Boeing 767-38E

Service difficulty reports · 1,055

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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 = '76738E'
  ORDER BY difficulty_date DESC"

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SDR 2023FA0000657Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG #1, INBD, FWD UPPER SIDE OF THE THRUST REVERSER, RING-OUT. T/R S/N R648-624, P/N 681L272G12, RING-OUT PRESUMED P/N 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000656Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG #1, OUTBD, FWD UPPER SIDE OF THRUST REVERSER, RING-OUT. THRUST REVERSER S/ N: R647-1020. THRUST MODEL NO: TR-CF6-F28FG10. RING-OUT PRESUMED P/N: 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000655Unknown · unknownFWD CARGO – LOWER FRAME – STA 412, LBL 34: SHOP MISTAKENLY DAMAGED LOWER LOBE FRAME WEB AT THE NOTED LOCATION. DAMAGE SIZE: 0.4”X0.6”.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000654Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUNCTION OF TWO (2) PANELS, LOWER REAR PART, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 2.6”, WIDTH: 1.2”.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Exhaust SystemSDR 2023FA0000653Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #2, STRUT INBD SIDE (LEFT), UNDOCUMENTED DOUBLER REPAIR ON PANEL 447ELX OUTER SKIN, B/T NAC STA 296 & NAC STA 302. EXISTING REPAIR DIMENSIONS: FILLER: 1.5”X5.5”; DOUBLER: 6.7”X5”.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000652Unknown · unknownENGINE #2 INLET COWL: FOUND DENTS BEYOND OF SRM 54-12-01 LIMITS ON THE EXTERIOR NOSE LE SKIN OF THE INLET COWL. DENT NO 1 – LOCATED 12 O’CLOCK 15” FROM THE AFT LIP A=0.88”, Y=0.047”, A/Y=18; DENT NO 2Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000651Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND CRACK AND EDGE DAMAGE AT ENG#2, INBD, FWD UPPER SIDE OF THRUST REVERSER, RING-OUT. THRUST REVERSER S/N R649-112, P/N 681L269G07. RING-OUT PRESUMED P/N 491B1330003-013.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Thrust ReverserSDR 2023FA0000650Unknown · unknownENGINE #2, CORE COWL, BETWEEN NAC STA 293.25 – NAC STA 298.75: DURING AIRCRAFT CONVERSION MAINTENANCE INSPECTIONS, FOUND AN EXISTING UNDOCUMENTED DOUBLER REPAIR ON THE INBOARD SIDE OF THE #2 ENGINE, CORE COWL AT THE TITANIUM FAIRING CUTOUT AREA. THE DOUBLER REOct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000649Unknown · unknownDURING AIRCRAFT MAINTENANCE INSPECTION, SHOP FOUND THREE UNDOCUMENTED EXISTING FILLER REPAIRS AND MULTIPLE NEW DENTS ON #1 INLET COWL ACOUSTIC PANELS.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000648Unknown · unknownSEC #46, STA 1197+124 – 1197+134, STR 1L-2L: DURING AIRCRAFT SURVEY AN EXISTING REPAIR WAS FOUND PER DOCUMENTATION THE REPAIR SHOULD BE LOCATED AT STA 1197+110, STR 1L-2L, HOWEVER THE ACTUAL LOCATION OF THE REPAIR IS BETWEEN STA 1197+124 TO STA 1197+134, STR-1Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000647Unknown · unknownSTRUT #1, OUTB’D SIDE, NAC STA 304.54 NWL 134: DURING AIRCRAFT SURVEY SHOP FOUND UNDOCUMENTED REPEIR OF 3.2”X1.2” IN AFT FAIRING PANEL.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000646Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUCTION OF BOTH SIDE OF C-DUCT, LOWER REAR PARTS, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 3”, WIDTH: 1”.Oct 22, 2023 · N278CM · Boeing 76738E · Engine Exhaust SystemSDR 2023FA0000645Unknown · unknown: INLET COWL – ACOUSTIC DYNAROHR PANEL: DURING MAINTENANCE ON AIRCRAFT, IAI’S SHOP FOUND A DENT AT INLET COWL – INNER BARREL ACOUSTIC PANEL OF ENG #2, RIGHT HAND, UPPER SEGMENT, BETWEEN 3-4 O’CLOCK. THE DENT LOCATED 7” FROM PANEL EDGE. DENT SIZE: Y=0.013”, A/Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000644Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND DOCUMENTED REPAIR AT SEC 48, STA 1725.5, STR 6R-8R. THE REPAIR WAS REMOVED TO REPLACE PARTS. SHOP HAS FOUND THE REPAIR ISN’T PER SRM 53-80-01, REPAIR5, DETAIL III AS ACCLAIMED AT THE DOCUMENT. THE CUTOUTS PREFORMED WOct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000643Unknown · unknownRFTA 02937-0229; FVCI SERVICE REQUEST; BOEING 767-300 SRM 54-52-70 IDENTIFICATION; BOEING 767-300 SRM 54-52-70 ALLOWABLE DAMAGE 1; BOEING 767-300 SRM 54-52-70 REPAIR4; DWG 313T2381; FVCI EO 23149-26 REV. “IR” DATE: 09/13/2023.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000642Unknown · unknownDURING CONVERSION AT IAI, SHOP MISTAKENLY PEELED WEB OF LOWER FWD CARGO FRAME AT STA 412, RBL 25. DAMAGE SIZE: 0.6”X1.1”. SINCE THERE IS NO APPLICABLE REPAIR FOR THE REPORTED DAMAGE IN BOEING SRM, IAI ENGINEERING ASSESSED FVCI FOR REPAIR INSTRUCTIONS.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000641Unknown · unknownDURING AIRCRAFT CARGO CONVERSION FROM PASSENGER TO FREIGHTER, AIRCRAFT MAINTENANCE DISCOVERED AN EXISTING UNDOCUMENTED FUSELAGE SKIN REPAIR LOCATED BETWEEN APPROXIMATE STATIONS 1583 AND 1629, BETWEEN S29L AND S34L, MEASURING APPROXIMATELY 46.7”X19.3”, AS NOTEDOct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000640Unknown · unknownSTRUT #1, OUTBD SIDE, NAC STA 296-302, NWL 145: DURING AIRCRAFT SURVEY SHOP FOUND TWO (2) UNDOCUMENTED DOUBLER REPAIRS IN ACCESS PANEL 437ELX.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000639Unknown · unknownBETWEEN NAC STA 304.6 – NAC STA 310.6: DURING MAINTENANCE INSPECTIONS ON DATUM AIRCRAFT FOUND EXISTING REPAIR ON THE OUTER SKIN PANEL LOCATED ON THE OUTBOARD SIDE OF STRUT # 2. THE SIZE OF THE REPAIR IS 6.1”X5”. NO DOCUMENTATION WAS FOUND FOR THIS REPAIR.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000638Unknown · unknownBETWEEN NAC STA 304.6 – NAC STA 310.6: DURING MAINTENANCE INSPECTIONS ON DATUM AIRCRAFT FOUND EXISTING REPAIR ON THE OUTER SKIN PANEL LOCATED ON THE OUTBOARD SIDE OF STRUT # 2. THE SIZE OF THE REPAIR IS 6.1”X5”. NO DOCUMENTATION WAS FOUND FOR THIS REPAIR.Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000637Unknown · unknownSEC # 41, STA 287, WL 135, RBL 6: DURING AIRCRAFT SURVEY SHOP FOUND A CRACK IN VERTICAL STIFFENER, NOSE WHEEL WELL STRUCTURE.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000636Unknown · unknownENGINE #1 RH FAN COWL AT IAI IN TLV, MAINTENANCE FOUND AN EXISTING DOUBLER REPAIR ON THE OIL TANK ACCESS DOOR AROUND THE LATCH LOCATED ON THE FAN COWL SKIN OUTBD ENG #2 BT NAC STA 159-161.8 AT 3 O’CLOCK. REPAIR SIZE: 2.8”X2.8”. FAN COWL S/N:Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000635Unknown · unknownENGINE #1 RH FAN COWL, OIL ACCESS DOOR LATCH: DURING CONVERSION AT IAI IN TLV, MAINTENANCE FOUND AN EXISTING DOUBLER REPAIR ON THE OIL TANK ACCESS DOOR AROUND THE LATCH LOCATED ON THE FAN COWL SKIN INBD ENG#1 BT NAC STA 159-161.8 AT 3 O’CLOCK. REPAIR SIZE: 2.8Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000634Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND EXISTING DOCUMENTED (FL 1267 30372) DOUBLER REPAIR AT STA 303 BETWEEN STR 22R-24R. THERE IS A MISMATCH BETWEEN THE DOCUMENT AND THE POSITION OF THE DOUBLER ON A/C. ACCORDING TO FL 1267 30372, THE DOUBLER LOCATION IS Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR 2023FA0000633Unknown · unknownSTRUT #2 BETWEEN NAC STA 294.2 TO NAC STA 304.5: DURING MAINTENANCE INSPECTION, FOUND TWO DOUBLER REPAIRS ON ACCESS PANEL 446CL LOCATED ON THE INBOARD SIDE OF STRUT #2 IN THE OUTER SKIN PANEL’S LOWER AND UPPER EDGES. Oct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000632Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI, FOUND EXISTING DOUBLER REPAIR AT ENG #2, THRUST REVERSER SKIN (ON TRACK FAIRING), OUTBD SIDE, NAC STA 201.5 – 214.5, 1 (ONE) O’CLOCK. THRUSTOct 22, 2023 · N278CM · Boeing 76738E · Nacelle/Pylon StructureSDR 2023FA0000631Unknown · unknownFUSELAGE SKIN – STA 1219, BETWEEN S-5R AND S-7R: DURING AIRCRAFT INSPECTION, SHOP FOUND AN EXISTING FASTENER REPAIR LOCATED 0.294” FROM BUTT SPLICE AT STA 1219. THE FASTENER WAS REMOVED. HOLE DIAMETER: 0.265”.Oct 22, 2023 · N278CM · Boeing 76738E · Fuselage Structure (General)SDR MK1Y20231018002Unknown · unknownENG #1, EXHAUST OUTER SKIN FOUND GROUP FOR RIVETS REPAIR.Oct 18, 2023 · N287CM · Boeing 76738E · Engine Collector/Tailpipe/NozzleSDR MK1Y20231018001Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND DAMAGE ON THE L/H APU DOOR.Oct 18, 2023 · N287CM · Boeing 76738E · Auxiliary Power Unit (APU) DoorsSDR UIEA2023092700854Unknown · unknownLI-ION EXTINGUSHING AGENT P/N LKFD IN RH SIDE LAST OVERHEAD BIN FOUND LEAKING NEEDS REPLACMENT(<P>REMOVED AND REPLACED LI-ION EXTINGUISHING AGENT REFERENCE ATLAS AIR EMERGENCY EQUIPMENT CONFIGURATION - 641GT </P>)Sep 27, 2023 · N641GT · Boeing 76738E · Fire Protection SystemSDR UIEA2023081100775Pbe · unknownL1 PBE INDICATOR STRIP SHOWS RED(<P><SPAN>REMOVED AND REPLACED PBE AT L1 DOOR IAW AMM 25-64-00</SPAN></P>)Aug 11, 2023 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2023071900758Unknown · unknownCAPT & F/O EVAS INOP(<P>INSTALLED NEW EVAS SECURITY SEAL STICKERS IAW EO6725A222. NO FURTHER DEFECTS NOTED</P>)Jul 16, 2023 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2023071400757Unknown · unknownFLIGHT ATTENDANT SEAT L4A PSU INOP.(<P>TRANSFER TO MDDR 189255 PER MEL 35-21-01-01A CAT B, DUE DATE 7/17/2023</P>)Jul 14, 2023 · N641GT · Boeing 76738E · Passenger Oxygen SystemSDR UIEA2023070500706Unknown · unknownFUEL LEAK ON PORT OF DRY BAY AT LH WING TANK(<P>FUEL LEAK WAS REPAIRED ON PORT OF DRY BAY AT LH WING TANK THE FUEL LEAK TEST WAS SATISFACTORY PER AMM 28-11-00-30-8-013</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Aircraft Fuel SystemSDR UIEA2023070500705Carrier Assy · unknownRH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2023070500704Carrier Assy · unknownRH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2023070500703Unknown · unknownUPPER HALF FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND STRINGER S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P> LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Miscellaneous StructureSDR UIEA2023070500702Unknown · unknownUPPER HALF FUSELAGE SKIN BETWEEN STA 412 / STA 434 AND STRINGER S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500701Unknown · unknownUPPER HALF FUSELAGE SKIN AT STA 287 AND STRINGER S-1 LH / S-2 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500700Unknown · unknownUPPER HALF FUSELAGE SKIN AT STA 266.5 AND STRINGER S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500699Unknown · unknownCORROSION ON KEEL BEAM HORIZONTAL WEB BETWEEN STA 785.9 / STA 880(<P>REPAIR WAS ATTENDED BY SR 3-5696704793 (MXA EO TRE6753615) APPROVED BY FAA FORM 8100-9</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500698Unknown · unknownFUSELAGE SKIN BETWEEN STA 157 AND STRINGER S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500697Unknown · unknownLH FUSELAGE SKIN BETWEEN STA 158.2 AND BELOW WL220 WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500696Unknown · unknownFUSELAGE SKIN BETWEEN STA 143 / STA 157 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500695Unknown · unknownFUSELAGE SKIN BETWEEN STA 132 / STA 143 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023070500694Unknown · unknownUPPER FUSELAGE SKIN BETWEEN STA 566 / STA 588 AND S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Miscellaneous StructureSDR UIEA2023070500693Unknown · unknownUPPER FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Miscellaneous StructureSDR UIEA2023070500692Unknown · unknownUPPER FUSELAGE SKIN BETWEEN STA 456 / STA 478 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Miscellaneous StructureSDR UIEA2023070500691Unknown · unknownUPPER FUSELAGE SKIN BETWEEN STA 266.5 / STA 276 AND S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)Jul 8, 2023 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2023051000450Lens · damagedL1 DOOR LOWER EXIT LIGHT HA BURNT OUT BULBS(<P>DURING REPLACEMENT FOUND EXIT SIGN HAS DAMAGED CLIP REMOVED AND REPLACED LENS COVER IAW 33-51-8. OK FOR SERVICE.</P>)May 10, 2023 · N641GT · Boeing 76738E · Emergency Lighting
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