N649GT
Service difficulty reports · 574
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 = 'N649GT' 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 = 'N649GT' 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 UIEA2026102300995Battery · inoperativeEMERGENCY FLASHLIGHT NEXT TO LAV LED NOT FLASHING. R & R FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECK GOOD.</P>)SDR UIEA2026101500987Limit Switch · failedREJECTED T/O AT 60KTS DUE TO EICAS MESSAGE. UNSCHEDULED STAB TRIM MESSAGE ALSO APPEARED TWICE DURING TAXI OUT(<P>RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR EXPERIENCED AN INTERNAL SHORT. R&R R/H STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER MODULE PER ASDR UIEA2026100900972Failsafe · damagedDETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DEFECT SIGNAL LOCATION: FAILSAFE STRAP (RH)(<P>REMOVED PLATE ASSY OF R/H MAIN L/G W/W LONGN AND L/G BESDR UIEA2026100900973Skin · crackedDURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATION WAS FOUND AT THE FAIL-SAFE STRAP, AND CORROSION WAS FOUND ON THE T-FITTING AND SKIN PANEL (P/N 145T3321-4 ) NEAR STR 22AR. REMAINING THICKSDR UIEA2026100900974Tee Fitting · crackedDURING EO 6753A070 PART 4 (SB 767-53A0100 R3 / AD 2012-09-04 TERMINATING ACTION) AT STA 955 R/H, CRACKS WERE FOUND AT THE 10 O'CLOCK (0.5€?) AND 4 O'CLOCK (NOT MEASURABLE) POSITIONS FROM THE LOWEST FAIL-SAFE STRAP HOLE PER 767 NDTM 51-00-16 / 51-00-19.(<P>STRSDR UIEA2026100900975Skin · corrodedCORROSION FOUND ON R/H INBOARD MAIN FLAP LOWER SKIN (DAMAGE SIZE: L=11.2", W=1.7")(<P>REPAIRED THE R/H INBD MAIN FLAP LOWER PANEL (P/N 113T2243-2) SKIN IN ACCORDANCE WITH BMN SP1-TLS-26-0036, WHICH WAS APPROVED BY FAA FORM 8100-9 DATED 08OCT2026. NO FURTHER DESDR UIEA2026100900976Structure · corrodedCORROSION FOUND ON L/H INBOARD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=19")(<P>PER BOEING RDR SP1-TLS-26-0037-05B, INSTALLATION OF CHORD (P/N 113T2225-401) ON THE FLAP (P/N 113T2201-23A) FOR AIRCRAFT N649GT HAS BEEN APPROVED AS STRUCTURALLY ACCEPTABLE. REMOVED LSDR UIEA2026100900977Flap · damagedCORROSION FOUND ON RT INBD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=12") REMOVED RT INBD MAIN FLAP LOWER CHORD AND REPLACED WITH NEW CHORD PER SRM 51-40-02. HOLE COPIED PER SRM 51-40-05. NUT-PLATES INSTALLED PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR UIEA2026100900978Skin · corrodedL/H WING LEADING EDGE NR 1 SLAT SKIN, FOUND DENSE CORE CORROSION (DAMAGE SIZE: L = 2.5", W=5.4") REPAIRED LT WING LEADING EDGE NR 1 SLAT SKIN IAW SRM 51-70-10 AND BMN SP1-TLS-26-0028. NO FURTHER DEFECTS NOTED.SDR UIEA2026072800658Seal · brokenGALLEY ELT TAMPER TAPE BROKEN. REMOVED AND REPLACED GALLEY ELT IAW AMM 25-63-03. OPS CHK OK.SDR UIEA2026060900455Circuit Card · faultedRAT DEPLOYED RIGHT AFTER ROTATION ON TAKE-OFF. GREEN PRESSURE LIGHT ILLUMINATED(<P>REMOVED AND REPLACED LH ENG SPEED CARD & STOWED RAT PER AMM 73-21-54. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026060300430Oxygen Mask · inoperativeCENTER SUPERNUMERARY SEAT O2 MASK INOPERATIVE. REMOVED AND REPLACED CENTER SUPERNUMERARY O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD. NO LEAKS NOTED.SDR UIEA2026060100424Stowage Box · no testCAPTAIN SIDE O2 MASK AUDIO INTERCOM WILL NOT TEST. R & R CAPT SIDE O2 MASK STOWAGE IAW AMM 35-11-51 AND IPC 35-11-52-15. OPS CHECK GOOD. NO DEFECTS NOTED.SDR UIEA2026052600364Tag · brokenFLIGHT DECK ELT RH DO NOT REMOVE TAG BROKEN (PORTABLE ELT)(<P>REMOVED AND REPLACED FLIGHT DECK RH PORTABLE ELT IAW B767 AMM 25-63-03 & AIPC 25-63-52-97 AND EO 6725A129. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051800341Window · noisyLOUD WHISTLING NOISES ON BOTTOM OF L1 WINDOW. PER CREW DEBRIEF, ACTUAL WINDOW IS L2 ( SLIDING WINDOW ). CLEANED AND INSPECTED L2 WINDOW AERODYNAMIC ALONG WITH L1 WINDOW IAW AMM 12-16-02 AND 56-11-00 W/ NO DEFECTS NOTED. ALSO CLEANED AND INSPECTED L2 BULB SEALSDR UIEA2026040500127Fan · vibrationDURING CLIMB, RIGHT ENGINE FAN VIBRATION REACHED 4.3. DURING CRUISE, VIB 0.8. PERFORMED BLADE LUBE PER AMM 72-31-02. SPINNER RE-TORQUED PER AMM 72-31-01. TRIM BALANCE AND VIBRATION SURVEY PER AMM 72-31-00. #1 BEARING CHECKS GOOD. N2 VIBE AT POWER 2.0, FAN VISDR UIEA2026032700110Handle · out of adjustEMERGENCY WINDOW OUTSIDE HANDLE POPS OUT. ADJUSTED SPRING LOADED BALL LATCH OF WINDOW R2 EXTERIOR EMERGENCY ESCAPE HANDLE IAW AMM 56-11-04. OPS CHK GOOD AT THIS TIME.SDR UIEA2025111801297Lanyard · unsecureELT BY LAVATORY HAS STRING HANGING. SECURED THE ELT STRING IAW AMM 25-63-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.SDR UIEA2025102401278Skin · damagedAIRCRAFT STRUCK BY LIGHTNING. LIGHTNING STRIKE DAMAGE FOUND ON R/H INLET COWL 3:00 POSITION(<P>PERFORMED PHASE 1 LIGHTNING STRIKE INSPECTION IAW B767 AMM 05-51. R/H ENGINE COWL DAMAGE FOUND WITHIN LIMITS IAW SRM 54-15-01-1A-1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025100401256Hf Comm · abnormalBOTH HF COMM RADIO INOP AND SELCAL INOP(<P>T/S WITH FIM 23-11 FT 804. RESECURED CONNECTIONS AT HF ANTENNA. OPS CHK GOOD PER AMM 23-11-00</P>)SDR UIEA2025092601246Cover · detachedEMERGENCY EXIT LIGHT COVER FELL OFF L1 DOOR. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03. NO FURTHER DEFECTS NOTED.SDR UIEA2025071400949Bracket · damagedFLIGHT DECK FIRE EXTINGUISHER HOLDING BRACKET INOPERATIVE. RE-ADJUSTED FLIGHT DECK FIRE EXTINGUISHING BRACKET IAW B767 AMM 26-26-02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR UIEA2025062100789Latch · out of adjustON LANDING, FO WINDOW NR 2 EXTERNAL EMERGENCY ESCAPE HANDLE UNLATCHING. ADJUSTED FO WINDOW #2 EMERGENCY ESCAPE HANDLE LATCH & PERFORMED SYSTEM OPS CHECK OF EXTERNAL ESCAPE HANDLE IAW AMM 56-11-04. OPS CHECK GOOD AT THIS TIME. NO OTHER DEFECTS NOTED.SDR UIEA2025052900705Skin · crackedSERVICE DOOR CUTOUT, AFT LOWER CORNER FUSELAGE FOUND CRACKS INDICATION, ON OPEN HOLES: #4, POSITION 8 O'CLOCK (SKIN AND BEAR STRAP) APPROX AND HOLE #5, POSITION 8 O'CLOCK (SKIN) AND 2 O'CLOCK (BEAR STRAP) APPROX.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 RSDR UIEA2025052900706Bear Strap · crackedFORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE #5: 1. ON SKIN AT 3 O´CLOCK POSITION. 2. ON BEAR STRAP AT 9 O´CLOCK POSITION.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 FIGURE 201 DETAIL III. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300722Skin · dentedLH WING, SPOILER #3, LOWER SURFACE, DENT AT 10.5" FROM AFT EDGE AND 6" FROM OUTBD EDGE.(<P>AFFECTED AREA WAS REPAIRED IN ACCORDANCE WITH B767 SRM 57-70-01-2R-1 PAG 2-5 FIG 201 SHEET 4 AND SRM 51-70-03-0G-0 PAR 5. L FIG 16. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300723Wedge · damagedLH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEESDR UIEA2025060300724Bushing · corrodedFRETTING CORROSION ON BUSHING P/N BACB28X20E085 INSTALLED IN THE FWD SHEAR PIN HOLE OF THE FWD ENGINE MOUNT (P/N 311T2211-7), RH SIDE.(<P>BUSHING WAS REPLACED (P/N BACB28X20E085) PER DWG 311T2211-7 ID SHEET 1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300725Fuel Tank · leakingFUEL LEAK AT CENTER TANK BETWEEN STGR L-6 AND LBL 97.5.(<P>THE SEALANT IN THE FUEL TANK STRUCTURE WAS REPAIRED PER AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300726Wedge · damagedLH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG.201 SHEETSDR UIEA2025060300728Wedge · damagedLH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEETSDR UIEA2025060700735Skin · corrodedRH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION.(<P>RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION LEVEL 2 WAS REPAIRED IAW CMA-TLS-25-0045. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060700736Skin · corrodedRH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION AROUND FASTENERS. L= 6.0 IN W=1.5 IN.(<P>RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION LEVEL 2 AROUND FASTSDR UIEA2025031700353Evas Unit · inoperativeDURING EVAS OPS CHECK, FOUND CAPTAINS EVAS INOP (BLOWER INOP)(<P>REMOVED & REPLACED EVAS CAPTAINS SIDE AS PER B-767-300 AMM 25-60-99. OPS CHECK GOOD.</P>)SDR UIEA2025031200260Skin · no discrepancyLIGHTNING STRIKE AT 17000 FT. SUSPECT STRIKE IMPACT ON CAPTAIN'S SIDE IN THE VICINITY OF THE NOSE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE PHASE INSPECTION IAW B767 AMM 05-51-19. FOUND LIGHTNING IMPACT AND POSSIBLE EXIT POINT AT 2 TO 3 O'CLOCK POSITION BETWEEN STSDR UIEA2025021200132Wire Harness · damagedAIR TURN BACK DUE TO APU SHUTDOWN IN FLIGHT. LEFT GENERATOR ON MEL SO APU IS REQUIRED. APU RESTARTED ON 3RD ATTEMPT.(<P>PER ENGINEERING AND MANAGEMENT REQUEST, R/R APU HARNESS WIRE PN: W020-212R-24 IAW WDM 49-14-11-1 AND SWPM 20-25-00 AND SWPM 20-60-00. DUE TOSDR UIEA2024122901187Transcowl · damagedLH ENG T/REV WIRE MESH DAMAGED AT 0700 O'CLOCK POSITION. C/W EO 6778A019 REV 5 PART 1 INTERIM REPAIR. C/W PART 2 PERMANENT REPAIR AT NEXT A-CHECK.(<P>REMOVED TRANSLATING COWL FROM L/H THRUST REVERSER OUTBOARD HALF IAW AMM 78-31-10. OK TO INSTALL TRANSLATING COSDR UIEA2024122901188Radome · erodedFWD FUSELAGE RADOME SURFACE, FOUND SEVERAL AREAS OF EROSION.(<P>INSPECTED SURFACE DEFECT AT NOSE RADOME. FOUND EVIDENCE OF PEELING PAINT IAW B767 AMM 53-12-01 CLEANED AND PAINTED AREA IAW B767 AMM 53-12-01</P>)SDR UIEA2024122901189Oxygen Mask · contaminatedLAV PORTABLE OXYGEN MASK CONTAMINATED.(<P>REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS REQUIRED PER 767 AMM 35-31-01. OPS CHK GOOD.</P>)SDR UIEA2024122901190Panel · loose#2 ENGINE I/B CORECOWL HINGES DAMAGED, DIFFICULT TO OPEN AND CLOSE. REQUIRES EVALUATION.(<P>EVALUATED AND FOUND SKIRT PANEL WITH LOOSE AND MISSING FASTENERS. LOCATED AND INSTALLED NEW FASTENERS IAW SRM 51-40-02-06. OPS CHECK GOOD.</P>)SDR UIEA2024122901191Cdu · inoperativeLEFT T/R INOP.(<P>REMOVED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OK TO INSTALL. INSTALLED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OPS CHECK GOOD.</P>)SDR UIEA2024120301158Switch · faultedUNSCHEDULED STAB TRIM MSG ON DECENT. CLEARED SHORTLY AFTER.(<P>R/R STAB TRIM LIMIT SWITCH MODULE ASSY IAW AMM 27-48-01. OPS CHECK GOOD NO DEFECTS NOTED. PERFORMED MCDP GROUND TEST 40, 65 AND 66. ALL TEST GOOD, NO DEFECTS NOTED. PARTS EFECTIVE PER IPC 27-48-01-SDR UIEA2024111301085Elt · inoperativeREF W/O 138840, DURING OPS CHECK OF FIXED ELT FOUND TO BE INOPERATIVE.(<P>R/R FIXED ELT PER EO OT-23-0084. OPS CHECK GOOD. DMI 220446 CLOSED</P>)SDR UIEA2024082300843Skin · damagedRH OTBD AILERON TRAILING EDGE LIGHTNING STRIKE(<P>TRANSFER TO NON-MEL DMI 215328 DUE DATE 27AUG24.</P> / <P>LP 1872886 M1: C/W PART 3 PERMANENT REPAIR PER ATLAS EA 6757A156- CS REV 0. NON-MEL DMI 215328 CLOSEDSDR UIEA2024080200776Indication Sys · faultedAFTER LANDING O2 BOTTLE INDICATES 40 PSI. CONFIRMED EICAS IND INOP. REF DMI 213995 PER MEL 35-11-02-01 CAT B DUE DATE 8AUG24. MMP PERFORMED. BOTTLE #1 1400 PSI, BOTTLE #2 1300 PSI, AVERAGE 1600 PSI. R/R VOLT AVG UNIT PER AMM 35-11-06. OPS CHECK GOOD.SDR UIEA2024072600753Averaging Unit · faultedON GROUND OXYGEN PRESSURE SHOWS 40 PSI.(<P>R/R AVERAGING UNIT IAW AMM 35-11-06. OPS & LEAK CHECK GOOD. DMI 213524 CLOSED.</P>)SDR UIEA2024040800267Shroud · damagedL1 DOOR EMERGENCY ESCAPE ROPE SHROUD DAMAGED.(<P>PERFORMED TIME LIMITED REPAIR ON L1 DOOR ESCAPE ROPE RETAINER SHROUD IAW EA 6725A0025. TRANSFER TO NON-MEL DMI 206255 & 206256 DUE DATE 8APR2024. LP 1807206 M2: R/R SHROUD IAW AMM 52-09-01. NO FURTHER DEFECTS NOSDR UIEA2024021700090Elt · unknownDURING OPS CHECK OF FIXED ELT PER W/C # A-23--339-01(<P>TRANSFERRED TO MDDR 203168 PER DDG 25-63-10-02C CAT D DUE 16JUM24. MX ACTIONS C/W, PLACARDS INSTALLED. PRFORMED ELT OPS CHECK PER CAD A-23-999-01, TEST NORMAL. THIS CLEARS DMI 203168, PLACARD REMOVED. </PSDR UIEA2024012400022Sensor · out of toleranceMAIN CARGO DOOR SHOWS OPEN DURING CRUISE. INDICATION WENT OUT DURING DESCENT AT FL 340. "MAIN CARGO DOOR" EICAS MSG.(<P>FOUND MAIN CARGO DOOR LOCKED WARNING SENSOR S892 OUT OF TOLERANCE. RESHIMMED & ADJUSTMENTED SENSOR TO WITHIN LIMITS, DOOR OPS CHECK NORMAL ISDR UIEA2023122201010Computer · unknownRETURN TO BLOCK AFTER LOW SPEED RTO DUE MASTER CAUTION LIGHT AND BEEPER. "AUTOTHROTTLE DISCONNECT" EICAS MSG. SPED WAS AROUND 40KTS.(<P>DEFERRED IAW MEL 22-30-01 DMI 199674 CONDITION INSP IAW AMM 05-51-14 NOT REQUIRED AS RTO WAS BELOW 40 KNOTS.R/R TMC COMPUTER
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