# Service difficulty reports: N1229A A list on [N1229A](https://openairdocs.org/aircraft/N1229A.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 8 · 362 reports - [SDR ABXA20261020476](https://openairdocs.org/sdr/ABXA20261020476.md): Lamp · inoperative · Oct 20, 2026 · N1229A · Boeing 767306 · Fire Detection > DURING FIRE TEST, R ENG OVHT DID NOT ILLUMINATE DURING TEST. MTC REPLACED THE LAMP FOR KORRY SWITCH IAW AMM 33-13-00. OPS CHKD GOOD. ACFT RETURNED TO SERVICE. - [SDR ABXA20260909399](https://openairdocs.org/sdr/ABXA20260909399.md): Spring · missing · Sep 9, 2026 · N1229A · Boeing 767306 · Main Landing Gear Attach Section > DURING WALK AROUND FOUND LEFT MLG FORWARD DOWN LOCK WITH ONE SPRING MISSING. MTC REMOVED AND REPLACED LEFT MLG DOWN LOCK SPRING (BOTH) IAW AMM 32-32-05. A/C RETURNED TO SERVICE. - [SDR ABXA20260908398](https://openairdocs.org/sdr/ABXA20260908398.md): Pitot System · malfunctioned · Sep 8, 2026 · N1229A · Boeing 767306 · Pitot/Static Anti-Ice System > DURING TAXI OUT CAPT PITOT HEAT ON EICAS, A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX REMOVED AMD REPLACED CAPT SIDE UPPER PITOT PROBE IAW AMM 34-11-01. EXECUTED PITOT, LOW RANGE, AND HIGH RANGE LEAK CHECK IAW B767 AMM 34-11-00. LEAK CHECK PASS. - [SDR ABXA20260821371](https://openairdocs.org/sdr/ABXA20260821371.md): Skin · cracked · Aug 21, 2026 · N1229A · Boeing 767306 · Fuselage Main, Plate/Skin > DURING MAINT, PRE FLIGHT MAINT FOUND A SUSPECTED 4" CRACK AT FUSELAGE SECTION 48 AT STA 1660 BETWEEN STRINGER 13R AND 14R ON RIGHT SIDE ABOVE STAB CENTER LINE. MAINT GROUNDED A/C. REMOVED DAMAGED, REPAIRED IAW B767-300 SRM 53-80-010 REPAIR 7 DETAIL. AND RET - [SDR ABXA20260722332](https://openairdocs.org/sdr/ABXA20260722332.md): Elt · defective · Jul 22, 2026 · N1229A · Boeing 767306 · Emergency Locator Beacon > LEFT PORTABLE ELT LANYARD BROKEN & TANGLED. REMOVED AND REPLACED LEFT PORTABLE ELT ASSY IAW B767 AMM 25-60-03. A/C RETURNED TO SERVICE. - [SDR ABXA20260712320](https://openairdocs.org/sdr/ABXA20260712320.md): Lamp · inoperative · Jul 12, 2026 · N1229A · Boeing 767306 · Emergency Lighting > DURING PREFLIGHT, ONE OF THE ENTRY DOOR'S OVERHEAD LIGHT BULBS ARE BURNED OUT. DEFERRED FOR DEPARTURE, THEN NEXT LEG RELAMPED ENTRY DOOR EMERGENCY LIGHT IAW B767 AMM 33-51-03. OPS CHECK GOOD. PLACARDS REMOVED. NO REACTIVATION PROCEDURES APPLIED. LP 39515-61/3 - [SDR ABXA20260528230](https://openairdocs.org/sdr/ABXA20260528230.md): Warning Message · false activation · May 28, 2026 · N1229A · Boeing 767306 · Landing Gear Position and Warning > CREW GOT AIR/GND DISAGREE STATUS MESSAGE IN FLIGHT. PERFORMED B767 FIM TASK 810 1803. NO FAULTS WITH PROX INDICATION FOUND AT THIS TIME. ACFT OK FOR RETURN TO SERVICE REF FIM TASK. - [SDR ABXA202604043144](https://openairdocs.org/sdr/ABXA202604043144.md): Landing Gear · unknown · Apr 3, 2026 · N1229A · Boeing 767306 · Landing Gear System > DURING PUSHBACK, TRACTOR WENT INTO PROTECTION MODE, DURING TURN ACFT WENT BTB FOR AN INSPECTION MTX GROUNDED ACFT AND INSPECTED NOSE LANDING GEAR C/W PHASE 1 INSPECTION IAW AMM 05-51-29, NO DEFECTS WERE NOTED AND RETURNED ACFT FOR SERVICE. - [SDR ABXA20260226079](https://openairdocs.org/sdr/ABXA20260226079.md): Cover · missing · Feb 26, 2026 · N1229A · Boeing 767306 · Emergency Lighting > FOUND L1 DOOR EMERGENCY LIGHT MISSING COVER REPLACED AND RELAMPED LIGHT ASSY IAW AMM 33-51-01 OPS CHECK GOOD.AC IN SERVICE. - [SDR ABXA20260208063](https://openairdocs.org/sdr/ABXA20260208063.md): Failsafe · not reported · Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, Structure > DURIING C6 CHECK, ON WO 15843154, REPAIRED RH FAILSAFE TRIM-OUT AND RE-ASSEMBLY, STA. 955 IAW ABX-EA-5350-0014-0013. (RH FAILSAFE) AND AMES DOC. 47207ORD04. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE. - [SDR ABXA20260208062](https://openairdocs.org/sdr/ABXA20260208062.md): Failsafe · not reported · Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, Structure > DURIING C6 CHECK, ON WO 15843154, REPAIRED THE LT FAILSAFE TRIM-OUT AND RE-ASSEMBLY, BS 955 IAW EA-5350-0013-0013. LT FAILSAFE AND AMES DOC. 47207ORD03. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE. - [SDR ABXA20260212061](https://openairdocs.org/sdr/ABXA20260212061.md): Floorbeam · not reported · Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, Floor Beam > DURING C6 CHECK, ON WO 15843154, ACCOMPLISHED ABX-REA-5300-65992-00 (MODIFY - STA 390 TO 720 MAIN DECK FLOORBEAMS AND LOWER DECK CEILING, FQIS WIRE SEPARATION PROVISION, B767). C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE. - [SDR ABXA20251213329](https://openairdocs.org/sdr/ABXA20251213329.md): Transducer · malfunctioned · Dec 13, 2025 · N1229A · Boeing 767306 · Brake Anti-Skid Section > DURING TAKEOFF ANTI SKID EICAS MSG. AT 40 KNOTS, ABORTED TAKEOFF (ATO) AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C, PERFORMED FIM 32-423 FT 803 AND FOUND MESSAGE TRANSDUCER 6, UNABLE TO ERASE. R & R ANTISKID TRANSDUCER 6 IAW AMM 32-42-06. OP TESTED GOOD. - [SDR ABXA20250819181](https://openairdocs.org/sdr/ABXA20250819181.md): Start Valve · failed · Aug 19, 2025 · N1229A · Boeing 767306 · Engine Start Valves/Controls > DURING TAXI OUT, LEFT ENGINE START VALVE FAILED TO OPEN. NO ROTATION, L ENG STARTER EICAS, VALVE LIGHT. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-80-00-2-1. AIRCRAFT RETURNED TO SERVICE. - [SDR ABXA20250127023](https://openairdocs.org/sdr/ABXA20250127023.md): Generator · malfunctioned · Jan 27, 2025 · N1229A · Boeing 767306 · AC Generator-Alternator > DURING TAXI AFTER STARTING LH ENG,GOT LEFT ENG. CONTROL AND LEFT GEN DRIVE DISSCONNECT LIGHT, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C,MTX DEFERRED LH GEN IAW MEL ABX-24-00-1-1.AND RETURNED A/C TO SERVICE. - [SDR ABXA20241207245](https://openairdocs.org/sdr/ABXA20241207245.md): Control Panel · failed · Dec 7, 2024 · N1229A · Boeing 767306 · Autopilot System > DURIING CRUISE BOTH FD BARS FAILED LATERAL GUIDANCE FD BAR APPEARED, BUT DID NOT GIVE PROPER GUIDANCE FROM MCP. AIRCRAFT DIVERTED TO SFO. MAINTENANCE GROUNDEDTHE AIRCRAFT. MAINTENANCE RPLEACED MODE CONTROL PANEL PER 767 AMM 22-11-02,, MCDP TEST 04 PASSED, AIRC - [SDR ABXA20241011186](https://openairdocs.org/sdr/ABXA20241011186.md): Tat Probe · failed · Oct 11, 2024 · N1229A · Boeing 767306 · Outside Air Temperature Indicator/Sensor > CREW REPORTED EICAS MSG "TAT PROBE" INFO: NO A/T, NO L NAV, NO V NAV DURING CLIMB STAGE AND PERFORMED AN AIR TURNBACK. MTC GROUNDED THE AIRCRAFT, REMOVED AND REPLACED TAT PROBE IAW B767 AMM 34-12-02 OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. - [SDR ABXA20240917176](https://openairdocs.org/sdr/ABXA20240917176.md): Hydraulic Line · leaking · Sep 17, 2024 · N1229A · Boeing 767306 · Hydraulic System, Main > DURING CRUISE, STARTED TO LOOSE CENTER HYD QTY, PILOT DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT( KMSY) AND LANDED SAFELY. AC WAS.MTX GROUNDED AC AND BEGAN LOOKING FOR HYD LEAK PERFOMED TAIL SKID SYSTEM TEST PER AMM 32-71-00, DURING TEST AND GEAR H - [SDR UIEA2024061800527](https://openairdocs.org/sdr/UIEA2024061800527.md): Lens · broken · Jun 20, 2024 · N1229A · Boeing 767306 · Emergency Lighting > CABIN CREW ENTRY, LOWER PANEL LEFT SIDE, EMERGENCY SIGN LENS, BROKEN(

EMERGENCY SIGN LENS FROM CABIN CREW ENTRY WAS REPLACED IAW AMM 33-51-02-412-003 REV 142 DATE 22 APR 2024

) - [SDR UIEA2024061800528](https://openairdocs.org/sdr/UIEA2024061800528.md): Fuel Cell · leaking · Jun 20, 2024 · N1229A · Boeing 767306 · Fuel Storage > RH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4(

RH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4. FUEL LEAK WAS REPAIRED, IAW AMM 28-11-00-308-013 REV 142 22APR24. THE FUEL LEAK TEST SATISFACTORY.

) - [SDR UIEA2024061800529](https://openairdocs.org/sdr/UIEA2024061800529.md): Stiffener · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Miscellaneous Structure > SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36.(

SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36 WAS FABRICATED IAW DRAWING 141T5170 AND ORDER M6753450 ISSUED - [SDR UIEA2024061800530](https://openairdocs.org/sdr/UIEA2024061800530.md): Stiffener · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Miscellaneous Structure > SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 REAR FACE OF WEB WITH CRACK ON STIFFENER LBL26.(

SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 REAR FACE OF WEB WITH CRACK ON STIFFENER LBL26. STIFFENER WAS RE - [SDR UIEA2024061800531](https://openairdocs.org/sdr/UIEA2024061800531.md): Skin · corroded · Jun 20, 2024 · N1229A · Boeing 767306 · Wing, Plate/Skin > LH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 SAFETY LINE ATTCH POINT WITH POINTS OF CORROSION.(

LH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 WAS REPAIRED IAW SRM 57-20-01-2R-7 FIG 201 SHEET 1 PAG 1-2 AND SRM 51-70-17-2R-4 REPAIR - [SDR UIEA2024061800532](https://openairdocs.org/sdr/UIEA2024061800532.md): Hinge · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage, Door Hinge > EXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL(

EXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL. BROKEN HINGE IS REMOVED AND THE HINGE IS REPLACED WITH A NEW ONE IAW SRM 51-40-02-0G-0 REV 125 15APR24, SRM 51-10-02-0G- - [SDR UIEA2024061800533](https://openairdocs.org/sdr/UIEA2024061800533.md): Lanyard · missing · Jun 20, 2024 · N1229A · Boeing 767306 · Fuel Storage > LH WING, FIXED LEADING EDGE STRUCTURE AREA FUELING STATION (PANEL 521 QB) LANYARD OF CAP (COLOR RED) MISSING.(

THE LANYARD OF FUEL CAP ADAPTER WAS REPLACED IAW AMM 28-11-04-404-019 REV: 142 DATE: 22-APR-24

) - [SDR UIEA2024061800534](https://openairdocs.org/sdr/UIEA2024061800534.md): Door · punctured · Jun 20, 2024 · N1229A · Boeing 767306 · Fluid Service Doors > LH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WITH ONE PUNCTURED.(

LH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WAS REPAIRED IAW SRM 57-41-01-2R-1 FIG 201 SHEET 3 PAG 2-4 & SRM 51-70-17-0G-0 PAR 4B F - [SDR UIEA2024061800537](https://openairdocs.org/sdr/UIEA2024061800537.md): Floor Panel · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Floor Panel > ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.(

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.WAS PERFORMED REPAIRED IAW SRM 53-00-53- - [SDR UIEA2024061800539](https://openairdocs.org/sdr/UIEA2024061800539.md): Access Panel · damaged · Jun 20, 2024 · N1229A · Boeing 767306 · Wing, Plate/Skin > LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, CLAMP OVER HYDRAULIC LINE DAMAGED(

LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, OVER HYDRAULIC LINE CLAMP WAS REPLACED IAW AMM 20-10-11 - [SDR UIEA2024061800540](https://openairdocs.org/sdr/UIEA2024061800540.md): Panel · unknown · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Miscellaneous Structure > UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKE DETECTION SYSTEM, CEILING PANELS, OBSTRUCTED SEVERAL INTAKE ORIFICES, EVALUATION(

UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOK - [SDR UIEA2024061800541](https://openairdocs.org/sdr/UIEA2024061800541.md): Skin · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Leading Edge Devices > RH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94(

RH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94. THE TEAR ON THE SKIN OF THE SLAT #10 WAS REPAIRED IAW 53-43-01-2R-2 REV 125 15APR24, AMM 30-11-06-404-009 REV 142 22APE24, AMM 27-81-02-42 - [SDR UIEA2024061800542](https://openairdocs.org/sdr/UIEA2024061800542.md): Floor Panel · damaged · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Floor Panel > ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE.(

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE WAS REPAIRED IAW SRM 53-00 - [SDR UIEA2024061800543](https://openairdocs.org/sdr/UIEA2024061800543.md): Floor Panel · damaged · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Floor Panel > ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124AXF, MISSING MATERIAL AFT RIGHT CORNER, CRACK ON RIGHT LATERAL EDGE (NEAR LOCK) AND MISSING MATERIAL FWD RIGHT CORNER(

ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COM - [SDR UIEA2024061800544](https://openairdocs.org/sdr/UIEA2024061800544.md): Door · leaking · Jun 20, 2024 · N1229A · Boeing 767306 · Emergency Exits > EXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(

SEAL OF EXTERNAL FUSELAGE, LH EMERGENCY EXIT DOOR WAS REPLACED IAW AMM 52-09-06-404-003 REV 142, APR 22, 2024. CHECK FOR LEAKS WAS PERFORMED, NO FOUND EXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(

SEAL OF EXTERNAL FUSELAGE, LH EMERGENCY EXIT DOOR WAS REPLACED IAW AMM 52-09-06-404-003 REV 142, APR 22, 2024. CHECK FOR LEAKS WAS PERFORMED, NO FOUND EXTERNAL FUSELAGE, LEAK ON RH EMERGENCY EXIT DOOR.(

SEAL OF RH EMERGENCY EXIT DOOR WAS REPLACED IAW AMM 52-09-06-404--003 REV 142, APR 22, 2024; CHECK FOR LEAKS WAS PERFORMED, NO LEAKS FOUND

) - [SDR UIEA2024061800546](https://openairdocs.org/sdr/UIEA2024061800546.md): Frame · cracked · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Main, Frame > CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE.(

CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE. WAS REPAIRED IAW TRE6753695 ISSUED DATE JUN 08/2024, FVCI CONTROL# 24088- - [SDR UIEA2024061900551](https://openairdocs.org/sdr/UIEA2024061900551.md): Support Angle · corroded · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Miscellaneous Structure > AFT FUSELAGE SECTION 48, CORROSION ON INTERNAL SKIN, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR(

AFT FUSELAGE SECTION 48, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02 - [SDR UIEA2024061900554](https://openairdocs.org/sdr/UIEA2024061900554.md): Stringer · damaged · Jun 20, 2024 · N1229A · Boeing 767306 · Fuselage Main, Longeron/Stringer > SECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456(

SECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456. THE STRINGER SEGMEMT WAS REPLACED PER SRM 51-10-02-0G-0 PAR 9 REV 125 15APR24 AND SRM 51-40-02-0G-0 REV 125 15APR24.

) - [SDR UIEA2024031400146](https://openairdocs.org/sdr/UIEA2024031400146.md): Oxygen Mask · inoperative · Mar 13, 2024 · N1229A · Boeing 767306 · Passenger Oxygen System > O2 MASK INOP SUPERNUMERARY, TRANSFERRED TO MDDR 204626 PER MEL 35-11-03-02A. O2 MASK FAILED TO TEST. FOUND STOWED INCORRECTLY. RESTOWED O2 MASK AT SUPERNUMARY SEAT CLOSEST TO LAV IAW AMM 35-11-51. OPS TEST GOOD IAW AMM 35-11-00. THIS CLEARS MDDR 204626, PLACA - [SDR UIEA2024030600143](https://openairdocs.org/sdr/UIEA2024030600143.md): Button · stuck · Mar 6, 2024 · N1229A · Boeing 767306 · Crew Oxygen System > OBSERVER INTERCOM WILL NOT TRANSMIT USING HEADSET MIC.(

FOUND RESET TEST BUTTON STUCK ON OXYGEN MASK BOX. REMOVED AND REPLACED OBSERVER OXYGEN MASK BOX IAW AMM 35-11-51. PERFORMED HEADSET MIC OPS CHECK IAW AMM 23-51-00, OPS CHECK GOOD. NO DEFECTS NOTED AT TH - [SDR UIEA2024022600129](https://openairdocs.org/sdr/UIEA2024022600129.md): Elt · damaged · Feb 22, 2024 · N1229A · Boeing 767306 · Emergency Locator Beacon > PORTABLE ELT BY L1 DOOR CORD RIPPED..(

REMOVED AND REPLACED L1 DOOR PORTABLE ELT IAW AMM 25-63-03. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024022200112](https://openairdocs.org/sdr/UIEA2024022200112.md): Elt · damaged · Feb 22, 2024 · N1229A · Boeing 767306 · Emergency Locator Beacon > PORTABLE ELT BY L1 DOOR CORD IS RIPPED(

REMOVED AND REPLACED L1 DOOR POTABLE ELT IAW AMM 25-63-03. OPS CHK GOOD.

) - [SDR UIEA2024020500070](https://openairdocs.org/sdr/UIEA2024020500070.md): Altimeter · malfunctioned · Feb 5, 2024 · N1229A · Boeing 767306 · Altimeter, Barometric/Encoder > CAPT ALTIMETER MOMENTARILY WENT A FEW THOUSAND FEET LOW THEN RAPIDLY RECOVERED PASSING FL 340 IN CLIMB AND DESCENT. VSI ANOMALY NOTED AS WELL(

PERFORMED OPS TEST OF AIR DATA COMPUTING SYS, OPS TEST GOOD IAW AMM 34-12-00, NO DEFECTS NOTED.

) - [SDR UIEA2024011500015](https://openairdocs.org/sdr/UIEA2024011500015.md): Unknown · unknown · Jan 14, 2024 · N1229A · Boeing 767306 · Emergency Equipment > DEMO ESCAPE HARNESS ASSY BAG OPEN AND FOUND UNSERVICEABLE(

TRANSFER TO MDDR 200998 PER DDG 25-20-01 CAT E 120 DAYS DUE 13MAY2024. LP 1716038 M4: REMOVED AND REPLACED ESCAPE HARNESS DEMO BAG IAW AMM 25-60-00. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 200998. - [SDR UIEA2023011930039](https://openairdocs.org/sdr/UIEA2023011930039.md): Seal · leaking · Jan 16, 2023 · N1229A · Boeing 767306 · Fuselage Main, Bulkhead > SECTION48, PRESSURE DOME, CONTROL CABLES E1B AND E1A, AIR PRESSURE SEALS WITH EVIDENCE OF AIR LEAK(

SECTION48, PRESSURE DOME, CO-NTROL CABLES E1B AND E1A, AIR PRESSURE BULGE ON LH FUSELAGE SKIN AT STA 654+57.5 AND 3" ABOVE STGR 30 LH.(

DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-6 GUIDELINES

) - [SDR UIEA2023011930035](https://openairdocs.org/sdr/UIEA2023011930035.md): Skin · damaged · Jan 16, 2023 · N1229A · Boeing 767306 · Fuselage Main, Plate/Skin > LIGHTNING STRIKE ON LH FUSELAGE SKIN AT STA 1647.5 AND 3.5" BELOW STGR 34 LH.(

LIGHTNING STRIKE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8

) - [SDR UIEA2023011930034](https://openairdocs.org/sdr/UIEA2023011930034.md): Skin · damaged · Jan 16, 2023 · N1229A · Boeing 767306 · Fuselage Main, Plate/Skin > LH FUSELAGE SKIN AT STA 232.5 AND 4" BELOW STGR 30 LH DAMAGED. REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8

) - [SDR UIEA2023011200033](https://openairdocs.org/sdr/UIEA2023011200033.md): Fuel Tank · leaking · Jan 16, 2023 · N1229A · Boeing 767306 · Fuel Storage > LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14(

LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14 WAS REPAIRED PER AMM 28-11-00-308-057 REQUIREMENTS

) - [SDR UIEA2023011200032](https://openairdocs.org/sdr/UIEA2023011200032.md): Relief Valve · out of limits · Jan 16, 2023 · N1229A · Boeing 767306 · Fuel Storage > SURGE TANK PRESSURE RELIEF VALVE R, OUT OF LIMITS IAW TASK A-28-004-00-02(

SURGE TANK PRESSURE RELIEF VALVE R, WAS REPLACED PER AMM 28-13-04-002-002 REQUIREMENTS

) Next page: https://openairdocs.org/aircraft/N1229A/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 = 'N1229A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1229A/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.