Boeing 737-2X6C
Service difficulty reports · 1,351
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 = '7372X6C' 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.
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 = '7372X6C' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 7AHR201204062390Seat Track · corrodedCORROSION ON SEAT TRACK AT BS 616 RBL 46. CORROSION FOUND TO BE OUT OF LIMITS, R & R SEAT TRACK IAW SRM.SDR 7AHR201204062375Seat Track · corrodedCORROSION ON SEAT TRACK AT BS 663 TO 747 AT RBL 24.75. R & R SEAT TRACK IAW SRM.SDR 7AHR2012040635012Spar · corrodedCORROSION AT LOWER RT WING L/E FWD SPAR AT WBL 227.0 TO WBL 522.0. REMOVED CORROSION, FABRICATED 2 REPAIR STRAPS AND INSTALLED IAW CURRENT SRM.SDR 7AHR201204052466Skin · corrodedCORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, MATERIAL LOSS WITHIN LIMITS. ALODINED AND PRIMED STRUCTURE IAW CURRENT SRM.SDR 7AHR201204052467Skin · corrodedCORROSION ON LEFT WING INTERNAL SURFACE AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE AND PRIMED IAW CURRENT SRM.SDR 2012F00072Skin · corrodedCORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE, AND PRIMED STRUCTURE IAW CURRENT SRM.SDR 7AHR201204032220Stringer · corrodedCORROSION AT AFT FUSELAGE BULKHEAD AT BS 1016, STRINGER 17L. CUT OUT DAMAGED STRINGER 17L FROM 1016 TO 1026 TO ACCESS STRINGER TIE FITTING. FABRICATED REPAIR PART AND INSTALLED IAW SRM.SDR TSAA1153010Skin · crackedDURING SERVICE CHECK, FOUND A 2 INCH CRACK ON THE RT SIDE FUSELAGE AT BS 360+5.5, ABOVE STRINGER 15R. THE CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3826, SB 737-53A1177 REVISION 6 & SRM 53-30-03 FIGURE 48.SDR TSAA1153009Skin · crackedDURING SERVICE CHECK FOUND A 2.5" CRACK ON THE RT SIDE FUSELAGE AT BS 360+4, BELOW STRINGER 14R. THE CRACK WAS REPAIRED IAW ENGINEERING CHANGE ORDER 3824, SB 737-53A1177 REV 6 & SRM 53-30-03, FIGURE 48.SDR TSAA1153008Skin · crackedDURING SERVICE CHECK, FOUND A 4" FUSELAGE SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS807+3 STRINGER 18L. THE CRACK WAS REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL XI.SDR TSAA1154007Fairing · damagedAFT LT PYLON FAIRING ASSY-WING TO NACELLE STRUCTURE DAMAGED. REPLACED NR1 ENGINE TO WING AFT FAIRING IAW AMM 54-51-32. NO MAJOR REPAIR REQUIRED. THE ACFT WAS RETURNED TO SERVICE.SDR TSAA1153005Skin · crackedDURING THE DAILY SERVICE CHECK, A 2 IN CRACK AT BODY STA 259.5, 1 IN ABOVE STRINGER 16R WAS DISCOVERED DURING THE VISUAL CHECK OF THE FUSELAGE. THE CRACK WAS CONFIRMED WITH HFEC INSP AND WAS REPAIRED IAW SRM 53-30-3, FIG 48 DETAIL VIII. THE ACFT WAS RETURNEDSDR TSAA1156003Window · crackedNON-ETOPS FLIGHT 54 HNL-ITO. ON DESCENT, THE CAPTAIN’S NR 2 WINDOW OUTER PANE CRACKED. GLASS REMAINED INTACT AND THERE WAS NO LOSS OF PRESSURIZATION. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE CAPTAIN’S NR 2 WINDOW IAW AMM 56-12-11 ANSDR TSAA1179002Oil Filter · separatedFLT 40. AFTER ADVANCING THE THROTTLES THE CREW NOTED THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATE FOLLOWED BY A DECREASE IN NR 2 ENGINE OIL QUANTITY. THE CREW ABORTED THE TAKE-OFF AND SHUTDOWN THE NR 2 ENGINE AND RETURNED TO THE CARGO RAMP. MAINTENANCESDR TSAA1132001Lock · lack of lubeLANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF. CLEANED AND LUBED LANDING GEAR LOCK MECHANISM. OPS CK OK IAW AMM 32-31-31. ACFT RETURNED TO SERVICE.SDR TSAA1027019Indicator · failedDURING CLIMB, THE CREW SELECTED FLAPS UP AND NOTED A SPLIT-FLAP INDICATION, WITH NO ROLL ENCOUNTERED. CREW ATTEMPTED TO SELECT FLAPS 1 WITH NO EFFECT. CREW DECLARED AN EMERGENCY, ACCOMPLISHED T/E FLAPS DISAGREE CHECK LIST WITH FLAPS 15. ACFT LANDED WITHOUT SDR TSAA1027018Connector · damagedNON-ETOPS CARGO FLIGHT 551. DURING LANDING, WHEN THE CREW LOWERED THE FLAPS, THERE WAS A FLAP ASYMMETRY INDICATION AT FLAPS 1. THE CREW FOLLOWED QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PIN 5SDR TSAA1021016Clamp · dislodgedON DESCENT, AT ABOUT FL 240, THE CREW EXPERIENCED THE ALTITUDE WARNING HORN SOUND. CREW CHECKED THE CABIN ALTITUDE, CANCELLED THE HORN, DONNED OXYGEN MASKS, AND ESTABLISHED COMMUNICATION. CREW DECLARED AN EMERGENCY AND CONTINUED AN EMERGENCY DECENT TO BELOW SDR TSAA1072015Fire Loop · failedNON-ETOPS CARGO FLT 14. CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE UPPER OVERHEAT LOOP IN ACCORDANCE WITH MM 26-11-11. OPS CSDR TSAA1072014Element · false activationCREW NOTED THE NR1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NR1 ENGINE LOWER FIRE DETECTION SENSING ELEMENT IAW AMM 26-11-11, AND OPS CHECK WAS SATISFSDR EE4Y100357Structure · corrodedFWD CARGO COMPARTMENT BULKHEAD BS 540 BTWN STR 22L AND 23L CHORD HORIZ FLANGE WITH CORROSION (THE CORROSION REQUIRES A MAJOR REPAIR).SDR EE4Y100340Stringer · crackedTAIL COMPARTMENT, STA 1132, STRINGER 5 RIGHT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.SDR EE4Y100339Stringer · crackedTAIL COMPARTMENT STA 1132 STRINGER 5 LT WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.SDR EE4Y100338Bulkhead · corrodedLOWER FUSELAGE, FWD CARGO COMPARTMENT, STA 540 BULKHEAD BETWEEN STRINGER 22 LT AND 23 LT CHORD HORIZONTAL FLANGE WITH CORROSION. THE CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y100336Floorbeam · corrodedUPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 847 BETWEEN RBL 42 AND RBL 59. THE CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y100335Floorbeam · corrodedUPPER FUSELAGE, FLOORBEAM LOWER FLANGE WITH CORROSION AT STA 867 BETWEEN RBL 26 AND RBL 56. THE CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y100337Floorbeam · corrodedUPPER FUSELAGE, FLOORBEAM WITH CORROSION AT UPPER FLANGE AT STA 344 BETWEEN LBL 43 & RBL 11. THE CORROSION REQUIRES MAJOR REPAIR.SDR EE4Y100334Bear Strap · crackedMAIN CARGO DOOR, FWD UPPER CORNER CUTOUT, FUSELAGE SKIN, BEAR STRAP WITH CRACK. THE CRACK REQUIRES A MAJOR REPAIR.SDR EE4Y100333Floorbeam · corrodedUPPER FUSELAGE, BS 787 FLOORBEAM, LOWER FLANGE CORRODED. THE DAMAGE REQUIRES A MAJOR REPAIR.SDR EE4Y100332Bulkhead · dentedFUSELAGE BULKHEAD BS 1016, AFT FACE, WEB DENTED AT WBL 166, RBL 7. THE DENT REQUIRES A MAJOR REPAIR.SDR EE4Y100330Bear Strap · crackedUPPER FUSELAGE, FWD ENTRY DOOR, LOWER HINGE CUTOUT AT BS 304.5 WL 235, INTERNAL BEAR STRAP WITH CRACK. THE CRACK REQUIRES MAJOR REPAIR.SDR EE4Y100319Spar · corrodedRIGHT WING LEADING EDGE FRONT SPAR LOWER CHORD WITH CORROSION ON LOWER FLANGE. THE CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y100309Skin Panel · dentedLOWER EXTERNAL FUSELAGE AT BS 727A+6.25 BETWEEN STR 22R AND STR 23R SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR.SDR EE4Y100264Skin Panel · dentedLOWER FUSELAGE, AT BS 727+12.5 BETWEEN STRINGER 20 RT AND STRINGER 21 RT SKIN WITH DENT. THE DENT REQUIRES MAJOR REPAIR.SDR EE4Y100263Skin · crackedLOWER FUSELAGE, SKIN CRACKED AT BS 308 BELOW STRINGER 18RT. THE CRACK REQUIRES A MAJOR REPAIR.SDR CA100715006Circuit Breaker · weakDURING CLIMB-OUT THROUGH FL290 MULTIPLE ELECTRICAL EQUIPMENT FAILURES OCCURRED. ALL GENERATOR & TRANSFORMER RECTIFIER INDICATIONS NORMAL. A TRANSFER BUSS CIRCUIT BREAKER FOUND TRIPPED. AFTER A COOLING PERIOD CREW RESET CIRCUIT BREAKER. ALL SYSTEMS RETURNEDSDR TSAA1028013Indicator · failedMX FERRY FLIGHT. AFTER TAKEOFF THE CREW NOTED THE LOSS OF FUEL INDICATION FOR THE NR 1 FUEL TANK. THE CREW RETURNED TO DEPARTURE. MX R & R THE NR 1 TANK FUEL QUANTITY INDICATOR IAW AMM 28-41-61.SDR EE4Y100243Cargo Track · corrodedUPPER FUSELAGE MAIN CARGO CABIN, CARGO TRACK AT BL 0, BETWEEN BS 460 AND BS 500B+8.5 WITH CORROSION.SDR EE4Y100242Track · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 440, LBL 24, WL 208 TRACK LOWER FLANGE WITH CORROSION.SDR EE4Y100241Strap · corrodedLEFT MAIN WHEEL WELL CEILING STRAP WITH CORROSION AT BS 703, LBL 50, WL 200.SDR EE4Y100240Skin · corrodedLOWER EXTERNAL FUSELAGE AT BS 907 BETWEEN STRINGER 25RT AND STRINGER 26RT WITH SKIN BULGED.SDR EE4Y100239Stringer · corrodedLOWER FUSELAGE, AFT CARGO COMPARTMENT AT BS 865.5 STRINGER 27RT WITH CORROSION.SDR EE4Y100238Beam · corrodedEMPENNAGE RT HORIZONTAL STABILIZER UPPER T/E BEAM WITH CORROSION AT ELEV STA 94.27, 213.32.SDR EE4Y100237Stringer · corrodedLOWER FUSELAGE AFT SECTION AT BS 977 STR 20LT WITH CORROSION.SDR EE4Y100236Stringer · corrodedLOWER FUSELAGE E&E COMPARTMENT FROM BS 344 TO BS 360 STR 25LT WITH CORROSION.SDR EE4Y100235Frame · crackedUPPER FUSELAGE MAIN CARGO CABIN AT BS 986.5 BETWEEN STR 2L AND 3L, FUSELAGE FRAME WITH CRACK.SDR EE4Y100234Frame · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 727A FROM STR 25L TO STR 27R FRAME WITH CORROSION.SDR EE4Y100233Skin · gougedLOWER AFT FUSELAGE INTERNAL SECTION AT BS 1003 BETWEEN STRINGERS 20 AND 21 RT FUSELAGE SKIN WITH GOUGE.SDR EE4Y100232Skin · bulgedRT WING TRAILING EDGE SECTION NR 6 FLAP TRACK FAIRING O/B LATERAL STEEL STRAP WITH BULGED SKIN AND WEAR.SDR EE4Y100230Bear Strap · cracked((EE4Y)) LOWER FUSELAGE AFT CARGO COMPARTMENT BS 844 BETWEEN STRINGERS 23 & 24RH, BEAR STRAP DOUBLER WITH CRACK. (W/O Y10122, SUB JOB 1, ITEM 230).
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