N855GT
Service difficulty reports · 125
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 = 'N855GT' 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 = 'N855GT' 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 P5CA2026042000020Tire · warning messageTIRE PRESSURE EICAS & STS MSG OCCURRED AFTER T/O. PERFORMED CONDITIONAL INSPECTION ON MLG 11 & 12 AXLE IAW AMM 05-51-25 (1-8) & AMM 32-45-04-206-011, NO DAMAGE NOTED TO RH BODY GEAR. BRAKE SYS TEST PASS. NO LEAKS NOTED. OPS CHK GOOD AT THIS TIME. R & R MLG 11SDR P5CA2026012300014Stringer · crackedCRACK DAMAGE ON THE STRINGER S-5L, AT AFT SIDE OF STA 2360.(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. 2. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-033 REV 1. 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2SDR P5CA2026012000002Stringer · crackedCRACK DAMAGE ON THE STRINGER S-8R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50870 (SRM 53-80-03-2R-2 REV: 47) JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000003Stringer · crackedCRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50869 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000004Stringer · crackedCRACK DAMAGE ON THE STRINGER S-6R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50868 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000005Stringer · crackedCRACK DAMAGE ON THE STRINGER S-5L, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50867 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000006Stringer · crackedCRACK DAMAGE ON THE STRINGER S-2L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50876 (SRM 53-60-03-2R-8 REV: 47) AND EI T2026A53M-087 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000007Stringer · crackedCRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2360. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 50872 (SRM 53-80-03-2R-3 REV 47). INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO:SDR P5CA2026012000008String · crackedCRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S 50877 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2026012000009Stringer · crackedCRACK DAMAGE ON THE STRINGER S-7L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50878 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2026012000010Stringer · crackedCRACK DAMAGE ON THE STRINGER S-9L, AT STA 930. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 60010 (SRM 53-20-03-2R-1 REV 47) AND EI NO: T2026A53M-050 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 SDR P5CA2026012000011Stringer Splice · crackedCRACK DAMAGE ON THE STRINGER AND STRINGER SPLICES S-10R, AT FWD AND FWD SIDE OF STA 2180. REPAIR DAMAGE AREA IAW W/S NO: 50871 (SRM 53-60-03-2R-3 REV: 47) AND EI NO: T2026A53M-076 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2026012000012Stringer · crackedCRACK DAMAGE ON THE STRINGER S-3L, AT AFT SIDE OF STA 2360.(<P>1. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-034 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2026012000013Battery Pack · no testFOUND EXTERIOR EMER LT (L6690) INOP. PERFORM WIRING CONTINUITY CHECK AND SYSTEM TROUBLESHOOTING IAW WDM 33-51-72 REV 35, FOUND M5168 BATTERY FUNCTION FAILED. PERFORM BATTERY REPLACEMENT AT M5168 IAW AMM 33-51-04-900-803 REV 49. CONDITION CHECK NORMAL AND PERSDR P5CA2025041600013Shear Tie · damagedFUSELAGE SECTION 46 - FUSELAGE SKIN (P/N: 146U3867-5) - PUNCTURE BETWEEN STA 2000 AND S38L TO S39L - CATEGORY B REPAIR.(<P>SHEAR TIE REPLACED AS PER SRM 51-10-02. NEW SHEAR TIE HOLES TRANSFERRED AS PER SRM 51-40-05. NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02.SDR P5CA2025041900014Web · crackedEMP - RH HORIZONTAL STAB TIP FAIRING I/B CLOSURE WEB, FOUND CRACK.(<P>CRACK - WEB REPLACED AS PER SRM 51-10-01. NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100015Skin · damaged#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042100016Skin · damaged#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100017Skin · damaged#20 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100018Skin · damaged#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042100019Skin · damaged#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042100020Skin · damaged#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042200021Beam · crackedLHW NO.11 K-FLAP AT WS 569 D-BEAM LWR ATT BOLT AREA, FOUND CRACK.(<P>CRACK AREA REPAIRED AS PER RI NO: RI-57-41-17558 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042200022Channel · crackedLH HORIZONTAL STAB TIP T/E FAIRING FWD U CHANNEL CRACK.(<P>U CHANNEL REPLACED AS PER RI NO: RI-55-10-17562 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300023Seat Track · damagedM/D STA 1510, 1530, 1550 LBL 11 SEAT TRACK SLOT HOLE ELONGATED.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-9 REPAIR 9 FIG 201 AND RI NO: RI-53-65-17570 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300024Web · crackedEMP - RH HORIZONTAL STAB TIP FAIRING CLOSURE WEB LWR CHORD CRACK.(<P>LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300025Rib · crackedEMP - RH HORIZONTAL STAB TIP FAIRING INTERNAL AREA MOST AFT RIB, FOUND CRACK.(<P>RIB REPLACED AS PER SRM 51-10-02. NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW RIB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2025042300026Beam · crackedRHW I/B L/E D-BEAM AT I/B PDU AREA O/B FOUND CRACK ILES 520.(<P>CRACK AREA REPAIRED AS PER RI-57-41-17559 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300027Support Beam · damagedRHW ILE 450 I/B SUPPORT BEAM UPPER FTG FOUND HOLE ELONGATED.(<P>SUPPORT BEAM REPAIRED AS PER SRM 57-41-09-2R-2 REPAIR 2 FIG 203 DETAIL IV AND RI-57-41-17586 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2025042300028Skin · damaged#21 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2024110800048Pcb · failedREJECTED TAKE OFF @ 110 KNOTS MASTER WARING ON EICAS.(<P>REMOVED & REPLACED MAWEA PRINTED CIRCUIT CARD (MASTER MONITORS) AMM 31-51-02/401, HIGH ENERGEY STOP INSPECTION C/W IAW AMM 05-51-10-202-001</P>)SDR P5CA2024072100015Warning Message · false activationLOW AIRSPEED REJECT DUE TO "CONFIG SPOILER" AT 40 KTS(<P>CMC SHOWED NO EXISTING FAULT. PERFORMED SPOILER TEST AND T/O CONFIG GND TEST, TEST PASSED. NO MAINT MSG IAW 27-61-00/501 AND 31-52-00/501. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER AMM 05-51-10.</P>)SDR P5CA2024061500014Actuator · faultedSPEED BRAKE HANDLE POPPED UP DURING TAKEOFF ROLL. LOW SPEED. TAKEOFF CONFIG WARNING APPEARED. AUTOSPOILER SYSTEM DEACTIVATED. R & R ACTUATOR IAW AMM 27-62-00, OPS CHECKED GOOD.SDR P5CA2023052000027Switch · unknownRTO AT APPROXIMATELY 140 KTS DUE TO "CONFIG SPOILERS" WARNING MSG AND SIREN. GROSS T/O WT 442.0(<P>PERFORMED HIGH ENERGY STOP INSPECTION IAW B747 AMM 05-51-10, NO DEFECTS NOTED. SPEEDBRAKE HANDLE SWITCH REPLACED IAW AMM 27-62-10, OPS CHECK GOOD. </P>)SDR P5CA2023041300008Unknown · unknownRH WING NO.21 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER <SPAN>CMM 57-55-42</SPAN></P>)SDR P5CA2023041300009Unknown · unknownRH WING NO.19 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER <SPAN>CMM 57-55-42</SPAN></P>)SDR P5CA2023041300010Unknown · unknownRH WING NO.20 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P>REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42</P>)SDR P5CA2023041700011Unknown · unknownSB 747-57-2369, NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(<P><SPAN>SB 747-57-2369, </SPAN><SPAN>NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16190 REV A</SPANSDR P5CA2023041700012Unknown · unknownSB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(<P>SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16189 REV.A </P>)SDR P5CA2023041800013Unknown · unknownAPU COMPARTMENT LH STA 2664.19 FRAME FOUND CRACKED (AT ELECTRICAL CABLE ATT BRACKET AREA).(<P>APU COMPARTMENT LH STA 2664.19 FRAME WL 305 CRACK AREA REPAIRED IAW RI-53-82-16186 REV.A. </P>)SDR P5CA2023041800014Unknown · unknownLHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 FOUND WORN.(<P><SPAN>LHW O/B REFUEL PNL 521</SPAN>CB FWD HINGE P/N: 116U4152-5 WORN AREA TIME-LIMIT REPAIRED IAW RI-52-00-16187 REV.A.</P>)SDR P5CA2023041900015Unknown · unknownL/H WING I/B L/E CAVITY NO.7 V LINK (COUNT FROM I/B) UPPER BRACKET FOUND ELONGATED.(<P>LHW ILES 442.84 RIB SUPPORT BEAM ATTACHMENT FLANGE FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-57-00-16173 REV.A.</P>)SDR P5CA2023042300017Rod · unknownRHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED.(<P>RHW REFUEL PANEL I/B ROD CLEVIS PN: <SPAN>116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16197 REV.A</SPAN></P>)SDR P5CA2023042300018Rod · unknownLHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED(<P><SPAN>LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16199 REV A</SPAN></P>)SDR P5CA2023042300019Rod · unknownLHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FOUND ELONGATED.(<P>LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FABRICATED AND REPLACED IAW RI-52-49-16198 REV.A</P>)SDR P5CA2023042400020Unknown · unknownRH WING NO.18 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(<P><SPAN>REPAIRED WITH ADHESIVE PASTE AS PER </SPAN><SPAN>CMM 57-55-42</SPAN></P>)SDR P5CA2023042400021Unknown · unknownRH HORI. STAB. TIP FAIRING AFT WEDGE U CHANNEL FOUND CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16183 REV.A</P>)SDR P5CA2023042400022Unknown · unknownLH HORI. STAB. TIP FAIRING AFT WEDGE U CHANNEL FOUND CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16182 REV.A</P>)SDR P5CA2023032600006Unknown · unknownLOGPAGE 1669079 ITEM 6, AIRCRAFT WAS STRUCK BY A CARGO CONTAINER @ APPROX STATION STRINGER 44 AFT OF CARGO DOOR(<P>LOGPAGE 1669079 M6: EVALUATING DAMAGE AT STA 2100 TO STA 2120 STR 44 AFT OF BULKHEAD CARGO DOOR; REMOVED "BKND-OUT" GOUGE AT FUSELAGE AND ELEVATESDR P5CA2022051200111Detector · inoperativeMAIN CARGO SMOKE DETECTOR MID 11 INOP(PLACED ON MDR 165471 IAW MEL 26-14-01-04A, CAT C.REMOVED AND REPLACED MAIN DECK MID SMOKE DETECTOR #11 IAW AMM 26-14-01/401. OPS CHECK NORMAL. THIS CLEARS MDDR 165471.)
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