# N307GB: 1975 Lockheed L-1011-385-1-15, registration cancelled 2015-05-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 8, 2015 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Lockheed L-1011-385-1-15](https://openairdocs.org/model/lockheed-l-1011-385-1-15) (registry code 5265015) - Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs) - Serial number: 193U1131 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 7, 1996 - Certificate issued: November 13, 2006 - Last registry action: November 17, 2009 - Mode S code: A339EB - Owner when cancelled: [Great Southwest Aviation Inc](https://openairdocs.org/faa-owner/GREAT%20SOUTHWEST%20AVIATION%20INC) - Location: [Roswell, NM](https://openairdocs.org/faa-place/NM/Roswell) - Owner type: Corporation - Owner's area on the map: 33.3734° N, 104.5294° W: Placed by OpenAirDocs: center of Roswell, NM, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N307GB - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=307GB - Page: https://openairdocs.org/deregistered/N307GB-2015-05-08 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 Lockheed L-1011-385-1-15: https://openairdocs.org/model/lockheed-l-1011-385-1-15.md ## Service difficulty reports (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ARWA20040103](https://openairdocs.org/sdr/ARWA20040103), Jan 19, 2004: LINER. DAMAGED. ENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND IN - [SDR ARWA20032101](https://openairdocs.org/sdr/ARWA20032101), Dec 6, 2003: SPOILER. MALFUNCTIONED. AFTER LANDING FOUND NR 4 SPOILER STILL UP ON RIGHT WING, NR 2 SPOILER FLOATING AND WILL NOT REACT TO INPUTS ON RIGHT WING AND THE RIGHT WING MOVES VERY SLOWLY. - [SDR ARWA20031205](https://openairdocs.org/sdr/ARWA20031205), Dec 5, 2003: SOCKET. MALFUNCTIONED. NR 2 ENGINE GREEN LIGHT DID NOT COME ON FOR TAKEOFF AT TTPP. TAKEOFF ABORTED AND RETURNED TO RAMP. RESET LIGHT SOCKET ON ANNUNCIATOR PANEL. OPERATIONAL CHECK NO - [SDR ARWA20030911](https://openairdocs.org/sdr/ARWA20030911), Sep 15, 2003: DRAIN LINE. LEAKING. SYSTEM B REVERSER QTY LOW AND DECREASING. SWITCHED POWERS OFF, STOPPED FLUID LOSS. REMOVED AND REPLACED 2R SYSTEM CASE DRAIN LINE. RAN ENGINE OPERATIONAL CHECK - [SDR ARWA20030406](https://openairdocs.org/sdr/ARWA20030406), Apr 28, 2003: SENSOR. FAILED. STALL WARNING NR 1 CHANEL FAILED IN FLIGHT, CONTINOUS STICK SHAKER IN FLIGHT. DE-SELECTED NR 1 CHANEL AND RETURNED TO MIAMI AS ADVISED BY FLIGHT CONTROL. DUMPED - [SDR ARWA20030405](https://openairdocs.org/sdr/ARWA20030405), Apr 27, 2003: ACCESS PANEL. LEAKING. WITH BOTH OUTFLOW VALVES CLOSED, MAX PRESSURE DIFFERENTIAL 4.5 INCHES CABIN CLIMBING. CHECK FOR PNEU LEAK. RETURNED TO MIA. SECURED INNER PANEL ON C-2 FOR HTE U - [SDR ARWA20030311](https://openairdocs.org/sdr/ARWA20030311), Mar 18, 2003: CONNECTOR. LOOSE. SYSTEM "B" RESERVOIR QUANTITY LOW AND DECREASING. SWITCHING PUMP AND ATM OFF STOPPED FLUID LOSS. TIGHTENED CONNECTOR AT "B" SYSTEM ATM PRESSURE SWITCH IAW M/M 2 - [SDR ARWA20030107](https://openairdocs.org/sdr/ARWA20030107), Jan 30, 2003: ACTUATOR. FAILED. AFTER TAKEOFF RED INTRANSIT LIGHT ILLUMINATED. ALSO PERFORMED CHECKLIST, NO CHANGE. RETURNED TO MIAMI. REMOVED AND REPLACED RT TURN LANDING GEAR DOOR LOCK ACTUA - [SDR ARWA20030109](https://openairdocs.org/sdr/ARWA20030109), Jan 30, 2003: PROXIMITY SENSOR. FAILED. DURING RETRACTED GEAR RED INTRANSIT LIGHT ON FLIGHT ENGINEER PANEL SHOWS RT GEAR DOOR LIGHT ON WITH GEAR DOWN. ALL INDICATIONS NORMAL. WITH GEAR UP NO FEEL VIBR - [SDR ARWA20030104](https://openairdocs.org/sdr/ARWA20030104), Jan 22, 2003: ENGINE. VIBRATION. NR 3 ENGINE VIBRATION DURING CRUISE AT 350 FT LOW POSITION A-B 2.8 CAUTION LIGHT ON. SHUTDOWN ENGINE AT 06:35 Z. REMOVE AND REPLACE ALL NR 3 ENGINE C-1 BLADES I - [SDR ARWA20030103](https://openairdocs.org/sdr/ARWA20030103), Jan 19, 2003: BLADE. DAMAGED. NR 3 ENGINE AT 370 FEET, BOTH CHANNEL A AND B 2.7 CAUTION LIGHT ON. SHUTDOWN ENGINE 1200Z. FEELING THE VIBRATION ON THE FLOOR. REMOVED AND INSPECTED MASTER AND - [SDR ARWA20021110](https://openairdocs.org/sdr/ARWA20021110), Nov 23, 2002: MODULE. FAILED. LOST (A) HYDRAULIC SYSTEM QUANTITY JUST BEFORE TOUCHDOWN. REMOVED AND REPLACED HIGH PRESSURE FILTER HOUSING IAW MM. OPERATIONS AND LEAK CHECK NORMAL IAW MM. - [SDR ARWA20020402](https://openairdocs.org/sdr/ARWA20020402), Apr 14, 2002: INDICATOR. FAULTY. ABORTED TAKEOFF AT 110 KTS, DUE TO NR 2 ENGINE EPR NOT AT TO POWER (1.2 EPR). REMOVED AND REPLACED NR 2 EPR INDICATOR IAW 77-11-00.` - [SDR ARWA20011121](https://openairdocs.org/sdr/ARWA20011121), Nov 23, 2001: FUEL CAP. MISSING. AFTER T/O, FUEL LEAK FROM TOP OF LEFT WING. APPROX 10,000 LBS LOST FROM 2L; TANK NR 1 DID NOT DUMP FUEL INTRANSIT LIGHT DID NOT BLINK WITH SWITCH ON. APPROX 10, - [SDR ARWA0010713](https://openairdocs.org/sdr/ARWA0010713), Jun 29, 2001: FLOORBEAM. CORRODED. DURING SCHEDULE MAINTENANCE FLOORBEAM AT FS 237 HAS EVIDENCE OF CORROSION UNDER MOON COVER. REMOVED TO EVALUATE. REMOVED CORROSION AT FS 237 IAW SRM 51-21-01 FO - [SDR ARWA0010712](https://openairdocs.org/sdr/ARWA0010712), Jun 29, 2001: FLOORBEAM. CORRODED. DURING SCHEDULE MAINTENANCE FLOORBEAM AT FS 251 HAS EVIDENCE OF CORROSION. REMOVE TO EVALUATE. REMOVED CORROSION ON FS 251 FLOORBEAM AS PER SRM 51-21-01, FOUND - [SDR ARWA0010711](https://openairdocs.org/sdr/ARWA0010711), Jun 29, 2001: SUPPORT. CORRODED. DURING SCHEDULE MAINTENANCE WALL SUPPORT FS 281 BL 22L HAS CORROSION BEYOND LIMITS. INSTALLED FLOORBEAM REPAIR AT FS 281 BL22L IAW SRM 53-21-00 FIG 815. - [SDR ARWA0010710](https://openairdocs.org/sdr/ARWA0010710), Jun 29, 2001: FLOORBEAM. CORRODED. DURING SCHEDULE MAINTENANCE FLOORBEAM FS 281 FROM BL 22L TO BL 22R HAS EVIDENCE OF CORROSION. REMOVED FLOOR TO EVALUATE. REMOVED CORROSION AT FLOORBEAM STA 281 - [SDR ARWA0010709](https://openairdocs.org/sdr/ARWA0010709), Jun 29, 2001: FLOOR PANEL. DURING SCHEDULE MAINTENANCE. N/R 488. DISCREPANCY: FWD ENTRY AREA, FLOOR PANEL SUPPORT STRUCTURE IS CORRODED FROM STA 260 TO STA 280 AT LBL30. CORRECTIVE ACTION - [SDR ARWA0010708](https://openairdocs.org/sdr/ARWA0010708), Jun 29, 2001: FLOORBEAM. CORRODED. DURING SCHEDULE MAINTENANCE FWD ENTRY AREA, STA 281 FLOORBEAM, TOP CAP HAS CORROSION FROM APPROX LBL 48 TO RBL 48. REMOVED CORROSION AT FLOORBEAM STA 281 IAW SR - [SDR ARWA0010714](https://openairdocs.org/sdr/ARWA0010714), Jun 29, 2001: BRACKET. DURING SCHEDULE MAINTENANCE. N/R 633. DISCREPANCY: EVIDENCE OF CORROSION, RIGHT WING TO FUSELAGE BRACKET AT WHEEL WELL. CORRECTIVE ACTION: REMOVED CORROSION, FI - [SDR ARWA0010701](https://openairdocs.org/sdr/ARWA0010701), Jun 29, 2001: PANEL. CRACKED. DURING SCHEDULE MAINTENANCE RT HORIZONTAL STABILIZER L/E PANEL AT T/E OF PANEL 331A HAS CRACK AT I/B CORNER. INSTALLED DOUBLER REPAIR AT RT HORIZONTAL STABILIZE - [SDR ARWA0010707](https://openairdocs.org/sdr/ARWA0010707), Jun 29, 2001: FITTING. DURING SCHEDULE MAINTENANCE. N/R 493. DISCREPANCY: C2 CARGO DOOR CUT-OUT, CENTER UPPER DOOR SILL PIVOT CLEVIS ATTACH FITTING IS CRACKED. CORRECTIVE ACTION: REMO - [SDR ARWA0010706](https://openairdocs.org/sdr/ARWA0010706), Jun 29, 2001: SPLICE. DURING SCHEDULE MAINTENANCE. N/R 235. DISCREPANCY: SPLICE CRACKED AT FS 1203 BELOW WL200. CORRECTIVE ACTION: REMOVED CRACKED SPLICE & REPLACED WITH NEW ONE IAW - [SDR ARWA0010705](https://openairdocs.org/sdr/ARWA0010705), Jun 29, 2001: SPLICE. DURING SCHEDULE MAINTENANCE. N/R 234. DISCREPANCY: FS 1183 BELOW WL 200 CRACK ON SPLICE. CORRECTIVE ACTION: INSTALLED SPLICE AT FS 1183 RH IAW SRM 51-40-01. - [SDR ARWA0010704](https://openairdocs.org/sdr/ARWA0010704), Jun 29, 2001: FLOOR SUPPORT. CRACKED. DURING SCHEDULE MAINTENANCE. FLOOR PANEL SUPPORT BETWEEN SEAT TRACK 10&11 CRACKED AT FS 980. REPLACED CRACKED FLOOR PANEL SUPPORT AT FS 980 BETWEEN SEAT TRACK 1 - [SDR ARWA0010703](https://openairdocs.org/sdr/ARWA0010703), Jun 29, 2001: FRAME. DURING SCHEDULE MAINTENANCE. N/R 470. DISCREPANCY: R/H ECS COMPARTMENT STATION 449 BULKHEAD FRAME IS CRACKED ON FWD SIDE BETWEEN STRINGER 26 AND STRINGER 27. CO - [SDR ARWA0010702](https://openairdocs.org/sdr/ARWA0010702), Jun 29, 2001: FRAME. CRACKED. DURING SCHEDULE MAINTENANCE, LT ECS COMPARTMENT, STATION 449 BULKHEAD FRAME IS CRACKED ON FWD SIDE BETWEEN STRINGER 41 TO STRINGER 42. STOP DRILLED CRACK, CUT A - [SDR ARWA990305](https://openairdocs.org/sdr/ARWA990305), Mar 18, 1999: ENGINE. FAILED. FLT 507 - ENGINE VIBRATION ON NR 1. VIBRATION METER AT 2 UNITS, ALL OTHER PARAMETERS NORMAL, THROTTLE ON NR 1 ENGINE WAS IMMEDIATELY REDUCED, WHERE NR 1 VIBRATI - [SDR ARWA981019](https://openairdocs.org/sdr/ARWA981019), Oct 19, 1998: ACTUATOR. INOP. L/E TRANS LIGHT ON, AFTER SLAT/FLAP RETRACTION. FLAPS RECYCLED, LIGHT REMAINED ON, AIRFRAME VIBRATES SLIGHTLY WITH FLAPS RETRACTED. SLAT DEGREE IND SHOWS 1-2 DE - [SDR ARWA981018](https://openairdocs.org/sdr/ARWA981018), Oct 16, 1998: COMPARATOR. DIRTY. AIR TURNBACK, LE TRANS LIGHT ON AFTER SLAT RETRACTION. FLAPS RECYCLED, LE TRANS LIGHT REMAINED ON. LIGHT WENT OUT WHEN FLAPS WERE RETRACTED AFTER LANDING. CLEAN - [SDR ARWA980797](https://openairdocs.org/sdr/ARWA980797), Jul 10, 1998: AMPLIFIER. FAILED. MIA - FLT 239 - AFTER TAKEOFF, NR 3 ENGINE N1 INDICATOR FAILED. INDICATED 20.7 PERCENT AT ALL THRUST SETTINGS AND N2, HIGH READINGS DUMPED 5 LBS OF FUEL. CORREC - [SDR ARWA980601](https://openairdocs.org/sdr/ARWA980601), Jun 9, 1998: CONNECTOR. LOOSE. DURING TAKEOFF, THE TAKEOFF AURAL WARNING SOUNDED, AT THE SAME TIME L/E EXT LIGHT WAS FLICKERING. ALSO RT WING NR 7 SLAT MONITORING LIGHT FLICKERING. RETURNED T - [SDR ARWA980505](https://openairdocs.org/sdr/ARWA980505), May 14, 1998: BOOST PUMP. SHORTED. MIA - FLT 501 - TANK NR 1 LEFT FUEL BOOST PUMP LOW PRESS LIGHT ILLUM PUMP INOP. THIS WAS PLACED ON DMI. AFTER REFUELING AIRCRAFT, A FUEL LEAK WAS NOTED AT THE 1 - [SDR ARWA980402](https://openairdocs.org/sdr/ARWA980402), Apr 2, 1998: AOA SENSOR. MALFUNCTIONED. WINDSHEAR WARNING COMES ON SHORTLY AFTER TAKEOFF AND AT APPROX 1.000 DURING LANDING APPROACH. REMOVED AND REPLACED AOA SENSORS. REMOVED AND REPLACED LONGITUDINA - [SDR ARWA980401](https://openairdocs.org/sdr/ARWA980401), Mar 31, 1998: INU. INOPERATIVE. F/O ADI FAILED FULL NOSE UP. AFTER T/O WINDSHEER ALERT WARNING ON AT 50 FT ANGLE AND 1000 ON APPROACH. FLAP ASSEMETRY DET FOULT LIGHT ON DURING FLAP RETRACTION. - [SDR ARWA980307](https://openairdocs.org/sdr/ARWA980307), Mar 24, 1998: MONITOR. INOPERATIVE. A/C BLOCK TURNBACK WITH SPOILER NR 5 INDICATION ON SPI NOT WORKING. AFTER A/C ON BLOCKS ENGINE SHUT DOWN, NR 1 ENGINE VIBRATION SHOWED 4 UNITS. ENTERED SPI FOR - [SDR ARWA970603](https://openairdocs.org/sdr/ARWA970603), Jun 16, 1997: ENGINE. FLAMED OUT. AGT - FLT 604 - CRUISHING AT FL 390, NR 2 ENIGNE FLAMED OUT. DESCENDED TO FL 310 AND ATTEMPTED TO RESTART. N3 ROTATION WAS INDICATED. ENGINE DID NOT START. FLIG - [SDR ARW970603](https://openairdocs.org/sdr/ARW970603), Jun 16, 1997: GEARBOX. FAILED. CRUISING AT FL 390 NR 1 ENGINE FLAMED OUT. DESCENDED TO FL310 AND ATTEMPTED RESTART. N3 ROTATION WAS INDICATED. ENGINE DID NOT START. FLIGHT DIVERTED TO RBR AND - [SDR ARWA9703005](https://openairdocs.org/sdr/ARWA9703005), Mar 13, 1997: RETRACT MECH. MALFUNCTIONED. SLAT/FLAP LODGE WARN CAME ON AT ROTATION AND UNABLE TO RETRACT SLATS. NORMAL FOR LANDING ON RETURN TO TJSJ. RESET SLAT ASSYMETRY BRAKES. OPERATED SLATS SEVERAL --- 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.