# Service difficulty reports: N229AZ A list on [N229AZ](https://openairdocs.org/aircraft/N229AZ.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 · 71 reports - [SDR IXXA20260613051](https://openairdocs.org/sdr/IXXA20260613051.md): Cradle · broken · Jun 13, 2026 · N229AZ · Boeing 767323 · Emergency Equipment > CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER BOTTOM BROKEN. PLACED ON DEFERRAL 74109 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-25-63-04-01. DUE 23 JUNE 2026. REMOVED AND REPLACED CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER IN ACCORDANCE WITH B767 SRM 51-4 - [SDR IXXA20251101071](https://openairdocs.org/sdr/IXXA20251101071.md): Inertia Reel · not reported · Nov 1, 2025 · N229AZ · Boeing 767323 · Emergency Equipment > NUMBER 6 EMERGENCY INERTIAL REEL REQUIRES REPLACEMENT. PLACED ON DEFERRAL 67545 MINIMUM EQUIPMENT LIST 25-61-01-01 CATEGORY C. DUE 12 NOVEMBER 2025. REMOVED AND REPLACED #6 INERTIA DESCENT DEVICE IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 25-61-05. NO OTHE - [SDR IXXA20250828049](https://openairdocs.org/sdr/IXXA20250828049.md): Bracket · broken · Aug 28, 2025 · N229AZ · Boeing 767323 · Emergency Equipment > CENTER PEDESTAL EMERGENCY FLASHLIGHT HOLDER BROKEN. MAINTENANCE PLACED ON DEFERRAL 65656 MINIMUM EQUIPMENT LIST 25-63-04-01 CATEGORY C. DUE 07 SEPTEMBER 2025. IN ACCORDANCE WITH B767 FIM 52-71 FAULT TREE 816 AND B767 WDM 52-71-12 BITE PROCEDURE FOR PROXIMITY S - [SDR IXXA20250812043](https://openairdocs.org/sdr/IXXA20250812043.md): Relay · unknown · Aug 12, 2025 · N229AZ · Boeing 767323 · Electrical Power System > MULTIPLE EICAS MESSAGE WITH STANDBY POWER AUTO DURING DESCENT FL290. EMERGENCY DECLARED TO KCVG. AIRCRAFT LANDED WITHOUT INCIDENT NO OTHER PRECAUTIONARY ACTIONS TAKEN. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE. LINE MAINTENANCE REMOVED AND REPLACED - [SDR IXXA20250713030](https://openairdocs.org/sdr/IXXA20250713030.md): Computer · faulted · Jul 13, 2025 · N229AZ · Boeing 767323 · Central Computers > AIR TURN BACK INITIATED DUE TO MULITPLE ENGINE INDICATION FLUCTUATIONS FOR EXHAUST GAS TEMPERATURE, OIL PRESSURE, OIL TEMPERATURE AND OIL QUANTITY. STATUS MESSAGE EICAS DISAGREE ON THE GROUND AFTER LANDING. NO EMERGENCY DELCARED. SYSTEM DEFERRED 64215, MEL CAT - [SDR IXXA20250502001](https://openairdocs.org/sdr/IXXA20250502001.md): Skin · dented · May 1, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Plate/Skin > EXTERIOR FUSELAGE SHIN HAS SEVERAL OUTWARDLY PROTUDING DENTS BETWEEN STA 654+44 - STA 654+68, AT STRINGERS S-R1 THOUGH S-4L. 8110-3 ISSUED. - [SDR IXXA20250430006](https://openairdocs.org/sdr/IXXA20250430006.md): Floor Support · gouged · Apr 30, 2025 · N229AZ · Boeing 767323 · Fuselage Miscellaneous Structure > APPROX 8" AFT OF AFT ENTRY DOOR L2 FLOOR STRUCTURE HAS GOUGE - [SDR IXXA20250430005](https://openairdocs.org/sdr/IXXA20250430005.md): Skin · chafed · Apr 30, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Plate/Skin > #1 PYLON UNDER PANEL 431AT SKIN HAS CHAFFING MARK AT NAC STA 155 APPROX AS MARKED - [SDR IXXA20250430004](https://openairdocs.org/sdr/IXXA20250430004.md): Skin · worn · Apr 30, 2025 · N229AZ · Boeing 767323 · Wing, Plate/Skin > L WING WINGLET L/E PANEL HAS 1 FASTENER HOLE THAT IS OVER SIZED - [SDR IXXA20250430003](https://openairdocs.org/sdr/IXXA20250430003.md): Stringer · gouged · Apr 30, 2025 · N229AZ · Boeing 767323 · Wing, Longeron/Stringer > R WING INTERNAL STRINGER L10 HAS 1 FASTENER HOLE AT APPROX WS 850 RIB 26 WITH GOUGE DAMAGE AT FASTENER HOLE - [SDR IXXA20250430002](https://openairdocs.org/sdr/IXXA20250430002.md): Stiffener · dented · Apr 30, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Structure > MAIN CABIN LONGITUDINAL STIFFER ABOVE CANTED BULKHEAD AT APPROX STA 1021 HAS 3 EACH DENTS AT APPROX RBL30 - [SDR IXXA20250430001](https://openairdocs.org/sdr/IXXA20250430001.md): Stiffener · dented · Apr 30, 2025 · N229AZ · Boeing 767323 · Fuselage Miscellaneous Structure > MAIN CABIN LONGITUDINAL STIFFENER ABOVE CANTED BULKHEAD AT APPROX BS 1043+14 RBL 23 HAS DENT/GOUGE ON TOP AREA - [SDR IXXA20250421002](https://openairdocs.org/sdr/IXXA20250421002.md): Floor Panel · delaminated · Apr 18, 2025 · N229AZ · Boeing 767323 · Fuselage Floor Panel > FLOOR PANEL AT L2 DOORWAY STA 1461-1582 LBL 60-80 HAS PUNCTURE. HAECO WO 32011 NR 35279 - [SDR IXXA20250417001](https://openairdocs.org/sdr/IXXA20250417001.md): Former · cracked · Apr 17, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > R/H WING L/E AREA NOSE FORMER ANGLE IS CRACKED AT APPROX LES490. REF HAECO WO 320011 NR 34425 - [SDR IXXA20250429003](https://openairdocs.org/sdr/IXXA20250429003.md): Frame · gouged · Apr 16, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Frame/Spar/Rib > #2 ENG I/B CORE COWL HAS GOUGE ON 4TH FRAME FROM FWD - [SDR IXXA20250429002](https://openairdocs.org/sdr/IXXA20250429002.md): Frame · gouged · Apr 16, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Frame/Spar/Rib > #2 ENG I/B CORE COWL HAS GOUGE ON 2ND FRAME FROM FWD - [SDR IXXA20250429001](https://openairdocs.org/sdr/IXXA20250429001.md): Frame · gouged · Apr 16, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Frame/Spar/Rib > #2 ENG I/B CORE COWL HAS GOUGE ON 3RD FRAME FROM FWD - [SDR IXXA20240421003](https://openairdocs.org/sdr/IXXA20240421003.md): Attach Bracket · cracked · Apr 16, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Attach Fittings > RIGHT UPPER WING TO BODY PANEL 196DR PANEL LANDING ATTACH BRACKET IS CRACKED. REF HAECO WO 320011 NON ROUTINE 35368 - [SDR IXXA20250427001](https://openairdocs.org/sdr/IXXA20250427001.md): Former · cracked · Apr 11, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > RH WING NOSE FORMER IS BROKEN AT OSS 429. REF HAECO WO 320011 NR 35357 - [SDR IXXA20250422001](https://openairdocs.org/sdr/IXXA20250422001.md): Former · cracked · Apr 11, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > RIGHT WING LEADING EDGE NOSE FORMER IS BROKEN AT OSS 456. HAECO WO 320011 AND NR 35356 - [SDR IXXA20250410002](https://openairdocs.org/sdr/IXXA20250410002.md): Bracket · cracked · Apr 9, 2025 · N229AZ · Boeing 767323 · Wing Miscellaneous Structure > 5 SLAT O/B L/E PANEL NOSE FORMER BRACKET CRACKED AND FASTENER PULLING THROUGH - [SDR IXXA20250408002](https://openairdocs.org/sdr/IXXA20250408002.md): Splice · gouged · Apr 8, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Floor Beam > FWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES STA 654+110, LBL 32, WL 196 - [SDR IXXA202504080101](https://openairdocs.org/sdr/IXXA202504080101.md): Splice · gouged · Apr 8, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Floor Beam > FWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES, STA 654+88, RBL 11 WL 196 - [SDR IXXA20250410001](https://openairdocs.org/sdr/IXXA20250410001.md): Access Panel · corroded · Apr 7, 2025 · N229AZ · Boeing 767323 · Wing, Plate/Skin > RIGHT WING LOWER ACCESS PANEL 632AB IS WORN AND CORRODED - [SDR IXXA20250423001](https://openairdocs.org/sdr/IXXA20250423001.md): Window Frame · damaged · Mar 28, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Structure > MAIN CABIN WINDOW FRAME AT STA 808-828 HAS THREAD DAMAGE - [SDR IXXA20250418001](https://openairdocs.org/sdr/IXXA20250418001.md): Floor Support · corroded · Mar 27, 2025 · N229AZ · Boeing 767323 · Fuselage Miscellaneous Structure > FORWARD CARGO FLOOR STRUCTURE INTERCOSTAL CORRODED TO EXFOLIATION @ STA 478 TO STA 500, APPROX. RBL 34 REF HAECO WO 320011 NR35320 - [SDR IXXA202504030012](https://openairdocs.org/sdr/IXXA202504030012.md): Fan Cowl · gouged · Mar 26, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Main Frame > #2 ENG FAN COWL DOOR I/B INSIDE SURFACE AFT REPAIR PLATES HAS A GOUGE AND WEAR - [SDR IXXA20250424001](https://openairdocs.org/sdr/IXXA20250424001.md): Rib · gouged · Mar 20, 2025 · N229AZ · Boeing 767323 · Wing, Rib/Bulkhead > FABRICATE RIGHT WING LEADING EDGE RIB USING ALTERNATE FINISH. HAECO W.O. 320011 AND NR 35297 - [SDR IXXA20250329001](https://openairdocs.org/sdr/IXXA20250329001.md): Bracket · cracked · Mar 20, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > #1 PYLON UNDER DOOR #437BL HYDRAULIC VENT LINE SUPPORT BRACKET IS CRACK. - [SDR IXXA20250424005](https://openairdocs.org/sdr/IXXA20250424005.md): Beam · cracked · Mar 19, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > RIGHT WING LEADING EDGE BULL NOSE BEAM IS CRACKED AT OSS 664.58. REF HAECO WO 320011 NR 35285 - [SDR IXXA20250425002](https://openairdocs.org/sdr/IXXA20250425002.md): Door Frame · gouged · Mar 17, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Structure > MAIN CARGO DOOR CUTOUT AFT FRAME HAS 1EA HOLE WITH EVIDENCE OF CORROSION BETWEEN STR 20L AND 21L - [SDR IXXA202504210001](https://openairdocs.org/sdr/IXXA202504210001.md): Floorboard · delaminated · Mar 14, 2025 · N229AZ · Boeing 767323 · Fuselage Floor Panel > FLOORBOARD RBL 73 TO RBL 88 FROM STA 388 TO 522 HAS LARGE DENT. REF WO HAECO 320011 NR 35259 - [SDR IXXA20250425001](https://openairdocs.org/sdr/IXXA20250425001.md): Frame · gouged · Mar 10, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Frame > MAIN CARGO DOOR CUTOUT AFT FRAME IS GOUGED BETWEEN STR 20L AND 21L. HAECO W.O. 320011 AND NR 35218 - [SDR IXXA20250425005](https://openairdocs.org/sdr/IXXA20250425005.md): Stringer · gouged · Mar 5, 2025 · N229AZ · Boeing 767323 · Wing, Longeron/Stringer > RH WING INTERNAL LOWER STRINGER L-10 FWD SKIN ATTACH FLANGE HAS MILTIPLE GOUGES AT THE ATTACH FASTENERS BETWEEN RIB 30 AND RIB 31 SPORADICALLY THROUGHOUT. REF HAECO WO 320011 NR 35010 - [SDR IXXA20250423002](https://openairdocs.org/sdr/IXXA20250423002.md): Retainer · gouged · Mar 5, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Structure > FLIGHT DECK L2 SLIDING WINDOW CUTOUT FWD LOWER SEAL RETAINER DAMAGE - [SDR IXXA20250422006](https://openairdocs.org/sdr/IXXA20250422006.md): Rib · gouged · Mar 5, 2025 · N229AZ · Boeing 767323 · Wing, Rib/Bulkhead > RH WING INTERNAL RIB 23 WEB IS DENTED AND GOUGED AT THE SAME LOCATION ON THE INBD SIDE BETWEEN STRINGERS L-5 AND L-6. REF HAECO WO 320011 NR 34976 - [SDR IXXA20250422005](https://openairdocs.org/sdr/IXXA20250422005.md): Landing · corroded · Mar 4, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon, Plate/Skin > #2 PYLON OTBD STRUT ATTACH ACCESS PANEL LANDING (A/C SIDE) HAS PITTING. REF HAECO WO 320011 NR 34926 - [SDR IXXA20250426002](https://openairdocs.org/sdr/IXXA20250426002.md): Rib · gouged · Mar 3, 2025 · N229AZ · Boeing 767323 · Engine Thrust Reverser > #2 ENGINE OUTBOARD THRUST REVERSER INNER FRAME HAS A GOUGE. HAECO W.O. 320011 AND NR 34816 - [SDR IXXA20250422007](https://openairdocs.org/sdr/IXXA20250422007.md): Floorbeam · corroded · Mar 3, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Floor Beam > FWD CARGO COMPARTMENT STA 520 ATTACH ANGLE BELOW R/H PDU CORRODED O/B NUTPLATE. REF HAECO WO 320011 NR 34726 - [SDR IXXA2020422002](https://openairdocs.org/sdr/IXXA2020422002.md): Attach Angle · corroded · Mar 3, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Attach Fittings > FWD CARGO COMPARTMENT STA 514 ATTACH ANGLE BELOW RH PDU CORRODED AROUND NUT PLATES. REF HAECO WO 320011 NR 34725 - [SDR IXXA20250421006](https://openairdocs.org/sdr/IXXA20250421006.md): Floorbeam · corroded · Mar 3, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Floor Beam > FWD CARGO COMPARTMENT STA 500 TOP OF FLOOR BEAM CORRODED AND SPLITTING BELOW LOWER SILL OF CARGO DOOR. REF HAECO WO 320011 NON ROUTINE 34724 - [SDR IXXA20250418002](https://openairdocs.org/sdr/IXXA20250418002.md): Angle · cracked · Mar 3, 2025 · N229AZ · Boeing 767323 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT LEFT SIDEWALL SUPPORT CRACKED AT STA 654+33, WL 158. REF HAECO WO 320011 AND NR 34720 - [SDR IXXA20250411001](https://openairdocs.org/sdr/IXXA20250411001.md): Angle · cracked · Mar 3, 2025 · N229AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > #2 PYLON INBD ACCESS HYDRAULIC BAY AFT OTBD STRUCTURE CLIP CRACKED. REF HAECO WO 320011 NON ROUTINE 34843 - [SDR IXXA20250422003](https://openairdocs.org/sdr/IXXA20250422003.md): Fitting · corroded · Mar 1, 2025 · N229AZ · Boeing 767323 · Fuselage Main, Keel > AFT KEEL BEAM FITTING FWD OF 149BL ACCESS HAS CORROSION. REF HAECO WO 320011 NR 34676 - [SDR IXXA20250426001](https://openairdocs.org/sdr/IXXA20250426001.md): Fuel Panel · corroded · Feb 28, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > RIGHT WING LOWER PANEL 631AB IS WORN AND CORRODED. HAECO W.O. 320011 AND NR 34518 - [SDR IXXA20250425003](https://openairdocs.org/sdr/IXXA20250425003.md): Access Panel · corroded · Feb 28, 2025 · N229AZ · Boeing 767323 · Wing, Plate/Skin > LEFT WING LOWER ACCESS PANEL 532AB IS WORN AND CORRODED - [SDR IXXA202504211005](https://openairdocs.org/sdr/IXXA202504211005.md): Access Panel · corroded · Feb 28, 2025 · N229AZ · Boeing 767323 · Wing, Plate/Skin > LEFT WING LOWER ACCESS PANEL 531AB IS WORN AND CORRODED, HAECO WO 320011 AND NR 34514 - [SDR IXXA20250421005](https://openairdocs.org/sdr/IXXA20250421005.md): Skin · corroded · Feb 28, 2025 · N229AZ · Boeing 767323 · Leading Edge Devices > R/H WING #12 L/E SLAT T/E WEDGE LOWER SURFACE IS CORRODED APPROX 11" INBOARD OF THE OUTBOARD END OF THE SLAT - [SDR IXXA20250428003](https://openairdocs.org/sdr/IXXA20250428003.md): Former · cracked · Feb 27, 2025 · N229AZ · Boeing 767323 · Wing Main, Frame Structure > RIGHT WING LEADING EDGE FORMER IS CRACKED AT APPROX OSS 560 - [SDR IXXA20250424006](https://openairdocs.org/sdr/IXXA20250424006.md): Web · gouged · Feb 27, 2025 · N229AZ · Boeing 767323 · Wing Miscellaneous Structure > RH WING OTBD LE AREA BULL NOSE WEB EXISTING REPAIR IS GOUGED IN THE RADIUS AT APPROX LES 690. REF HAECO WO 320011 NR 34437 Next page: https://openairdocs.org/aircraft/N229AZ/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 = 'N229AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N229AZ/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.