N76526
Service difficulty reports · 30
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 = 'N76526' 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 = 'N76526' 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 CALA2026072217945Power Supply · inoperativeROW 20 21 FED EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FOR EMERGENCY LIGHT IAW AMM 33-51-06. OPS CHECKED GOOD.SDR CALA2026031614583Battery Pack · faultedOPERATIONAL CHECK OF THE EMERGENCY LIGHTS. EXTERIOR EMERGENCY LIGHT INOPERATIVE, LT SIDE AFT OF AFT EMERGENCY EXIT DOOR. REPLACED THE LAMPS LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04-960-801. NO HELP. IAW FIM 33-50, TASK 801, REPLACED THE LIGHT ASSYSDR CALA2025120211690Indicator · unreliableAIRSPEED UNRELIABLE. PER FLIGHT CREW FO'S SIDE AIRSPEED WAS UNRELIABLE, ABOUT 50 KNOTS OFF OTHER SIDE/STBY. CDS BITE SHOWED AIRSPEED DISAGREE MESSAGE MX MSG 31-65060. NO OTHER ASSOCIATED FAULTS ON SMYD OR ADIRU BITE FOUND. 15 LEGS AGO THERE WERE A COUPLE ASDR CALA2025082608135Skin · crackedONE CRACK SIGNAL NOTED L=0.500 INCH AT HORIZ STAB LH SIDE BETWEEN STA 101.90 AND STA 111.10 LOCATED 2.375 INCH FRONT FROM REAR SPAR. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN BETWEEN HSS 101.90 AND STA 111.10 LOCATED TO 2.375 INCH FRONT FROM REAR SPAR. IASDR CALA2025082608134Skin · crackedTWO CRACKS SIGNAL NOTED AT STAB RT SIDE HSS 129.50, FIRST CRACK L=0.250 INCH LOCATED TO 9.125 INCH AFT FROM FRONT SPAR, SECOND CRACK L= 0.375 INCH LOCATED TO 17.310 INCH AFT FROM FRONT SPAR REPAIRED RT HORIZONTAL LOWER SKIN HSS 129.50, LOCATED TO 9.125" AFT FSDR CALA2025062605887Girt Bar · out of adjustDOOR 1R GIRT BAR NOT STOWING IN DISARM POSITION. READJUSTED DOOR 1R GIRT BAR CLIP IAW AMM 25-66-01, OPS CKS NORMAL.SDR CALA2025041003677Controller · defectiveIN AIR RECEIVED LEFT PACK LIGHT. WOULD NOT CLEAR WITH TRIP RESET FLAGGED AS SDR SUGGEST TROUBLESHOOTING PER THE FOLLOWING FIM TASK..L (R) PACK LIGHT IS ON (WITHOUT MASTER CAUTION RECALL) - FAULT ISOLATION REFERENCE: 21-53 TASK 820 ACCOMPLISHED STEP.D OF MEL 21SDR CALA2025012802083Battery Pack · dischargedEMERGENCY LIGHTS @ ROW 28 - 32 & AFT RIGHT DOOR SIGNS INOP. R&R AFT-PACK, BATTERY, EMERGENCY POWER #99-3351-3-0015. REF. AMM 33-51-06-960-805. OPPS CHECK GOOD AT THIS TIME.SDR CALA2025010601783Engine · faultyPER FLIGHT CREW: E2 IFSD AT 30K FT. NO SIGNIFICANT EVENT BEFORE SD. OIL PRESSURE SEEMED TO DROP NORMALLY AS E2 SPOOLED DOWN. WINDMILLED FOR 20-25 MINUTES AS A/C RETURNED TO SFO. ACCOMPLISHED VISUAL INSPECTION OF ENG #2. BLADES WERE WINDMILLING FREELY UPON ARRISDR CALA2024122701670Transmitter · faultedON APPROACH FLAPS STUCK AT 25 DEG. FLAP/SLAT ELECTRONIC UNIT SHOWS LEG 0 FAULT TE FLAP SNSR R, MSG NO: 27-52260, INTRMTNT INACTIVE, R FL POS +194.0, D728B PIN J7, J8. GROUND TEST PASSED. FLAP OPERATION NORMAL, NO SPIT. REMOVED AND REPLACED RH FLAP POSITION TRASDR CALA2024100402563Skin · crackedFOUND CRACK AND CORROSION EXFOLIATION AT THE FUS EXTERNAL SKIN STA 917 BTW STRG 21L AND STRG 22L AT BOTTOM HALF OF THE VACUUM WASTE VENT CUTOUT REQUIRE REPAIR PER SRM 53-70-01-2R-3. (REF: AAR NR 1000021409) ION, INSPECTION THRESHOLD 50,000 CYCLE METHOD (LFEC)SDR CALA2024040300961Fuel Sys · out of balanceDURING CLIMB FUEL IMBAL IN MAIN WITH 5000LBS REMAINING IN CENTER TNK. ON ARRIVAL FOUND RIGHT MAIN TANK READING 800 LBS HIGH COMPARED STICK TABLE REF. AMM 12-11-02-993-953. FUELED MAIN TANKS TO 8500 INDICATION. (BLANK). REQUEST DEFERRAL PER MEL. DDP C/W DEFERRESDR CALA2022120703318Pump · faultedHYD 1 ENG PUMP LOW PRESSURE MAINTAINED AT 3000 PSI. REMOVED ENG #1 EDP, COMPLETED REMOVAL OF ENG 1 EDP AND INSTALLED NEW EDP ON ENG 1. REPLACED #1 ENG AGB ROTATING SEAL FOR HYD PUMP. INSTALLED #1 HYD PUMP. INSTALLED NEW MAGNETIC CARBON SEAL. OPS CHECK GOOD.SDR CALA2022102702973Skin · crackedR/H HORIZONTAL STAB. LOWER SKIN AT STA.129.50 I/B SIDE HAS A CRACK 26 INCHES FROM FWD SPAR ABOUT .50 IN.LENGTH.(MARKED) ACCOMPLISH REPAIR REF. SRM 55-10-01 PRIOR TO FURTHER FLIGHT. (REF. BAM N/R 000983735) INSPECTIONS PER SRM 55-10-01-2R -11 REPAIR 11 TABLE 20SDR CALA2022102402925None · crackedR/H HORIZONTAL STAB. LOWER SKIN AT STA.129.50 I/B SIDE HAS A CRACK 26 INCHES FROM FWD SPAR ABOUT .50 IN.LENGTH.(MARKED) ACCOMPLISH REPAIR REF. SRM 55-10-01 PRIOR TO FURTHER FLIGHT. (REF. BAM N/R 000983735) INSPECTIONS PER SRM 55-10-01-2R -11 REPAIR 11 TABLE 20SDR CALA2022100302589Skin · unknownR/H HORZ. STAB. SKIN REPAIR AT STA 92.70 SFR CREATED.SDR CALA2021122702447Roller Track · defectiveRTO 100KTS DUE TO REVERSER ENG 2 MASTER CAUTION ON DURING TAKE OFF PERFORMED EAU BITE PROCEDURE PER FIM 78-31 TASK 801. FOUND UPDATED WITH PARTS INFO FOR EAU. PER FIM 78-31 TASK 817 INSPECTED SSPS ROLLER ASSEMBLY AND FOUND FAULTS HYD ISO VALVE SENSOR S830, RSDR CALA2021083001451Indicator · split*DECLARED EMERGENCY*FLAPS TRAILING EDGE FLAP LOCKOUT ON APROACH L/R SPLIT AT LESS THAN FLAP 5. HANDLE MOVED TO F-2 PER PROCEDUR E. FLAPS WENT TO F-2 UPON LANDIN DECREASING FROM 210K TO APROX 190K,FROM FLAPS5 TO FLAPS2, GOT A SYM LOCK WITH ONE SIDE AT 2 UNITS SDR CALA2019082001380Skin · crackedRH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT RIB LOCATION STA 138.7, 25" FROM FORWARD SPAR - REF FLEET CYCLE LOG 9688574 LOG FOR DIP ONLY. REPAIRED SKIN CRACK PER SRM 55-10-01, REPAIR 11. SEE FLEET CYCLE LOG 9688574 FOR DETAILS OF REPAIR ACCOMPLISH ED. INSDR CALA20190821379Skin · crackedRH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT RIB LOCATION STA 157.1, 30" FROM FORWARD SPAR - REF FLEET CYCLE LOG 9688575 LOG FOR DIP ONLY. REPAIRED SKIN CRACK PER SRM 55-10-01, REPAIR 11. SEE FLEET CYCLE LOG 9688575 FOR DETAILS OF REPAIR ACCOMPLISH ED. INSDR CALA2019081601373Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT RIB LOCATION STA 138.7, 25" FROM FORWARD SPAR - REF FLEET CYCLE LOG 9688568 LOG FOR DIP ONLY. REPAIRED SKIN CRACK PER SRM 55-10-01, REPAIR 11. SEE FLEET CYCLE LOG 9688565 FOR DETAILS OF REPAIR ACCOMPLISH ED. INSDR CALA2019081601372Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT RIB LOCATION STA 129.5, 10" FROM FORWARD SPAR - REF FLEET CYCLE LOG 9688565 LOG FOR DIP ONLY. REPAIRED SKIN CRACK PER SRM 55-10-01, REPAIR 11. SEE FLEET CYCLE LOG 9688565 FOR DETAILS OF REPAIR ACCOMPLISH ED. INSDR CALA2018120202487Light · inoperativeRT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK. ACP IDT INSP OF RT AFT OW EPL LIGHT RELAMP REF GMM 09-10-05. OPS CK GOOD.SDR CALA2018120202485Light · inoperativeLT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED OPS CHECK OK ACP IDT INSP OF EPL LIGHT AT L AFT OW REF GMM 09-10-05. OPS CK GOOD.SDR CALA2018012800367Valve · failedBEHIND ON FUEL PLAN. WET MOTOR ENG REF 71-00-00-700-822-F00 (LEAKING IN FLIGHT). FOUND RIGHT VSV DRAIN LEAKING UPON ARRIVAL AT HANGER, MOTOR NR 2 ENG AND FOUND FUEL LEAKING FROM HPTACC DRAIN. R&R HPTACC VALVE, REF AMM 75-21-01. ACP NR 2 ENG RUN AND ACTUATORS SDR CALA2017060501718Switch · intermittentDURING AIRCRAFT POWER FAILURE, EMERGENCY LIGHTS ON ROWS 21, 22, 23 DID NOT OPERATE. VERIFIED WITH THE FLIGHT CREW, CYCLED THE LIGHT SWITCH AND EMERGENCY LIGHTS WORKED OK.SDR CALA2016080100483Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN AREA, HAS A CRACK INDICATION AT HSS 147.90 AND ABOUT 10 INCHES FROM T/E. IAW EA 5510-01843 REV E STEP 2. REMOVED DAMAGE AND INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11.SDR CALA2016080100482Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN AREA, FOUND A CRACK INDICATION AT HSS 101.90 AND ABOUT 10.5 INCHES FROM T/E. IAW EA 5510-01843 REV. E STEP 5. REMOVED DAMAGE AND INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11.SDR CALA2015082700708Trim Motor · failedELECTRIC STAB TRIM FAILED AFTER TAKEOFF. R & R OF STAB TRIM MOTOR IAW FORM 44-0008. OPERATIONS CHECKED NORMAL IAW AMM 27-41-71.SDR CALA2015070600552Wire Harness · shortedDURING CRUISE FL 370, NR 1 ENG EGT WENT TO 965C EGT, EGT IN NORMAL RANGE AT IDLE. ALL OTHER ENG INDICATIONS NORMAL. FOUND NR 1 ENG LT EGT THERMOCOUPLE PROBE SHORTED WHEN TROUBLE SHOT HIGH ENG EGT. REPLACED THERMOCOUPLE PROBE HARNESS. ACCOMPLISHED TASK IAW
Back to N76526