# Service difficulty reports: N130G, cancelled Dec 10, 2003 A list on [N130G, cancelled Dec 10, 2003](https://openairdocs.org/deregistered/N130G-2003-12-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 55 reports - [SDR SWIA972584](https://openairdocs.org/sdr/SWIA972584.md): Computer · malfunctioned · May 17, 2001 · N130G · Emb EMB120RT · Integrated Flight System > WHEN AUTOPILOT IS ENGAGED ON CAPTAINS SIDE, THE YOKE AND AIRCRAFT OSCILLATE ON ROLL AXIS CONTINUOUSLY. YOKE ROLLS ABOUT 2 INCHES TRAVEL. REMOVED AND REPLACED NR 1 AHC85 PER MM 34-21-01. OPS CHECK GOOD PER MM 34-21-00. AUTOPILOT OPS CHECK GOOD PER MM 22-10- - [SDR SWIA972578](https://openairdocs.org/sdr/SWIA972578.md): Control Box · malfunctioned · May 16, 2001 · N130G · Emb EMB120RT · Landing Gear Selector > AFTER SELECTING GEAR UP, ALL RED AND GREEN INDICATING LIGHTS REMAINED ILLUMINATED. FOLLOWED QRH AND RECYCLED LANDING GEAR WITH SAME RESULTS. RETURNED FOR LANDING. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. REMOVED AND REPLACED LANDING GEAR CONTROL BO - [SDR SWIA972571](https://openairdocs.org/sdr/SWIA972571.md): Servo · failed · Apr 22, 2001 · N130G · Emb EMB120RT · Autopilot Main Servo > CO-PILOT''''S AUTOPILOT SERVO FAILURE, AMBER A ANNUNCIATED, VIBRATION ASSOCIATED WITH FAILURE PRIOR TO SERVO FAILURE. EXECUTED QRW PROCEDURES, VIBRATION REMAINED. REMOVED AND REPLACED AILERON SERVO, IAW MM 22-10-09, OPS CHECK GOOD. P/N 622-5734-002, S/N ON - [SDR SWIA972479](https://openairdocs.org/sdr/SWIA972479.md): Flap · malfunctioned · Mar 26, 2001 · N130G · Emb EMB120RT · Trailing Edge Flap Control System > OUTBOARD FLAPS DO NOT EXTEND PAST 35 DEGREES WHEN SELECTED TO 45 DEGREES. INSPECTED OUTBOARD FLAPS AND TRACK SYSTEM. ALL FOUND GOOD. CLEANED CONNECTORS AT BOTH LEFT AND RIGHT ACTUATORS. PERFORMED SEVERAL FUNCTIONAL CHECKS WITH NO FAULTS FOUND. - [SDR SWIA972432](https://openairdocs.org/sdr/SWIA972432.md): Control Panel · malfunctioned · Mar 9, 2001 · N130G · Emb EMB120RT · Flight Controller > WITH GEAR DOWN, FLAP 25 DEGREES, FLIGHT CONTROLS GET STUCK WHILE ATTEMPTING TO ROLL TO THE RIGHT. CHECKED AILERONS. COULD NOT DUPLICATE PROBLEM. SUSPECT AUTOPILOT DID NOT DISENGAGE. INSTALLED SERVICEABLE APP-65A. OPS CHECK GOOD AT THIS TIME. P/N: 622-66 - [SDR SWIA972316](https://openairdocs.org/sdr/SWIA972316.md): Warning Light · illuminated · Jan 28, 2001 · N130G · Emb EMB120RT · Data Recorders (Flight/Maintenance) > TRIM AURAL WARNING WITH TRIM IN GREEN BAND AT TAKEOFF. ABORTED TAKEOFF. RESET AURAL WARNING COMPUTER. RAN AIRCRAFT WITH TRIM SET TO TAKEOFF. COULD NOT DUPLICATE. CYCLED TRIM OUT OF GREEN BAND FORWARD AND AFT. TRIM AURAL WARNING CHECKS GOOD. RAN TRIM THR - [SDR SWIA972286](https://openairdocs.org/sdr/SWIA972286.md): Display · failed · Jan 18, 2001 · N130G · Emb EMB120RT · Attitude Gyro and Indicating System > JUST AFTER ROTATION FIRST OFFICERS EADI FAILED. RETURNED TO SEA. INSTALLED SERVICEABLE RIGHT EADI. OPS CHECKS GOOD 34-23-01. S/N ON: 893, S/N OFF: 2674. - [SDR SWIA972009](https://openairdocs.org/sdr/SWIA972009.md): Light · illuminated · Oct 1, 2000 · N130G · Emb EMB120RT · Fuel Pressure Indicating > ABORTED TAKEOFF AT 90 - 100 KNOTS DUE TO FUEL LIGHT ON MAIN ANNUNCIATOR PANEL. DUE TO ABORT COULDN''T TELL WHICH SIDE HAD LOW FUEL PRESSURE. FOUND THE LEFT FUEL FILTER LIGHT WAS ILLUMINATING. REMOVED AND REPLACED LEFT LOW PRESS FUEL FILTER IAW MM 73-00-00. - [SDR SWIA971990](https://openairdocs.org/sdr/SWIA971990.md): Fcu · failed · Sep 22, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control System > OUTBOARD PAIR OF FLAPS DID NOT EXTEND BEYOND 25 DEGREES TO 45 DEGREES (LAST 2 SEGMENTS) WHEN COMMANDED. DIVERTED TO RDD FROM CEC. RERACKED FLAP CONTROL UNIT. OPS CHECKS GOOD. - [SDR SWIA971964](https://openairdocs.org/sdr/SWIA971964.md): Altimeter · malfunctioned · Sep 7, 2000 · N130G · Emb EMB120RT · Altimeter, Barometric/Encoder > AT 2000 FT ON CAPTAINS ALTIMETER, FIRST OFFICERS ALTIMETER READS 2100 FT. AT 5000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS READS 5200 FT, AT 8000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS ALTIMETER READS 8250 FT AND AT 14000 FT FIRST OFFICERS READS 14300 FT. TR - [SDR SWIA971925](https://openairdocs.org/sdr/SWIA971925.md): Sequence Valve · out of adj · Aug 7, 2000 · N130G · Emb EMB120RT · Landing Gear Door Retract Section > AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT. RETURNED TO PDX. FOUND RIGHT GEAR DOOR SEQUENCE VALVE OUT OF ADJUSTMENT. ADJUSTED PER MM 32-32-04. PERFORMED MULTIPLE GEAR SWINGS. OPS CHECKS GOOD. - [SDR SWIA971710](https://openairdocs.org/sdr/SWIA971710.md): Dpu · failed · Feb 25, 2000 · N130G · Emb EMB120RT · Integrated Flight System > CO-PILOT EHSI WENT BLANK IN FLIGHT. COULD NOT TRANSFER ANY NAVIGATION INFORMATION TO SCREEN. RETURN TO LAX, INSTALLED SERVICEABLE DPU 864 ON NR 2 SIDE. OPS CK GOOD, SN: 7059, SN OFF: 4381. - [SDR SWIA971646](https://openairdocs.org/sdr/SWIA971646.md): Control Unit · malfunctioned · Jan 4, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control System > ON CLIMB-OUT, CONTROL FAULT APPEARED WITH FLAP HANDLE UP, OVERHEAD FLAP CONTROL PANEL INDICATED NAC WAS FULLY EXTENDED. CONTROL FAULT INITIALLY WOULD NOT RESET, RESET SUCCESSFUL PER QRH 3RD TRY. RETURNED TO PDX. REPLACED FLAP CONTROL UNIT IAW 270000 AND CLE - [SDR SWIA971643](https://openairdocs.org/sdr/SWIA971643.md): Controller · malfunctioned · Jan 3, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control System > CONTROL FAULT ILLUMINATED IN FLIGHT AND WOULD NOT CANCEL. FAULT CORRECTED ITSELF AFTER 5 MINUTES. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST PER MM 275000. FUNCTIONAL TEST GOOD, NO DISCREPENCIES NOTED. UNABLE TO DUPLICATE PROBLEM. - [SDR SWIA971278](https://openairdocs.org/sdr/SWIA971278.md): Oil Syst · reqd service · Oct 8, 1998 · N130G · Emb EMB120RT · Turbine Engine Oil System > OIL PRESSURE 1 WARNING AT V1 AND INTERMITTENT PRESSURE DROPS DURING CLIMBOUT. RETURNED TO AIRPORT. VISUALLY INSPECTED LEFT ENGINE AND NO OIL LEAKS EVIDENT. INSPECTED FILTER BY PASS AND CHIP DETECTOR LIGHTS, CHECKS NORMAL. SERVICED ENGINE WITH 2 QUARTS EXXO - [SDR SWIA971235](https://openairdocs.org/sdr/SWIA971235.md): Ahrs · out of adjust · Aug 3, 1998 · N130G · Emb EMB120RT · Integrated Flight System > RECEIVED HEADING FLAG, RMI FLAG BOTH SIDES WITH GYRO PRECESSING ALL THE TIME INFLIGHT. RETURNED TO LAX. RE-ORIENTED NR 1 AND NR 2 AHRS IAW MM 34-00-00. OPERATED SYSTEM ON GROUND AND ALL CHECKS OK. - [SDR COMA9810050](https://openairdocs.org/sdr/COMA9810050.md): Wheel · cracked · Feb 26, 1998 · N130G · Emb EMB120RT · Wheel/Ski/Float > MECHANIC REMOVED WHEEL ASSEMBLY FROM A/C DUE TO TIRE WAS FOUND FLAT. WHEEL SHOP INFLATED TIRE AND FOUND INBOARD HALF CRACKED AT BOTTOM OF KEY INSERT BOSS. WHEEL HALF (P/N 300-604-1) HAS BEEN REMOVED FROM SERVICE. - [SDR COMA9710500](https://openairdocs.org/sdr/COMA9710500.md): Acm · failed · Dec 19, 1997 · N130G · Emb EMB120RT · Cabin Cooling System > LAV SMOKE DETECTOR ACTIVATED. CABIN FILLED WITH SMOKE. REPLACED THE LEFT AIR CYCLE MACHINE. - [SDR COMA9710499](https://openairdocs.org/sdr/COMA9710499.md): Sign · loose · Dec 17, 1997 · N130G · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT SIGN AT ROW 5C IS LOOSE. REPLACED SIGN ASSY. - [SDR COMA9710476](https://openairdocs.org/sdr/COMA9710476.md): Sign · broken · Nov 16, 1997 · N130G · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT SIGN AT 5C BROKEN. REPLACED EXIT SIGN. - [SDR COMA9710244](https://openairdocs.org/sdr/COMA9710244.md): Safety Pin · not removed · May 6, 1997 · N130G · Emb EMB120RT · Landing Gear Retraction/Extension System > THE RT MLG WOULD NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM LANDING GEAR. - [SDR COMA9710240](https://openairdocs.org/sdr/COMA9710240.md): Flap Warning · illuminated · May 3, 1997 · N130G · Emb EMB120RT · Trailing Flap Position Indicating System > FLAPS FAIL WARNING DURING TAKEOFF ROLL. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS. COULD NOT DUPLICATE DISCREPANCY. - [SDR COMA9710174](https://openairdocs.org/sdr/COMA9710174.md): Lead · broken · Mar 13, 1997 · N130G · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System > RT PROPELLER DE-ICE SYSTEM INOP. REPLACED DEFECTIVE ELECTRICAL LEAD ON RT PROPELLER. - [SDR COMA9710159](https://openairdocs.org/sdr/COMA9710159.md): Door · not latched · Feb 25, 1997 · N130G · Emb EMB120RT · Fluid Service Doors > SERVICE DOOR WARNING DURING TAKEOFF. FOUND THE FUEL SINGLE POINT SERVICE DOOR UNLATCHED. SECURED DOOR LATCHES AND AIRCRAFT CONTINUED SERVICE. - [SDR COMA9710155](https://openairdocs.org/sdr/COMA9710155.md): Control · malfunctioned · Feb 19, 1997 · N130G · Emb EMB120RT · Landing Gear Position and Warning > NLG GREEN LIGHTS ARE INTERMITTENT. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR CONTROL FOR TROUBLESHOOTING. - [SDR COMA9710095](https://openairdocs.org/sdr/COMA9710095.md): Pitchlock Screw · bent · Jan 28, 1997 · N130G · Emb EMB120RT · Propeller Controlling System > ACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR PROPELLER FEATHERING PROBLEMS. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0159 WAS FOUND TO BE BENT APPROXIMATELY 0.25 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PA - [SDR COMA9710017](https://openairdocs.org/sdr/COMA9710017.md): Test Switch · sticks · Jan 2, 1997 · N130G · Emb EMB120RT · Stall Warning System > COPILOTS STALL WARNING SYSTEM ACTIVATES PERIODICALLY. TEST BUTTON IS STICKING. REPLACED THE STALL WARNING TEST PANEL. - [SDR COMA9610406](https://openairdocs.org/sdr/COMA9610406.md): Control Unit · malfunction · Dec 17, 1996 · N130G · Emb EMB120RT · Landing Gear Retraction/Extension System > AFTER TAKEOFF, WHEN LANDING GEAR SELECTED UP, THE LT MLG INDICATED DOWN. CYCLED GEAR CONTROL WITH SAME RESULTS. ELECTRICAL OVERRIDE PROCEDURE WAS USED TO EXTEND LANDING GEAR FOR LANDING. REPLACED THE LANDING GEAR CONTROL ASSY. - [SDR COMA9610394](https://openairdocs.org/sdr/COMA9610394.md): Annunciator · malfunctioned · Dec 11, 1996 · N130G · Emb EMB120RT · Trailing Flap Position Indicating System > REPEATED FLAP CONTROL FAULT WARNINGS DURING FLIGHT. REPLACED THE FLAP ANNUCIATOR UNIT. - [SDR COMA9610289](https://openairdocs.org/sdr/COMA9610289.md): Seals · worn · Sep 26, 1996 · N130G · Emb EMB120RT · Propeller Controlling System > LEFT PROPELLER IS SLOW TO FEATHER OR UNFEATHER. REPLACED PROPELLER TRANSFER TUBE SEALS. - [SDR COMA9610216](https://openairdocs.org/sdr/COMA9610216.md): Floor Beam · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN LEFT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04. - [SDR COMA9610215](https://openairdocs.org/sdr/COMA9610215.md): Floor Beam · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN RIGHT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04. - [SDR COMA9610214](https://openairdocs.org/sdr/COMA9610214.md): Butt Strap · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, SEVERAL RIVETS WERE FOUND LOOSE OR WITH CORROSION AT ENTRY FLOOR, LT BUTT STRAP. REMOVED AND REPLACED WITH ORIGINAL TYPE AND SIZE RIVETS, 19 TOTAL PER EMB 120 SRM CHAPTER 51. - [SDR COMA9610213](https://openairdocs.org/sdr/COMA9610213.md): Cross Beam · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND PASSENGER FLOOR SUPPORT CROSSBEAM T-SECTION CORRODED AT FUSELAGE FRAME 16. REMOVED CORRODED T-SECTION, LOCATED, DRILLED AND INSTALLED NEW PART PER EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9610212](https://openairdocs.org/sdr/COMA9610212.md): Support Section · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND PASSENGER SEAT LEFT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE. - [SDR COMA9610211](https://openairdocs.org/sdr/COMA9610211.md): Support Section · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND PASSENGER SEAT RIGHT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE. - [SDR COMA9610210](https://openairdocs.org/sdr/COMA9610210.md): Seat Track · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > DURING 2C INSPECTION, FOUND SEAT TRACKS FOR RIGHT HAND SIDE PASSENGERS SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS. - [SDR COMA9610209](https://openairdocs.org/sdr/COMA9610209.md): Stringer · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04. - [SDR COMA9610208](https://openairdocs.org/sdr/COMA9610208.md): Butt Strap · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND BUTT STRAPS TO HAVE SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER EMB M/M 51-21-04. - [SDR COMA9610207](https://openairdocs.org/sdr/COMA9610207.md): Bolt · rusted · Jun 15, 1996 · N130G · Emb EMB120RT · Battery Box Structure > DURING 2C INSPECTION, FOUND FORWARD INBOARD CORNER OF BATTERY COMPARTMENT AT FRAME 4 TO HAVE SIGNS OF CORROSION. FURTHER INSPECTION FOUND NOSE GEAR FORWARD DOOR, AFT HINGE, HARDWARE TO BE CORRODED. REPLACED HARDWARE AND CLEANED BATTERY COMPARTMENT. - [SDR COMA9610206](https://openairdocs.org/sdr/COMA9610206.md): Track · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > DURING 2C INSPECTION, FOUND GALLEY FLOOR ATTACHMENT TRACK TO BE CORRODED. REMOVED CORRODED TRACK AND REPLACED WITH A SERVICEABLE TRACK. - [SDR COMA9610205](https://openairdocs.org/sdr/COMA9610205.md): Floor Beam · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C INSPECTION, FOUND SURFACE CORROSION ON FLOOR BEAM THAT GALLEY FLOOR ATTACHMENT TRACK MOUNTS TO. REMOVED SURFACE CORROSION TREATED AREA AND PAINTED TO SERVICEABLE CONDITION. - [SDR COMA9610204](https://openairdocs.org/sdr/COMA9610204.md): Seat Track · corroded · Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > DURING 2C INSPECTION, FOUND SEAT TRACKS FOR LEFT HAND SIDE PASSENGER SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS. - [SDR COMA9610177](https://openairdocs.org/sdr/COMA9610177.md): Bolt · broken · Jun 11, 1996 · N130G · Emb EMB120RT · Wheel/Ski/Float > ON PREFLIGHT INSPECTION, MECHANIC NOTICED TWO BOLTS MISSING FROM THE RIGHT MAIN INBOARD WHEEL ASSEMBLY. BOLTS ARE PRESUMED TO HAVE BROKEN AND FALLEN OUT. WHEEL/TIRE ASSEMBLY WAS REMOVED AND REPLACED. - [SDR COMA9610106](https://openairdocs.org/sdr/COMA9610106.md): Roller · worn · Mar 18, 1996 · N130G · Emb EMB120RT · Cargo/Baggage Doors > CARGO DOOR WILL NOT OPEN. FORWARD LOWER ROLLER CAME OUT OF THE TRACK. REPLACED DOOR ROLLER, OPERATES NORMAL. - [SDR COMA9610050](https://openairdocs.org/sdr/COMA9610050.md): Bolt · missing · Jan 31, 1996 · N130G · Emb EMB120RT · Landing Gear Doors > LEFT MLG INTRANSIT INDICATOR REMAINED ON AFTER LANDING GEAR RETRACTED. REPLACED MISSING BOLT ON INBOARD FORWARD GEAR DOOR LATCH HANDLE. ACFT RETURNED TO SERVICE. - [SDR COMA9511998](https://openairdocs.org/sdr/COMA9511998.md): Fcu · defective · Nov 9, 1995 · N130G · Emb EMB120RT · Fuel Control/Turbine Engines > LEFT ENGINE WILL NOT START. REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. - [SDR COMA9511988](https://openairdocs.org/sdr/COMA9511988.md): Latch Assy · broken · Oct 23, 1995 · N130G · Emb EMB120RT · Landing Gear Door Retract Section > THE LEFT MAIN LANDING GEAR DID NOT RETRACT. REPLACED A BROKEN LANDING GEAR DOOR LATCH ASSEMBLY. - [SDR COMA9511989](https://openairdocs.org/sdr/COMA9511989.md): Antenna · defective · Oct 19, 1995 · N130G · Emb EMB120RT · Weather Radar System > RADAR CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPLACED THE RADAR ANTENNA. - [SDR COMA9511983](https://openairdocs.org/sdr/COMA9511983.md): Transponder · defective · Oct 16, 1995 · N130G · Emb EMB120RT · ATC Transponder System > NR 2 TRANSPONDER INOPERATIVE. REPLACED THE NR 2 TRANSPONDER. Next page: https://openairdocs.org/deregistered/N130G-2003-12-10/reports.md?page=2 ## 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 = 'N130G' AND deregistration_id = 'N130G-2003-12-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N130G-2003-12-10/reports --- 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.