Boeing 737-524

Service difficulty reports · 1,586

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 = '737524'
  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 CALA0300022Oven · inoperativeTHE AIRCRAFT WAS RETURNED TO LAX AFTER SMOKE WAS REPORTED IN THE AFT GALLEY. THE AIRCRAFT LANDED SAFELY AT LAX WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT GALLEY RIGHT OVEN VERY HOT TO THE TOUCH AND THE COMPARTMENT ABOVE THE OVEN WAS ALSO VERY HOT. MAINTENAFeb 2, 2003 · N19623 · Boeing 737524 · Buffet/GalleysSDR CALA0300018Intercostal · crackedINSPECTION FOUND CENTER FLOOR INTERCOSTAL AT CENTERLINE OF AIRCRAFT CRACKED IN TWO PLACES AT STA 344-360. THE CRACKS WERE 1" IN LENGTH. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jan 22, 2003 · N14613 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0300072Skin · damagedMAINTENANCE DISCOVERED A CREASE TO THE FUSELAGE SKIN AT BS 807 BETWEEN S26R AND S27R DURING GROUND OPERATIONS IN CLE. WHEN THE CREASED AREA WAS CUT OUT THE UNDERLYING SHEAR TIE WAS FOUND DAMAGED AND WAS REPLACED. A PERMANENT FUSELAGE SKIN REPAIR WAS PERFORMEJan 18, 2003 · N46625 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200579Skin · damagedINSPECTION FOUND FUSELAGE SKIN CREASED AT STA 826, S28R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.Dec 10, 2002 · N18612 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200568Battery Pack · inoperativeINSPECTION FOUND EMERGENCY EXIT LIGHT OVER L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGHT WAS RESTORED.Dec 1, 2002 · N14662 · Boeing 737524 · Emergency LightingSDR CALA0200567Cargo Track · crackedINSPECTION FOUND A 7 INCH CRACK IN TIE DOWN RAIL AT STA 807, RBL 14. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202.Nov 26, 2002 · N27610 · Boeing 737524 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200566Skin · crackedINSPECTION FOUND A 1/8" CRACK IN SKIN OF CO-PILOT'S WINDSHIELD POST AT UPPER R/H CORNER. A DOUBLER WAS INSTALLED IAW SRM 53-10-01.Nov 26, 2002 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200565Web · crackedINSPECTION FOUND A 2" CRACK IN WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 25, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200562Angle · crackedINSPECTION FOUND A 1" CRACK IN ANGLE AT STA 500-520, BL O. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.Nov 24, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200561Angle · crackedINSPECTION FOUND A 1" CRACK IN ANGLE AT STA 344-360, LBL 12. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 24, 2002 · N27610 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200560Skin · dentedA DENT WAS DISCOVERED IN FUSELAGE SKIN AT STA 360 ABOUT 3" ABOVE CUSP LINE AND 22" AFT OF L-1 DOOR. INSTALLED DOUBLER IAW SRM 53-00-01.Nov 23, 2002 · N27610 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200556Keelbeam · wornINSPECTION FOUND DEEP WEAR ON KEEL BEAM AT BS 710-727, RBL 8 (LOWER FILLET PANEL ATTACH FLANGE). A FILLER AND STRAP REPAIR WAS INSTALLED IAW ECRA 5311-01143.Nov 21, 2002 · N14609 · Boeing 737524 · Fuselage Main, KeelSDR CALA0200554Web · crackedINSPECTION FOUND A 2" CRACK IN MAIN DECK WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.Nov 15, 2002 · N14609 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200521RingLH WHEEL WELL FAIRING SUPPORT RING HAS 16" CRACK. REMOVED AND REPLACED FAIRING RING IAW SRM 51-40-02.Nov 2, 2002 · N14660 · Boeing 737524 · Fuselage Structure (General)SDR CALA0200499Fire Loop · malfunctionedTHE WHEEL WELL FIRE LIGHT ILLUMINATED AND THE FIRE WARNING BELL SOUNDED SHORTLY AFTER THE LANDING GEAR WAS RETRACTED ON TAKEOFF FROM IAH. THE WARNING WAS INTERMITTENT AT FIRST AND EVENTUALLY BECAME STEADY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANED WITHOUOct 17, 2002 · N16617 · Boeing 737524 · Fire DetectionSDR CALA0200496Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB UPPER FLANGE BETWEEN STA 344 AND 360, BL 0. THE FLOOR SUPPORT WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.Oct 12, 2002 · N33608 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200480Solenoid · inoperativeTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. THE GEAR OVERRIDE TRIGGER WAS USED AND THE GEAR RAISED. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A GEAR SWING AND COULD NOT DUPLICATE THE FAILURE. THE LAOct 2, 2002 · N17620 · Boeing 737524 · Landing Gear Retraction/Extension SystemSDR CALA0200442Slide · unserviceableTHE L1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS OUT OF GREEN BAND. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.Aug 26, 2002 · N59630 · Boeing 737524 · Escape SlideSDR CALA0200357Wire · out of positionTHE WHITE EMERGENCY PATH LIGHT AT SEAT 18C WAS FOUND INOPERATIVE DUE TO A PULLED WIRE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81.Jun 19, 2002 · N27610 · Boeing 737524 · Light System WiringSDR CALA0200340Detector · shortedTHE APU FIRE WARNING SOUNDED AFTER APU START ON FINAL APPROACH TO ATL. THE BELL WAS SILENCED AND THE APU FIRE CHECKLIST WAS RUN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE PROBLEM WAS IDENTIFIED AS A FALSE FIRE WARNING ANDJun 12, 2002 · N17644 · Boeing 737524 · Fire DetectionSDR CALA0200334Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 907 BETWEEN S22R AND S23R. REPAIRED IAW SRM 53-00-01, FIGURE 224.Jun 9, 2002 · N16647 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200329Bottle · dischargedTHE R1 DOOR SLIDE BOTTLE PRESSURE WAS FOUND AT ZERO DURING SLIDE INSPECTION. THE R1 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-60-10.Jun 7, 2002 · N16632 · Boeing 737524 · Escape SlideSDR CALA0200328Pin · crackedTHE LT MLG ACTUATOR BEAM ARM FAILED ULTRASONIC INSPECTION. THE AFT LUG (ANTI-ROTATION PIN LUG) HAD A 3 INCH CRACK. THE LT MLG ASSEMBLY WAS REMOVED AND REPLACED IAW MM 32-11-00.Jun 5, 2002 · N59630 · Boeing 737524 · Main Landing GearSDR CALA0200323Skin · crackedINSPECTION FOUND A 1/8" CRACK IN CAPTAIN'S WINDOW POST SKIN AT STA 215. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.May 28, 2002 · N69603 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200167Cargo Track · corrodedINSPECTION FOUND RT TIE DOWN TRACK IN FRONT OF AFT CARGO THRESHOLD CORRODED AT STA 767-870. A NEW TRACK SECTION WAS INSTALLED IAW SRM 53-00-53.Apr 3, 2002 · N69602 · Boeing 737524 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200166Cargo Track · corrodedINSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 877-947. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53.Apr 2, 2002 · N69602 · Boeing 737524 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200165Floor Support · crackedINSPECTION FOUND FOUR 1 INCH CRACKS IN CABIN FLOOR SUPPORT BETWEEN STA 482B AND 520, BL 0. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.Apr 2, 2002 · N69602 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200163Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 540, RBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.Apr 1, 2002 · N69602 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200152Skin · gougedINSPECTION FOUND FUSELAGE SKIN PANEL GOUGED AFT OF L/H HORIZONTAL STABILIZER FORWARD ATTACH FITTING AT STA 1104, WL 265. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01110.Mar 27, 2002 · N33637 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0200138Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD LUG CORRODED. AN OVERSIZED BUSHING WAS INSTALLED IAW MM 55-10-06.Mar 18, 2002 · N33637 · Boeing 737524 · Horizontal Stabilizer StructureSDR CALA0200137Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD AND AFT LUGS CORRODED. OVERSIZED BUSHINGS WERE INSTALLED AT EACH LOCATION IAW CMM 55-10-06.Mar 18, 2002 · N33637 · Boeing 737524 · Horizontal Stabilizer StructureSDR CALA0200083Angle · corrodedINSPECTION FOUND Z-ANGLE IN L-I DOOR AREA CORRODED AT STA 294-360. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-02.Feb 20, 2002 · N19636 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200082Attach Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD ATTACH FITTING ON CENTER BOX LUG FACE CORRODED AROUND BUSHING FORWARD LUG FACE. THE BUSHING WAS REMOVED AND AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06.Feb 18, 2002 · N19636 · Boeing 737524 · Horizontal Stabilizer, Attach FittingsSDR CALA0200072Angle · corrodedINSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 294-312, LOCATED INLINE WITH RIGHT SIDE OF COCKPIT DOORWAY, RBL 12. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.Feb 14, 2002 · N19636 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200063Acm · leakingSMOKE AND FUMES ENTERED THE CABIN AFTER TAKEOFF FROM IAH. SOME ALARMS IN THE CABIN ACTIVATED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE R/H ACM TURBINE OIL SEAL BLOWN. THE R/H ACM AND COALESCER BAG WAS REMOVED ANDFeb 6, 2002 · N14613 · Boeing 737524 · Cabin Cooling SystemSDR CALA0200055Skin · dentedTHE AFT CARGO DOOR SKIN WAS DENTED IN TWO PLACES BY A BELTLOADER. ONE DENT WAS WITHIN LIMITS AND WAS REWORKED TO INITIAL CONTOUR. A DOUBLER WAS INSTALLED AT THE SECOND DENT IAW SRM 52-00-01, FIGURE 203.Jan 29, 2002 · N33635 · Boeing 737524 · Cargo/Baggage DoorsSDR CALA0200043Web · crackedINSPECTION FOUND A 1" CRACK IN WEB AT STA 927-947.5, LBL 26. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.Jan 27, 2002 · N33635 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200042Intercostal · crackedINSPECTION FOUND A 1" CRACK IN INTERCOSTAL AT CABIN FLOOR AREA, STA 344-360. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-00.Jan 26, 2002 · N33635 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200041Web · crackedINSPECTION FOUND A 2" CRACK IN WEB AT STA 380-400, BL 0, MAIN DECK FLOOR. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.Jan 26, 2002 · N33635 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200040Web · crackedINSPECTION FOUND A 2" CRACK IN WEB AT STA 927-947.5, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-2.Jan 25, 2002 · N33635 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0200030Seal · leakingSMOKE ENTERED THE COCKPIT AND CABIN ON TAKEOFF FROM EWR. THE APU WAS RUNNING AND BOTH ENGINE BLEEDS WERE ON WITH BOTH PACKS OPERATING. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. BOTH ENGINES WERE BORESCOPED. MAINTENANCE FOUND THE AIJan 22, 2002 · N37615 · Boeing 737524 · Turbine Engine Oil SystemSDR CALA0101015Fan · failedCREW REPORTED SMOKE IN CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE FOUND THAT THE FIRST CLASS GALLEY NR 1 OVEN WAS ON AND THE EXHAUST FAN WAS NOT OPERATING. THE OVEN AND CONNov 29, 2001 · N14613 · Boeing 737524 · Buffet/GalleysSDR CALA0100959Wire · brokenESCAPE PATH LIGHT INOP AT ROW 5. REMOVED AND REPLACED FLOOR SECTION WIRING AND LIGHT ASSEMBLY.Oct 17, 2001 · N17663 · Boeing 737524 · Light System WiringSDR CALA0100867Floor Support · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORTS AT STA 540, BL 0 ON RT AND LT SIDES. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.Sep 12, 2001 · N19634 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0100866Intercostal · crackedINSPECTION FOUND A 1/2" CRACK IN INTERCOSTAL AT BS 482B-520, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.Sep 12, 2001 · N19634 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0100865Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT BS 540, LBL 2. THE FLOOR SUPPORT WAS REMOVED AND REPLACED 51-10-02.Sep 12, 2001 · N19634 · Boeing 737524 · Fuselage Miscellaneous StructureSDR CALA0100823Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AND GOUGED AFT OF R-2 DOOR AT STA 990 BETWEEN S14R AND 15R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.Aug 29, 2001 · N19634 · Boeing 737524 · Fuselage Main, Plate/SkinSDR CALA0100807Wire · shortedTHE EMERGENCY AISLE LIGHTING AT ROWS 5-9 LEFT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE FOUND SEAT 8 MOUNTED EMERGENCY LIGHT WIRING SHORTED. THE SHORTED SECTION OF WIRING WAS REPAIRED IAW WDM 33-51-41.Aug 26, 2001 · N24633 · Boeing 737524 · Light System WiringSDR CALA0100758Ground Wire · looseTHE OVERHEAD EMERGENCY LIGHT AT L-1 DOOR FAILED TO ILLUMINATE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND NUT BACKED OFF OF GROUND 622 GROUNDING STUD AND GROUND WIRE LOOSE. THE NUT WAS REPLACED AND THE GROUND WIRE WAS SECURED. OPERATIONAL CHECKS WERE GOOD.Aug 11, 2001 · N14628 · Boeing 737524 · Emergency LightingSDR CALA0100749Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 4, LBL 30, AND RBL 38. A STRAP DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-51.Aug 8, 2001 · N24633 · Boeing 737524 · Fuselage Main, Floor Beam
Back to Boeing 737-524