# N15948: 1998 Embraer EMB-145EP, registration cancelled 2016-07-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 11, 2016
- Exported to: Senegal
- Status when cancelled: Valid registration
- 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: 145056
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: July 6, 2016
- Last registry action: July 6, 2016
- Mode S code: A0EEA3
- Owner when cancelled: [Msn145056 LLC](https://openairdocs.org/faa-owner/MSN145056%20LLC)
- Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon)
- Owner type: Corporation
- 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/N15948
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15948
- Page: https://openairdocs.org/deregistered/N15948-2016-07-11

From the FAA registry file of October 29, 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 (97, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA20131026191](https://openairdocs.org/sdr/ASOA20131026191), Oct 26, 2013: DUCT. CRACKED. CREW REPORTED PACK 1 AND 2 FAILED IN FLIGHT AND A BAD ODOR AFTER SELECTING. RESET PACK 2 CREW CONTINUED TO DESTINATION WITH PACKS DEACTIVATED AND LANDED WITHOUT
- [SDR ASOA20130915168](https://openairdocs.org/sdr/ASOA20130915168), Sep 15, 2013: LIGHT. INOPERATIVE. DURING TESTING, NR 3 EMERGENCY LIGHT FAILED TO ILLUMINATE. MX REPLACED THE LIGHT STRIP, OPS TESTED THE SYS AND CLEARED THE DISCREPANCY.
- [SDR ASOA20130421138](https://openairdocs.org/sdr/ASOA20130421138), Apr 20, 2013: SKIN. CORRODED. DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 20R-20L. MX R & R THE SKIN IAW EC5320-01787. THE ACFT WAS APPROVED
- [SDR ASOA20130421137](https://openairdocs.org/sdr/ASOA20130421137), Apr 20, 2013: STRINGER. CORRODED. DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130421136](https://openairdocs.org/sdr/ASOA20130421136), Apr 20, 2013: STRINGER. CORRODED. DURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20130421135V](https://openairdocs.org/sdr/ASOA20130421135V), Apr 20, 2013: SILL. CORRODED. DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130210012](https://openairdocs.org/sdr/ASOA20130210012), Feb 10, 2013: SKIN. CRACKED. DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2R. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION 
- [SDR ASOA20130210011](https://openairdocs.org/sdr/ASOA20130210011), Feb 10, 2013: SKIN. CRACKED. DURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION O
- [SDR ASOA20120405051](https://openairdocs.org/sdr/ASOA20120405051), Apr 6, 2012: CONNECTOR. BROKEN. DURING MX INSPECTION, LT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE 
- [SDR ASOA20120405050](https://openairdocs.org/sdr/ASOA20120405050), Apr 5, 2012: CONNECTOR. DISCONNECTED. DURING MX INSPECTION, THE RT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. RESECURRED THE EXIT SIGN INVERTER ELECTRICAL CONNECTOR, OPS TESTED WITH 
- [SDR C2XA11IA138](https://openairdocs.org/sdr/C2XA11IA138), Jul 2, 2011: DIMMER. DEFECTIVE. IAH - FLIGHT 2060, DURING TAXI THE CREW REPORTED A RELAY CLICKING ON THE CAPTAINS SIDE WITH LOTS OF FUMES. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE R
- [SDR C2XA11IA074](https://openairdocs.org/sdr/C2XA11IA074), Apr 21, 2011: BLADE. BROKEN. FLIGHT 2031, CREW REPORTED NR 2 ENG LP VIBRATIONS EXCEEDED LIMITS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT
- [SDR C2XA11IA055](https://openairdocs.org/sdr/C2XA11IA055), Mar 17, 2011: CONTROL HANDLE. INOPERATIVE. IAH - FLIGHT 2544, THE CREW REPORTED THAT THE GEAR WAS SLOW TO RETRACT ON DEPARTURE FROM DAL WITH THE ASSOCIATED WARNINGS. THE AIRCRAFT CONTINUED TO IAH WHERE I
- [SDR C2XA10IA339](https://openairdocs.org/sdr/C2XA10IA339), Dec 17, 2010: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT LIGHT AT THE WING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR
- [SDR C2XA10IA284](https://openairdocs.org/sdr/C2XA10IA284), Nov 4, 2010: WARNING SYSTEM. MALFUNCTIONED. IAH - 500 FEET ABOVE THE GROUND THE CREW REPORTED A LANDING GEAR AIR/ GRND FAIL MESSAAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE
- [SDR C2XA10IA279](https://openairdocs.org/sdr/C2XA10IA279), Oct 30, 2010: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2876, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS 
- [SDR C2XA10SH362](https://openairdocs.org/sdr/C2XA10SH362), Oct 25, 2010: SKIN. CRACKED. SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET HEAD FR 78 RT SIDE. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN FR 78 RT SIDE IAW EC5330-02260. THE AIRCRAFT
- [SDR C2XA10SH361](https://openairdocs.org/sdr/C2XA10SH361), Oct 25, 2010: SKIN. CRACKED. SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET AT RT SIDE FR 77. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN RT SIDE FR 77 IAW EC5330-02260. THE AIRCRAFT W
- [SDR C2XA10SH360](https://openairdocs.org/sdr/C2XA10SH360), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 29) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM L-FL
- [SDR C2XA10SH359](https://openairdocs.org/sdr/C2XA10SH359), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 29) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER BEAM CROSSB
- [SDR C2XA10SH358](https://openairdocs.org/sdr/C2XA10SH358), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 33) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM 
- [SDR C2XA10SH357](https://openairdocs.org/sdr/C2XA10SH357), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 33) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FR 33
- [SDR C2XA10SH356](https://openairdocs.org/sdr/C2XA10SH356), Oct 25, 2010: YOKE. CRACKED. SHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIR
- [SDR C2XA10SH355](https://openairdocs.org/sdr/C2XA10SH355), Oct 25, 2010: DOOR FRAME. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR STRUCTURE CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER STRUCTU
- [SDR C2XA10SH354](https://openairdocs.org/sdr/C2XA10SH354), Oct 25, 2010: BRACKET. WORN. SHV - DURING C-CHECK RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) MISSING. MAINTENANCE REMOVED AND REPLACED RT AILERON C
- [SDR C2XA10SH353](https://openairdocs.org/sdr/C2XA10SH353), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FL
- [SDR C2XA10SH352](https://openairdocs.org/sdr/C2XA10SH352), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 58 CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANG
- [SDR C2XA10SH351](https://openairdocs.org/sdr/C2XA10SH351), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 44 HAS CORROSION (LEVEL 2 LOCAL) TO CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L
- [SDR C2XA10SH350](https://openairdocs.org/sdr/C2XA10SH350), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 44 TO CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT F
- [SDR C2XA10SH349](https://openairdocs.org/sdr/C2XA10SH349), Oct 25, 2010: BEAM. CORRODED. SHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLA
- [SDR C2XA10SH348](https://openairdocs.org/sdr/C2XA10SH348), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEA
- [SDR C2XA10SH347](https://openairdocs.org/sdr/C2XA10SH347), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 38) CTR OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CTR OMEGA BEAM L-F
- [SDR C2XA10SH346](https://openairdocs.org/sdr/C2XA10SH346), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 FLANGE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 19-20 IAW EMB-145 SR
- [SDR C2XA10SH345](https://openairdocs.org/sdr/C2XA10SH345), Oct 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK (FR 38) LT OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLA
- [SDR C2XA10IA275](https://openairdocs.org/sdr/C2XA10IA275), Oct 24, 2010: PROXIMITY SENSOR. DIRTY. IAH - FLIGHT 2541, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND THE THRUST REVERSERS WOULD NOT DEPLOY ON LANDING. THE AIRCRAFT LANDED AT IAH WIT
- [SDR C2XA10IA255](https://openairdocs.org/sdr/C2XA10IA255), Sep 15, 2010: SKIN. DAMAGED. IAH - FLIGHT 2149, DURING POST FLIGHT INSPECTION THE CREW REPORTED A HOLE IN THE RIGHT LOWER SIDE OF RUDDER II. MAINTENANCE REPLACED THE DAMAGED SECTION OF SKIN
- [SDR C2XA10IA207](https://openairdocs.org/sdr/C2XA10IA207), Jul 25, 2010: MODULE. INOPERATIVE. IAH - FLIGHT 2547, DURING CLIMB THE CREW REPORTED THAT THE AUTO PRESSURIZATION WAS NOT WORKING AND THAT THE EICAS INDICATIONS WERE INTERMITTENT. THE AIRCRAFT RE
- [SDR C2XA10IA160](https://openairdocs.org/sdr/C2XA10IA160), May 23, 2010: INDICATOR. DEFECTIVE. CRP - FLIGHT 2894, DURING CLIMB THE CREW REPORTED THAT THE NUMBER ONE FUEL QUANTITY INDICATOR DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT I
- [SDR C2XA10IA133](https://openairdocs.org/sdr/C2XA10IA133), Apr 26, 2010: LIGHT. OUT OF ADJUST. LRD - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW TWELVE TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE EMERGENCY LIGHT,
- [SDR C2XA10IA126](https://openairdocs.org/sdr/C2XA10IA126), Apr 22, 2010: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, 
- [SDR C2XA10IA079](https://openairdocs.org/sdr/C2XA10IA079), Feb 22, 2010: LIGHT. SHORTED. IAH - FLIGHT 2720, THE CREW REPORTED, SMELLED ELECTRICAL SMOKE AND CB11 FOR THE COCKPIT READING LIGHTS POPPED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE
- [SDR C2XA10IA045](https://openairdocs.org/sdr/C2XA10IA045), Jan 29, 2010: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT ROW 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMB
- [SDR C2XA10IA027](https://openairdocs.org/sdr/C2XA10IA027), Jan 18, 2010: UNKNOWN. ODOR. IAH - FLIGHT 2372, THE FLIGHT ATTENDANT REPORTED A SMELL OF FUEL IN THE CABIN DURING DESCENT WITH THE SMELL COMING FROM THE WING AREA AND AFT. THE SMELL DISSIPA
- [SDR C2XA09TY119](https://openairdocs.org/sdr/C2XA09TY119), Jun 17, 2009: UNKNOWN. FUMES. THERE WERE SUFFOCATING FUMES AND ODOR REPORTED BY THE GROUND WORKERS COMING FROM THE CARGO BIN. THE CARGO BIN WAS INSPECTED AND FOUND ODOR TO BE RESIDUAL FROM A
- [SDR C2XA09CL071](https://openairdocs.org/sdr/C2XA09CL071), May 21, 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 DURING THE ULTRASOUND INSPEC
- [SDR C2XA09TY063A](https://openairdocs.org/sdr/C2XA09TY063A), Apr 20, 2009: CONNECTOR. LOOSE. SEAT 12BC SIDEWALL AFT EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR AND OPS CHECKED GOOD. IAW EMB 145 AMM 33-50-14
- [SDR C2XA08IA042](https://openairdocs.org/sdr/C2XA08IA042), Jan 29, 2008: SKIN. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE
- [SDR C2XA06IA082](https://openairdocs.org/sdr/C2XA06IA082), Jun 2, 2006: WIRE HARNESS. DISCONNECTED. OKC - FLIGHT 2637, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIR
- [SDR C2XA06TY006](https://openairdocs.org/sdr/C2XA06TY006), Jan 10, 2006: CASTING. CRACKED. MAIN DOOR FRAME STRUCTURE UPPER FWD STOP HOLE IS CRACKED (TOP INBOARD HOLE). REMOVED AND REPLACED CASTING FOR UPPER FWD PAX DOOR STOP IAW EMB 145 SRM 51-40-02.
- [SDR C2XA06TY005](https://openairdocs.org/sdr/C2XA06TY005), Jan 10, 2006: FLOORBEAM. CORRODED. GALLEY AREA RT OMEGA BEAM CORRODED. BLENDED OUT CORROSION, APPLIED HYSOL, FABRICATED REPAIR DOUBLER, DRILLED COUNTERSANK, ALODINED, PRIMED. INSTALLED PAINT. ALL

All 97: https://openairdocs.org/deregistered/N15948-2016-07-11/reports.md

## Other aircraft with N15948

- [Cancelled 1989-03-15](https://openairdocs.org/deregistered/N15948-1989-03-15): Piper PA-28R-200, S/N 28R7335110. Triennial form not returned

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