Boeing 737-282C

Service difficulty reports · 121

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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 = '737282C'
  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 TSAA20130822007Clamp · failedDURING CLIMB, AT 3000 FT, CREW NOTICED THE LT WING TO BODY OVERHEAT WARNING LIGHT ILLUMINATED. AFTER 2 MINUTES, THE RT WING TO BODY OVERHEAT WARNING ALSO ILLUMINATED. RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED DUCT CLAMP AT THE KEAug 22, 2013 · N826AL · Boeing 737282C · Pneumatic Distribution SystemSDR TSAA20120713004Engine · power lossDURING TAKEOFF/CLIMB AT APPROXIMATELY 400 FEET, NR 2 ENGINE FAILURE/LOSS OF POWER WITH HEAVY VIBRATION. COMPLETED ENGINE FAILURE AND SHUTDOWN CHECKLIST. INFLIGHT EMERGENCY DECLARED. REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD.Jul 13, 2012 · N826AL · Boeing 737282C · Engine (Turbine/Turboprop)SDR TSAA20120531002Frame · crackedCRACK APPROX 2.6250 FOUND AT BS 927, STRINGER 23L. REPAIR COMPLIED WITH IAW SRM 53-30-3, FIG 48, DETAIL XI.May 31, 2012 · N826AL · Boeing 737282C · Fuselage Main, FrameSDR 7AHR201192030Frame · crackedAFT PIT CRACKED, FRAME LOWER CHORD AT BS 907 AND STRINGER 26R.Oct 16, 2011 · N826AL · Boeing 737282C · Fuselage Main, FrameSDR 7AHR2011092029Seat Track · crackedMAIN CABIN SEAT TRACK UPPER FLANGE CRACKED STATION 727B AT RBL 24.75Oct 8, 2011 · N826AL · Boeing 737282C · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR2011092028Floorbeam · corrodedUPPER FUSELAGE FLOOR STRUCTURE HEAVY AMOUNT OF CORROSION UNDER NUTLPLATE ON LOWER CHORD OF FLOORBEAM AT BS 787 AT RBL 24Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor BeamSDR 7AHR2011092027Beam · elongatedDURING THE ACCOMPLISHMENT OF ECO 3731 SB 737-57A-1266 INSPECTION OF THE MAIN LANDING GEAR BEAM TO WING ATTACH FITTINGS IT WAS DISCOVERED THAT THE MLG BEAM PIN RETAINER LOCK BOLT FITTING IS ELONGATED ON BOTH LT AND RT MLG BEAM.Sep 23, 2011 · N826AL · Boeing 737282C · Wing, Landing Gear Attach FittingsSDR 7AHR2011092026Skin · corrodedAFT FUSELAGE HAS EVIDENCE PILLOWING (CORROSION) AT BODY STA 1016 AT STR 25L AND 24L AROUND FASTENERS.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092025Floor Support · corrodedAFT FUSELAGE CABIN FLOOR STURCTURE AT BODY STA 947 TO 967 AT LBL 12 HAS EVIDENCE OF CORROSION.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092024Floor Support · corrodedAFT BAGAGGE COMPARTMENT FLOOR SUPPORTS AT BODY STATION 770 AT SPLICE STRAP ATTACHED HAS SIGNS OF CORROSIONSep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092023Transition Panel · corrodedAFT PIT TRANSITION PANEL CORRODED JUST AFT OF CARGO DOOR ON THE RT SIDE AT BODY STATION 887.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092022Skin · corrodedAFT FUISELAGE BODY STA 976.6 AT STRINGER 25L, EDGE OF WATER SERVICING DOOR HAS EVIDENCE OF CORROSION.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092021Stringer · corrodedAFT BAGGAGE COMPARTMENT AT BODY STA 947.6, STRINGER 26L, HAS CORROSION OUT OF LIMITS.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Longeron/StringerSDR 7AHR2011092020Intercostal · corrodedAFT BAGGAGE COMPARTMENT INTERCOSTAL UPPER FLANGE CORRODED OUT OF LIMITS BETWEEN BODY STATION 767 AND 787 AT STRINGER 25RSep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092019Threshold · corrodedFORWARD FUSELAGE FLOOR STRUCTURE AT L1 DOOR CENTER THRESHOLD AREA HAS LIGHT CORROSION ON UPPER SURFACE STRUCTURE AND UNDER NUTPLATESSep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092018Floor Support · corrodedFORWARD CABIN FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT LBL 6 BETWEEN BODY STATION 294.5 AND 312.0.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092017Floor Support · corrodedAFT BAGGAGE COMPARTMENT FLOOR SUPPORT SPLICE PLATE HAS SIGNS OF CORROSION ON BOTTOM SIDE AT BODY STA 770.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092016Floor Support · corrodedCORROSION UNDER TIE DOWN AT STRINGER 26R AT SHEAR TIE FLOORBOARD SUPPORT AT BODY STATION 384.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092015Floorbeam · corrodedAFT FUSELAGE FLOOR STRUCTURE HAS CORROSION AT FLOOR SUPPORT BODY STA 957 BETWEEN RT SIDE OF SEAT TRACKS AT RBL 24 AND 45.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor BeamSDR 7AHR2011092014Floor Support · corrodedAFT FUSELAGE FLOOR STRUCTURE AT LT LAVATORY WALL, FLOOR IS CORRODED AT BODY STATION 947 TO 967.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092013Sill · corrodedFORWARD CABIN FLOOR STURCTURE AT BODY STATION 312 TO 344 AT MOP SILL HAS CORROSION AROUND FASTNER HOLES.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092012Floorbeam · corrodedFORWARD CABIN FLOOR STRUCTURE (FRAME) HAS CORROSION AT BODY STA 312 BETWEEN RBL 24 AND RBL 45.Sep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Floor BeamSDR 7AHR2011092011Skin · crackedDURING THE ACCOMPLISHMENT OF ECO 3735, FORWARD ENTRY AND FORWARD GALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT INSPECTION, IT WAS DETERMINED THAT THE FORWARD ENTRY DOOR, LOWER HINGE CUTOUT HAS 1 EACH CRACKED FASTENER HOLE. CRACK IS IN THE LOWER B-5 HOLESep 23, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092010Skin · corrodedAFT PIT AT STATION 907 TO 929 AT STRINGER 26R HAS CORROSION AROUND FASTENER. FASTENERS ARE PULLING THROUGH.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092009Floor Support · corrodedAFT FUSELAGE FLOOR STRUCTURE HAS CORROSION ON FLOOR SUPPORT AT BODY STATION 955 INBD OF SEAT TRACK AT RBL 24.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092008Floor Support · corrodedAFT BAGGAGE COMPARTMENT FLOOR SUPORT AT RBL 8" HAS CORROSION THAT IS OUT OF LIMITS AT SPLICE STRAP BODY STA 770.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092007Skin · corrodedCORROSION AROUND FASTNERS AT LT LOWER SURFACE OF WING AT STATION WRL 167 BEHIND FUEL ACCESS PANEL NR 7204.Sep 22, 2011 · N826AL · Boeing 737282C · Wing, Plate/SkinSDR 7AHR2011092006Floor Support · corrodedAFT PIT FLOOR SUPPORT AT BODY STATION 770 HAS CORROSION AND WAS FOUND TO BE OUT OF LIMITS AT SPLICE STRAPSep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092005Angle · corrodedAFT FUSELAGE FLOOR STRUCTURE AT AFT LAVATORY FORWARD WALL AS CORROSION AT ATTACH ANGLE AT INBD FASTENER HOLE.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR 7AHR2011092004Skin · corrodedPILLOWING CORROSION AROUND FASTENERS AT BODY STA 787, STRINGER 27R.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092003Structure · corrodedCORROSION UNDER FLOORBOARD SPLICE AT STA 464 BETWEEN STRINGER 27R AND 26R IN FORWARD PIT.Sep 22, 2011 · N826AL · Boeing 737282C · Fuselage Main, StructureSDR 7AHR2011092001Skin · corrodedFUSELAGE LOWER LOBE AT BODY STATION 807 TO 827 AT STRINGER 26R TO 27R HAS EVIDENCE OF PILLOWING (CORROSION).Sep 21, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR 7AHR2011092002Access Panel · corrodedAFT FUSELAGE AT POTABLE WATER SERVICING PANEL HAS EVIDENCE OF CORROSION AROUND PANEL.Sep 21, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR TSAA2011F00203Skin · corrodedFUSELAGE LOWER LOBE BETWEEN STA 827 AND 807 AT STRINGER 27R AND 26R HAS POSSIBLE PILLOWING AROUND FASTENERS (CORROSION).Sep 20, 2011 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR TSAA1126004Connector · shortedDURING CRUSE FLIGHT, THE CREW NOTED THE NR1 ENGINE OVERHEAT WARNING LIGHT ILLUMINATED. THE CONDITION WAS INTERMITTENT AND EXTINGUISHED. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MX FOUND A SHORTED CONNECTOR IN THE LOWER FIRE AND OVERHEAT DETECTOR LApr 9, 2011 · N826AL · Boeing 737282C · Fire Protection System WiringSDR TSAA1012020Unknown · odorNON-ETOPS CARGO FLIGHT 25. UPON ARRIVAL, AN ELECTRICAL ODOR WAS REPORTED BY THE PILOT IN THE COCKPIT. MX INSPECTED COCKPIT AND FOUND NO DEFECTS OR ODORS. MX INSPECTED THE E & E BAY AND FOUND WATER IN THE BAY. ACFT WAS TOWED TO HANGAR, DRIED OUT, AND RETURNDec 19, 2010 · N826AL · Boeing 737282C · Air Distribution SystemSDR TSAA1053017Stiffener · corrodedWING CTR SECTION LOWER BEAM AT RBL 40.875 IS CORRODED AT BS 612 AND BS 630. MAINTENANCE ACTION: REPLACED ANGLE IN ACCORDANCE WITH SRM 51-10-1. CLEANED AND TREATED AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-6 AND FOUND WITHIN LIMITS.Oct 5, 2010 · N826AL · Boeing 737282C · Fuselage Miscellaneous StructureSDR TSAA1026012Circuit Breaker · failedDURING CLIMB, THE CREW NOTED THE NR 2 TRANSFER BUS CIRCUIT BREAKER POPPED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE NR 2 TRANSFER BUS CIRCUIT BREAKER (C821) AND OPERATIONALLY CHECKED SATISFACTJun 15, 2010 · N826AL · Boeing 737282C · DC Power Distribution SystemSDR TSAA1026011Relay · failedNON-ETOPS CARGO FLIGHT 16. DURING CLIMB THE ACFT EXPERIENCED A NR2 BUS POWER FAILURE CAUSING THE LOSS OF USE OF ALL INSTRUMENTS AND SYS POWERED BY THE NR 2 BUS. CREW ACCOMPLISHED APPROPRIATE CHECK LISTS LANDED WITHOUT FURTHER INCIDENT. MX R & R THE NR2 TRANJun 14, 2010 · N826AL · Boeing 737282C · DC Power Distribution SystemSDR TSAA0953011Skin · crackedDURING SCHEDULED INSP A 3" CRACK WAS DISCOVERED AT BS 440, 450, S-16R FUSELAGE SKIN. REPAIRED SKIN BY REMOVING CRACK DEFECT, CONDUCTED HFEC INSP, ENLARGED TRIM BY 0.040" INSURANCE CUT, INSTALLED DOUBLER/ TRIPLER, MAINTAINED A 0.5" MIN. CORNER RADIUS, MAINTAINNov 23, 2009 · N841AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR TSAA0977007Transmitter · defectiveON TAKEOFF, NR 1 EPR FROZE AT 1.14 WHILE SETTING TAKEOFF POWER. OTHER NR 1 INDICATIONS NORMAL. ABORTED TAKEOFF AT 70 KTS. RETURNED TO RAMP. MX: REMOVED AND REPLACED EPR INDICATOR, DID NOT FIX. REMOVED AND REPLACED EPR TRANSMITTER IAW AMM 77-11-21. OPS CHJul 21, 2009 · N826AL · Boeing 737282C · Engine Pressure Ratio (EPR)SDR TSAA0932003Uplock Sensor · dirtyFLT 11, HNL- LIH - NOSE GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO HNL. ALL THREE GREEN LIGHTS ILLUMINATED WHEN LANDING GEAR EXTENDED. FLIGHT TERMINATED UNEVENTFUL. CLEANED UPLOCK SENSOR. TEST IAW 32-61-41. OPERATIONAL CHECK/GEAR SWING OKAY. Apr 16, 2009 · N826AL · Boeing 737282C · Landing Gear Position and WarningSDR TSAA0932002Control Cable · out of adjustFLT 320: TEST FLIGHT, LANDING GEAR LEVER WOULD NOT GO UP AFTER TAKEOFF. WARNING HORN ON AFTER FLAP RETRACT. RETURNED TO SJO, UNEVENTFUL LANDING. PERFORMED ADJUSTMENT AND TEST FOR THE GROUND SPOILER INTERLOCK VALVE CABLE AS PER MM 27-62-51, PAR 2 AND 3. PERApr 2, 2009 · N826AL · Boeing 737282C · Landing Gear Retraction/Extension SystemSDR TSAA0952001Switch · obstructedFLT 952, HNL-ITO -ON TAKEOFF, THE AFT CARGO LIGHT CAME ON. RETURNED TO HNL, NO EMERGENCY. MAINTENANCE FOUND A STRAP LODGED BETWEEN THE DOOR AND SWITCH. REPOSITIONED THE STRAP, VERIFIED DOORS OPS CHECK OK. NO PRESSURE PROBLEMS NOTED. AIRCRAFT RETURNED TO SJan 21, 2009 · N826AL · Boeing 737282C · Door Warning SystemSDR TSAA0827019Indicator · failedCARGO FLIGHT 940 HNL-KOA, ON DESCENT TO KOA, THE CREW WAS ONLY ABLE TO EXTEND THE FLAPS TO 8 UNITS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND OPERATIONALLY CHApr 8, 2008 · N826AL · Boeing 737282C · Trailing Flap Position Indicating SystemSDR TSAA0877012Indicator · failedFLIGHT 269 HNL-LIH - AT TAKEOFF, THE CREW NOTED THE NR 1 EGT READ LOW AT APPROXIMATELY 250 DEGREES AND ELECTED TO ABORT THE TAKEOFF AT 90 KTS AIRSPEED. THE AIRCRAFT WAS TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NRMar 4, 2008 · N826AL · Boeing 737282C · Engine EGT/TIT Indicating SystemSDR TSAA0829008Hose · failedNON-ETOPS FLIGHT 215 HNL-LIH, DURING CRUISE FLIGHT, THE CREW NOTED THE HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO. CREW COMPLETED THE HYDRAULIC SYSTEM A FAILURE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCFeb 15, 2008 · N826AL · Boeing 737282C · Hydraulic System, MainSDR TSAA0734055Dadc · failedNON-ETOPS CARGO FLIGHT 946 HNL-KOA - DURING CLIMB, THE CREW NOTED WARNING FLAGS IN THE FIRST OFFICER’S AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED INDICATOR. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITALOct 5, 2007 · N826AL · Boeing 737282C · Air Data ComputerSDR TSAA0753052Skin · crackedWHILE ACCOMPLISHING VISUAL INSPECTION DURING SERVICE CHECK, A CRACK WAS DISCOVERED AT BS 306 AT STR 18. MAINTENANCE ALONG WITH ENGINEERING IS RESEARCHING THE REPAIR. ECO 3673 REPAIRED CRACKED. 8100-9 WAS RECEIVED FROM BOEING. AIRCRAFT WAS RETURNED TO SERVISep 20, 2007 · N826AL · Boeing 737282C · Fuselage Main, Plate/SkinSDR TSAA0731036Accessory Unit · failedNON-ETOPS FLIGHT 226 HNL-OGG - WHEN THE CREW APPLIED TAKEOFF POWER, THE CONFIGURATION WARNING HORN SOUNDED. CREW ABORTED TAKE OFF AT 60 KNOTS INDICATED AIRSPEED. CREW RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP SLAT Jun 25, 2007 · N826AL · Boeing 737282C · Leading Edge Slat Control System
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