N1181A
Service difficulty reports · 435
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 = 'N1181A' 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 = 'N1181A' 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 21GA0260904001None · pilot errorDURING CRUISE, THE FLIGHT CREW EXPERIENCED A SHUTDOWN OF THE LEFT ENGINE AND SUBSEQUENTLY DIVERTED THE AIRCRAFT TO PUNTA CANA (PUJ). THE AIRCRAFT LANDED SAFELY IN PUJ AT APPROXIMATELY 1256Z. PRELIMINARY INFORMATION RECEIVED FROM THE CREW INDICATES THAT THE FUSDR ABXR2026042900008Structure · crackedLEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACKSDR ABXR2026042900007Skin Panel · delaminatedLEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED.SDR ABXR2026042900006Skin · crackedFOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2SDR ABXR2026042900005Angle · crackedVERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUESDR 21GA20250906018Warning Message · false activationON APPROACH, SELECTED FLAPS TO 20. RECEIVED TE FLAP DISAGREE EICAS MESSAGE. DID GO AROUND, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURE. NO DEFECTS NOTED.SDR UIEA2024072400743Escape Reel · unwanted deploy1 EA ESCAPE INERTIAL REEL DEVICE FULL OUT(<P>TRANSFER TO DMI 213408 PER MEL 25-61-01-01 CAT C DUE DATE 4AUG2024. PN 379103D-29</P> / <P>LP 1239968 ITEM 5 / ONT / 27JUL24: INSTALLED 1 EA INERTIA REEL IAW B767 AMM 25-61-01. NO FUTHER DEFECTS NOTED. THIS CLEARS MSDR UIEA2024033000230Escape Reel · unwanted deployINERTIAL ESCAPE REEL DROPPED DURING DESCENT(<P>REVOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW AMM 25-51-05. THIS CLEARS MDDR 205698. PLACARD REMOVED.</P>)SDR UIEA2024032300207Escape Reel · unwanted deployINERTIAL REEL DEPLOYED ON TAKE-OFF ROLL(<P>R/R DEPLOYER DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024031900161Target · out of adjustNOSE AIR/GRND STATUS MESSAGE(<P>INSTALLED TARGET AND ADJUSTMENT BRACKET INSTALLED IAW BOEING AMM 32-61-03 AND OPS CHECK CARRIED OUT IAW AMM 32-61-03, OPS CHECK GOOD.</P>)SDR UIEA2024022800135Escape Reel · unknownONE ESCAPE REEL REMOVED FROM AIRPLANE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS )(<P>REMOVED AND REPLACED ESCAPE REEL IAW AMM 25-61-04. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR 203776. PLACARDS REMOVED. MCC NOSDR UIEA2024010800008Escape Reel · unknownONE INERTIA DESCENT REEL FELL OUT OF HOLDER AND UNWOUND ON CLIMBOUT(<P>REPLACED THE SECOND AFT INERTIA DESCENT REEL DEVICE IAW AMM 25-61-05. THIS CLEARS MDDR 200637. MCC NOTIFIED.</P>)SDR UIEA2023121500998Escape Reel · unknownESCAPE REELS REQUIRE INSPECT/STOWING MULTIPLE UNLOCKED DURING TAKEOFF(<P>R/R INERTIAL ESCAPE REEL IAW AMM 25-61-05. OPS CHECK GOOD. DMI 199173 CLOSED.</P>)SDR UIEA2023060800611Unknown · unknownFWD CARGO COMPARTMENT, FLOOR LEVEL, CORROSION ON FRAME WEB UPPER CHORD AT STA 654+44 LBL20(<P>AFFECTED ITEM WAS REPAIRED IAW B767 SRM 53-00-07-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060700607Unknown · unknownLH INBD FLAP, SUPPORT RIB AT IFS 129 APPROX INNER SKIN WITH DENT(<P>AFFECTED AREA WAS REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060700606Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 632 AND STRINGER S-25LH(<P>AFFECTED AREA WAS REPAIRED PER TRE6753601 (IAI CUSTOMER SERVICE #CS-26206-003). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700605Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700604Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060700603Linkage · unknownVERTICAL STABILIZER REAR SPAR, UPPER PCA LINKAGE, RH HINGE WITH FREE PLAY(<P>UPPER PCA LINKAGE WAS REPLACED PER AMM 27-21-02-022-035 / -038. OPS CHECK GOOD</P>)SDR UIEA2023060700602Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-6 AND RBL 97.42, WING CENTER SECTION(<P> </P> / <P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-6 AND RBL 97.42 WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P>)SDR UIEA2023060700601Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-10 AND LBL 97.42, WING CENTER SECTION(<P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-10 AND LBL 97.42, WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P> / <P> </P>)SDR UIEA2023060700600Unknown · unknownFUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION(<P>FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION WAS REPAIRED AND TEST WAS SATISFACTORY.</P>)SDR UIEA2023060700599Pca · unknownRUDDER UPPER PCA WITH FREE PLAY OUT OF LIMITS(<P>RUDDER UPPER PCA WAS REPLACED PER AMM 27-21-02-422-038. OPS CHECK GOOD</P>)SDR UIEA2023060600595Unknown · unknownHORIZONTAL STABILIZER CENTER SECTION UPPER SKIN SURFACE WITH CORROSION DAMAGE BETWEEN RBL13.833 / RBL 32.67 AND STGR 3.(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6755054 (BOEING SR 3-5632149492). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060600594Unknown · unknownVERTICAL STABILIZER, RH SURFACE, COMPOSITE PANEL DESBONDED BETWEEN AUXILIARY SPAR TO FRONT SPAR BETWEEN FSS 220.521 / FSS 321.046(<P>REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600593Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 174.5 AND 5 INCH ABOVE OF STRINGER S-27LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023060600592Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+44 / STA 654+66 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600591Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+22 / STA 654+44 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600590Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600589Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 325 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600588Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 412 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600587Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 390 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600586Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 196.5 AND 8.5 INCH LOWER OF STRINGER S-21LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600585Hinge Fitting · unknownSTABILIZERS - HORIZONTAL STABILIZER - RH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755055 REV 1. NO FURTHER DEFECTS NSDR UIEA2023060600584Hinge · unknownSTABILIZERS - HORIZONTAL STABILIZER - LH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755056. NO FURTHER DEFECTS NOTED. SDR UIEA2023060600583Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1562 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753595 REV 1 ISSUED ON MAY 15, 2023 (FVCI PROJECT NO. 23088-6). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500580Unknown · unknownCORROSION ON INTERNAL FUSELAGE BEARSTRAP BETWEEN STA 1540 AND STRINGER S-10RH / S-11RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753594 ISSUED ON MAY 09, 2023 (FVCI PROJECT NO. 23088-5). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500579Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 654+110 AND STRINGER S-9RH / S-10RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753589 (FVCI PROJECT NO. 23088-7). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500578Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-14RH / S-15RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753590 ISSUED ON MAY 04, 2023 (FVCI PROJECT NO. 23088-1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500577Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-12RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753591 (FVCI PROJECT NO. 23088-2). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500576Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-8RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753592 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-3). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500575Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1480 / DSTA 876.3 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753593 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-4). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500574Panel · unknownCORROSION ON PANEL UNDER ROLLER TRAYS BETWEENÂ STA 564+66 AND STA 564+88 FROMÂ FWD CARGO COMPARTMENT, FLOOR LEVEL.(<P>PANEL WAS REPLACED PER SRM 51-10-02-0G PAR.9. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500573Unknown · unknownLIGHTNING STRIKE DAMAGE ON FASTENER OF FUSELAGE EXTERNAL SKIN BETWEEN STA 566 AND STRINGERS S-27LH AND S-28LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500572Bushing · unknownCORROSION ON BUSHINGS FROM RH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757194 (CMM 57-54-13 REPAIR 2-1)</P> / <P>MAJOR REPAIR PN: 113T1108-17 AND 113T1108-23</P>)SDR UIEA2023060500571Bushing · unknownCORROSION ON BUSHINGS FROM LH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757193 (CMM 57-54-13 REPAIR 2-1) MAJOR REPAIR. PN: 113T1108-17 AND 113T1108-23</P>)SDR UIEA2023032400282Hpc · unknownON TAXI OUT R ENG BLEED LIGHT AND EICAS MESSAGE ON FOLLOWED STEP 3 OF APPLICABLE DDG 36-11-02 LIGHT AND DID NOT CLEAR PER MCC GUIDANCE RH ENGINE TO 70 PERCENT AND MESSAGE DID NOT CLEAR(<P>REMOVED AND REPLACED THE RH ENGINE HIGH PRESSURE CONTROLLER IAW B767 AMMSDR UIEA2023030300201None · noneESCAPE REEL HANDLE FELL OUT AFTER LANDING(<P>R/R DESCENT DEVICE "B" IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023011100014None · noneDURING DEPARTURE IN CLIMB OUT, ACFT ENTERED AREA OF SEVERE TURBULENCE & W/S, ACFT INDICATED O/S OF 285, SPEED TAPE WITH NO ASSOCIATED OVERSPEED WARNINGS IAW 05-51-04, DATA FROM OUR ENGINEERING TEAM SHOWS AIRCRAFT DID NOT SHOW "G" LOADS OF SEVERE TURBULENCE. NOSDR UIEA2022112101199Guard · damagedEMERGENCY LIGHT GUARD INOP WITH GUARD CLOSED, EMER LIGHT REMAIN UNARMED. R/R EMERGENCY LIGHT GUARD IAW AMM 33-51-00. OPS CHECKED GOOD.
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