Embraer EMB-120RT

Service difficulty reports · 5,310

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'EMB120RT'
  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 COMA0110157Sensor · malfunctionedFLIGHT 5049 - THREE KNOB POWER LEVER SPLIT DURING T/O. REPLACED THE RT ENGINE T2 SENSOR.Nov 16, 2001 · N269CA · Emb EMB120RT · Fuel Controlling SystemSDR SWIA200110355Fastener · looseSERVICE DOOR LIGHT ILLUMINATED ON CLIMB THROUGH 10,000 FEET. LIGHT WENT OUT ON DESCENT WHILE SLOWING. RETURNED TO FAT. FOUND 1 CAMLOCK ON INBOARD FUEL SERVICE DOOR LOOSE. RESECURED CAMLOCK AND INSPECTED ALL SERVICE DOORS MICROSWITCHES. NO FAULTS FOUND. WNov 14, 2001 · N196CA · Emb EMB120RT · Fluid Service DoorsSDR ASOA01234Odor · detectedUPON DEPARTURE FROM OKC, AT APPROXIMATELY 5000 FEET, CAPTAIN STARTED TO SMELL A HOT BURNING ODOR COMING FROM THE AIR VENTS. HE TURNED THE PACKS OFF, AND THE SMELL WENT AWAY. NO WARNING INDICATIONS WERE RECEIVED FROM THE AIR CONDITIONING SYSTEM. AIRCRAFT LANNov 13, 2001 · N286AS · Emb EMB120RT · Air Distribution SystemSDR COMA0110156Battery · dischargedFLIGHT #5044. EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY LIGHTS BATTERY.Nov 12, 2001 · N264CA · Emb EMB120RT · Emergency LightingSDR ASOA01239Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 20 RIGHT BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM Nov 11, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA0110155Wheel · crackedFLIGHT 5825 DURING PREFLIGHT INSPECTION, THE CREW NOTICED THAT THE RIGHT MAIN INBOARD WHEEL INNER HALF WAS CRACKED AND A PORTION OF THE FLANGE WAS SLIGHTLY PROTRUDING. THE WHEEL FLANGE HAD GOUGED THE LOWER TORQUE-LINK OF THE RIGHT MAIN GEAR.THE WHEEL ASSEMBLNov 11, 2001 · N259CA · Emb EMB120RT · Wheel/Ski/FloatSDR ASOA01240Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 16. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM 51-Nov 10, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01233Skin · corrodedDURING C-CHECK INSPECTION IN BNA, THE LOWER FUSELAGE WAS FOUND CORRODED ON THE EXTERNAL SKIN BETWEEN FRAMES 7 AND 8 WHERE THE DME ANTENNA MOUNTS BETWEEN STRINGERS 21 LEFT AND 21 RIGHT. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. A NEW INSIDE DOUBLER WAS Nov 10, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA01232Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 24 AND 32. MAINTENANCE REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW CPM 51-14-00. THE SEAT TRACK WAS REMOVED IAW SRM 51-40-02. A NEW SEAT TRACNov 10, 2001 · N280AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01231Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 22 AND 32. MAINTENANCE REMOVED THE SEAT TRACK IAW SRM 51-40-2. A NEW SEAT TRACK WAS LOCATED AND DRILLED IAW SRM 51-25-00 AND 51-40-6. AIRCRAFT WINov 10, 2001 · N280AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01220Battery Pack · dischargedFLT 4812 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 9, 2001 · N237AS · Emb EMB120RT · Emergency LightingSDR ASOA01219Battery · dischargedDURING HANGAR INSPECTION IN TXK, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 7, 2001 · N260AS · Emb EMB120RT · Emergency LightingSDR SWIA200110339Actuator · failedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION ACTUATOR. SWUNG GEAR CHECK GOOD. LEAK CHECK GOOD.Nov 4, 2001 · N1105G · Emb EMB120RT · Landing Gear ActuatorSDR SWIA200110274Computer · faultyON TAKEOFF ROLL SYSTEM NR 1 STALL WARNING LIGHTS ILLUMINATED. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER. OPS CHECK GOOD.Oct 25, 2001 · N1117H · Emb EMB120RT · Stall Warning SystemSDR COMA0110152Pin · brokenFLIGHT MECHANICS TAXIED A/C TO HANGAR FROM GATE AND FELT A BRAKE DRAGGING. A/C WAS JACKED AND THE LEFT INBD BRAKE WAS FOUND TO BE DRAGGING. AFTER THE BRAKE WAS REMOVED, IT WAS DISCOVERED THAT ONE OF THE RETURN SPRING ASSEMBLIES "PIN" WAS BROKEN AT END THAT ATOct 23, 2001 · N267CA · Emb EMB120RT · BrakeSDR COMA0110154CapFLIGHT #5057. DURING CRUISE FLIGHT THE RIGHT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, CREW DECLARED AN EMERGENCY AND PERFORMED AN INFLIGHT SHUT DOWN OF THE RIGHT ENGINE.REPLACED THE RIGHT ENGINE OIL SERVICING FILLER CAP AND NECK.Oct 22, 2001 · N259CA · Emb EMB120RT · Engine Oil PressureSDR COMA0110153Controller · faultyFLIGHT #5009. DURING CLIMB OUT OF MCO A LOUD AIR NOISE EMANATING FROM THE NOSE AREA, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE LANDING GEAR RELAY BOX.Oct 22, 2001 · N267CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR ASOA01249Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS DISCOVERED CORRODED FROM FRAME 13 TO STATION 6653.1. MAINTENANCE REMOVED AND REPLACED RIGHT CORRODED BUTT STRAP IAW SRM 51-40-02. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01248Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP, FROM FRAME 16 TO STATION 6653.1, WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01247Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION FOUND ON THE CENTER BUTT STRAP FROM FRAMES 13 TO 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CENTER BUTT STRAP IAW SRM 51-40-02. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01246Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP FROM FRAME 14 TO STATION 6653.1 WAS FOUND CORRODED. THE CORROSION WAS FOUND TO BE OUT OF LIMITS AT FRAMES 14 AND 15. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS INSOct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01245Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 19 LEFT FROM FRAME 13A TO FRAME 18. MAINTENANCE REMOVED THE CORRODED 19 LEFT STRINGER FROM FRAME 13A TO FRAME 18 IAW SRM 51-25-00. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-2. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01244Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 17 LEFT WAS FOUND CORRODED BETWEEN FRAME 21 AND STATION 6653.1. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER IAW SRM 51-25-00, 51-20-00, 51-10-02, AND 51-30-01. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01254Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT WALL SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED FROM FRAME 17 TO 32. THE LEFT, AFT SECTION, OF THE WALL SEAT TRACK WAS ALSO FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 38. MAINTENANCE REMOVED CORRODED SEATOct 20, 2001 · N274AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01253Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND TO BE CORRODED OUT OF ALLOWABLE LIMITS FROM FRAME 15 TO FRAME 32. MAINTENANCE REMOVED CORRODED FORWARD SECTION OF THE RIGHT FLOOR SEAT TRACK. A NEW SEAT TRACK WAS FABRICOct 20, 2001 · N274AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01252Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, FORWARD SECTION, WAS FOUND CORRODED FROM FRAME 17 TO FRAME 26. CORROSION WAS ALSO FOUND ON THE LEFT FLOOR SEAT TRACK, AFT SECTION, FROM FRAME 32 TO 39. MAINTENANCE REMOVED AND REPLACED BOTH FORWARDOct 20, 2001 · N274AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01251Buttstrap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT AFT BUTT STRAP HAS CORROSION BETWEEN FRAMES 32 AND 39. MAINTENANCE REMOVED AND REPLACED CORRODED BUTT STRAP IAW SRM 51-40-02. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01250Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE CROSS BEAM AT FRAME 16 WAS CORRODED FROM THE LEFT BUTT STRAP TO THE LEFT WALL. MAINTENANCE REMOVED AND REPLACED CORRODED CROSS BEAM IAW SRM 51-40-02. (M)Oct 20, 2001 · N274AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR SWIA200110253Bolt · brokenUPON GEAR RETRACTION LEFT MAIN GEAR DOOR STAYED OPEN. RECYCLED GEAR AND IT STILL REMAINED OPEN. FOUND A BROKEN BOLT ON THE LEFT INBOARD FORWARD DOOR ACTUATOR ARM. INSTALLED A NEW BOLT. OPS CHECK GOOD.Oct 15, 2001 · N200CD · Emb EMB120RT · Landing Gear Door ActuatorSDR SWIA200110246Computer · malfunctionedFLYING ILS INTO JAC WHEN APP MODE SELECTED ON FCP, THE COMMAND BARS STARTED MOVING UP AND DOWN RAPIDLY, GYRO AND COMPUTER FLAGS APPEARED AND ATTITUDE DISPLAY APPEARED ON MAP. RESET ATT MON PER QRH, WHICH CANCELLED FLAGS, BUT PRESSING APPR MODE IT ALL HAPPENEDOct 11, 2001 · N196SW · Emb EMB120RT · Integrated Flight SystemSDR ASOA01205Audio Panel · faultyFLT 4916 - ON DESCENT INTO DFW, FIRST OFFICER SMELLED AN ELECTRICAL SMELL FOLLOWED BY VISUALLY SEEING SMOKE COMING FROM HIS COMM PANEL. AN EMERGENCY WAS NOT DECLARED, BUT FIRE TRUCKS WERE REQUESTED. AIRCRAFT LANDED SAFELY IN DFW. AFTER LANDING NO FURTHER SMOct 9, 2001 · N275AS · Emb EMB120RT · Audio Integrating SystemSDR SWIA200110237Pump · defectiveDURING CLIMB TO 16000 FT NR 2 ENGINE TORQUE FLUCTUATED THEN RAPIDLY DROPPED TO 11 PERCENT TQ. OTHER ENGINE INDICATIONS WERE NORMAL. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RIGHT ENGINE HMU AND FUEL PUMP IAW MM 73-21-00. OPS AND LEAK COct 9, 2001 · N269UE · Emb EMB120RT · Engine Fuel PumpSDR ASOA01203Battery Pack · dischargedDURING HANGAR MAINTENANCE IN MCN, BOTH LEFT AND RIGHT SIDE AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Oct 7, 2001 · N238AS · Emb EMB120RT · Emergency LightingSDR ASOA012006Skin · crackedDURING SCHEDULED MAINTENANCE IN TXK, A SKIN CRACK, APPROXIMATELY .75 INCH LONG, WAS FOUND .5 INCH ABOVE THE TOP BRACKET FASTENER ON THE CAPTAINS LOWER FORWARD CORNER OF THE DV WINDOW POST. MAINTENANCE PERFORMED A TEMP REPAIR IAW ASA EO 120-53-1068. MAINTENANCOct 5, 2001 · N274AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA01200Skin · crackedDURING SCHEDULED MAINTENANCE IN TXK, A SKIN CRACK, APPROX .75 INCH LONG, WAS FOUND .5 INCH ABOVE THE TOP BRACKET FASTENER ON THE CAPTAINS LOWER FORWARD CORNER OF THE DV WINDOW POST. MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW ASA EO 120-53-0168. THIS EO PROOct 5, 2001 · N274AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA01199Battery Pack · dischargedFLT 4659 - DURING SCHEDULED INSPECTION IN ABY, THE NR 1 EMERGENCY LIGHTING BATTERY WAS WEAK. THIS CAUSED THE FORWARD ROW OF ESCAPE PATH LIGHTS TO GO OUT AFTER APPROXIMATELY TEN SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTING BATTERY PACOct 4, 2001 · N247AS · Emb EMB120RT · Emergency LightingSDR ASOA01196Battery Pack · dischargedFLT 4349 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY DOOR/CLOSET EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Oct 3, 2001 · N242AS · Emb EMB120RT · Emergency LightingSDR SWIA200110220Fcu · malfunctionedON TAKEOFF WE GOT THE FLAP AND ADVANCED SWS ON MAP AND CONTROL FAULT. ASYMMETRY AND DISAGREEMENT ON OVERHEAD FLAP PANEL AND FLAP DEG. INDICATOR WENT TO 0 DEGREES. ABORTED TAKEOFF. POWERED DOWN 5 MINUTES AND IT REPLICATED SAME PROBLEM AFTER POWER UP. RE-RACKOct 2, 2001 · N200CD · Emb EMB120RT · Trailing Edge Flap Control SystemSDR ASOA01195Support · corrodedWHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 21 RIGHT AT FRAMES 17, 18, 18A, 18B AND 21. CORROSION WAS ALSO FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 19 RIGHT AT FRAMES 20 AND 21. MAINTENANCE Oct 1, 2001 · N245AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA01194Stringer · corrodedWHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 18 RIGHT, BETWEEN FRAMES 19 AND 20. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEMENT. (M)Oct 1, 2001 · N245AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01193Stringer · corrodedWHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 21 RIGHT, BETWEEN FRAMES 19 AND 20 AND ALSO BETWEEN FRAMES 21 AND 22. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIROct 1, 2001 · N245AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA0110150Sensor · malfunctionedFLIGHT 5038. T/O TRIM AURAL WARNING WHEN POWER LEVERS ADVANCED. COULD NOT DUPLICATE DISCREPANCY AND A/C RETURNED TO SERVICE. DURING CALLBACK MAINTENANCE THE LEFT ELEVATOR TRIM PROXIMITY SENSOR WAS DETERMINED TO BE DEFECTIVE AND WAS REPLACED.Oct 1, 2001 · N267CA · Emb EMB120RT · Central WarningSDR COMA0110147Wire · brokenFLIGHT 5025. OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOP. REPAIRED BROKEN WIRE AT LIGHT FIXTURE. OPERATIONAL CHECK SATISFACTORY.Sep 30, 2001 · N268CA · Emb EMB120RT · Light System WiringSDR COMA0110148Roller · wornFLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY.Sep 28, 2001 · N264CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0110151LightFLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY.Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0110149LightFLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY.Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0110145Circuit BreakerFLIGHT #5057. DURING PRE-FLIGHT CREW DISCOVERED THE CIRCUIT BREAKER FOR THE FLIGHT IDLE STOP SOLENOID TRIPPED.PERFOMRED RESET AND OPERATIONAL CHECK OF THE FLIGHT IDLE STOP CIRCUIT BREAKER.Sep 25, 2001 · N463CA · Emb EMB120RT · Battery Overheat Warning SystemSDR COMA0110144Gauge · faultyFLIGHT #5062. DURING TAKE OFF FROM NAS THE RIGHT ENGINE PROPELLER AUTO FEATHERED AT 80 KNOTS, ABORTED TAKE OFF AND RETURNED TO THE GATE.REPLACED THE RIGHT ENGINE TORQUE GAUGE.Sep 24, 2001 · N259CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA0110143Indicator · faultyFLIGHT #5017. DURING TAKE OFF AT MCO THE LEFT ENGINE DIGITAL TORQUE INDICATION WAS INTERMITTENT, TAKE OFF WAS ABORTED AND REUTRNED TO THE GATE.REPLACED THE LEFT ENGINE TORQUE GAUGE.Sep 22, 2001 · N463CA · Emb EMB120RT · Power Indicating SystemSDR SWIA200110204Strap · out of positionCLIMBING THROUGH 22,000 CABIN ALT LIGHT ON MAP. CABIN WOULD NOT RESPOND IN AUTO. SWITCH TO MANUAL, WOULD NOT RESPOND. AFTER ABOUT 30 SECONDS CABIN STARTED DESCENDING. DIVERTED FROM STS TO SFO.SECURED INSULATION ON AFT PRESSURE BULKHEAD AND REPOSITIONED BONSep 21, 2001 · N200CD · Emb EMB120RT · Pressure Regulator/Outflow Valve
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