C2XA10IA322), Dec 6, 2010: BALLAST. OVERHEATED. DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR AT SEAT 6A. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT AT SEAT 6A ON MEL, - [SDR C2XA10IA317](https://openairdocs.org/sdr/C2XA10IA317), Nov 30, 2010: LIGHT. OVERHEATED. TUL - FLIGHT 2972, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A SMOKE SMELL AND FLICKERING CABIN LIGHTING. MAINTENANCE INSPECTED THE LIGHTING AND PLACED THE - [SDR C2XA10SH249](https://openairdocs.org/sdr/C2XA10SH249), Jul 25, 2010: BATTERY. OVERTEMP. LEFT BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA135](https://openairdocs.org/sdr/C2XA10IA135), Apr 26, 2010: SKIN PANEL. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BETWEEN THE CAPTAINS DV WINDOW AND WINDSHIELD. MAINTENANCE PERFORMED - [SDR C2XA10IA090](https://openairdocs.org/sdr/C2XA10IA090), Mar 7, 2010: UNKNOWN. ODOR. IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED - [SDR C2XA100IA088](https://openairdocs.org/sdr/C2XA100IA088), Mar 7, 2010: UNKNOWN. ODOR. IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED - [SDR C2XA09IA284](https://openairdocs.org/sdr/C2XA09IA284), Nov 6, 2009: LIGHT. INOPERATIVE. IAH - FLIGHT 3020, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE NUMBER FIVE AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA09SH280](https://openairdocs.org/sdr/C2XA09SH280), Aug 5, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM IAW EC 5320-01467. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH261](https://openairdocs.org/sdr/C2XA09SH261), Aug 3, 2009: BATTERY. DISCHARGED. SHV - DURING C-CHECK PROXIMITY LIGHT 3 AND 4 FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY IAW EMB-145 AMM 33-50-0 - [SDR C2XA09SH260](https://openairdocs.org/sdr/C2XA09SH260), Aug 3, 2009: HINGE. WORN. SHV - DURING C-CHECK MAIN DOOR LOWER HINGE LOCK PIN HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED MAIN DOOR LOWER HINGE IAW EMB-145 AMM 52-18-00. T - [SDR C2XA09SH259](https://openairdocs.org/sdr/C2XA09SH259), Aug 3, 2009: HINGE. WORN. SHV - DURING C-CHECK LT AILERON OUTBOARD HINGE POINT HAS MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE POINT IAW EMB-145 SRM 51-4 - [SDR C2XA09SH258](https://openairdocs.org/sdr/C2XA09SH258), Aug 3, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAME 17-24 IAW EMB-145 - [SDR C2XA09SH257](https://openairdocs.org/sdr/C2XA09SH257), Aug 3, 2009: SUPPORT BRACKET. CRACKED. SHV - DURING C-CHECK FRAME 10 SUPPORT BRACKET CRACKED JUST UNDER LEFT DV WINDOW LOWER CUTOUT FRAME. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAME 10 - [SDR C2XA09SH256](https://openairdocs.org/sdr/C2XA09SH256), Aug 3, 2009: CHANNEL. CRACKED. SHV - DURING C-CHECK FRAME 10 CRACKED AT STRINGER 13L. MAINTENANCE REMOVED AND REPLACED CHANNEL AT FRAME 10 STRINGER 13L IAW EMB-145 SRM 51-40-02 AND CPM 51-21- - [SDR C2XA09SH255](https://openairdocs.org/sdr/C2XA09SH255), Aug 3, 2009: DOUBLER. CORRODED. SHV - DURING C-CHECK RT DOUBLER AT FRAME 61 CORRODED (LEVEL 2 LOCAL) AT RIVET HOLES (BEHIND CARBON CROSS BEAM). MAINTENANCE REMOVED AND REPLACED RT DOUBLER AT F - [SDR C2XA09SH254](https://openairdocs.org/sdr/C2XA09SH254), Aug 3, 2009: BUTTSTRAP. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) FRAME 46-53. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM BUTTSTRAP FRAME 46-53 IAW - [SDR C2XA09SH253](https://openairdocs.org/sdr/C2XA09SH253), Aug 3, 2009: FITTING. CRACKED. SHV - DURING C-CHECK LEFT O/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT O/B LEADING EDGE SPLICE SHEAR CLIP IAW EMB-145 SRM 5 All 118: https://openairdocs.org/deregistered/N16927-2019-09-06/reports.md ## Other aircraft with N16927 - [Cancelled 1942-10-05](https://openairdocs.org/deregistered/N16927-1942-10-05): Sikorsky S-43, S/N 4316. Owner: [Pan American Airways Inc](https://openairdocs.org/faa-owner/PAN%20AMERICAN%20AIRWAYS%20INC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) --- 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.