Boeing 737-824
Service difficulty reports · 9,828
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 = '737824' 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 = '737824' 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 CALA2026072618012Web · crackedRIGHT WING OTBD L/E AREA BULL NOSE WEB IS CRACKED AT LOWER ATTACH FLANGE APPROX OFSS 620. ACCOMPLISHED ANGLE REPAIR IAW REO-G26003, REV IR AND ECRA 5741-01722.SDR CALA2026072618010Web · gougedLOWER FUSELAGE KEEL BEAM TRUSS WEB IS NICKED AT LIGHTNING HOLE CUTOUT, APPROX BS 605, LBL 4. ACCOMPLISHED BLENDOUT REPAIR IAW REO-G26010, REV IR. AND ECRA 5349-01004.SDR CALA2026072617998Latch · wornFWD RT LATCH ON H/P PNUMATIC DOOR192, DOOR HAS WORN INTO PREVIOUS REPAIR AND STRIKER PLATE IS MISSING. REMOVED DAMAGED REPAIR STRAP IAW SRM 57-10-13-2R-3, CUT FILLER AND STRAP TO SHAPE FROM 0.125" IAW SRM 57-10-13-2R-3, TABLE 201, FOUND PREVIOUS REPAIR FSDR CALA2026072617996Trunnion · corrodedLEFT WING REAR SPAR LT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD BUSHING HOLE. REMOVED AND REPLACED LT MLG TRUNNION FITTING ASSY (INCLUDING BUSHINGS) IAW DWG 115A5002, SH7 AND SRM 51-40-02-0G-0.SDR CALA2026072417985Stop Fitting · gougedFWD CARGO DOOR AFT SIDE LOWER STOP FITTI NG HAS A GOUGE ON UPPER SURFACE. REPLACED STOP FITTING IAW DWG 143A6117 REV A AND SRM 51-40-02.SDR CALA2026072417983Door Frame · scratchedFWD CARGO DOOR AFT END LOWER SIDE CORNER FRAME HAS MULTIPLE SCRATCHES. REPLACED CORNER FRAME IAW DWG 143A6110, REV A.SDR CALA2026072417974Battery · inoperativeONE FLASHLIGHT INOPERATIVE, FWD GALLEY. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN FWD GALLEY IAW AMM 25-64-00. OPS NORMAL.SDR CALA2026072317949Skin · corrodedBULGING FASTENERS AROUND PAN AREA. PERFORMED INTERIM REPAIR TO EXTERNAL SKIN ON WASTE TANK AREA BTW BS 847 - 867, S22 - 26L IAW EO 260399 REV. P1, EO 260399, REV. P2, EO 260399 REV. IR AND EC/RA 5360-02183.SDR CALA2026072417987Warning Message · false activationSPEED LIMIT FLAG ON CREW REPORTED SPEED LIMUT FLAG WAS ONLY ON CAPT'S SIDE. ACCOMPLISHED FIM TASK 27-32T831 SMYD 1 SHOWS 27-31004 ON LAST LEG, NO OTHER LEGS. ACCORDING TO FIM THERE WAS AN INTERMITTENT SMYD PROBLEM. AUTO SLAT FAIL LIGHT CAME ON FOUND MX MSGSDR CALA2026072417964Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK. REPLACED EMERGENCY BATTERY AT LOCATION #M1672, LIGHTS RELATED TO THIS PACK DID NOT COME ON, SUSPECT BAD POWER SUPPLY. POWER SUPPLY IS ON AOG. REFERRED TO MM# 33-51-06-960-805. PERFORMED AMM 33-51-06-SDR CALA2026072117912Lamp · inoperativeINSEAT EXIT LIGHT ROW 38C DOES NOT ILLUMINATE. REMOVED SEAT 38C EXIT PATH LIGHT FIXTURE LAMPS. INSTALLED NEW CONDITION LAMPS AT ROW 38C EXIT PATH LIGHT FIXTURE. OPS CHECK SATISFACTORY AT THIS TIME. REF COLLINS CMM 25-22-55.SDR CALA2026081118478Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM STA 312 LBL 10. ACCOMPLISHED PERMANENT REPAIR AT FLOORBEAM BS 312 BETWEEN LBL 32 AND RBL 20 PER SRM 53-10-51-2R-17 REPAIR 17 FIG. 203SDR CALA2026072718033Window Frame · crackedCRACKS FOUND AT HOLE NR 3 OF RT SIDE NR 3 WINDOW FRAME. PERFORMED A REPAIR IAW EA 5310-08195, REV C, OPP 004 , & EC/RA 5310-08980.SDR CALA2026072317961Warning Horn · false activationRTO AT ABOUT 100KTS FOR TO COFIG LIGHT/HORN. ACCOMPLISHED TAKEOFF WARNING SYSTEM TEST IAW AMM 31-51-00-710-803-C2. OPS CHKD GOOD, NO FAULTS, NO MESSAGES. REF FIM 31-51 TASK 803 ACCOMPLISHED INITIAL EVALUATION. TAKEOFF WARNING REPORT SHOWED FAULT MESSAGE 31SDR CALA2026072217945Power Supply · inoperativeROW 20 21 FED EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FOR EMERGENCY LIGHT IAW AMM 33-51-06. OPS CHECKED GOOD.SDR CALA2026072417963Fan · failedFA REPORTS SMOKE AND FUMES IN AFT OF ACFT. SUBSIDED WITH QRC UPDATED. PER CHECKLIST, SHUTDOWN RECIRC FANS AND SMOKE & ODOR STOPPED. PERFORMED SMOKE ODOR IN THE CABIN INSP IAW AMM 05-51-26-800-801-C1. RESET BREAKER & PERFORMED OPS CHECK & RT RECIRC FAN GENERASDR CALA2026072017901Light · faultedCHRONIC LVL-C: EMERGENCY EXIT SIGN LIGHT FLICKERING ON 21DEF, REPLACED WINDOW L IGHT OVER WING EXIT LED LIGHT ASSY IAW AMM TASK 33-21-01-960 -802-1. CHKD WIRING & CONNECTOR FOR DEFECTS. NOTE FAULTS. R & R UPPER LINING ASSY IAW AMM 25-21-20-020-003. R & R ESDR CALA2026072017870Stop Fitting · gougedL-2 DOOR FWD TOP STOP FITTING GOUGED AT THE FWD UPPER CORNER OF THE DOOR. REMOVED AND REPLACED STOP FITTING IAW B737 DWG 147A6116 REV F AND 147A6125 REV-. ADJUSTMENT CHECK ACCOMPLISHED ON AAR GSO NRC 9288328.SDR CALA2026072017858Angle · corrodedHORIZONTAL STAB ACTUATOR COMPARTMENT STA 1088 BULKHEAD FORWARD FACE HAS EVIDENCE OF CORROSION ABOVE THE APU AIR INLET DUCT ATTACH TO THE BULKHEAD. REMOVED, FABRICATED NEW STIFFENER 5 AND REPLACED IAW SRM 51-40-02-0G-0,51-40-05-0G-0,51-40-08-0G-0,51-20-01-0G-0,SDR CALA2026071617830Lens · missing22C EMERGENCY PATH LIGHT LENS MISSING. REPLACED LENS AND UPL. OPS CHECKS GOOD.SDR CALA2026071617824Battery Pack · faultedFAILED EMERG. LIGHT CAPACITYCHECK. AOG C/W. REPLACED EMERGENCY LIGHT BATTERY PACK M1670. OP CKS GOOD. M.M. 33-51-06-960-801.SDR CALA2026071617822Battery Pack · faultedM1675 FAILED EMERG. LIGHT CAPACITY CHK. PART NIS, AOG C/W. REPLACED BATTERY PACK M1675. OPMCKS GOOD. MM 33-51-06-960-801.SDR CALA2026073018108Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STAB.LOWER SKIN, FWD OF AFT SPAR FASTENER ROW, 3 INCHES OTBD OF HSS 120.30. REMOVED ONE PRE-EXISTING DOUBLERS & 3 FILLERS. CUT AND REMOVED CRACK. NDT CONFIRMED CRACK WAS REMOVED, PREVIOUS CUTOUT & OUTER ROW FASTENERS FSDR CALA2026072017892Sensor · faultedCREW REPORTS LEADING EDGE FLAP TRANSIT LIGHT AFTER TAKEOFF. OVERHEAD INDICATOR FOR NR 3 LEADING EDGE FLAP INDICATING NOT RETRACTED. FOLLOWED FIM 27-88 TASK 820 AND COMPLETED FSEU BITE CHECK, PASSED. LOOKED AT PREVIOUS FAULT HISTORY LEG 0 HISTORY SHOWS F3 PROXSDR CALA2026072017853Structure · damagedREPAIR ON LOWER WING STRUCTURE FOR 192DR HIGH-PRESSURE DUCT DOOR IS DAMAGED. AFTER DISASSYMBLY FOUND TRIMOUT HAS NOT BEEN DONE CORRECTLY & NEEDS TWO MORE 3/16 HILOCKS AT 3D MIN ON EITHER SIDE OF CUTOUT IAW SRM 57-10-13-2R-3. EVALUATED AND MEASURED DAMAGE BOTHSDR CALA2026071917849Skin · corrodedLEFT WING UPPER SKIN IS CORRODED APPROX BETWEEN WS 180 AND WS 204 AND STRINGER U-14. ACCOMPLISHED BLEND REPAIR IAW AAR REO-G25997 REV IR DATED 13-JUL-26 AND UAL ECRA 5723-01059. LEFT WING UPPER SKIN CORROSION, SKIN REPAIRED. ACCOMPLISHED BLEND REPAIR IAW AASDR CALA2026071617816Battery Pack · discharged(SUPPORT TASK) M1670 BATTERY PACK LOW VOLTAGE TRANSCRIBED FROM AAR GSO NR 9288012. ORIGINATED BY V942811 SDR COMPLETED REMOVED AND REPLACED M1670 BATTERY PACK AND PERFORMED OPS CHECK AND OPS CHECK GOOD IN REF WITH B737 AMM TASK 33-51-06-960-805. AAR GSO MECH VSDR CALA2026081318569Spar Web · corrodedCORROSION AT THE RT OUTER WING SPAR WEB AT FUEL BOOST PUMP IAW ECRA 5720-03656. PERFORMED AN INSPECTION OF REPAIR TO RT WING FRONT SPAR WEB AT FUEL BOOST PUMP CUTOUT ON ACFT IAW PART 2 OF LATEST REVISION OF ECRA 5720-03656. ACCOMPLISHED INTERIM REPAIR PERFORMSDR CALA2026081118476Bulkhead Web · crackedCRACK FOUND IN LT WHEEL WELL AT UPPER SECTION OF FWD WALL (BS 663) IAW AAR N/R 100048007, ACCOMPLISHED REPAIR (CATEGORY B) AT LT VERTICAL PRESSURE DECK WEB IAW SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 2 PARAGRAPH 5 FIG 204. ACCOMPLISHED REPAIR (CATEGORY B) AT SDR CALA2026080318232Skin · nickedNICK WAS FOUND OUT OF LIMITS ON FUSELAGE SKIN BETWEEN BS 500AD - 500E, STR 27R - 26R. PERFORMED REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 500D 500E AND STR 27R / STR26R - ALL WORKS WERE ACCOMPLISHED IAW SRM 53-00-01-2R-1, SRM-51-20-01-0G-0,AMM 20-60-07-913SDR CALA2026072117902Floorbeam · corrodedPASSENGER CABIN FLOORBEAM STA 344 LBL 55 UNDER SEAT TRACK. ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN FLOORBEAM UPPER TEE BS 344 LBL 55 IAW SRM 53-10-51-2R-18, REPAIR 18, FIG. 207.SDR CALA2026071617845Sign · inoperativeRIGHT AFT OVERWING LOWER EMERGENCY SIGN LIGHTS ARE INOP. EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - REPLACED EXIT SIGN ASSY AT RIGHT OVERWING DOOR. REF AMM 33-51-01-960-802. OPS CHECK GOOD.SDR CALA2026071617844Light · looseEMERGENCY EXIT PATH GUIDANCE LIGHT ON 10C LOOSE AND DANGLING OUT OF THE SEAT. EMERGENCY FLOOR PROX LIGHT PLASTIC HOUSING WAS BROKEN. INSTALLED NEW PLASTIC HOUSING REF AMM 33-51-11.SDR CALA2026071617838Transmitter · faultedOIL FILTER BYPASS MESSAGE SHOWS ON ENGINE DISPLAY ENG 1 AFTER STARTUP. MESSAGE DISSAPEARED. MESSAGE REAPPEARED AFTER TAKE OFF. DIVERTED TO CVG. C/W EEC BITE FIM 73-00 TASK 801 & FOUND NO RECENT FAULTS. REMOVED & INSPECTED SCAVENGE FILTER PER MEL 7902A & AMSDR CALA2026071317733Intercostal · crackedRIGHT WING FIXED UPPER T/E PANEL JUST INBD OF THE DEFLECTION CONTROL RIB SUB-STRUCTURAL INTERCOSTAL IS CRACKED IN THE RADIUS AND THROUGH THE ATTACH FASTENERS REMOVED AND REPLACED R/H WING,FIXED T/E INTERCOSTAL INBD OF THE DEFLECTION CONTROL RIB SUBSTRUCTURE ISDR CALA2026071317731Bracket · crackedRIGHT WING ABOVE 651GB,FIXTURE PANEL HAS BRACKET CRACKED THAT ATTACHES TO FLAP DEFLECTION FITTING. REMOVED AND REPLACED RH WING,FIXTURE PANEL BRACKET IAW B737 SRM 51-40-02 AND BAC DWG# 115A6200 REV:B DOT REMOVED.SDR CALA2026071217702Skin · corrodedL/H EXTERIOR FUSELAGE SKIN HAS CORROSION AROUND LAV EXHAUST VENT BETWEEN BS907 AND BS927 AND BETWEEN STR S-21L AND STR S-22L. REMOVED DAMAGE REF SRM 53-00-01-1A-1. ORIG .125, REMOVED .012, REMAINING .113 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A FIG 103 DSDR CALA2026071217700Web · corrodedRIGHT WING OTBD L/E AREA BULL NOSE WEB IS CORRODED ON THE UPPER ATTACH FLANGE AT APPROX OFSS 580. REMOVED CORROSION AND EVALUATED MATERIAL REMOVED .002, ORIGINAL THICKNESS .050, REMAINING THICKNESS .048 FOUND WITHIN LIMITS IAW SRM 57-41-02. RESTORED SURFACE FSDR CALA2026071417747Skin · damagedLIGHTNING STRIKE DAMAGE LOCATED AT STATION 214 AND 7" BELOW FLOOR LINE STRINGER 17R. DAMAGE IS AWAY FROM FASTENER.BLENDED AREA REMOVED .017" OF MATERIAL ORIGINAL THICKNESS IS .040". BLEND IS OUT OF LIMITS. A REPAIR IS NEEDED FOR THIS AREA. REQUESTING A THICKNESDR CALA2026072117934Skin · corrodedPOSSIBLE CORROSION UNDER VACUUM WASTE PAN SKIN. (REF. AAR NR 1000079184). PERFORMED REPAIR AT VACUUM WASTE PAN SKIN AREA BTW STA 847 TO STA 867 AND S-23L TO S-25L IAW EO 260347 REV. P1, EO 260347 REV. P2, EO 260347 REV. IR AND EC/RA 5360-02179.SDR CALA2026071217724Door · out of limitsAFT ENTRY LIGHT ON DOOR HANDLE UNABLE TO CLOSE OPENED AT ALTITUD PERFORMED AFT ENTRY DOOR SYSTEM TEST REF AMM 52-13-00-700-805. INTERIOR DOOR HANDLE CLOSES AND OPENS WITHIN TORQUE RANGE SPECIFIED IN AMM. NO DEFECTS FOUND AT THIS MOMENT. PERFORMED CABIN PRESSURSDR CALA2026071217697Plate · crackedUNDER SPOILER #8 IN TRAILING EDGE CAVITY AT APPROX ORSS 297, WIGGLE PLATE CRACKED. REMOVED AND REPLACED WIGGLE PLATE IAW BAC DWG 115A3712 REV A. AAR GSO MECH V933707. COMPLETED ESFR REMOVED AND REPLACED WIGGLE PLATE IAW BAC DWG 115A3712 REV ASDR CALA2026071217695Plate · crackedUNDER SPOILER #8 IN TRAILING EDGE CAVITY AT APPROX ORSS 308, WIGGLE PLATE CRACKED. REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02, DWG 115A3712 REV A. COMPLETED SFR REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-21 BAC DWG 115A3712 REV ASDR CALA2026072117936Skin · crackedAFTER EVALUATION REQUIRE ACCESS TO FOM REPAIR ON LH HORIZONTAL STAB STA 101.9 IN-SPAR RIB 1, STIFFENER AND NR 2 STIFFENER. PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB LOWER SKIN AT STA 101.9 IN SPAR RIB 1, STIFFENER, AND NR 2 STIFFENER. THIS REPAIR IS A SDR CALA2026071517792Bulb · inoperativeLEVEL B, CHRONIC FOR EMERGENCY LIGHTS/ EXIT ROW LIGHTS ABOVE 21DEF NOT WORKING. R & R TWO BULBS IN FLOOR PROXIMITY LIGHT AT SEAT 20ABC. PREFORMED OPS TEST OF EMERGENCY LIGHTS AND OPS CHECK OK IAW AMM 33-51-00.SDR CALA2026071217687Battery Pack · no testEMERGENCY BATTERY PACK M1674 FAIL. REMOVED AND REPLACED NEW BATTERY PACK M1674. IAW AMM 33-51-06-960-805. TEST GOOD FOR SERVICE.SDR CALA2026071217685Channel · corrodedCORROSION RH CHANNEL ZEE AFT CARGO FLOOR FROM BS 747 TO 787. REMOVED AND REPLACED NEW SHIELD ON RH CHANNEL ZEE AFT CARGO FLOOR, APPLIED ALODINE PRIMER IAW SRM 51-40-02-0G-0 STEP 4 SRM 51-40-05-0G-0 STEP 4.C AMM 51-21-41-370-802 AMM 51-21-72-370-804 SRM 51-40SDR CALA2026071217683Channel · corrodedCORROSION RT CHANNEL ZEE FWD CARGO FLOOR AT STA 500H AND STA500F. COMPLETED REMOVE AND INSTALLED RH ZEE CHANNEL FWD CARGO AT STA 500H AND STA 500F IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G, SRM 51-40-08-0G-0.SDR CALA2026071217681Channel · corrodedCORROSION LT CHANNEL ZEE FWD CARGO FLOOR FROM BS 500 TO 500H. COMPLETED REMOVED AND INSTALLED LT ZEE CHANNEL FWD CARGO AT BS 500 AND 500H IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G, SRM 51-40-08-0G-0.SDR CALA2026071217679Channel · corrodedAFT CARGO BAY, RT. SIDE "Z" CHANNEL, MULTIPLE: CORROSION SPOTS AND LOOSE RIVETS ON FRAMES COMPLETED REMOVAL AND INSTALLED Z" CHANNEL R/H SIDE AFT CARGO BTW STA 727 TO 767. IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0, SRM 51-40-08-0G-0 AND SRM 53-00-53-2R-5.
Back to Boeing 737-824