Boeing 737-130

Service difficulty reports · 287

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 = '737130'
  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 CALA9801859Actuator · inoperativeTHE GEAR HANDLE WAS PLACED IN THE OFF POSITION AFTER TAKEOFF AND THE NOSE GEAR CAME DOWN. THE GEAR HANDLE WAS PLACED UP AND THE NOSE GEAR RAISED. THE GEAR HANDLE WAS THEN PLACED TO OFF AND THE GEAR STAYED UP. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEMSep 25, 1998 · N77204 · Boeing 737130 · Landing Gear Retraction/Extension SystemSDR CALA9801589Bulb · failedNO NOSE GEAR INDICATION WAS RECEIVED WHEN GEAR WAS EXTENDED ON APPROACH. A GO-AROUND WAS INITIATED AND THE NOSE GEAR LIGHTS DID NOT TEST. THE NOSE GEAR INDICATOR LIGHT BULBS WERE REPLACED AND TESTED GOOD. GOOD INDICATIONS WERE RECEIVED WITH GEAR EXTENDED ANAug 31, 1998 · N77204 · Boeing 737130 · Landing Gear Position and WarningSDR CALA9801498Hyd Pump · leakingTHE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST FOR LOSS OF HYD WAS COMPLETED. THE AIRCRAFT WAS RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE Aug 23, 1998 · N77204 · Boeing 737130 · Hydraulic Pump (Electric/Engine), MainSDR CALA9801218Accessory Unit · inoperativeTHE GEAR HANDLE STOPPED IN THE OFF POSITION WHEN RAISING THE GEAR AFTER TAKEOFF. THE GEAR TRIGGER WAS PULLED AND THE GEAR CAME UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. TESTS WERE CONDUCTED IAW MM 32-09-200 AND ALL CHECKED GOOD.Jul 8, 1998 · N16201 · Boeing 737130 · Landing Gear Position and WarningSDR CALA9801171Engine · malfunctionedTHE NR 1 ENGINE LOST POWER DURING CLIMB-OUT OF EWR AT 1800 FEET. THE ENGINE WENT TO IDLE POWER. THE NR 1 ENGINE WAS SHUT DOWN PER FLIGHT MANUAL AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. Jun 25, 1998 · N14209 · Boeing 737130 · Engine (Turbine/Turboprop)SDR CALA9801157Power Supply · inoperativeINSPECTION FOUND FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK/POWER SUPPLY WAS REMOVED AND REPLACED.Jun 23, 1998 · N14206 · Boeing 737130 · Emergency LightingSDR CALA9801049Switch · inoperativeTHE UNSAFE NOSE GEAR INDICATION ILLUMINATED ON APPROACH. TO EWR. THE GEAR WAS CYCLED, APPROPRIATE CHECKLISTS WERE COMPLIED WITH, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG DOWNLOCK SWITCH AT FAULT. THE NLG DOWNLOCK SWITCH WAS REMOVEJun 13, 1998 · N14206 · Boeing 737130 · Landing Gear Position and WarningSDR CALA9801052Socket · corrodedINSPECTION FOUND AFT EXTERIOR EXIT SLIDES INOPERATIVE BOTH SIDES. THE RIGHT EXTERIOR SLIDE LIGHT SOCKET WAS CORRODED. THE SOCKET WAS REPLACED. IN ADDITION, BATTERY PACK M572 WAS REPLACED, OPERATION OF BOTH LIGHTS CHECKED GOOD.Jun 12, 1998 · N77204 · Boeing 737130 · Emergency LightingSDR CALA9800702Hyd Lines · puncturedTHE A SYSTEM HYDRAULIC FLUID LEVEL DROPPED TO ZERO WHILE ON DESCENT INTO PHL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO HYDRAULIC FLEX LINES AT LT ELEVATOR PCU PUNCTURED. THE FLEX LINES WERE REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECApr 27, 1998 · N14208 · Boeing 737130 · Hydraulic System, MainSDR CALA9800680Torque Tube · damagedWHEN FLAPS WERE EXTENDED ON APPROACH, THE FLAP INDICATOR DID NOT MOVE. THE FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE RT INBOARD FLAP TORQUE TUBE DAMAGED. THE TORQUE WAS REMOVED AND REPLACED IAW MM 27-51-Apr 19, 1998 · N14206 · Boeing 737130 · Trailing Edge Flap Control SystemSDR CALA9800648Frame · corrodedINSPECTION FOUND BS 706L FRAME LUG HOLE CORRODED AT LT MLG. AN OUTER BUSHING FOR BEAM AND TWO EACH HAT BUSHINGS FOR FRAME LUG WERE FABRICATED AND INSTALLED IAW ECRA 5310-03713.Apr 8, 1998 · N14206 · Boeing 737130 · Fuselage Main, FrameSDR CALA9800647Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE FRAME TRUNNION BEAM SUPPORT FITTING IN RT WHEEL WELL AT BS 706. THE BEAM WAS REPLACED IAW ECRA 5311-01045.Apr 7, 1998 · N14206 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9800660Skin · crackedINSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-21-31.Mar 4, 1998 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9701684Line · leakingTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO BUF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT WING AFT SPAR PRESSURE HYDRAULIC LINE LEAKING. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE LDec 1, 1997 · N14208 · Boeing 737130 · Hydraulic System, MainSDR CALA9701680Hyd Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE FLEX LINE LEAKING. THE LINE WAS REPLACED WINov 26, 1997 · N44214 · Boeing 737130 · Hydraulic System, MainSDR CALA9701432Slide · low pressureL-1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH MM 25-61-311.Oct 11, 1997 · N77215 · Boeing 737130 · Escape SlideSDR CALA9701355Hyd Line · rupturedTHE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ILLUMINATION OF A PUMP LOW PRESSURE LIGHTS. THE A-SYSTEM HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULC PRESSURE LISep 12, 1997 · N44214 · Boeing 737130 · Hydraulic System, MainSDR CALA9701279Engine · failedSPARKS WERE REPORTED COMING FROM THE NR 1 ENGINE EXHAUST WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.Sep 1, 1997 · N408PE · Boeing 737130 · Engine (Turbine/Turboprop)SDR CALA9701250Stud · failedTHE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE ENROUTE FROM CAE TO EWR. THE ENG WAS SHUTDOWN AND THE A/C WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTTOM STUD ON NR 1Aug 28, 1997 · N44214 · Boeing 737130 · Turbine Engine Accessory DriveSDR CALA9701247Hyd Line · leakingTHE A SYS HYD LOW PRESSURE LIGHT FLICKERED AND HYD QTY WAS ZERO WHILE EN ROUTE TO EWR. BOTH A HYD LOW PRESSURE LIGHTS ILLUMINATED STEADILY SHORTLY AFTERWARDS. THE LOSS OF A HYD SYS PRESSURE CHECKLIST WAS ACCOMP. A MANUAL GEAR EXTENSION AND ALTERNATE FLAP EXTAug 27, 1997 · N14211 · Boeing 737130 · Hydraulic System, MainSDR CALA9701234Dnlock Actuator · inoperativeTHE LANDING GEAR WAS EXTREMELY STIFF DURING RETRACTION FROM UP TO OFF WITH NO NOTICEABLE DETENT AT OFF. THE NOSE GEAR EXTENDED APPROXIMATELY 12 TO 15 SECONDS AFTER MAINS. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR IAW MM 32-33-21 PAGE 401. THE GAug 23, 1997 · N77204 · Boeing 737130 · Landing Gear Retraction/Extension SystemSDR CALA9701243Pcu · inoperativeA/C ATTEMPTED TO BANK LT WITH YAW DAMPER ON AND AUTOPILOT ENGAGED WHILE CLIMBING THRU 17,000 FT. THE YAW DAMPER WAS SWITCHED OFF AND ROLL ARRESTED. BANK ANGLE DID NOT EXCEED 15 DEG. APPROPRIATE CHECKLISTS COMPLETED AND THE FLT CONTINUED W/O PROBLEM. THE RUDDERAug 22, 1997 · N14208 · Boeing 737130 · Rudder Control SystemSDR CALA9701223Hyd Line · leakingTHE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHT WHILE AT CRUISE. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SUPPLY LINE LEAug 15, 1997 · N44214 · Boeing 737130 · Hydraulic System, MainSDR CALA9701040Actuator · inoperativeTHE LT MLG UNSAFE INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES FROM UP TO NEUTRAL POSITION UNTIL THE LIGHT EXTINGUISHED. THE LT MLG ACTUATOR WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOJul 10, 1997 · N14206 · Boeing 737130 · Landing Gear ActuatorSDR CALA9700980Fuel Control · malfunctionedA FUEL ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON TAKEOFF. THE CREW TURNED OFF THE LEFT PACK AND THE ODOR DISSIPATED. THE FLIGHT CONTINUED TO EWR WITHOUT FURTHER PROBLEM. THE ODOR OCCURRED AGAIN AFTER ENGINE SHUTDOWN AT GATE. MAINTENANCE FOUND THE NR 1Jul 1, 1997 · N14212 · Boeing 737130 · Fuel Control/Turbine EnginesSDR CALA9701028Angle · corrodedINSPECTION FOUND VERTICAL AND HORIZONTAL SUPPORT ANGLES FOR RT UPPER STRUT AND FLOORBEAM CORRODED AT STA 267. THE CORRODED AREA WAS CUT OUT, DOUBLERS, FILLER, AND A SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND 51-30-2.Jun 28, 1997 · N408PE · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9701025Frame · crackedINSPECTION FOUND FIVE EACH CRACKS IN AFT CARGO DOOR FRAME AT BS 827, STRINGER 23R. THE CRACKS WERE 1 TO 2.5 INCHES LONG. THE FRAME WAS REPAIRED IAW SRM 53-10-4 AND 51-10-2.Jun 18, 1997 · N408PE · Boeing 737130 · Fuselage Main, FrameSDR CALA9700912Wire Harness · damagedTHE APU FIRE LIGHT ILLUMINATED ON SHORT FINAL INTO CLE DURING APU START. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE APU HAD TORCHED ON START RESULTING IN BURN THROUGH OF HARNESS FOR TAILPIPE FIRE DETECTOR. THE APU COMBUSTOR AND TJun 17, 1997 · N33202 · Boeing 737130 · APU System WiringSDR CALA9700843Hydraulic Line · chafedTHE A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO NEAR ZERO WHILE EN ROUTE. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC PRESSURE LINE ON RT WING IN ENGINE PYLON Jun 6, 1997 · N44214 · Boeing 737130 · Hydraulic System, MainSDR CALA9700860Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 360, STRINGER 17L. THE DENTED SECTION OF SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 28 AND ECRA 5330-02523.May 20, 1997 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9700734Batt Charger · burnedAN ELECTRICAL ODOR WITH A SLIGHT TRACE OF HAZE WAS NOTICED IN THE CABIN WHILE ON DESCENT INTO CLE. THE GASPER FAN AND GALLEY POWER WAS TURNED OFF AND THE ODOR DECREASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BATTERY CHARGER IN E AND E COMPMay 15, 1997 · N24213 · Boeing 737130 · Battery/Charger SystemSDR CALA9701024Stringer · crackedINSPECTION FOUND CRACKS TOTALING 4 INCHES IN LENGTH IN RT WING STRINGER 13, AT WBL 135. REPAIR ANGLES WERE REMOVED AND THE CRACKS WERE STOP DRILLED. THE REPAIR ANGLES WERE REINSTALLED IAW SRM 51-10-2 AND BOEING DRAWING 65C34533.May 13, 1997 · N408PE · Boeing 737130 · Wing, Longeron/StringerSDR CALA9701029Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RT UPPER CORNER OF NOSE WHEEL WELL ANGLE AT STA 267. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-0, 51-10-2, AND ECRA 5340-01300.May 12, 1997 · N408PE · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9701023Stringer · crackedINSPECTION FOUND A 5 INCH CRACK IN RT WING STRINGER 13 AT WBL 80. THE STRINGER WAS REPAIRED IAW ECRA 5710-01815.May 12, 1997 · N408PE · Boeing 737130 · Wing, Longeron/StringerSDR CALA9701027Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT UPPER FORWARD CORNER OF L-2 DOOR AT STA 947, S7L. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03510 AND SRM 53-30-3.May 8, 1997 · N408PE · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9701026Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF L-2 DOOR, STA 986, S7L. THE CRACK WAS ROUTED OUT, DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03510, SRM 51-30-2, AND BOEING DRAWING 65C35747.May 8, 1997 · N408PE · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9701022Skin · crackedINSPECTION FOUND .5 INCH CRACKS AND CORROSION IN FUSELAGE SKIN AT STA 283, S10R. THE CORROSION WAS REMOVED AND THE CRACKED AREA OF SKIN WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5330-02543.May 8, 1997 · N408PE · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9700940Battery Pack · dischargedTHE R-1 DOOR PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-42 AND 33-51-101.May 5, 1997 · N408PE · Boeing 737130 · Emergency LightingSDR CALA9700939Battery Pack · dischargedTHE R-2 DOOR PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-50-42 AND 33-51-101.May 5, 1997 · N408PE · Boeing 737130 · Emergency LightingSDR CALA9700938Battery Pack · dischargedTHE LT ESCAPE HATCH PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-50-42 AND 33-51-101.May 5, 1997 · N408PE · Boeing 737130 · Emergency LightingSDR CALA9700937Battery Pack · dischargedTHE L-1 DOOR EXTERIOR EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-71, 33-50-42, AND 33-51-31.May 5, 1997 · N408PE · Boeing 737130 · Emergency LightingSDR CALA9700936Battery Pack · dischargedTHE R-2 DOOR EXTERIOR EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-71, 33-50-42, AND 33-51-31.May 5, 1997 · N408PE · Boeing 737130 · Emergency LightingSDR CALA9700643Strut · crackedA GRINDING SOUND WAS HEARD COMING FROM LANDING GEAR AREA DURING TAXI. MAINTENANCE FOUND THE NR 2 BRAKE ASSEMBLY DAMAGED DUE TO A SHEARED BOLT AND THE LT MLG INNER CYLINDER WAS CRACKED. THE LT MLG INNER CYLINDER WAS REMOVED AND REPLACED. IN ADDITION, THE NRMay 4, 1997 · N24213 · Boeing 737130 · Main Landing Gear Strut/Axle/TruckSDR CALA9700620Fire Loop · corrodedEN ROUTE, AT FL310 WHEN ENGINE ANTI-ICE TURNED ON ENGINE FIRE WARNING SOUNDED. FOLLOWED PROCEDURES PER QRH. FIRE WARNING AGAIN SOUNDED SHUTDOWN NR 1 ENGINE, DISCHARGED BOTH FIRE BOTTLES. DIVERTED TO ROA. INSPECTION FOUND CORRODED FIRE LOOP. REPLACED FIRE Apr 28, 1997 · N403PE · Boeing 737130 · Fire DetectionSDR CALA9700608Line · chafedLOST A-SYSTEM HYDRAULICS IN FLIGHT. REPLACED NUMBER 2 ENGINE HYDRAULIC SUPPLY LINE AT RIGHT WING ROOT.Apr 23, 1997 · N77204 · Boeing 737130 · Hydraulic System, MainSDR CALA9700648Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT UPPER EDGE OF BULKHEAD STA 178. THE DENTED AREA WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6.Apr 22, 1997 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9700647Skin · lightning strikeINSPECTION FOUND A LIGHTNING BURN AT FASTENER HEAD FOURTEEN INCHES AFT OF R-1 DOOR, STRINGER 9L. THE DAMAGED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Apr 22, 1997 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9700646Skin · crackINSPECTION FOUND A .0937 INCH CRACK AND CORROSION IN FUSELAGE SKIN AT STA 312, STRINGER 26L. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Apr 21, 1997 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9700644Skin · crackedINSPECTION FOUND A .125 INCH CRACK IN LT WING LEADING EDGE SKIN AT LE STA 219.67. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5720-01569 AND 5720-01570.Apr 20, 1997 · N14209 · Boeing 737130 · Wing, Plate/SkinSDR CALA9700645Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT UPPER ATTACH BRACKET OF R-1 DOOR WEB. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Apr 18, 1997 · N14209 · Boeing 737130 · Passenger/Crew Doors
Back to Boeing 737-130