N35204
Service difficulty reports · 94
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N35204' AND registry_match = 'registration' 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 n_number = 'N35204' AND registry_match = 'registration' 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 CALA2026033014916Pitot Tube · faultedFEEL DIFF PRESS LIGHT ON AFTER TAKEOFF FULL NOSE UP TRIM FOR LA NDING REF FIM 27-31 TASK 815. FLUSHED OUT R/H ELEV PITOT. NO CLOGS NOTED. L/H PITOT HAS OBSTRUCTION. REMOVED ELEVATOR PITOT PROBE REF AMM 27-31-94-000-801. CONDUCTED ELEVATOR PITOT STATIC FLUSHISDR CALA2025110710985Slide · unpackedF/A REPORTS DOOR 1R HAS EXCESS SLIDE MATERIAL LOOSE. REMOVED AND REPACKED Z FOLD ON DOOR 1R ESCAPE SLIDE AND REINSTALLED DOOR 1R ESCAPE SLIDE IN REF TO AMM 25-66-01, NO FURTHER DEFECTS AT THIS TIME VERIFIED INSTALL OF DOOR SLIDE 1R RII REF GMM 09-25-05.SDR CALA2025081407761Structure · no discrepancyPERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03385 ON OR BEFORE 29-JULY-2027 REF LP 5753762 FOR INTERIM REPAIR.SDR CALA2025080407235Stub Beam · damagedSTA 616 LH STUB BEAM HAS AN ELONGATED HOLE. REPAIRED BS616 L/H STUB BEAM AS REQ IAW REO-G25531 REV IR AND ECRA NO. 5311-03385 REV-.SDR CALA2025081407754Skin · corrodedAFT PIT LT SIDE, FUSELAGE SKIN CORRODED AROUND THE LAVATORY EXHAUST VENT ATTACHMENT BETWEEN BS 907 AND BS 927 AND BETWEEN STRINGERS S19L AND S22L. ACCOMPLISHEDD INTERIM REPAIR OF THE AFT PIT LT SIDE, FUSE SKIN IAW ECRA 5370-01182 PT1.SDR CALA2025071406498Skin · crackedR-2 DOOR, INNER UPPER SKIN, UPPER CENTER LIGHTENING HOLE IS CRACKED. REPAIRED R-2 DOOR INNER UPPER SKIN REFERENCE UNITED EC/RA# 5210-03403.SDR CALA2025070906383Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION AT STA 294, RBL 53. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER ECRA 5321-01330 REV H. ORIGINAL MAT .094, REMOVED .017, REMAINING .077. INSTALLED NEW CREASE BEAM IAW SRM 51-SDR CALA2025071706651Floorbeam · corrodedAFT WET AREA RT FLOORBEAM BS 947 HAS SURFACE CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-70-51-1A-1. REMOVED AND T-ANGLE REPAIR PER B737-800 SRM 51-40-02. REFABRICATED AND REPLACED T-ANGLE REPAIR PER B737-800 SRM 53-70-51-2R-5.SDR CALA2025071706650Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION FROM BS 294-348, LBL60. REMOVED CORROSION IAW B737-800 SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A, ORIGINAL THICKNESS .125" REMOVED .045", REMAINING .080". REMOVED AND RSDR CALA2025071706649Stop Fitting · worn(SUPPORT TASK) L-2 DOOR, UPPER FWD DOOR STOP FITTING IS GOUGED. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW SRM 52-10- 90-1A-1. REMOVED AND REPLACED UPPER FWD STOP FITTING PN#147A6128 U53 IAW SRM 51-40-02 AND DWG 147A6125 REVB. RESTORED SURFACE PROTECTION ISDR CALA2025070106106Crease Beam · corrodedAFT WET AREA RH DOOR CREASE BEAM HAS MULTIOPLE SPOTS OF CORROSION. REMOVED CORROSION ORG THICKNESS .180 REMOVED .105 REMAINING .075 AND FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A AND SRM 53-70-15-1A-1. REMOVED CREASE BEAM PER B737-800 SRM 51-40-02. SDR CALA2025070106105Floor Support · corrodedMAIN CABIN STA 946 RBL 50 SUPPORT HAS CORROSION, WITH 100% MATERIAL LOSS ON UPPER SURFACE. REMOVED AND REPLACED INTERCOSTAL AT ST STA.949 - STA 967 RBL50 PER B737-800 SRM 51-40-02 AND BAC DWG 147A5762SDR CALA2025071506571Service Panel · corroded(SUPPORT TASK) AFT CARGO COMPARTMENT,WASTE SERVICE PAN HAS CORROSION.SDR CALA2025062706002Web · corrodedAFT CARGO COMPARTMENT, SILL PLATE INNER WEB HAS EXFOLIATED CORROSION. REMOVED AND REPLACED AFT CARGO COMP SILL PLATE, LOCATED AND DRILLED, IAW B737-800 SRM 51-40-02, 51-40-05.SDR CALA2025062305813Floor Support · cracked(B737-53-3-0737) MAIN CABIN FWD WET AREA, MACHINED INTERCOSTAL FROM STA 344-360 BL 0 HAS 2EA POSSIBLE CRACKS IN UPPER FLANGE AT FLOOR PANEL ATTACH HOLES. REMOVED AND REPLACED MACHINED INTERCOSTAL IAW DWG NO. 141A540010 REV B AND SRM 51-40-02.SDR CALA2024080800390Pump · malfunctionedCENTER TANK LEFT FUEL PUMP INOP. CENTER TANK RIGHT BOOST PUMP ON MEL 2802D ON LOG PAGE 8819950. PLACING BOTH CENTER FUEL TANK BOOST PUMPS ON MEL 2802E. LOG PAGE 8819950 CLEARED. CENTER FUEL TANK QTY 4.75. T/S PER FIM 28-22 TASK 822-C1. FOUND STATUS CODE 2 ONSDR CALA2024042201187Web · damagedE & E BAY WEB BS 323.7 TO 351.2 DAMAGED.SDR CALA2024042201151Angle · crackedE&E COMPARTMENT DOOR CUTOUT FRAME/WEB, LH SIDE FWD CORNER EXTRUSION ANGLE IS CRACKED L/P IS FOR ESFR PURPOSES SEE NR 1952113 ESFR CREATED ESFR # 1035845SDR CALA2024040200924Panel · missingNR 1 ENGINE PYLON PANEL HEAT SHIELD COATING MISSING FROM LOWER SECTION OF PANEL - APPROXIMATLY 10 SQ INCHES. REMOVED ENG 1 INBD AFT PYLON ACEESS PANEL FOR MX AT IAH. INSTALLED #1 ENGINE INBOARD PYLON PANEL REF AMM 54-53-01.SDR CALA2023021000383Door · missingPDA 3 RIGHT NLG DOOR LEADING EDGE EROSION BOOT MISSING -- SEE PHOTO PHOTO ADDED IF NEEDED ECRA 5280-01284 REV-B IS AVAILABLE FOR DEFERRAL.... PARTS ADDED TO LOG .. REF IPC 32-22-11-05 ITEM 275 PARTS USED: 00-0609-3-7367,QTY :1 29-3222-3-0008,QTY :1 REPLACED SDR CALA2023011000081Position Sensor · inoperativeNOSE GEAR INDICATES DOWN AFTER T/O. QRH DONE. DIVERTING TO IAH. REMOVED AND REPLACED NOSE LANDING GEAR DOWN POSITION SENSOR S853. OPS CHECK NORMAL.SDR CALA2022092102423Skin · crackedC-SCAN CRACK INDICATIONB LH HORIZONTAL STABILIZER APPROX STA 117, 10.5" FROM AFT SPAR. TRANSCRIBED FROM AERSALE NRC 23739 EMP STAMP# ALD011. INITIAL DVI AND LFEC EVERY 9,00 FLT CYC THEREAFTER IAW SRM 55-10-01, INSPECTION THRESHOLD AT 56,00 TOTAL FLT CYC AND THSDR CALA2022081602071Handle · looseDOOR 1L ASSIST HANDLE LOOSE.TIGHTEN THE HANDLE OK TO USE.SDR CALA2022072701884Harness · damagedFOUND DANAGED EPL HARNESS P/N BR9635-30-24 THAT RUNS FROM SEAT ROW 34ABC TO 36ABC. SUPPORT TASK GOOD IAW B737-800 AMM 25-22-00-710-027 REMOVED THE DAMAGED SECTION OF WIRES AND SPLICED WIRES IAW SWPM 20-30-12 AT STA 792 BETWEEN SEAT ROWS 34ABC & 35ABC. OPS CKD SDR CALA2022072701899Harness · chafedEPL WIRING BETWEEN SEAT ROWS 34 & 35 ABC IS DAMAGED CAUSING THE AFT CABIN EMERGENCY LIGHTS TO APPEAR WEAK. (REF. N/R 000149). SUPPORT TASK NSA EMX N/R 00153. REPAIRED DAMAGED EEPL SEAT TO SEAT CABLE WITH 2 EA SPLICES AT REPORT, FORM 46-0024, ENTERED BY UAL INSSDR CALA2022072701896Power Supply · inoperativeAFT CABIN SEATS EMERGENCY LIGHT BATTERY PACK IS WEAK. SUPPORT TASK NSA EMX N/R 00149. TROUBLESHOT AND FOUND BAD EMERGENCY POWER SUPPLY AT STA 952 LEFT 00153. PERFORMED THE EMERGENCY ESCAPE PATH LIGHTING OPERATIONAL ENTERED BY UAL INSPECTION U354653, DATE 26JUSDR CALA2022072001838Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRAC KED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 0SDR CALA2022072001837Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRAC KED REMOVED AND REPLACED SHEAR FITTING AT STATION 54-0 AND LBL 6.14 INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00113 AND HANGER N/R 5867202 SDR CALA2022072001836Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/RSDR CALA2022072001835Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRA CKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 40.87 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U301243 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL DATA WAS DASDR CALA2022072001834Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 LBL32.40 IS CRACKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 ACCOMPLISHED BY V905004, AND INSPECTED BY 932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00115 SDR CALA2022072001833Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/RSDR CALA2022072001832Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRA CKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 AND SSFR REPORT, FORM 46-0024,ENTERD BY UAL INSPECTION U301243, RBL 54.60 IAW B737-800. SRM 51-40-02 AND DWG NO. 111A2000. 7-15-2022 REVSDR CALA2022072001831Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAS DWG 111A2000 REV ORIGINAL SEE NSA EMX N/RSDR CALA2022072001830Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/RSDR CALA2022072001814Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRA CKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 ACCOMPLISHED BY V905004, AND INSPECTED BY V932009. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/RSDR CALA2022071801777Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKEDSDR CALA2022071801776Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKEDSDR CALA2022071801775Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKEDSDR CALA2022071801782Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKEDSDR CALA2022071801781Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKEDSDR CALA2022071801779Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKEDSDR CALA2022071801778Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKEDSDR CALA2022071501756Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 LBL32.40 IS CRACKEDSDR CALA2022071501755Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRA CKEDSDR CALA2022071501753Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKEDSDR CALA2022040800929Tire · damagedPDA 1 REFERENCE #3 TIRE CAME APART WHICH CLASSIFIES AS A PDA EVENT REMOVED AND REPLACED #3 MLG TIRE FOR TREAD LOSS INSPECTION COMPLETION.#3 TIRE WAS REPLACEDSDR CALA2022040800920Tire · damagedFOUND ON ARRIVIAL TO GATE,RH MLG,INBD TIRE SHREDDED,FLAT, AND MISSING INBD PLIES. REMOVED AND REPLACED #3 MLG TIRE IAW AMM 32-45-11-400-801. REF LOG PAGE 8337559 FOR TREAD LOSS INSPECTION COMPLETION. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1987286 SN OFF 03SDR CALA2022040600895None · missingPDA 3 LEFT WING #2 SLAT HAS ONE FASTENER HEAD BROKEN OFF/MISSING AND ANOTHER LOOSE AT ACTUATOR ATTACH POINT -- SEE PHOTO PHOTO ADDED PHOTO ADDED PHOTO ADDED UPDATE -- ONE FASTENER MISSING AND 3 FASTENERS LOOSE -- SEE PHOTO INSTALLED MISSING HI LOCK AND TIGHTENSDR CALA2021101101848None · contaminated*EMERGENCY DECLARED* LOSS OF SYS A HYD QTY FOLLOWED BY LOSS OF SYS A PRESSURE INFLIG HT RUN THRU. AN ADDITIONAL 30 SECONDS TO 1 MINUTE ELAPSED BEFORE EMDP SELECTED OFF. DEBRIEF OF F/O. HE STATED THAT AT CRUISE THE MASTER CAUTION CAME MATL AND LABOR UPDATED ON
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