# N15932: 1997 Embraer EMB-145EP, registration cancelled 2022-12-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 31, 2022 - 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: 145.015 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: September 12, 2019 - Last registry action: September 12, 2019 - Mode S code: A0EE7A - Owner when cancelled: [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC) - Location: [Austin, TX](https://openairdocs.org/faa-place/TX/Austin) - Owner type: LLC - Owner's area on the map: 30.2706° N, 97.7426° W: Placed by OpenAirDocs at the center of ZIP code 78701, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N15932 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15932 - Page: https://openairdocs.org/deregistered/N15932-2022-12-31 From the FAA registry file of November 4, 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 (116, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20131218294V](https://openairdocs.org/sdr/ASOA20131218294V), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING NR 4 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510 - [SDR ASOA20131218293](https://openairdocs.org/sdr/ASOA20131218293), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING, NR 3 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC551 - [SDR ASOA20131218292](https://openairdocs.org/sdr/ASOA20131218292), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK, THE HORIZONTAL STAB HINGE PIN FITTING NR 2 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC551 - [SDR ASOA20131218291V](https://openairdocs.org/sdr/ASOA20131218291V), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK, HORIZONTAL STAB HINGE PIN FITTING NR 1 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01 - [SDR ASOA20131218290](https://openairdocs.org/sdr/ASOA20131218290), Dec 18, 2013: SKIN. CRACKED. DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-80 AND STRINGERS 3-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND - [SDR ASOA20131218289](https://openairdocs.org/sdr/ASOA20131218289), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK, THE RUDDER II UPPER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM - [SDR ASOA20131218288](https://openairdocs.org/sdr/ASOA20131218288), Dec 18, 2013: HINGE FITTING. WORN. DURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW EC57 - [SDR ASOA20131218287](https://openairdocs.org/sdr/ASOA20131218287), Dec 18, 2013: FRAME. CRACKED. DURING C-CHECK, LEFT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. R & R FRAME SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE - [SDR ASOA20131218286](https://openairdocs.org/sdr/ASOA20131218286), Dec 18, 2013: STRINGER. CRACKED. DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 14. R & R STRINGER SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218285](https://openairdocs.org/sdr/ASOA20131218285), Dec 18, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK, RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN - [SDR ASOA20131218284](https://openairdocs.org/sdr/ASOA20131218284), Dec 18, 2013: SUPPORT. CORRODED. DURING C-CHECK, LAVATORY WASTE DRAIN SUPPORT ASSY WAS FOUND TO BE CORRODED. R & R SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131218283](https://openairdocs.org/sdr/ASOA20131218283), Dec 18, 2013: SILL. CORRODED. DURING C-CHECK, SERVICE DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-02. ACFT - [SDR ASOA20130627094](https://openairdocs.org/sdr/ASOA20130627094), Jun 27, 2013: SKIN. CRACKED. DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 77 BETWEEN STR 3L & 4L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER R - [SDR ASOA20130627093](https://openairdocs.org/sdr/ASOA20130627093), Jun 27, 2013: SKIN. CRACKED. DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 78 BETWEEN STR 5L & 6L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER R - [SDR ASOA20130627092](https://openairdocs.org/sdr/ASOA20130627092), Jun 27, 2013: SKIN. CRACKED. DURING 5A INSPECTION, A CRACK INDICATION WAS FOUND AROUND A RIVET AT FR 79 BETWEEN STR 5L & 6L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A DOUBLER R - [SDR ASOA20130627091](https://openairdocs.org/sdr/ASOA20130627091), Jun 27, 2013: SKIN. CRACKED. DURING 5A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR75 ABOVE STR02L. MX REMOVED THE DAMAGED PORTION OF SKIN AND PERFORMED A T - [SDR ASOA20130606083](https://openairdocs.org/sdr/ASOA20130606083), Jun 7, 2013: FIREWALL. CRACKED. DURING APU CHANGE THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER LT MOUNTING POINT. MX PERFORMED AN SRM DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RET - [SDR C2XA10SH226](https://openairdocs.org/sdr/C2XA10SH226), Jul 7, 2010: BATTERY. OVERTEMP. DFW - BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA247](https://openairdocs.org/sdr/C2XA09IA247), Oct 1, 2009: ENGINE. LEAKING. IAH - DURING MAINTENANCE INSPECTION AN OIL SMELL WAS REPORTED IN THE CABIN WITH THE NR 2 ENGINE BLEED AND PACS ON FULL HOT. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA09IA246](https://openairdocs.org/sdr/C2XA09IA246), Sep 29, 2009: ACM. SEIZED. IAH - FLIGHT 2619, THE CREW REPORTED A BURNING RUBBER SMELL FROM THE PACKS IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND - [SDR C2XA09TY218](https://openairdocs.org/sdr/C2XA09TY218), Aug 14, 2009: INVERTER. INOPERATIVE. TYS - A/C IN FOR AN A-CHECK WHEN INSPECTION FOUND THE MAIN PAX DOOR EXIT SIGN EMERGENCY LIGHT TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER AND - [SDR C2XA09IA132](https://openairdocs.org/sdr/C2XA09IA132), May 20, 2009: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT STRIP BETWEEN ROWS 8 & 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGH - [SDR C2XA09IA130](https://openairdocs.org/sdr/C2XA09IA130), May 16, 2009: LANDING GEAR. LOW. FLIGHT 2468, AFTER TAKEOFF THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED - [SDR C2XA09IA128](https://openairdocs.org/sdr/C2XA09IA128), May 15, 2009: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 2934, DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED - [SDR C2XA09CL044](https://openairdocs.org/sdr/C2XA09CL044), Apr 20, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO - [SDR C2XA09TY038](https://openairdocs.org/sdr/C2XA09TY038), Mar 1, 2009: INLET. CORRODED. AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND EIGHT BOLT HOLES ON THE NUMBER ONE ENGINE INTAKE INLET THAT WERE CORRODED. MAINTENANCE REPAIRED THE COR - [SDR C2XA09TY034](https://openairdocs.org/sdr/C2XA09TY034), Feb 24, 2009: INLET. CORRODED. DURING A C-CHECK INSPECTION EIGHT BOLT HOLES WERE FOUND SHOWING CORROSION ON THE NR 1 ENGINE INTAKE MOUNT FLANGE. THE HOLES WERE CLEANED AND REAMED TO REMOVE AL - [SDR C2XA09TY031](https://openairdocs.org/sdr/C2XA09TY031), Feb 17, 2009: FRAME. DAMAGED. FRAME 31 HAS MAINTENANCE INDUCED DAMAGE STR 15R AND 16R. CUT OUT DAMAGE AREA ON FRAME 31 & FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-00-04. AIRCRAFT STILL - [SDR C2XA09IA017](https://openairdocs.org/sdr/C2XA09IA017), Jan 11, 2009: BALLAST. BURNED. DURING POST FLIGHT INSP, CREW REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT AND F/A JUMPSEAT AREA WITH NO VISIBLE SMOKE. MX INSPECTED THE ACFT, AND - [SDR C2X2008F00044](https://openairdocs.org/sdr/C2X2008F00044), Sep 6, 2008: ELECTRONIC UNIT. INOPERATIVE. THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR E - [SDR C2XA07IA248](https://openairdocs.org/sdr/C2XA07IA248), Dec 16, 2007: SKIN. CRACKED. IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A CRACK IN THE UPPER RT WING SKIN. THE CRACK WAS INSPECTED AND PLACED ON A 500 FLIGHT CYCLE DEFERRAL IN ACC - [SDR C2XA07SH029](https://openairdocs.org/sdr/C2XA07SH029), May 13, 2007: SMOKE DETECTOR. INOPERATIVE. SHV - DURING ROUTINE MAINTENANCE THE BAGGAGE COMPARTMENT SMOKE DETECTOR FAILED THE OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR IAW EMB 145 A - [SDR C2XA06SH135](https://openairdocs.org/sdr/C2XA06SH135), Dec 9, 2006: FLOORBEAM. CRACKED. SHV - MAJOR - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CRACKED AT FR 22 AND CORRODED BETWEEN FRAMES 19A-22. MAINTENANCE REMOVED THE DAMAGED AREAS AND - [SDR C2XA06SH134](https://openairdocs.org/sdr/C2XA06SH134), Dec 8, 2006: FIREWALL. CHAFED. SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR IA - [SDR C2XA05BT027](https://openairdocs.org/sdr/C2XA05BT027), May 9, 2005: ODOR. DETECTED. CREW REPORTED, BURNING ODOR COMING FROM RELAY BOX UNDER GEAR PINS. MAINTENANCE PERFORMED VISUAL INSPECTION OF LEFT HAND POWER DISTRIBUTION PANEL, NO ARCING OR B - [SDR C2XA05CL028](https://openairdocs.org/sdr/C2XA05CL028), Apr 25, 2005: ODOR. DETECTED. PIT FLT 2864, THE CREW REPORTED AN ELECTRICAL BURNING ODOR. CLEVELAND SENT A MAINTENANCE CREW TO INSPECT AND TROUBLESHOOT THE ODOR, THE MAINTENANCE CREW FOUND A - [SDR C2XA04SH570](https://openairdocs.org/sdr/C2XA04SH570), Dec 6, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH569](https://openairdocs.org/sdr/C2XA04SH569), Dec 3, 2004: FLOOR SUPPORT. CORRODED. DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED AT FRAME 29. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01177. - [SDR C2XA04SH568](https://openairdocs.org/sdr/C2XA04SH568), Dec 3, 2004: FLOOR SUPPORT. CORRODED. DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5320-01177. AIRCRAFT R - [SDR C2XA04SH563](https://openairdocs.org/sdr/C2XA04SH563), Dec 2, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVIC - [SDR C2XA04SH566](https://openairdocs.org/sdr/C2XA04SH566), Nov 20, 2004: FLOOR SUPPORT. CORRODED. DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EC5320-0117. AIRCRA - [SDR C2XA04SH556](https://openairdocs.org/sdr/C2XA04SH556), Nov 18, 2004: BEAM. CORRODED. DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE - [SDR C2XA04SH555](https://openairdocs.org/sdr/C2XA04SH555), Nov 17, 2004: FRAME. CRACKED. DURING C-CHECK EDDY CURRENT INSPECTION OF THE PASSENGER DOOR STOP ATTACHMENT AT STRING 14L HAD A CRACK INDICATION. REAMED HOLE TO OVERSIZED CONDITION INSTALLED - [SDR C2XA04SH554](https://openairdocs.org/sdr/C2XA04SH554), Nov 17, 2004: BEARING CAP. SCRATCHED. DURING C-CHECK, THE LEFT MAIN GEAR BEARING CAP WAS FOUND SCRATCHED IN THE BEARING TRACK. REPLACED THE AFFECTED CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE - [SDR C2XA04BT086](https://openairdocs.org/sdr/C2XA04BT086), Aug 8, 2004: LIGHT. MALFUNCTIONED. ATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00. - [SDR C2XA04TY054](https://openairdocs.org/sdr/C2XA04TY054), Mar 20, 2004: LENS. CRACKED. TYS A/C 932 WAS IN FOR A SERVICE CHECK AND MAINTENANCE FOUND THE LEFT CABIN WALL EXIT LIGHT DAMAGE. MAINTENANCE REMOVED AND REPLACED THE EXIT WALL LENS IAW 145 - [SDR C2XA03BT102](https://openairdocs.org/sdr/C2XA03BT102), Oct 24, 2003: LIGHT. INOPERATIVE. CREW REPORTED, EMERGENCY AISLE PATH FLOOR LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY AISLE PATH FLOOR LIGHT STRIP IAW EMB145 MM 3 - [SDR C2XA03CL178](https://openairdocs.org/sdr/C2XA03CL178), Oct 23, 2003: INVERTER. FAILED. DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGNS IN AISLE OVER EXIT DOORS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL - [SDR C2XA03CL177](https://openairdocs.org/sdr/C2XA03CL177), Oct 23, 2003: LIGHT. INOPERATIVE. CLE FLIGHT 2163 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. - [SDR C2XA03CL175](https://openairdocs.org/sdr/C2XA03CL175), Oct 22, 2003: CONNECTOR. DIRTY. CLE FLIGHT 2163 THE CREW REPORTED THE EXIT SIGN OVER ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR FOR THE EXIT SIGN. OPERATIONAL CHEC All 116: https://openairdocs.org/deregistered/N15932-2022-12-31/reports.md ## Other aircraft with N15932 - [Cancelled 1973-02-23](https://openairdocs.org/deregistered/N15932-1973-02-23): Piper PA-34-200, S/N 34-7350110. Exported to Germany. Owner: [Moody Walter P](https://openairdocs.org/faa-owner/MOODY%20WALTER%20P), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) --- 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.