N858GT
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 = 'N858GT' 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 = 'N858GT' 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 P5CA2023082800086Unknown · unknownLHW MOST I/B T/E LOWER FIXED PANEL AFT SUPPORT AT WBL 128-212 WORN.(<P>SUPPORT WORN AREA REPAIRED AS PER RI #RI-57-00-16461 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082800085Unknown · unknownRH WLG I/B STRUT DOOR FWD EDGE LOWER FITTING WORN AND CRACK(<P>WORN AND CRACK FITTING REPAIRED AS PER RI #RI-52-80-16471 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082800084Unknown · unknownRHW MOST I/B LOWER FIXED PANEL AFT SUPPORT BEAM WBL 128-212 FOUND WORN(<P>SUPPORT BOTH WORN AREA REPAIRED AS PER RI #RI-57-22-16462 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082800083Rib · unknownRH HORIZONTAL STAB TIP FAIRING I/B RIB UPPER CHORD CRACK(<P>UPPER CHORD REPLACED AS PER SRM 51-10-02 NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 ). NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082800082Unknown · unknownLH I/B ELEVATOR L/E SKIN ELEV. STA 119.358 PER EA 4855A0004 HAS BEEN REVISED EA 4855A005 PERMANENT REPAIR WITHIN 500 FC PER EA(<P>L/E SKIN REPAIRED AS PER RI #RI-55-20-16459 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082500079Unknown · unknownLH I/B ELEVATOR UPPER L/E PANEL DAMAGE 4EA LOCATION(<P>DAMAGE AREA REPAIRED AS PER RI #RI-55-20-16459 REV A. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023082400078Unknown · unknownFLIGHT COMPARTMENT L1 WINDOW STRUCTURE UPPER CHORD CORNER CHORD AT STA 288 BL 1.0 FOUND SLOT(<P>SLOT WAS CONFIRMED A PRODUCTION GAP BETWEEN THE CHORD AND THE CENTER WINDSHIELD POST AS PER ATLAS AIR EO #4853A118 REV 3 </P>)SDR P5CA2022041300110None · noneSTATUS MESSAGE ENG 2 OIL SYS(<P>COMPLETED LOW PRESSURE INSP PER AMM 71-00-00 NO DEFECT. GBX INSP COMPLETED PER 72-60-00 NO DEFECT.</P> / <P>ADDITIONAL INSP FPI OF #2 ENG OIL SUPPLY TUBE PER BOEING SPM 70-11-06 NO DEFECTS. OIL CAP INSP PER AMM 12-13-03 NO DEFECSDR P5CA2021102900404None · noneATB - AFTER TAKE-OFF NOSE GEAR FAILED TO RETRACT.(<P>TRANSFERRED TO MDDR 155894 IAW MEL 32-30-01, CAT B.</P>)SDR P5CA2021093000370Channel · noneEMP - RH HORI STAB TIP FAIRING T/E SUPPORT CHANNEL 2 PLACES CRK(<P>REPLACE THE CRACKED CHANNEL IAW <SPAN>RI 55-10-14999.</SPAN></P>)SDR P5CA2021100300373Bracket · noneLHW NO.7 V/C FLAP TRANSLATING WIRE LINK BRACKET FOUND DAMAGED(<P>LHW NO.7 V/C FLAP WIRE LINK BRACKET REPLACED AS PER RI-57-00-15033 REV. A.</P>)SDR P5CA2021100300375Ceiling Panel · noneAFT CARGO STA 1920-1980 L/R CEILING FOUND TORN (2EA)(<P>AFT CARGO STA 1920-1980 L/R CEILING REPLACED AS PER AMM 25-52-01 , LH CEILING LINER REPLACED IAW RI-25-54-15034 REV.A</P>)SDR P5CA2021100400377None · noneL/G - L/H WLG FORWARD SECONDARY DOOR L/E HEAT SHIELD ASSEMBLY EXT. SKIN FOUND DELAMINATION(<P>DELAMINATION AREA PERFORMED REPAIR AS PER RI-52-80-15004 REV A.</P>)SDR P5CA2021100500378None · noneFWD CARGO DOOR CONTROL SWITCH CHANGE (GROUP 1) THE 4EA EXISTING CLIPS COMMON TO THE STRINGERS FOUND MISMATCH SB.(<P>4EA EXISTING CLIPS INSTALL IAW RI-52-00-14998 REV A</P>)SDR P5CA2021101300384None · noneNO. 19 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021101300385None · noneNO. 6 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)SDR P5CA2021101300386None · noneNO. 21 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021101300387None · noneNO. 7 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021101300388None · noneNO. 8 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021042200152Intercostal · crackedMAIN DECK SIDE CARGO DOOR LATCH FRAME SPLICE INTERCOSTAL WEB (146U6145-1), DOUBLER (65B17613-30), AND INNER CHORD (146U6157-10) - CRACK DAMAGE AT STA 1707 WL210 TO WL200 - CAT C REPAIR(<P ><SPAN>PERFORMED TIME LIMITED / REPAIR OF MAIN DECK SIDE CARGO DOOR IAW SDR P5CA2020071500265Actuator · damagedBODY GEAR STRG EICAS AND STATUS. FOUND LT BODY GEAR INBOARD STEERING ACTUATOR DAMAGED. REMOVED AND REPLACED L BODY / GEAR INBOARD STEERING ACTUATOR IAW AMM 32-53-11, SYSTEM OPS CHECK / GOOD.SDR P5CA2020041300141Hydraulic Line · leakingAFTER TAKE-OFF EICAS MESSAGE "GEAR TILT". RETURNED TO AIRPORT.(<P ><SPAN>REPLACED BODY GEAR SENSOR (OFF PART: PN 8-935-01, NSN) AND FOUND LT BODY GEAR TRUCK TILT HYDRAULIC LINE LEAKING. REPLACED FLEX LINE / WITH TEMPORARY LINE PER GMM 3.24.1. PERFORMED LEAKSDR P5CA2019092300197Rib · crackedCRACK - FOUND LT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB410-YB430, TTL: 3EA. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PARTS IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL. OFF PARTS (PNSDR P5CA2019092300196Rib · crackedCRACK - FOUND RT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB 420. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300195Fairing · crackedCRACK - FOUND LT HST TIP FAIRING CRACKED AT STAB BL 435, YB400-YB410, 1 EACH. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW SRM 51-40-02 REV 28 AND DWG NR 65B03521 SHEET 06. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300194Bolt · brokenBROKEN - BOLT, LOWER FUSELAGE STA 1243, PRESSURE BULKHEAD FASTENER LBL 120. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW DWG NR 65B07992, SH 113 AND SRM 51-40-02 REV 28. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300193Rib · crackedCRACK - FOUND RT HST TIP FAIRING RIB CRACKED AT STAB BL 435, YB410~YB430, TTL=2 EA. REMOVED THE DAMAGE RIBS IAW SRM 51-40-02 REV 28. INSTALLED THE NEW RIBS IAW SRM 51-40-02 REV 28, DWG NR 65B03521 SH6 AND SH7. JOB COMPLETED AND CONDITION CHECK NORMAL. OFF PARTSDR P5CA2019092300192Bolt · brokenBROKEN - BOLT, LOWER FUSELAGE STA 1243, PRESSURE BULKHEAD FASTENER RBL 120. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 28. INSTALLED NEW PART IAW DWG NO 65B07992, SH 115 & SRM 51-40-02 REV 28. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300191Plate · corrodedCORROSION - PLATE, LOWER FACE OF UNDER MAIN DECK CARGO FLOOR, STA 2359 LBL 50. ACCOMPLISHED RPL PLATE AT LWR FACE OF UNDER M/D CGO FLOOR STA 2359, LBL 50 IAW AMM 51-41-12-202-037 REV 30. CONDITION CHECKS NORMAL. ADAPTER PART OFF (PN: 65B17393-13, SN: NSN)SDR P5CA2019092300190Structure · crackedCRACK ON LOWER CHORD OF HORIZONTAL STABILIZER, RT TIP, AT STAB BL 421.5. REPAIRED DAMAGED AREA IAW EI NR T2019A55M-3713 REV 2. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300189Web · crackedCRACKS ON LOWER CHORD, UPPER CHORD, AND WEB OF LT SIDE HORIZONTAL STABILIZER; TRAILING EDGE AT STAB BL 421.5. REPAIRED DAMAGED AREAS IAW EI NO T2019A55M-3727 REV 3. JOB COMPLETED AND CONDITION CHECKS NORMAL. CRACK LENGTH 0.5", 3", 5"SDR P5CA2019092300188Rib · wornWORN - FASTENER HOLES ON THE RT WING, L/E RIB AT IFSS 443.67. ACCOMPLISHED EI NO T2019A57M-3618 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019072000156Cap · open1 HOUR INTO FLIGHT "ENGINE 2 OIL SYSTEM" STATUS. 2 HOURS IN FLT FLT COMPACT ENG INDICATIONS DISPLAYED ON LOWER EICAS. ENGINE 2 READING NORMAL, OIL PRESSURE 27-30 PSI, APPROXIMATELY 7 HOURS INTO FLT ENG 2 OIL DISPLAYED OIL FILTER STATUS MESSAGE. ALL ENG 2 INDICSDR P5CA2018061500091Warning Message · false activationCABIN ALTITUDE EICAS DURING CRUISE, NO EICAS MESSAGE FOUND. STS MESSAGE, & CMC MESSAGE AFT ARR SPOT. BOTH OUTFLOW VALVE TESTED OKAY. ALL DOOR & OUTLETS OK, BOTH CPCS GND TEST PASSED AIW AMM 21-31-00/501. DOOR & SEAL INSPECTED OF ALL REVR AND OUTFLOW IAW SDR P5CA2015102200167Target · out of adjustEICAS MESSAGE, GEAR TILT AFTER TAKEOFF MSG, EXTINGUISHED AFTER A FEW SECONDS. GEAR RETRACTED NORMAL, FOUND CMC MSG, 32723 INTERMITTENT FAULT NOT ACTIVE PERFORMED BODY GEAR TRUCK TILT SENSOR TEST OF LT BODY GEAR IAW AMM 32-61-12-820-801 FOUND SENSOR AND TARGETSDR P5CA2015101800165Sensor · out of adjustGEAR TILT EICAS, PERFORMED ADJUSTMENT/TEST OF THE LT BODY GEAR TRUCK TILT SENSOR IAW AMM 32-61-12-820-801. TEST SATISFACTORY. MEASURED GAP BETWEEN TILT SENSOR AND TARGET AND FOUND OK. ACCOMPLISHED OVERWEIGHT LANDING CONDITION INSPECTION IAW AMM 05-51-39/201SDR P5CA2015092500156Skin · damagedLIGHTNING STRIKE DAMAGE ON THE FASTENER OF LT FUSELAGE EXTERNAL SURFACE AT BS 306, S14L. ACCOMPLISHED EI NR T2015A53B-2157, REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2015092500157Skin · damagedLIGHTNING STRIKE DAMAGE ON THE FASTENERS OF LT FUSELAGE EXTERNAL SURFACE AT BS 200 AND BS 220 BETWEEN S15-16L. REPAIR DAMAGE AREA IAW EI NR T2015A52B-2146, REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2015092500158Skin · dentedFOUND A DENT ON THE EXTERNAL SKIN, NEAR BS 1940, S34R. REPAIRED THE DAMAGED SKIN IAW EI T2015A53B-2112, REV 2. CHECKED NORMAL.SDR P5CA2014110900051B-Nut · looseOIL QUANTITY NR 2 ENGINE DECREASED TO ZERO OVER A 2 HOUR PERIOD, DIVERTED. PRESSURE AND TEMPERATURE STAYED NORMAL. FOUND NR 5 BEARING SCAVENGE TUBE B-NUT LOOSE. TORQUED B-NUT IAW AMM 79-21-09. PERFORMED GROUND RUN AND NO LEAKS NOTED.SDR P5CA2014090700038Unknown · unknownLOW SPEED RTO; 20 KTS FOR A MASTER CAUTION MESSAGE. A/T DISCONNECTED. ENTERED RUNWAY, MESSAGE GONE. BRAKE TEMP & LT; 1.0, TAXI BACK NORMAL T/O BUT SLIGHT VARIANCE IN AIRSPEED. ACFT TRYING TO FLY AT V1. AIRSPEED INDICATION JUMPED DURING CLIMBOUT. INFO NOTSDR P5CA2014081100027Iru · out of alignmentECIAS MESSAGE, FMC AND AUTOTHROTTLE DISCONNECTED BEFORE TAKEOFF, NO PLF MESSAGE NOTED BOTH FMC & IRS SYS; ALL 3 IRU REALIGNED AND FMC LT & RT; GROUND TESTED GOOD. FMC LT & RT SERVO LOOP GROUND TEST ALSO PASSENGER IAW AMM 34-01-00.SDR P5CA2014080500024Ball Screw · nickedDURING NR 5 BALLSCREW LUBRICATION, FOUND A NICK ON NR 5 BALLSCREW. REPLACED NR 5 BALLSCREW ASSY AND OPS CHECK NORMAL IAW AMM 27-51-41.SDR P5CA2014060400018Warning Horn · false activationREJECTED TAKEOFF AT 65 KNOTS DUE TO TAKEOFF WARNING HORN. NO RECORDED FAULT MESSAGES AND NOT RECENT HISTORY; BITE CHECK CARRIED OUT AND SATISFACTORY IAW AMM 31-51-00. TAKEOFF WARNING TEST CARRIED OUT AND SATISFACTORY AMM 31-52-00. FUNCTIONS CHECKED, CONFIG F
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