N952CA
Service difficulty reports · 268
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 = 'N952CA' 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 = 'N952CA' 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 U2RA2023032900014Unknown · unknownAFTER FUEL UPLIFT, FUEL FOUND VENTING FROM R/H WING SURGE TANK. ALLOWED FUEL TO FINISH VENTING - OPERATIONALLY CHECKED FUEL SYSTEM AND CONTINUED WITH MISSION. NO DEFECTS NOTED - SUSPECT THERMAL EXPANSION CAUSED VENTING.SDR U2RA2023022000007None · noneRECEIVED INTERMITTANT FIRE CARGO AFT WARNING MESSAGE DURING GO AROUND - INSPECTED AFT CARGO FOR SMOKE/FIRE AND FOUND NONE. FIRE DETECTION SYSTEM TEST ACCOMPLISHED PER AIRCRAFT MAINTENANCE MANUAL 26-16-00 WITH NOW DEFECTS NOTED.SDR U2RA2023020600006Not Reported · not reportedRIGHT SIDE EMERGENCY EXIT DOOR "BATTERY OK" TEST LAMP IS INOPERATIVE - RESEATED BATTERY, CLEANED BATTERY CONNECTION, VERIFIED PROPER VOLTAGE, OPS CHECK SATISFACTORY PER AMM 52-23-14.SDR U2RA2023011000002Fire Warning · false activationMAIN DECK FIRE WARNING ACTIVATED AFTER LANDING. NO STATUS OR EICAS MESSAGE SHOWN. - NO FIRE PRESENT. PERFORMED GROUND TEST PER AIRCRAFT MAINTENANCE MANUAL 26-14-00. SYSTEM OPS CHECKS GOOD.SDR U2RA2023011000001Fire Warning · false activationMAIN DECK FIRE WARNING, MASTER WARNING AND FIRE BELL ON TAKEOFF ROLL. REJECTED TAKEOFF. FIRE BELL CONTINUED TO SOUND AFTER SILENCED. - NO FIRE PRESENT. DISCOVERED MOISTURE IN CARD FILE M5206 CAUSED BY PALLETS BEING LOADED WET AND WATER DRIPPING INTO THE ELESDR U2RA2022121400057Battery Pack · inoperativeLEFT UPPER DECK EMERGENCY DOOR BATTERY OK TEST LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK PER AIRCRAFT MAINTENANCE MANUAL 52-23-14. OPS NORMALSDR U2RA2022080300039Powerpack · inoperativeRIGHT UPPER DECK DOOR ASSIST BOTTLE POWER PACK DOES NOT TEST - REMOVED AND REPLACED POWER PACK IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR U2RA2022062600024None · noneFUEL DISCOVERED LEAKING FROM THE RIGHT WING SURGE TANK. EXTENUATING CIRCUMSTANCES INCLUDE PARKING CONFIGURATION THAT LEFT THE AIRCRAFT TILTED TO THE RIGHT. RIGHT WING SURGE TANK WAS SUMPED OF FUEL - NO FURTHER LEAKS WERE NOTED.SDR U2RA2022061700020None · noneGROUND EQUIPMENT DAMAGE TO NUMBER 1 ENGINE INLET COWLING - ACCOMPLISHED TIME LIMITED MAJOR REPAIR OF COWLING PER FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER 220092-1 REVISION IR DATED 6/14/2022.SDR U2RA2022060900018None · noneDURING REFUEL, FUEL SPILLED FROM THE RIGHT WING OVERBOARD VENT. - SUMPED RIGHT WING SURGE TANK AND CONTINUED REFUEL OF AIRCRAFT PER AIRCRAFT MAINTENANCE MANUAL 12-11-10 WITHOUT INCIDENT. NO DEFECTS NOTED PER AIRCRAFT MAINTENANCE MANUAL 28-21-00SDR U2RA2022060600015None · noneDURING INSPECTION FOUND ELONGATED FASTENER HOLES COMMON TO LONGERON’S P/N 65B0279-13 (L/H) AND P/N 65B0279-14 (R/H) BETWEEN BS 2742 AND BS 2775. REPAIRED AS DIRECTED IN FVCI EO # 22071-6 REV B. DATED 05/21/2022 AND APPROVED BY FORM 8130-3 ISSUED BY DERT-71016SDR U2RA2022060600014None · noneDURING INSPECTION FOUND ELONGATED FASTENER HOLES ALONG THE #4 PYLON OUTBOARD SKIRT BEAM LOWER CHORD @ NAC STA 400 TO 420.55. REPAIRED AS DIRECTED IN FVCI EO # 22071-4 REV C. DATED 05/29/2022 AND APPROVED BY FORM 8130-3 ISSUED BY DERT-710167-SW; DATED 05/30/20SDR U2RA2022060600017Frame · elongatedDURING INSPECTION FOUND 5 EACH ELONGATED FASTENER HOLES COMMON TO THE P/N 65B02789 FRAME STRAP @ BS 2775.3. REPAIRED AS DIRECTED IN FVCI EO # 22071-8 REV C. DATED 05/26/2022 AND APPROVED BY FORM 8130-3 ISSUED BY DERT-710167-SW; DATED 05/29/2022. REPAIR CATEGSDR U2RA2022060600012None · noneDURING INSPECTION OF THE R/H #5 MED CUT-OUT AFT UPPER CORNER, INTERNAL BEAR STRAP FOUND CRACKED. ACCOMPLISHED REPAIR AS REQUIRED BY BOEING SB 747-53A2839 PART 5, TO INCLUDE DEVIATION (DAMAGE REMOVAL TRIM OUT RADIUS REDUCED TO 1.0” INSTEAD OF 1.5” AS REQ. BY SSDR U2RA2022060600011None · noneCORROSION DAMAGE FOUND AT LEFT WING L/E PANEL SUPPORT BEAM @ OLES 1510 APPROXIMATE. REMOVED DAMAGED SECTION AND SPLICED IN REPLACEMENT BEAM AS REQUIRED PER B747-400 SRM 57-41-13 REPAIR 3, BAC SR #4-5471089571, AND FORM 8100-9 ISSUED BY BOEING; DATED 05/29/202SDR U2RA2022060600016Seat Track · chafedDURING INSPECTION FOUND CHAFFING DAMAGE TO CARGO COMPARTMENT “TIE-DOWN” TRACK P/N 65B18740-10 BETWEEN BS 1900 AND BS 1920. REPAIRED AS DIRECTED IN FVCI EO # 22071-7 REV A. DATED 05/20/2022 AND APPROVED BY FORM 8130-3 ISSUED BY DERT-710167-SW; DATED 05/27/2022SDR U2RA2022060600013Skin Panel · elongatedDURING INSPECTION FOUND ELONGATED FASTENER HOLES ALONG FORWARD SEGMENT OF THE #4 PYLON OUTBOARD SKIRT BEAM SKIN PANEL P/N 323U2384-134. REPAIRED AS DIRECTED IN FVCI EO # 22071-3 DATED 05/10/2022 AND APPROVED BY FORM 8130-3 ISSUED BY DERT-710167-SW; DATED 05/2SDR U2RA2022010400001Battery Pack · dischargedUPPER DECK R/H DOOR EMERGENCY ASSIST BOTTLE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE UPPER DECK R/H DOOR EMERGENCY SYSTEM BATTERY PACK PER B747 AMM 52-23-14.SDR U2RA2021112400068None · noneRIGHT EMERGENCY ESCAPE DOOR BATTERY TEST FUNCTION INOPERATIVE - RESEATED CONNECTOR ON THE BATTERY PACK AND SYSTEM FUNCTIONS NORMAL PER AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR U2RA2021110100068Battery Pack · dischargedDURING DAILY SERVICE CHECK, FOUND R/H UPPER DECK ENTRY DOOR EMERGENCY ASSIST BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER AMM - OPERATIONAL CHECK NORMAL.SDR U2RA2021082430051Skin · dentedREF. LP 49190-3, HAITEC W/O H1-21-05-00060/17084 & NRC 0021, AND FVCI E/O #21123-3: FWD. CARGO DOOR HAS DAMAGE TO THE LOWER FORWARD CORNER – EXTERIOR SKIN IS DENTED AND CREASED. ACCOMPLISHED DOUBLER REPAIR TO THE FWD. CARGO DOOR LOWER FORWARD CORNER AS PER FSDR U2RA202008040002Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-153-01-01, ENLARGED BOLT HOLES NOTED ON NUMBER 1 PYLON PANEL NUMBER 452EL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202008040001Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-153-01-04, ENLARGED BOLT HOLE NOTED ON NUMBER 4 PYLON PANEL NUMBER 482EL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202010160009Skin · gougedGOUGE NOTED ON NUMBER 1 PYLON UNDERWING FAIRING UPPER SIDE SKIN PANEL AT NACELLE STATION 338. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20322-5.SDR U2RA20201016006Skin · deformedDEFORMATION NOTED ON SKIN OF NUMBER 4 PYLON LEFT UPPER FAIRING DOOR FORWARD SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-2.SDR U2RA202010160005Panel · crackedCRACK NOTED ON NUMBER 4 PYLON LEFT UPPER SIDE SKIN. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-1.SDR U2RA202010160004Fitting · nickedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, A NICK WAS NOTED ON THE NUMBER 2 PYLON FAN COWL AFT SUPPORT BEAM OUTBOARD AREA. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314.SDR U2RA202010160003Angle · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-814-00-02, 1 EACH CRACK NOTED ON ANGLE OF NUMBER 2 PYLON PANEL 464B INBOARD UPPER FORWARD SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20305-1.SDR U2RA202010160002Angle · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-814-00-02, 1 EACH CRACK NOTED ON SKATE ANGLE OF NUMBER 3 PYLON INBOARD FAIRING AT NACELLE STATION 457. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20305.SDR U2RA202010160001Stanchion · crackedDURING ACCOMPLISHMENT OF TASK CARD 53-510-00-01, 1 EACH CRACK NOTED ON STANCHION AT FORWARD CARGO DOOR CUTOUT AREA AT BODY STATION 560 STRINGER S-35R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20307.SDR U2RA202010190004Stiffener · crackedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-53A2465 REVISION 5, FOUND NOSE WHEEL WELL SIDE PANEL STIFFENER CRACKED AT BODY STATION 265-STA 280 WATERLINE 170, LEFT BUTTOCK LINE 30. FABRICATED STIFFENER IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INCSDR U2RA202010160010Skin · gougedGOUGE NOTED ON NUMBER 1 PYLON UNDERWING FAIRING SKIN PANEL AT NACELLE STATION 332. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-5.SDR U2RA202010150002Door Frame · crackedDURING ACCOMPLISHMENT OF SB 747-53A2450 REV 8, 2 EACH CRACKED FASTENER HOLE NOTED AT NR 5 RIGHT MAIN ENTRY DOOR CUTOUT, 1 EACH AT BODY STATION 2231 STRINGER S-19R. REPAIR ACCOMPLISHED IN ACCORDANCE WITH B747-400SF STRUCTURAL REPAIR MANUAL 53-60-15-2R-2, WITH SDR U2RA202010150001Strap · crackedDURING ACCOMPLISHMENT OF SB 747-53A2450 REV 8, 2 EACH CRACKED FASTENER HOLES WERE NOTED, 1 EACH AT BODY STATION 2231 STRINGER S-16L AND 1 EACH AT BODY STATION 2231 STRINGER S-19L. REPAIRS ACCOMPLISHED IN ACCORDANCE WITH B747-400SF STRUCTURAL REPAIR MANUAL 53-SDR U2RA202010190003Bracket · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-806-00-01, A CRACK WAS NOTED ON A PNEUMATIC TUBE SUPPORT BRACKET, INSIDE NUMBER 1 PYLON PANEL 451B. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 20293-4.SDR U2RA202007110005Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-03, CRACKS WERE NOTED ON THE EXTERNAL SURFACE OF NUMBER 3 PYLON PANEL NUMBER 472FL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316-8.SDR U2RA202007110004Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, CRACKS WERE NOTED ON THE EXTERNAL SURFACE OF NUMBER 2 PYLON PANEL NUMBER 462GL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316.SDR U2RA202007110003Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-04, CHAFING WAS NOTED ON SKIN OF NUMBER 4 PYLON PANEL NUMBER 482FR. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20319-1.SDR U2RA202007110002Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-03, ENLARGED BOLT HOLE NOTED ON NUMBER 3 PYLON PANEL NUMBER 472ER. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202007110001Skin · corrodedDURING ACCOMPLISHMENT OF DAMAGE TOLERANCE INSPECTION FOR SATELITE COMMUNICATION SYSTEM ANTENNA DOUBLER, CORROSION WAS NOTED ON THE SKIN INTERIOR AT BODY STATION 1480 FROM STRINGER S-10L TO STRINGER S-11L. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLESSDR U2RA202010160007Skin · dentedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-04, DENT WITH GOUGES WAS NOTED ON THE SKIN OF NUMBER 4 ENGINE LEFT CORE COWL OUTER SURFACE AT NACELLE STATION 182.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20SDR U2RA202010160006Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-04, DENT WITH GOUGES WAS NOTED ON THE SKIN OF NUMBER 4 ENGINE LEFT CORE COWL OUTER SURFACE AT NACELLE STATION 182.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20SDR U2RA202007100004Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-814-01-01, CHAFING WAS NOTED ON DOUBLER OF NUMBER 1 ENGINE LEFT CORE COWL INNER FACE AFT SIDE FRAME. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER 20316-10.SDR U2RA202007100003Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING NOTED ON THE SKIN OF THE NUMBER 1 ENGINE LEFT THRUST REVERSER COWL INNER FACE LOWER BIFURCATION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20319-2.SDR U2RA202007100002Structure · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING WAS NOTED ON THE SKIN OF NUMBER 1 ENGINE RIGHT THRUST REVERSER COWL INNER SURFACE FORWARD SIDE, NAC STA 131.78. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUSDR U2RA202007100001Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 53-804-01-01, EXISTING BLEND REPAIR NOTED ON SKIN AT LOWER FUSELAGE STA 1801 S-38R TO S-39R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC, ENGINEERING ORDER NUMBER 20288.SDR U2RA202007090003Skin · crackedDURING ACCOMPLISHMENT OF TASK 57-810-01-01, A CRACK WAS NOTED ON THE SKIN OF THE LEFT WING INBOARD FIXED LEADING EDGE NOSE BEAM CUTOUT, ADJACENT TO THE NUMBER 11 KRUEGER FLAP INBOARD LINK, LEADING EDGE ILES 543.93. REPAIR ACCOMPLISHED, IN ACCORDANCE WITH FLIGSDR U2RA202007090002Exhaust Duct · crackedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-02, A DENT WAS NOTED ON THE OUTER SKIN OF THE NUMBER 2 ENGINE EXHAUST SLEEVE, NACELLE STATION 318 NEAR 7 O`CLOCK POSITION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMSDR U2RA202007090001Skin · crackedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-53A2390, CRACKED FASTENER HOLES WERE NOTED AT SKIN PANEL UNDER LONGERON EXTENSION FITTING 1 EACH BODY STATION 1480 STRINGER S-32L AND 1 EACH AT BODY STATION 1480 BETWEEN STRINGERS S-32R AND S-34R. REPAIR ACSDR U2RA202007080004Skin · corrodedDURING ACCOMPLISHMENT OF TASK CARD 55-820-01-01, CORROSION WAS NOTED ON THE SKIN OF THE RIGHT HORIZONTAL STABILIZER UPPER SURFACE AT STABILIZER STATION 385 STRINGER 5. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20322-1.
Back to N952CA