N642GT
Service difficulty reports · 622
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 = 'N642GT' 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 = 'N642GT' 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 UIEA2025030800239Skin · corrodedUPPER FUSELAGE SURFACE WITH CORROSION AT THE BASE OF THE TOP TCAS ANNTENA.(<P>UPPER FUSELAGE SURFACE CORROSION AT THE BASE OF THE TOP TCAS ANNTENA. REPAIR WAS PERFORMED IN ACCORDANCE WITH TRE6753716 FEB 24, 2025. FVC TITLE REPAIR- FUSELAGE SKIN- CROWN AREA-CORSDR UIEA2025030800242Transmitter · faultedTRANSMITER POSITION FLAPS M489 LOW INSULATION RESISTANCE.(<P>FLAP POSITION TRANSMITTER M489 WAS REPLACED IAW AMM 27-51-45-422-030 REV 144. FLAP POSITION TRANSMITTER M489 ADJUSTED AND TEST PERFORMED IAW AMM 27-51-45-822-161 REV 144. NO FURTHER DEFECTS NOTED.</PSDR UIEA2025030800245Skin · dentedLOWER HALF OF FUSELAGE, BTW STA 654+44 AND 654+66, BTW STR 34L AND 33L, DENT ON SKIN.(<P>THE DENT WAS EVALUATED AND FOUND OUT OF LIMIT. IT WAS REPAIRED IAW SRM 53-00-01-2R-29 REPAIR 29. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031100258Servo · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN BOTH YAW DAMPER SERVOS.(<P>YAW DAMPER SERVOS LH AND RH WERE REPLACED IAW AMM 22-21-02-414-016 REV 144. (OFF PART RH PN: 1540500-9 SN: 973BC, LH PN: 1536600-5 SN: 1856BA) INSTALLATION TEST WAS SATISFACTORY.SDR UIEA2025031100259Actuator · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN SERVO VALVE.(<P>RUDDER RATIO CHANGER ACTUATOR WAS REPLACED I.A.W AMM 27-21-15-422-024 OPERATONAL TEST WAS PERFORMED AND NO LEAKS FOUND, TORQUE APPLIED 280 LB-IN, 360 LB-IN S/N 0823114404 DATE 12DEC2026.</PSDR UIEA2025031800355Skin · corrodedVERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".(<P>VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".THE VERTICAL STABILIZER LEADING EDGE TIP HAS BEEN REPLACED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025031800356Skin · corrodedVERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A).<BR>(<P>VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A) WAS REPLACED IAW SRM 51-10-02-0G-0 REV. 127 15-DEC-24.SDR UIEA2025032100365Stowage Box · no testDMI 225437 PASSENGER #3 OXIGEN MASK REST SWITCH DOESN'T TEST. SEAT NOT ALLOWED TO BE OCCUPIED.(<P>STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001 REV 144, 22DEC2024 AND TEST WAS SATISFACTORY. NO FOUND LEAKS.</P>)SDR UIEA2025032100366Skin · dentedRH WING, INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WITH DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 SDR UIEA2025032100367Skin · dentedRIGHT WING INBD FLAP UPPER AND LOWER SKIN WITH SEVERAL DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DESDR UIEA2025032100368Skin · delaminatedRH WING, OUTBOARD FLAP, LOWER SURFACE, 9" TO 24" FROM INBOARD EDGE AND 23.5" TO 34" FROM LEADING EDGE, DELAMINATION.(<P>RH WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 PAG 1,4 FIG 201 SHEET 3 REV 127 15-DECSDR UIEA2025032100369Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1646, LH SIDE.(<P> APU FUEL SHROUD LINE WAS REPLACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDI NG TEST 0.5 MILLIHOMS SN: B0005830 DATE: 04-JSDR UIEA2025032100370Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1720.5, LH SIDE.(<P>APU FUEL SHROUD LINE WAS REPL ACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDING TEST 0.5 MILLIHOMS SN B0005830 DATE: 04-JSDR UIEA2025032100371Fuel Line · bentACCESS PANEL 197DL, FUEL LINE BENT.(<P>ACCESS PANEL 197DL, FUEL LINE WAS REPLACED. IAW AMM 28-13-06-404-005. REV 144. DEC 22, 2024. NO MORE ACTIONS REQUIRED. GOOD FOR SERVICE.</P>)SDR UIEA2025032100372Anti-Skid Valve · no testMLG, WHEEL #5, BRAKE UNIT, WHEN TEST WAS BEING PERFORMED, THE RECORDED PRESSURE WAS LOWER THAN PERMITTED.(<P>ANTISKID VALVE OF BRAKE #5 WAS REPLACED. IAW AMM 32-42-03-404-017. REV 144. DEC 22, 2024. TORQUE APPLIED: 105 LB IN. S/N: 0524121903. DATE: 15-MAY-25. SDR UIEA2025032200376Skin · corrodedRH WING INBOARD TE FLAP, CORROSION LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 R1 ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025020500119Oxygen Mask · inoperativePASSENGER #3 OXYGEN MASK INOP.(<P>TRANSFER TO DMI 225437 PER MEL 35-11-03-02A CAT C DUE DATE 15FEB25</P> / <P>LP 1810355 ITEM M10, 21MAR25: STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001. TEST SATISFACTORY, NO FOUND LEAKS. IPC 35-11-52-15 REV 76 22FEB25SDR UIEA2024120301162Seal · damagedRIGHT O/B T/E FLAP WITH SEAL DAMAGED AT INBOARD SIDE.(<P>REMOVED DAMAGED SEAL AT R/H O/B T/E FLAP, I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW SEAL AS REQUIRED AT R/H O/B T/E FLAP, I/B SIDE AREA PER BOEING 767-300 AMM 57-25-01-05 & AMMSDR UIEA2024120301163Latch · brokenENG #2 NACELLE STRUT, INBOARD ACCESS PANEL WITH LATCH BROKEN.(<P>REMOVED DAMAGED LATCH AT ENG #2, NACELLE STRUT INBOARD ACCESS PANEL AREA, LOCATED, CLEANED, TRIMMED, SECURED, ADJUSTED, SAFETY WIRE, INSTALLED NEW LATCH AS REQUIRED AT ENG #2 NACELLE STRUT, INBOASDR UIEA2024120301164Shutoff Valve · faultedLEFT TR INOP(<P>REMOVED DEFECTIVE REVERSER PRSOV REF 767-300 M/M 78-34-05-004-001-H00. OK TO INSTALL SERVICEABLE UNIT.</P> / <P>INSTALLED SERVICEABLE PRSOV REF 767-300 M/M 78-34-05-404-009-H00. INDICATOR AND OPERATION GOOD WITHOUT ENGINE OPERATING REF 767-300 SDR UIEA2024112801118Shutoff Valve · faultedDURING CRUISE, RECEIVED A MASTER WARNING "CABIN ALT". COMPLIED W/ QRH. FL380. CABIN ALT 11,000' DPSI 7.0. USED MANUAL PRESSURIZATION MODE TO CONTROL & STABILIZED CABIN ALT. "CABIN AUTO INOP" CAUTION MSG. COMPLIED W/ QRH PROC. "CABIN ALT AUTO 1" AND "CABISDR UIEA2024101501005Attach Fitting · corrodedLH UPPER HORIZONTAL STABILIZER PIVOT FITTING ATTACHMENT WITH CORROSION(<P><SPAN DATA-OLK-COPY-SOURCE="MESSAGEBODY">REMOVE FASTENERS FROM ALTERNATE ROWS, REAM THE AFFECTED HOLES THRU THE ENTIRE STACK-UP IN 1/64 INCH INCREMENTS UNTIL FASTENER HOLE IS CLEAN, ROUNSDR UIEA2024101501008Fuse Pin · crackedSUPPORT #6 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101501010Fuse Pin · crackedSUPPORT #3 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101501011Panel · damagedEVALUATE AND REPAIR AS REQUIRED, INDUCED DAMAGE TO RH HORIZONTAL STABILIZER T/E PANEL(<P>RH HORIZONTAL STABILIZER T/E PANEL WAS REPAIRED IAW SRM 55-10-01-2R-1 FIG 201 SHEET 4 PAGE 1-5 AND SRM 51-70-07- 0G-0 PAR 5.D FIG 11 PAG 16,37 REV 126 15/AUG/24</P>)SDR UIEA2024101501012Pivot Assy · corrodedHORIZONTAL STABILIZER - PIVOT FITTING - UPPER ATTACHMENT - MOST OUTBOARD REAR BOLT HOLE WITH INDICATION OF CORROSION(<P>TRE6755057 WAS PERFORMED AND NIL DAMAGE FOUND, TRE6755057 WAS BASED ON OEM MESSAGES CMA-PAO-24-0103</P>)SDR UIEA2024101501014Support Fitting · wornFLAP SUPPORT #1 FITTING OUTBOARD ACTUATOR SPAR FITTING WEAR FOUND 3 HOLES WITH CORROSION INDICATION (LOCATED 12:00, 08:00 AND 10:00 O´CLOCK)(<P>CORROSION WAS REMOVED, REAMING THE AFFECTED HOLES AND FREEZE PLUGS WERE INSTALLED. THIS REPAIR WAS BASED ON CMA-PASDR UIEA2024101501017Pin · corrodedLEFT 6-6 PIN FLAP SUPPORT #4 WITH CORROSION(<P>PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-04-402-135. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024101701042Transmitter · failedLEFT WING TRANSMITTER FLAP POSITION #1 WITH FAIL(<P>LEFT WING TRANSMITTER FLAP POSITION #1 WAS REPLACED AND TESTED IAW AMM TASK 27-51-45-422-030 REV 143 DATE 22 AUG 24, TEST OK, 50 IN LB WERE APPLIED. S/N 0818911494 DUE DATE 04 APR 25</P>)SDR UIEA2024101701050Packing · leakingFUEL LEAK IN MAIN FUEL BOOST PUMP WING RH(<P>THE PACKING AT THE MAIN FUEL BOOST PUMP WING RH WAS REPLACED. NO LEAKS WERE FOUND IAW AMM 24-22-03-004-001 AND 28-22-03-404-027 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 55 LB-IN AND 35 LB-IN. S/N: 0821902601 DATE: SDR UIEA2024101701051Union · leakingFUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH(<P>FUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH WAS R/R & NO LEAKS WERE FOUND IN IAW AMM 28-41-09-004-001-002 AND 28-41-09-404-028-002 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 240 LB-IN S/N:SDR UIEA2025081501124Warning Light · false activationMAIN CARGO DOOR DISCRETE LIGHT ON AFTER 2ND ENGINE START(<P>MDC CHECKED IAW AMM 52-31-00. OPENED & INSPECTION CHECKED GOOD. THIS CLOSES MDDR 236249 </P>)SDR UIEA2025081501125Starter · failedJUST BEFORE ENGINE START, A VERY STRONG ELECTRICAL SMELL OVERWHELMED THE FLIGHT DECK. SMELL GOES AWAY AFTER PACKS ARE SHUT OFF(<P>APU STARTER WAS BURNT AND WAS DETERMINED TO BE THE CAUSE OF THE SMOKE SMELL. R/R APU STARTER PER AMM 49-41-01. OPS CHK OK. NO DEFESDR UIEA2024060700500Control Panel · faultedFO SIDA UNABLE TO TURN VOR EMERGENCYIN MANUAL MODE(<P>REMOVED AND REPLACED VOR CONTROL PANEL IAW AMM 34-51-02. NO DEFECTS NOTED AT THIS TIME. VERIFIED PART EFFECTIVITY IAW IPC 31-11-11-17</P>)SDR UIEA2024060500494Stowage Box · unknown/FO OXYGEN STOWAGE BOX REQ REPLACEMENT(<P>R/R F/O'S OXYGEN STOWAGE BOX REF 35-11-51 LEAK CHECK GOOD OPS CHECK GOOD. PART EFFECTIVITY VERIFIED IAW AIPC 35-11-52-15</P>)SDR UIEA2024060500476Stowage Box · no testFIRST OBSERVERS OXYGEN MASK NOT TESTING(<P>SUSPECT FO'S OXYGEN STORAGE BOX AND MASK WITH FIRST OBSERVERS SEAT PER AMM 35-11-51. DEFERRING FIRST OBSERVERS SEAT TO DMI 210052 PER MEL 25-11-02-01 CAT A DUE DATE 06JUN24. PLACARDS INSTALLED. LEAK CHECKS OK. REMOVESDR UIEA2024031400148Disc · missingON PREFLIGHT A CHUNK OF THE O2 BLOWOUT DISC WAS DISCOVERED MISSING. REMOVED AND REPLACED O2 BLOWOUT DISK IAW AMM 20-10-23 AND AIPC 35-11-09-01.SDR P5CA2023121100118Elt · unknownBOTH ELT ANTENNA CABLES TANGLED AND NOT WRAPPED APPROPRIATELY. REMOVED AND REPLACED L1 DOOR SIDE ELT PER AMM 25-63-03/401. OPS CHK GOOD.SDR P5CA2023080300060Drain Valve · unknownLEFT WING, INSPAR LOWER SURFACE EXTERIOR, SUMP DRAIN MAIN TANK, WITH FUEL LEAK(<P>MAIN TANK SUMP DRAIN VALVE WAS REPLACED IAW AMM 28-11-05-404</P> / <P>CHECK FOR LEAKS WAS PERFORMED AND NO FOUND LEAKS</P>)SDR P5CA2023080300061Unknown · unknownLEFT WING, OUTBOARD FLAP, LOWER SURFACE, WS 764.2, WITH PERFORATION(<P>LEFT WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED IAW 57-00-00.</P>)SDR P5CA2023080300062Unknown · unknownDURING TASK 52-32-00-705-041, FOLLOWINGS STEPS ARE NOT SATISFACTORY: -STEP(K)(3)(D)4 S9024 SWITCH. "DOOR NOT CLOSED" LIGHT IS ON (INSTEAD OF OFF). -STEP(K)(3)(H)2 S9024 SWITCH. "DOOR NOT LATCHED" LIGHT IS O (INSTEAD OF ON). STEP(K)(3)(I)2 S9020 SWITCH. "DOORSDR P5CA2023080300063Unknown · unknownLIGHTING STRIKE ON UPPER FUSELAGE OUTER SKIN AT STA.396.75 AND 5" BELOW STGR 3RH(<P>LIGHTNING STRIKE WAS REPAIRED ON UPPER FUSELAGE OUTER SKIN AT STA 396 AND 5" BELOW STR 2 RH </P>)SDR P5CA2023080300064Unknown · unknownAFT CARGO DOOR, AFT AND UPPER OUTER SKIN WITH GOUGE(<P> AFT CARGO DOOR, AFT AND UPPER OUTER SKIN WAS REPAIRED. PER SRM 52-30-01-2R- 6 REV 122. </P>)SDR P5CA2023080900069Unknown · unknownMAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WITH CRACK(<P>SUMMARY: MAIN DECK FLOOR STRUCTURE STA 654+88 LBL 54 SEAT TRACK WAS REPAIRED IAW IAI SUPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P> / <P> </P>)SDR P5CA2023080900070Unknown · unknownMAIN DECK FLOOR STRUCTURE STA 654+88 LBL 5 SEAT TRACK WITH CRACK(<P>MAIN DECK FLOOR STRUCTURE AT STA 654+88 AND AT RBL 11 SEAT TRACK WAS REPAIRED PER SUPPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P>)SDR P5CA2023080900071Unknown · unknownCRACK ON PYLON #1 FWD UPPER SPAR WEB BETWEEN NAC STA 221.25 - 237.5, POWER FEEDER CABLE CUTOUT(<P>REPAIR WAS ACCOMPLISHED BY MXA EO TRE6754178 (SR ID 4-5858404778) <SPAN>AND BOEING SB 767-54-0090</SPAN></P>)SDR P5CA2023081100072Bottle · unknownCARGO 1 BTL EICAS MSG(<P>REMOVED AND REPLACED #1 CARGO BTL IAW AMM 26-23-02. OPS CHK GOOD.</P>)SDR P5CA2023050200024Unknown · unknown3 EA INERTIAL ESCAPE REELS FELL OUT(<P>TRANSFER TO DMI 184857 PER MEL 25-61-01-01 CAT C, DUE DATE 11MAY2023.</P> / <P>LP 1749741 M2: INSTALL DESCENT DEVICE 3 EACH PER REELS AMM 25-61-05/401. SN: 30767, 30764 & 30768</P>)SDR P5CA2023042000016Unknown · unknown2 EA ESCAPE REELS INOP. 2 ESCAPE REELS NEED TO BE RE-STOWED ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS ) TRANSFER TO DMI 184127 PER MEL 25-61-01-01 CAT C, DUE 29APR23. MX PROCEDURE C/W. INSTALLED 2 EACH DEVICE PSDR P5CA2022101000198Escape Reel · inoperative4 ESCAPE REELS INOP.(<P>REMOVED AND REPLACED DESCENT REELS IAW AMM 25-61-05. OPS CHECK GOOD</P>)
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