Boeing 737-724
Service difficulty reports · 3,423
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 = '737724' 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 = '737724' 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 CALA2022060601443Structure · damagedWEB P/N 141A5180-16 LIGHTENING HOLE ENLARGMENT. REF AVO 9764 C/W STEPS 1.A,B,C, ENLARGE LIGHTNING HOLE TO FACILITATE REPAIRS PERFORMED STEP 1 (D) AS REQUIRED PER AVO 9764 , NO DEFECTS DUE TO BIRDSTRIKE. STEP 1.D, REQUIRES INSPECTION OF OF THE NOTED AT THIS TISDR CALA2022060601442Skin · dentedDENT FOUND ON INSPECTION OF BIRD STRIKE AFT OF AOA VANE. ACCOMPLISHED DETAILED VISUAL INSP IAW STEP 2 OF AVO 9718. NO PER AVO9718 PERFORMED STEP 3 HFEC PER PART 6 51-00-00 PROCEDURE REF STEP 2 OF AVO 9718. AOA SENSOR DAMAGED FURTHER DISCREPENCIES EXIST. NEED SDR CALA2022052301320Fire Detector · activated*EMERGENCY DECLARED*FIRE ALARM ACTIVATED IN LAV AFT AIRCAFT RIGHT TALKED TO CREW AND PASSENGER. PASSENGER CLAIMED SHE SPRAYED AIR FRESHENER AFTER PERFORMING NUMBER TWO. TESTED SMOKE DETECTOR WITH NO FAULTS. REF AMM 26-14-00.SDR CALA2022052301319Speed Switch · looseREJECTED TAKEOFF AT 130KNOTS DUE TO TAKEOFF COFIGURATION HORN AND ANNUNCIATION. FOUND SWITCH ASSY SPEEDBRAKE LOOSE, WILL NEED REPLACEMENT ADD EMP:U332357 ACCOMPLISHED FIM 31-51 TASK 803 FOUND SPEED BRAKE TAKE-OFF WARNING SW S651, ACCOMPLISHED TAKE OFF WARNINSDR CALA2022051801270Skin · crackedRIGHT WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.64 -- SEE PHOTO,S PHOTO ADDED -- CRACK IS APPROX 2" LONG ......IDT AC NEEDED TO VERIFY AND MARK ENDS OF CRACK REPAIR AS GIVEN IN REPAIR 3 NO MORE THAN 6000 FLIGHT CYCLES OR 24 MONSDR CALA2022050901179Aoa · missingBIRD STRIKE RIGHT SIDE AFT OF RADOME. AOA IS MISSING. REMOVED AND REPLACED RIGHT SIDE AOA SENSOR AS PER AMM CORRECTION, COMPLETED PER AMM 34-21-05-400-801 UP TO SUBTASK CORRECTION OF STEP INSTALLED FROM STEP 3G(1) UP TO AND INCLUDING APPLIED SEALANT AROUND THESDR CALA2022042701084Fseu · failedLE FLAPS TRANSIT LIGHT FLASHING INTERMITTENTLY IN FLIGHT WITH FL APS RETRACTED FSEU BITE CONFIRMED MESSAGE 27-81205 SLAT 3 PROX INBD FAULT LAST AND TRAILING EDGES. VERIFIED PROPER OPERATION OF STICK SHAKERS. COLLARED CB ON P 18-2 PANEL " STALL WARNING ASY MODESDR CALA2022042701095Control Unit · fault messageAUTOBRAKE FAIL MSG UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. EVALUATE, CONTACT TOMC. MAC METER INITIATED FOR WITH VENDOR ID V902239 MAC RELATED WORK ORDER 000000003042072 AND PRTR CORREA, LINY (V902239) RESDR CALA2022041801013Position Sensor · inoperativeTRAILING EDGE FLAP DISAGREE ON APPROACH ALT FLAP EXTN LOCKING LGOPAGE UNLOCKING FOR S/O REF LOG8405001,INSTALLED LEFT HAND FLAP POSITION TRANSMITTER REF AMM 27-58-01-400-801. ALL TESTS PASS. ADD EMP:U192656,U221680SDR CALA2022022200489Seal · brokenPDA 3 LEFT WING OUTBD AFT T/EDGE FLAP HAS ONE AERODYNAMIC SEAL BROKEN OFF / MISSING JUST INBOARD OF #1 FAIRING -- SEE PHOTO REQUEST DEFERRAL CDL APPLIED -- SHEETMETAL ASST REQD TO REPLACE SEAL WITH RIVETS -- PARTS ADDED PER IPC 27-51-22-01 DISPATCH DESK: 7 SDR CALA2022021600404Strap · looseBOTH NAV1 AND NAV2 SHOW FAIL. NAV1 THRU 10K FT NAV2 15 MIN LATER TS PER FIM 22-15-00 TASK 813. MULTIPLE FAULTS FOUND DURING BITE AFTER CONFERRING WITH TOMC IN REGARDS TO THE NAV TUNING PANEL LIBRARY TEST. FAILURE 1 AND 2, ACMP FIM 34-31 TASK 801 WITH PARTICULASDR CALA2022013100271Sensor · faultedGOT LE FLAPS TRANSIT LT DURING INITIAL TAKE OFF ROLL. LOW SPEED REJECT HISTORY PREV LEG CREW REPORTS LE FWD LIGHT. #8 SLAT IN TRANSIT BEFORE AND AFTER REMOVED #8 LEADING EDGE SLAT OUTBOARD PROX SENSOR AND MOUNTED ACP SPLICED WIRES IAW SWPM. TAKE OFF ROLL. THEYSDR CALA2022011700157Skin · damagedAIRCRAFT SKIN HAS GROUND DAMAGE STA.400 TO STA.420, S-20L TO S-22L. VISUALLY INSPECTED AREA OF REMOVED FUSELAGE SKIN STA 400-420 BETWEEN S20L AND S22L. NO FURTHER DAMAGE NOTED. OK TO CONTINUE. CUT AND REMOVED DAMAGE TO SKIN FROM STA.400 TO STA.420 BETWEEN S-SDR CALA2022011700156Stringer · damagedSTRINGER S-21L IS BROKEN BETWEEN STA.400 AND STA.420 DUE TO GROUND DAMAGE. VISUALLY INSPECTED AREA OF REMOVED DAMAGED STRINGER 21L BETWEEN STA 380-440 LH. NO FURTHER DAMAGE NOTED. OK TO CONTINUE CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN STA.380 AND STASDR CALA2022011400141Shear Tie · damagedSHEAR TIE DAMAGED AT STA.420 BETWEEN S-20L AND S-21L. VERIFIED SHEAR TIE PER AVO 713-22-01-06-01 REV. C. STEP B.3.. OK TO CONTINUE. MGH QC775 VERIFIED SHEAR TIE PER AVO 713-22-01-06-01 REV. C. STEP B.3. VERIFIED REFORM OF SHEAR TIE. PERFORMED HFEC OF REWORKEDSDR CALA2022010700039Pressure Blkhd · crackedLEFT WW VERTICAL PRESSURE DECK WEB CRACKED APPROX 2" BETWEEN LBL 40.00 AND LBL 45.64 --- SEE PHOTO,S COMPLIED WITH HFEC REF NDT PART 6 51-00-00 23. CRACK VERIFIED. REF SRM 57-10-10-2R4 STEP 4B. PERFORMED HFEC PER STEP 4C NO C/W SRM 57-10-10 2R4 STEP 4E HFEC ONSDR CALA2022010700038Pressure Blkhd · crackedLEFT WW VERTICAL PRESSURE DECK WEB CRACKED APPROX 1" BETWEEN LBL 31.83 AND LBL 40.00 --- SEE PHOTO,S COMPLIED WITH HFEC REF NDT PART 6 51-00-00 23. CRACK VERIFIED. REF SRM 57-10-10-2R4 STEP 4B. PERFORMED HFEC PER STEP 4C NO C/W SRM 57-10-10 2R4 STEP 4E HFEC ONSDR CALA2021122702453Seal · missingPDA 3 #6 T/EFGE FLAP FAIRING OUTBD SIDE CENTER SEAL COMPLETELY MISSING -- SEE PHOTO PHOTO ADDED REPLACED MISSING SEAL. REF SRM 57-53-70-2R-2. REPAIR 2 PAR 4 ALTERNATIVE 1 REPAIR.SDR CALA2021122002413Radar · warning messagePWS WARNING AS TO THRUST WAS APPLIED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORMED FIM 34-43 TASK 815 FOR PREDICTIVE WINDSHEAR, NO FAULTS SPEED REJECTED TAKE OFF LESS THAN 60 KTS. REALIGNED ADIRU''S FOUSDR CALA2021121702374Light · damagedROW 15ABC UPPER SEAT MOUNTED EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED RED EMERGENCY LIGHT REF MM 33-51-11 AND CONFIG DRAWING 3350DD12295A01. OPS CK OK. VERIFIED OPERATION OF EMERGENCY LIGHTIN.SDR CALA2021112302162None · nonePDA 1 A SET OF CHOCKS DEPARTED THE AIRCRAFT DURING DEPARTURE OUT OF EWR FLT2077 ON 11/22/2021. WE ARE NOT SURE WHERE EXACTLY THE CHOCKS WERE LOCATED BEFORE THEY DEPARTED. SUBSEQUENT INSPECTION OF THE AIRCRAFT REVEALED NO DAMAGES. PERFORMED EXTERIOR INSPECTION SDR CALA2021111702125Slide · deployedDOOR 1R PARTIALLY DEPLOYED SLIDE DEPLOYED SLIDE-NOT INFLATED/FEL L OUT CASE LOCKING FOR MX FERRY UNLOCKED TO CREATE MAA FOR STT ON CALL MX LOCKED BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODESDR CALA2021110102017Windshear Sys · noneRTO DUE WINDSHEAR AT 96 KTS REVIEWED PARAMETERS IAW 05-51-07-210-801. NO MTC ACTION REQUIREDSDR CALA2021102901998Transceiver · inoperativeWX RADAR WILL NOT TEST. NO DISPLAY ON ND. AMBER WXR TEST REMAINS DISPLAYED WITH WXR ON PLACED WX RADAR ON MEL DISPATCH DESK: 1 NAME: RD DATE: 26-OCT-21- NOC DESK: 7367 NAME: RK DATE: 26-OCT-21- DEFERRED DIRECTLY BY TSDR CALA2021102501968None · noneFWD ENTRY DOOR LIGHT ON T/O PER CAPT THROUGH DISPATCH CALL TO TOMC, LOW SPEED ABORT 70 KNOTS CLEANED PROX SENSOR DOOR LIGHT INDICATION AND CHECK OPERATION IAW AMM 52-11-00-860-804 AND PERFORMED INSPECTION HIGH ENERGY STOP IAW AMM 05-51-07-210-801 ALL NORMALSDR CALA2021102201953None · failedBOTH AUTOPILOTS INOP CWS A AND B INOP R&R STAB TRIM INTERLOCK RELAY R 850 REF WDM 27-41-12. NO HELP PERFORMED LAND VERIFY TEST, TEST FAILED, PER DFCS SUMMARY - NEED MORE TROUBLESHOOTING. SUSPECT LRU IS ''STAB TRIM RLY'', (FCC-A/B INTERFACE, J1C-D03). PER FIM 2SDR CALA2021102201943None · wornREF LP 72444378. WASTE TANK DRAIN BALL VALVE LEAKING. PERF ECRA 2011-01000 SPILL CLEAN UP PROCEDURES FOR CARGO COMPARTMENT. IMMEDIATE CLEAN UP C/W PER PARAGRAPH 2. A. 17.0 DIP REQUIRED WITHIN 7 DAYS TO ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTISDR CALA2021101401864Valve · leakingHYD SYS B FAILED AFTER TAKEOFF. QTY ZERO. RUNNING LEAK AT FLOW VALVE REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER REF AMM 27-51-67 LEAKED CHECK GOOD, HYD SYS B QTY IS AT 94SDR CALA2021091501575Fastener · missingPDA 3 14 FASTENERS MISSING ON UPPER WING PANEL ABOVE LT MLG. PANEL 551BT REPLACED 14 SCREWS ON PANEL 551BT. REF AMM 32-32-11-400-801 AND 20-50-11-910-801. PANEL SECURE.SDR CALA2021091301566Flap System · faultedUPON FLAP EXTENSION FLAPS DISAGREED W/ RIGHT FLAP INDICATING MOR E THAN LEFT. PER LOG PAGE #7034746 : LEFT FLAP DISAGEE AT 0 DEGREE FLAP SETTING SIGNIFICANT FUEL BURN DELTA.REF FIM TASK 27-51 TASK 840 PERFORMED FSEU BITE NO FAULTS AND TRAILING EDGE ASYM SKEW SDR CALA2021090801522Vortex Gen · damagedPDA 2 ONE AFT BODY VORTEX GENERATOR MISSING ABOVE LEFT HORIZONTAL STABILIZER -- SEE PHOTO PHOTO ADDED CDL CARD 553010 FIGURE 102 CDL DEFERRAL ONLY 1 MISSING ON LEFT SIDE -- ALL OTHERS ARE PRESENT -- REQUEST APPROVED CDL APPLIED -- PARTS ADDED PER IPC 53-31-21-SDR CALA2021090601511Pump · overheatedHYD PUMP ELEC 1 OVERHEAT 1HR45M INTO FLIGHT ILLUMINUTED. RAN CKL IST IMMEDIATELY TURNED OFF REPLACED B SYSTEM HYD PUMP PER AMM 29-11-21-00-801-001 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1173015 SN OFF 7092 IPC REFERENCE # 29-11-21-000-801-001 PUMP, HYD ELESDR CALA2021090301502Probe · inoperative1100LB FUEL IMBAL AFTER T/O. NO LOW PRESS LIGHT ON. FUEL BURN N ORMAL AFTER CHECKLIST. CAPT REPORTED DURING FLIGHT THAT RIGHT ENG WAS FEEDING OFF RIGHT WING WITH FUEL STILL IN CTR TANK. (1800 LBS CTR TANK REMAINING AT TIME OF IMBALANCE). CAPT ADVISED THEY SDR CALA2021081801371Guard · damagedEMERGENCY LIGHTS STAY ON WHEN FLIGHT DECK SWITCH IS IN THE OFF POSITION. FOUND AFT FLT ATTENDANTS PANEL SWITCH GUARD DAMAGED AND PARTIALLY DEPRESSING SWITCH. REMOVED AND REPLACED SWITCH GUARD REF SWPM 20-84-14. OPS CK OK. OIL SERVICE ACCOMPLISHED AT CLE FOR FLSDR CALA2021081801364Warning Message · intermittentAUTOPILOT A WILL NOT ENGAGE AUTOPILOT B ENGAGES BUT KICKS OFF AF TER STICKERS APPLIED NO GROUND TIME. DEFER REVIEWED FAULT HISTORY AND FOUND "AIL PRESS SW-1" FAULT, PERFORM ED LRU REPLACEMENT TEST "ROLL SENS" TEST, TEST PASSED. REF. FIM TASK 22-13 TASK 804. INSDR CALA2021080901281Indicator · faulted*DECLARED EMERGENCY* IAS DISAGREE.CAPT SIDE IAS 235.FO SIDE IAS 247 CAPT SIDE APPEARS CORRECT.FL380. SAT-50. LOCKED BY TOMC SR MANAGER DUE TO EMERGENCY BEING DECLARED FOR LANDING UNLOCKING FOR UPDATE. LOOKED AT CAPT AND F/O PITOT PROBE, NO NOTICEABLE BLOCKAGE SDR CALA2021072601194Sensor · malfunctioned*EMERGENCY DECLARED* LEADING EDGE SLAT 7 ILLUMINATED. LE FLAP TRANSIT LIGHT ON FWD I LLUMINATED. PER CREW, SELECTED FLAPS 5, LEADING EDGE TRANSIT AND OVERHEAD SLAT 7 STAYED ILLUMINATED FOR APPROX 5 MIN THEN EXTINGUISHED. SELECTED FLAPS 15, SAME... DECLARED EMSDR CALA2021072601192Control Panel · faultedFAULT LIGHT ILLUM IN ALL POSITIONS IN FLIGHT AND ON GROUND WITH ENGINES RUNNING OHMED OUT ENGINE 1 LOOP B. AND HARNESS. FROM M279 ALL VALUES WITHIN LIMITS REF FIM TASK 26-10-T805. REPLACED FIRE DETECTION PANEL IN COCKPIT REF AMM 26-00-01-000-801 ADD EMP:13769SDR CALA2021071601114Flap · missingPDA 3 LEFT WING INBOARD T/EDGE FLAP OUTBOARD END UPPER SEAL MISSING -- SEE PHOTO . GAP 1 -- ALL OTHER SEALS PRESENT -- REQUEST DEFERRAL THIS IS UPPER SEAL BETWEEN INBOARD AND OUTBOARD FLAPS AT SEAL DISPATCH DESK: 84 NAME: DA DATE: 12-JUL-21SDR CALA2021070501032Circuit Card · unsecureON CLIMB OUT MULTIPLE SYSTEMS ON THE OVERHEAD AND FWD PANEL ANN UNCIATORS FAILED T/S IAW SSM 30-41-11, 33-18-11, 32-61-11, 26-21-11, 32-42-11, 28-43-11, 27-81-31, AND 29-35-11. FOUND M564 NOT SECURED. RE-INSTALLED IAW AMM 33-18-00-960-806. ALL OPS CHECKS NORMSDR CALA2021062800987Drain · leakingENG 1 HYD LOW PRESS LIGHT ON IN FLIGHT QUAN DROPED TO 0 FOUND HYD LEAK COMING FROM RETURN FILTER CASE & CLAM FOUND RETURN FILTER CASE BEND FOUND LEAK COMMING FROM THE FILTER CASE DRAIN ASSY. REPLACED CAS E AS PER AMM 29-11-61 PB401. PRECAUTIONARY REPLACED EDP SDR CALA2021062800974Indicator · split*EMERGENCY DECLARED FOR LANDING* FLAP POSITION INDICATOR HAS NEEDLES SPLIT FLAPS SPLIT ON APPROACH 1 AT 15 1 AT 25 LOCKED L/P UNLOCKED FOR SIGNOFF. LP OPEN. FURTHER DETAILS AWAITEDSDR CALA2021062800973Actuator · inoperativeA AUTOPILOT INOP...WOULD NOT ENGAGE. B AUTOPILOT INOP AS WELL. B WOULD ENGAGE THEN DISCONNECT ACCOMPLISHED CHECKS OF AUTOPILOT B,PASSES LAND VERIFY MCP TEST 6 HE A AILERON ACTUATOR IS BAD, FAILS AILERON BITE CHK FOR HYDRAUL ICS INPUT. 0.30 TO 60.35 , AUTOPILOSDR CALA2021062300944Sensor · faultedAIR RETURN FOR #6 SLAT LIGHT ON OVERHEAD BITE SHOWS SL6 PROX. OUTBOARD. LATCHED LEG 0 AND 1. ADD FAULT: 27-81210 FULLY RETRACTED. SITTING AT THE GATE, #6 SLAT LIGHT GOES FROM ON TO OFF. SLATS PARTS UPLOAD SPLICED IN #6 SLAT SENSOR REF BSWPM 20-10-13 AND W.SDR CALA2021062000913Processor · faultedFUEL QUANTITY INDICATION, FLIGHT COMPARTMENT ERROR OR BLANK CENT ER TANK UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MSDR CALA2021061800895Beam · crackedMOP SEAL AT STUB BEAM 616R CRACKED-N/R 061:29-5710-1-2814/001 00 135-5866697 REPAIRED CREASE BEAM AT STUB BEAM AT STA. 616R/H SIDE IAW B737-7 CTION OF REPAIR AT 36,000 FLIGHT CYCLES OR 12 YEARS AFTER REPAIR INSTALLATION WITH REPEAT INSPECTIONS AT 36,000 FLIGHTSDR CALA2021061500881Beam · crackedMOP SEAL AT STUB BEAM 616R CRACKED-N/R 061:29-5710-1-2814/001 00 135-5866697SDR CALA2021061400873Pcu · leakingSTANDBY RUDDER POWER CONTROL UNIT APPEARS TO BE LEAKING AT FORWARD LOWER "B" NUT OR UNION. SECURED B NUTS. CLEANED AREA. OPPERATED STANDBY HYDRAULICS AND CYCLED RUDDER SEVERAL TIMES. NO LEAKS NOTED.SDR CALA2021061100852Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA. 540 RBL 32.40 IS CRACKED. N /R 00108 REMOVED AND REPLACED SHEAR FITTING AT STA 540 ABD RBL 32.40 IAW B737-700 SRM 51-40-02, AMM 28-11-00 AND DWG 111A2000 REV ORIGINA L. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION USDR CALA2021061100849Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA. 540 LBL 40.87 IS CRACKED. N /R 00114 REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 40.87 IAW B737-700 SRM 51-40-02 AMM 28-11-00 AND DWG 111A2000REV ORIGINAL SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354
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