N438GT

Service difficulty reports · 22

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 = 'N438GT' 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.

SDR UIEA2026091100873Stiffener · corrodedCORRODED STRUCTURE, LT HORIZONTAL STAB INTERNAL ELEV STA 256.82 AREA. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 107. FABRICATED NEW PARTS IAW EI T2026A55M-1790, REV 1, & WS 60655. INSTALLED FABRICATED PARTS IAW SRM 51-40-02-0G-0, REV 107, & DWG 65B0Sep 11, 2026 · N438GT · Boeing 747409F · Elevator Miscellaneous StructureSDR UIEA2026091100872Angle · corrodedFOUND M/D CARGO FLOOR STRUCTURE CORRODED AT BS 2280, RBL 55. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0, REV 107. FABRICATED NEW PART IAW WS 60678. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0, REV 107, AND DWG 146U3482, SH 3, REV B. JOB COMPLETED AND COSep 11, 2026 · N438GT · Boeing 747409F · Fuselage Miscellaneous StructureSDR UIEA2026091100871Retainer · corrodedCORRODED RETAINER, RT BODY L/G WW INBD DOOR OUTBD EDGE. REMOVED CORROSION RETAINER IAW SRM 51-40-02-0G-0, REV 107. INSTALLED NEW PART IAW DWG 65B10920, SH 3, REV B, AND SRM 51-40-02-0G-0 REV 107. JOB COMPLETED AND CONDITION CHKD NORMAL.Sep 11, 2026 · N438GT · Boeing 747409F · Landing Gear DoorsSDR UIEA2026091100870Retainer · corrodedCORRODED RETAINER, LT BODY L/G W/W INBD DOOR. REMOVED CORROSION RETAINER IAW SRM 51-40-02-0G-0, REV 107. INSTALLED NEW RETAINER IAW DWG 65B10920 SH 3 REV B AND SRM 51-40-02-0G-0 REV 107. JOB COMPLETED AND CONDITION CHKD NORMAL.Sep 11, 2026 · N438GT · Boeing 747409F · Landing Gear DoorsSDR UIEA2026091100869Web · corrodedCORRODED WEB LT HORIZONTAL STAB INTERNAL ELEV STA 381.8. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 107. FABRICATED PART IAW EGAT W/S 60656. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 107 AND DWG 65B03682 SH 2 REV C. JOB COMPLETED AND CONDITSep 11, 2026 · N438GT · Boeing 747409F · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2026091100868Skin · dentedDENTED SKIN, LT WING INBD MID FLAP LWR SKIN. PERFORMED PERMANENT REPAIR OF LT WING INBD MID FLAP LOWER SKIN AT WBL 335.55 IAW SRM 57-53-01-2R-1 REV 107, SRM 51-70-10-2R-2 REV 107 & SRM 51-70-10-2R-0 REV 107. CONDITION CHKD SATISFACTORY.Sep 11, 2026 · N438GT · Boeing 747409F · Trailing Edge FlapsSDR UIEA2026091100867Skin · dentedDENTED SKIN, LT WING INBD MID FLAP LWR SKIN INBD SIDE. PERFORMED PERMANENT REPAIR OF DENT DAMAGE ON THE OUTER SKIN OF LT WING INBD MID FLAP LOWER INBD PANEL ASSY AT WBL 295 IAW EGAT EI T2026A57M-1808 REV 1. CONDITION CHECK IS SATISFACTORY.Sep 11, 2026 · N438GT · Boeing 747409F · Wing, Plate/SkinSDR UIEA2026091100866Skin · debondedDEBONDED SKIN, LT WING INBD AILERON EXTERNAL LWR SKIN. REMOVED THE DISBONDED MATERIAL & CLEANED THE AREA. MEASURED THE DAMAGED AREA (L= 3", W= 1", 2" & FROM T/E, 28" FROM THE OTBD EDGE LWR SKIN, WITHOUT CORE DAMAGE). BONDED THE REPAIR PLIES WITH RESIN, CURESep 11, 2026 · N438GT · Boeing 747409F · Wing, Plate/SkinSDR UIEA2026091100865Rib · crackedCRACK DAMAGE ON THE RIB OF LT WING FIXED L.E. AT ILES 756.95. REPAIRED THE CRACKED AREA IAW EI T2026A57M-1712 REV 1. 2. CONDITION CHKD NORMAL AND JOB COMPLETED.Sep 11, 2026 · N438GT · Boeing 747409F · Wing, Rib/BulkheadSDR UIEA2026072200638Engine · malfunctionedNR 2 ENGINE FAILED TO SPOOL ABOVE IDLE WHEN T/O THRUST SET. RESPONDS SLOWLY TO THRUST LEVER INPUTS. PERFORMED MPA RUNS ON NR 2 ENGINE, NO FAULTS NOTED. PERFORMED HIGH-ENERGY STOP CONDITIONAL INSP IAW AMM 05-51-10. NO FAULTS NOTED.Jul 22, 2026 · N438GT · Boeing 747409F · Engine Fuel and ControlSDR UIEA2025081101119Torque Box · corrodedAFT CARGO COMPT TORQUE BOX PANEL AT STA 1840 TO STA 1860 RBL 6 TO RBL 23 FOUND WITH SURFACE CORROSION(<P>WEB REMOVED AND REPLACED AS PER BOEING DWG 65B06314. NO FURTHER DEFECTS NOTED.</P>)Aug 19, 2025 · N438GT · Boeing 747409F · Fuselage Main, StructureSDR UIEA2025081601126Bulb · inoperativeEMER SLIDE LIGHT L01533 FOUND LIGHT FUSED.(<P>EMER SLIDE LIGHT LAMPS (2EA) REMOVED AND REPLACED AND OPS TEST CARRIED OUT AS PER B747 AMM 33-51-10-962-001 REV 114, FOUND SATIS.</P>)Aug 19, 2025 · N438GT · Boeing 747409F · Emergency LightingSDR UIEA2025081601127Battery · no testREF TO TASKCARD 33-050-01-01, FOUND EMER LIGHT AT SLIDE LIGHT L1533 AND EXIT SIGN NOT ILLUMINATED.(<P>EMER BATT ASSY M1969 REMOVED AS PER B747 AMM 33-51-04-002-009-001 REV 114 AND REPLACED AS PER B747 AMM 33-51-04-402-012-001 REV 114 AND OPS TEST CARRIED OUT. Aug 19, 2025 · N438GT · Boeing 747409F · Emergency LightingSDR UIEA2025081801129Floorbeam · corrodedMAIN DECK COMPT AFTER ADDITION FLOOR PANELS OPEN UP FOR REPAIR LH STA 988 LBL 77 TO 90 FLOOR BEAM UPPER CHORD FOUND CORROSION(<P>MAIN DECK COMPT LH STA 988 LBL 77 TO 90 DAMAGED FLOOR BEAM UPPER CHORD REPAIRED, COMPLIED AS PER B747-400F SRM 53-00-51 REPAIR 3 REAug 19, 2025 · N438GT · Boeing 747409F · Fuselage Main, Floor BeamSDR UIEA2025081801130Spar · crackedRHW I/B T/E REAR SPAR UPPER CHORD AT WS 540 AREA FOUND CRACKED(<P>CRACKED AT RHW I/B T/E REAR SPAR UPPER CHORD AT WS 540 AREA REPAIRED AS PER EN #3398-25 REV 0 REPAIR CATEGORIZED AS €ŒCATEGORY A€? PERMANENT REPAIR AND REPAIR CLASSIFIED AS €ŒMAJOR REPAIR€? Aug 19, 2025 · N438GT · Boeing 747409F · Wing SparSDR UIEA2025081801131Support Angle · corrodedAFT CARGO COMPT SUPPORT ANGLE AT STA 1900 LBL 6 & RBL 6 FOUND CORRODED(<P>AFT CARGO COMPT SUPPORT ANGLE AT STA 1900 LBL 6 & RBL 6 FOUND CORROSION OUT OF LIMIT AND REPAIRED CARRIED OUT AS PER B747-400F SRM 53-60-07-2R-6 REPAIR 6 REV 104 & EN# 3459-25 REV 0. NOAug 19, 2025 · N438GT · Boeing 747409F · Fuselage Miscellaneous StructureSDR UIEA2025033100419Smoke Detector · false activationDURING CRUSE FLIGHT, A FIRE MAIN DECK AFT EICAS MESSAGE ILLUMINATED. CREW RETURNED N438GT TO ANC.<BR>(<P>EFFECTED SMOKE DETECTORS 11 AND 12 FOR ZONE 12 LOOP A AND ZONE 11 LOOP A WERE REMOVED, CLEANED AND REINSTALLED. OPERATION TEST AND SYSTEM TEST WERE PERFORMMar 31, 2025 · N438GT · Boeing 747409F · Smoke DetectionSDR UIEA2025033000416Fire Detector · false activationDURING FLIGHT, CREW INDICATED FIRE MAIN DECK AFT EICAS MESSAGE. CREW RETURNED TO ANC FOLLOWING EVENT.(<P>REPLACED THE MAIN DECK ZONE 12 LOOP A DETECTOR IAW AMM 26-14-01. OPS CHECK GOOD. TEST PASSED MESSAGE CLEARED.Mar 30, 2025 · N438GT · Boeing 747409F · Fire DetectionSDR UIEA2025012300104Fire Warning · false activationMAIN DECK FIRE INDICATION AND EICAS MSG IN FLIGHT (TRANSPORTING FRESH FLOWERS). NO FIRE ON BOARD.(<P>MDC DET EXCESSIVE MOISTURE EXPELLED. MSG NO LONGER ACTIVE. MSG ERASED IAW AMM 26-13-01. NO FURTHER DEFECTS NOTED.</P>)Jan 23, 2025 · N438GT · Boeing 747409F · Fire DetectionSDR UIEA2025011500064Fire Warning · false activationANC TOWER ALERTED CREW OF ENG 3 FIRE. CREW REPORTED NO FIRE OR OVERHEAT INDICATION. AHM DID NOT REPORT FIRE OR OVERHEAT CONDITION. A/C RETURNED TO BLOCKS.(<P>PERFORMED OPEN COWL GVI OF ENG 3 & ENG 4. NO DEFECTS NOTED. ACCOMPLISHED ENG FIRE INSPECTION PER 72-0Jan 16, 2025 · N438GT · Boeing 747409F · Fire DetectionSDR UIEA2024082100841Actuator · leakingFUEL IMBALANCE 2-3 EICAS, LE L4 FLAP DRIVE MESSAGE. FOR FUEL IMBALANCE FOLLOWED QRH TO MONITOR FOR ENG FUEL LEAK.(<P>PERFORMED #2 & #3 FUEL LEAK CHK INTERNALLY / EXTERNALLY AND NO LEAK FOUND PER AMM 28-22-07. R/R #2 CROSSFEED VALVE ACTUATOR THEN OPS & LEAK CHEAug 21, 2024 · N438GT · Boeing 747409F · Fuel Transfer ValveSDR UIEA2024072300731Circuit Card · faultedENG 4 FIRE LOOP A & B INOP. WORK DONE PER AMM 26-10-01 & 26-11-00. INSTALLED NEW CIRCUIT CARD FOR ENG 4 OVHT DET LP A POSITION A19, ENG 4 FIRE DET LP A POSITION A16, ENG 4 FIRE DET LP B POSITION A17 & ENG 4 OVHT DET LP B POSITION A20. PERFORMED GROUND TEST IAJul 22, 2024 · N438GT · Boeing 747409F · Fire Detection
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