Boeing 737-201

Service difficulty reports · 2,471

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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 = '737201'
  ORDER BY difficulty_date DESC"

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SDR USAASB95029Fuel Control · failedFLT NR 8582 - RSW - AFTER SECOND APU START ATTEMPT APU FIRE LIGHT ILLUMINATED APU FIRE SWITCH PULLED AND BOTTLE DISCHARGED. REMOVED AND REPLACED THE APU FCU. ADJUSTED CRACK PRESSURE. CLEANED SHROUD DRAINS. REPLACED IGNITOR LEADS. APU OPS NORMALLY. (M)Dec 16, 1995 · N234US · Boeing 737201 · APU Engine Fuel and ControlSDR USAA951335Skin · delaminationINT - DURING 'DROP IN-AV' VISUAL/ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES AND LOCATIONS, FROM BS 727-908 LEFT WINDOW BELT PANEL BS 727-908 LEFT SIDE. REPLACED UPPER ROW OF FASTENERS BS 727-908 S-14 L. REPAIRED PER EA 31780. (M)Dec 15, 1995 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951334Skin · delaminationINT - DURING 'TRANSIT CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 RHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951333Skin · delaminationINT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951332Skin · delaminationINT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 360-540 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951331Stringer · corrodedROA - DURING 'CX-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED STRINGER CAUSED BY LAVATORY SPILL, STRINGER 27L AT BS 947. REMOVED CORRODED STRINGER SECTION AND SPLICED IN NEW SECTION. REPAIRED PER SRM 53-10-3 FIG 1. (M)Dec 15, 1995 · N226US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA95020Line · failedFLT NR 221 - DEN - AIR TURN BACK, DURING CLIMB-OUT OF DEN, FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. THE AIRCRAFT WAS RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC LINE FROM THE NR 2 B-SYSTEM MODULE. PERFORMED LEAK CHECK AND SYDec 15, 1995 · N207AU · Boeing 737201 · Hydraulic System, MainSDR F3LA95019Pcu · malfunctionedFLT NR 465 - DEN -UPON ARRIVAL, FLIGHT CREW REPORTED RUDDER TRIM REQUIRED ONE FULL UNIT OF RIGHT RUDDER ADJUSTMENT TO ESTABLISH ZERO DEGREE DRIFT. MAINTENANCE REPLACED THE RUDDER POWER CONTROL UNIT AND SYSTEM CHECKED OK. (M)Dec 14, 1995 · N217US · Boeing 737201 · Rudder Control SystemSDR USAA951342Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC FOUND FUSELAGE SKIN CRACK, 4.25 INCH LONG, STRINGER 18L, STATION 780. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Dec 12, 1995 · N244US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951339Stringer · corrosionROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 6 INCHES OF STRINGER CORRODED STRINGER 27R AT STATION 965. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M)Dec 12, 1995 · N244US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951338Stringer · corrodedROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 45 INCHES OF STRINGER 27L CORRODED, STRINGER 27L BETWEEN STATION 948 TO 993. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M)Dec 12, 1995 · N244US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951337Skin · crackedROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, STATION 303.37 STRINGER 10-L, IN FUSELAGE SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3, FIG 21 DETAIL 1. (M)Dec 6, 1995 · N241US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA95018Coalesor · dirtySLC - AIR TURN BACK. UPON TAKEOFF, FLIGHT CREW REPORTED AN ODOR IN THE COCKPIT AFTER TURNING ON LEFT PACK. THE SMOKE DETECTOR IN THE FORWARD LAVATORY ACTIVATED AND THE AIRCRAFT WAS RETURNED TO SLT. MAINTENANCE INSPECTED THE AIRCRAFT INTERIOR AND THE AIR CONNov 28, 1995 · N214AU · Boeing 737201 · Humidity Control SystemSDR USAA951235Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 30 INCH BY 2 INCH CORROSION AT STRINGER 27 LEFT BS 947 TO 977. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. (M)Nov 22, 1995 · N224US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA95016Battery Pack · dischargedFAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND SYSTEM CHECKED OK. (M)Nov 16, 1995 · N214AU · Boeing 737201 · Emergency LightingSDR USAASB95003Fuel Pump · failedPHL - FL 330, CLIMBING OUT OF LGA, AT FL 280, THE LEFT ENGINE SHUT DOWN AND COULD NOT BE RESTARTED. FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN FUEL PUMP FAILED AND REPLACED IT. (M)Oct 23, 1995 · N225US · Boeing 737201 · Engine Fuel PumpSDR USAA951133Skin · crackedCLT - DURING A UNSCHEDULED MAINTENANCE INSPECTION, VISUALLY FOUND A 6 INCH BY 4 INCH .5 INCH BY .150 INCH DENT WITH 9.5 INCH CRACK, LOCATED LEFT WBL 86 AT THE WING LEADING EDGE. INSTALLED INTERIM REPAIR PER EA 40063. (M)Oct 11, 1995 · N262AU · Boeing 737201 · Wing, Plate/SkinSDR USAA951050Stringer · corrosionROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPAIRED PER SRM 53-10-3, FIG 1. (M)Sep 29, 1995 · N263AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951003Oil Press Xmittr · failedBUF - FLT NR 1063 - ON CLIMB-OUT FROM BUF, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO BUF WHERE LANDING WAS WITHOUT INCIDENT. SET WAS 11 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURESep 23, 1995 · N265AU · Boeing 737201 · Engine Oil PressureSDR USAA951134Stringer · corrosionCLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M)Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951089Stringer · corrodedCLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2. REPLACED END STRINGER 28R, RBL 6. (M)Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950990Stringer · corrodedROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 8 INCH BY 3 INCH CORRODED AREA ON BOTTOM AND SIDES OF STRINGER. STRINGER 27L BENEATH FRAME AT BS 967. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIR PER SRM 53-10-3 FIG 1. (M)Sep 15, 1995 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950963Stringer · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER CORROSION FOUND UNDER STRINGER 27L AT STATION 967. REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3. (M)Aug 18, 1995 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950839Strap · unsecurePIT - FLT 0281 - THE REAR PASSENGER DOOR WAS CLOSED WITH THE SAFETY STRAP OUTSIDE. AIRCRAFT RETURNED TO PIT. MAINTENANCE SECURED THE RIGHT REAR SERVICE DOOR SAFETY STRAP IN THE HOLDER. NO DAMAGE WAS NOTED TO THE DOOR OR FUSELAGE. (M)Aug 3, 1995 · N229US · Boeing 737201 · Passenger/Crew DoorsSDR F3LA95015Anti-Skid Contl · failedBZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHECK. SYSTEM CHECKED OK. A FAULT WAS FOUND ON THE ANTI-SKID MODULE TEST AND THE LEFT OUTBOARD ANTI-Jul 31, 1995 · N217US · Boeing 737201 · Brake Anti-Skid SectionSDR USAA950927Stringer · corrodedROA - DURING 'BX CHECK' VISUAL INSPECTION, FOUND 13 .125 INCH LONG STRINGER CORRODED FUSELAGE STATION 967 JUST TO THE LEFT OF WATER TANK. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIRED PER SRM 53-10-3 FIG 1 FUSELAGE STRINGER Jul 28, 1995 · N237US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950926Stringer · corrodedINT - DURING 'CD-6' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BETWEEN STATION 967 AND 986.5 AT S-27L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950925Stringer · corrodedINT - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH CORRODED AREA BETWEEN STATION 947.5 AND 967 AT S-26L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA95014Oil Temp Bulb · failedOMA - AIR TURNBACK, FLIGHT CREW REPORTED HIGH OIL TEMPERATURE INDICATED ON RIGHT ENGINE. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO OMAHA. UPON ARRIVAL IN OMAHA, MAINTENANCE REPLACED THE OIL TEMPERATURE SENSING BULB, CHECKED AND CLEANED ELECTRICAL CONNECTIJul 20, 1995 · N214AU · Boeing 737201 · Engine Oil TemperatureSDR USAA950767Actuator · leakingBOS - FLT NR 0284 - ON TAKEOFF, THE MASTER CAUTION LIGHT ILLUMINATED. THE HYDRAULIC SYSTEM 'A' PRESSURE WAS FLUCTUATING ABOVE ZERO, AND THE HYDRAULIC SYSTEM 'A' QUANTITY REACHED ZERO. FLIGHT RETURNED TO BOS. MAINTENANCE REPLACED THE NR 6 SPOILER ACTUATOR DUJul 18, 1995 · N247US · Boeing 737201 · Drag Control ActuatorSDR USAA950748Hydraulic Line · leakingROC - FLT 2274 - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAME ON. FLIGHT RETURNED TO ROC WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT RT MAIN GEAR UPLOCK CYCJul 8, 1995 · N240AU · Boeing 737201 · Hydraulic System, MainSDR USAA950615Switch · failedBWI - FLT 2190 - FLIGHT EN RUOTE ORD TO PHL, WHEN NR 2 ENGINE FILTER BYPASS LIGHT CAME ON AND NR 2 ENGINE SHUTDOWN. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL FILTER BYPASS SWITCH AND ENGINE OIL FILTER. (M)Jun 19, 1995 · N241US · Boeing 737201 · Engine Oil Indicating SystemSDR USAA950614Strap · looseEWR - FLT 371 - LOUD BANGING NOISE ON CLIMB-OUT. WARNING STRAP CAUGHT IN FORWARD GALLEY SERVICE DOOR. FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED STRAP FROM FORWARD GALLEY SERVICE DOOR. INSPECTED DOOR AND FUSELAGEJun 19, 1995 · N228US · Boeing 737201 · Galley DoorsSDR USAA950642Actuator · failedBWI - FLT 1120 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR. (W)Jun 18, 1995 · N234US · Boeing 737201 · Landing Gear ActuatorSDR USAA950613Flex Hose · failedJAX - FLT 104 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. FLIGHT RETURNED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC FLEX LINE. (M)Jun 18, 1995 · N249US · Boeing 737201 · Landing Gear Retraction/Extension SystemSDR USAA950612Fuel Pump · failedPHL - FLT NR 63 - CREW NOTICED FLUCTUATION IN NR 1 ENGINE DURING CLIMB-OUT OF PHL. FUEL FLOW/EPR AND N1 FLUCTUATIONS WERE NOTED ALONG WITH A SLIGHT OIL PRESSURE FLUCTUATION. CREW RETURNED TO PHL WITH NR 1 ENGINE AT IDLE. MAINTENANCE REPLACED FUEL PUMP AND FJun 17, 1995 · N227AU · Boeing 737201 · Engine Fuel PumpSDR USAA950596R/T Unit · failedCLT - FLT 97 - FLIGHT EN ROUTE PIT TO MIA WHEN RADAR QUIT WORKING. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED R/T UNIT. RADAR WORKED NORMAL. (M)Jun 4, 1995 · N228US · Boeing 737201 · Weather Radar SystemSDR USAA950532Anti-Ice Duct · crackedTPA - FLT 1569 - ON CLIMB-OUT OF TPA, NR 1 ENGINE OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE COWL ANTI-ICE DUCT. (M)May 22, 1995 · N260AU · Boeing 737201 · Airfoil Anti/De-ice SystemSDR USAA950527Fitting · crackedJFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED. FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE May 17, 1995 · N232US · Boeing 737201 · Engine Thrust ReverserSDR USAA950513Transceiver · failedCLT - FLT 1257 - FLIGHT EN ROUTE FLL TO DCA WHEN WEATHER RADAR FAILED. AIRCRAFT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WEATHER RADAR TRANSCEIVER. (M)May 14, 1995 · N229US · Boeing 737201 · Weather Radar SystemSDR USAA950457Generator · failedCLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED. APU WAS ON MEL. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD. OPS CHECK NORMAL. REFERENCE 95ZZZM54.May 6, 1995 · N252AU · Boeing 737201 · AC Generator-AlternatorSDR 95ZZZM54Csd · failedCLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED. APU WAS ON MEL. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD. OPS CHECK NORMAL. REFERENCE USAA950457.May 6, 1995 · N252AU · Boeing 737201 · Alternator-Generator DriveSDR USAA950410Start Valve · failedGSO - FLT 2243 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 START VALVE OPEN LIGHT CAME ON. CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TO GSO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED START VALVE ASSEMBLY AND START VALVE SWITCH. RAN NR 1 ENGINE, LEAK AApr 26, 1995 · N254AU · Boeing 737201 · Engine Start Valves/ControlsSDR F3LA95010Switch · malfunctionDEN - UPON ARRIVAL, FLIGHT CREW REPORTED LANDING GEAR UNSAFE (INTRANSIT) LIGHTS ILLUMINATED WITH GEAR HANDLE UP. MAINTENANCE REPLACED THE LANDING GEAR HANDLE MICROSWITCH AND CHECKED OK. (M)Apr 25, 1995 · N205AU · Boeing 737201 · Landing Gear Position and WarningSDR USAA950380Duct · failedBOS - FLT 2176 - NR 2 ENGINE OVERHEAT CAME ON DURING CLIMB-OUT. RETARDED THROTTLE, LIGHT WENT OUT. FLIGHT RETURNED TO BOS WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT ENGINE COWL ANTI-ICE SUPPLY DUCT BLOWN BETWEEN CROSS OVER DUCT AND Apr 14, 1995 · N255AU · Boeing 737201 · Air Intake Anti/De-Ice SystemSDR USAA950379Pump · failedCLT - FLT 2126 - FLIGHT EN ROUTE BWI TO ATL WHEN 'A' SYSTEM HYDRAULICS FAILED. CREW DIVERTED FLIGHT TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGNE HYDRAULIC PUMP. REPLACED 'A' SYSTEM RETURN AND BOTH CASE DRAIN FILTERS. NApr 13, 1995 · N244US · Boeing 737201 · Hydraulic Pump (Electric/Engine), MainSDR USAA950375Prbc · failedGSO - FLT 8002 - FLIGHT EN ROUTE MLB TO BWI WHEN THROTTLES SPLIT. AIRCRAFT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT ENGINE PRBC. RAN ENGINE, OPS CHECK GOOD. (W)Apr 6, 1995 · N239US · Boeing 737201 · Compressor Bleed ValveSDR USAA950358Clamp · looseCLT - NR 2271 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 ENGINE INDICATED HIGH EGT AND FUEL FLOW. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE SECURED LOOSE CLAMP ON 13 STAGE DUCT. LEAK CHECK OK. RAN ENGINES, CHECKS NORMAL. NApr 4, 1995 · N239US · Boeing 737201 · Pneumatic Distribution SystemSDR USAA950357Duct · failedORF - FLT 2271 - DURING CLIMB-OUT OF ORF, NR 1 ENGINE REVERSE LIGHT AND NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED DUCT ASSEMBLY AND REPAIRED WIRING IN WIRING BUNDLE 2198. Apr 3, 1995 · N239US · Boeing 737201 · Engine Anti-Icing SystemSDR USAA950309Beam · crackedGSO - DURING UNSCHEDULED MAINTENANCE VISUAL INSPECTION, FOUND 1.5 INCH CRACK, FORWARD END OF WEB AT THE NLG ACTUATOR SUPPORT FITTING BEAM AT STATION 227. REPAIRED PER EA 30088, SRM 51-40-2 FIG 1. (W)Mar 30, 1995 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
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