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 CALA2026043015864Lens · cracked4B BOTH EPL LIGHT LENS CRACKED. REQUEST TO DEFER EPL'S ARE FULLY OPERATIONAL. REMOVED AND REPLACED 4B BOTH EPL LIGHT LENS WITH A NEW ONE AS PER 33-51-11SDR CALA2026043015862Lens · cracked24,25,26,28,29,30,31,34,35,36,37 AND 38C EPL LIGHT LENS CRACKED. REQUEST TO DEFER, EPL'S ARE FULLY OPERATIONAL. TOMC OK TOMC APPROVED ITEM DEFERRED. CHANGE SFR TO NO REMOVED AND REPLACED LIGHT LENS ON SEATS 24,25,26,28,29,30,31,34,35,36,37, AND 38C PER AMM 32SDR CALA2026042915837Floor Support · crackedLEFT UPPER CENTER WING BS 540 FLOORBEAM HAS CRACKS AND BENT. REMOVED AND REPLACEDF LT FLOORBEAM BS 540 IAW SRM 51-40-02 AND DWG 143A5240, REV-.SDR CALA2026042915835Floorbeam · crackedRIGHT UPPER CENTER WING STA-540 FLOOR SUPPORT STRUCTURE CROSSBEAM HAS CRACKS AND BENT. REMOVED AND REPLACED RT FLOOR SUPOORT BS 540 SRM 51-40-02 AND DWG 143A5240 REV:- .SDR CALA2026042915825Skin · crackedONE CRACK SIGNAL NOTED AT HORIZONTAL STAB LOWER SKIN PANEL RT SIDE, HSS 138.70 INBD SIDE L=1 INCH LOCATED TO 16.400 INCH AFTER FROM FWD SPAR. INSTALLED NEW REPAIR PARTS ON LOWER SKIN PANEL IAW SRM 51-40-02-0G-0. REMOVED PREVIOUS REPAIR PARTS AT HORIZONTAL STASDR CALA2026042815783Shield · corrodedFWD CARGO SHIELD WITH CORROSION. REMOVED FWD CARGO SHIELD, LOCATED AND DRILL NEW SHIELD, INSTALLED FWD CARGO SHIELD IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, DWG 143A8126, REV G,SDR CALA2026042815775Battery Pack · inoperativeLEFT AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-06-960-805, OPS CHECKED GOODSDR CALA2026042815764Unknown · odorPILOT REPORTED SLIGHT OIL ODOR WITH APU SUPPLYING BLEED PRESSURE FOR PACKS ON TAXI IN. SMELL DISSAPATED QUICKLY AFTER ARRIVAL AT GATE. FLIGHT CREW REPORTED NO ODORS DURING ANY PHASE OF PREVIOUS FLIGHT. INSPECTED APU BLEED DUCT FOR EVIDENCE OF OIL LEAKAGE. NO ESDR CALA2026060116719Panel · corrodedFUSELAGE LEFT SIDE FWD RAM AIR DOOR HAS SIGN S OF CORROSION ON THE INNER STIFFNER CHANNEL. ALL WORK ACCOMPLISHED ON AAR GSO NON-ROUTINE 9289072. REMOVED AND REPLACED FWD MODULATION PANEL PER AMM 21-51-23.SDR CALA2026042815771Floorbeam · corrodedAFT WET AREA FLOORBEAM UPPER TEE UPPER SURFACE STA 986.5 WITH CORROSION SPOTS LBL 26 - 44. REF NR 100024966 AT AFT WET AREA FLOORBEAM STA 986.5" FROM LBL 50" TO RBL 50". ACCOMPLISHED REPAIR OF THE UPPER TEE SECTION OF THE FLOORBEAM STA 986.5" FROM LBL 50" TO SDR CALA2026042815769Seat Track · corrodedAFT WET AREA; POSSIBLE CORROSION ON SEAT TRACK BTW STA 927 TO 907, RBL 44 AND RBL 24.75. REMOVED AND INSTALLED 2 EA NEW SEAT TRACK BTW STA 927 TO 907, RBL 44 AND RBL24.75 AT AFT WET AREA IAW SRM 51-40-02-0G-0.SDR CALA2026052916614Stub Beam · gougedR2 DOOR UPPER STUB BEAM HAS LIGHT SCRATCHES. REMOVED DAMAGE, ORIGINAL THICKNESS .060, REMOVED .026, REMAINING IS .034, FOUND OUT OF LIMITS IAW SRM 52-10-02-1A-4 DETAIL E. REMOVED AND REPLACED STUB BEAM IAW DWG 147A6149 REV E AND 147A6502 REV F.SDR CALA2026042915823Stub Beam · gougedR2 DOOR LOWER STUB BEAM GOUGED. ALL WORK PERFORMED ON AAR GSO NON-ROUTINE 9288443. REMOVED DAMAGE, ORIGINAL THICKNESS .060, REMOVED .025, REMAINING .035. OUT OF LIMITS IAW SRM 52-10-02-1A-4 DETAIL E. REMOVED AND REPLACED STUB BEAM 147A6149-6 IAW DWG 147A6149.SDR CALA2026042915821Skin · gougedR2 DOOR INNER SKIN LOWER HINGE CUTOUT HAS A DEEP SCRATCH AND BARE METAL. TALL WORKED PERFORMED ON AAR GSO NON-ROUTINE 9288623. FABRICATION OF NEW INNER SKIN IAW DWG 147A6152. REMOVED AND REPLACED LWR INNER SKIN PN# 147A6152-6 IAW DWG 147A6502 REV F.SDR CALA2026042815751Seat Track · corrodedCORROSION ON LH OB PAX SEAT TRACK BETWEEN BS 360 AND 380. REMOVED CORROSION, EVALUATED, REMOVED, LOCATED NEW PART AND DRILLED HOLES AND INSTALED LT SEAT TRACK BETWEEN BS 360 AND 480 IAW SRM 51-10-02-0G-0, SRM 53-00-52-1A FIG A-A, SRM 51-40-02-0G-0, STEP 7SDR CALA2026042415702Release Mech · brokenFWD DOOR SLIDE GIRT BAR STOP RELEASE BROKEN. L1 DOOR. PART AOG. REMOVED AND REPLACED GIRT BAR STOP IAW IPC 25-66-00-13.SDR CALA2026042815747Support Frame · gougedLEFT-SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA727 JUST ABOVE FLAP TRACK #4 HAS A DEEP GOUGE. REPAIRED SUPPORT FRAME LOCATED AT L/H WING TO BODY FAIRING STA 727 AS PER AAR WORK INSTRUCTIONS ESR 33-15106 AND EC/RA 5360-02134.SDR CALA2026042715737Computer · failedRA FLAG AND AUTOPILOT DISCONNECT. FO SIDE NOT ABLE TO USE NOSE UP TRIM.F/O STAB TRIM SWITCHES NOSE UP TRIM INOP. ACCOMPLISHED BASIC GVI OF VISIBLE CONTROL CABLES IN FWD&AFT E&E BAYS, WHEEL WELL, AND JACKSCREW COMPARTMENT, NO DEFECTS NOTED. FOUND EXCESSIVE MSDR CALA2026042715727Stiffener · crackedEA5510-01843 REV. J. CRACK. LEFT HORIZONTAL STAB STA 92,7 INBOARD SIDE OF RIB #1 HAD EVIDENCE OF CRACK AT VERTICAL STIFFINER #2 TRANSITION RADIO. REF AAR NR 100015416. REPAIRED STIFFENER NO. 2 AT L/H HORIZONTAL STAB STA 92.7 RIB #1 AS PER SRM 55-10-09-2R-5. SDR CALA2026042415720Transition Panel · corrodedFWD CARGO RIGHT SIDE TRANSITIONAL PANEL FROM STA 520-500H HAVE SIGN OF CORROSION AT MULTIPLE PLACES. REMOVED CORROSION ON FWD PIT RT TRANSITION PANEL BS 500A-500I IAW SRM 51-10-02. ORIG MAT THICKNESS .040, MATERIAL LOSS .010, MATERIAL REMAINING .030 FOUND OUSDR CALA2026042415718Bulkhead Web · crackedMACHINING PURPOSES ONLY MACHINE REPAIR MATERIAL FOR PART 1 REPAIR WEB PER SRM 57-10-10-2R-3 TABLE 202. COMPLETED MACHINED MATERIAL FOR PART 1 REPAIR WEB PER SRM 57-10-10- 2R-3 TABLE 202.SDR CALA2026042415716Floor Support · dentedFLOOR SUPPORT AT APPROX STA 273 IS BENT JUST AFT OF COCKPIT DOOR. REMOVED, REPLACED AND INSTALLED NEW INTERCOSTAL PN# 141A5214Y5 FROM BS 260 TO BS 277 LBL 12 WL 208 IAW BOEING DWG 141A5740 REV C AND 140A9810 REV- AND B737-800 SRM 51-40-04-0G-0.SDR CALA2026042415714Floorbeam · corrodedCORROSION - FWD WET AREA FLOORBEAM STA 328 AT RBL 46. INSTALLED REPAIR AT FWD WET AREA FLOORBEAM UPPER CHORD REPAIR FROM RBL-20.5 TO RBL-65 STA 328 REF SRM 51-40-02-0G-0 AND 53-10-51-2R-7,SDR CALA2026042415695Access Panel · looseEMERG DOOR ACCESS PANEL ROW 21 ABC LOOSE AND NEEDS RESTOW. RESECURED EMERGENCY EXIT DOOR ACCESS PANEL PER AMM 52-49-00. ACFT GOOD TO CONTINUE.SDR CALA2026042415680Skin Panel · crackedWHILE PERFORMING EXTERNAL CROWN INSPECTIONS FOUND NUMEROUS DISCREPANCIES IN THE EXTERNAL FUSELAGE SKIN AREA BETWEEN STA.727C & STA727F BETWEEN STR4L & STR4R. REPAIRED DISCREPANCIES IN THE EXTERNAL FUSELAGE CROWN SKIN AREA BETWEEN STA.727C & STA727F BETWEEN SSDR CALA2026042915833Stub Frame · crackedEA-5310-07694-009: FOUND 2.50 INCH CRACK ON R1 DOOR STUB FRAME DURING NDT HFEC INSPECTION. REMOVED AND REPLACED R1 STUB FRAME IAW B737-800 SRM 51-40-02 AND 51-40-05 AND BAC DWG 141A8370 REV D. ADJUSTMENT OF UPPER ROLLER LATCH PLATE ON CUSTOMER CARD 57-524SDR CALA2026042815746Frame · gougedAPU DOOR ASSY FRAME HAS A DEEP GOUGE LOCATED AFT OF THE AFT HINGE. REPAIRED APU DOOR ASSY FRAME STA 1154.60 LBL 18 AS PER EC/RA 5240-01751.SDR CALA2026042415712Floorbeam · corrodedCORROSION - AFT WET AREA FLOOR BEAM STA 947.5 UPPER T CHORD UPPER SURFACE WITH CORROSION AT RBL 50. AFT WET AREA FLOOR BEAM AT STA 947.5 RBL 50, ACCOMPLISHED REPAIR AT FLOOR BEAM AT STA 947.5 RBL 50 IN REF TO B737-800 SRM-53-70-51-2R-5, SRM 51-40-02-0G-0 & DWSDR CALA2026042415678Floor Support · corrodedAFT WET AREA FLOOR SUPPORT BS 947.5 + 3 UPPER SURFACE WITH CORROSION RBL 51. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0 & DWG 147A5760.SDR CALA2026042415676Hinge · crackedCRACKED APU DOOR ASSY INTERNAL @ APPROXIMATELY STA 1020 HINGE AREA FWD AND AFT SIDE. FABRICATED 2EA HINGE FRAME AT APU DOOR ASSY INTERNAL STA 1020 FWD AND AFT IAW DWG 148A6353-127 AND DWG 148A6353-128. INSTALLED IAW SRM 51-40-02-0G-0.SDR CALA2026042315638Support · crackedFOUND CRACK NR 1 PYLON LOWER AFT FIXED FAIRING INTERNAL AFT SUPPORT CRACKED. REMOVED AND REINSTALLED L/T AFT FAIRING IN REF B737 AMM 54-52-04-010-802 & 54-52-04-410-802. REMOVED AND REPLACED NR 1 PYLON LOWER AFT FIXED FAIRING INTERNAL AFT SUPPORT PER SRM SDR CALA2026042315632Intercostal · corrodedMAIN CABIN AFT WET AREA, INTERCOSTAL CORRODED ON UPPER SURFACE BETWEEN BS 947.5 AND 967 APPROX LBL-25 REMOVED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL REF SRM 51-40-05, DWG 147A5650 REV- AND SRM 51-40-02. REMOVED DAMAGE, ORIG .080, MATERIAL LOSS .020, RSDR CALA2026042115557Light · inoperative35C EMERGENCY PATH LIGHT OUT. REPLACED WITH FLOOR PROXIMITY LIGHT (35C) ASSY AND CHECK OK IAW AMM 33-51-11-960-802.SDR CALA2026050516020Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR , I/B ROW. CRACK LENGTH - 3/4". REPAIRED LEFT HORIZONTAL STAB LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR IAW SRM 55-10-01-2R-11.SDR CALA2026042315630Intercostal · corrodedONE INTERCOSTAL HAS CORROSION ON UPPER SURFACE INSIDE E & E COMPARTMENT FROM APPROX BS 330-344, S23L. REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02 AND BAC DWG 141A8131 REV A.SDR CALA2026042115552Door Frame · crackedRIGHT MLG CENTER DOOR FRAME CRACKED NEAR THE LOWER FORWARD ATTACH POINT. REMOVED RT MLG DOOR ASSY IAW AMM 32-13-11-000-803, REPAIR PARTS IAW SRM 52-80-02-2R-2 AND SRM 51-40-02-0G-0 .REINSTALLED RT MLG DOOR ASSY IAW AMM 32-13-11-420 -803. ACCOMPLISHED RT MLG SDR CALA2026082718972Wedge · dentedLEFT WING, NR 2 SLAT HAS A DENT ON THE UPPER SURFACE T/E WEDGE. EVALUATED 1EA DENT ON NR 2 SLAT T/E WEDGE IN UPPER SURFACE IN ZONE 3. DENT MEASURES 30.4" FROM I/B EDGE AND 4.5" FROM T/E W= 1.1", Y= .021" W/Y=47. AFTER FURTHER EVALUATION DENT FOUND TO BE WITHISDR CALA2026042315662Girt Bar · unraveledGIRT BAR DOOR 1L HARD TO LATCH IN PLACE ... FABRIC IN THE WAY REF. 25-66-01-400-804 ACCOMPLISHED ESCAPE SLIDE REPACK UNSCHEDULED. OPS NORMAL . RENDER SAFE CHECKLIST COMPLETE. VERIFIED SLIDE PIN REMOVED AND STOWED AND CORRECT INSTALLATION OF L1 DOOR SLIDE REFERSDR CALA2026042215616Bracket · loose1R GIRT BAR BRACKET IS LOOSE ADJUSTED THE GIRT BAR RETAINER CLIP ON DOOR 1R,AND VERIFIED THE GIRT BAR STAYS INSIDE THE RETAINER CLIP IN REF TO AMM 25-66-01.SDR CALA2026042215600Oven · odorOVEN 205 BEGAN TO SMOKE BEFORE COOKING FA PULLED BREAKER TO STOP THE SMOKE. OPERATED OVEN FOR 20 MINUTES, NO EVIDENCE OF SMOKE OR ODOR, INSPECTED SURROUNDINGS, NO DEFECTS NOTED.. PLACED OVEN ON NEF 2510AU PRECAUTIONARY. CREW OBSWERVED APPARENT SMOKE COMING FSDR CALA2026042115554Blower · failedWX RADAR NOT WORKING. PAINTS SOLID GREEN ACROSS THE SWEEP IN ARE AS OF KNOWN TSTRMS PERFORMED FIM 34-43 TASK 802. PER CREW BRIEF, NO FAIL MESSAGES OR OTHER FAULTS NOTED. RESET R/T CB AS PRECAUTION. OPERATIONAL CHECK OF WX RADAR NORMAL. REMOVED AND REPLACED WX SDR CALA2026052116424Support Angle · corrodedCORROSION-FWD WET AREA L-1 CUTOUT THRESHOLD I/B SUPPORT ANGLE. REMOVED AND REPLACED SUPPORT ANGLE AT L1 DOOR THRESHOLD I/B POSITION IAW SRM 51-40-02-0G-0, AND DWG 141A8110,SDR CALA2026042215592Transition Panel · corrodedFWD CARGO LEFT SIDE TRANSITIONAL PANEL FROM STA 500E-500B HAVE SIGN OF CORROSION AT MULTIPLE PLACES. TRANSCRIBED FROM AAR GSO NON-ROUTINE 9288805 ORIGINATED BY AAR GSO MECH V899802 COMPLETED ESFR AREA OF CORROSION FOUND TO BE EXFOLIATED ON FWD CARGO LH TRANSISDR CALA2026042015542Floor Support · corrodedMAIN CABIN AFT WET AREA, INTERCOSTAL CORRODED ON UPPER SURFACE BETWEEN BS 927 AND 947.5 APPROX RBL10. REMOVED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-05 AND DWG 147A5760 REV-.SDR CALA2026041715450Light · missingRED EMERGENCY EXIT GUIDANCE LIGHT AT ROW 20 IS MISSING/BROKEN. REMOVED AND REPLACED EMERGENCY GUIDENCE LIGHT. REF. AMM 33-51-00. OPS CHECK GOOD.SDR CALA2026050516018Skin · damagedAFTER FEED THRU CABLE EXTERNAL DOUBLER REMOVAL FOUND MULTIPLES ELONGATE HOLES. PERFORMED REPAIR ON EXTERNAL SKIN BTW STA 727D TO 727F AND S-1 T O S-3R ALL WORKS WERE ACCOMPLISHED IAW EO 260181 REV.P1, EO 2601 81 REV. IR AND EC/RA 5360-02128. CLASSIFIED AS A SDR CALA2026050516014Skin · crackedCRACK FOUND AT LT HORIZONTAL STAB LOWER SKIN AT STAB STA 120.30, 10" FROM REAR SPAR, I/B ROW. CRACK LENGTH 1". ESFR COMPLETED ACCOMPLISHED REPAIR AT LEFT HORIZONTAL STAB LOWER IN SPAR SKIN AT HSS 120.30 IAW SRM 55-10-01-2R-11,SDR CALA2026042415698Skin · damagedACCOMPLISH INSP ECTION REQUIREMENTS OF THE RH WING LOWER SKIN REPAIR AREA BETWEE N WSTA 564 ? 591 AT S-9L PER PART 2, TABLE 2SDR CALA2026042115550Floorbeam · corrodedAFT WET AREA POSSIBLE CORROSION ON FLOORBEAM BS 986, LBL 50. PERFORMED REPAIR ON AFT WET AREA FLOORBEAM BTW BS 986, LBL 50. DAMAGE TOLERANCE OF THE INITIAL STRUCTURE WITH THIS REPAIR INSTALLED IAW SRM 53-70-51-2R-4 2A, STEP 2A. . ALL WORK ACCOMPLISHED IAW SDR CALA2026042015538Angle · corrodedL1 DOOR CUTOUT LOWER SILL AREA,, ONE ANGLE ATTACHED TO THE INNER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN BS 328 AND BS 344. . REMOVED, LOCATED, DRILLED AND INSTALLED NEW INNER ANGLE IAW SRM 51-40-05 AND DWG 141A8112 REV-.
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