N33286
Service difficulty reports · 77
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 = 'N33286' 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 = 'N33286' 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 CALA2026010812805Rib · crackedRT HORIZONTAL STAB RIB HSS 92.7 HORIZONTAL FLANGE AT STIFFENER NR 2 CRACKED. INSTALLED REPAIR AT RT HORIZONTAL STAB RIB HSS 92.7 STIFFENER NR 2 IAW SRM 55-10-09-2R-5.SDR CALA2026010612703Skin · dentedREPLACE FWD CARGO DOOR EXTERNAL SKIN, REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN PER SRM 51-40-02-0G-0 AND DWG#143A6110.SDR CALA2026010612702Skin · dentedREPLACE AFT CARGO DOOR EXTERNAL SKIN. REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN PER SRM 51-40-02-0G-0 AND DWG#143A6110.SDR CALA2026010712746Channel · corrodedFWD CARGO LEFT ZEE CHANNEL WAS CORRODED, BS 500A - 500I. R & R FWD CARGO LEFT ZEE CHANNEL IAW SRM 51-40-02-0G-0, AND DWG 143A7500.SDR CALA2026010612700Channel · corrodedFWD CARGO RIGHT ZEE CHANNEL IS CORRODED FROM BS 500A TO 500I AT NUT PLATE HOLES AND OTHER AREAS. REMOVED AND REPLACED FWD CARGO RH ZEE CHANNEL FROM 500A TO 500I PER SRM 51-40-02-0G-0 AND DWG#143A7500SDR CALA2025122912482Pressure Deck · dentedFLIGHT DECK FLOOR DENTED AT BS 257, BL 0 TO LBL 12. REPAIRED FLIGHT DECK FLOOR WEB AT BS 257, RBL 6 TO LBL17 IAW 53-10-51-2R-2 ,SRM 51-40-02-0G-0.SDR CALA2026011312916Floorbeam · corrodedCABIN FLOORBEAM STA 380 RBL 5 WITH CORROSION AREA. REMOVED CORROSION ON FLOORBEAM BS 380, LBL2 AND RBL 5 & INSTALLED REPAIR IAW EC/RA #5330-07672, REV. ORIGINAL.SDR CALA2026011312915Stub Frame · crackedCRACK FOUND AT FWD GALLEY DOOR STUB FRAME INTERNAL ABOVE SEAL DEPRESSOR. CRACK LENGTH ; 1". (REF AAR 99981339) REMOVED AND REPLACED R1 GALLEY DOOR CUTOUT FWD UPPER CORNER STUB FRAME REF. USED B737-800 SRM 51-40-02-0G-0 AND DRW 141A8370. REMOVED AND REPLACED SDR CALA2025121912253Floorbeam · crackedCABIN FLOOR BEAM CRACKED AT BS 540, RBL 1. R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0.SDR CALA2025121712179Door Frame · corrodedL2 CUTOUT STRUCTURE INNER CHORD STA 947.5-967.5 UPPER SURFACE WITH SEVERAL CORROSION AREAS. FOUND CORROSION OUT OF LIMITS, INNER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWG 147A8501. REMOVED AND REPLACED L2 DOOR INNER CHORD REF. SRM 51-40-02-SDR CALA2025121512117Door Frame · corrodedR2 CUTOUT STRUCTURE INNER CHORD STA 947.5-986.5 UPPER SURFACE WITH SEVERAL CORROSION AREAS. R2 DOOR CUTOUT STRUCTURE INNER CHORD FOUND CORROSION OUT OF LIMITS, INNER CHORD WAS REMOVED AND REPLACED AS PER REF. SRM 51-40-02-0G-0 AND DWG #147A8501. REMOVED ANDSDR CALA2025121512090Floorbeam · corrodedCABIN FLOORBEAM STA 947.5 LBL 51 UPPER SURFACE WITH CORROSION AREA AROUND HARD POINT. INSTALLED REPAIR AT STA 947.5 LBL26 TO LBL50" REF B737-800 SRM 53-70-51-2R-5, AND AAR ESR-WI #2024007-7-13298 REV IR, AND UNITED EC/RA 5370-01209, REV ORIGINAL. INSTALLED RESDR CALA2025121512088Floorbeam · corrodedCABIN FLOORBEAM STA 947.5 RBL 50 UPPER SURFACE WITH CORROSION AREA AROUND HARD POINT. CABIN FLOOR BEAM STA 947.5 RBL 50 UPPER SURFACE FOUND CORROSION OUT OF LIMITS REPAIRED IAW B737 SRM 53-70-51-2R-5 AND SRM 51-40-02-0G-0. INSTALLED REPAIR ON CABIN TRANSVERSSDR CALA2025121212060Floor Support · scratchedCABIN FLOOR SUPPORT BS 907-927 RBL 51, UPPER SURFACE WITH SCRATCHED. AREA AROUND HARD POINT. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN BS 907 TO 927, RBL 51, IAW SRM 51-40-02-0G-0.SDR CALA2026090119135Bulkhead Web · crackedVERTICAL PRESSURE WEB CRACKED BTWN LBL 31.53 & 40. REPAIRED AREA IAW SRM 57-10-10-2R-3, & SRM 51-40-02-0G-0.SDR CALA2025121011982Floorbeam · corrodedCABIN FLOORBEAM, BS 328, RBL 38 UPPER SURFACE CORRODED. FLOORBEAM BS 328 EXISTING REPAIR TEE ANGLE BETWEEN LBL 6 & RBL 63 FOUND OUT OF LIMITS ,TEE ANGLE WAS REMOVED AND REPLACED IAW 51-40-02-0G-0, AND DWG 141A5720.SDR CALA2025121011980Floor Support · crackedCABIN FLOOR SUPPORT,BS 500I - 520, BL 0 STABILIZER ASSY UPPER ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DWG 143A5400.SDR CALA2025120811907Floor Support · crackedCABIN FLOOR INTERCOSTAL BS 344-360, LBL 11 UPPER SURFACE CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400.SDR CALA2025120811905Floor Support · crackedCABIN FLOOR INTERCOSTAL BS 344 - 360, BL 0 UPPER SURFACE CRACKED AREA. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A5400.SDR CALA2025120811885Angle · crackedCABIN FLOOR SUPPORT BS 380 +3, RBL 10 STABILIZER ASSY UPPER ANGLE CORRODED. REMOVED AND REPLACED UPPER ANGLE IAW SRM 51-40-02-0G-0 AND DWG 143A5410.SDR CALA2025120811879Angle · crackedCABIN FLOOR SUPPORT BS 380 - 400, BL 0 STABILIZER ASSY UPPER ANGLE CRACKED. REMOVED AND REPLACED UPPER ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5410.SDR CALA2025120811877Angle · crackedCABIN FLOOR SUPPORT BS 380-400, LBL 13 STABILIZER ASSY UPPER ANGLE CRACKED. REMOVED AND REPLACED THE UPPER CHORD IAW SRM 51-40-02-0G-0 AND DWG 143A5410.SDR CALA2025092309169Connector · disconnectedEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. 21A SIDEWALL EMERGENCY LIGHT INOPERATIVE. EMERGENCY LIGHT FUNCTION OF 21A SIDEWALL LT INOPERATIVE. FOUND CONNECTOR BEHIND LIGHT ASSY DISCONNECTED. CONNECTED LIGHT ASSY. OPS CK OF SIDEWALL AND EMER LT GOOD REF AMSDR CALA2025060905395Hose · kinkedFROM CAPTAIN: HYDRAULIC SYSTEM "B" TOTAL QTY LOSS (0), PRESSURE 60. BRAIDED LINE FROM THE BOTTOM OF THE R HYDR ACCOUSTIC FILTER IS THE LEAK. FOLLOWING FIM 29-10 TASK 811. (SYS B HYD PRESSURE BELOW 2800PSI). FOUND HOSE AS116-08-0294 LEAKING WITH SHARP BEND. NOSDR CALA2025050604496Life Raft · expiredINFLATABLE LIFE RAFT INSPECTION {B737-25-3-1065} - AFT CABIN FWD LIFE RAFT OVERHAUL DUE WITHIN 150 DAYS. (JULY 2025). P/N 64356-101. M/E# 58-2581-9-0001. S/N M11034. W/C# 29-2564-1-2104. REQUEST DIP FOR AFT CABIN FWD LIFE RAFT OVERHAUL DUE DATE WITHIN 150 DAYSSDR CALA2025012101956Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1694 FAILED CAPACITY CHECK.....EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REMOVED AND REPLACED BATTERY PACK M1694 IAW 33-51-06-960-805. OPS CK GOOD.SDR CALA2025011601919Life Raft · expiredINFLATABLE LIFE RAFT INSPECTION {B737-25-3-1065} - FWD CABIN LIFE RAFT OVHL DUE DATE JAN 2025 REMOVED AND REPLACED FWD CABIN LIFE RAFT REF AMM 25-64-00.PARTS USED: 58-2581-9-0001, QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1392371 SN OFF 545RAFT, 56 PERSDR CALA2024122201614Unknown · odorFISHY ODOR COMING OUT OF GALLEY 430 REPORTED BY FA. THEY COULD N OT FIND THE SOURCE GATE GOURMET REPLACED AFT GALLEY CARTS AND CONTAINERS ALSO REPLACED OVEN RACKS. NO FISHY ODERS PRESENT.SDR CALA2023122603725Floor Support · corrodedFWD WET AREA FLOOR SUPPORT STA 294.5+3 LBL 11 SHOWS EVIDENCE OF CORROSION. REF. AAR N/R:9674080SDR CALA2022111603150Fmc · faultedVNAV FAILED ON DEPARTURE WORKED FOR A SHORT TIME ON CLIMB THEN FAILED AGAIN. AND STANDBY BOTH FMC'S INFLT.TRUE AIRSPEED WAS INDICATING APPROX 100 KTS HIGHER ON FO'S PFD THEN CAPT'S, INDICATED AIRSPEED ALL THREE MATCHED, CAPT'S- FO'S INSTALLED TAT PROBE. APPLIESDR CALA2022062201555Warning Message · false indicationRTO DUE TO TAKEOFF CONFIG WARNING . ACCOMPLISHED TAKEOFF WRN BITE TEST FIM 31-51 TASK 801, T.O.W RPRT FAULTS 31-51 TASK 822. PSEU BITE PER FIM 32-09 TASK 801. NO DEFECTS NOTED. GUANCHE, MIGUEL (V915408) TECH HAS ACCOMPLISHED TAKEOFF WRN BITE TEST FIM 31-51 TASSDR CALA2021102501970None · fluctuatesFUEL QUANTITY INDICATION, FLIGHT COMPARTMENT FLUCTUATES OR IS TO O HIGH OR TOO LOW NO. 1 TANK 850 LBS LOWER THAN RIGHT AT LEVEL OFF W/CTR FUEL. TRIM NRML. FF/ F USED SAM E. TTL CONTNUED DECRE RAN FQIS BITE TEST FOUND TANK 1 DEGRAD COMPENSATOR DATA BAD. CURRENTSDR CALA2021070501034Erosion Shield · missingPDA 3 RT NLG DOOR MISSING LEADING EDGE EROSION BOOT. SEE PHOTO. PHOTO. PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 5280-01284 REV C. ISSUED DIP TO INSPECT PER PART 2 AT INTERVALS NOT TO EXCEED 7 DAYS AND PERMANENT REPAIR PER PART 3 WITHIN 30 DAYS. APPROVED TO SDR CALA2020123001414Line · damagedNUMBER 2 HYDRAULIC PUMP LOW PRESSURE FOUND ON ENGINE NR 2 HYD SUPPLY HOSE NOT CONNECTED. FOUND HOSE END BY PYLON DAMAGED. 15501-12-2014, ME 29-2913-3-0003). FOUND THREADED END THAT REMOVED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE HOSE ASSEMBLY (P/N CONNECSDR CALA2020120201317Switch · inoperativeON APPROACH KSEA LOC ON CAPT SIDE ID AND LOC INTERMITTENT AND AUTO PILOT DID NOT CAPTURE UPDATE PER CAPT: WITH A/P A ENGAGED AIRCRAFT TURNED RIGHT INSTEAD OF LEFT TO CAPTURE THE LOCALIZER. LOCALIZER INDICATION ALSO INTERMITTENT ON CAPT SIDE. F/O SIDE WORKS GSDR CALA2020022980509Floorbeam · corrodedFWD WET AREA STA 328 FLOOR BEAM "T" CAP HAS CORROSION AT RBL 12. REF TO PEMCO NR 2695N340 BLENDED OUT CORROSION AT STA 328 RBL 12. ORIGINAL T 0.130, ALLOWABLE LOSS 10% MAT LOSS 0.032. FOUND TO BE OUT OP LIMIT IAW B737-800 SRM 53-10-51. REPLACED T CAP FROM RLBSDR CALA2020022400462Skin · crackedDURING C-SCAN INSPECTION, CRACK WAS FOUND ON R/H HORIZONTAL, 50" AT 24" TO 24.5" AFT OF FROT SPAR ON I/B SIDE OF RIB AT STA-138.7 0. VERIFIED BY HFEC. REF TO PEMCO NR 2695N442 REPAIRED LOWER SKIN ON R/H HORIZONTAL .50 AT 24" TO 24.5'' AFT OF FRONT SPAR ON I/B SDR CALA2020020800360Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, LBL 15 CRACKED. REF TO PEMCO NR 295N482. REMOVED AND REPLACED OVER WINGBOX STA 540 LBL 15 SHEAR FITTING IAW B737-800 SRM 51-40-02.SDR CALA2020020800361Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, RBL 6.5 CRACKED. REF TO PEMCO NR 2695N480 REMOVED AND REPLACED OVER WINGBOX STA 540 RBL 6.5 SHEAR FITTING IAW B737-800 SRM 51-40-02.SDR CALA2020020800356Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, LBL 40.87 CRACKED. REF TO PEMCO NR 2695N486 REMOVED AND REPLACED OVER WINGBOX STA 540 LBL 40.87 SHEAR FITTING IAW B737-800 SRM 51-40-02. WORKED BY V928513/722394. INSPECTED BY Q948. ENTERED BY V927862. REMOVED AND REPLACESDR CALA2020020800355Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, LBL 6.5 CRACKED. REF TO PEMCO NR 2695N479 REMOVED AND REPLACED OVERWING BOX STA 540 LBL 6.5 SHEAR FITTING IAW B737-800 SRM 51-40-02.SDR CALA2020020800362Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, RBL 15 CRACKED. REF TO PEMCO NR 2695N481. REMOVED AND REPLACED OVER WNG BOX STA 540 RBL 15. SHEAS FITTING IAW B737-800 SRM 51-40-02.SDR CALA2020020800359Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, LBL 32.5 CRACKED. REF TO PEMCO NR 2695N483. REMOVED AND REPLACED OVER WING BOX STA 540 LBL 32.5 SHEAR FITTIN G. IAW B737-800 SRM 51-40-02.SDR CALA2020020800358Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, RBL 32.5 CRACKED. REF TO PEMCO NR 2695N484. REMOVED AND REPLACED OVERWING BOX STA 540 RBL 32.5 SHEAR FITTING IAW B737-800 SRM 51-40-02.SDR CALA2020020800357Fitting · crackedOVER WINGBOX SHEAR FITTING AT STA 540, RBL 40.87 CRACKED. REF TO PEMCO NR 2695N485. REMOVED AND REPLACED OVER WINGBOX STA 540 RBL 40.87 SHEAR FITTING IAW B737-800 SRM 51-40-02.SDR CALA2019062201023Lamp · inoperativeAFT INTERIOR EMERGENCY INCANDESCENT LIGHT AT AFT LH OVERWING EXIT INOP. RELAMPED, CKS GOOD.SDR CALA2019062201021Lamp · inoperativeAFT INTERIOR EMERGENCY INCANDESCENT LIGHT AT AFT RH OVERWING EXIT INOP. RELAMPED, CKS GOOD.SDR CALA2019062201020Light · inoperativeBOTH INTERIOR EMERGENCY EVAC INCANDESCENT LIGHTS AT RH FWD OVERWING EXIT INOP. RELAMPED, CKS GOOD.SDR CALA2019062201022Light · inoperativeEMERGENCY EVAC LIGHT AT SEAT 8C IS INOP. RELAMPED OVERWING EXIT EEL LIGHT, CKS GOOD.SDR CALA2019042200631Valve · leakingAFTER TAKEOFF FUEL LEAK FROM RIGHT VENT. FUEL WILL NOT REMAIN BA LANCED CREW REPORTED FUEL LEAK STOPPED WHEN CTR TANK PUMPS ARE OFF ACCESSED AND CK FLOAT VALVES. NO DISCREPANCIES FOUND. REMOVED AN NANCE CW STS AVIATION. V916738. D REPLACED #2 SPAR VLV BODY. R
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