# N311EA: 1972 Lockheed L-1011-385-1, registration cancelled 2004-02-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 23, 2004
- Exported to: Thailand
- Status when cancelled: Triennial form not returned
- Airframe: [Lockheed L-1011-385-1](https://openairdocs.org/model/lockheed-l-1011-385-1) (registry code 5265010)
- Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554)
- Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Serial number: 193A-1012
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: May 1, 1987
- Certificate issued: November 8, 1989
- Last registry action: December 18, 2001
- Mode S code: A34AED
- Owner when cancelled: [Arena Aviation Inc](https://openairdocs.org/faa-owner/ARENA%20AVIATION%20INC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.0845° N, 115.1461° W: Placed by OpenAirDocs at the center of ZIP code 89119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N311EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311EA
- Page: https://openairdocs.org/deregistered/N311EA-2004-02-23

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 Lockheed L-1011-385-1: https://openairdocs.org/model/lockheed-l-1011-385-1.md

## Service difficulty reports (58, newest 50)

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

- [SDR WRNA200300011](https://openairdocs.org/sdr/WRNA200300011), May 21, 2003: PRESSURE SWITCH. LEAKING. DURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENG
- [SDR WRNA200300010](https://openairdocs.org/sdr/WRNA200300010), May 21, 2003: FIRE LOOP. FALSE ACTIVATION. AFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF 
- [SDR WRNA200200007](https://openairdocs.org/sdr/WRNA200200007), Oct 22, 2002: FIRE LOOP. SHORTED. Enroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silenced, #1 engine shutdown per procedures. 
- [SDR WRNA200200006](https://openairdocs.org/sdr/WRNA200200006), Oct 18, 2002: DUCT. DETACHED. Aircraft at F/L 280 outflow valves full closed cabin climbing at 2,000 ft/min. Manual and stby control no help. Aircraft returned to departing airport. Fuel dum
- [SDR WRNA200200004](https://openairdocs.org/sdr/WRNA200200004), Aug 22, 2002: COMPUTER. UNSERVICEABLE. During Climb to cruise altitude Both Mach Feel Fail Lights came on. Fuel dump procedures carried out for Max landing wt (26K lbs dumped). Aircraft landed normal
- [SDR WRNA00023](https://openairdocs.org/sdr/WRNA00023), Nov 13, 2001: COVER. OUT OF POSITION. AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRA
- [SDR WRNA200100018](https://openairdocs.org/sdr/WRNA200100018), Nov 13, 2001: COVER. SEPARATED. AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRA
- [SDR 20010529SG003](https://openairdocs.org/sdr/20010529SG003), Apr 23, 2001: ENGINE. VIBRATION. ENGINE SHUTDOWN FOR HIGH VIBRATION INDICATION AT FL350. IN CRUISE INDICATION 3 AND AMBER LIGHT. BOTH A AND B PICKUPS. LOW SELECTION INDICATES THIS PROBLEM. TEST
- [SDR WRN2001F00000](https://openairdocs.org/sdr/WRN2001F00000), Apr 22, 2001: TURBINE BLADES. FAILED. INSPECTION REVEALED IP TURBINE BLADE FAILURE. REMOVED AND REPLACED ENGINE IAW TRADEWINDS CARD L2-130-A01 AND FORMS TWM-7103B AND TWM-7103BB. AIRCRAFT RUN AND LE
- [SDR 2001F00004](https://openairdocs.org/sdr/2001F00004), Apr 14, 2001: O-RING. PINCHED. NR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGED (PINCHED) O-
- [SDR WRN2001F00001](https://openairdocs.org/sdr/WRN2001F00001), Apr 12, 2001: COMPRESSOR. STALLED. ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR
- [SDR 20010509SG004](https://openairdocs.org/sdr/20010509SG004), Apr 12, 2001: COMPRESSOR. STALLED. ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR
- [SDR 20000516AP005](https://openairdocs.org/sdr/20000516AP005), Mar 30, 2000: CARD. MALFUNCTIONED. NR 2 ENGINE FILTER PRESSURE LIGHT, ALSO ENGINE VIB FILTER PRESSURE LIGHT CAME ON DURING CRUISE. NR 2 ENGINE SHUTDOWN. A/C CAME IN WITH NORMAL APPROACH AND LANDI
- [SDR 20000615AP019](https://openairdocs.org/sdr/20000615AP019), Jan 9, 2000: DOUBLER. CORRODED. DURING INSPECTION OF FESC, CORROSION FOUND BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV VENTILATION DUCT. REMOVED AND REPLACED COR
- [SDR 20000405AP001](https://openairdocs.org/sdr/20000405AP001), Jan 9, 2000: DOUBLER. CORRODED. DURING INSPECTION OF FESC, FOUND CORROSION BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV. VENTILATION DUCT REMOVED AND REPLACED COR
- [SDR 2000ZZZM250](https://openairdocs.org/sdr/2000ZZZM250), Oct 19, 1999: OIL PUMP. FAILED. NR 2 ENGINE RAPID LOSS OF OIL QTY ENGIEN RAN APPROXIMATELY 2 MINUTES PRIOR TO SHUTDOWN WINDMILLED WITH NO OIL QTY 23 MINUTES OIL PRESSURE NR 2 LIGHT ON. RETURNE
- [SDR 98ZZZM404](https://openairdocs.org/sdr/98ZZZM404), Mar 18, 1998: HYD LINE. LEAKING. SYSTEM 'C' HYD RSVR QTY LOW AND DECREASING. SWITCHING PUMP OFF DID NOT STOP FLUID LOSS. REF MANUAL GEAR EXTENSION, ATM TURNED OFF FLUID LOSS STOPPED AT AROUND T
- [SDR 98ZZZM193](https://openairdocs.org/sdr/98ZZZM193), Jan 16, 1998: ACTUATOR. FAILED. AFTER TAKEOFF DURING FLAP RETRACTION FLAP/SLAT LOCK LIGHT ON, L/E TRANS LIGHT REMAINED ON. GREEN SLAT LIGHTS ON LEFT WING. NO LIGHTS ON RT WING. AIRCRAFT RETURN
- [SDR 97ZZZX3958](https://openairdocs.org/sdr/97ZZZX3958), Aug 22, 1997: TIRE. FAILED. ON TAKEOFF ROLL, NR 6 TIRE BLEW. TIRE RUBBER DAMAGED HYDRAULIC LINE AND T/E WING PANEL. ACFT DUMPED FUEL AND RETURNED TO BASE. LANDING NORMAL. NR 5 AND NR 6 TIR
- [SDR 97ZZZX3800](https://openairdocs.org/sdr/97ZZZX3800), Aug 4, 1997: RUDDER STUD. SHEARED. BQN - DURING TAXI, CREW NOTICED A BINDING WITHIN THE RUDDER PEDALS FOLLOWED BY A 'POP' SOUND FROM UNDERNEATH COCKPIT FLOOR. AIRCRAFT RETURNED TO GATE. BQN MAINT
- [SDR 97ZZZX3393](https://openairdocs.org/sdr/97ZZZX3393), Jul 14, 1997: BRACE ASSY. CRACKED. RIGHT MLG DOWNLOCK JURY BRACE FOUND CRACKED UPON MAINTENANCE WALK-AROUND. REMOVED AND REPLACED DOWNLOCK JURY BRACE IAW 32-11-14. AIRCRAFT RETURNED TO SERVICE. (
- [SDR 97ZZZM707](https://openairdocs.org/sdr/97ZZZM707), Jun 2, 1997: ACTUATOR. FAILED. AFTER TAKEOFF, LEFT GEAR INTRANS DOOR, F/E LEFT GEAR OR DOOR LIGHTS ON GEAR RETRACTED. AIRCRAFT DUMPED FUEL AND RETURNED TO BQN WITH A NORMAL LANDING. WHEN AIRC
- [SDR 97ZZZM674](https://openairdocs.org/sdr/97ZZZM674), May 23, 1997: WATER SEPARATOR. FAILED DUCT. APPROX 20 MINUTES AFTER TAKEOFF, LOST CONTROL OF CABIN PRESSURE DUE TO LEAK AT 28,000 FEET. A LOUD NOISE OCCURRED AT THE SAME TIME. RETURNED TO GSO, LANDING NOR
- [SDR 97ZZZM570](https://openairdocs.org/sdr/97ZZZM570), Apr 9, 1997: PANELS. MISSING. AFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS
- [SDR 97ZZZM569](https://openairdocs.org/sdr/97ZZZM569), Apr 9, 1997: PANELS. MISSING. AFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS
- [SDR 97ZZZM571](https://openairdocs.org/sdr/97ZZZM571), Apr 8, 1997: ACTUATOR. FAILED. ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT ON, WITH RED DOOR AND RED INTRANSIT LIGHT ON. FUEL JETTISON FROM 76,000 LBS TO 30,000 LBS. AIRCRAFT LANDED NORMALLY. R
- [SDR 96ZZZX5798](https://openairdocs.org/sdr/96ZZZX5798), Oct 30, 1996: LINE. CRACKED. A-HYD SYS RAPIDLY DEPLETED AT 33,000 FEET. SYS SHUTDOWN IAW FLIGHT MANUAL. AIRCRAFT LANDED NORMALLY. FOUND HYD LINE IN NR 1 PYLON AREA LEAKING. REPAIRED LINE IA
- [SDR 96ZZZX5797](https://openairdocs.org/sdr/96ZZZX5797), Oct 29, 1996: PDU MOTOR. CRACKED. A-HYD RESERVOIR QTY LOW AND LOW QTY LIGHT ON. TURNED OFF HYD PUMP - LEAK STOPPED. AIRCRAFT LANDED NORMAL. FOUND SLAT A-SYS PDU HYD MOTOR HOUSING CRACKED. REMOVE
- [SDR 96ZZZM1536](https://openairdocs.org/sdr/96ZZZM1536), Oct 18, 1996: LOCK ACTUATOR. FAILED. MAIN GEAR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT. LANDING NORMAL. REMOVED AND REPLACED MAIN GEAR DOOR LOCK AC
- [SDR 96ZZZM371](https://openairdocs.org/sdr/96ZZZM371), Feb 20, 1996: PROX LOGIC BOX. MALFUNCTIONED. NOSE GEAR OR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB, RETURNED TO AIRPORT. LANDING WAS NORMAL. ADJUSTED NOSE GEAR UPLOCK SENSOR IAW 32-61-04. RE
- [SDR DLSP96004](https://openairdocs.org/sdr/DLSP96004), Feb 16, 1996: SKIN. CRACKED. ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN WAS FOUND WITH AN APPROXIMATE 1 INCH LONG CRACK RUNNING HORIZONTALLY FROM THE FORWARD EDGE OF THE S
- [SDR DLSP96003](https://openairdocs.org/sdr/DLSP96003), Feb 16, 1996: ANGLE. OVERSIZE HOLES. ATL - DURING CONTRACT MAINTENANCE AT DALA, C/W AD 94-05-01, REPLACEMENT OF FUSELAGE LT AND RT WING TO FUSELAGE AT TACH UPPER ROOT JOINT FAIL-SAFE ANGLE, SEVERAL
- [SDR DLSP96002](https://openairdocs.org/sdr/DLSP96002), Feb 16, 1996: SKIN. CRACKED. ATL - DURING CONTRACT MAINTENANCE WITH DALA, FOUND FUSELAGE SKIN AT FS 1363 CRACKED IN THE TYPICAL MANNER DEPICTED IN THE L1011 SRM 53-11-00, FIGURE 826, REPAIR
- [SDR DLSP96001](https://openairdocs.org/sdr/DLSP96001), Feb 16, 1996: SKIN. CRACKED. ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN AT FS 1363 IS CRACKED IN THE TYPICAL MANNER DEPICTED IN SRM 53-11-00, FIGURE 826, REPAIR. THE CRACK
- [SDR 96ZZZM283](https://openairdocs.org/sdr/96ZZZM283), Feb 4, 1996: PRESS CTLR. FAILED. AIRCRAFT DEPARTED BQN EN ROUTE TO GSO, CREW EXPERIENCED DIFFICULTY WITH CABIN PRESSURIZATION. C/B 3X14 PULLED AND RESET TO NO AVAIL. AIRCRAFT RETURNED TO BQN. L
- [SDR 95ZZZM520](https://openairdocs.org/sdr/95ZZZM520), Sep 12, 1995: ANGLE. CRACKED. DURING NORMAL SERVICING OF ATM, MAINTENANCE NOTICED A CRACK LOCATED AT FS 1363 WL 147 (APPROXIMATELY) ON THE RIGHT SIDE. ANGLE 1561639-101 REPAIRED IAW SRM 53-1
- [SDR 95ZZZM506](https://openairdocs.org/sdr/95ZZZM506), Sep 2, 1995: PIN. CRACKED. WHILE PERFORMING ROUTINE MAINTENANCE, MECHANIC FOUND LEFT MLG RETRACT ACTUATOR PIN CRACKED AT AFT HOUSING. MLG PIN WAS REMOVED AND REPLACED IAW 32-11-27. AIRCRA
- [SDR 95ZZZX4103](https://openairdocs.org/sdr/95ZZZX4103), Jul 8, 1995: BULKHEAD. CRACKED. ACCOMPLISHED AD 95-12-24. DISCOVERED CRACKS ON RIGHT LOWER OUTBOARD SECTION OF FS 1363 BULKHEAD BY VISUAL INSPECTION. PERFORMED BOLT HOLE EDDY CURRENT INSPECTIO
- [SDR 95ZZZW622](https://openairdocs.org/sdr/95ZZZW622), Apr 18, 1995: SPAR WEB. CRACKED. WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8
- [SDR 95ZZZW621](https://openairdocs.org/sdr/95ZZZW621), Apr 18, 1995: SPAR WEB. CRACKED. WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8
- [SDR DALR950002](https://openairdocs.org/sdr/DALR950002), Apr 17, 1995: FITTING. CRACKED. ATL - DURING LETTER CHECK AT DALR, THE NLG SHOCK STRUT SUPPORT FITTING ON THE RBL 22 BULKHEAD WAS FOUND CRACKED NEAR FS 449. CRACKS WERE REPAIRED PER DER APPROV
- [SDR DALR950006](https://openairdocs.org/sdr/DALR950006), Apr 6, 1995: FITTING. CORRODED. ATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVES
- [SDR DALR950013](https://openairdocs.org/sdr/DALR950013), Apr 5, 1995: WING SKIN. CRACKED. ATL - DURING LETTER CHECK, COMPLYING WITH AD 94-05-01 AND AD 93-17-01. AT THE REPLACEMENT OF THE LEFT WING INBOARD REAR SPAR SECTION, A CRACK WAS FOUND IN THE U
- [SDR DALR950005](https://openairdocs.org/sdr/DALR950005), Apr 3, 1995: SPAR CAP. CRACKED. ATL - DURING LETTER CHECK AT DALR. THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP WAS FOUND WITH A CRACK IN ITS LEFT SIDE OUTBOARD END. THIS CRACK IS TYPIC
- [SDR DALR950004](https://openairdocs.org/sdr/DALR950004), Apr 3, 1995: SPAR CAP. CRACKED. ATL - DURING LETTER CHECK AT DALR, WING CENTER SECTION FS 1043 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DE
- [SDR DALR950003](https://openairdocs.org/sdr/DALR950003), Apr 3, 1995: SPAR CAP. CRACKED. ATL - DURING LETER CHECK AT DALR. THE WING CENTER SECTION INTERMEDIATE SPAR UPPER CAP AT FS 1103 WAS FOUND CRACKED AT THE LEFT SIDE OUTBOARD END. THE CRACK IS T
- [SDR DALR950001](https://openairdocs.org/sdr/DALR950001), Apr 3, 1995: FITTING. CORRODED. ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10 DURING THE REPLACEMENT OF THE INBOARD LEFT AND RIGHT REAR SPAR WEB AND REWORK OF T
- [SDR DALR950008](https://openairdocs.org/sdr/DALR950008), Mar 31, 1995: SKIN. CRACKED. ATL - DURING LETTER CHECK A DALR. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER RIGHT SIDE OF THE FS 983 PRESSURE BULKHEAD UNDER THE FUSELAGE-TO-WING BOX LON
- [SDR DALR950010](https://openairdocs.org/sdr/DALR950010), Mar 30, 1995: DOUBLER. CRACKED. ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 FUSELAGE NLG WHEELWELL MOD. FS 328 PER DL EO.7-53207-3AD. AN ADDITIONAL CRACK WAS FOUND THAT WAS B
- [SDR DALR950009](https://openairdocs.org/sdr/DALR950009), Mar 30, 1995: LONGERON. CORRODED. ATL - DURING LETTER CHECK AT DALR. CONSIDERABLE CORROSION WAS FOUND AT FS 328 ON THE VERTICAL FLANGE OF THE LBL 22 NLG WHEELWELL SIDEWALL LOWER LONGERON. A NEW 

All 58: https://openairdocs.org/deregistered/N311EA-2004-02-23/reports.md

## FAA accident and incident reports (1)

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 19780201005259I](https://openairdocs.org/incident/19780201005259I), Feb 1, 1978: Lkheed 1011/ (N311EA), Boston, MA, Minor damage. Pilot struck a snowbank during taxi for takeoff.

## Other aircraft with N311EA

- [Registered now](https://openairdocs.org/aircraft/N311EA): Tomark Aero CZ Sro VIPER SD-4, S/N 0100, built 2017

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