Boeing 737-2B7

Service difficulty reports · 1,360

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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 = '7372B7'
  ORDER BY difficulty_date DESC"

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SDR USAASB00296Duct · crackedTPA-LGA - FLT 2676 - AFTER TAKEOFF, THE RIGHT ENGINE START VALVE LIGHT AND THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. 15 MINUTES SINGLE ENGINE TIME. MAINTENANCE FOct 18, 2000 · N282AU · Boeing 7372B7 · Engine Anti-Icing SystemSDR USAASB00292Circuit Breaker · defectiveTYS - FLT 2700 - EN ROUTE FROM BWI TO MSY, AT FL310, THE NR 1 TRANSFER BUS CIRCUIT BREAKER TRIPPED WHICH AFFECTED CAPTAINS AVIONICS AND THE CABIN PRESSURIZATION TO RISE. CAPTAIN ACCOMPLISHED AN EMERGENCY DESCENT TO FL110 AND TRIED TO RESET CIRCUIT BREAKER. COct 16, 2000 · N285AU · Boeing 7372B7 · AC Power Distribution SystemSDR USAA001734Skin · crackedTPA - FOUND SKIN CRACKED 2 INCHES, LT HORIZ STAB LOWER SKIN STATION 188. INSTALLED REPAIR DOUBLER PER SRM 55-10-3 FIG 3. (M)Oct 12, 2000 · N285AU · Boeing 7372B7 · Horizontal Stabilizer, Plate/SkinSDR USAASB00287Gcu · malfunctionedRDU - FLT 2990 - EN ROUTE FROM LGA TO PBI, THE NR 1 BUS OFF LIGHT ILLUMINATED. CREW STARTED APU BUT WAS UNABLE TO POWER THE BUS. FLIGHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANE FOUND A TENNIS RACKET BEHIND Oct 5, 2000 · N285AU · Boeing 7372B7 · AC RegulatorSDR USAASB00285Windshield · crackedBDL - FLT 2612 - EN ROUTE FROM MHT TO BWI, THE FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. COCKPIT VISION WAS AFFECTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO BDL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFIOct 4, 2000 · N267AU · Boeing 7372B7 · Flight Compartment WindowsSDR USAASB00284Actuator · leakingEWR - FLT 2636 - EN ROUTE FROM PBI TO LGA, CAPTAIN NOTICED THAT SYSTEM A HYDRAULIC QUANTITY HAD DECREASED FROM 2.2 GALLONS TO 1.2 GALLONS. ON DESCENT TO LGA, AS AIRCRAFT SLOWED AND FLAPS WERE EXTENDED, HYDRAULIC QUANTITY WENT TO .5 GALLONS. CREW WAS ABLE TO Oct 3, 2000 · N282AU · Boeing 7372B7 · Drag Control ActuatorSDR USAASB00281Panel · failedBDL - FLT 2742 - ON APPROACH INTO BDL, FROM FLL, FLIGHT EXPERIENCED A COMPLETE LOSS OF ALL ELECTRICAL, INCLUDING PRESSURIZATION. STANDBY POWER AND BATTERY POWER WERE FINE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BUS PROTECTION POct 1, 2000 · N275AU · Boeing 7372B7 · AC Power Distribution SystemSDR USAASB0279Fuel Control · failedBWI - FLT 2797 - ON CLIMB-OUT FROM BWI, AT FL080, THE NR 2 ENGINE FLAMED OUT. N1, N2 AND OIL PRESSURE WAS PRESENT. CREW TRIED TO RESTART/RELIGHT NR 2 ENGINE, BUT COULD NOT. AN EMERGENCY WAS DECLARED AND THE PASSENGERS WRE BRIEFED ON EMERGENCY PROCEDURES. FSep 30, 2000 · N268AU · Boeing 7372B7 · Fuel Control/Turbine EnginesSDR USAASB00278Wire · chafedLGA - FLT 2984 - EN ROUTE FROM JAX-LGA, AT FL310, FLIGHT ENCOUNTERED A COMPLETE ELECTRICAL FAILURE FOR THREE SECONDS. BOTH GENERATORS NEVER TRIPPED, JUST ALL ELECTRICAL WENT OUT. STANDBY POWER WORKED FINE. BOTH AUTOPILOTS DISENGAGED AND PRESSURE WAS NORMAL.Sep 29, 2000 · N275AU · Boeing 7372B7 · Electrical Power System WiringSDR USAASB00265Acm · leakingBWI - FLT 2704 - ON DESCENT INTO BWI, FROM TPA, FUMES OF SULFUR/RUBBER SMELL WAS NOTICED THROUGH OUT THE CABIN. ODOR WAS STRONGEST IN SEAT ROWS 13 TO 17 AND WAS MOST NOTICEABLE WHEN ENGINE ANTI-ICE WAS SELECTED. SMELL DISSIPATED WHEN ENGINE ANTI-ICE WAS TURNSep 20, 2000 · N286AU · Boeing 7372B7 · Cabin Cooling SystemSDR 20000920SH018Stringer Clip · crackedPARTS PURCHASED NEW FROM BOEING STOCK, FOUND CRACKED IN OUTSIDE RADII OF CLIP IN EXTERNAL LAMINATE. (X)Sep 20, 2000 · Boeing 7372B7 · Fuselage Structure (General)SDR USAASB00261Motor · failedORD - FLT 2658 - EN ROUTE FROM BWI TO MDW, FLIGHT ENCOUNTERED A FLAP PROBLEM. WHILE CONFIGURING AIRCRAFT FOR LANDING, FLAPS WOULD NOT EXTEND BEYOND 15 DEGREES. HYDRAULIC PRESURE WAS NORMAL. CREW EXECUTED A MISSED APPROACH AND THE FLAPS RETRACTED NORMALLY. Sep 17, 2000 · N275AU · Boeing 7372B7 · Trailing Edge Flap Control SystemSDR USAASB00254Landing Gear · failedEWR - FLT 2621 - AFTER TAKEOFF FROM LGA, EN ROUTE TO MCO, CREW COULD NOT GET LANDING GEAR TO RETRACT AS GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. FLIGHT DIVERTED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHSep 13, 2000 · N266AU · Boeing 7372B7 · Landing Gear Retraction/Extension SystemSDR USAASB00253Cooler · failedTPA - FLT 2746 - ON CLIMB-OUT FROM TPA, AT APPROX 12,000 FEET, THE CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE AND HIGH OIL PRESSURE. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINSep 13, 2000 · N277AU · Boeing 7372B7 · Engine Oil CoolerSDR USAA001418Skin · crackedPIT - FOUND ON WALKAROUND, SKIN CRACKED 1.5 INCHES, BS 727 WL 208.1 A/C RT. INSTALLED EXTERNAL DOUBLER (8.5 BY 12) PER SRM 53-30-03 FIG 6. (M)Aug 29, 2000 · N288AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA001351Stringer · corrodedTPA - FOUND STRINGER CORRODED 2 INCHES, STATION 986.5, STRINGER 27 LEFT. INSTALLED NEW SECTION OF STRINGER PER SRM 53-10-3 FIG 1. (M)Aug 25, 2000 · N286AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA001316Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A RIGHT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-02. (M)Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA001318Pressure Panel · crackedCLT - FOUND PRESSURE DECK WEB CRACKED .5 INCH, STATION 670, RBL 12. INSTALLED FILLER AND DOUBLER PER EA 67747. (M)Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Floor PanelSDR USAA001317Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A LEFT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-1. (M)Aug 24, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA001299Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, AFT SPAR, AFT OUTBOARD CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical StabilizerSDR USAA001298Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, FRONT CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA001297Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, AFT CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical StabilizerSDR USAA001296Clevis · corrodedCLT - FOUND AFT SPAR CLEVIS CORRODED .013 INCH BY .028 INCH, VERT FIN, AFT SAPR, AFT OUTBOARD CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7 · Vertical StabilizerSDR P2EA000237Slat · lack of lubeMCI - FLT 821 - NR 3 SLAT PARTIAL EXTENDED AT FLAPS 5. QRH ACCOMPLISHED. FLAPS EXTENDED NORMALLY ON FINAL. LANDING WAS UNEVENTFUL. MEASURED DETENT ARMS AND FOUND WITHIN LIMITS PER MM 27-81-21. LUBRICATED NR 3 SLAT PER MM 12-22-71. OPERATIONALLY CHECKED FAug 20, 2000 · N127NJ · Boeing 7372B7 · Leading Edge Slat Control SystemSDR USAASB00221Acm · inadequateMIA - FLT 2738 - ON TAKEOFF, AT 100 KNOTS, THE AFT CARGO DOOR LIGHT ILLUMINATED AND THE AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMB. CREW ACCOMPLISHED CHECKLISTS, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIAug 18, 2000 · N266AU · Boeing 7372B7 · Cabin Cooling SystemSDR USAASB00229Power Supply · failedIAD - MAINTENANCE FOUND THE OUTBOARD EXTERIOR EMERGENCY LIGHT FOR THE RIGHT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK NORMAL. (M)Aug 17, 2000 · N269AU · Boeing 7372B7 · Emergency LightingSDR USAA001281Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, AFT SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-03 AND EA 67849. (M)Aug 17, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA001254Gusset · crackedCLT - FOUND GUSSETT CRACKED .5 INCH, NLG ACTUATOR ATTACH BEAM GUSSETT, STATION 259.5, BL 0. INSTALLED NEW PART PER SRM 51-30-00. (M)Aug 15, 2000 · N282AU · Boeing 7372B7 · Landing Gear Retraction/Extension SystemSDR USAA001236Torque Box · crackedCLT - FOUND TORQUE BOX CRACKED .25 INCH, STATION 1112, LEFT SIDE JUST BELOW UPPER TORQUE BOX. INSTALLED DOUBLER AND FILLER PER EA 67773 AND SRM 51-40-3. (M)Aug 14, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, StructureSDR USAA001237Strap · crackedCLT - FOUND STRINGER STRAP CRACKED .75 INCHES LONG, 2 INCHES AFT OF STATION 1138, RT SIDE. INSTALLED REPAIR PER EA 67733, AND SRM 53-00-01 FIG 221. (M)Aug 14, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB00212Battery · dischargedBWI - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES, TWO EACH. OPERATIONAL CHECK NORMAL. (M)Aug 8, 2000 · N279AU · Boeing 7372B7 · Emergency LightingSDR USAASB00211Battery Pack · dischargedBWI - MAINTENANCE FOUND THE EXTERIOR LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Aug 8, 2000 · N266AU · Boeing 7372B7 · Emergency LightingSDR USAA001207Clip · crackedCLT - FOUND ATTACH CLIP CRACKED .5 INCH, STATION 380, STRINGER 26L ON BAFFLE ATTACH CLIP. REPLACED PER SRM 51-10-01. (M)Aug 7, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001206Shim · crackedCLT - FOUND SHIM CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 22R AND STRINGER 23R. REPLACED ATTACH CLIP SHIM PER SRM 51-10-01. (M)Aug 7, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001157Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 440, STRINGER 22R. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)Aug 4, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001149Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 2 INCHES, BS 663, BL 0. INSTALLED STIFFENER FILLER AND DOUBLER PER EA 67727. (M)Aug 4, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA001141Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 907, STRINGER 21R FUSELAGE FRAME UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3. (M)Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA001140Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 328 AFT LOWER CORNER FS 0 CUTOUT. INSTALLED DOUBLER PER TR 53-10-19A. (M)Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA001139Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STRINGER 13 STATION 1138. INSTALLED NEW TIE CLIP PER SRM 51-10-01. (M)Aug 2, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001112Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 951 FRAME WL 254 RT SIDE. FABRICATED REPAIR AND INSTALLED PER TR 53-30-07A. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA001111Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 951 FRAME, WL 254 LT SIDE. FABRICATED AND INSTALLED REPAIR PER TR 53-30-07A. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA001110Cap · corrodedCLT - FOUND T-CAP CORRODED 2 INCHES, FS 312, RBL 35. CUTOUT DAMAGED FABRICATED REPAIR AND INSTALLED PER 53-10-9 FIG 5. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001109Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 727B, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001108Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 685, STRINGER 4. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001107Clip · crackedCLT - FOUND CLIP CRACKED .250 INCH, STATION 685, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001106Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, FS 663, STRINGER 10L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001105Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 3R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001104Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, FRAME 597 AT STRINGER 8L TIE CLIP. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Aug 1, 2000 · N282AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA001138Frame · corrodedTPA - FOUND FRAME WEB CORRODED 4 INCHES BY 3 INCHES, FRAME STATION 277, LT LOWER LOBE. REPLACED SECTION PER SRM 51-40-2 FIG 1, SRM 53-10-4 FIG 9A EA 66638. (M)Aug 1, 2000 · N268AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAASB00203Indicator · failedJAX - FLT 2675 - EN ROUTE FROM BOS-TPA, NEAR SAV, SYSTEM A HYDRAULIC QUANTITY SLOWLY DROPPED FROM REFILL (RF)TO ONE GALLON IN ABOUT 2 HOURS OF FLIGHT. NO LOW PRESSURE OR OVERHEAT LIGHT WAS NOTED. CREW RECYCLED HYDRAULIC QUANTITY BREAKER WITH NO CHARGE. CREWJul 31, 2000 · N285AU · Boeing 7372B7 · Hydraulic Quantity Indicator
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