N38727
Service difficulty reports · 75
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 = 'N38727' 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 = 'N38727' 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 CALA2026070917632Light · inoperativeEMERGENCY EXIT WINDOW LIGHT INOP. AT 21F. REMOVE AND REPLACE EMERGENCY EXIT WINDOW LIGHT. AT 21F. OPS CHECK GOOD.SDR CALA2025110310838Wire · shortedL2 DOOR, EMERGENCY EXIT LIGHT SIGN DOES NOT ILLUMINATE. M1672 BATTERY PACK REMOVED AND DISCONNECTED FROM D10744. AFT GALLEY CEILING LIGHT ASSEMBLY(M01678) REMOVED AND DISCONNECTED FROM D11460. D40100P AND J DISCONNECTED. D40044 P & J DISCONNECTED. TROUBLESHOOTSDR CALA2025103110773Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK. REPLACED THE M1675 BATTERY , OPS CHKD GOOD IAW MM 33-51-06-960-805.SDR CALA2025103110772Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK. REPLACED THE M1672 BATTERY, OPS CHKD GOOD IAW MM 33-51-06-960-805.SDR CALA2025103110771Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1668 FAILED CAPACITY CHECK. REPLACED THE M1668 BATTERY, OPS CHKD GOOD IAW MM 33-51-06-960-805.SDR CALA2025100709753Skin · corrodedAFT LAV SERVICE PANEL COUTOUT AFT LOWER CORNER SKIN IS BULGING AND RIVETS PULLING THROUGH. AFT LAV SVC PNL CORROSION. PERFORMED REPAIR TO THE FUSELAGE SKIN P/N'S 146A3231-4,146A3201- 7 AND INTERNAL DOUBLER BETWEEN STA 807-887 AND S19L - S24R IAW EC/RA 5360-0SDR CALA2025091508884Window Frame · crackedFOUND DAMAGE CRACK AT THE R3 WINDOW FRAME POST HOLE 5, REF TO EA 5310-08195 REV C OP 004. (REF AAR NR 1000043323). ACCOMPLISHED REPAIR OF HOLE # 5 AT THE RH # 3 WINDOW FRAME POST IAW ECRA #:5310-08676.SDR CALA2025101510115Window Frame · crackedRIGHT NR 3 WINDOW FRAME E-F POST CRACKED AT 5TH LOWER FASTENER HOLE. PERFORMED INTERIM REPAIR TO THE 5TH FASTENER HOLE FROM THE BOTTOM OF THE R3 WINDOW FRAME E-F POST IAW PART 1.SDR CALA2025101510114Window Frame · crackedRH NO. 3 WINDOW FRAME E-F POST CRACKED AT 5TH LOWER FASTENER HOLE - INTERIM REPAIR AT THE REPAIRED AREA OF THE RIGHT HAND #3 WINDOW FRAME E-F POST, REPAIRED AREA OF THE RH #3 WINDOW FRAME E-F POST REF ECRA 5310-08676.SDR CALA2025073107145Lens · missingSEAT 1B EMERG LIGHT COVER MISSING. REPLACED FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 1B, CHECKS OK. REF AMM 33-51-11.SDR CALA2025062305781Window · arcedWINDOW 2 BEGAN ARCING EXTERIOR PANE R2 CRACKED AND DAMAGED THIS IS FOR R1 WINDOW R&R. UPDATING M&L TO REFLECT (35MH AND 22GT) ACP E-LOTO, REMOVED 2 EACH EFIS PANELS REF AMM31-62-12-000-801, REMOVED DFCS CONTROL PANEL REF AMM22-11-34-000-801, REMOVED RH WINSHEISDR CALA2025041603916Computer · malfunctionedON TAKEOFF ROLL THRUST LEVERS SPLIT AND AUTO THROTTLES DISENGAGED. BITE OF AT SHOWS ASM2 AT DISC RATE MON. REF FIM 22-32 TASK 819. CURRENT FAULT BITE AND SERVO MOTOR TEST SHOWS NO FAULTS. DUE TO INFLIGHT FAULTS AND FLIGHT CREW REPORT. REPLACED ASM #2 REF AMMSDR CALA2025031702867Module · faultedCREW REPORTED FLIGHT CONTROL B SYS HYD OVERHEAD LIGHT ON FOLLOWED QRH TURNED ON STDBY RUDDER ADDING WHAT CREW SENT IN ON E-MAIL ,ON DEPARTURE MASTER CAUTION ILLUMINATED WITH FLT CONT LIGHT AND LOW PRESSURE LIGHT ON OVERHEAD PANEL ON FLT CONT B SIDE. FLYING PILSDR CALA2025021702342Proximity Sensor · faultedLEADING EDGE SLATS TRANSIT LIGHT STAYS ON 7 ON FLAP RETR SLAT 7 TRAN SIT LT STAYED ON W/ASS A LE FLAPS TRANSI T LT ON. SLIGHT ASSEMETRY/ROLL. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED. PERSDR CALA2025011501910Light · inoperativeSEAT 23C EMERGENCY PATH LIGHTING MODULE IS BRKN OFF FROM SEAT. L T NOT WORKING. SWAPPED LIGHTS AT 23C WITH 34C - EMERGENCY LIGHT AT 34C REQUIRES REPLACEMENT. REPLACED BROKEN LIGHTING MODULE AT SEAT 34C,OPS CHECKED GOOD.SDR CALA2024062100052Controller · inoperativeAIRCRAFT IS HOT. CANNOT BE COOLED ON GND OR AIR UNTIL REACHING CRUISE. BITE TEST CABIN TEMP CONTROL, CTC HAS NO POWER TO BIT TEST, REST SYS, NO HELP. R & R CABIN TEMP CONTROLLER PER AMM 21-61-01 OPS CHKD GOOD. PERFORMED TEST, BOTH PACKS & SELECTING CABIN TEMSDR CALA2024012200167Window Frame · crackedAC 0727, LEFT-HAND NO. 3 WINDOW FRAME POST E-F CRACK INTERIM REPAIR. LEFT-HAND NO. 3 WINDOW FRAME (POST E-F) REPAIR ON AIRCRAFT N38727 PER PART 2 OF THE LATEST REVISION OF ECRA 5611-01336. AFTER OCTOBER 14, 2025, BUT BEFORE NOVEMBER 14, 2025, PLANNING TO CONTASDR CALA2023122103706Intercostal · crackedFWD CARGO COMPARTMENT BETWEEN STA 480 TO STA 500, L 21 STRINGER, LONGITUDINAL LAP SPLICE IS CRACK SEE DOT (103-43). REF AAR N/R 9216662. REMOVED AND REPLACED INTERCOSTAL (143A7550-11) AT FORM ATTACHED OP-84 FOR ACCOMPLISHMENT OF HEAT FWD CARGO COMPARTMENT STA SDR CALA2023120803603Window Frame · crackedFOR SDR TRACKING PURPOSE ONLY "737NG LH #1 WINDOW FRAME INSPECTION AND PREVENTATIVE MOD" REF AAR N/R 9217043.SDR CALA2023112703484Skin · crackedCRACK FOUND ON LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 129.50, 17 FROM FRONT SPAR I/B ROW. CRACK LENGTH 1.218 REF N/R 9216514 REPAIRED CRACK AT LEFT HORIZONTAL STABALIZER LOWER SKIN STA. ACCOMPLISHED BY V938928. 129.50, 17" FROM FRONT SPAR I/B ROW INSDR CALA2023060501752Shutoff Valve · leakingDIVERT FOR SUSPECTED FUEL LEAK LEAKS. PERFORMED CROSSFEED VALVE FUNCTIONAL TEST IN REF TO MM28-22-00-7 ING FLOAT VALVE REF MM28-13-11. NO DEFECTS NOTED. NO UNWANTED TR ROTABLE PARTS CHANGE WAS INDICATED - TT # 1101271 SN OFF 1424 PERFORMED BOOST PUMP PRESSURSDR CALA2022101002758Pcu · false activationUNCOMMANDED ROLLL LEFT AND RIGHT AT 2500FT PERFORMED DFCS FLIGHT FAULTS CHK, NO FAULTS BOTH A/B SYSTEMS. CURRENT STS- NO FAULTS FOR A/P. PEFORMED DFCS LAND VERIFY BITE I.A.W. AMM 22-11-00, "PASSED". ENGAGED & DISENGAGED A/P''S MULTI- PLE TIMES WITH NO KICKBACKSDR CALA2022071301714Stop Fitting · crackedRIGHT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED AND BENT -- SEE SAFETY BULLETIN PHOTO,S.. PHOTO,S ADDEDSDR CALA2021080901281Indicator · faulted*DECLARED EMERGENCY* IAS DISAGREE.CAPT SIDE IAS 235.FO SIDE IAS 247 CAPT SIDE APPEARS CORRECT.FL380. SAT-50. LOCKED BY TOMC SR MANAGER DUE TO EMERGENCY BEING DECLARED FOR LANDING UNLOCKING FOR UPDATE. LOOKED AT CAPT AND F/O PITOT PROBE, NO NOTICEABLE BLOCKAGE SDR CALA2021043000579Fitting · crackedSHEAR FITTING AT STA540 RBL40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87. IAW B73 7-700 SRM 51-60-02 ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000578Fitting · crackedSHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.SDR CALA2021043000577Fitting · crackedSHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.SDR CALA2021043000582Fitting · crackedSHEAR FITTING AT STA540 RBL6.14 IS CRACKED-N/R6 227155 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000581Fitting · crackedSHEAR FITTING AT STA540 RBL15.04 IS CRACKED-N/R 6227154 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW B737 -700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000580Fitting · crackedSHEAR FITTING AT STA540 RBL32.40 IS CRACKED-N/R 6227153 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW B737 -700 SRM 51-40-02 ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000576Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA540 LBL6.14 IS CRACKED-N/R 6227150 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000575Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA540 LBL15.04 IS CRACKED-N/R 6227149 REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 15.04. IAW B737-700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL. SS FR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 4SDR CALA2021043000574Fitting · crackedSHEAR FITTING AT BS 540, LBL 32.4 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000573Fitting · crackedSHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01209.SDR CALA2021043000572Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED-622 7146 REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5716-01208.SDR CALA2019063001104Thermocouple · malfunctionedEGT EXCEED 965 DEGREEES AFTER TAKEOFF. EGT NORM AFTER THROTTLE R ETARDED PER CREW VERBAL, # 2 ENGINE. BY VERBAL FROM CREW AIRCRAFT WAS NOT IN AN OVERWEIGHT CONDITION AT LANDING. 73-10322, 77-20862, 77-20872, 75-10362, 775-30412, 77-20872, 75-20462, AND 75-3041SDR CALA2019030400350Skin · dentedNOTE THIS DAMAGED TRANSFERED FROM LOGPAGE 9006123. DENT IN FUSELAGE SKIN, STA. 827-847, STR. 25LT-27RT. VERIFIED REMOVAL OF DAMAGED MATERIAL. PERFORMED HFEC AROUND CUTO UTS. REF: NDT P6 51-00-00-23. ALSO PERFORMED THICKNESS CHECK 0.002"REMOVED FROM BURNISHED ASDR CALA2018092401978Module · faultyCAPT AND F/O UNRELIABLE AIRSPEED/ALTIMETER AND ENG LIGHT ON. AIR SPEED DISAGREE BY200 KTS CREW REPORTS CAPT AIRSPEED DROPPED TO 80KTS. EEC BITE FLT HISTORY SHOWS MSG 73-31641 & 73-31642 ADIRU TOTAL PRESSURE DISAGREE FLUSHED CAPT & F/O PITOT SYSTEM PER AMM 34-1SDR CALA2017122204571Door Frame · corrodedL1 DOOR FRAME CORRODED AT BS 303.9 JUST ABOVE UPPER DOOR HINGE. REPAIRED THE DOOR FRAME BETWEN STRINGERS 9L AND 10L IAW ECRA 5311-01889.SDR CALA2017121804498Hinge · corrodedFOUND CORROSION ON THE L1 DOOR UPPER HINGE FITTING. REMOVED AND REPLACED UPPER FUSELAGE HINGE FITTING AT L1 DOOR P/N 141A8186-4 PER SRM 51-40-02 REF BOEING DWG # 141A8180.SDR CALA2017121804497Fitting · corrodedFOUND CORROSION ON S10 LT FITTING. FABRICATED NEW FITTING.SDR CALA2017112104176Bulkhead · crackedPRESSURE BULKHEAD CRACKED, RBL 31.8 TO RBL 40. INSTALLED A REPAIR IAW SRM 57-10-10, REPAIR 3, ALTERNATIVE 2.SDR CALA2017082802921Altimeter · malfunctionedCAPT ALTIMETER CLIMBED APPROX 900 FT AND RETURNED IN APPROX ONE SECOND. PERFORMED BIT/OP TEST OF LEFT AND RIGHT HAND ADIR'S UNITS. NO FAULTS FOUND SYS GROUND TEST GOOD IAW AMM 34-21-00.SDR CALA2013081900579Stringer Splice · corrodedSTRINGER SPLICE CORRODED S24L AT BS 887. STRINGER SPLICE WAS REPLACED REF DWG 147A3287 AND SRM 51-40-02.SDR CALA2013081900578Stringer · corrodedAFT CARGO BAY STRINGER CORRODED BEYOND LIMITS BS 867 S24L. R & R STRINGER REF DWG 146A3230 AND SRM 51-40-02.SDR CALA2013081600571Intercostal · corrodedAFT CARGO BS 847-867, BETWEEN STRINGERS S25-26L, FOUND HEAVY IGC CORROSION AT INTERCOSTAL LOCATED FWD OF WASTE TANK. DAMAGE ON AFT CARGO INTERCOSTAL FOUND TO BE OUT OF LIMITS, REMOVED, FABRICATED, AND INSTALLED REF SRM 53-00-53, 51-40-02.SDR CALA2013081600570Floorbeam · corrodedFLOORBEAM, BS 1016 AT LBL 32 CORRODED ON AFT FLANGE. REPAIRED IAW ECRA 5310-05843SDR CALA2013081600569Floorbeam · corrodedAFT WET AREA, FLOORBEAM BS 986.5. TOP AREA AT RBL 12 CORRODED AROUND FASTERNER HOLE. REPAIRED IAW ECRA 5310-05842.SDR CALA2013081600568Angle · corrodedAFT WET AREA L-2 DOOR, ZEE ANGLE HAS SURFACE CORROSION LOCATED BETWEEN BS 947.5 AND BS986.5 ALONG THE SURFACE. REMOVED, VERIFIED AND INSTALLED L-2 DOOR ZEE ANGLE REF DWG 147A8540-1 AND SRM 51-40-02.SDR CALA2013081200559Angle · corrodedAFT WET AREA, R2 DOOR ZEE ANGLE HAS SURFACE CORROSION LOCATED BETWEEN BS 947.5 AND 962 IN SEVERAL AREAS ALONG THE SURFACE. REMOVED, VERIFIED, TRANSFERED HOLES AND INSTALLED ZEE ANGLE IAW DWG 147A8540-1 AND SRM 51-40-02.
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