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 COMA9810056Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I, REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810055Tcas Tray · corrodedDURING 2C INSPECTION ZONE 100 TASK 5310-132-01I, FOUND TCAS SUPPORT TRAY CORRODED BEYOND LIMITS. REMOVED CORRODED TRAY AND BUILT UP NEW SERV TRAY IAW STC ST00075W1-D.Mar 4, 1998 · N241CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810054Sign · brokenEMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN.Mar 4, 1998 · N162CA · Emb EMB120RT · Emergency LightingSDR COMA9810053Battery · dischargedCABIN DOOR EMERGENCY EXIT SIGN IS INOPERABLE, EMERGENCY FLOOR PATH LIGHTING TO ROW 3 IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.Mar 3, 1998 · N168CA · Emb EMB120RT · Emergency LightingSDR COMA9810049Spinner Bulkhead · crackedDURING PREFLIGHT INSPECTION, THE RIGHT PROPELLER SPINNER BULKHEAD WAS FOUND TO BE CRACKED APPROXIMATELY 1.5 INCH ALONG THE BULKHEAD OUTER WALL BEHIND BLADE NR 2. AIRCRAFT WAS FERRIED BACK TO CVG HANGAR AND BULKHEAD REMOVED FOR REPAIR. DAMAGE APPEARS TO BE DUMar 2, 1998 · N255CA · Emb EMB120RT · Propeller Spinner SectionSDR WTAA980040Structure · bird strikeSBA - BIRD STRIKE ON LANDING REPORTED. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X)Mar 1, 1998 · N193YV · Emb EMB120RT · Aircraft StructuresSDR WTAA980039Oil Cooler · failedSBA - LEFT ENGINE LOST OIL PRESSURE ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED LEFT ENGINE OIL COOLER AND SERVICED. PERFORMED ENGINE RUN. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)Mar 1, 1998 · N455UE · Emb EMB120RT · Engine Oil CoolerSDR C2XA98CL022Water Separator · faultedCLE - FLT 3116 - CREW REPORTED A DUCT LEAK LIGHT ON THE RIGHT ENGINE DURING DEPARTURE, CREW PERFORMED QRH ITEMS AND LIGHT EXTINGUISHED AT THE 3 MINUTE MARK. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 WATER Mar 1, 1998 · N31711 · Emb EMB120RT · Humidity Control SystemSDR C2XA98CL020Brake Stator · brokenCLE - FLT 3355 - CREW REPORTED FEELING THE BRAKES GRABBING ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THEN REMOVED AND REPLACED THE LEFT OUTBOARD BRAKE ASSEMBLY DUE TO A BROKEN STATOR, IAW EMB-120 MM 32-41-05. OPERATIONAL AND LEAK CHECKS WEREFeb 28, 1998 · N26714 · Emb EMB120RT · BrakeSDR MASA98043Fuse · failedCLT/GNV - FLT 5593 - PILOT REPORTED BOTH AFT EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FUSE. AIRCRAFT WAS RETURNED TO SERVICE. (X)Feb 27, 1998 · N287UE · Emb EMB120RT · Emergency LightingSDR COMA9810051Lamp · failedONE LAMP INOP AT FORWARD EMERGENCY FLOOR PATH LIGHTING. REPLACED LAMP.Feb 27, 1998 · N137H · Emb EMB120RT · Emergency LightingSDR COMA9810050Wheel · crackedMECHANIC 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.Feb 26, 1998 · N130G · Emb EMB120RT · Wheel/Ski/FloatSDR C2XA98IA102Support · crackedIAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 19 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA068Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA067Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA066Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA065Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA064Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA063Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA062Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA061Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA060Bracket · crackedIAH - DURNG C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 20 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA059Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 20 FO THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA058T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA057T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA056Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA055Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA054Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA053Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA052Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW EMB120 SRM 53-00-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR C2XA98IA051Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA050T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA049T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA048T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA047Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 40. MAINTENANCE REPAIRED THE AFFECTED AREA IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01043 AND THE AIRCRAFT WAS APPROVED FORFeb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA046Rib · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01020, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEFeb 26, 1998 · N16719 · Emb EMB120RT · Wing, Rib/BulkheadSDR C2XA98IA045T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER T-PROFILE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA044T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA043Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA042Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-4--02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA041Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA040Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA039Bracket · crackedIAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 20 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA038Trunnion · corrodedIAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR SPRING BOX LOWER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRUNNION IAW EMB120 CMM ERAM 32-21-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear Attach SectionSDR C2XA98IA037Trunnion · corrodedIAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR STRUT SPRING BOX UPPER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ALL WORK ACCOMPLISHED IAW ERAM CMM 32-2Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear Attach SectionSDR C2XA98IA036Pin · corrodedIAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK LOWER PIVOT PIN WAS FOUND TO BE CORRODED IN SIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PIVOT PIN IAW ERAC CMM 32-31-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing GearSDR C2XA98IA035Pin · corrodedIAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK UPPER PIVOT PIN WAS FOUND TO BE CORRODED INSIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE PIN IAW ERAM CMM 32-31-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing GearSDR MASA98039Wire · shortedFLT 5508 - MIA-TLH - ON START UP IN MIA, CREW NOTICED THE EMERGENCY TRACK LIGHTS IN THE MIDDLE FLOOR SECTION WOULD NOT ILLUMINATE. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. IN SUBSEQUENT MAINTENANCE, A SHORTED WIRE WAS REPAIRED. (M)Feb 25, 1998 · N340JS · Emb EMB120RT · Light System WiringSDR C2XA98IA034Actuator · inoperativeIAH - DURING FLT 3794 - FROM LRD, THE PILOT REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO LRD WITHOUT INCIDENT, AND WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR RETRACT ACTUATOR, AND THE AIRCRAFTFeb 25, 1998 · N22727 · Emb EMB120RT · Landing Gear ActuatorSDR C2XA98CL017Signal Cond Unit · failedCLE - FLT 3079 - CREW REPORTED THE AUTOFEATHER SYSTEM WOULD NOT TEST, THE TORQUE WOULD RISE BUT NO ARM LIGHT OR NP CHANGE WAS NOTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITION UNIT IAW EMB-120-MM 77-1Feb 24, 1998 · N15732 · Emb EMB120RT · Engine BMEP/Torque Indicating
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