Boeing 767-33A

Service difficulty reports · 1,978

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 = '76733A'
  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 ABXR2026060400010Angle · crackedRIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1Jun 4, 2026 · N1997A · Boeing 76733A · Wing, Attach FittingsSDR ABXR2026060400009Frame · corrodedCORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511.Jun 4, 2026 · N1997A · Boeing 76733A · Fuselage Main, FrameSDR CNMA2026040004Pressure Valve · inoperativeL HPSOV EICAS MSG, AND L BLEED LIGHT ILLUMINATEDApr 21, 2026 · N351AX · Boeing 76733A · Pneumatic SystemSDR CNMA2026030002Altimeter · inoperativeCA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.Mar 31, 2026 · N351AX · Boeing 76733A · Altimeter, Barometric/EncoderSDR 2026FA0000047Thrust Reverser · delaminatedDURING AIRCRAFT CARGO CONVERSION AT IAI MAINTENANCE FOUND THE INNER SKIN OF THE ENGINE #1 INBOARD THRUST REVERSER DELAMINATED AT NAC STA 230. THE DAMAGE WAS EVALUATED AND FOUND TO BE BEYOND REPAIR LIMITS. WORK PERFORMED IAW REA NO: MF03036R0233.Jan 20, 2026 · N407EG · Boeing 76733A · Engine Thrust ReverserSDR 2026FA0000046Frame · crackedDURING MAINTENANCE INSPECTIONS AT IAI FACILITIES, SHOP FOUND A CRACK IN ENGINE #1 INLET COWL AFT BULKHEAD OUTER FRAME FLANGE, BETWEEN 11 O'CLOCK AND 12 O'CLOCK. WORK PERFORMED IAW REA NO: MF03036R0235.Jan 20, 2026 · N407EG · Boeing 76733A · Fuselage Structure (General)SDR 2026FA0000045Frame · crackedDURING MAINTENANCE INSPECTIONS AT IAI FACILITIES, SHOP FOUND A CRACK IN ENGINE #2 INLET COWL AFT BULKEAD OUTER FRAME FLANGE, BETWEEN 12 O'CLOCK AND 1 O'CLOCK THE CRACK WAS TRIMMED OUT PER SRM 51-10-02. WORK PERFORMED IAW REA NO MF03036R0229.Jan 20, 2026 · N407EG · Boeing 76733A · Nacelle/Pylon, Frame/Spar/RibSDR 2026FA0000044Angle · gougedDURING INSPECTION OF THE LEFT-HAND CORE COWL OF ENGINE #1 (P/N: 224M4761-513, S/N: 2014001), A GOUGE WAS FOUND ON THE EXISTING FRAME REPAIR ANGLE. WORK PERFORMED IAW REA NO: MF03036R0219.Jan 20, 2026 · N407EG · Boeing 76733A · Nacelle/Pylon, Frame/Spar/RibSDR 2026FA0000043Frame · puncturedDURING MAINTENANCE INSPECTIONS AT IAI, A PUNCTURE WAS FOUND ON THE WEB OF FRAME STA 1417 BETWEEN STR 37R AND 39R. WORK PERFORMED IAW REA NO: MF03036R0237.Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, FrameSDR 2026FA0000042Ring · wornDURING MAINTENANCE INSPECTION, WEAR DAMAGE FOUND ON ENGINE NR 1, RIGHT FAN REVERSER, AFT CLOSEOUT RING AT THE LOWER AND UPPER CORNERS.WORK PERFORMED IAW REA NO: MF03036R0222.Jan 19, 2026 · N407EG · Boeing 76733A · Engine Thrust ReverserSDR 2026FA0000041Frame · corrodedDURING CONVERSION, CORROSION WAS FOUND ON THE FRAME AT STA1480, BETWEEN STR 22L AND STR 24L. WORK PERFORMED IAW- REA NO: MF03036R0202.Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, FrameSDR 2026FA0000039Frame · damagedDURING CONVERSION AT IAI FACILITIES, SHOP FOUND DAMAGED FRAME WEB AT STA 478, BETWEEN STR - 27R AND STR - 28R (LARGE CARGO DOOR SURROUND). WORK PERFORMED IAW - REA NO: MF03036R0206.Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, FrameSDR 2026FA0000038Frame · corrodedCORROSION FOUND ON FRAME STA 1439, OUTER FLANGE, TWO LOCATIONS BETWEEN STR 17L-18L.Jan 19, 2026 · N407EG · Boeing 76733A · Fuselage Main, FrameSDR 2026FA0000037Channel · crackedDURING MAINTENANCE INSPECTIONS AT IAI FACILITIES SHOP FOUND A CRACK ON CHANNEL. DAMAGED AND ENLARGED FASTENER HOLES ON OUTER SKIN FAIRING. WORK PERFORMED IAW REA MF03036R0216.Jan 19, 2026 · N407EG · Boeing 76733A · Engine Exhaust SystemSDR 2026FA0000036Skin · abnormalDUE TO EXISTING EXTERNAL REPAIR IN FUSELAGE SKIN, SHOP CANNOT INSTALL SHEAR TIE, P/N 95292-257 IN ACCORDANCE WITH DWG REQUIREMENTS.Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/SkinSDR 2026FA0000035Shear Tie · damagedSHOP FOUND SIX (6) EXISTING 7/32" DIAMETER FASTNER HOLES DURING SALVAGED SHEAR TIE, P/N BACF3T01G7G16 REMOVAL AT STA 390, BETWEEN STR-20L AND STR-21L. REFER TO FIGURES 1 AND 2 FOR E.M AND FASTENER SPACING.Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Internal Mounting StructureSDR 2026FA0000034Tear Strap · gougedDURING INSTALLATION OF P/N 368-53-11-90830-235 SHEAR TIE PER DWG 371-53-11-C3147, VIEWS 1B3 AND 1B12, A GOUGE WAS FOUND ON THE TEAR STRAP AT STA 368, BETWEEN STR 20L AND 21L. THE GOUGE WAS REMOVED, AND THE RESULTING BLEND-OUT DIMENSIONS ARE 1.00" X 0.320". THEJan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, StructureSDR 2026FA0000033Skin · mechanic errorDURING INSTALLATION OF SHEAR TIE PER DWG 371-53-00-C4157 VIEWS 5C8-1 AND 1B5, THE SHOP MISTAKENLY DAMAGED THE COUNTERSINK OF ONE FASTENER HOLE COMMON TO THE FUSELAGE SKIN AT BS 1241, BETWEEN STR 27R AND 28R.Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/SkinSDR 2026FA0000032Frame · mechanic errorDURING CNV WORK SHOP CAUSED DAMAGE TO THE FRAME EDGE AT SPLICE AREA, OUTER FLANGE.Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, FrameSDR 2026FA0000031Doubler · corrodedDURING INSTALLATION OF DOUBLER PER DWG 371-53-11-C3164, CORROSION WAS DETECTED ON THE OUTER FLANGE OF FRAME BS 390 BETWEEN STR 19R AND 20R.Jan 18, 2026 · N407EG · Boeing 76733A · Fuselage Main, Plate/SkinSDR 2026FA0000025Bracket · misinstalledACCORDING TO INSTALLATION 371-53-00-C4178-003 SHOP REQ TO REMOVE AND REPLACE TWO EXISTING BRACKETS.HOWEVER INSTALLATION OF FITTINGS WILL RESULT IN SHORT EDGE MARGIN.BRACKETS ARE DIFFRENT THAN WHAT ITS SHOULD BE PER DWG 145T8722. IN ADDITION THE FOUR FASTNERJan 15, 2026 · N407EG · Boeing 76733A · Fuselage Main, Floor BeamSDR NACA2025101000006Igniter · wornNR 2 ENGINE UPPER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 UPPER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.Oct 10, 2025 · N567NC · Boeing 76733A · Spark Plug/IgniterSDR NACA2025101000005Igniter · wornNR 2 ENG LOWER IGNITER PLUG WORN BEYOND LIMITS. REMOVED AND REPLACED NR 2 LOWER IGNITER PLUG IAW AMM 74-21-02-004-001-N00 AND AMM 74-21-01-404-014-N00. OPS CHECK GOOD.Oct 10, 2025 · N567NC · Boeing 76733A · Spark Plug/IgniterSDR NACA2025101000004Cable · crackedNR 2 ENG LOWER IGNITION EXCITER CABLE BUSHING UNDER CERAMIC SLEEVE CRACKED. DOT 048200. REMOVED AND REPLACED NR 2 ENG LOWER IGNITION EXCITER CABLE IAW B767 AMM 74-21-01-004-001-N00. TEST OK. PO # GYR10300795. TW ID T100360-1 D/D 8/12/26. MECH: ALD025 10/06/Oct 10, 2025 · N567NC · Boeing 76733A · Ignition System WiringSDR NACA2025101000003Circuit Card · faultedLEFT ENGINE FAILED AUTOMATIC FIRE / OVERHEAT LOGIC /TEST SYSTEM (AFOLTS) SYSTEM CHECK. CARDS WERE REPLACED WITH PN S332T301-181 SN 940, 699, 8823 AND 6780Oct 10, 2025 · N567NC · Boeing 76733A · Fire DetectionSDR NACA2025101000002Valve · crackedIP VALVE ON #1 ENGINE HAS SIGNS OF CRACKING AND CORROSION ON FUSELAGE. INSTALLED SERVICEABLE IP VALVE ON # 1 ENG IAW AMM 36-11-06-404-033-002. NO LEAK NOTED.Oct 10, 2025 · N567NC · Boeing 76733A · Turbine Engine Air Inlet SectionSDR NACA2025101000001Vane · brokenONE EA FAN EXIT VANE OF THE NR 2 ENGINE HAS A BROKEN PLATFORM AT THE INNER BASE OF PART. PERFORMED EVALUATION IF 1 EACH FAN EXIT VALVE OF #2 ENG BROKEN PLATFORM NO ADITIONAL DEFECTS NOTED. REPAIRED FAN EXIT VALVE IAW 72-33-02-308-003-N00 .Oct 10, 2025 · N567NC · Boeing 76733A · Turbine Engine Air Inlet SectionSDR NACA2025100400002Screen · damagedNR 1 FAN EXIT CASE BLEED AIR DUCT, BLEED SCREENS 8 EA FROM UPPER DUCTS ARE BROKEN / MISSING. REMOVE AND REPLACE 6 EA SCREENS ON #1 ENG ESN 724378 IAW AMM 72-00-00-416-342-N00 REMAINING 2 EA UPPER SCREENS FOUND TO BE IN SERVICEABLE CONDITION IAW AMM TASK 75-3Oct 4, 2025 · N567NC · Boeing 76733A · Engine Bleed Air SystemSDR NACA2025100400001Sense Line · chafedSTATIC PRESSURE SENSE LINE TUBE CHAFED ON #2 ENG. INBD FAN COWL. REMOVED AND REPLACED STATIC PRESSURE SENSE LINE TUBE ON #2 ENG INBD FAN COWL. LEAK TEST AND STATIC TEST GOOD IAW B767 AMM 71-00-02-844-002-N00 STEP 2 AMM 71-00-02-844-077-N00 STEP 7 AMM 71-00-Oct 4, 2025 · N567NC · Boeing 76733A · Engine Indicating SystemSDR NACA2025093000008Seal · deterioratedNR 2 ENGINE SEAL ATTACHED TO OIL DRAIN COLLECTOR IS DAMAGED & DETERIORATING. REMOVED & REPLACED NR 2 ENG SEAL ATTACHED TO OIL DRAIN COLLECTOR IAW AMM 51-31-01-302-001 AND 51-31-01-392-013.Sep 30, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil SystemSDR NACA2025093000007Exciter · damagedNR 1 ENG TOP IGNITION EXCITER INSIDE OUTPUT RECEPTACLE WELL HAS DAMAGE / SIGNS OF ARCING ON THE CONTACT BUTTON. REMOVED AND REPLACED #1 ENG TOP IGNITION EXCITER IAW B767 AMM 74-11-01-004-001-N00 AND AMM 74-11-01-404-019 STEP 3.Sep 30, 2025 · N567NC · Boeing 76733A · ExciterSDR NACA2025093000006Igniter · wornNR 1 ENG. SYS. 1 TOP IGNITION EXCITER PLUG IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.Sep 30, 2025 · N567NC · Boeing 76733A · Spark Plug/IgniterSDR NACA2025093000005Sealant · missing10 O'CLOCK (FWD LOOKING) FAN EXIT STRUT LOWER SURFACE MISSING SEALANT ON NR 2 ENGINE. APPLIED SEALANT ON FAN EXIT STRUT LOWER SURFACE #2 ENG AT 10 O'CLOCK PER B767 AMM 73-3405 TASK 72-34-05-404-005-N00 PAR D (3) (E).Sep 30, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)SDR NACA2025093000004Liner · misinstalled6 TO 7 O'CLOCK (LOOKING FWD) FAN EXIT LINER NOT PROPERLY FAIRED ON #2 ENGINE. REPAIRED FAIRED FAN EXIT LINER ON #2 ENGINE AT 6 TO 7 O'CLOCK POSITION, REPLACED BROKEN SUPPORT BRACKETS FOR LINER REF MAN-PW4ENG-109 PG 18 AND SRM 51-40-02 STEP 4 (B).Sep 30, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)SDR NACA2025093000003Control Unit · faultedBUSS POWER CONTROL UNIT HAS A FAULT MESSAGE IDG / OIL OUT. PERFORMED BPCU BITE PROCEDURE PER B-767 FIM 24-30 FAULT TREE 801. BITE PROCEDURE OK.Sep 30, 2025 · N567NC · Boeing 76733A · DC Generating SystemSDR NACA202510229002Clamp · misinstalledNR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148.Sep 30, 2025 · N567NC · Boeing 76733A · Nacelle/Pylon StructureSDR NACA2025093000001Oil Tube · unsecureBROKEN CLAMP ON OIL TUBE FWD OF OIL TANK ON #1 ENGINE. INSTALLED NEW CLAMP ON FIRE EXT. TUBE FWD OF OIL TANK ON #1 ENGINE PER AMM 20-11-00 TABLE 213/20-11-00-993-830Sep 30, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil SystemSDR NACA2025092600002Sealant · missingSEVERAL FAN EXIT (INNER FRONT) FAIRINGS SEGEMENTS MISSING SEALANT AROUND COMPRESSOR SECTION CASE ON NR 2 ENG. APPLIED RTV SEALANT TO FAN EXIT (INNER FRONT) FAIRING SEGMENTS IAW B767-300 REF. AMM 72-34-03.Sep 26, 2025 · N567NC · Boeing 76733A · Engine (Turbine/Turboprop)SDR NACA2025092600001Clamp · unsecureNR 2 ENGINE IDG WIRING HARNESS CLAMPS NOT PROPERLY INSTALLED. PERFORMED PROPERLY INSTALLATION OF THE CLAMPS IN THE IDG WIRE HARNESS AT #2 ENGINE IAW SWPM 20-10-12 STEP Y PG 148 .Sep 26, 2025 · N567NC · Boeing 76733A · Nacelle/Pylon StructureSDR NACA2025092300001Igniter · wornNR 1 ENG IGNITOR PLUG FOR SYSTEM 2 (BOTTOM PLUG) IS WORN BEYOND LIMITS. IGNITER PLUG REPLACED IAW AMM 74-21-02-404-014-N00.Sep 23, 2025 · N567NC · Boeing 76733A · Spark Plug/IgniterSDR IXXA20250918053Power Supply · inoperativeFOUND INTERIOR EMERGENCY LIGHTS RIGHT CEILING, DOOR EXIT SIGN AND DOOR THRESHOLD LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. PLACED ON DEFERRAL 66237. MINIMUM EQUIPMENT LIST ATI-33-51-01-01 CATEGORY D. TROUBLESHOT IN ACCORDANCE WITH B767 IAI WIRING DIAGRAMSep 18, 2025 · N1439A · Boeing 76733A · Emergency LightingSDR IXXA20250908001Tube · dentedA DENT WAS FOUND DURING C-CHECK MAINTENANCE VISIT LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7. THE DENT WAS MEASURED AS L=0.400" W=0.700" D=0.129". DENT TO BE RE INSPECTED AT NEXT C-CHECK TO BE CONSIDERED PERMANENTSep 8, 2025 · N1439A · Boeing 76733A · Aircraft Fuel Distribution SystemSDR IXX2025F00019Beam · corrodedFLC DOOR CUTOUT LWR SILL BEAM EXFOLIATED STA622Sep 8, 2025 · N1439A · Boeing 76733A · Fuselage Main, StructureSDR IXXA2025090300018Tube · dentedLEFT WING FUEL DISTRIBUTION TUBE HAS A DENT, LOCATED INSIDE 532BB BETWEEN LOWER STRINGER L-6 AND L-7Sep 3, 2025 · N1439A · Boeing 76733A · Aircraft Fuel Distribution SystemSDR IXXA20250831002Skin · corrodedRIGHT WING TOP EXTERNAL SKIN CORRODED AT SKIN SPICE AT WING STA 383.5-395Aug 31, 2025 · N1439A · Boeing 76733A · Wing, Plate/SkinSDR IXX2025F00016Skin · delaminatedVERTICAL STAB PANEL LEFT SIDE DELAMINATEDAug 31, 2025 · N1439A · Boeing 76733A · Vertical Stabilizer, Plate/SkinSDR 21GA202509030017Controller · faultedON APPROACH, RECEIVED WHEEL WELL FIRE EICAS MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED DETECTION CONTROL CARD.Aug 29, 2025 · N1997A · Boeing 76733A · Fire DetectionSDR NACA2025082000002Elec Connector · damagedDURING TROUBLESHOOTING FOUND LEFT FWD FBP CONNECTOR D1550 PIN #6 WILL NOT SECURE. REPLACED FUEL PUMP CONNECTOR D1550 PER SWPM 20-61-00 OPS CHECK GOOD PER AMM 28-42-01Aug 20, 2025 · N567NC · Boeing 76733A · Fuel System WiringSDR NACA2025082000001Pressure Switch · failedAFTER LEFT ENGINE START L FWD BOOST PUMP PRESSURE LIGHT ILLUMINATED AND ASSOCIATED EICAS MESSAGE. REPLACED LEFT FWD PUMP PRESSURE SWITCH OPS CHECK GOOD PER AMM 28-42-01 PART IS UNKNOWN TO TRAX.Aug 20, 2025 · N567NC · Boeing 76733A · Fuel Boost PumpSDR NACA2025081700001Cooler · failedRIGHT ENGINE OIL QTY DROPPED FROM 17 UNITS TO 12 DURING FLIGHT. SUSPECT OIL LEAK STILL PRESENT. FOUND OIL PUDDLING AT 6 OCLOCK OF ENGINE WITH EVIDENCE OF OIL LEAKAGE ON THE LH SIDE OF ENGINE CORE EMANATING FROM AIR/OIL COOLER. REMOVED AND REPLACED #2 ENGINE AIAug 17, 2025 · N567NC · Boeing 76733A · Turbine Engine Oil System
Back to Boeing 767-33A