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 CALA2011111500736Battery · dischargedMULT-33-3-0001 DOOR R1 EMERGENCY LIGHT FOUND DIM. DOOR R1 EMER LIGHT POWER PACK BATTERY REPLACED AND TEST CARRIED OUT NORMAL AMM 33-51-06 S/N ON : 803761 S/N OFF:30748.SDR CALA2011111500735Actuator · failedAFTER T/O RT RAM DOOR FULL OPEN LIGHT ILLUMINATED. MX ADVISED US TO RESET RAM AIR DOOR CB'S (RAM AIR MOD RT AND RAM AIR MOD CONT RT). DOOR REMAINED OPEN WITH NOTICEABLE VIBRATION. AIR RETURN W/O INCIDENT. REMOVED AND REPLACED RT RAM AIR DOOR ACTUATOR IAW ASDR CALA2011102800696Pressure Switch · inoperativeNR 1 FUEL FILTER BYPASS LIGHT ILLUMINATED INFLIGHT. PER FIM TASK 73-05-00-810. REMOVED NR 1 ENG FUEL FILTER. NO CONTAMINATION FOUND. REPLACED FILTER PER AMM 73-11-02-400-801. ALSO REMOVED AND REPLACED NR 1 ENG FUEL FILTER DIFF PRESSURE SWITCH AMM 73-34-01.SDR CALA2011102800694Cable · faultyFLIGHT ATTENDANT AND THREE PAXS INCLUDING ONE PASS TRAVELING PILOT REPORTED A HOT SMELL LIKE SOMETHING BURNING JUST AFTER DOOR CLOSURE. AFTER INTERVIEWING FLT CREW AND PAX, ISOLATED FAULT AREA BETWEE N 20B,C AND 21A,B,C. FOUND SEB CABLE BETWEEN 20B AT J2 CONSDR CALA2011102000679Lens · missingOVERWING EXIT ABOVE DOOR AT ROW 20 MISSING. INSTALLED OVERWING EXIT LENS P/N 29-3351-3-0025. OK FOR SERVICE WPB 2779242.SDR CALA2011102000677Connector · looseNR 2 ENGINE A LOOP INOPERATIVE AFTER TAKEOFF, RECIEVED A FAULT LIGHT, INTERMITTENT CONTACT. MX RESET CIRCUT BREAKER IAW INSTRUCTION, FAULT LIGHT WENT OUT. CONTINUED ON TO DESTINATION. 2 HRS LATER FAULT LIGHT ILLUMINATED AGAIN, LANDED IAW QRH. FOUND CONNECSDR CALA2011101900671Wire · missingEMERGENCY PATH LIGHT AT SEAT 10ABC INOP. FOUND WIRE (GRD) MISSING FROM FLOOR CONNECTION TO SEAT HARNESS. NEEDS WIRE AND PINS/PLUG ASSY. NSU DFW.SDR CALA2011101800666Seal · wornON TAKEOFF AN AIRCRAFT ON GROUND BEHIND US REPORTED WHAT THEY THOUGHT WAS FUEL LEAKING FROM LEFT WING. TEMP AND DEWPOINT WAS 26/08 VERY DRY AIR CONTINUED TO NEXT LOG PAGE 8912999 LOG NOTED SEE L/P 8912999 FOR CORRECTIVE ACTION AND SIGN OFF - CHECKED VOLUMETRSDR CALA2011100700651Regulator · inoperativeAT CRUISE AND CLIMB DUCT PRESSURE SPLIT OF 30 PSI L/12PSI R/46 PSI ON DESCENT R/35PSI L/8PSI CABIN VSI ON PRESSURIZATION PANEL FLUCTUATED FROM 0 CLIMB TO 1000 FT PER MIN T/S REF AMM 36-10 FOUND A/C TO BE OK. RAN LEFT ENGINE AND ALL PRESSURE GOOD SEE L/P 89127SDR CALA2011093000633Valve · faultyAIR MIX VALVE STUCK FULL COLD POSITION LEFT PACK. PLACED LT PACK ON MEL C/W DDP A/C OK TO CONT SVC. REMOVED AND REPLACED LEFT AIR MIX VALVE, PERFORMED TEST OPS CHECK GOOD, REF AMM 21-61-02. MEL REMOVED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1400635 S/SDR CALA2011092700627Unknown · malfunctionedSHUT DOWN NR 1 ENGINE PER "FUEL LEAK" CHECK LIST. WINDMILL APPROX 45 MIN. MAINTAINED HYDRAULIC PRESSURE AND POSITIVE OIL PRESSURE. PERFORMED POWERPLANT ADJ & TEST 3A,3B,5,8 & TEST 13. ALL TEST PARAMETERS NORMAL. FUEL FLOW NORMAL FOR BOTH ENGS.SDR CALA2011092200618Probe · obstructedAMBER "IAS DISAGREE" ON BOTH LEFT & RIGHT AIRSPEED INDICATORS. LEFT AIRSPEED .78 MACH/230KTS, AMBER AIRSPEED BUG AT 230 KTS (AT 41,000) NO PROBE HEAT BREAKERS POPPED. T/S PER FIM 31-62. FOUND F/O'S PITOT PROBE WITH BLOCKAGE. REPLACED SAME PER AMM 34-11-01. SDR CALA2011091900603Skin · crackedRT HORIZONTAL STAB LOWER SPAR SKIN SHOWS CRACK AT STA 129.50 I/B DRAIN HOLE (MARKED). REPAIRED RT HORZ STAB SKIN CRACK AT STA 129.50 USING REPAIR 11/CHAP 55-10-01 PG 201-217. REPAIR IS A CAT B PER TABLE 204/ PG216. INSP THRESHOLD 56,000 FLT CYCLES AFTER RESDR CALA2011091600601Indication Sys · malfunctionedLARGE DISPARITY BETWEEN FOB GAUGES AND FMC FUEL. GAUGES DISPLAYED 900LBS LESS TOTAL FUEL. CORRECTED STA TO BHM (IAH ENTERED IN ERROR) PERFORMED FUEL QTY BITE TEST IAW FIM 28-41-00-810-801 NO FAULTS FOUND. VERIFIED FUEL LOAD USING STICKS NR 6 RT 5.4 AT 7,498SDR CALA2011091600600Unknown · malfunctionedDURING DESCENT STARTING AT 15000 FT 3 DIFFERENT TIMES THE AIRCRAFT SNAP ROLLED TO APPROXIMATELY 30 DEG OF RIGHT BANK REMAINED THERE FOR A SECOND OR TWO THEN ROLLED AGGRESSIVELY BACK TO WINGS LEVEL OVER SHOOTING WING LEVEL CONTINUED ON NEXT LOG PAGE. T/S PER FISDR CALA2011091400596Actuator · bypassingLANDING GEAR LEFT SIDE, GREEN LIGHT DOES NOT COME ON WITH LANDING GEAR LEVER DN, LEFT GEAR RED LIGHT ON, INDICATIONS NORMAL AFTER ALTERNATE GEAR EXTENSION. DUE TO HISTORY, PERFORMED A/C GEAR SWING IAW AMM 32-32-00-710- 801. DUPLICATED FAULT & FOUND DOWN LOCKSDR CALA2011091200591Proximity Sensor · faultyON APPROACH INTO GUM GEAR HANDLE SELECTED DOWN, LEFT MAIN LG UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT ON FRONT PANEL OR OVERHEAD PANEL. QRH UTILIZED AND MANUALLY EXTENDED GEAR. LANDED NORMAL. FOUND S0302 FAULTY, REPLACED SENSOR PER AMM 32-61-31. OPS CHESDR CALA2011091200587Adiru · malfunctionedAFTER DESCENT FROM FL 400, MULTIPLE FLAGS ILLUMINATED: ALT LIMI T, ALT DISAGREE, BOTH EEC LIGHTS ALTN, SINGLE CHANNEL SPEED TRIM AND COMPLETE LOSS OF AIRSPEED ON F/O SIDE (ALSO REF PAGE 8742 412). REPLACED RIGHT ADIRU PER AMM 34-21-01 PERFORMED ADIRU OPS TESTSDR CALA2011090100570O2 Generator · dischargedREF L/P 8853586 FOR SMOKE SMELL IN CABIN FOUND O2 GENERATOR AT 10ABC DISCHARGED AND CAUSE OF ODOR REPLACED SAME IAW AMM 35-22-11-401. OK FOR SERVICE.SDR CALA2011090100568Control Module · failedAFTER TAKEOFF OUT OF DFW LANDING GEAR LEVER STIFF TO GO FROM UP TO OFF AND STIFF TO LATCH OFF. R&R LANDING GEAR CONTROL LEVER MODULE IAW AMM 32-31-11. PERFORMED GEAR SWING IAW AMM 32-32-00. OPS CHECK NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT 1407483 SDR CALA2011083000566Fseu · inoperativeFLAPS WOULD NOT EXTEND PAST 10 DEGREES ON LANDING PERFORMED ALT FLAP LANDING AT FLAPS 15 DEGREES. FSEU SHOWS FAULT 27-53279-L 28VAC EXC INV. FAULT CLEARS. CK`S VOLTAGES IAW FIM 27-51-00-810-822. VOLTS CHECK GOOD. R&R FSEU PRECAUTIONARY. PERF ALL TEST IAWSDR CALA2011082900559Slide · defectiveSLIDE NOT PROPERLY ARMED AT DOOR 1L CAUSING THE LANYARD TO BE EXPOSED REMOVE AND REPLACE SLIDE ASSY PER AMM TASK 25-66-01-000-400- 801 END ROTABLE PARTS CHANGE WAS INDICATED - TT # 1481981 SN OFF 03422 SLIDE, B737NG, OFF 29-2561-9-0003 3422 ON 29-2561-9-0003SDR CALA2011081200533Skin · dentedA DENT MARK WAS FOUND ON LWR EDGE OF FWD CARGO DOOR OUTER SKIN. DENT MEASURED 1.5 INCH BY 3 INCH WITH A DEPTH OF 0.095 INCH WHICH EXCEEDS SRM 52-30-01 ALLOWABLE DAMAGE. INTERIM REPAIR C/W PER PART-1 OF ECRA 5310-05309, REV-A. INITIATED A DIP TO "PERFORM A PERSDR CALA2011072200507Intercostal · crackedSTRESS WEB UPPER FLANGE CRACKED AT FASTENER HOLE STA 328 TO STA 344 APPROX LBL 45. REPLACED INTERCOSTAL AT STA 328 TO 344 AS REQUIRED IN ECRA-5321-01524.SDR CALA2011070800473Electronic Unit · malfunctionedCOMM NR 1, 2, 3 (HEAD) FAILED. COULD NOT TRANS/OR RECEIVE FOUND REU AT FAULT KEEPING A HOT MIC CONDITION. REMOVED AND REPLACED REU PER 23-51-01. OPS CHECK GOOD. ALL VHF'S TRANSMIT/RECEIVE ROTABLE PARTS CHANGE WAS INDICATED - TT 1433513, S/N OFF 03064 UNITSDR CALA2011053100406Skin · damagedAS PER ECRA 5330-04134 INITIATE DIP FOR PERMANENT REPAIR. PER ECRA 5330-04134 TO ACCOMPLISH PERMANENT REPAIR WITHIN 24 MONTHS FROM MAY 28 2011. PLANNING TO CONTACT ESC AFTER 21 MONTHS BEFORE 22 MONTHS FOR PERMANENT REPAIR INSTRUCTION. FUSELAGE SKIN DAMAGED SDR CALA2011051600368Cable Assy · disconnectedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF LANDING WEIGHT 148.0 SMOOTH LANDING REF FIM 32-30-00-810-813. FOUND GSBV INTERLOCK ACTUATING CABLE DISCONNECTED. RECONNECTED REF AMM 27-12-00-820-803 FIM REPAIR CONFIRMATION GOOD.SDR CALA2011050600349Unknown · odorAPPROX 2000 FEET ELECTRICAL SMELL BURNING/HOT WAS DETECTED BY COCKPIT CREW & F/A FIRST CLASS. OVENS WERE NOT IN OPS. PERFORMED FIM 21-00-00-810-806. NO FAULTS NOTED. RUN BOTH ENGINES AT TAKEOFF POWER, BLEED ON PACKS ON, RECIRC FANS ON. NO ODOR OR BURNING SDR CALA2011042800324Warning System · false indicationON CLIMB OUT, NR 2 ENGINE EGT EXCEDANCE BOX FLASHEDRED. NO PARAMETERS EXCEEDED. INSPECTED CDU FOR EXCEEDANCES, NONE DETECTED. THIS IS A NUISANCE FAULT MESSAGE. CLEARED & RESET DEU. OK TO CONTINUE. NOTIFIED ENG DESK IN IAH. OK TO CONTINUE.SDR CALA2011042600310Skin · gougedPER ENGINEERING REQUEST, STA 380 S10 REPAIR REQUIRES FURTHER EVALUATION BY BOEING, REF NR 5750953. REPAIRED STA 400 STRINGER 10L GOUGED PER EC/RA 5331-01557. D.SDR CALA2011040400256Unknown · malfunctionedON T/O FROM EWR NOTICED A SMALL SPLIT IN N1 ON CLIMBOUT ACARS MESSAGE ON PRINTER NOTIFYING US THAT LEFT PACK WAS OFF. LEAD US TO BELIEVE WE HAD A PACK PROBLEM WHEN WE IN FACT HAD A NR 1 ENG. BLEED TRIP ON T/O WITH NO INDICATION/ MASTER CAUTION OR WARNING. SDR MZZA2011030700008Adiru · failedBOTH EEC ALTN LIGHT ILLUMINATED. CDU BITE TEST FOUND ADIRU NR 1 (LT) FAULTY. REMOVED AND REPLACED SAME PER AMM 34-21-01. ALL CHECK NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT 1445854, S/N OFF 01549 UNIT, ADIRU, AI OFF 29-3421-9-0002 1549, ON 29-3421-SDR CALA2011030400118Window · crackedR2 WINDOW STARTED DEVELOPING CRACKS IN LOWER RIGHT CORNER. CREW OBSERVED PROGRESSIVE AREA LENGTHENING IN DELAMINATION AND CRACKS REMOVED AND REPLACED R2 WINDOW PER AMM 56-12-11. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1433394 S/N OFF 02399 IPC REFERENCE NSDR CALA2011021500092O2 Generator · failedA OXYGEN GENERATOR AT LAVATORY 2 L DID NOT FIRE. TEMPERATURE INDICATOR DID NOT TURN BLACK. DRAGER P/N E71720-00, BOEING P/N S417T401-43, LOT NR ARNA-F 001. EA 3520-01277. NO OTHER DEFECTS NOTED.SDR MZZA2011021000006Battery · dischargedA/C LEFT EMERGENCY FLIGHTLIGHT WILL NOT TEST. REMOVED AND REPLACED SAME FLASHLIGHT BATTERY PER AMM 25-64-00, OPS CK & TEST OK.SDR CALA2011052000377O-Ring · not seatedENGINE OIL QUANTITY DROPPED OFF RAPIDLY INFLIGHT. ON APPROACH - DROPPED AS LOW AS 12 PERCENT, 19 PERCENT AT GATE ON ARRIVAL. DIVERTED TO DEN TO AVOID ENGINE DAMAGE. FOUND OIL LEAKING FROM AROUND MCD'S. REMOVED & REPLACED O-RINGS & D-RINGS ON ALL 3 MCD'S. SDR CALA2011052000376Acm · contaminatedDURING LIFT OFF SMOKE BILLOWING OUT OF CAPTAINS SIDE AIRVENT. D ON O2, SMOKE GOGGLE RAN QRH. RETURNED TO EWR REF LP'S 4393415, 4383411, 8210336 AND 8210335 FOR CORRECTIVE ACTIONS. ALSO PERFORMED HIGH POWER ENG RUN W/ BLEEDS AND PACKS ON (NR 1 AND NR 2) NO SMSDR CALA2011013100050Cable · looseAFTER T/O LANDING GEAR HANDLE COULD NOT BE RAISED TO UP POSITION. INSTALLED LOCKING WASHER ON RIGHT MAIN LANDING GEAR TELEFLEX CABLE REF M/M 27-62-51. JACKED A/C REF M/M 7-11-01 AND PERFORMED MLG OPERATIONAL TEST REF M/M 32-32-00 CHECK GOOD OK TO CONTINUE.SDR CALA2011013100049Unknown · smokeON TAKEOFF ROLL AT ABOUT 110 KNOTS, CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE, AS WE PITCHED UP SMOKE INCREASED DRAMATICALLY FILLED THE COCKPIT FROM CEILING DOWN TO THE POINT WHERE F/O HEAD WAS NOT VISIBLE AND BREATHING IMPAIRED. SMOKE WAS COMING OUT OF EXHASDR CALA2011012100030Skin · crackedSUPPORT TASK - CRACK INDICATION LOCATED AT RT HORIZ STAB LOWER SURFACE AT STA 133 BETWEEN RIBS 5 AND 6. REPAIRED CRACK ON RT HORIZONTAL STAB IAW EC/RA 5510-02144.SDR CALA2011011700026Battery · dischargedON PREFLIGHT - F/A FOUND AFT FLASHLIGHT NOT FLASHING. R&R'ED BATTERY AFT OUTBOARD FLASHLIGHT. IND TEST OK - TO CONTINUE.SDR CALA2011032900223Structure · wornSUPPORT TASK: GROUND PNEUMATIC ACCESS DOOR CENTER OUTBOARD LATCH WORN INFRASTRUCTURE REPAIRED GROUND PNEUMATIC ACCESS DOOR AREA STRUCTURE PER EC/RA 5350-01993.SDR MZZA2011011000001Control Unit · failedDURING FLIGHT F/O UNABLE TO TRANSMIT USING R/T SWITCH OR HAND MIC VHF RADIOS MAKING POPPING SOUNDS AND TRANSMIT- TING WHEN RADIO NOT IN USE, INTERFERING WITH ATC COMMUNICATIONS. REF FIM 23-11-00-810-806. FOUND REU AT FAULT. REMOVED AND REPLACED REU PER AMM 2SDR CALA2010122200629Battery Pack · dischargedMULT-33-3-0001; LT EXTERIOR OVERWING HATCH EMERGENCY EXIT LIGHT IS INOP. REMOVED & REPLACED BATTERY PACK M1668, PERFORMED OPS CHECK GOOD IAW B737-700AMM 33-51-06.SDR CALA2010122200628Wire · brokenMULT-33-3-0001; SEAT ROW 22 RT OVERHEAD STOWAGE BIN EMERGENCY EXIT AISLE LIGHT IS INOP. REPAIRED WIRE AT BULB, WIRE W4142 AT STA 680 WITH AN ENVINOMENTAL SPLICE IAW BSWPM 20-10-13 & AMM 33-55-11, EMERGENCY LIGHT CHECKS GOOD IAW J/C 29-0550-8-0002.SDR CALA2010122200627Wire · brokenMULT-33-3-0001, SEAT ROWS 1 & 2 LT EMERGENCY EXIT FLOOR PROXIMITY LIGHTS ARE INOP. REPAIRED BROKEN WIRE WITH ENVIROMENTAL SPLICE IAW BSWPM 20-10-13, WIRE W3142 AT STA 399. OPS CHECKED GOOD IAW B737-700 AMM 33-55-11.SDR CALA2010120300604Oven · smokeON TAXI OUT F/A REPORTED ALARM (SMOKE) IN AFT LAV, A/C LEFT ACTIVATED AFTER F/A OPENED REAR GALLEY OVEN. F/A REPORTED SMOKE INITIALLY CAME FROM OVEN BUT DISSIPATED. LAV ALARM CONTINUED TO SOUND AT GATE. INSPECTION FOUND NO SMOKE. MX CALLED PER F/A BRIEFINGSDR MZZA2010120100032Skin · dentedAFT CARGO DOOR HAS DENT APPROX 5 INCHES THRU 8 INCHES BELOW DOOR HANDLE & GOUGE 13 INCHES BETWEEN BELOW DOOR HANDLE 8 INCHES LONGTO BTM EDGE STA 827. GOUGE EXTENDING TO FUSELAGE BETWEEN STA 787 & 827, 57 INCHES LONG BETWEEN STRINGERS S25R & 25L. GROUND DAMAGSDR MZZA2010120100031Skin · damagedREF L/P: 7905537 AND NON ROUTINE 4337457 AFT CARGO DOOR HAS A DENT APPROX 5 INCHES THRU 8 INCHES BELOW DOOR HANDLE AND GOUGE 13 INCHES BELOW DOOR HANDLE 8 INCHES LONG TO BOTTOM EDGE STA 827. NON ROUTINE CLOSED IN ERROR. REPAIR COMPLETED IAW ECRA 5232-01112 RSDR CALA2010111900586Wire Harness · brokenSUPPORT TASK - EMERGENCY LIGHT WIRE BROKEN AT SEAT ROW 30, O/B LEG. REMOVED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROW 30 LT IAW CMM 25-25-99. OPS CHECK WILL BE PERFORMED ON EA 4420- 01009 REV E OPS 36 STEP 2A. WORK PERFORMED BY SX992.
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