# N271SK: 2000 Embraer EMB-145LR, registration cancelled 2019-08-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 6, 2019
- Exported to: Zambia
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145305
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 7, 2000
- Certificate issued: May 14, 2018
- Last registry action: September 12, 2018
- Mode S code: A2ABCD
- Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE)
- Location: Bungay Norfolk, United Kingdom
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N271SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=271SK
- Page: https://openairdocs.org/deregistered/N271SK-2019-08-06

From the FAA registry file of November 3, 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-145LR: https://openairdocs.org/model/embraer-emb-145lr.md

## Service difficulty reports (71, newest 50)

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

- [SDR UHLA2015030600152](https://openairdocs.org/sdr/UHLA2015030600152), Mar 6, 2015: SOLENOID. FAULTY. THE CREW REPORTED THAT THEIR WAS A NOISE IN THE COCKPIT DURING CLIMB AND SUSPECTED THE NLG DOORS WERE OPEN. THE CREW DIVERTED THE ACFT AND LANDED WITHOUT INCIDE
- [SDR CHQA20141201342](https://openairdocs.org/sdr/CHQA20141201342), Dec 1, 2014: PRESSURE SWITCH. FAULTY. THE CREW REPORTED THAT ON CLIMB OUT, THEY RECEIVED A RUDDER OVER BOOST MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RUDDER SY
- [SDR CHQA20141028325](https://openairdocs.org/sdr/CHQA20141028325), Oct 28, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20 UNDER THE RAMP ANGLE. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02.
- [SDR CHQA20141028322](https://openairdocs.org/sdr/CHQA20141028322), Oct 28, 2014: FITTING. CRACKED. DURING INSPECTION THE SHEAR CLIP AT FRAME 62 & STRINGERS 6R & 8R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04.
- [SDR CHQA20141027327](https://openairdocs.org/sdr/CHQA20141027327), Oct 27, 2014: FITTING. CRACKED. DURING INSPECTION THE SHEAR CLIP AT FRAME 80 & STRINGER 8L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141027326](https://openairdocs.org/sdr/CHQA20141027326), Oct 27, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SUPPORT FROM FRAME 44 TO 50. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141027324](https://openairdocs.org/sdr/CHQA20141027324), Oct 27, 2014: SUPPORT. CRACKED. DURING INSPECTION THE LT WING BOX ANGLE SUPPORT WAS FOUND TO BE CRACKED BETWEEN FRAME 44 & 45. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141027323](https://openairdocs.org/sdr/CHQA20141027323), Oct 27, 2014: DOUBLER. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM PREVIOUS REPAIR AT THE CARBON CROSS MEMBER. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10 & 51-40-
- [SDR CHQA20131231472](https://openairdocs.org/sdr/CHQA20131231472), Dec 31, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE NR 1 EMERGENCY LIGHT BATTERY WAS NOT CHARGING. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS
- [SDR CHQA20130823325](https://openairdocs.org/sdr/CHQA20130823325), Aug 23, 2013: BALLAST. INOPERATIVE. DURING TAXI, CREW REPORTED A BURNING ODOR AND VISIBLE SMOKE IN THE CABIN COMING FROM THE CABIN LIGHTING BALLAST AT ROW 1. RETURNED TO GATE, REPLACED BALLAST. NO
- [SDR CHQA20130728196](https://openairdocs.org/sdr/CHQA20130728196), Jul 28, 2013: FLAP SYSTEM. MALFUNCTIONED. DURING CRUISE, RECEIVED A FLAP FAIL MESSAGE. FOLLOWED QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPS CHECKED 
- [SDR CHQA20130726195](https://openairdocs.org/sdr/CHQA20130726195), Jul 26, 2013: CONTROL UNIT. FAILED. DURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR REPLACED. O
- [SDR CHQA20130726194](https://openairdocs.org/sdr/CHQA20130726194), Jul 26, 2013: VELOCITY SENSOR. FAULTY. DURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR WERE REPLAC
- [SDR CHQA20130516165](https://openairdocs.org/sdr/CHQA20130516165), May 16, 2013: GCU. FAILED. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERE
- [SDR CHQA20130516164](https://openairdocs.org/sdr/CHQA20130516164), May 16, 2013: GENERATOR. FAILED. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERE
- [SDR CHQA20130416117](https://openairdocs.org/sdr/CHQA20130416117), Apr 16, 2013: PROXIMITY SWITCH. FAULTY. CREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT 
- [SDR CHQA20130416116](https://openairdocs.org/sdr/CHQA20130416116), Apr 16, 2013: ELECTRONIC UNIT. FAULTY. CREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT 
- [SDR CHQA20130326091](https://openairdocs.org/sdr/CHQA20130326091), Mar 26, 2013: PROXIMITY SENSOR. FAULTY. CREW REPORTED THAT THE LEFT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED WHEN THE LANDING GEAR LEVER WAS SELECTED DOWN. THE CREW DECLARED AN EMERGENCY AND THE
- [SDR CHQA20130324090](https://openairdocs.org/sdr/CHQA20130324090), Mar 24, 2013: LIGHT. DEFECTIVE. CREW REPORTED THAT DURING LANDING THERE WAS AN ELECTRICAL SMELL COMING FROM THE LIGHTING BALLAST AT ROWS 5 AND 6. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENA
- [SDR CHQA20130126030](https://openairdocs.org/sdr/CHQA20130126030), Jan 26, 2013: SWITCH. INOPERATIVE. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE DID NOT CLEAR. THE
- [SDR CHQA20130125029](https://openairdocs.org/sdr/CHQA20130125029), Jan 25, 2013: BLEED VALVE. FAULTY. CREW REPORTED THAT DURING CLIMB, THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK. THE CREW DIVERTED TO
- [SDR CHQA20121229004](https://openairdocs.org/sdr/CHQA20121229004), Dec 29, 2012: THERMOSTAT. FAULTY. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MA
- [SDR CHQA20121229003](https://openairdocs.org/sdr/CHQA20121229003), Dec 29, 2012: VALVE. FAULTY. CREW REPORTED, DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTE
- [SDR CHQA20121126446](https://openairdocs.org/sdr/CHQA20121126446), Nov 26, 2012: STRUT. LOW. CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, 
- [SDR CHQA20121126445](https://openairdocs.org/sdr/CHQA20121126445), Nov 26, 2012: STRUT. LOW. CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, 
- [SDR CHQA20121126444](https://openairdocs.org/sdr/CHQA20121126444), Nov 26, 2012: STRUT. LOW. CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, 
- [SDR CHQA20120917352](https://openairdocs.org/sdr/CHQA20120917352), Sep 17, 2012: ENGINE. FAILED. CREW REPORTED THAT DURING FLIGHT THAT THE ENGINE 2 OIL PRESSURE DROPPED INTO THE AMBER RANGE AND THE ENGINE ITT ROSE INTO THE RED. THE CREW SHUT DOWN THE ENGINE
- [SDR CHQA20120907331](https://openairdocs.org/sdr/CHQA20120907331), Sep 7, 2012: SKIN. DENTED. DURING INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R. THE DENT ON THE RIGHT FUSELAGE SKIN BETW
- [SDR CHQA20120906336](https://openairdocs.org/sdr/CHQA20120906336), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 12 AND FRAME 13 AND BETWEEN STINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REV
- [SDR CHQA20120806330](https://openairdocs.org/sdr/CHQA20120806330), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-012394 REVISION B, 
- [SDR CHQA20120906329](https://openairdocs.org/sdr/CHQA20120906329), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21R AND 20R WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B,
- [SDR CHQA20120906328](https://openairdocs.org/sdr/CHQA20120906328), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 11 AND FRAME 12 AND STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-012394 REVISION B, DE
- [SDR CHQA20120906327](https://openairdocs.org/sdr/CHQA20120906327), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 16 AND FRAME 18 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A DETAILS E
- [SDR CHQA20120906326](https://openairdocs.org/sdr/CHQA20120906326), Sep 6, 2012: SKIN. DAMAGED. DURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 19 AND FRAME 21 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A.
- [SDR CHQA20120903345](https://openairdocs.org/sdr/CHQA20120903345), Sep 3, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 23. THE RIGHT OMEGA BEAM AT FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.
- [SDR CHQA20120830344](https://openairdocs.org/sdr/CHQA20120830344), Aug 30, 2012: FRAME. DAMAGED. DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 31 AT STRINGER 15R. FRAME 31 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.
- [SDR CHQA20120829343](https://openairdocs.org/sdr/CHQA20120829343), Aug 29, 2012: FRAME. DAMAGED. DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 30 AT STRINGER 15R. FRAME 30 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.
- [SDR CHQA20120829342](https://openairdocs.org/sdr/CHQA20120829342), Aug 29, 2012: FRAME. DAMAGED. DURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 25 AT STRINGER 15R. FRAME 25 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.
- [SDR CHQA20120827341](https://openairdocs.org/sdr/CHQA20120827341), Aug 27, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER OMEGA BEAM AROUND THE ANCHOR NUT WAS FOUND CORRODED BETWEEN FRAME 24 AND FRAME 25. THE CENTER OMEGA BEAM AROUND ANCHOR NUT BETWEEN
- [SDR CHQA20120824340](https://openairdocs.org/sdr/CHQA20120824340), Aug 24, 2012: STRUCTURE. CORRODED. DURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE
- [SDR CHQA20120824339](https://openairdocs.org/sdr/CHQA20120824339), Aug 24, 2012: STRUCTURE. CORRODED. DURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE
- [SDR CHQA20120823338](https://openairdocs.org/sdr/CHQA20120823338), Aug 23, 2012: BEAM. CORRODED. DURING INSPECTION, THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED AND THE NEW PART WAS I
- [SDR CHQA20120822346](https://openairdocs.org/sdr/CHQA20120822346), Aug 22, 2012: SKIN. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE LEFT WING UPPER SKIN AT THE GROUND SPOILER CENTER HINGE CUTOUT. THE LEFT WING UPPER SKIN AT THE GROUND SPOILER HINGE
- [SDR CHQA20120822337](https://openairdocs.org/sdr/CHQA20120822337), Aug 22, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 HAD AND EXISTING REPAIR THAT WAS FOUND TO BE CORRODED. THE LEFT OMEGA BEAM AT FRAME 20 EXISTING REPAIR WAS RE
- [SDR CHQA20120822335](https://openairdocs.org/sdr/CHQA20120822335), Aug 22, 2012: ANGLE. CRACKED. DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 
- [SDR CHQA20120822334](https://openairdocs.org/sdr/CHQA20120822334), Aug 22, 2012: ANGLE. CRACKED. DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 
- [SDR CHQA20120822333](https://openairdocs.org/sdr/CHQA20120822333), Aug 22, 2012: ANGLE. CRACKED. DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 
- [SDR CHQA20120822332](https://openairdocs.org/sdr/CHQA20120822332), Aug 22, 2012: ANGLE. CRACKED. DURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 
- [SDR CHQA20120822325](https://openairdocs.org/sdr/CHQA20120822325), Aug 22, 2012: UPLOCK BRACKET. CRACKED. DURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCO
- [SDR CHQA20120822324](https://openairdocs.org/sdr/CHQA20120822324), Aug 22, 2012: UPLOCK BRACKET. CRACKED. DURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCO

All 71: https://openairdocs.org/deregistered/N271SK-2019-08-06/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20130515008749I](https://openairdocs.org/incident/20130515008749I), May 15, 2013: Embraer EMB-145LR (N271SK), Manchester, NH, No damage. During initial climbout of klga the crew heard a relay clicking about once every 10 seconds from behind the captains seat. This prompted a view of the MFD…
- [Incident 20120917021129I](https://openairdocs.org/incident/20120917021129I), Sep 17, 2012: Embraer EMB-145LR (N271SK), Louisville, KY, No damage. On September 17, 2012 at approximately 2045Z, CHQ6143 enroute from lga to sdf shut the number two engine shut down due to engine vibration and high EGT…

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