Boeing 767-231

Service difficulty reports · 757

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '767231'
  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 UIEA2020110402348Web · corrodedFWD CARGO STA 632 RBL 37-43 CORROSION ON THE OUTBOARD SIDE FWD FACE OF THE WEB. REMOVED CORROSION FROM WEB AT STA 632 RBL 37-43 AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-51-1A-1. REPAIRED WEB, IAW B767 SRM 53-00-07-2R-3.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020110402349Frame · corrodedFWD CARGO BILGE AREA, TOP OF FRAME SUPPORT HAS CORROSION ON UPPER SUREFACE STA 540 S35R. REMOVED CORROSION FROM FAIL SAFE STRAP STA 540 STR 35R AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-07-1A-1. REPAIRED FAIL SAFE STRAP, IAW FAS EA 20034 REV IR.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, FrameSDR UIEA2020110402350Stringer Splice · corrodedAFT PIT STRINGER SPLICE HAS EXFOLIATED CORROSION ON BOTH SIDES AND BULGING SKIN STA 1307 35L. UPON EVALUATION OF STR 35L AND SPLICE AT SAT 1307, FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 35L, IAW B767 SRM 53Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, Longeron/StringerSDR UIEA2020110602356Floorbeam · corrodedFWD CARGO PIT FLOOR STA 742 BEAM LBL 23 IN BOTTOM AFT SIDE TOP FLANGE HAS 3 SQUARE IN OF EXFOLIATED CORROSION. REMOVED CORROSION ON BOTTOM SIDE OF FLANGE 'J' CHANNEL AT STA 742 LBL 23 IN AN AREA 6.5"X1", IAW B767 SRM 51-10-02. ORIGINAL MATERIAL 100, REMAININDec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, Floor BeamSDR UIEA2020110602357Stringer · corrodedAFT OF FWD CARGO PIT STA 774 STR 37R HAS 3 SQ IN EXFOLIATED CORROSION. STR 37R AT STA 774 FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 37R, IAW B767 SRM 53-00-03-2R-2.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, Longeron/StringerSDR UIEA2020111002375Support · corrodedON PROCESS INSPECTION OF REMOVAL, FOUND CORROSION ON INTERCOSTAL RBL 28 FROM STA 610 TO 635. REMOVED CORROSION FROM INTERCOSTAL STA 610-635 RBL 28 AND FOUND OUT OF LIMITS, IAW B767 SRM 53-00-04-1A-1. FABRICATED NEW INTERCOSTAL AND APPLIED PROTECTIVE FINISHESDec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020111002376Skin · damagedREF DMI 127742 LP 1158798. CORROSION DAMAGE ON SKIN PANEL (P/N 146T3230-1) NEAR STA 1329, S-35L-CATEGORY-C TIME LIMITED REPAIR CW PART 3 OF EO 6753A851 PERMANENT REPAIR. COMPLIED WITH INSTALLATION OF PERMANENT REPAIR AT STA 1324-1460 STR 33L-39L, PER PART 3 Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, Plate/SkinSDR UIEA2020111002377Stringer · corrodedAFT OF FWD CARGO PIT STA 774 STR 36R HAS 5 SQ IN EXFOLIATED CORROSION AND CRACKED. STR 36R STA 774, FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS, IAW B767 SRM 53-00-03-1A-1. REPAIRED STR 36R, IAW B767 SRM 53-00-03-2R-2.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, Longeron/StringerSDR UIEA2020111302387Floor Support · corrodedFWD PIT CORROSION UNDER NUTPLATE LOWER SIDE OF WEB 566-588 RBL 4. REMOVED AND EVALUATED FWD CARGO INTERCOSTAL AT STA 566-588 RBL 4 AND FOUND OUT OF LIMITS, IAW B767 SRM 51-10-02. FABRICATED NEW AND INSTALLED INSTERCOSTAL, IAW B767 SRM 51-40-02 AND 53-30-53.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020111702408Floor Support · corrodedAFT PIT CARGO FLOOR SUPPORT EXFOLIATED STA 1263 LBL 24. REMOVED AND EVALUATED AFT CARGO FLOOR SUPPORT AT STA 1263 LBL 24 FOUND OUT OF LIMITS WITH 100% MATERIAL LOSS. FABRICATED NEW AND INSTALLED FLOOR SUPPORT, IAW B767 SRM 51-10-02, 51-40-02 AND DWG 96F56678Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020111702413Floor Support · corrodedFLOOR BEAM STA 615-632 AND BETWEEN RBL 33-24 HAS CORROSION ON LOWER SURFACE. UPON THE EVALUATION OF FLOOR BEAM AT STA 615-632 BETWEEN RBL 24-33 THE CORROSION ON THE 'L' ANGLES 2 EA WERE FOUND CORRODED WITH 100% MATERIAL LOSS, IAW B767 SRM 51-10-02. FABRICATEDec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020112002431Liner · corrodedDURING OPEN OF BULK CARGO DOOR INNER LINER FOUND EXFOLIATED CORROSION ON INNER SKIN LOWER SECTION. REMOVED AND REPLACED THE BULK CARGO DOOR DUE TO EXFOLIATED CORROSION ON THE INNER SKIN, IAW B767 AMM 52-36-01.Dec 5, 2020 · N650GT · Boeing 767231 · Cargo/Baggage DoorsSDR UIEA2020112402454Doubler · corrodedUPON REMOVAL OF Z-STIFFNER AT BULK CARGO THRESHOLD, FOUND DOUBLER AT AFT SIDE OF FRAME 1417 CORRODED. REMOVED AND REPLACED THE CORRODED DOUBLER AT THE AFT SIDE OF THE FRAME AT STA 1417 STR 32L-34L, IAW FAS EA 20031 REV R.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, StructureSDR UIEA2020112802468Frame · corrodedFWD PIT-CORROSION ON UNDERSIDE OF FRAME FLANGE AT STA 522 LBL 42. UPON EVALUATION OF FRAME J CHORD STA 522 LBL42, FOUND 100% OUT OF LIMITS AND REPAIRED, IAW B767 SRM 53-00-07-2R-4.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, FrameSDR UIEA2020112902470Door Frame · corrodedFWD PIT CORROSION ON MAIN FRAME AFT DOOR JAMB AT THRESHOLD. EVALUATED 615.5 FRAME LOWER CHORD STR 33R-34R AND FOUND 100% OUT OF LIMITS AND REPAIRED, IAW FAS EA 20036 REV IR.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Main, StructureSDR UIEA2020120102497Web · corrodedFWD CARGO WEB AT STA 522-588 INBOARD OF STRAP HAS CORROSION IN VARIOUS PLACES. REMOVED THE CORROSION FROM THE WEB AT STA 522-588 AND FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-02. FABRICATED AND INSTALLED NEW WEB, IAW B767 SRM 51-40-02 AND B767 SRM 53-30-Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020120202503Floor Support · corrodedFLOOR SUPPORT STRUCTURE HAS CORROSION FROM STA 610-STA 632 AND RBL 38-RBL 24. FLOOR SUPPORT STA 610-632 RBL 24-38 FOUND 100% MATERIAL LOSS AND FOUND OUT OF LIMITS. NEW FLOOR SUPPORT PN 143T5000-34 WILL BE INSTALLED ON NR-00891, PER CUSTOMER REQUEST. CORROSIDec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020120302506Support · corrodedFWD CARGO LOWER MAIN SILL RBL 44.9 AFT OF ST 605 TO STA 632 HAS CORROSION ON INNER CHORD AND UNDERLYING ATTACH STRUCTURE. INNER CHORD, FAIL SAFE STRAP AND 5 EA BACK UP FITTINGS FOUND OUT OF LIMITS. REMOVED AND REPLACED INNER CHORD, FAIL SAFE STRAP AND 4 EA BDec 5, 2020 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2020120802539Shear Tie · corrodedFWD CARGO COMPARTMENT BILGE AREA HAS CORRODED SHEAR TIE AT STA 698 BL 0. SHEAR TIE AT STA 698 BL 0 FOUND OUT OF LIMITS WITH 100% MATERIAL LOSS. REMOVED AND REPLACED SHEAR TIE, IAW B767 SRM 51-40-02, BOEING DWG 143T1212 REV D.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Internal Mounting StructureSDR UIEA2020120802540Shear Tie · corrodedFWD CARGO BILGE AREA SHEAR TIE HAS CORROSION UNDER IT, STA 698 BETWEEN S36L-37L. SHEAR TIE AT STA 698 STR36L-37L FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02-0G-0.Dec 5, 2020 · N650GT · Boeing 767231 · Fuselage Internal Mounting StructureSDR UIEA2020081401745Rivet · pulledDURING WALKAROUND, PILOT FOUND A "PULLED THROUGH" RIVET ON THE IN FUSELAGE ABOVE AND AFT OF THE CABIN PRESSURE OUTFLOW VALVE.(<P>REF LOGPAGE 1157429, ITEM# 20 FOR PERMANENT REPAIR IAW EO # 6753A871. REF LOGPAGE 1157428 ITEM #18 FOR HFEC INSPECTION M15, DMI # 1Aug 10, 2020 · N650GT · Boeing 767231 · Fuselage Main, Plate/SkinSDR UIEA2020081401746Fuse · failedCREW ENTRY DOOR EMERGENCY LIGHT INOP (NO VOLTAGE AT FIXTURE)(<P ><SPAN>FOUND ON THE BATTERY POWER / SUPPLY FUSE #2 WAS LOOSE, REINSTALLED FUSE IAW B767 SWPM 20-84-18. OPS CHECK / GOOD IAW B767 AMM 33-51-00.</SPAN></P>)Aug 10, 2020 · N653GT · Boeing 767231 · Emergency LightingSDR UIEA2020081281732Skin · delaminatedFOUND METAL DELAMINATION FORWARD OF FWD EQUIPMENT EXHAUST VALVE. REPAIRED AREA IAW SRM 53-00-01-2R-1 REPAIR 1 AND EO 6753A871 REV 6 PERMANENT REPAIR.Aug 8, 2020 · N650GT · Boeing 767231 · Fuselage Main, Plate/SkinSDR UIEA2020052641120Fire Bottle · unwanted deployRH ENG BOTTLE #2 DISCHARGE LIGHT AND ADVISORY MSG ON REMOVED, SERVICED AND REINSTALLED FIRE BOTTLE IAW AMM 26-21-03May 19, 2020 · N651GT · Boeing 767231 · Fire Bottle, FixedSDR UIEA2020041700757Eadi · malfunctionedCA PFD, EICAS, FO PFD WENT BLANK. FIRE MARSHALL SMELLED SMOKE IN COCKPIT.(<P>REPLACED CA EADI & EHSI. REPLACED F/O EADI AND UPPER EICAS SCREENS IAW AMM 31-41-01. CKS GOOD. C/W SMOKE INSPECTION IAW AMM 05-51-56, NO SMOKE/ FUMES PRESENT.</P><P>OFF: P/N 622-7999-Apr 16, 2020 · N652GT · Boeing 767231 · Attitude Gyro and Indicating SystemSDR UIEA2020020410161Terminal Block · arcedAT 15000 IN A CLIMB, THE CREW NOTICED AN ACRID/NOXIOUS FUME IN THE COCKPIT. THE CREW RETURNED TO IAH ON OXYGEN AND RAN "THE SMOKE FIRE OR FUMES" QRH CHECKLIST. ON RUNWAY EXIT, THE EVACUATION CHECKLIST WAS RUN. LANDING WEIGHT 243,000 LBS, BELOW 272,000 LBS MLW.Feb 1, 2020 · N653GT · Boeing 767231 · Ice/Rain Protection System WiringSDR UIEA2020020100159Unknown · odorAPPROX 10-15 MIN AFTER TAKEOFF IN CLIMB AT FL340, CAPT AND F/O NOTED AN ACRID SMELL IN THE COCKPIT. "SMOKE, FIRE OR FUMES" QRH RUN ON GROUND, EVACUATION CHECKLIST RUN.(<P>PERFORMED INSPECTION IAW AMM 05-51-56/201 AND 21-00-21. COULD NOT DUPLICATE SMELL. PERFORJan 31, 2020 · N653GT · Boeing 767231 · Air Distribution SystemSDR UIEA2019102875799Escape Reel · unwanted deployDESCENT DEVICE DEPLOYED IN CREW SERVICE AREA.(<P>TRANSFERRED TO MDDR 119657 PER MEL 25-61-01-01, CAT 'C', DUE DATE: 04-NOV-19.</P><P>LP 1083015 - M10: REMOVED AND REPLACED DESCENT DEVICE IAW MAINTENANCE MANUAL SUPPLEMENT 25-61-03. THIS CLEARS DMI #119657. MCC Oct 25, 2019 · N653GT · Boeing 767231 · Emergency EquipmentSDR UIEA2019091805533Line · defectiveRT ENG OIL QTY WENT TO 0 FOR 20 MINUTES. REMOVED AND REPLACED OIL QTY TRANSMITTER IAW AMM 79-31-01. OPS CHECKS GOOD BUT NO FIX, FURTHER TROUBLESHOOTING NEEDED. LP 1092409 - M3: REMOVED AND REPLACED TUBE ASSY #4 BRG SCAVENGE ON #2 ENG PER REQUEST IAW AMM 79-21-Sep 18, 2019 · N651GT · Boeing 767231 · Engine Oil Distribution (Airframe Furnished)SDR UIEA2019083005405Module · leakingITEM 1: LEFT HYDRAULIC SYSTEM EICAS MESSAGE QTY ON, AFTER GEAR UP. LOSS OF INDICATION VALVE, PRESSURE WAS 3000+. ITEM 2: CENTER HYDRAULIC SYSTEM EICAS MESSAGE QTY CAME ON AFTER GEAR UP. QTY WAS +-50. PRESSURE WAS 200. T/S PER FIM 29-11 FT 831, FOUND MONITOR UNAug 30, 2019 · N650GT · Boeing 767231 · Trailing Edge Flap Control SystemSDR UIEA2019082905327Elt · not reportedEMERGENCY LOCATOR TRANSMITTER. REMOVED AND REPLACED EMERGENCY LOCATOR TRANSMITTER IAW AMM 25-63-03.Aug 27, 2019 · N652GT · Boeing 767231 · Emergency Locator BeaconSDR UIEA2019082905326Escape Reel · not reportedMAIN ENTRY DESCENT DEVICE NEEDS TO BE REPLACED. REMOVED AND REPLACED MAIN ENTRY DESCENT DEVICE IAW B767 AMM 25-61-03.Aug 27, 2019 · N652GT · Boeing 767231 · Emergency EquipmentSDR UIEA2019081975207Warning Message · false activationLE FLAP DISAGREE. REF QRH, RETURNED TO DEPARTURE. OCCURRED ON RETRACTION FROM FLAP 5 TO FLAP 1. T/S IAW B767 FIM 27-81 FAULT TREE 808. NO CURRENT FAULTS FOUND. PERFORMED A BITE TEST ON THE PSEU FOUND "LVR NOT IN DENT" FAULT IN THE LAST FLIGHT LEG. PERFORMED LAug 17, 2019 · N651GT · Boeing 767231 · Leading Edge Slat Control SystemSDR UIEA2019072904887Skin · dentedLOWER EMPENNAGE SKIN HAS A DENT BS 1800 BETWEEN STR 36L - 37L. (<P>INSPECTED, EVALUATED, AND REPAIRED DENT AT STA 1805 36L - 37L IAW SRM 53-00-01, IAI EA CS-22572-007.</P>)Jul 28, 2019 · N653GT · Boeing 767231 · Fuselage Main, Plate/SkinSDR UIEA2019072904888Panel · corrodedLT WING UPPER TE PNL. FWD EDGE BULGING, JUST FWD OF I/B END OF O/B AILERON. (<P>REMOVED CORROSION, REPAIRED, AND RESTORED PROTECTIVE FINISHES AT LT WING UPPER SURFACE PANEL. FWD OF O/B AIL I/B SIDE ON TE SKIN IAW FAS EA 19023 REV. 1R. </P>)Jul 28, 2019 · N653GT · Boeing 767231 · Wing, Plate/SkinSDR UIEA2019072904889Skin · corrodedRT WING IB MAIN FLAP UPPER SURFACE HAS AREA OF CORROSION 14 INCHES FROM I/B END. (<P>COMPLIED WITH EA 19025 REV. 1R, RT WING I/B MAIN FLAP, UPPER SURFACE I/B SIDE. </P>)Jul 28, 2019 · N653GT · Boeing 767231 · Trailing Edge FlapsSDR UIEA2019072904891Stringer · corrodedBS 415 STR 33R CORRODED. (<P>REPAIRED STR 33R AT STA 405 - STA 434 IAW SRM 53-00-03-2R-2.</P>)Jul 28, 2019 · N653GT · Boeing 767231 · Fuselage Main, Longeron/StringerSDR UIEA2019072904892Stringer · crackedSTA 438 STR 36R IS CRACKED. (<P>REPAIRED STRINGER AT STA 434-480 STR 36 IAW SRM 53-00-03-2R-2.</P>)Jul 28, 2019 · N653GT · Boeing 767231 · Fuselage Main, Longeron/StringerSDR UIEA2019070104647Stringer Clip · crackedDURING HFEC INSPECTION, FOUND FLOOR POST TO FRAME CRACKED ON MIDDLE FASTENER, LOWER FASTENER AND UPPER O/B RADIUS ON AFT SIDE OF FLOOR POST STATION 1395 STR 33R. (<P>REMOVED AND REPLACED STA 1395 STR 33R CLIP IAW SRM 51-40-02 AND DWG 146T1516 REV C.<BR /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Fuselage Main, Attach FittingsSDR UIEA2019070104645Floor Panel · damagedBULK CARGO RT FLOOR PNL HAS MULTIPLE REPAIRS, DENTS AND 1 PUNCTURE. (<P>FABRICATED NEW BULK CARGO FLOOR PNL RT IAW SRM 53-60-53. FLOOR PNL REMOVED AND WILL BE RE-INSTALLED ON TASK NR-00004.<BR /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Fuselage Floor PanelSDR UIEA2019070104643Fairing · delaminated#2 ENG STRUT FAIRING I/B SIDE PERMANENT REPAIR IS DELAMINATED ON INTERIOR SURFACE, VIEWED THRU ACCESS DOOR #447BL AREAS MARKED.(<P>REPAIRED #2 ENGINE STRUT FAIRING I/B SIDE, P.N. 313T3381-1 IAW SRM 51-70-10-2R-0.<BR /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Engine Cowling SystemSDR UIEA2019070104642Support Angle · corrodedKEEL BEAM AREA FWD MLG ACCESS PNL SUPPORT ANGLE CORRODED. (<P>UPON FURTHER EVALUATION, FOUND SUPPORT ANGLE WITH 100% MATERIAL LOSS IAW SRM 53-50-12. REMOVED AND REPLACED SUPPORT ANGLE ON KEEL BEAM AREA FWD MLG IAW SRM 51-40-02.<BR /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2019070104641Floor Panel · corrodedBULK CARGO COMP. LT FLOOR PNL HAS AREAS OF CORROSION ON UPPER SURFACE BS 1461-1540. (<P>REMOVED, FABRICATED, AND INSTALLED NEW BULK CARGO LT FLOOR PNL IAW SRM 53-60-53.<BR /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Fuselage Floor PanelSDR UIEA2019070104640Escape Reel · defectiveMAIN ENTRY DESCENT DEVICE (P/N: 379103D-29, S/N: 21244) IS NOT IN GOOD CONDITION.(<P>REMOVED AND REPLACED MAIN ENTRY DESCENT DEVICE IAW AMM 25-61-00.<BR DATA-MCE-BOGUS="1" /></P>)Jun 30, 2019 · N651GT · Boeing 767231 · Emergency EquipmentSDR UIEA2019061764500Window · failedL1 WINDOW DURING CLIMB OUT CRACKING AND SMOKING FROM OUTER BOTTOM CORNER TURNED OFF WINDOW HEAT(<P>INSPECTED L1 WINDOW FOR DAMAGE IAW 767 AMM 56-11-00 NOTED NONE. FOUND L1 WINDOW ELECT CONNECTOR TERMINAL LOOSE AT LWR LH CORNER CLEANED AND SECURED TERMINAL END Jun 14, 2019 · N653GT · Boeing 767231 · Flight Compartment WindowsSDR UIEA2019042543944Fastener · corroded#2 ENGINE TURBINE SECTION 6 EA PT7 PROBES ATTACH HARDWARE CORRODED. DOT 127-046.(<P>CLEANED #2 ENGINE TURBINE SECTION PT7 PROBE ATTACH HARDWARE IAW B767 SOPM 20-30-03 AND AMM 77-21-02.</P>)Apr 22, 2019 · N650GT · Boeing 767231 · Engine Indicating SystemSDR UIEA2019042403945Tube · cracked#2 ENGINE TURBINE SECTION COOLING TUBE, 8:00 POSITION HAS A 1 IN CRACK AT PREVIOUS WELD. (<P>REMOVED AND REPLACED #2 ENGINE TURBINE SECTION COOLING TUBE IAW B767 AMM 75-24-08.</P>)Apr 22, 2019 · N650GT · Boeing 767231 · Turbine SectionSDR UIEA2019042543946Stiffener · corrodedKEEL BEAM, R/H O/B STIFFENER AT STA 786 BULKHEAD HAS CORROSION. (<P>REMOVED SPLICE FITTING (STIFFENER), FABRICATED, AND INSTALLED NEW SPLICE (STIFFENER) P/N 7075T651. .500 BARE PLATE, PO #1904679 DIM (3.6' X 14.2") AT KEEL BEAM R/H STA 786 BULKHEAD IAW B767 DWApr 22, 2019 · N650GT · Boeing 767231 · Fuselage Miscellaneous StructureSDR UIEA2019042543947Connector · damagedENGINE #1 IDG ELEC PLUG D00412 HAS DAMAGED BACKSHELL. (<P>REMOVED AND REPLACED #1 ENGINE IDG PLUG D00412 IAW B767 WDM 24-11-11 AND PERFORMED A GOOD OPS CHECK IAW B767 AMM 24-11-00.</P>)Apr 22, 2019 · N650GT · Boeing 767231 · Electrical Power System WiringSDR UIEA2019042543948Starter · inoperativeAPU STARTER IS INOP. (<P>REMOVED AND REPLACED APU STARTER ASSY IAW B767 AMM 49-41-01. PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 49-41-01. NO DEFECTS NOTED.</P>)Apr 22, 2019 · N650GT · Boeing 767231 · APU Start/Ignition System
Back to Boeing 767-231