# Service difficulty reports: N307GB, cancelled May 8, 2015

A list on [N307GB, cancelled May 8, 2015](https://openairdocs.org/deregistered/N307GB-2015-05-08.md).

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

- [SDR ARWA20040103](https://openairdocs.org/sdr/ARWA20040103.md): Liner · damaged · Jan 19, 2004 · N307GB · Lkheed 1011385115 · Turbine Engine Air Inlet Section
  > 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 INTERNAL GEARBOX CHIP DETECTORS AND OIL FILTERS, NO EVIDENCE OF ENGINE FAILURE NOTED. ACOMPLISHED BOR
- [SDR ARWA20032101](https://openairdocs.org/sdr/ARWA20032101.md): Spoiler · malfunctioned · Dec 6, 2003 · N307GB · Lkheed 1011385115 · Drag Control Actuator
  > 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.md): Socket · malfunctioned · Dec 5, 2003 · N307GB · Lkheed 1011385115 · Engine Ignition Analyzer System
  > 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 NORMAL IAW MM 71-00-20. AIRCRAFT RETURNED TO SERVICE.
- [SDR ARWA20030911](https://openairdocs.org/sdr/ARWA20030911.md): Drain Line · leaking · Sep 15, 2003 · N307GB · Lkheed 1011385115 · Hydraulic System, Auxiliary
  > 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 NORMAL, NO LEAKS NOTED.
- [SDR ARWA20030406](https://openairdocs.org/sdr/ARWA20030406.md): Sensor · failed · Apr 28, 2003 · N307GB · Lkheed 1011385115 · Speed-Attitude Correction System
  > 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 FUEL 1508Z-1520Z DOWN TO LANDING WEIGHT. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK SENSOR IAW
- [SDR ARWA20030405](https://openairdocs.org/sdr/ARWA20030405.md): Access Panel · leaking · Apr 27, 2003 · N307GB · Lkheed 1011385115 · Hydraulic Compartment Doors
  > 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 UNLOCK ACTUATOR ACCESS. AIRCRAFT WILL HOLD PRESSURATION OK FOR SERVICE IAW MM # 21-31-00, PAGE 1
- [SDR ARWA20030311](https://openairdocs.org/sdr/ARWA20030311.md): Connector · loose · Mar 18, 2003 · N307GB · Lkheed 1011385115 · Hydraulic System, Main
  > 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 29-11-00. OPERATIONAL CHECK ON GROUND NORMAL.
- [SDR ARWA20030107](https://openairdocs.org/sdr/ARWA20030107.md): Actuator · failed · Jan 30, 2003 · N307GB · Lkheed 1011385115 · Landing Gear Door Actuator
  > AFTER TAKEOFF RED INTRANSIT LIGHT ILLUMINATED. ALSO PERFORMED CHECKLIST, NO CHANGE. RETURNED TO MIAMI. REMOVED AND REPLACED RT TURN LANDING GEAR DOOR LOCK ACTUATOR IAW MM 32-33-08. ADJUSTED ROD ASSEMBLY IAW MM 32-12-05 SYSTEM TESTED NORMAL.
- [SDR ARWA20030109](https://openairdocs.org/sdr/ARWA20030109.md): Proximity Sensor · failed · Jan 30, 2003 · N307GB · Lkheed 1011385115 · Landing Gear Position and Warning
  > 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 VIBRATION. RETURNED TO MIA. REMOVED AND REPLACED PROX SWITCH CARD J-7. PERFORMED MAIN LANDING GEAR R
- [SDR ARWA20030104](https://openairdocs.org/sdr/ARWA20030104.md): Engine · vibration · Jan 22, 2003 · N307GB · Lkheed 1011385115 · Engine (Turbine/Turboprop)
  > 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 IAW MM 72-31-01. REMOVED AND REPLACED VIBRATION MONITOR IAW MM 77-31-00. COMPLETED TRIM BALANCE CH
- [SDR ARWA20030103](https://openairdocs.org/sdr/ARWA20030103.md): Blade · damaged · Jan 19, 2003 · N307GB · Lkheed 1011385115 · Turbine Section
  > 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 INTERNAL GEAR-BOX MAGNETIC CHIP DETECTOR AND OIL FILTERS IAW MM. NO EVIDENCE OF INTERNAL FAILU
- [SDR ARWA20021110](https://openairdocs.org/sdr/ARWA20021110.md): Module · failed · Nov 23, 2002 · N307GB · Lkheed 1011385115 · Hydraulic System, Main
  > 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.md): Indicator · faulty · Apr 14, 2002 · N307GB · Lkheed 1011385115 · Engine Pressure Ratio (EPR)
  > 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.md): Fuel Cap · missing · Nov 23, 2001 · N307GB · Lkheed 1011385115 · Fuel Storage
  > 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 10,000 LBS FUEL JETTISON TO REDUCE LANDING WEIGHT. AIRCRAFT RETURNED TO TTPP AND LANDED WITHOUT INCI
- [SDR ARWA0010713](https://openairdocs.org/sdr/ARWA0010713.md): Floorbeam · corroded · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 FOUND OUT OF LIMITS IAW SRM 51-21-01. INSTALLED FLOORBEAM REPAIRED IAW SRM 53-21-00 FIG 815.
- [SDR ARWA0010712](https://openairdocs.org/sdr/ARWA0010712.md): Floorbeam · corroded · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 OUT OF LIMITS AS PER 51-21-01. INSTALLED FLOORBEAM REPAIR ON FS 251 IAW SRM 53-21-00 FIG 815.
- [SDR ARWA0010711](https://openairdocs.org/sdr/ARWA0010711.md): Support · corroded · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 BL 22L TO BL 22R IAW SRM 51-21-01. FOUND OUT OF LIMITS IAW SRM 51-21-01. INSTALLED FLOORBEAM REP
- [SDR ARWA0010709](https://openairdocs.org/sdr/ARWA0010709.md): Floor Panel · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Aircraft Structures
  > 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: REMOVED AND REPLACED FLOOR PANEL STA260 TO 280 AT LBL 30 IAW SRM 51-40-01.
- [SDR ARWA0010708](https://openairdocs.org/sdr/ARWA0010708.md): Floorbeam · corroded · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 SRM 51-21-01, FOUND OUT OF LIMITS IAW SRM 51-21-01, INSTALLED FLOORBEAM REPAIR IAW SRM 53-21-00 FIG 8
- [SDR ARWA0010714](https://openairdocs.org/sdr/ARWA0010714.md): Bracket · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Aircraft Structures
  > DURING SCHEDULE MAINTENANCE. N/R 633. DISCREPANCY: EVIDENCE OF CORROSION, RIGHT WING TO FUSELAGE BRACKET AT WHEEL WELL. CORRECTIVE ACTION: REMOVED CORROSION, FILLED AREA WITH DEVCON, FABRICATED -11 DOUBLER AND INSTALLED WITH HILOCKS. PRIMED + PAINTED AS REQUIR
- [SDR ARWA0010701](https://openairdocs.org/sdr/ARWA0010701.md): Panel · cracked · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Horizontal Stabilizer, Plate/Skin
  > 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 STABILIZER L/E IAW DRAWING AS 11269.
- [SDR ARWA0010707](https://openairdocs.org/sdr/ARWA0010707.md): Fitting · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Aircraft Structures
  > DURING SCHEDULE MAINTENANCE. N/R 493. DISCREPANCY: C2 CARGO DOOR CUT-OUT, CENTER UPPER DOOR SILL PIVOT CLEVIS ATTACH FITTING IS CRACKED. CORRECTIVE ACTION: REMOVED FASTENERS C2 CARGO DOOR CENTER UPPER DOOR SILL PIVOT FITTING, CLEAN SURFACE CORROSION IAW SRM 51
- [SDR ARWA0010706](https://openairdocs.org/sdr/ARWA0010706.md): Splice · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Aircraft Structures
  > DURING SCHEDULE MAINTENANCE. N/R 235. DISCREPANCY: SPLICE CRACKED AT FS 1203 BELOW WL200. CORRECTIVE ACTION: REMOVED CRACKED SPLICE & REPLACED WITH NEW ONE IAW SRM 51-40-01.
- [SDR ARWA0010705](https://openairdocs.org/sdr/ARWA0010705.md): Splice · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Aircraft Structures
  > 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.md): Floor Support · cracked · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 10 & 11 IAW SRM 51-40-4.
- [SDR ARWA0010703](https://openairdocs.org/sdr/ARWA0010703.md): Frame · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, 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. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT BULKHEAD FRAME STA 449. INSTALLED REPAIR ANGLES + DOUBLERS A
- [SDR ARWA0010702](https://openairdocs.org/sdr/ARWA0010702.md): Frame · cracked · Jun 29, 2001 · N307GB · Lkheed 1011385115 · Fuselage Main, Frame
  > 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 AND TRIMMED REPAIR ANGLES, DRILLED, PRIMED PAINTED AND PREPPED AREA. INSTALLED PARTS AND INSTALLED
- [SDR ARWA990305](https://openairdocs.org/sdr/ARWA990305.md): Engine · failed · Mar 18, 1999 · N307GB · Lkheed 1011385115 · Engine (Turbine/Turboprop)
  > 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 VIBRATION METER WENT OT 1 UNIT. AFTER PHONE PATH WITH FLIGHT CONTROL, THE FLIGHT WAS DIVERTED TO SJU. TH
- [SDR ARWA981019](https://openairdocs.org/sdr/ARWA981019.md): Actuator · inop · Oct 19, 1998 · N307GB · Lkheed 10113851 · Leading Edge Slat Actuator
  > 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 DEGREE EXTENSION WITH SLAT UP. AFTER LANDING L/E TRANS LIGHT EXTINGUISHED WHEN FLAPS RETRACTED. RE
- [SDR ARWA981018](https://openairdocs.org/sdr/ARWA981018.md): Comparator · dirty · Oct 16, 1998 · N307GB · Lkheed 10113851 · Leading Edge Slat Position Indicating System
  > 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. CLEANED AND RESEATED THE SLAT ASYMMETRY COMPARATOR. ALSO, CHECKED BOTH SLAT ASYMMETRY BRAKE TRANSDUCE
- [SDR ARWA980797](https://openairdocs.org/sdr/ARWA980797.md): Amplifier · failed · Jul 10, 1998 · N307GB · Lkheed 1011385115 · Fuel Control/Turbine Engines
  > 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. CORRECTED BOTH N1 AND N2. REMOVED AND REPLACED NR 3 ENGINE SPEED CONTROL AMPLIFIER, OPS CHECKED ENGINE
- [SDR ARWA980601](https://openairdocs.org/sdr/ARWA980601.md): Connector · loose · Jun 9, 1998 · N307GB · Lkheed 10113851 · Leading Edge Slat Position Indicating System
  > 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 TO BLOCKS. FOUND LOOSE CANNON PLUG IN RT NR 7 SLAT ASYMMETRY BRAKE COMPARTMENT. CLEANED AND SECUR
- [SDR ARWA980505](https://openairdocs.org/sdr/ARWA980505.md): Boost Pump · shorted · May 14, 1998 · N307GB · Lkheed 1011385115 · Fuel Boost Pump
  > 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 LEFT FUEL BOOST PUMP. FURTHER INVESTIGATION REVEALED BURNED ELECTRICAL CONNECTORS HOLES IN THE P
- [SDR ARWA980402](https://openairdocs.org/sdr/ARWA980402.md): Aoa Sensor · malfunctioned · Apr 2, 1998 · N307GB · Lkheed 1011385115 · Stall Warning System
  > WINDSHEAR WARNING COMES ON SHORTLY AFTER TAKEOFF AND AT APPROX 1.000 DURING LANDING APPROACH. REMOVED AND REPLACED AOA SENSORS. REMOVED AND REPLACED LONGITUDINAL ACCELEROMETERS. OPS CHECK NORMAL AS PER MM 34-62-00 AND WINDSHEAR 060-4033. (M)
- [SDR ARWA980401](https://openairdocs.org/sdr/ARWA980401.md): Inu · inoperative · Mar 31, 1998 · N307GB · Lkheed 1011385115 · Inertial Guidance System
  > 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. DURING CLIMBOUT L 5, 6 AND R 5, 6 SPOILER AND ROLL SPOILER LIGHT ON, PUSH LIGHT ON. REMOVED AN
- [SDR ARWA980307](https://openairdocs.org/sdr/ARWA980307.md): Monitor · inoperative · Mar 24, 1998 · N307GB · Lkheed 1011385115 · Engine Vibration Analyzer
  > 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 NR 5 SPOILER ON DMI 2. REMOVED AND REPLACED VIBRATION MONITOR AND PERFORMED ENGINE RUN UP AND TES
- [SDR ARWA970603](https://openairdocs.org/sdr/ARWA970603.md): Engine · flamed out · Jun 16, 1997 · N307GB · Lkheed 1011385115 · Engine (Turbine/Turboprop)
  > 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. FLIGHT DIVERTED TO RBR AND LANDED WITHOUT INCIDENT. CAUSE OF FLAME-OUT IS UNDER INVESTIGATION. (X)
- [SDR ARW970603](https://openairdocs.org/sdr/ARW970603.md): Gearbox · failed · Jun 16, 1997 · N307GB · Lkheed 1011385115 · Turbine Engine Accessory Drive
  > 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 LANDED WITHOUT INCIDENT. TROUBLESHOOTING NOTED GEARBOX FAILURE. REMOVED AND REPLACED NR 1 ENG
- [SDR ARWA9703005](https://openairdocs.org/sdr/ARWA9703005.md): Retract Mech · malfunctioned · Mar 13, 1997 · N307GB · Lkheed 1011385115 · Leading Edge Slat Control System
  > 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 TIMES PER M/M 27-81-00. CHECK OK ON GROUND.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N307GB' AND deregistration_id = 'N307GB-2015-05-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N307GB-2015-05-08/reports

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