N1229A
Service difficulty reports · 362
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N1229A' AND registry_match = 'registration' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA20261020476Lamp · inoperativeDURING 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 ABXA20260909399Spring · missingDURING 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 ABXA20260908398Pitot System · malfunctionedDURING 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 ABXA20260821371Skin · crackedDURING 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 RETSDR ABXA20260722332Elt · defectiveLEFT PORTABLE ELT LANYARD BROKEN & TANGLED. REMOVED AND REPLACED LEFT PORTABLE ELT ASSY IAW B767 AMM 25-60-03. A/C RETURNED TO SERVICE.SDR ABXA20260712320Lamp · inoperativeDURING 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 39515-61/3SDR ABXA20260528230Warning Message · false activationCREW 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 ABXA202604043144Landing Gear · unknownDURING 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 ABXA20260226079Cover · missingFOUND L1 DOOR EMERGENCY LIGHT MISSING COVER REPLACED AND RELAMPED LIGHT ASSY IAW AMM 33-51-01 OPS CHECK GOOD.AC IN SERVICE.SDR ABXA20260208063Failsafe · not reportedDURIING 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 ABXA20260208062Failsafe · not reportedDURIING 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 ABXA20260212061Floorbeam · not reportedDURING 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 ABXA20251213329Transducer · malfunctionedDURING 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 ABXA20250819181Start Valve · failedDURING 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 ABXA20250127023Generator · malfunctionedDURING 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 ABXA20241207245Control Panel · failedDURIING 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, AIRCSDR ABXA20241011186Tat Probe · failedCREW 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 ABXA20240917176Hydraulic Line · leakingDURING 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 HSDR UIEA2024061800527Lens · brokenCABIN CREW ENTRY, LOWER PANEL LEFT SIDE, EMERGENCY SIGN LENS, BROKEN(<P>EMERGENCY SIGN LENS FROM CABIN CREW ENTRY WAS REPLACED IAW AMM 33-51-02-412-003 REV 142 DATE 22 APR 2024</P>)SDR UIEA2024061800528Fuel Cell · leakingRH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4(<P>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.</P>)SDR UIEA2024061800529Stiffener · crackedSECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36.(<P>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 UIEA2024061800530Stiffener · crackedSECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 REAR FACE OF WEB WITH CRACK ON STIFFENER LBL26.(<P><SPAN>SECTION 41 FLOOR STRUCTURE, </SPAN><SPAN>FLOOR BEAM B. STA 246 REAR FACE OF WEB </SPAN><SPAN>WITH CRACK ON STIFFENER LBL26. STIFFENER </SPAN><SPAN>WAS RESDR UIEA2024061800531Skin · corrodedLH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 SAFETY LINE ATTCH POINT WITH POINTS OF CORROSION.(<P>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 REPAIRSDR UIEA2024061800532Hinge · crackedEXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL(<P>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 UIEA2024061800533Lanyard · missingLH WING, FIXED LEADING EDGE STRUCTURE AREA FUELING STATION (PANEL 521 QB) LANYARD OF CAP (COLOR RED) MISSING.(<P>THE LANYARD OF FUEL CAP ADAPTER WAS REPLACED IAW AMM 28-11-04-404-019 REV: 142 DATE: 22-APR-24</P>)SDR UIEA2024061800534Door · puncturedLH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WITH ONE PUNCTURED.(<P>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 FSDR UIEA2024061800537Floor Panel · crackedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.(<P>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 UIEA2024061800539Access Panel · damagedLEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, CLAMP OVER HYDRAULIC LINE DAMAGED(<P>LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, OVER HYDRAULIC LINE CLAMP WAS REPLACED IAW AMM 20-10-11SDR UIEA2024061800540Panel · unknownUPPER 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(<P>UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKSDR UIEA2024061800541Skin · crackedRH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94(<P>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 27-81-02-42SDR UIEA2024061800542Floor Panel · damagedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE WAS REPAIRED IAW SRM 53-00SDR UIEA2024061800543Floor Panel · damagedZONE 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(<P><SPAN>ZONE 100, LOWER HALF FUSELAGE, </SPAN><SPAN>FORWARD CARGO COMSDR UIEA2024061800544Door · leakingEXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPSDR UIEA2024061900553Door · leakingEXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPSDR UIEA2024061800545Seal · leakingEXTERNAL FUSELAGE, LEAK ON RH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF RH EMERGENCY EXIT DOOR </SPAN><SPAN>WAS REPLACED IAW AMM 52-09-06-404--</SPAN><SPAN>003 REV 142, APR 22, 2024; CHECK FOR LEAKS </SPAN><SPAN>WAS PERFORMED, NO LEAKS FOUND</SPAN></P>)SDR UIEA2024061800546Frame · crackedCRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE.(<P>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 UIEA2024061900551Support Angle · corrodedAFT FUSELAGE SECTION 48, CORROSION ON INTERNAL SKIN, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR(<P>AFT FUSELAGE SECTION 48, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02SDR UIEA2024061900554Stringer · damagedSECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456(<P>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.</P>)SDR UIEA2024031400146Oxygen Mask · inoperativeO2 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, PLACASDR UIEA2024030600143Button · stuckOBSERVER INTERCOM WILL NOT TRANSMIT USING HEADSET MIC.(<P>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 THSDR UIEA2024022600129Elt · damagedPORTABLE ELT BY L1 DOOR CORD RIPPED..(<P>REMOVED AND REPLACED L1 DOOR PORTABLE ELT IAW AMM 25-63-03. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022200112Elt · damagedPORTABLE ELT BY L1 DOOR CORD IS RIPPED(<P>REMOVED AND REPLACED L1 DOOR POTABLE ELT IAW AMM 25-63-03. OPS CHK GOOD.</P>)SDR UIEA2024020500070Altimeter · malfunctionedCAPT ALTIMETER MOMENTARILY WENT A FEW THOUSAND FEET LOW THEN RAPIDLY RECOVERED PASSING FL 340 IN CLIMB AND DESCENT. VSI ANOMALY NOTED AS WELL(<P>PERFORMED OPS TEST OF AIR DATA COMPUTING SYS, OPS TEST GOOD IAW AMM 34-12-00, NO DEFECTS NOTED.</P>)SDR UIEA2024011500015Unknown · unknownDEMO ESCAPE HARNESS ASSY BAG OPEN AND FOUND UNSERVICEABLE(<P>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 UIEA2023011930039Seal · leakingSECTION48, PRESSURE DOME, CONTROL CABLES E1B AND E1A, AIR PRESSURE SEALS WITH EVIDENCE OF AIR LEAK(<P><SPAN DIR="LTR" ROLE="PRESENTATION">SECTION48, PRESSURE DOME, CO-</SPAN><SPAN DIR="LTR" ROLE="PRESENTATION">NTROL CABLES E1B AND E1A, AIR PRESSURE </SPAN><SPASDR UIEA2023011300036Skin · corrodedBULGE ON LH FUSELAGE SKIN AT STA 654+57.5 AND 3" ABOVE STGR 30 LH.(<P>DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-6 GUIDELINES</P>)SDR UIEA2023011930035Skin · damagedLIGHTNING STRIKE ON LH FUSELAGE SKIN AT STA 1647.5 AND 3.5" BELOW STGR 34 LH.(<P>LIGHTNING STRIKE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8</P>)SDR UIEA2023011930034Skin · damagedLH FUSELAGE SKIN AT STA 232.5 AND 4" BELOW STGR 30 LH DAMAGED. REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-8</P>)SDR UIEA2023011200033Fuel Tank · leakingLH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14(<P>LH FUEL LEAK AT CENTER TANK BETWEEN STGR L-10 AND LBL 14 WAS REPAIRED PER AMM 28-11-00-308-057 REQUIREMENTS</P>)SDR UIEA2023011200032Relief Valve · out of limitsSURGE TANK PRESSURE RELIEF VALVE R, OUT OF LIMITS IAW TASK A-28-004-00-02(<P>SURGE TANK PRESSURE RELIEF VALVE R, WAS REPLACED PER AMM 28-13-04-002-002 REQUIREMENTS</P>)
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