Boeing 767-34AF

Service difficulty reports · 6,321

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 = '76734AF'
  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.

SDR IPXA09654812Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 8R HAS 1 INCH DIA HOLE I/B AFT CORNER 2 HOLES 1 INCH DIA. REPAIR PER EO B767-5320-32410-A.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654811Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL POSITION 2R HAS DAMAGE. EXISTING REPAIR DAMAGED 1" X 2" UPPER SKIN AND CORE DAMAGED IN THE AFT POSITION OF AN EXISTING REPAIR LOCATED 2 INCHES FROM AFT EDGE. EXISTING REPAIR IS 4" X 4". REPAIR PER EO B767-5320Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654810Floor Panel · damagedINSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 2R HAS 1 INCH HOLE, 2 INCHES AFT OF THE CENTER LOCK, 1 INCH HOLE 2 INCHES AFT OF FWD EDGE OF PANEL 6 INCHES FROM RT EDGE, .75 INCH HOLE AFT OF FWD EDGE OF PANEL 3 .5 INCH FROM EDGE. REPAIR PER EO B767-5320-32412-AFeb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654809Floor Panel · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED AT POS 2R/3R. FABB'ED MAIN CARGO DECK FLOOR PANEL IAW B767-5320-9693-E STEPS B 1 THROUGH 6 STEPS B 7 THROUGH 12, PREVIOUSLY COMPLIED WITH ON EO B767-5320- 9693 APPX B.Feb 23, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654808Floor Panel · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGE AT POSITION 2R. FABRICATED MAIN CARGO DECK FLOORBOARD IAW B767-5320-9693-E STEPS B1 THROUGH 6 STEPS B7 THROUGH 12, PREVIOUSLY COMPLIED WITH ON EO B767-5320 -9693 APPX B THIS CLEARS D394364 LP 200901/3.Feb 23, 2009 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654840Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL HAS .75 INCH HOLE IN CENTER OF POSITION 5, DEF 387484. TRANSFERRED TO NRC 363350. REMOVED DAMAGE & INSTALLED REPAIR PER EO B767-5320-32392A.Feb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654839Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL HAS .75 INCH HOLE IN CENTER POSITION 4 (DEF387483). TRANSFERRED TO NRC 353652. REMOVED DAMAGE & INSTALLED REPAIR REF EO B767-5320-32392A.Feb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654838Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL IN CENTER OF POSITION 3 HAS HOLE. TRANSFERRED TO NRC 323651. REMOVED DAMAGE REF EO B767-5320-32391A. DAMAGE REMOVAL VERIFIED. OK TO INSTALL REPAIR. POTTED CORE & CURED AS PER SRM 53-00-50-2R. INSTALLED REPAFeb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654837Floor Panel · damagedMAIN CARGO FLOOR PANEL IN CENTER POSITION 6/7 HAS 4 SMALL HOLES. TRANSFERRED TO NRC 353653. REMOVED DAMAGE REF EO B767-5320-32393-A. POTTED CORE & APPLIED REPAIR PLIES IAW EO B767-5320-32393 AND SRM 53-00-50-2R.Feb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654799Floor Panel · damagedINSPECTION TYPE:N/A MAIN DECK FLOOR PANEL AT STA 627 BL 0 DAMAGED 1 INCH HOLE IN TOP SKIN AT CENTER OF PANEL. DAMAGE 59 INCHES FROM AFT OF PANEL AND 3.5 INCHES FROM RT EDGE OF PANEL. REPAIR PER EO B767-5320-32392-A.Feb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654798Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL DAMAGED AT STA 671 BL 0, 14 INCHES FROM AFT EDGE OF PANEL 3 INCHES FROM RT SIDE OF PANEL PUNCTURE .75 INCH DIA. REPAIR PER EO B767-5320-32392-A.Feb 22, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654817Circuit Card · not seatedINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS. CHECK CARRIED OUT PER TASK PER FIM 26-18-00 AND FOLLOWED WDM 26-18-21. NOTICED CARD M691 NOT SEATED PROPERLY. SAME RESEATED C/W TASK 26-18-00 TEST PASSED. PERFORMED ENGINE RUN Feb 20, 2009 · N309UP · Boeing 76734AF · Overheat DetectionSDR UPS09654817Duct · leakingINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS.Feb 20, 2009 · N309UP · Boeing 76734AF · Pneumatic Distribution SystemSDR UPS09654723Wedge · damagedINSPECTION TYPE:N/A RIGHT O/B FLAP T/E WEDGE DAMAGED CUTOUT 3.5 X 6.0. REPAIRED PER EO B767-5750-32178-B.Feb 15, 2009 · N318UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654752Floor Support · crackedINSPECTION TYPE:6C BULK CARGO COMPT STA 1461 RBL 15 FLOOR SUPPORT CHANNEL FOUND CRACKED. BULK CARGO COMPT STA 1461 RBL 15 FLOOR SUPPORT CHANNEL REPAIRED AS PER SRM 51-70-11 FIG 1.Feb 12, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654783Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. 0.375 INCH LENGTH. RT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R 1 FIG 201.Feb 11, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654756Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1502 RBL 8 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1502 RBL 8 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654755Floor Support · dentedINSPECTION TYPE:6C BULK CARGO COMPT STA 1527 LBL 13 FLOOR PANEL NUT CHANNEL FOUND DENT. BULK CARGO COMPT STA 1527 LBL 13 FLOOR PANEL SUPPORT CHANNEL REPAIRED AS PER SRM 51-70-11 FIG 1.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654754Floor Support · dentedINSPECTION TYPE:6C BULK CARGO COMPT STA 1534 RBL 15 FLOOR PANEL NUT CHANNEL FOUND DENT. BULK CARGO COMPT STA 1534 RBL 15 FLOOR PANEL SUPPORT CHANNEL REPAIRED AS PER SRM 51-70-11 FIG 1.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654753Floor Support · dentedINSPECTION TYPE:6C BULK CARGO COMPT STA 1510 RBL 26 FLOOR PANEL NUT CHANNEL FOUND DENT. BULK CARGO COMPT STA 1510 RBL 26 FLOOR PANEL SUPPORT CHANNEL REPAIRED AS PER SRM 51-70-11 FIG 1.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654751Floor Support · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1417 LBL 29 FLOOR PANEL SUPPORT CHANNEL FOUND DEFORMED. BULK CARGO COMPT STA 1417 LBL 29 FLOOR SUPPORT CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654750Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1502 LBL 8 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1502 LBL 8 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654749Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1461 RBL 15 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1461 RBL 15 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654748Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1461 RBL 8 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1461 RBL 8 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654747Floor Support · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1417 LBL 22 FLOOR PANEL SUPPORT CHANNEL FOUND DEFORMED. BULK CARGO COMPT STA 1417 LBL 22 FLOOR PANEL SUPPORT CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654746Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1439 LBL 22 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1439 LBL 22 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654745Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1480 RBL 15 STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 RBL 15 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654805Slat · delaminatedINSPECTION TYPE:C LT WING NR 3 SLAT UPPER SURFACE DELAMINATION. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203 REV 43. DOUBLER MATERIAL 2024T3-0016IN AND ADHESIVE FILM AF163-2K0010IN. REPAIR DOUBLER SIZE 4.125 X 5 INCHES.Feb 11, 2009 · N322UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654789Floorbeam · crackedINSPECTION TYPE:C MAIN E/E COMPT MAIN DECK FLOORBEAM MID CHORD AT VERTICAL EDGE CRACK 0.75 INCH LENGTH. MAIN E/E COMPT M/D FLOORBEAM MID CHORD UPPER VERTICAL FLANGE REPAIRED AS PER SRM 53-10-51-2R 2 REPAIR 2 REV (43), THIS IS CLASSIFIED AS A MAJOR REPAIR WITHFeb 11, 2009 · N322UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09654821Hinge Fitting · crackedINSPECTION TYPE:C LT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. CRACK 1 INCH LENGTH. LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654782Repair · chafedINSPECTION TYPE:C RT WING I/B AFT FLAP UPPER I/B AREA FOUND DEEP CHAFED ON EXISTING REPAIR PATCH. METAL HOT BOND REPAIR PERFORMED ON RT WING I/B AFT FLAP UPPER I/B AREA EXISTING REPAIR PATCH AS PER SRM 51-70-10 REPAIR 4 FIG 202.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654781Panel · damagedINSPECTION TYPE:C RT WING INTERSPAR LOWER SKIN PANEL INTERNAL AREA FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED ON RT WING INTERSPAR LOWER SKIN PANEL INTERNAL AREA AS PER SRM 51-70-10 REPAIR 4 FIG 202.Feb 10, 2009 · N322UP · Boeing 76734AF · Wing, Plate/SkinSDR UPS09654780Panel · misrepairedINSPECTION TYPE:C LT WING NR 6 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH NON- STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654779Panel · misrepairedINSPECTION TYPE:C RT WING NR 7 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH NON- STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654777Floor Panel · damagedINSPECTION TYPE:6C FLOOR PANEL FOUND HOLES AT POSITION 11-12 UNDER CENTER LOCK RIGHT SIDE ABOUT 1" X .5" APPROX. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REPAIR AREA ABOUT 1" X .5" AT TWO LOCATION.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654776Floor Panel · damagedINSPECTION TYPE:6C MAIN DECK CARGO, FLOOR PANEL FOUND HOLE ABOUT 1" X .5" AND DENT MARK ABOUT 2" X 2.5" APPROX AT STA 678, LBL 7 APPROX. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654760Flap · delaminatedINSPECTION TYPE:C LT WING O/B FLAP I/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654759Flap · misrepairedINSPECTION TYPE:6C RT WING I/B MAIN FLAP LOWER T/E MID AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A(1) FIG 5 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654758Flap · damagedINSPECTION TYPE:6C LT WING O/B FLAP LWR TRAILING EDGE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-06 PARA 5A(1) FIG 9 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654757Fairing · delaminatedINSPECTION TYPE:N/A RT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03, PARA 5A (1) FIG 5 REV 43.Feb 10, 2009 · N322UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654807Bracket · crackedINSPECTION TYPE:C RT WING - L/E LES 675 UPPER FIXED SUPPORT AFT BRACKET FOUND CRACKED. CRACK 1 INCH LENGTH. RT WING - L/E LES 675 UPPER FIXED SUPPORT AFT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Feb 10, 2009 · N322UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS09654806Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1086 RBL 25 BELOW FLOOR SUPPORT CLIP FOUND CRACKED. CRACK 0.75 INCH LENGTH. AFT CARGO COMPT STA 1086 RBL 25 BELOW FLOOR SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654804Stiffener · crackedINSPECTION TYPE:C RT WING - LES 662 FRONT SPAR STIFFENER FOUND CRACK. CRACK 0.375 INCH LENGTH. RT WING - LES 662 FRONT SPAR STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Feb 10, 2009 · N322UP · Boeing 76734AF · Wing SparSDR UPS09654788Attach Angle · crackedINSPECTION TYPE:C MAIN DECK FLOOR SUPPORT ATTACH ANGLE CRACK JUST AT STA 1580 RBL 75 CRACK 1.125 INCH LENGTH. MAIN DECK FLOOR SUPPORT ATTACH ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 JUST AT STA 1580 RBL 75.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654787Attach Angle · crackedINSPECTION TYPE:C MAIN DECK FLOOR SUPPORT ATTACH ANGLE FOUND CRACKED JUST AT STA 1580 LBL 75. CRACK 1 INCH LENGTH. MAIN DECK FLOOR SUPPORT ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 AT BS 1580 LBL 75 AREA.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654786Fitting · crackedINSPECTION TYPE:C MAIN EQUIPMENT CENTER STA 246 LBL 50 CLIP FOUND CRACKED, 0.75 INCH. MAIN EQUIPMENT CENTER STA 246 LBL 50 CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Feb 10, 2009 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09654820Antenna · misinstalledINSPECTION TYPE:C FUSELAGE - UPPER GPS ANTENNA FOUND INSTALLED, AT BS 654+33 STR 1L-1R, REMOVE GPS ANTENNA AND REPAIR THE CROWN SKIN AT THE DISCREPANT UPPER GPS ANTENNA POSITION. SURVEY SEQ 322-F1-03, FUSELAGE BS 654+33 BETWEEN STR 1L TO STR 1R SKIN REPAIRED Feb 9, 2009 · N322UP · Boeing 76734AF · Global Positioning SystemSDR UPS09654641Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 964 RBL 4. REPAIRED PER EO B767-5320-32226-A.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654640Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 1096. REPAIRED PER SRM 53-00-50-2R.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654639Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL DAMAGED FS 486 AND 491 LBL 84. REPAIRED PER EO B767-5320-32227-A.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor Panel
Back to Boeing 767-34AF