# Service difficulty reports: N379AZ A list on [N379AZ](https://openairdocs.org/aircraft/N379AZ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 57 reports - [SDR IXXA20261019105](https://openairdocs.org/sdr/IXXA20261019105.md): None · none · Oct 19, 2026 · N379AZ · Boeing 767323 · Standard Practices/Structures > DUE TO BOMB THREAT CREW RETURNED TO ORIGINATING STATION. EMERGENCY WAS DECLARED BY CREW. AIRCRAFT LANDED WITHOUT INCIDENT. UPON LANDING AIRCRAFT WAS GROUNDED FOR INSPECTION. LAW ENFORCEMENT DID A THOUROUGH INSPECTION OF WHOLE AIRCRAFT. NO BOMB WAS DISCOVERED. - [SDR IXXA20261015099](https://openairdocs.org/sdr/IXXA20261015099.md): Crank Assy · loose · Oct 15, 2026 · N379AZ · Boeing 767323 · Flight Compartment Windows > DURING PRE-DEPARTURE CHECK FOUND FIRST OFFICER'S WINDOW CRANK ASSEMBLY LOOSE. FOUND GEARBOX MOUNTING HRADWARE LOOSE. RESECURED GEARBOX ASSEMBLY IAW B767 AMM 56-11-04. OPERATIONAL CHECK GOOD. - [SDR IXXA20261008092](https://openairdocs.org/sdr/IXXA20261008092.md): Switch · inoperative · Oct 8, 2026 · N379AZ · Boeing 767323 · Turbine Engine Oil System > AT APPROX 100-400 FT, RT OIL FILTER EICAS MSG APPEARED. QRH PROCEDURES WERE FOLLOWED. BEFORE RT ENG SHUTDOWN, ALL ENG PARAMETERS NORMAL. WAITED 2 MINS AT IDLE & EICAS STILL DID NOT CLEAR. RT ENG SHUTDOWN IAW QRH. NO RESTART ATTEMP. RETURNED TO ORIGINAL STA - [SDR IXXA20260916084](https://openairdocs.org/sdr/IXXA20260916084.md): Life Vest · missing · Sep 16, 2026 · N379AZ · Boeing 767323 · Life Jacket > DURING DAILY CK FOUND SUPERNUMERARY SEAT (RIGHT SIDE NEXT TO LAV) MISSING LIVE VEST. DEFERED MEL D 76976. LIFE VEST INSTALLED IN STOWAGE BIN UNDER RIGHT SUPERNUMERATY SEAT. - [SDR IXXA20260916083](https://openairdocs.org/sdr/IXXA20260916083.md): Life Vest · missing · Sep 16, 2026 · N379AZ · Boeing 767323 · Life Jacket > DURING DAILY CK FOUND SUPERNUMERARY SEAT (MIDDLE) WITHOUT LIFE VEST. DEFERED MEL D 76975. VERIFIED LIFE VEST INSTALLED IN STOWAGE BIN UNDER MIDDLE SUPERNUMERARY SEAT. - [SDR IXXA20260814001](https://openairdocs.org/sdr/IXXA20260814001.md): Bulkhead · corroded · Aug 14, 2026 · N379AZ · Boeing 767323 · Fuselage Main, Bulkhead > LWW BULKHEAD STA 955 APPROX LEFT HAND BUTT LINE 86 HAS AREA OF CORROSION - [SDR IXXA20260812001](https://openairdocs.org/sdr/IXXA20260812001.md): Longeron Splice · corroded · Aug 12, 2026 · N379AZ · Boeing 767323 · Fuselage Main, Longeron/Stringer > LEFT OVERWING LONGERON IS CORRODED BETWEEN BS 930 - 940. - [SDR IXXA20260811002](https://openairdocs.org/sdr/IXXA20260811002.md): Duct · cracked · Aug 11, 2026 · N379AZ · Boeing 767323 · Nacelle/Pylon, Main Frame > INBD CORE COWL EXHAUST DUCT IS CHAFED ON THE LEADING EDGE - [SDR IXXA20260811001](https://openairdocs.org/sdr/IXXA20260811001.md): Frame · gouged · Aug 11, 2026 · N379AZ · Boeing 767323 · Wing Spar > PANEL 573BB AFT FRAME IS SEVERELY GOUGED - [SDR IXXA20260806001](https://openairdocs.org/sdr/IXXA20260806001.md): Skin · corroded · Aug 6, 2026 · N379AZ · Boeing 767323 · Fuselage Main, Plate/Skin > CORROSION ON SKIN AT BS 955 WHERE THE PICKLE FORK COMES IN CONTACT BELOW THE FLOOR. - [SDR IXXA2026080501](https://openairdocs.org/sdr/IXXA2026080501.md): Access Panel · worn · Aug 5, 2026 · N379AZ · Boeing 767323 · Wing, Plate/Skin > LEFT WING T/E PANEL 561PB HAS FASTENER HOLE ELONGATED - [SDR IXXA20260803001](https://openairdocs.org/sdr/IXXA20260803001.md): Stiffener · chafed · Aug 3, 2026 · N379AZ · Boeing 767300 · Nacelle/Pylon Miscellaneous Structure > #1 PYLON HYDRAULIC BAY LOWER RIBS ARE CHAFFED FROM HYDRAULIC SUPPLY HOSE. - [SDR IXXA20260801001](https://openairdocs.org/sdr/IXXA20260801001.md): Rib · cracked · Aug 1, 2026 · N379AZ · Boeing 767323 · Wing, Rib/Bulkhead > RIB AT W/S/ 499.60 CRACKED L/W L/E - [SDR IXXA20260731002](https://openairdocs.org/sdr/IXXA20260731002.md): Bracket · cracked · Jul 31, 2026 · N379AZ · Boeing 767323 · Fuselage Main, Structure > WHILE REMOVING MDCD FWD LWR CORNER SEAL DEPRESSOR, FOUND MOUNTING CHANNEL/BRACKET TO BE CRACKED. - [SDR IXXA20260731001](https://openairdocs.org/sdr/IXXA20260731001.md): Frame · chafed · Jul 31, 2026 · N379AZ · Boeing 767323 · Nacelle/Pylon, Main Frame > THE UPPER CHORD IS DEEPLY CHAFED, ON THE BULKHEAD ON TOP OF THE RIGHT PYLON, LOCATED AT THE FWD O/B CORNER OF THE 441BT PANEL. - [SDR IXXA20260730003](https://openairdocs.org/sdr/IXXA20260730003.md): Splice Plate · cracked · Jul 30, 2026 · N379AZ · Boeing 767323 · Wing, Plate/Skin > RW LE STA 258 LOWER SPAR FOUND CRACKED. LOWER SPLICE PLATE WAS REMOVED, FABRICATED, AND INSTALLED. REFERENCE AMES WO N379AZ-25 NR 192946-0600-0024 - [SDR IXXA20260730002](https://openairdocs.org/sdr/IXXA20260730002.md): Skin Panel · worn · Jul 30, 2026 · N379AZ · Boeing 767323 · Wing, Plate/Skin > RW L/E PANEL 611ST HAS 1EA FASTENER HOLE ELONGATED. ELONGATED HOLE WAS REAMED OVERSIZED TO.3745 IN. A FREEZE PLUG WAS THEN INSTALLED. THE ORIGINAL FASTENER HOLE WAS THEN LOCATED, DRILLED AND COUNTERSUNK TO ACCEPT THE OEM FASTENER FOR PANEL INSTALLATION. REFER - [SDR IXXA20260730001](https://openairdocs.org/sdr/IXXA20260730001.md): Pad · gouged · Jul 30, 2026 · N379AZ · Boeing 767323 · Nacelle/Pylon, Main Frame > NUMBER 1 ENGINE INBD FAN COWL HAS GOUGED RUB PAD - [SDR IXXA20260722002](https://openairdocs.org/sdr/IXXA20260722002.md): Former · cracked · Jul 22, 2026 · N379AZ · Boeing 767323 · Wing Main, Frame Structure > RIB AT W.S. 430.00 CRACKED L/W L/E - [SDR IXXA20260722001](https://openairdocs.org/sdr/IXXA20260722001.md): Seal Depressor · bent · Jul 22, 2026 · N379AZ · Boeing 767323 · Fuselage Main, Structure > MAIN DECK CARGO DOOR CUTOUT, AFT LWR CORNER SEAL DEPRESSOR IS BENT UP - [SDR IXXA20260717001](https://openairdocs.org/sdr/IXXA20260717001.md): Support Angle · cracked · Jul 17, 2026 · N379AZ · Boeing 767323 · Leading Edge Devices > NR 7 SLAT, T/E SUPPORT ANGLE CRACKED JUST INBD OF CENTER AUX ARM. - [SDR IXXA2026072701](https://openairdocs.org/sdr/IXXA2026072701.md): Angle · cracked · Jun 3, 2026 · N379AZ · Boeing 767323 · Fuselage Miscellaneous Structure > VERTICAL ANGLE ON FRONT SIDE OF FRAME 1085 RBL 26 IS CRACKED - [SDR IXXA20260517043](https://openairdocs.org/sdr/IXXA20260517043.md): Crank Assy · loose · May 17, 2026 · N379AZ · Boeing 767323 · Flight Compartment Windows > R2 WINDOW CRANK SHIFTS SIDE TO SIDE WHEN OPENING WINDOW. APPEARS TO BE LOOSE. TIGHTENED AND RETORQUED R2 WINDOW CRANK IAW B767 SRM 51-40-02 AND B767 AIPC 56-11-04-01. OPERATIONAL CHECK GOOD. - [SDR IXXA202603027017](https://openairdocs.org/sdr/IXXA202603027017.md): Handle · stiff · Feb 27, 2026 · N379AZ · Boeing 767323 · Passenger/Crew Doors > CREW ENTRY DOOR ARMED LEVER IS EXTREMELY DIFFICULT TO LOCK. OPERATIONAL CHECK OF L1 DOOR IAW AMM 52-11-00-862-004, NOTED NO FAULTS. - [SDR IXXA20260223015](https://openairdocs.org/sdr/IXXA20260223015.md): Latch · sticking · Feb 23, 2026 · N379AZ · Boeing 767323 · Passenger/Crew Doors > CREW ENTRY DOOR LOCK LATCH STICKS TO STOW/LOCK. SOMETIMES CANNOT LOCK DOOR. ACCOMPLISHED INTERNAL AND EXTERNAL MANUAL OPERATION OF THE L1 ENTRY/SERVICE DOOR IN ACCORDANCE WITH B767 AMM 52-11-00. L1 DOOR OPENS, CLOSES, LOCKS AND UNLOCKS AS INTENDED. - [SDR IXXA20250319014](https://openairdocs.org/sdr/IXXA20250319014.md): Indicator · malfunctioned · Mar 17, 2025 · N379AZ · Boeing 767323 · Central Computers > CREW REPORTED ON TAXI OUT BOTH EICAS SCREENS BLANK FOLLOWED BY COMPACT MODE. UPPER EICAS BLANK THEN HOT ELECTRICAL SMOKE NOTED. CREW ELECTED A BLOCK RETURN FOR FAULT ISOLATION AND CORRECTIVE ACTIONS. AIRCRAFT GROUNDED FOR MAINTENANCE. GENERAL VISUAL INSPECTI - [SDR IXXA2024091201](https://openairdocs.org/sdr/IXXA2024091201.md): Panel · cracked · Sep 12, 2024 · N379AZ · Boeing 767323 · Fuselage Miscellaneous Structure > P33 REAR PANEL CRACKED STA 303 LBL11. - [SDR IXXA2024091001](https://openairdocs.org/sdr/IXXA2024091001.md): Bracket · cracked · Sep 10, 2024 · N379AZ · Boeing 767323 · Wing Miscellaneous Structure > LEFT WING LE BRACKET LES 475 CRACKED. - [SDR IXXA2024090901](https://openairdocs.org/sdr/IXXA2024090901.md): Panel · worn · Sep 9, 2024 · N379AZ · Boeing 767323 · Fuselage Miscellaneous Structure > THE FOOTREST PANELS LOCATED WHERE THE PILOT PLACES HIS FEET IS WORN - [SDR IXXA20240906001](https://openairdocs.org/sdr/IXXA20240906001.md): Sleeve · delaminated · Sep 6, 2024 · N379AZ · Boeing 767323 · Engine Thrust Reverser > #1 ENGINE OUTBOARD T/R SLEEVE AFT UPPER EDGE COMPOSITE DELAMINATED. - [SDR IXXA2024090502](https://openairdocs.org/sdr/IXXA2024090502.md): Skin · damaged · Sep 5, 2024 · N379AZ · Boeing 767323 · Wing, Longeron/Stringer > HOLE INBD OF STRINGER 6.5 IS OVERSIZED - [SDR IXXA2024090501](https://openairdocs.org/sdr/IXXA2024090501.md): Door Sill · corroded · Sep 5, 2024 · N379AZ · Boeing 767323 · Fuselage Miscellaneous Structure > CORROSION AT THE UPPER CHORD AT LOWER SILL FOR THE CUTOUT FOR THE BULK CARGO DOOR STA 1426, S33L - [SDR IXXA2024090403](https://openairdocs.org/sdr/IXXA2024090403.md): Skin · corroded · Sep 4, 2024 · N379AZ · Boeing 767323 · Fuselage Main, Plate/Skin > LAP SEAM AT S36R BETWEEN STA. 1197+66 AND 1197+88 CORROSION - [SDR IXXA2024090402](https://openairdocs.org/sdr/IXXA2024090402.md): Skin · damaged · Sep 4, 2024 · N379AZ · Boeing 767323 · Leading Edge Devices > #5 SLAT HAS COMPOSITE REPAIR @ I/B END - [SDR IXXA2024090401](https://openairdocs.org/sdr/IXXA2024090401.md): Stringer · corroded · Sep 4, 2024 · N379AZ · Boeing 767323 · Fuselage Main, Longeron/Stringer > ALC STRINGER 36R STA 1197+72 TO 1197+74 CORROSION - [SDR IXXA2024091101](https://openairdocs.org/sdr/IXXA2024091101.md): Skin · cracked · Aug 14, 2024 · N379AZ · Boeing 767323 · Fuselage Main, Plate/Skin > RI LOWERR AFT DOOR CORNER CUTOUT CRACKED - [SDR IXXA2024090902](https://openairdocs.org/sdr/IXXA2024090902.md): Diffuser · deteriorated · Aug 14, 2024 · N379AZ · Boeing 767323 · Flight Compartment Equipment > THE FOOTREST DIFFUSER ASSMBLIES ARE WORE, LOCATED WHERE THE F/O PLACES HIS/HER FEET ON THE FLOOR BELOW THE RUDDER PEDALS. PART NUMBERS 214T1119-10 AND -11 - [SDR IXXA20240731054](https://openairdocs.org/sdr/IXXA20240731054.md): Sliding Window · out of adjust · Jul 27, 2024 · N379AZ · Boeing 767323 · Flight Compartment Windows > PRE-DEPARTURE, CREW REPORTED FO WINDOW NOT FULLY CLOSING. STOPS AT "CLOSED" HANDLE 1 SHY OF FULLY CLOSED. SUBSEQUENT TO GENERAL VISUAL INSPECTION, LINE MAINTENANCE IDENTIFIED #2 WINDOW OUT OF ADJUSTMENT. WINDOW READJUSTED PER B767 AMM 56-11-02. OPERATIONAL CHE - [SDR IXXA202407152049](https://openairdocs.org/sdr/IXXA202407152049.md): Carriage · cracked · Jul 12, 2024 · N379AZ · Boeing 767323 · Flight Compartment Windows > FOLLOWING ROUTINE MAINTENANCE, FIRST OFFICER'S OPENABLE WINDOW SLIDING TRACK BRACKET CRACKED IN TWO PLACES. REMOVED AND REPLACED FIRST OFFICER'S #2 OPENABLE WINDOW SLIDING TRACK BRACKET IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-04. OPERATIONAL CHECK - [SDR IXXA20230901161](https://openairdocs.org/sdr/IXXA20230901161.md): Panel · cracked · Sep 10, 2023 · N379AZ · Boeing 767323 · Wing Structure > DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 15 INCH CRACK FOUND AT LEFT WING STATION 587 LEADING EDGE. AIRCRAFT GROUNDED. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE AT STATION 587.15 IAW B767-300 SRM 51-70- - [SDR IXXA2023091160](https://openairdocs.org/sdr/IXXA2023091160.md): Panel · cracked · Sep 10, 2023 · N379AZ · Boeing 767323 · Wing Structure > DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 8 INCH CRACK FOUND AT LEFT WING STATION 571 LEADING EDGE. AIRCRAFT GROUNDED. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE AT STATION 571.8 IAW B767-300 SRM 51-70- - [SDR IXXA20230911059](https://openairdocs.org/sdr/IXXA20230911059.md): Panel · cracked · Sep 10, 2023 · N379AZ · Boeing 767323 · Wing Structure > DURING REPAIRS OF DAMAGES TO THE #5 SLAT INBOARD SIDE, LINE MAINTENANCE REPORTED 18 INCH CRACK FOUND AT LEFT WING STATION 464 LEADING EDGE. REMOVED AND REPAIRED DAMAGE ON LEFT WING FIXED LEADING EDGE SEGMENT BY WAY OF A COMPOSITE REPAIR UNDER VACUUM IAW B767 - [SDR IXXA20230905052](https://openairdocs.org/sdr/IXXA20230905052.md): Unknown · unknown · Sep 2, 2023 · N379AZ · Boeing 767323 · Air Conditioning System > ON DESCENT PASSING THROUGH 11000 UNTIL 9000, CREW REPORTED A HARSH RUBBER SMELL IN THE FLIGHT STATION. LANDING WAS WITHOUT INCIDENT AND NO PRECAUTIONARY ACTIONS. ON ARRIVAL, ODOR DISSIPATED. AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. COMPLIED WITH A - [SDR IXXA20230905051](https://openairdocs.org/sdr/IXXA20230905051.md): Unknown · unknown · Sep 2, 2023 · N379AZ · Boeing 767323 · Cabin Cooling System > POST FLIGHT CREW REPORTED, AFTER ARRIVING AT GATE STRONG RUBBER ODOR WAS NOTED IN THE FLIGHT STATION. INITIATED DEFERRAL MAINTENANCE ITEM 44639 OF THE LEFT AIR CONDITIONING PACK IAW B767 200/300 MINIMUM EQUIPMENT LIST 21-51-01-01. COMPLIED WITH CONDITIONAL IN - [SDR 2023F00219](https://openairdocs.org/sdr/2023F00219.md): Drive Shaft · grooved · Jul 7, 2023 · N379AZ · Boeing 767323 · Engine (Turbine/Turboprop) > ENGINE WAS REMOVED DUE TO END OF LEASE AND TRANSPORTED TO ENGINE SERVICE FACILITY FOR OVERHAUL. ACCORDING TO THE ENGINE TEARDOWN REPORT A LINE INSPECTOR FOUND A BOLT BETWEEN THE RADIAL DRIVE SHAFT (RDS) AND THE FAN FRAME. THE BOLT HAS CAUSED MAJOR DAMAGE TO TH - [SDR IXXA2023022601](https://openairdocs.org/sdr/IXXA2023022601.md): Skin · cracked · Feb 26, 2023 · N379AZ · Boeing 767300 · Passenger/Crew Doors > EXTERNAL SKIN FOUND CRACKED L! DOOR CUTOUT - [SDR IXXA20222001](https://openairdocs.org/sdr/IXXA20222001.md): Frame · none · Sep 20, 2022 · N379AZ · Boeing 767 · Fuselage Main, Frame > STATION 654 BETWEEN STRINGER 7R - 8R HAS ELONGATED HOLES. - [SDR IXXA20221404](https://openairdocs.org/sdr/IXXA20221404.md): Shear Plate · corroded · Sep 14, 2022 · N379AZ · Boeing 767 · Fuselage Structure (General) > FWD ENTRY SHEAR PLATE HAS CORROSION. - [SDR IXXA20221403](https://openairdocs.org/sdr/IXXA20221403.md): Stringer Splice · none · Sep 14, 2022 · N379AZ · Boeing 767 · Fuselage Main, Floor Beam > FLOOR BEAM FUS STA 654 STR 5R STRINGER SPLICE HAS ELONGATED HOLES. - [SDR IXXA20221402](https://openairdocs.org/sdr/IXXA20221402.md): Stringer Splice · none · Sep 14, 2022 · N379AZ · Boeing 767 · Fuselage Main, Floor Beam > FLOOR BEAM FUS 654 STR 6 HAS ELONGATED HOLES. Next page: https://openairdocs.org/aircraft/N379AZ/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N379AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N379AZ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.