# Service difficulty reports: N617AZ A list on [N617AZ](https://openairdocs.org/aircraft/N617AZ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA20260907079](https://openairdocs.org/sdr/IXXA20260907079.md): Sliding Window · inoperative · Sep 7, 2026 · N617AZ · Boeing 767332 · Flight Compartment Windows > FIRST OFFICER'S SLIDING WINDOW WILL NOT CLOSE PROPERLY. ACCOMPLISHED ADJUSTMENT OF FIRST OFFICER'S #2 WINDOW IN ACCORDANCE WITH B767 AMM 56-11-02-825-122. OPERATIONAL CHECK GOOD. - [SDR IXXA20260622054](https://openairdocs.org/sdr/IXXA20260622054.md): A/C Pack · inoperative · Jun 22, 2026 · N617AZ · Boeing 767332 · Cabin Cooling System > RETURNED TO BLOCK DUE TO LEFT PACK TEMPERATURE EICAS, LEFT PACK INOPERATIVE AND SMOKE IN THE COCKPIT. AIRCRAFT GROUNDED FOR INSPECTION AND MAINTENANCE. ACCOMPLISHED PHASE 1 CONDITIONAL INSPECTION IN ACCORDANCE WITH B767 AMM 05-51-00 AND B767 AMM 21-00-21-102- - [SDR IXXA2026053044](https://openairdocs.org/sdr/IXXA2026053044.md): Stud · missing · May 30, 2026 · N617AZ · Boeing 767332 · Escape Slide > EMERGENCY ESCAPE SLIDE PANEL MISSING FASTNER APPROXIMATELY LEFT FORWARD WIND. APPLIED SPEED TAPE TO PANEL IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL 8.14D. TIME LIMITED ITEM 73720 INITIATED IAW ATI-8.14D-SPEED-TAPE DUE 21 SEPT 2026. REPLACED FASTENER O - [SDR IXXA2026060153044](https://openairdocs.org/sdr/IXXA2026060153044.md): Fastener · missing · May 30, 2026 · N617AZ · Boeing 767332 · Escape Slide > EMERGENCY ESCAPE SLIDE PANEL MISSING FASTNER APPROXIMATELY LEFT FORWARD WIND. APPLIED SPEED TAPE TO PANEL IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL 8.14D. TIME LIMITED ITEM 73720 INITIATED IN ACCORDANCE WITH ATI-8.14D-SPEED-TAPE DUE 20 SEPTEMBER 2026. - [SDR IXXA202605190001](https://openairdocs.org/sdr/IXXA202605190001.md): Bracket · cracked · May 19, 2026 · N617AZ · Boeing 767332 · Leading Edge Devices > LEFT WING L/E NR 6 SLAT LOWER TRAILING CLOSEOUT PANEL SUPPORT BRACKET JUST OTBD OF MID AUX TRACK, IS CRACKED. REFERENCE AMES WO N617AZ-20 NR 192362-0500-0011 - [SDR IXXA20260519002](https://openairdocs.org/sdr/IXXA20260519002.md): Web · cracked · May 19, 2026 · N617AZ · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure > NR 2 ENGINE STRUT FAIRING 447DB OTBD STIFFENER AND WEB CRACKED. - [SDR IXXA20260519001](https://openairdocs.org/sdr/IXXA20260519001.md): Hinge · worn · May 19, 2026 · N617AZ · Boeing 767332 · Nacelle/Pylon, Main Frame > O/B HYDRAULIC BAY DOOR FWD HINGE EXCESSIVE PLAY - [SDR IXXA2026051601](https://openairdocs.org/sdr/IXXA2026051601.md): Skin · chafed · May 16, 2026 · N617AZ · Boeing 767332 · Nacelle/Pylon, Plate/Skin > CHAFE DAMAGE ON THE NR 2 ENGINE, FWD NACELLE STRUT UPPER SKIN AT NSTA 150.9 - [SDR IXXA20260510003](https://openairdocs.org/sdr/IXXA20260510003.md): Cam · corroded · May 10, 2026 · N617AZ · Boeing 767332 · Cargo/Baggage Doors > MAIN DECK CARGO DOOR LATCH CAM HOOK AT STA. 480 HAS CORROSION REFERENCE AMES WO N617AZ-20 NR 19236208000004 - [SDR IXXA20260510002](https://openairdocs.org/sdr/IXXA20260510002.md): Cam · corroded · May 10, 2026 · N617AZ · Boeing 767332 · Cargo/Baggage Doors > MAIN CARGO DECK DOOR LATCH CAM HOOK AT STA. 430 HAS CORROSION REFERENCE AMES WO N617AZ-20 NR 192362-0800-0005 - [SDR IXXA20260510001](https://openairdocs.org/sdr/IXXA20260510001.md): Frame · cracked · May 10, 2026 · N617AZ · Boeing 767332 · Fuselage Main, Frame > FRAME AT REAR OF HYD BAY NAC 375, IB ANGLE ON AFT SIDE OF FRAME IS CRACKED. - [SDR IXXA20260508001](https://openairdocs.org/sdr/IXXA20260508001.md): Frame · cracked · May 8, 2026 · N617AZ · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > FRAME AT REAR OF HYD BAY NAC 375, OB ANGLE ON AFT SIDE OF FRAME IS CRACKED. REFERENCE AMES WO N617AZ-20 NR 192362-0400-0050 - [SDR IXXA20251013065](https://openairdocs.org/sdr/IXXA20251013065.md): Latch · faulted · Oct 13, 2025 · N617AZ · Boeing 767332 · Flight Compartment Windows > CREW REPORTED RIGHT SIDE EMERGENCY EXIT WINDOW EXTERNAL LATCH WILL NOT STAY LATCHED. ADJUSTED RIGHT SIDE WINDOW EMERGENCY EXIT EXTERNAL HANDLE SPRING PIN IN ACCORDANCE WITH IAI SUPPLEMENTAL MAINTENANCE MANUAL B767 56-11-04. OPERATIONAL CHECK GOOD. - [SDR IXXA202509198054](https://openairdocs.org/sdr/IXXA202509198054.md): Seal · missing · Sep 18, 2025 · N617AZ · Boeing 767332 · Emergency Equipment > PORTABLE BREATHING EQUIPMENT SEALS ARE NOT ATTACHED. REINSTALLED EXISTING SERVICEABLE PORTABLE BREATHING EQUIPMENT WITH NEW SECURITY SEAL IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL 9.10. - [SDR IXXA20250219008](https://openairdocs.org/sdr/IXXA20250219008.md): Lamp · inoperative · Feb 16, 2025 · N617AZ · Boeing 767332 · Emergency Lighting > FOLLOWING DAILY CHECK INSPECTIONS, LINE MAINTENANCE REPORTED RIGHT OVERHEAD EMERGENCY LIGHT OUT. IN FLIGHT DECK, RIGHT OVERHEAD EMERGENCY LIGHT RELAMPED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 33-51-00. NO ADDITIONAL FAULTS NOTED. - [SDR IXXA20241025070](https://openairdocs.org/sdr/IXXA20241025070.md): Control Panel · failed · Oct 24, 2024 · N617AZ · Boeing 767332 · Central Warning > DURING CRUISE "FWD EQUIPMENT COOLING" DISPLAYED & CLEARED (3-5 MINUTES). SUBSEQUENT TO THE 1ST FAULT MESSAGE DISPLAY AND CLEARING, FWD EQPT OVHT ANNUNICIATED. IN CREW'S APPLICATION OF ATI QRH PROCEDURES FOR FWD EQPT OVHT MESSAGE. CABIN PRESSURE & CABIN PRESS - [SDR IXXA2024060702](https://openairdocs.org/sdr/IXXA2024060702.md): Rib · damaged · May 23, 2024 · N617AZ · Boeing 767332 · Wing, Rib/Bulkhead > AFTER REMOVAL OF THE LEFT WING LEADING EDGE SKIN, AN ELONGATED FASTENER HOLE WAS NOTED AT OSS 1017 THROUGH THE LEADING EDGE RIB AND THE UPPER LEADING EDGE SKIN PANEL SPLICE PLATE. THE ELONGATED HOLE WAS REAMED TO A TRUE AND ROUND CONDITION WITH A DIAMETER OF 0 - [SDR IXXA2024060701](https://openairdocs.org/sdr/IXXA2024060701.md): Rib · damaged · May 20, 2024 · N617AZ · Boeing 767332 · Engine Thrust Reverser > #1 ENGINE INBOARD THRUST REVERSER INTERNAL CORE COWL ZEE RIB IS DAMAGED, POSSIBLY FROM CONTACT WITH ENGINE COMPONENTS, ACTAUL CAUSE IS UNKNOWN. NO DAMAGE WAS FOUND ON THE ENGINE. THE TR DAMAGE IS 15 INCHES UP FROM THE LOWER BIFURCATION. - [SDR IXXA2024060503](https://openairdocs.org/sdr/IXXA2024060503.md): Fitting · gouged · May 20, 2024 · N617AZ · Boeing 767332 · Engine Thrust Reverser > #1 ENGINE INBD T/R FITTING HOUSING (POD FITTING) AROUND THE OPEN UP ACTUATORS ROD END HAS MULTIPLE COUGES - [SDR IXXA2024061402](https://openairdocs.org/sdr/IXXA2024061402.md): Skin · gouged · May 19, 2024 · N617AZ · Boeing 767332 · Nacelle/Pylon, Plate/Skin > #2 PYLON SKIN AND BULLNOSE PANEL 441AT RUBBING AND CAUSED GOUGES ON THE SKIN AT THE FORWARD EDGE - [SDR IXXA2024060502](https://openairdocs.org/sdr/IXXA2024060502.md): Skin · gouged · May 17, 2024 · N617AZ · Boeing 767332 · Wing, Plate/Skin > R/H WING L/E SKIN JUST OTBD OF THE PYLON HAS 4EA HEAVILY GOUGED AREAS ON THE UPPER SUFACE IN LINE WITH #8 SLAT INBD ROTARY ACTUATOR TIEROD AND 1EA FASTENER MISSING THROUGH SKIN JUST INBD OF THE TELESCOPING TAI DUCT AND 9 DAMAGED FASTENER HOLES. BOTH INBOARD A - [SDR IXXA2024061101](https://openairdocs.org/sdr/IXXA2024061101.md): Skin · damaged · May 16, 2024 · N617AZ · Boeing 767332 · Wing, Plate/Skin > LW UPPER LEADING EDGE SKIN HAS 6 FASTENERS PULLED THRU THE SKIN JUST O/B OF O/B SLAT ROTARY ACTUATOR - [SDR IXXA2024060501](https://openairdocs.org/sdr/IXXA2024060501.md): Skin · gouged · May 16, 2024 · N617AZ · Boeing 767332 · Wing, Plate/Skin > LW LEADING EDGE SKIN IS GOUGED AT OB SIDE AFT OF #6 SLAT, 1.25 INCHES FROM THE INBOARD EDGE, 23 INCHES FROM THE AFT EDGE AND 1 INCH IN WIDTH - [SDR IXXA2024060505](https://openairdocs.org/sdr/IXXA2024060505.md): Skin · damaged · May 15, 2024 · N617AZ · Boeing 767332 · Wing, Plate/Skin > DURING ROUTINE MAINTENANCE IN GSO, MAINTENANCE DISCOVERED STATIC DISCHARGE DAMAGE TO THE MID TRAILING EDGE OF THE LEFT-HAND WINGLET. THE DAMAGE WAS REMOVED WITH A 0.130-INCH EDGE BLEND PER REF /C/ AND FOUND TO BE BEYOND PUBLISHED LIMITS. THE TRAILING EDGE IS - [SDR IXXA2024060504](https://openairdocs.org/sdr/IXXA2024060504.md): Link · gouged · May 15, 2024 · N617AZ · Boeing 767332 · Main Landing Gear Strut/Axle/Truck > RH MLG LOWER SIDE STRUT LINK AND LOWER LOCK LINKS ARE GOUGED DUE TO CONTACT WITH EACH OTHER. REWORK BLENDOUT OF LOWER STRUT LINK AREA 1- 3.675" LENGTH X 0.503" WIDTH, AREA 2- 3.555" LENGTH X 0.518 WIDTH - [SDR IXXA20240311012](https://openairdocs.org/sdr/IXXA20240311012.md): Battery · no test · Mar 11, 2024 · N617AZ · Boeing 767332 · Emergency Equipment > DURING SCHEDULED MAINTENANCE, EMERGENCY FLASHLIGHT BATTERY INOPERATIVE. EMERGENCY LIGHTING FLASHLIGHT BATTERY REMOVED AND REPLACED PER B767 AMM 25-64--02. DEFERRAL MAINTENANCE ITEM 50037 CLEARED. - [SDR IXXA20231015071](https://openairdocs.org/sdr/IXXA20231015071.md): Control Card · faulted · Oct 11, 2023 · N617AZ · Boeing 767332 · Fuel Controlling System > ON INITIAL DESCENT WHEN THRUST LEVERS WERE STARTING TO GO TO IDLE, LT ENG EXHIBITED INTENSE COMPRESSOR STALL AT 36000. AFTER COMPRESSOR STALL, ENGINE PARAMETERS STAYED IN NORMAL RANGE. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT & ACFT GROUNDED. BORESCOPE INS - [SDR IXXA2023011001](https://openairdocs.org/sdr/IXXA2023011001.md): Skin · gouged · Apr 10, 2023 · N617AZ · Boeing 767332 · Fuselage Structure (General) > GOUGE ON DOUBLER AT FWD LOWER CORNER BY AFT CARGO DOOR ## 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 = 'N617AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N617AZ/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.