Embraer EMB-120ER

Service difficulty reports · 8,287

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duckdb -csv -c "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 aircraft_model_key = 'EMB120ER'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA02IA089Hose · puncturedBPT- DURING FLIGHT 3636 APPROACH, THE CREW NOTED THAT THE #2 ENGINE OIL PRESSURE INDICATED LOW IN FLIGHT. THE PILOT FEATHERED THE #2 PROP, AND LANDED WITHOUT INCIDENT. BPT- MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE OIL COOLER INLET HOSE, SERVICED THE Apr 8, 2002 · N16731 · Emb EMB120ER · Engine Oil PressureSDR SWIA200210771Connector · dirtyANTISKID INOP MESSAGE ON LEFT SIDE ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED CANNON PLUGS AT ANTISKID HARNESS AND SWAPPED RIGHT SIDE TRANSDUCERS INBOARD TO OUTBOARD TRANSDUCERS. GROUND OPS CHECKS GOOD.Apr 8, 2002 · N251YV · Emb EMB120ER · Brake Anti-Skid SectionSDR C2XA02IA086Control Unit · failedFLIGHT 3583 IAH TO VCT -A- INDICATION CB POPPED FOR LANDING GEAR. RESET UNSUCCESSFUL, QRH UNSUCCESSFUL. RECYCLED GEAR, IT WOULD NOT COME UP OR DOWN, B SYSTEM INDICATES DOWN AND LOCKED, THE AIRCRAFT LANDED AT VCT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPApr 7, 2002 · N58733 · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200210782Indicator · faultyNR 1 ENGINE NH GAUGE (ANALOG & DIGITAL), INOP DURING FLIGHT. NL WAS OK. RETURNED TO PDX. LEFT ANALOG AND DIGITAL PORTION OF NH GAUGE READ EITHER -0- OR ERRATIC. NL WORKS FINE. REPLACED WIRE HARNESS 3115911-01 ON LEFT ENGINE. RAN ENGINES FOR OPS CHECK. OApr 5, 2002 · N295SW · Emb EMB120ER · Engine RPM Indicating SystemSDR SWIA200210776Battery Pack · dischargedFRONT HALF OF EMERGENCY LIGHTS ON FLOOR AND CEILING WILL NOT TEST OR TURN ON. REPLACED FORWARD EMERGENCY EXIT LIGHT BATTERY PACK.Apr 5, 2002 · N294SW · Emb EMB120ER · Emergency LightingSDR SWIA200210774Pump · malfunctionedRIGHT ENGINE SLUGGISH IN ACCELERATION. T6 WAS ABOUT 820 DEGREES USING TORQUE SETTINGS SUPPLIED ON THE RELEASE. REMOVED AND REPLACED RIGHT ENGINE FUEL PUMP AND HMU IAW MM 73-21-00. RUN CHECKS AND LEAK CHECKS GOOD. HMU: P/N: 786390-10, S/N OFF: F1829.Apr 5, 2002 · N268UE · Emb EMB120ER · Engine Fuel PumpSDR SWIA200210778Door Seal · looseON CLIMBOUT LOST CABIN PRESSURIZATION FOR ABOUT 1 MINUTE, THEN THE SYSTEM BEGAN WORKING NORMALLY AGAIN IN MANUAL AND AUTO MODE. RETURNED TO LAX. SECURED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT TO 7 PSID. OPS CHECK GOOD. NO DISCREPANCIES NOTED.Apr 4, 2002 · N562SW · Emb EMB120ER · Cargo/Baggage DoorsSDR SWIA200210775Actuator · failedUPON FLAP EXTENSION TO 15 DEGREES ON APPROACH TO OXR, BLUE SYSTEM HYDRAULIC FAILURE OCCURRED. FOLLOWED QRH. RETURNED TO LAX. REPLACED RIGHT NACELLE FLAP ACTUATOR PER MM 27-50-00. REPLACED RIGHT ENGINE HYDRAULIC PUMP. RUNUP AND OPS CHECK AND LEAK CHECK GOOApr 4, 2002 · N291SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR ASOA02205Battery · malfunctionedDURING GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THAT WHEN HER EMERGENCY LIGHT SWITCH WAS IN THE CLOSED POSITION THE EMERGENCY LIGHT CIRCUIT BREAKER WOULD POP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY IN THE NR 2 POSITION.Apr 3, 2002 · N267AS · Emb EMB120ER · Emergency LightingSDR SWIA200210777Warning System · malfunctionedDURING TAKEOFF ROLL, RECEIVED A HIGH SPEED TRIPLE CHIME AND AURAL WARNING. ABORTED TAKEOFF. CYCLED CIRCUIT BREAKER. GROUND OPS CHECK GOOD.Apr 3, 2002 · N271YV · Emb EMB120ER · Central WarningSDR SWIA200210770Oil System · lowAFTER TAKEOFF, AT ABOUT 1500 AGL, THE LEFT ENGINE OIL AURAL WARNING CAME ON. CONCURRENTLY HEARD RCCB'S CLICKING AND THE OIL NEEDLE FLUCTUATED. RETURNED TO DEN. ADDED 4 QUARTS OF OIL AND COMPLIED WITH ST72-344. NO DEFECTS NOTED. LEAK CHECK GOOD.Apr 2, 2002 · N298SW · Emb EMB120ER · Turbine Engine Oil SystemSDR ASOA02233Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP IN THE CARGO AREA BETWEEN FRAMES 40 AND 44 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM'S 51-40-02 AND 51-25-00. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Main, StructureSDR ASOA02232Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT BUTT STRAP BETWEEN FRAMES 20 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-40-02, 51-40-00, AND 51-21-02. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Main, StructureSDR ASOA02231Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT HAND SILL PLATE IN SPOTS BETWEEN FRAMES 29 AND 34. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRM'S 51-40-02, 51-40-02, 51-40-05, AND 51-20-02. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02230Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT SEAT TRACK SILL PLATE FLANGE WAS FOUND CORRODED BEYOND LIMITS AT FRAMES 17, 19 AND 22. WHILE REPAIRING THE SILL PLATE (P/N 120-05803-01) THE RIGHT OUTBOARD CROSSBEAM (P/N 12004149-002) AT FRAME 16 WAS ALSO FOUND CORApr 1, 2002 · N261AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02229Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT SECTION OF THE RIGHT WALL SEAT TRACK WAS CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE REMOVED THE CORRODED SEAT TRACK, FABRICATED A NEW ONE AND INSALLED IAW SRMS 51-40-02, 51-25-00, 51-21-02, 51-21-05 AND 51-10-00. Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02228Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE AFT SECTION OF THE LEFT FLOOR SEAT TRACK WAS CORRODED BETWEEN FRAMES 32 AND 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SEAT TRACK IAW SRMS 51-25-00 AND 51-21-02 AND AMM 53-01-05. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02227Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE COCKPIT RIGHT HAND OUTBOARD FLOOR SILL PLATE WAS CORRODED BETWEEN FRAMES 7 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-00, AND 51-40-02. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02226Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS FOUND CORRODED AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRMS 51-25-00, 51-21-03 AND 51-40-02. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02225Support · corrodedDURING C-CHECK INSPECTION IN BNA, THE COCKPIT STEP AREA FLOOR FLANGE, FORWARD LEFT CORNER WAS FOUND CORRODED AND BENT WITH SOME RIVETS THAT WERE PULLED THROUGH. MAINTENANCE RETURNED THE STEP SUPPORT TO ITS ORIGINAL CONTOUR AND REMOVED AND REPLACED THE PULLED Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02224Floor Support · corrodedDURING C-CHECK INSPECTION IN BNA, THE FLOORBOARD SUPPORT ANGLE WAS FOUND CORRODED AT FRAME 13. MAINTENANCE REPAIRED THE CORRODED SECTION OF THE FLOORBOARD SUPPORT ANGLE IN ACCORDANCE WITH SRMS 51-21-04, 51-21-05, 51-21-06, AND 51-40-02. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02223Stringer · corrodedDUIRNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 18 LEFT BETWEEN FRAMES 16 AND 18. MAINTENANCE REMOVED THE CORRODED SECTION OF THE STRINGER AND REPLACED IT WITH A SPLICE IAW SRMS 51-25-00, 51-40-02 AND 51-40-05. (M)Apr 1, 2002 · N261AS · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR SWIA200210767Eec · malfunctionedRIGHT EEC FAILURE ON TAKEOFF, ABORTED TAKEOFF. REMOVED AND INSTALLED SERVICEABLE RIGHT EEC IAW MM 73-22-00. REPLACED RIGHT ENGINE NP SENSOR WITH SERVICEABLE UNIT. LEAK CHECK ON ENGINE NP SENSOR CHECKS GOOD. NO LEAKS NOTED AT THIS TIME. RAN RIGHT ENGINE, EApr 1, 2002 · N293SW · Emb EMB120ER · Fuel Control/Turbine EnginesSDR SWIA200210768Autopilot Sys · malfunctionedJUST AFTER ROTATION, TRIPLE CHIME AUTOPILOT WITH ASSOCIATED AUTOPILOT FAIL RED MAP INDICATION AND TRIPLE CHIME TRIM FAIL WITH ASSOCIATED TRIM FAIL MAP LIGHT. RAN QRH, RETURNED TO PSP. COMMAND BARS ON CAPTAIN'S SIDE STUCK 15 DEGREES DOWN AND 30 DEGREES RIGHT.Mar 31, 2002 · N218SW · Emb EMB120ER · Autopilot SystemSDR ASOA02199Fuse · blownDURING A HANGAR INSPECTION IN MCN, THE FLOOR EMERGENCY LIGHTS IN FRONT OF THE GALLEY WERE INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN THE FUSE HOLDER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 30, 2002 · N503AS · Emb EMB120ER · Emergency LightingSDR C2XA02IA082Battery · dischargedIAH- WHILE PERFORMING MAINTENANCE TROUBLE SHOOTING, THE MECHANIC NOTED THAT THE #2 EMERGENCY BATTERY CHARGE WAS LOW. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROMar 30, 2002 · N17728 · Emb EMB120ER · Emergency LightingSDR SWIA200210764Filter · dirtyGREEN HYDRAULIC FILTER LIGHT ILLUMINATED ON TAKEOFF. ALL SYSTEM INDICATORS NORMAL. RETURNED TO SFO. INSTALLED NEW HYDRAULIC RETURN FILTER ON GREEN SYSTEM. PRESSURIZED SYSTEM. OPS CHECKS GOOD.Mar 29, 2002 · N295UX · Emb EMB120ER · Hydraulic Filter, MainSDR SWIA200210763Transponder · malfunctionedAFTER TAKEOFF, TRANSPONDER NR 1 REPORTED DIAG WITH NO ASSOCIATED NUMBER. ATC REPORTED NO ALTITUDE READOUT. SWITCHED TO NR 2 TRANSPONDER AND HAD NO REPLY LIGHT OR ALT INFORMATION AS REPORTED BY ATC. RETURNED TO PDX. RERACKED NR 1 TDR94 TRANSPONDER. INSPECTMar 28, 2002 · N271YV · Emb EMB120ER · ATC Transponder SystemSDR SWIA200210761Warning System · malfunctionedABORTED TAKEOFF DUE TO TRIM AURAL WARNING. TRIM WAS IN THE GREEN RANGE AT 38 DEGREES CG. CHECKED TRIM WARNING SYSTEM. OPS CHECKS GOOD.Mar 27, 2002 · N284YV · Emb EMB120ER · Central WarningSDR SWIA200210760Battery Pack · dischargedEMERGENCY LIGHTS AT ROW 6 AND FLOOR LIGHTING AT ROWS 3, 4 & 5 ARE INOPERATIVE. REPLACED CENTER BATTERY PACK PER 33-50-00. OPS CHECK GOOD.Mar 27, 2002 · N220SW · Emb EMB120ER · Emergency LightingSDR SWIA200210759Control Box · failedCOMMUNICATIONS FREQUENCY SWITCH FAILED AFTER DEPARTURE. DIVERTED BACK TO FAT. REMOVED AND REPLACED COMM-1 CONTROL BOX WITH SERVICEABLE UNIT. OPS CHECKS GOOD.Mar 27, 2002 · N251YV · Emb EMB120ER · VHF Communications SystemSDR SWIA200210758Outflow Valve · failedAIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REMOVED AND REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE. OPS CHECKS GOOD.Mar 27, 2002 · N579SW · Emb EMB120ER · Pressure Regulator/Outflow ValveSDR SWIA200210779Frame · corrodedINTERGRANULAR CORROSION FOUND IN FORWARD TOP INTERNAL AREA ACCESS HOLE ON PASSENGER DOOR. REMOVED AND REPLACED THE CORRODED FRAME IAW EMB SRM 51-40-02 AND 51-00-00.Mar 24, 2002 · N217SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200210756Fcu · malfunctionedFLAP CONTROL FAULT, INBOARD FLAPS STUCK. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD.Mar 24, 2002 · N224SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200210747Switch · out of adjustSERVICE DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED AVIONICS BAY DOOR MICROSWITCH. OPS CHECK GOOD.Mar 23, 2002 · N189SW · Emb EMB120ER · Door Warning SystemSDR SWIA200210746Computer · malfunctionedAFTER TAKEOFF RECEIVED CONTROL SINK, TERRAIN AND CONTINUOUS PULL UP WARNINGS UNTIL 50 FT AGL. RETURNED TO FAT. REPLACED GPWS COMPUTER. OPS CHECK GOOD IAW MM 34-44-00.Mar 23, 2002 · N223SW · Emb EMB120ER · Ground Proximity SystemSDR ASOA02186Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE FRAME 16 RIGHT INBOARD CROSS FRAME WAS FOUND TO HAVE CORROSION OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSS FRAME AT FRAME 16 IAW SRM'S 51-40-02 AND 51-40-07. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02185Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD FLOOR SILL WAS FOUND WITH CORROSION FROM FRAME 13 TO 23. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 51-25-00, 51-40-05, 51-21-02, 51-21-04, AND 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02184Sill · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15A AND 23. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 21-25-00 AND 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02183Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT WALL SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 32 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT WALL SET TRACK IAW SRM'S 51-25-00 AND 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02182Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS FROM FRAME 14 TO 32 AND FROM FRAMES 34 TO 40. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF THE RIGHT SEAT TRACK IAW SRM'S 51-21-00 AND 51-40-02. (MMar 20, 2002 · N285AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02181Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS CORRODED BETWEEN FRAMES 18 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED RIGHT BUTT STRAP IAW SRM'S 51-25-00 AND 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02180Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 13 AND 23. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRM'S 51-25-00, 51-21-02, 51-14-00, AND 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Miscellaneous StructureSDR ASOA02193Seat Track · corrodedDURING C-CHECK, FOUND INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT FLOOR SEAT TRACK BETWEEN FRAMES 17 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SEAT TRACK IAW SRM 51-40-02 AND ALSO REF ASA EO120-25-0007C, WHICH FACILITATES SEAT TRACK SMar 20, 2002 · N285AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02192Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD WALL SEAT TRACK FROM FRAME 14 TO FRAME 32 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED WALL SEAT TRACK IAW SRM 51-40-02 AND ALSO REF ASA EO120-25-0007C, WHICH FACILITATES SEAT TRAMar 20, 2002 · N285AS · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR ASOA02191Floorbeam · corrodedDURING C-CHECK FOUND INSPECTION IN BNA, THE LOWER AFT FLOOR FLANGE AT FRAME 13 WAS CORRODED. MAINTENANCE REPAIRED THE CORRODED FLOOR FLANGE IAW SRM 51-40-02. (M)Mar 20, 2002 · N285AS · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA200210741Warning System · malfunctionedON INITIAL TAKEOFF ROLL, TAKEOFF AUTO FEATHER AURAL WARNING WAS HEARD WITH AUTO FEATHER SWITCH ON. TAKEOFF WAS ABORTED. RETURNED TO THE GATE. PERFORMED SIMULATED TAKEOFF ENGINE RUNS. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME.Mar 19, 2002 · N296SW · Emb EMB120ER · Central WarningSDR SWIA200210740Control Servo · stiffAILERON CABLES ARE VERY STIFF. FOUND AILERON AUTOPILOT SERVO MOVEMENT STIFF. REPLACED SERVO IAW 22-10-05. AILERON AND AUTOPILOT OPS CHECKS GOOD.Mar 19, 2002 · N196SW · Emb EMB120ER · Autopilot Main ServoSDR C2XA02IA074Apu · overservicedSHV- APU BLEED CAUSES SMOKE WHEN BOTH PACKS TURNED OFF. SHV- MAINTENANCE INSPECTED THE AIRCRAFT, AND, THE AIRCRAFT WAS RELEASED IAW MEL. IAH- MAINTENANCE REMOVED EXCESS OIL FORM APU TO OBTAIN THE PROPER SERVICE LEVEL,PERFORMED A OPERATIONAL CHECK OF THE Mar 18, 2002 · N16718 · Emb EMB120ER · APU Bleed Air SystemSDR SWIA200210750Seal · defectiveON TAKEOFF RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. OIL PRESSURE RETURNED BACK IN THE GREEN ARC AND FLUCTUATED BETWEEN 60 & 50 PSID. OIL PRESSURE DROPPED BACK OFF AGAIN WITH ASSOCIATED WARNINGS. OIL PRESSURE STABILIZED AT 63 PSID ON DOWNWIND RETURNING Mar 17, 2002 · N199SW · Emb EMB120ER · Turbine Engine Oil System
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