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 CALA2019080901325Bulkhead · canningAPB FOUND TO HAVE AN "OIL CAN" CONDITION BETWEEN STR 2R AND 3RT. REPAIRED APB OIL CANNING BS 1016 BETWEEN S3R AND S5RT.SDR CALA2019081091321Frame · crackedCABIN FRAME CRACKED AT STA.867 RIGHT BETWEEN S-8RT AND S-9RT(I/B RIVET FOR A/C RAIL ATTACH BRACKET)HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IAW EC/RA 5310-07651,PART 1.SDR CALA2019081091320Frame · crackedCABIN FRAME CRACKED AT STA.380 RIGHT BETWEEN S-8RT AND S-9RT(I/ B RIVET FOR A/C RAIL ATTACH BRACKET) HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER.SDR CALA2019080901319Frame · crackedCABIN FRAME CRACKED AT STA.747 RIGHT BETWEEN S-8RT AND S-9RT(I/B RIVET FOR A/C RAIL ATTACH BRACKET).HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER. ALL WORK ACCOMPLISHED PER EC/RA 5310-07650,PART 1.SDR CALA2019080101279Intercostal · puncturedE&E COMPARTMENT DOOR CUTOUT,INTERCOSTAL WEB AT LBL 6.74 AND BETW EEN STA 323.7 AND 351.2 HAS HOLE PUNCHED IN IT. REPLACED INTERCOSTAL WEB AT LBL 6.74 BETWEEN BS 323.7 & 351.2 RE F SRM 53-10-15,51-40-02,51-40-05,51-20-01 AMM 52-48-41 AND BAC D WG 141A8511,141A8SDR CALA2019080101278Bracket · corrodedSKIN AND FRAME LOCATED BEHIND FWD ACCESSORY DOOR HAS CORROSION U NDER LEVELING COMPOUND BS 277.8 BETWEEN LBL5.7 AND RBL 5.7. REMOVED AND REPLACED CLIP P/N 141A3504-93 AT BS 227.8 BETWEEN LB L5.7 AND RBL 5.7 REF SRM 51-40-02 AND DWG 141A0650 AND REAPPLIED NEW LSDR CALA2019071501202Monitor · faultyENGINE VIBRATION VIBRATION HIGH ENGINE 1 ENG 1 VIB 3.3 ON CLB. 2.7 IN CRUISE. ENG 2 VIB 1.0 CRUISE. CAN FEEL VIB IN CNTRL COL. PERFORMED #1 ENG TRIM BALANCE VIB @ 2.5. NEXT ENG TRIM BALANCE NO DATA ACQUIRED. AVM COMP SHOWED DSP2 ERROR 22 AND ERROR 24 DURING SDR CALA2019071501201Monitor · faultyENGINE VIBRATION VIBRATION HIGH ENGINE 1 ENG 1 VIB 3.3 ON CLB. 2.7 IN CRUISE. ENG 2 VIB 1.0 CRUISE. CAN FEEL VIB IN CNTRL COL. PERFORMED #1 ENG TRIM BALANCE VIB @ 2.5. NEXT ENG TRIM BALANCE NO DATA ACQUIRED. AVM COMP SHOWED DSP2 ERROR 22 AND ERROR 24 DURING FISDR CALA2019071501204Light · missingEMERG EXIT LIGHT MISSING AT SEAT 15C RELAMPED OK. TESTS GOOD.SDR CALA2019070501144Slide · defectiveESCAPE SLIDE CABLE AT DOOR 1R NOT ATTACHED FOUND SAFETY TREAD BROKEN. REMOVED AND REPLACED DOOR 1R SLIDE PACK. REF AMM 25-66-01-400-801 AND REDENDER SAFE CK LIST ACP RII INSPECTION OF #1R SLIDE ASSY. INSTALLATION, REF. GMM 09- 25-05. TRACKING # 1296321 SN OFF SDR CALA2019063001104Thermocouple · malfunctionedEGT EXCEED 965 DEGREEES AFTER TAKEOFF. EGT NORM AFTER THROTTLE R ETARDED PER CREW VERBAL, # 2 ENGINE. BY VERBAL FROM CREW AIRCRAFT WAS NOT IN AN OVERWEIGHT CONDITION AT LANDING. 73-10322, 77-20862, 77-20872, 75-10362, 775-30412, 77-20872, 75-20462, AND 75-3041SDR CALA2019061700978Anti-Ice Valve · inoperativeCOWL VALVE OPEN LIGHT STAYS ON BRIGHT WHEN SWITCH IS MOVED TO ON ENG ANTI-ICE 1 REMOVED AND REPLACED NUMBER 1 ENGINE COWL ANTI ICE VALVE IAW AMM 30-21-11. OPS CHECK NORMAL.SDR CALA2019061700973Ballast · overheatedSMOKE BEGAN TO FILL THE BACK OF THE CABIN. A/C DEPLANED AS QUICK AS POSSIBLE. FOUND SMOKE SOURCE, CEILING LIGHT AND BALLAST ASSEMBLY OVERHEATED ABOVE SEATS 29-30 DEF. REPLACED LIGHT ASSEMBLY OPERATED NORMAL.SDR CALA2019060700901Switch · inoperativeAUTOPILOT 1 AND 2 DO NOT ENGAGE. REMOVED AND REPLACED CAPT''S AND F/O''S A/P DISCONNECT SWITCHES IAW AMM 22-11-41-400-801. OPS CHECK GOOD.SDR CALA2019053100860Sensor · defectiveWITH GEAR HANDLE UP AFTER TAKEOFF THE NOSE GEAR LIGHT SHOWS GREEN AND RED LIGHT. T/S PER FIM 32-09-00-810-818. BITE SHOWS FAULT 32-61004 LATCHED. INSPECTED S845 AND TB42. FOUND S845 OPEN, SUSPECT SENSOR BAD FROM STOCK. REPLACED TB42 AS PRECAUTION. REF AMM 32-6SDR CALA2019052700851Control Module · malfunctionedPRESSURIZATION PANEL WENT COMPLETELY BLANK APPROX 12000 REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE REF AMM 21-31-02. ALL TESTS PASSED. NO FAULTS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1165252 SN OFF 7041 PANEL, PRESS, C OFF 29-2131-9-0006 7041 ONSDR CALA2019052400833Pin · missingVIBRATION REF LOG 3297405, FOUND E&E BATTERY CHARGER TRAY MISSING MOUNTING PINS, BACK SIDE OF BATT CHARGER NOT SECURED TO SHELF PULLING ON BOX HANDLES BACKEND OF BATT CHARGER HITS FLOOR STRUCTURE. REMOVED BATT CHARGER REF 24-31-21-000-802-002, CB'S P92 A-4,E-1SDR CALA2019050300688Tube · chafedWHILE DESCENDING FROM FL390 TO FL330 CABIN ALT HORN SOUNDED. RAN CHECKLIST T/S PER FIM 36-10-00 REF IPC. 36-11-51-02 ITEMS ON NR 1 ENG 220,35, REPLACED LINES AND ON NR 2 ENG ITEM 35 REPLACED LINE. RAN ENG FOUND BLEED PRESSURE NOW WITHIN LIMITS. ALSO REF MM 36-SDR CALA2019042200630Thermocouple · failedR-ENG EGT OVERTEMP DURIN G CLIMB THRU 15000 FT. ARC TURNED AMBE R. MAX EG T SEEN WAS 918C. ENG 2 BITE TEST, MSG NMBR: 77-20872 THE TOP LEFT EGT SIGNAL 77-21-00-810-804-F00 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE - FAULT ISOLATION (T495S4)IS OUT OF RSDR CALA2019041200560Slide · low pressureDOOR 2R SLIDE PRESSURE GAUGE INDICATES NO PRESS URE. REMOVED AND REPLACED DOOR R2 SLIDE ASSY IAW AMM 25-66-01.DOOR OPENING AND CLOSING AS WELL AS ARMING AND DISARMING NORMAL.RII-SDR CALA2019032900490Unknown · odorSMOKE OR FUMES IN CABIN, SOURCE UNKNOWN. SMOKE SMELL APPROACHING DESCENT POINT. SMELL WAS NORMAL AFTER 5 MIN. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. PLEASE EVALUATE AND CONTACT UA TOMC. MAC METER INITIATED FOR WITH VENDOR. MAC RELATED WORK ORDER 0000000SDR CALA2019032900485Circuit Breaker · trippedALL 3 TOILETS ARE NOT FLUSHING. FOUND VACUUM WASTE CB POPPED ON P18-3 PANEL. PER FIM 38-30-00-810-811 CB 1423 WAS NOT CLOSED ON ARRIVAL. VERIFIED M1188 MODULE AT AFT GALLEY SECURE, LCM IN AFT PIT SECURE AND HARNESS, ALL LAV HARNESS SECURE UNDER SINKS. SYSTEM OSDR CALA2019031500406Access Door · dentedEXTERNAL FUSELAGE AT TAILCONE ACCESS DOOR APPROX BS1034 FOUND A DENT AT LOWER CENTER AREA REF N/R 9885924 INSTALLED DOUBLER REPAIR AND FILLER AT DAMAGE AREA BS1034, BL0 PER REF SRM 53-80-01 REPAIR NR 3 - LOWER CENTER AREA AND UNITED ECRA 5331-02336.SDR CALA2019030800367Skin · dentedREF ECRA 5331-02331 AC730, FUSELAGE SKIN STA 867-887, STR 22L-24L INTERIM REPAIR. PART 1, ITEM 2 TO INITIATE A DIP ON OR BEFORE AIRCRAFT REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, TO PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-02331. PLANNING TO CONTACT ENSDR CALA2019030400350Skin · dentedNOTE THIS DAMAGED TRANSFERED FROM LOGPAGE 9006123. DENT IN FUSELAGE SKIN, STA. 827-847, STR. 25LT-27RT. VERIFIED REMOVAL OF DAMAGED MATERIAL. PERFORMED HFEC AROUND CUTO UTS. REF: NDT P6 51-00-00-23. ALSO PERFORMED THICKNESS CHECK 0.002"REMOVED FROM BURNISHED ASDR CALA2019022500295Landing Gear · malfunctionedALL GEAR WOULD NOT RETRACT ON TAKEOFF AFTER DEBRIEFING CAPTAIN HE COMENTED THAT AFTER GETTING ON GROUND HE WAS ASKED TO CK MANUAL EXTENSION ACESS DOOR AND HE FELT LIKE DOOR MIGHT NOT HAVE BEEN SHUT WHILE PRESSING ON DOOR HE HEARD A AUDIBLE CLICK BUT IS NOT POSDR CALA2019020800226Bulkhead Web · crackedHFEC FOUND A CRACK INDICATION AT RIGHT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 45.64 AND 40.00 AND WL200.6 AND 192.0 REF AAR N/R 9885332 ACCOMPLISHED PERMANENT REPAIR AT RIGHT CENTER WING REAR SPAR VERTICAL PRESSRE WEB BETWEEN RBL 40.00 AND 45.SDR CALA2019020800216Floor Support · crackedMAIN CABIN INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0 HAS CRACK AROUND FWD FASTNER HOLE REF AAR N/R9885325 REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 TO STA 360 BL0 PER REF B737 SRM 51-40-02 ADD EMP:V900534SDR CALA2019020100193Landing Gear · malfunctionedON TAKEOFF GEAR DID NOT RETRACT. RAN GEAR DISAGREE CHECKLIST. NO CHANGE PERFORMED BITE ON PSEU AND FOUND NO CURRENT /EXISTING OR FAULT HISTORY. JACKED PLANE FOR GEAR SWING AND FOUND HE GER HANDLE NOT GOING PAST THE "OFF" POSITION. COULD NOT HEAR CONTROL LEVESDR CALA2019012800178Battery Pack · inoperativeCABIN EMERGENCY LIGHTS ON WITH SWITCH IN THE ARM POSITION. REPLACED EMER LT PACK M1668. CORRECTED FAULT AND EMER LTS OPS CK NORMAL REF 33-51-00.SDR CALA2019012800172Oxygen Bottle · leakingOXYGEN REGULATOR OPERATION LEAKING CAPTAIN'S OXYGEN DEPLETED INFLT LOCKING ITEM UNLOCKING PAGE PERFORMED O2 LK CHK. NO LKS NOTED AT BOTTLE AND AT ALL MASKS POSITIONS. REPLACED O2 BOTTLE PER AMM 12-15-21. REPLACED BOTH CAPT AND FO MASKS AS PRECAUTION DUE TO PRESDR CALA2019012500143Bearing · disintegratedLEFT FORWARD ENTRY DOOR WON'T CLOSE ACCOMP SLIDE RENDER SAFE CHK LIST. INSP DOOR CLOSE MECHANISM FOR UPPER AND LOWER GATES. FOUND UPPER GATE CAM FOLLOWER BEARING DISINTEGRATED. REMOVED AND REPLACED BEARING PER IPC REF 52-11-51-05 ITEM290 AND CMM REF 52-16-12/6SDR CALA2019012500142Frame · crackedREFERENCE FLEET CYCLE LOG PAGE 9638646 - PAX CABIN HAS A CRACKED FRAME AT STA 480 BETWEEN STR 8R AND 9R CUT OUT CRACKED AREA OF FRAME AND REPAIRED PER ECRA 5310-07561 REV. A. LOG PAGE CREATED FOR ESFR ONLY, VARIFIED LOG PAGE CLOSED.SDR CALA2019012500141Frame · crackedREFERENCE FLEET CYCLE LOG PAGE 9639455 - PAX CABIN HAS CRACKED FRAME AT STA 867 AND BETWEEN STR 8R & 9R. CUT OUT CRACKED AREA OF FRAME AND REPAIRED PER ECRA 5310-07561 REV. A. LOG PAGE CREATED FOR ESFR ONLY,VARIFIED LOG PAGE IS CLOSED.SDR CALA2019011800122Pressure Deck · crackedREF FLEET CYCLE LOG PAGE 9638267-RT MLG WW VERTICAL PRESSURE WEB CRACKED BETWEEN WL 192.0 AND WL 200.6 RBL 40.00 TO RBL 45.64 REPAIRED PRESSURE DECK WEB PER SRM 57-10-10 REPAIR 3, ALT 2. SEE FLEET CYCLE LOG 9638267 FOR DETAILS OF WORK ACCOMPLISHED. INITIA TED SDR CALA2019011800107Pressure Deck · crackedREF FLEET CYCLE LOG PAGE 9638271-LT MLG WW VERTICAL PRESSURE WEB CRACKED BETWEEN WL 192.0 AND WL 200.6 LBL40.0 TO LBL45.64 REPAIRED PRESSURE DECK WEB PER SRM 57-10-10 REPAIR 3, ALT 2. SEE FLEET CYCLE LOG 9638271 FOR DETAILS OF WORK ACCOMPLISHED. INITI ATED DIPSDR CALA2019011400104Pressure Panel · crackedREF FLEET CYCLE LOG PAGE 9638267-RT MLG WW VERTICAL PRESSURE WEB CRACKED BETWEEN WL 192.0 AND WL 200.6 RBL 40.00 TO RBL 45.64 REPAIRED PRESSURE DECK WEB PER SRM 57-10-10 REPAIR 3, ALT 2. SEE FLEET CYCLE LOG 9638267 FOR DETAILS OF WORK ACCOMPLISHED. INITIA TED SDR CALA2018122872653Plate · fireFO FLIGHT NUMBER REMINDER ON YOKE BEGAN TO SMOKE AND CATCH ON F IRE REMOVED AND REPLACED FO''SMEMORY DEVICE IAW AMM TASK 33-11-00-000-801 AND TASK 33-11-00-400-801.OPS CHECK NORMAL.SDR CALA2018121702589Transmitter · inoperativeFLAP ASSYMETRY STUCK BETWEEN 10-15 DEGREES TRAILING ASSYM IPC REFERENCE # 27-58-01-01 TRANSMITTER SENSOR AT FAULT. REMOVED AND REPLACED LEFT FLAP TRANSMITTER POSITION SENSOR IN REF TO B737- 7-8-9 AMM 27-58-01, OPS CHECKED GOOD. FLAPS OPS CHECKED GOOD. PERFORMESDR CALA2018121102555Wire Harness · shorted2 ENGINE BLEED TRIP OFF LIGHT ON STAYS ALLUMINATED AFTER CHECKLI ST CONTACT TOMC UNLOCKED FOR UPDATE REMOVED CANNON PLUG D528(OVER TEMP SWITCH), WOULD NOT RESET. REMOVED CANNON PLUG D30184, RESET BLEED LIGHT, LIGHT WENT OUT. REMOVED CANNON PLUG D30404 AND FOUNSDR CALA2018120202456Bearing · disengagedNR 1 TIRE LOOSE ON AXLE. UPON INSPECTION FOUND NR 1 TIRE INNER BEARING DISINTEGRATED. REMOVED AND REPLACED TIRE 32-45-11-401. OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED TT 1264140 SN OFF 0641 IPC REFERENCE 32-45-11-401.SDR CALA2018111402371Proximity Sensor · faultedLEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 2 PLACED #2 SLAT INDICATION ON MEL 2704E. REMOVED BULBS FROM AMBER INTRANSIT LIGHT ON FWD PANEL. C\W MEL MX PROCEEDURES. FOUND MSG # 27-81202 ON FSEU AND PULLED AND COLLORED C.B. FOR ADD FAULT: 27-81202 INDICATIONS. FSDR CALA2018101502113Spoiler Sys · malfunctionedSPOILERS AIRPLANE ROLLS RIGHT WHEN THE SPOILERS ARE DEPLOYED EMERGENCY DECLARED. FOURTH WRITEUP. ACFT CURRENTLY OOS.SDR CALA2018100802084Sensor · inoperativeLEFT BLEED TRIP OFF ILLUMINATES. PERFORMED ENGINE BLEED SYSTEM HEALTH CHECK PER TASK CARD 29-3611 -1-7802.FOUND BAR OUT OF RANGE. REMOVED AND REPLACED PER AMM 36- 11-03-400-801. TESTED GOOD. RAN ENGINE 85% N1 BLEED TRIP OF LIGHT ILLUMINATED AFTER 15 SECONDS. RSDR CALA2018100802070Motor · malfunctionedDURING FLT CONTROL RUDDER STANDBY CHECK WITH HYDRAULIC "A" SWITCH ON LOW PRESSURE LIGHT IS ON. R/R STBY RUDDER SOV MOTOR IAW 27-21-94...OPS AND LEAK CK GOOD -END-SDR CALA2018100102027B-Nut · looseHYDRAULIC FLUID FLUID LEAKAGE HYD A LEAK AFTER TAKEOFF HYD AT 86 ON TAXI OUT HYD A AT 40 AFTER GEAR UP THEN SLOWLY DECREASED FOUND PRESSURE LINE B NUT JUST FORWARD OF LEFT LANDING GEAR ACTUATOR LOOSE AND LEAKING. ALSO FOUND LEFT LANDING GEAR UPLOCK ACTUATOR SDR CALA2018092401978Module · faultyCAPT AND F/O UNRELIABLE AIRSPEED/ALTIMETER AND ENG LIGHT ON. AIR SPEED DISAGREE BY200 KTS CREW REPORTS CAPT AIRSPEED DROPPED TO 80KTS. EEC BITE FLT HISTORY SHOWS MSG 73-31641 & 73-31642 ADIRU TOTAL PRESSURE DISAGREE FLUSHED CAPT & F/O PITOT SYSTEM PER AMM 34-1SDR CALA2018091701943Battery Pack · dischargedROWS 30 THRU 34 SEAT AISLE EEL LIGHTS NOT COMING ON DURING CHECK. REPLACED BATTERY PACK AND CHARGER M1672. OPS CHECKS GOOD. REF AMM 33-51-06 C/W IDT REQUIREMENTS.SDR CALA2018082701848Probe · damagedDURING DESCENT, AIRSPEED AND ALTIMETER UNRELIABLE ON CAPTAIN`S AND FIRST OFFICER`S SIDES. ENGINE LIGHT ILLUMINATED. PERFORMED PITOT-STATIC FULL RATE LEAK CHECK TO 35000 FT & 300 KTS ON LEFT & RIGHT SYSTEMS, ALL PARAMETERS MATCH, NO DISAGREE FAULTS IAW AMM SDR CALA2018082001826Power Supply · inoperativeSEAT MOUNTED EMERGENCY LIGHTS AT SEATS 22ABC THROUGH 28ABC WERE INOPERATIVE. REPLACED THE M1670 POWER SUPPLY ASSY IAW AMM 33-51-06. CHECKED NORMAL.
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