N439GT
Service difficulty reports · 31
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 = 'N439GT' 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 = 'N439GT' 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 UIEA2026091800883Oil Filter · false indicationEICAS MESSAGE ENG 3 OIL FILTER DISPLAYED RAN QRH AND COMPLETED QRH SHUTDOWN ENG 3. PERFORMED FIM TASK 71-00 & TASK A07 PER BLOCK 41. AFTER ENG RUN NO DEBRIS WAS FOUND; CONTINUED IN SERVICE. PERFORMED FIM TASK 79-00 FAULT TREE FIG 103. MSG CLEARED AND NO BLOCKSDR UIEA2026070900585Tire · burstADVISE TIRE DEBRIS LEFT IN PVG. PLANNED ANC LANDING STOP ON RUNWAY. CITY OPS ADVISED 2 TIRES MISSING. PER AMM 32-45-01 & IPC 32-45-03-02. C/W BLOWN TIRES INSPECTION PER AMM 05-51-25-202-009. R & R NR 5, 6, 7, & 8 TORQUE LIMITER PER AMM 32-42-20 REV 116 & IPC SDR UIEA2026042700249Motor · failedTRONG FUMES IN FLIGHT DECK. APPLIED FIM 21-00-10 T/S, FOUND M/D PDU 6 RT ELECTRICAL MOTOR STUCK INOP. PDU 6 RH DEACTIVATED. R & R NR 6R PDU IAW AMM 25-53-01-004-001-004. OPS CHKD OK.SDR UIEA2026021300049Sequence Valve · faultedGEAR WOULD NOT STAY UP WITH THE LANDING GEAR HANDLE IN THE UP POSITION MOVED HANDLE TO THE OFF POSITION WHILE INDICATING UP AND THE GEAR REMAINED UP INSTEAD OF DROPPING. R & R NOSE GEAR SEQUENCE VALVE IAW AMM 32-34-07-004-001, 32-34-07-404-006 & IPC 32-34-07-SDR UIEA2026021500052Sequence Valve · faultedGEAR WOULD NOT STAY UP WITH THE LANDING GEAR HANDLE IN THE UP POSITION. MOVED HANDLE TO THE OFF POSITION WHILE INDICATING UP, AND GEAR REMAINED UP INSTEAD OF DROPPING. R & R NOSE GEAR SEQUENCE VALVE IAW AMM 32-34-07-004-001, 32-34-07-404-006 & IPC 32-34-07-02SDR UIEA2026013000021Trunnion · corrodedLEFT BODY GEAR INBOARD TRUNNION, AIRCRAFT SIDE HAS CORROSION. BLENDED AREA ON LT BODY GEAR INBD TRUNNION. PERFORMED NDT AND DVI INSP. NO DEFECTS NOTED. ACCOMPLISHED FLAP PEEN, APPLIED TREATMENT, PRIMER & TOPCOAT IAW SRM 53-40-90-2R-1, REP 1, PAGE 7. COMPLYESDR UIEA2026013000022Trunnion · gougedGOUGE ON LT NLG TRUNNION BEARING CAP FWD AND AFT I/B CORNER. REPAIRED DAMAGE ON LT NLG TRUNNION BEARING CAP FWD AND AFT INBD CORNERS. IAW BOEING MESSAGE EA C-TLS-26-0002-10B. PERMANENT REPAIR WITH NO ADDITIONAL SUPPLEMENTAL INSPECTIONS. NO FURTHER DEFECTS NOTSDR UIEA2026013000023Trunnion · corrodedCORROSION ON OTBD EDGE OF LT BODY GEAR TRUNNION CAP. BLENDED AREA ON OTBD EDGE OF LT BODY GEAR TRUNNION INBD CAP. PERFORMED NDT AND DVI INSP. NO DEFECTS NOTED. ACCOMPLISHED FLAP PEEN, APPLIED TREATMENT, PRIMER AND TOPCOAT PER 747 SRM 53-40-90-2R-1 REP 1 PG 7SDR UIEA2026013000024Junction Box · corrodedJUNCTION BOX COVER FOR RIGHT HAND BODY GEAR HAS CORROSION ON LOWER EDGE.(<P>REPAIRED AREA OF CORROSION ON RH BODY GEAR LOWER EDGE OF JUNCTION BOX PER SRM 51-70-13-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026013000025Junction Box · corrodedJUNCTION BOX COVER J15, FOR LT BODY GEAR HAS CORROSION ON LOWER EDGE. REPAIRED CORROSION OF THE J15 JUNCTION BOX OF THE LT BODY GEAR IAW SRM 51-70-13-2R-1. NO FURTHER DFECTS NOTED.SDR UIEA2026013000026Trunnion · corrodedCORROSION ON LT NLG TRUNNION BEARING CAP INBD SIDE. BLENDED OUT CORROSION ON THE LT NLG TRUNNION BEARING CAP INBD SIDE FACE AREA, WITHIN LIMITS. TREATED AREA PROTECTIVE FINISH ON BLENDED AREA IAW SRM 53-10-90-2R-1, REPAIR 1, FIG 201, DETAIL II. NO FURTHER DEFSDR UIEA2026013000027Trunnion · corrodedCORROSION ON RT NLG TRUNNION BEARING CAP INBD SIDE. BLENDED OUT CORROSION ON THE RT NLG TRUNNION BEARING CAP INBD SIDE IAW SRM 51-10-90-2R-1, FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025121301342Pca · faultedHYD PRESS ENG 1. FOLLOWED FIM 29-11 TASK 803, NO CMS MESSAGE FOUND. R & R HYDIM 1 PCA PER AMM 29-11-42-004-001 & IPC 29-11-42-01B. OPS CHKD GOOD.. PFMD ENG 1 IDLE RUN IAW 71-00-00, OPS CHECK GOOD. NO 30 DAY HISTORY.SDR UIEA2025071900978Engine · damagedENG #3 SEVERE DAMAGE. NO OIL QUANTITY. REMOVED AND REPLACED #3 ENGINE IAW AMM 71-00-02-004-001-J00. PERFORMED ENGINE TEST RUN IAW AMM 71-00-00-700-801-J00 TEST #3. ALL OPS SATISFACTORY AND NO LEAKS OBSERVED. REF W/O 149634.SDR UIEA2025030400205Slide · out of toleranceUPPER DECK COMP- REQUIRE TO REPLACE THE UPP DECK DOOR SLIDE RAFT PACK DUE TO SLIDE RAFT PACK BULKY & TOP COVER CANNOT OPEN OR CLOSE SMOOTHLY(<P>R/R UPPER DECK DOOR SLIDE RAFT PACK IAW AMM 25-68-02 REV 112. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030500206Floor Support · damagedMAIN DECK COMPT - AFTER OPEN UP CTR TANK FLOOR PANEL AT STA 1200 - STA 1220 MOST O/B FLOOR SUPPORT FOUND HOLE ELONGATED. FLOOR SUPPORT REPAIRED AS PER EN #1010-25 REV.0. NO FURTHER DEFECTS NOTED.SDR UIEA2025030500207Rib · crackedRT HORIZONTAL STAB CLOSURE RIB LWR CHORD FOUND CRACKED. LWR CHORD REPAIRED AS PER SRM 55-10-09 REPAIR 13 REV.103. NO FURTHER DEFECTS NOTED.SDR UIEA2025030500208Rib · crackedRH HORIZONTAL STAB CLOSURE RIB WEB FOUND CRACKED NEAR LWR CHORD AREA. WEB REPAIRED AS PER SRM 55-10-09 REPAIR 13 REV.103. NO FURTHER DEFECTS NOTED.SDR UIEA2025030600209Stiffener · crackedDURNG HFEC INSPECTION AT BETWEEN RH STA 320 - 300, WL 130 NOSE WHEEL WELL STIFFENER PER SB 747-53A2465 FOUND CRACK APPROX 1.7" AS MARKED.(<P>STIFFENER REMOVED AND REPLACED AS PER SRM 51-40-02 REV.103 & SB 747-53A2465. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030600210Bulkhead · crackedDURING OPEN HOLE HFEC INSP AT BS 2598 BULKHEAD LH FWD INNER CHORD FOUND 5TH HOLE FROM BOTTOM WITH CRACK INDICATION APPROX 7 O'CLOCK POS LOOK O/B AS MARKED.(<P>REPAIRED AS PER EN #1012-25 REV.0. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025030600211Skin · damagedRH INBD AILERON OTBD EDGE PREVIOUS DAMAGE NOTED. TAP TEST PER SRM 51-10-06-06-0G-2 WITHIN SRM LIMIT 51-70-02-17-0. RE-INSP AT A CHECK AND PERM REPAIR AT C-CHECK.(<P>REPAIRED RH INBD AILERON OTBD EDGE AS PER B747-400F SRM 51-70-17 REV.103. NO FURTHER DEFECTS NOSDR UIEA2025030600212Flap · damagedTRANSFER FROM ADD PAGE 2 OF 11, MDDR 224933 - RH WING VARIABLE CAMBER FLAP PERM REPAIR DUE WITHIN 25FC IAW EA-1957A200.(<P>RH WING VAIABLE CAMBER FLAP PERM REPAIRED AS PER B747-400F SRM 51-70-17 PARA 5B REV.103 & EA 1957A200 PART 3. DMI 224933 CLOSED.</P> / <!SDR UIEA2025030900248Strap · corrodedMAIN DECK COMPT - SIDE CARGO DOOR INNER LOWER STRAP AT FWD & AFT EDGE FOUND CORROSION.(<P>JOB ACCOMPLISHED AS PER EN #1011-25 REV.0 NO FURTHER DEFECTS NOTED. PN 65B17878-1</P>)SDR UIEA2024081900838Pdu · failed2 HR IN CRUISE FLIGHT, LEFT MID SPAN L/E FLAP INDICATED DEPLOYED, "FLAP PRIMARY" MASTER CAUTION. AFTER 5 MIN, FLAPS PRIMARY MASTER CAUTION, FLAP DRIVE CAUTION ANNUNCIATED, COULD NOT RETRACT IN FLIGHT, "LE MULTI DRIVE" STS MSG(<P>R/R L2 L/E SLAT PDU PER AMMSDR UIEA2024080300786Floor Panel · damagedMN DECK FLOOR PANELS JUST FORWARD OF SIDE CARGO DOOR LH HAS MULTIPLE CRACKS AND PUNCTURES.(<P>REFERENCE COBALT WO C1017 FOR SIGN OFFS. FAA FOR 8130-3 105870 FOR REPAIR OF MAIN DECK FLOOR PANEL JUST FWD OF SIDE CARGO DOOR LH SIDE. NO FURTHER DEFECTS NOTED PER SSDR UIEA2024080300785Floor Panel · damagedMN DK FLOOR PANEL LH SIDE AFT OF SIDE CARGO DOOR HAS MULTIPLE PUNCTURES AND CRACKS.(<P>REFERENCE COBALT WO C1016 AND C1018 FOR PROPER SIGN OFF. FAA FORM 8130-3 105871 FOR REPAIR OF MAIN DECK PANELS LH SIDE AFT OF SIDE CARGO DOOR. NO FURTHER DEFECTS NOTED PER SSDR UIEA2024080300784Floor Panel · damagedMN DK FLOOR PANEL LH SIDE AFT OF SIDE CARGO DOOR HAS MULTIPLE PUNCTURES AND CRACKS.(<P>REFERENCE COBALT WO'S C1016 AND C1018 FOR PROPER SIGN OFFS. FAA FOR 8130-3 105868 FOR REPAIR OF MAIN DECK PANEL LH SIDE AFT OF SIDE CARGO DOOR. NO FURTHER DEFECTS PER SRM 53SDR UIEA2024080300783Floor Panel · damagedMAIN DECK CAROG FLOOR PANEL 144U5825-54 AT STA 1200 HAS THREE FASTENER HOLES DAMAGED.(<P>REFERENCE COBALT WO C1022 FOR SIGN-OFFS. FAA FORM 8130-3 106133 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS THREE FASTENER HOLES DAMAGED. NO FURTHER DEFECTS NOTED PER SRSDR UIEA2024080300782Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 144U5825-64 AT STA 1200 HAS ONE FASTENER HOLE DAMAGED.(<P>REFERENCE COBALT WO C1021 FOR PROPER SIGN OFF. FAA FOR 8130-3 #106126 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS FASTENER HOLE DAMAGED. NO FURTHER DEFECTS NOTED PER SRM 53SDR UIEA2024080300781Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 144U5803-32 AT STA 1200 HAS ONE FASTENER HOLE DAMAGED.(<P>REFERENCE COBAL WO C1023 FOR PROPER SIGN OFF. FAA FORM 8130-3 106134 FOR REPAIR OF MAIN DECK CARGO FLOOR PANEL HAS ONE FASTENER HOLE DAMAGED. NO FURTHER DEFECTS NOTED PER SRMSDR UIEA2024122301181Oil Filter · warning messageON TAKEOFF ROLL "ENG 4 OIL FILT" EICAS. LOW SPEED 40 KIAS ABORT.(<P>REPLACED ENG OIL FILTER PER AMM 79-28-08 T/S PER FIM 79-00 FIG 103 NO DEFECTS FOUND. AIRCRAFT OK FOR SERVICE.</P>)
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