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 USAASB00103Charger · failedBNA - PILOT REPORTED THAT THE EMERGENCY PATH LIGHTS ILLUMINATED ON 4 ROWS IN THE CABIN. MAINTENANCE CYCLED CIRCUIT BREAKERS FOR TR1, 2 AND 3. OPERATIONAL CHECK GOOD. CLT - PILOT REPORTED THE NEXT DAY (4-5-00) THAT THE FLOOR PROXIMITY EMERGENCY LIGHTS ILLUMIApr 4, 2000 · N224US · Boeing 737201 · Emergency LightingSDR USAASB00094Circuit Board · malfunctionedCLT - FLT 1643 - ON CLIMB-OUT FROM CLT, CAPTAIN REPORTED THAT THE NR 4 LEADING EDGE SLAT WAS SLIGHTLY OUT OF ALIGNMENT AND THE AIRCRAFT HAD A TENDANCY TO WANT TO ROLL IN LEVEL FLIGHT. LEADING EDGE TRANSIT LIGHT REMAINED ILLUMINATED WITH FLAP HADNLE UP. FLIGHMar 31, 2000 · N227AU · Boeing 737201 · Leading Edge Slat Position Indicating SystemSDR USAASB00093Separator · dirtyCLT - FLT 1282 - ON DESCENT INTO CLT, AN ODOR WAS NOTED IN THE FLIGHT COMPARTMENT LIKE THAT OF DIRTY GYM SOCKS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WATER SEPARATOR BAGS PER MM. OPERATIONAL CHECK AND LEAK CHECK GOOD. Mar 30, 2000 · N263AU · Boeing 737201 · Humidity Control SystemSDR USAASB00100Battery Pack · inoperativePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT OVER THE FIRST CLASS SECTION IS FLASHING. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY PACK AT SEAT ROW 2. OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM GOOD. (X)Mar 27, 2000 · N224US · Boeing 737201 · Emergency LightingSDR USAASB00088Landing Gear · malfunctionedIAD - FLT 2739 - ON CLIMB-OUT FROM IAD, CAPTAIN COULD NOT RETRACT THE NOSE GEAR. GEAR WAS RECYCLED WITH SAME RESULT. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. IT WAS NOTED THAT CREW HAD ALL THREE GREEN SAFE LIGHTS. FLIGHT TAXIED Mar 26, 2000 · N247US · Boeing 737201 · Nose/Tail Landing GearSDR USAASB00086Controller · malfunctionedTPA - FLT 2970 - ON CLIMB-OUT FROM TPA, AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PULLED AND RESET CIRCUIT BREAKERS. RESEATED CABIN PRESSURE CONTROMar 25, 2000 · N261AU · Boeing 737201 · Cabin Pressure ControllerSDR USAA000388Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 15L FASTENER HOLES BS 538. INSTALLED REPAIR FILLER AND DOUBLER PER EA 66891. (M)Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000387Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCHES, BS 538, 1 INCH BELOW STRINGER 14L. INSTALLED DOUBLER PER EA 66891. (M)Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00075Battery · dischargedCLE - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE FORWARD MAIN ENTRY DOOR WOULD NOT STAY ILLUMINATED FOR MORE THAN 30 SECONDS. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (X)Mar 21, 2000 · N252AU · Boeing 737201 · Emergency LightingSDR USAA000384Skin · crackedTPA - FOUND FUSELAGE SKIN CRACKED, STATION 727A PLUS 8 INCHES AT STRINGER 18L. REPAIRED PER SRM 53-30-3 FIG 6. (M)Mar 20, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000383Frame · corrodedTPA - FOUND CORROSION ON FRAME, STATION 827 BETWEEN STRINGER 27L AND 27R. CORROSION LEVEL 1. REMOVED CORROSION AND SPLICED IN NEW PIECE PER SRM 53-10-4. (M)Mar 20, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAASB00073Controller · failedIAD - FLT 2808 - ON CLIMB OUT FROM IAD, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED CABIN PRESSURE CONTROLLER FUNCTIONAL TESTMar 18, 2000 · N242US · Boeing 737201 · Cabin Pressure ControllerSDR USAA000337Skin · crackedCLT - FOUND 1 INCH CRACK FUSELAGE, STATION 947.5 STRINGER 24L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 6. (M)Mar 10, 2000 · N252AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000334Skin · crackedCLT - FOUND 1 INCH CRACK FUSELAGE SKIN, STATION 947.5 STRINGER 24L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 6. (M)Mar 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00066Light · inoperativeORD - PILOT REPORTED THE EMERGENCY EVACUATION LIGHT AT SEAT ROW 16 ABC IS INOPERABLE AND THE WIRING UNDER SEAT 16C IS HANGING DOWN. MAINTENANCE REPAIRED WIRING AND RESECURED WIRING UNDER SEAT ROW 16C. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (X)Mar 6, 2000 · N240AU · Boeing 737201 · Emergency LightingSDR USAA000309Skin · crackedCLT - FOUND TWO CRACKS, 3.5 INCH AND 1 INCH, LT FUSE EXT STATION 759-763 AND STATION 780-781 STRINGER 17L. REPAIRED PER EA 66792. (M)Mar 6, 2000 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00064Battery Pack · failedCLE - MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT SIGNS BLINKING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Mar 6, 2000 · N263AU · Boeing 737201 · Emergency LightingSDR USAASB00062O-Ring · failedBWI - FLT 2635 - DURING CRUISE, EN ROUTE FROM BOS TO FLL, FLIGHT LOST SYSTEM A HYDRAULICS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. Mar 5, 2000 · N245US · Boeing 737201 · Drag Control ActuatorSDR USAA000292Stringer · corrodedCLT - FOUND 3 INCH BY 1 INCH OF CORROSION AT BS 980 TO 988, STRINGER 27L. INSTALLED NEW STRINGER PIECE PLU SPLICE PER SRM 53-10-3 FIG 1. CORROSION LEVEL 1. (M)Mar 1, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000287Bracket · corrodedCLT - CORROSION LEVEL 1, ANTENNA BRACKET CORRODED BETWEEN BS 500 AND 500B STRINGER 28L AND 28R. INSTALLED NEW PARTS PER SRM 51-10-01. (M)Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000288Frame · crackedCLT - FRAME CRACKED AT BS 663.75 STRINGER 3L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAA000289Frame · crackedCLT - FRAME CRACKED AT BS 663.75, STRINGER 2L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAA000290Frame · crackedFRAME CRACKED AT 663.75 STRINGER 2R. INSTALLED DOUBLER PER SRM 53-10-4 FIG 14. (M)Feb 29, 2000 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAA000286Angle · crackedCLT - FOUND 1.5 INCH CRACK ATTACH ANGLE, BS 664, STRINGER 18A, ATTACH ANGLE IT W/W. FABRICATED ATTACH ANGLE PER EO 5393G256 AND SRM 51-40-03. (M)Feb 28, 2000 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB00056Packing · failedCLT - FLT 7900 - WHILE ON TEST HOP, APPROACHING CLT, THE A HYDRAULIC SYSTEM LIGHT BEGAN FLICKERING. CAPTAIN SHUT DOWN PUMPS AND STARTED GETTING THE B HYDRAULIC SYSTEM LIGHT FLICKERING. CAPTAIN DECLARED AN EMERGENCY AND LANDED AT CLT WITHOUT FURTHER INCIDENT.Feb 28, 2000 · N260AU · Boeing 737201 · Hydraulic Filter, MainSDR USAA000275Floorbeam · crackedCLT - FOUND CRACK IN T-CAP, 2 INCHES, BL 0 AT STATION 663. INSTALLED REPAIR STRAPS AND ANGLES PER TR 57-10-04. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000276Web · crackedCLT - FOUND 4 CRACKS, .5 INCH, LBL 25, STATION 710 TO 714. INSTALLED DOUBLER PER EA 66602. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000277Tie Clip · crackedCLT - FOUND CRACK TIE CLIP .25 INCH, STATION 578, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000278Frame · crackedCLT - FOUND 2 INCH CHORD ANGLE CRACK, STATION 1138, STRINGER 5AL. INSTALLED CHORD SECTION AND DOUBLER PER SRM 51-40-3 FIG 1. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAA000279Stringer · corrodedCLT - FOUND CORROSION LEVEL 1, 6 INCHES, STATION 1006 STRINGER 24L. INSTALLED NEW PART PER SRM 51-10-1 FIG 1. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000280Fitting · corrodedCLT - FOUND CORROSION LEVEL 1, .5 INCH, INBOARD STAB FITTING ON GEAR BEAM INSIDE FLANGES. INSTALLED NEW PART PER SRM 20-10-19. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000281Frame · corrodedCLT - FOUND CORROSION LEVEL 1, 1 INCH BY 2 INCH, STATION 500B ABOVE STRINGER 26R UNDER TRANSITION PANEL AND FRAME. INSTALLED REPAIR DOUBLER PER SRM 53-10-4. (M)Feb 28, 2000 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAASB00054Hydraulic System · malfunctionedRDU - FLT 2746 - EN ROUTE FROM TPA-BOS, CAPTAIN SENT ACARS, MAY BE LOSING B SYSTEM HYDRAULICS. CAPT REPORTED B SYSTEM HYDRAULICS STARTED A STEADY DECLINE IN PRESSURE. CAPT DECLARED AN EMERGENCY AND DIVERTED TO RDU. FLT LANDED WITHOUT INCIDENT AND TAXIED TO Feb 27, 2000 · N248US · Boeing 737201 · Hydraulic Power SystemSDR USAASB00053Hydraulic Line · leakingJAX - FLT 2704 - EN ROUTE FROM TPA-BWI, AT FL290, CREW CONTACTED DISPATCH VIA ACARS THAT FLT LOST SYSTEM A HYD. AT THIS TIME, IT WAS DETERMINED TO CONTINUE TO BWI. HOWEVER, ANOTHER MESSAGE WAS RECEIVED FROM ACARS STATING THAT BOTH LOW PRESSURE LIGHTS WERE ONFeb 26, 2000 · N259AU · Boeing 737201 · Hydraulic System, MainSDR USAA000260Bulkhead · crackedBULKHEAD HAS A .25 INCH CRACK AT BS 663, LBL 25. SPLICED IN DOUBLER PER EA 66610 AND SB 737-53-1184. (M)Feb 24, 2000 · N260AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA000261Skin · crackedSKIN HAS A 3 INCH CRACK AT BS 727B STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 53-30-6 FIG 6. (M)Feb 24, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000262Skin · crackedSKIN HAS A 1 INCH CRACK AT 490 STRINGER 24. INSTALLED REPAIR DOUBLER, TRIPLER AND QUADRUPLER PER EA 54235. (M)Feb 24, 2000 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000263Skin · crackedSKIN HAS A 2.5 INCH CRACK AT BS 980, STRINGER 21L. INSTALLED DOUBLER PER SRM 53-303 FIG 1. (M)Feb 24, 2000 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000256Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 950, STRINGER 10R. INSTALLED FILLER AND DOUBLER PER TR 53-30-07. (M)Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000229Skin · crackedCLT - SKIN AT BS 947 BETWEEN STRINGER 11R AND 12R HAS A .125 INCH CRACK. INSTALLED DOUBLER PER SRM 53-30-3. (M)Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000230Stringer Clip · crackedCLT - STRINGER CLIP CRACKED AT BS 727B STRINGER 7L. REPLACED TIE CLIP PER SRM 51-10-1. (M)Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000231Channel · crackedCLT - CHANNEL HAS A 2 INCH CRACK AT BS 520 RBL 25 WL 206. INSTALLED PIVOT LINK PER SB 737-53-1120. (M)Feb 22, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000235Skin · crackedTPA - SKIN HAS A 1.5 INCH CRACK AT BS 727A STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 2 FIG 1. (M)Feb 22, 2000 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000236Skin · crackedTPA - SKIN HAS A .25 INCH CRACK AT BS 303.9. INSTALLED DOUBLER AND FILLER PER SRM 53-3-3 PAGE 76 FIG 21. (M)Feb 22, 2000 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000244Angle · crackedCLT - ANGLE CRACKED AT STATION 1138 ON HORIZ STABILIZER. REPAIRED PER SRM 51-40-3 FIG 1. (M)Feb 22, 2000 · N260AU · Boeing 737201 · Horizontal Stabilizer StructureSDR USAA000206Stiffener · crackedCLT - FOUND CRACK IN STIFFENER 1.75 INCHES, STATION 178, LBL 5.5 LOWER AFT SIDE VERTICAL STIFFENER. INSTALLED DOUBLER PER TR 53-10-17 AND SRM 20-40-04. (M)Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000196Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 765, STRINGER 19R FUSELAGE SKIN. REPAIRED PER SRM 53-30-3 FIG 6. (M)Feb 15, 2000 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA0209Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706, STRINGER 10L TIE CLIP. INSTALLED CLIP PER EO5393G227. (M)Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA0210Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .750 INCH LONG CRACK AT BS 707 TO 710, RBL 25 WEB. INSTALLED DOUBLER PER EA 66602. (M)Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA0211Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 616, STRINGER 5R CLIP. REPAIRED PER EO 5393G227. (M)Feb 15, 2000 · N260AU · Boeing 737201 · Fuselage Miscellaneous Structure
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