Boeing 737-924ER
Service difficulty reports · 3,682
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 = '737924ER' 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 = '737924ER' 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 CALA2025110310847Valve · stuckALL LAVS OUT OF SERVICE. FOUND LAV D GATE VALVE STUCK OPEN, DEPLETING VACUUM FROM OTHER TOILETS. AFTER MANUALLY CLOSING LAV D GATE VALVE ALL OTHER TOILETS OPS NORMAL ON GROUND. REF LOG PG 6790548 FOR WORK ACCOMPLISHED. OPS CHECK GOOD. NO LEAKS NOTED. NO FURTSDR CALA2025110210811Skin · crackedINSPECTING THE FASTENER HOLES ON LEFT WING INBD L/E, UPPER SPAR ATTACH, ON N/R 5000-0108, EA 5720-02922, FOUND 2 EXISTING HOLES OF 0.250" DIAMETER WITH CRACKS IN SKIN ONLY. ACCOMPLISHED REPAIR OF LTT WING INBD LEADING EDGE SKIN IAW SRM 57-41-01-2R-8.SDR CALA2025110210809Wire Harness · damagedEMERGENCY LIGHT WIRE HARNESS DAMAGED. REMOVED AND REPLACED THE DAMAGED SECTION OF WIRE HARNESS IAW DRAWING 40N018 10, REV ORIG. SHEET 2, PAGE 11, SWPM 20-90-14, AND AIPC 25-27-31-47A.SDR CALA2025110210807Wire Harness · damagedEMERGENCY LIGHT HARNESS AT BS 570 LT HAS A DAMAGED SECTION WIRING. REMOVED AND REPLACED DAMAGED SECTION WIRE HARNESS AT BS 570 IAW DRAWING 40N01810, REV ORIG. SHEET 2, PAGE 8, SWPM 20-90-14, AND AIPC 25-27-3 1-47A.SDR CALA2025112111386Channel · corrodedFWD CARGO COMPARTMENT RT ZEE CHANNEL POSSIBLE CORROSION BTW BS 500D - 500L. REMOVED, FABRICATED, LOCATED, DRILLED, AND PERFORMED COUTERSINK ON FWD CARGO RT ZEE CHANNEL. APPLIED ALODINE A ND PRIMER ALL WORK DONE IAW SRM 51-40-02-0G-0, 53- 00-53-2R-5, 51-40-0SDR CALA2025112111384Shield · corrodedAFT CARGO, FOUND MULTIPLE POINTS OF CORROSION ON RT SHIELD, BTW BS 767 - 787, REMOVED AND INSTALLED NEW SHIELD ON AFT CARGO COMPARMENT BTW BS 767 - 787, STRINGER 25 IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, AND 51-40-02-0G-0. ALL WORK PERFORMED CAPTURED ONSDR CALA2025111211141Skin · corrodedRIGHT WING LEADING EDGE LOWER SKIN UPPER SURFACE FROM OFSS 706 TO 696 HAS CORROSION. ACCOMPLISHED INTERIM REPAIR FOR CORROSION ON RT WING LOWER SKIN PANEL FORWARD OF FRONT SPAR BETWEEN OFSS 692 AND OFSS 704 IAW ECRA 5724-01040 REV A, PART 1.SDR CALA2025103110764Girt Bar · unpackedMATERIAL ON 1R DOOR SLIDE IS DRAGGING. REPACKED DOOR SLIDE GIRT BAR MATERIAL IAW AMM 25-66-01-000-804.SDR CALA2025103010758Skin · dentedLH FUSELAGE STA 500D- 500F BETWEEN S-16L TO S-17L HAS DAMAGE. PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN STA 500D - STA TO 500F AND S-16L - S-17L IAW EO 250389 REV P1, P2, P3, P4, P5 AND EO 250389 REV IR AND ECRA 5331-03186. THIS REPAIR IS CLASSIFIESDR CALA2025103010755Blades · damagedCOMPRESSOR STALL AT 2500 FT, ENG 2. ENG SHUTDOWN. NORMAL LANDING, PERFORMED INLET AND EXHAUST VISUAL INSP REF FIM 71-05 TASK 804.NO FOD OR DEFECTS NOTED. PERFORMED EEC BITE CHK REF MM 73-00 TASK 803. NO FAULTS FOUND. PERFORMED ACTUATORS TEST REF MM 71-00-0SDR CALA2025102910712Light · brokenEMERGENCY LIGHT AT SEAT 28 C, BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-11-960-802SDR CALA2025102910680Fuse · no testEMERGENCY LIGHTING SYSTEM OPS CHECK IAW B737-33-3-0235, EMERGENCY AISLE LIGHTS AT SEAT ROWS 29DEF AND 34DEF INOPERATIVE. REMOVED AND REPLACED FUSE OF EMERGENCY EXIT LIGHT BATTERY PACK M3379 IAW AMM 33-51-06-960-804 AND WDM 33-51-13-6.1. OPS CHKD NORMAL.SDR CALA2025102910710Rib · crackedCRACK INDICATIONS FOUND ON RT HORIZ STAB HSS 129.50 IN LWR SKIN RIB, (SECOND LAYER). REMOVED FWD SPAR WEB TO GAIN ACCESS IAW SRM 51-40-02. REMOVED & CUT CRACKED AREAS IAW SRM 55-10-09-2R-5 REPAIR 5. NDT VERIFIED NO CRACKS. FABRICATED TWO FILLERS AND TWO ANGLESDR CALA2025103010719Door · no discrepancyFA REPORTS DOOR 2R KEEPS MOVING UP INFLT PRESSURERIZATION WAS NORMAL. PERFORMED GVI OF DOOR 2R ROLLER CAMS, LATCH ROLLERS AND DOOR INDICATION SENSOR FOR WITNESS MARKS OR CONTACT WEAR. NO DEFECTS FOUND. REF FIM 52-10 TASK 815. DOOR OPENS AND CLOSES NORMALLY, ISDR CALA2025103010718Sensor · false activationDOOR WARNING ANNUNCIATOR IS ON FWD ENTRY ILLUMINATED ON DESCENT AROUND 6000 FT. FA PUSHE D HANDLE DOWN VI A CHECKL IST. LIGHT EXTIGUISHED. COULD NOT DUPLICATE FAULT REQUEST MEL 5203E ON FWD ENTRY DOOR. MEL 5203E TOMC REJECTING FOR MORE T/S. AMM 52-11-00-820-8SDR CALA2025102910716Sensor · faultedCHIME ALERTED LEFT ENGINE BLEED TEMP NEARING BLEED TRIP OFF, DURING CRUISE AND DESCENT. THE BLEED REPORT CAPTURED THAT THE PRE-COOLER OUTLET TEMPERATURE REACHED AS HIGH AS 490 °F, RESULTING IN A LOW BLEED DUCT PRESSURE OUTPUT OF 17 PSI. (SYSTEM HAS GONE INTO SDR CALA2025102810648Light · brokenSEAT 15C ON THE AISLE SIDE HAS A COVER TRIM PIECE MISSING WITH W IRE HANGING OUT UPDATE ADDING IMAGE PIC UPDATE REPLACEMENT LIGHT ASSEMBLY IS ATTACHED TO THE HARDNESS. NEED BUMPER INSTALL FIRST SEE LOG PAGE 6747943 INSTALLED EPL BUMPER ASSY AND LIGHT ASSY REF SDR CALA2025102810668Speed Brake · faultedSPEEDBRAKE DO NOT ARM LIGHT ILLUMINATED AT 70KTS DURING TAKEOFF. REQ MEL 2707F. VERIFIED MANUAL SPEEDBRAKE DEPLOYED AND STOWED. OPENED AND COLLARED C/B PER THE MEL. PLACARD APPLIED. PERFORMED FIM TASK 27-62 TASK 802 STEP E (2) . NO FURTHER ACTION REQUIRED . NSDR CALA2025102810645Anti-Ice Valve · faultedCOWL VALVE OPEN LIGHT STAYS ON BRIGHT WHEN THE ENG ANTI-ICE SWIT CH IS MOVED TO ON ENG-1 ENG1 COWL VALVE OPEN LIGHT STAYS ON W AMBER TAI ON MFD WHEN AI S ELEC TED ON REMOVED E1 COWL ANTIICE VALVE SN 1365C AND INSTALLED A NEW SERVICEABLE VALVE SN 875C PER AMM TSDR CALA2025102710562Unknown · odorMUSTY SMELL FROM A/C PACKS, STARTED DURING T/O ROLL AND CONTINUED DURING CLIMB. SMELL GONE AT CRUISE. PERFORMED ENGINE WASH AT LAST NIGHT STATION. WITH THAT INFO WE CHANGED RECICULATION FILTER AND RAN PACKS, CHECKED OK. MM 21-25-01. FIM 21-00 TASK 806.SDR CALA2025120111601Angle · corrodedFWD CARGO COMPARTMENT LOWER CENTER BULKHEAD ANGLE SUPPORT STA 500L POSSIBLE CORROSION. REMOVED AND REPLACED ANGLE SUPPORT AT FWD CARGO COMPARTMENT LOWER CENTER STA 500L ALL WORK DONE IAW 51-40-02-0G-0 STEP 4 AND 7, SRM-51-40-05-0G-0 STEP4 AND SRM 51-40-08-0G-SDR CALA2025102810628Battery · dischargedEMERGENCY LIGHT BATTERY AT M1672 AND M1695 ARE DEAD REPLACED BOTH BATTERIES IN REF TO AMM 33-51-06-960-805. OPS CHECK GOOD. EMERGENCY LIGHTS NOT A RII OR IDT INSPECTION ITEM. BATTERY RPLD.SDR CALA2025102810618Bracket · looseDOOR 1R GIRT BAR BRACKET LOOSE. PERFORMED INSPECTION AND OPS CHECK OF GIRT BAR LEAF SPRING NO DEFECTS NOTED. HARDWARE IS SECURE AND LEAF SPRING HOLD GIRT BAR SECURE REF AMM 25-66-10.SDR CALA2025102710590Unknown · odorODOR PRESENT IN FLIGHT DECK AND CABIN IN THE CLIMB FOR 3-5 MINUT ES UPON ARRIVAL SPOKE WITH CREW, ALL CREW REPORTED VERY FAINT SMELL THAT DISIPATED QUICKLY, HAD CREW FILL OUT SMOKE REPORT. RAN PACKS, OVENS, DID GVI ON ALL SURFACES IN COCKPIT AS WELL AS FWD ANDSDR CALA2025102810637Skin · crackedCRACK INDICATION FOUND AND VERIFIED: R/H HORIZ STAB LOWER SKIN STA 120.30 MARKED #1 .900"L 17" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVALUATED CRACK ON LOWER SKIN AND CUT OUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 55-10-01- 2R-11. FABRICSDR CALA2025102810635Skin · crackedCRACK INDICATION FOUND AND VERIFIED, R/H HORIZ ST AB LOWER SKIN STA 120.30 .800L 25.5" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVAL CRACK ON LOWER SKIN STA 120.30, 25.5 INCHES OF FRONT SPAR, CUTOUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 5SDR CALA2025102710574Channel · corrodedAFT CARGO, FOUND MULTIPLE POINTS OF CORROSION ON RT ZEE CHANNEL, BTW BS 867 TO 947. REMOVED AND REPLACED RT ZEE CHANNEL BTW BS 867 TO 947 IAW IAW SRM 53-00-53-2R-6, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, AMM 51-21-41-370-80, AMM 51-21-72-37SDR CALA2025102710565Stub Beam · gougedR-1 DOOR HANDLE BOX CUTOUT UPPER TORQUE TUBE BUSHING STUB BEAM IS GOUGED. REMOVED STUB BEAM GOUGED IAW B737-900 SRM 51-40-02. INSTALLED NEW STUB BEAM IAW B737-900 SRM 51-40-02, BAC DWG 141A6523.SDR CALA2025102410487Guide Arm · lack of lubeMAIN CAB DOOR LIGHT ON DURING TAXI POST LANDNG CLEANED/GREASED GUIDE ARM AREAS REF AMM 52-11-21-400-802 AND AMM 12-25-11-640-801. OPEN AND CLOSED DOOR WITH NO FAULTS FOUND. LIGHT TURNED ON AND OFF WHEN COMMANDEDSDR CALA2025102310447Fuse · inoperativeFOUND EMERGANCY LIGHTS ON ROW 15, 20 AND 21 INOPERATIVE. REMOVED AND REPLACED FUSES ON EMERGANCY BATTERY POWER SUPPLY ON STATION 565. REF AMM 33-51-06-960-804. OPS CHECK GOOD.SDR CALA2025102310441Pressure Deck · deformedCOCKPIT FLOOR DENTED JUST AFT OF PEDESTAL. ELEVATED FLIGHT DECK FLOOR WEB BETWEEN BS 250-260 LBL20-RBL20, FOUND AREAS WITH SHARP GOUGES, OUT OF LIMITS IAW SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 SECT 41. FLOOR STRUCTURE FIG 105 SHT 2 DETAIL D. REMOVED DAMAGED SDR CALA2025102210408Sign · brokenSEAT 39C AISLE EMERGENCY MARKER IS BROKEN REMOVED AISLE EMERGENCY LIGHT AT 39C, LACARD PLACED ON FA PANEL. REQUESTING 3319E MEL 3319E LIGHT IS WITHIN 2 SEAT ROWS OF A MONUMENT AND MUST WORK MOVED 34 C TO 39 C. OPS CHECKED EMERGENY AISLE LIGHTS. OPS CHECKED GOOSDR CALA2025102410499Valve · faultedLEFT BLEED TRIP OFF LIGHT ILLUMINATED REPEAT WRITE UP. NR 1 ENG HIGH STAGE REGULATOR (HSR) FAIL HEALTH CHECK TEST REGULATOR, REMOVED N REPLACED HI STAGE REGULATOR REF AMM 36-11-07 OPS CHECKS GOOD. PERFORMED HEALTH CHECK FOR 1 ENG, FOUND BLEED AIR REGULATOSDR CALA2025102310451Slide · no discrepancyDOOR 2R SLIDE FABRIC STICKING OUT PERFORM SLIDE PACK, CHECKED 2L. IAW AMM 25-66-01-200-802. GIRT FABRIC IN NORMAL FOLD & POSITION.SDR CALA2025102110363Battery Pack · inoperativeEMERGENCY EXIT LIGHTS STAY ON IN ARMED POSITION. REMOVED & REPLACED RIGHT EMERGENCY EXIT EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD REF AMM 33-51-06.SDR CALA2025102010315Bracket · looseR1 DOOR GIRT BAR BRACKETS LOOSE SEC. GIRT BAR BRACKETS. OPS NORMAL.SDR CALA2025102010272Lavatory · odorLAV E DOOR INSIDE DOOR NEEDS CLEANED FOUL SMELL LAV E WAS CLEANED BY CLEANERS NO MORE SMELL OK FOR SERVICESDR CALA2025102010268Potable Water · contaminatedDRAIN AND REFILL THE POTABLE WATER SYSTEMS WITH FRESH WATER PER THE GMM COFFEE HAS CHEMICAL TAST E AND SMELL. REMADE COFF EE SAME RESULT . SUSPECT WATER TANK NEEDS FLUSH DRAIN AND REFILLED POTABLE WATER SYSTEM,SDR CALA2025102010265Oven · dirtyOVEN 205 SMELLS LIKE ROTTEN FISH. CLEANED OVEN OK TO CONTINUE.SDR CALA2025102010261Unknown · odorON TAKEOFF, BURNING LUBRICANT SMELL. WAS NOT DURING TAXI/GROUND IDLE DEBRIEFED CREW. SMELL DISSAPTED SHORTLY AFTER TAKEOFF. FIRST FLIGHT AFTER #1 ENGINE WATER WASH COMPLETED OVERNIGHT. DEBRIEFED CREW. CREW STATED SMELL DISSIPATED VERY SHORTLY AFTER TAKEOFF ASDR CALA2025102010255Unknown · stainedLARGE BLACK STREAKS ON UNDERSIDE OF AIRCRAFT, STREAKS ARE TACKY TO TOUCH AND HAVE NO NOTICABLE ODOR OR COLOR OF ANY AIRCRAFT FLUIDS. APPEAR TO ORIGINATE FROM WHEEL WELL AREA. OPERATED BOTH HYD. ACMP, FOUND NO ACTIVE LEAKS, DRIPS, PUDDLES, OR POOLING. HYD. SSDR CALA2025102710554Bracket · crackedFITTING BROKEN BEHIND OF ACCESS PANEL 334NB, LT ELEVATOR. REPLACED BRACKET AT LT HORIZONTAL STABILIZER BEHIND PANEL 344NB IAW SRM 51-40-02-0G-0 & SRM 51-40-05-0G-0, DWG 183A7200-5 & DWG 183A7000. REPLACED BRACKET AT LT HORIZONTAL STABILIZER BEHIND PANEL 34SDR CALA2025102710552Skin · delaminatedLEFT WING OTBD AFT FLAP DISBOND AREA L=9INCH, W=7INCH AT LOWER SKIN TRAILING EDGE OF THE O/B AFT FLAP WEDGE. CLEANED, PREPPED, PERFORMED THE PERMANENT REPAIR AND RESTORED PAINT ON LT WING OTBD AFT FLAP OWER SKIN. ALL WORK DONE IAW SRM 57-53-01-1A-4, SRM 57-5SDR CALA2025102310431Fitting · crackedNR 1 PYLON AFT TRAILING EDGE FAIRING O/B FITTING CRACKED. REMOVED AND REPLACED NR 1 PYLON T/E FAIRING IAW SRM 51-40-02 AND DWG 313A2700 REV-.SDR CALA2025102110336Fitting · damagedEA-3271-01017-001 TAIL SKID ASSEMBLY SUPPORT FITTING REPLACEMENT UNDER WORK INSTRUCTIONS STEP 7 (B)(4) PRE-EXISTING HOLE AT .250. COMPLETED ALL STEPS PER UAL ECRA 5380-01430 REV- FOR REPAIR.SDR CALA2025102110331Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1673 FAILS OPERATIONAL CHECK. REMOVED AND REPLACED WITH NEW EMERGENCY LIGHTS BATTERY PACK M1673, INSTALLATION TEST GOOD IAW B737 AMM 33-51-06-960-805.SDR CALA2025102710550Stop Fitting · gougedAFT ENTRY DOOR (L2) UPPER STOP FITTING HAS GOUGE. REMOVED AND REPLACED L-2 DOOR UPPER FWD STOP FITTING IAW DWG 147A6125 REV- AND SRM 51-40-02-0G-0.SDR CALA2025102110325Fairing · crackedNUMBER 2 ENGINE AFT STRUT FAIRING POSSIBLE ON THE AFT BRACKET. REMOVED AND INSTALLED NR 2 ENGINE AFT STRUT FAIRING IAW SRM-51-40-02-0G-0, SRM 51-040-05-0G-0, SRM 51-40-08-0G-0, AIPC-54-52-04-02 ITEM 85, AMM 54-52-04-410-802.SDR CALA2025101710225Panel · dentedRIGHT WING INBOARD FLAP PANEL 653BB DENTED. REMOVED AND INSTALLED RT INBD FLAP PANEL 653BB IAW SRM 51-40-02-0G-0, DWG 654A0004-832 REV A.SDR CALA2025101710212Unknown · odorAROUND THE EXIT ROWS THERE IS A WEIRD SMELL. LIKE BURNING WIRES OR PLASTIC FAINT ODOR, NOT CONTINUOUS, FORWARD AND AFT OF OVERWING EXIT. UNABLE TO DETERMINE EXACT LOCATION LEFT OR RIGHT OF AISLE NOR ABOVE OR BELOW. NO OBVIOUS DEFECT NOTED. OK TO CONTINUE
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