Boeing 767-281
Service difficulty reports · 1,831
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767281' 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 aircraft_model_key = '767281' 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 ABXA20200522116Structure · corrodedFORWARD CARGO DOOR INTERIOR STRUCTURE 3RD CHORD FROM BOTTOM , BEHIND LIGHT SHROUD EXFOLIATION. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522115Structure · corrodedFORWARD CARGO DOOR INTERIOR STRUCTURE 3RD CHORD FROM BOTTOM REMOVED CORRODED MINOR CHORD AND ASSOCIATED PARTS. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522114Attach Angle · gougedNR 2 PYLON AFT FAIRING, AFT BULKHEAD, LEFT AND RIGHT ATTACH ANGLES AREGOUGED. THE AIRPLANE WAS GROUNDED.SDR ABXA2020063022113Seal · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.SDR ABXA2020063022112Structure · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522111Web · corrodedFWD CARGO DOOR INTERIOR LOWER WEB UPPER CHORD CORRODED. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522110Skin · corrodedFWD CARGO COMPARTMENT DOOR INTERIOR UPPER AFT WEB HAS LIGHT SURFACE CORROSION. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522109Skin · corrodedFWD CARGO DOOR INTERIOR LOWER FWD WEB HAS CORROSION. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522108Web · corrodedFWD CARGO DOOR INTERIOR LOWER WEB STA 560 HAS CORROSION. THE AIRPLANE WAS GROUNDED.SDR ABXA20200522107Skin · corrodedFWD CARGO DOOR INTERIOR LOWER AFT WEB HAS SURFACE CORROSION. THE AIRPLANE WAS GROUNDED.SDR ABXA202006302106Floor Support · corrodedFWD CARGO COMPARTMENT FLOORBOARD ATTACH FITTING CORRODED. THE AIRPLANE WAS GROUNDED.SDR ABXA20200720129Warning Message · illuminatedEICAS MESSAGE FOR THE LE SLAT ASSYM DURING APPROACH WHEN FLAPS 5 SELECTED. AIRCRAFT WAS GROUNDED.SDR ABXA2020062955104Stringer · corrodedSTR 38R CORRODED JUST FWD OF STA 434 FACTORY SPLICE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020051107058Warning System · activatedHOT BATT BUS FAILED IN-FLIGHT. CREW CALLED AND ADVISED THAT THEY HAD LEFT, RIGHT, AND CENTER IRSS FAIL, FIRE DETECTION AND PROTECTION FAIL, AND ALL SPAR VALVES FAIL. AIRCRAFT WAS GROUNDED.SDR ABXA2020062955105Stringer Splice · corrodedFLC STRINGER 39R APPROX. STA.752 CORROSION ON SPLICE PLATE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062951103Shear Tie · crackedFORWARD LOWER CARGO STA 368 BETWEEN S38L-S37L SHEAR TIE CRACKED FROM RIVET HOLE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062940101Longeron Splice · corrodedLONGERON EXTENSION FITTING AT KEEL AT STA.785 S38L CORRODED. THE AIRPLANE WAS GROUNDED.SDR UIEA2020050100925Panel · bulgedLH WING UPPER T/E PANEL SURFACE BULGED BEYOND LIMITS.(<P>REPAIRED DAMAGED CHORD IAW REA 47401 REV. 3 AND B767 SRM 57-20-10.</P>)SDR UIEA2020050100926Skin · corrodedSTA 1065 LOWER INTERNAL SKI AND STRINGERS HAVE SURFACE CORROSION.(<P>REMOVED CORROSION. DID SCAN INSPECTION, FOUND SKIN TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW REA 47401 REV A.</P>)SDR UIEA2020050100927Keelbeam · corrodedKEEL PANEL CROSS MEMBER CORROSION UNDER NUT PLACES.(<P>REPLACED KEEL PANEL IAW B767 SRM 51-10-02.</P>)SDR UIEA2020050100929Skin · delaminatedRT SIDE VERTICAL STAB SKIN DELAMINATED.(<P>REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS PER 47401REA15.</P>)SDR UIEA2020050100930Stringer · corrodedH2 STAB STRINGER 11 CORRODED.(<P>REPLACED STRINGER PER 767-200 SRM 51-40-02 AND REA 47401FAB03.</P>)SDR UIEA2020050100931Stringer · corrodedH2 STAB STRINGER 8 CORRODED.(<P>REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03 AND REA 47401FAB</P>)SDR ABXR2020042400024Stringer · corrodedHORIZONTAL STAB STRINGER 11 CORRODED. REPLACE STRINGER PER B767-200 SRM 51-40-02 AND REA 47401FAB03.SDR ABXR2020042400023Stringer · corrodedHORIZONTAL STAB STRINGER 8 CORRODED. REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03SDR ABXR2020042400022Skin Panel · delaminatedRIGHT SIDE VERTICAL STAB SKIN DELAMINATED. REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS.SDR ABXR2020042300020Skin · corrodedALC STA 1065 LOWER INTERNAL SKIN AND STRINGERS BETWEEN FUSELAGE DRAINS HAVE SURFACE CORROSION. BLEND OUT REQUIRED AT CORRODED AREA, REMOVED CORRODED AREA AT LOWER FUSELAGE SKIN STA 1080 TO STA 1131, STRINGER 38L TO 38R IAW B767-200 SRM 53-60-01 ALLOWABLE DAMAGSDR ABXR2020042300000Panel · corrodedTHE LEFT WING, UPPER T/E PANEL, UPPER SURFACE IS BULGED, ON THE FWD O/B CORNER, LOCATED JUST FWD OF THE O/B AILERON'S I/B END.BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-20-10 DET V. REPAIRED DAMAGED UPPER CHORD IAW AMES REA # 47401 REA 03.SDR ABXA202004051051Escape Reel · deployedINERTIAL ESCAPE REELS DEPLOYED. AIRCRAFT GROUNDED.SDR ABXR2020042300019Attach Fitting · corrodedKEEL PANEL ATTACH CROSS MEMBER AT STA.967 CORRODED UNDER NUT PLATES ON FORWARD AND AFT SIDES.BLENDED CORROSION AT STA 967 KEEL PANEL ATTACH CROSS MEMBER IAW B767 SRM 51-10-02 MEASURED T. 0.100. REMOVED T 0.055 FOUND TO BE OUT OF LIMITS TAG 8720 INSTALLED PN 14SDR UIEA2020030900407Angle · corrodedCORROSION ON ANGLE THAT ATTACHES FRAME AT STR 997 TO KEEL WEB.(<P>BLENDED CORROSION IAW B767 SRM 53-50-12 FIG 1001 DETAIL II. FOUND TO BE OUT OF LIMITS, COMPLIED WITH ENGINEERING DOC #47396REA07.</P>)SDR UIEA2020030900409Keelbeam · corrodedLLW - CORROSION ON KEEL WEB AT STA 1002 LBL 5. (<P><SPAN>BLENDED CORROSION IAW B767 SRM 53-50-12-1A, REPAIRED IAW ENGINEERING DOCUMENT 47396REA04 DUE TO BLEND BEING OUT OF LIMITS.</SPAN><BR /></P>)SDR UIEA2020030900410Splice Plate · corrodedCORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.(<P>COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06. REMOVED AND REPLACED SLICE PLATE L/W LES 745-807 IAW REA 47396REA05 & 47396REA06. </P>)SDR UIEA2020030900411Skin · crackedUPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.(<P>REPAIRED L/H FUSELAGE SKIN AT STA 1654.5 IAW B767 SRM 53-80-01-2R-4 REPAIR 4.</P>)SDR UIEA2020030900412Spar · corrodedCORROSION AROUND RIVET ON FRONT SPAR UPPER CHORD AT LES 730.(<P>BLENDED CORROSION. 0.013" MATERIAL REMOVED. BEYOND LIMITS. REPAIRED IAW AMES DOCUMENT 47396REA01.</P>)SDR UIEA2020030900413Rib · corrodedUPPER TRAILING EDGE PANEL ATTACH CHORD AT WS 434, 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE.(<P>BLENDED CORROSION ON UPPER CHORD ON AILERON RIB AT WS 434 TO DEPTH OF .017", MAX DEPTH ALLOWED.008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMISDR UIEA2020030900414Attach Bracket · crackedATTACHED BRACKET BEHIND AFT LOWER CORNER SEAL DEPRESSOR IS CRACKED ON UPPER CARGO DOOR.(<P>REMOVED AND REPLACED CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)SDR UIEA2020030900415Structure · corrodedFLANGE UNDER PANEL 335AT HAS CORROSION ON UPPER SURFACE.(<P>REMOVED CORROSION IAW B767 SRM 55-10-09. FOUND TO BE OUT OF LIMITS OT .090" R.T .077. INSTALLED UPPER CHORD IAW B767 SRM 51-40-02.</P>)SDR UIEA2020030900416Rib · crackedL HORIZONTAL LEADING EDGE INBD END RIB IS CRACKED.(<P>CUT OUT DAMAGE AND REPAIRED IAW B767 SRM 55-10-09 REPAIR 1.</P>)SDR UIEA2020030900417Angle · crackedCLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLE.(<P>REMOVED AND REPLACED CRACKED CLOSE OUT ANGLE UNDER RUDDER IAW BOEING DOCUMENT #173T1215 AND B767-200 SRM 51-40-02.</P>)SDR UIEA2020030900418Structure · corrodedL HORIZ STAB UPPER CHORD ATTACH FITTING UNDER PANEL 335AT HAS CORROSION UNDER NUT PLATES, AND ALSO CORRODED NUT PLATES. (<P><SPAN>CORROSION BENEATH 335AT FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED CORRODED CHORD IAW BOEING DWG 182T7103.</SPANSDR UIEA2020030900419Attach Bracket · crackedATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IS CRACKED.(<P>REMOVED AND REPLACED ATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)SDR ABXR2020022410011Attach Fitting · corrodedLEFT HORIZ STAB. UPPER CHORD ATTACH FITTING UNDER PANEL 335AT HAS CORROSION UNDER NUT PLATES & ALSO CORRODED NUT PLATES.CORROSION BENEATH 335AT FOUND TO BE OUT OF LIMITS. REMOVED , FABRICATED & REPLACED CORRODED CHORD ( PN 182T7103-77) IAW BOEING DWG 182T7103SDR ABXR202002240010Flange · corrodedFLANGE UNDER PANEL 335AT HAS CORROSION ON UPPER SURFACE.REMOVED CORROSION IAW B767-200 55-10-09 ALLOWABLE DAMAGE FOUND TO BE OUT OF LIMITS OT ".090 R.T .077SDR ABXA2020030520042Panel · corrodedLH WING FUEKL TANK PANEL 533AB CORRODED. AIRCRAFT WAS GROUNDED.SDR ABXR2020022700013Skin · crackedUPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.REPAIRED L/H FUSELAGE SKIN STA: 1654.5 I.A.W. B767 SRM 53-80-01-2R-4 REPAIR 4.SDR ABXR2020022400012Attach Fitting · corrodedUPPER TRAILING EDGE PANEL ATTACH CHORD AT WS.434 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE. BLENDED CORROSION ON UPPER CORD ON AILERON RIB AT WS 434 TO A DEPTH OF 0.17", MAX DEPTH ALLOWED .008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMISDR ABXR2020022104009Splice Plate · corrodedCORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06 SEE BACK AND PARTIAL WS 27 PGS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED. COMPLETED HOLE SCAN ON SPLICE PSDR ABXR2020022140003Spar · corrodedFRONT SPAR UPPER CORD CORRODED AROUND RIVET .013" MATERIAL REMOVED , FOUND TO OUT OF LIMITS. REPAIRED PER AMES ENGINEERING DOCUMENT REA 47396REA01.SDR ABXA2020030514043Attach Angle · corrodedLH WW AR STA 1021 ATTACH ANGLE CORRODED. AIRCRAFT WAS GROUNDED.
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