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 IPXA09655380Floor Panel · puncturedINSPECTION TYPE:C DMI D396291 - 1 HOLE FOUND AT 1ST FLOOR PANEL FROM LT SIDE POS 13 ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.Mar 30, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655379Floor Panel · puncturedINSPECTION TYPE:N/A D396289 - 1 HOLE FOUND AT 7TH FLOOR PANEL FROM LT POS 12R ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.Mar 30, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655378Floor Panel · puncturedINSPECTION TYPE:C D396293 - 1 HOLE FOUND AT 3RD FLOOR PANEL FROM LT SIDE POS 2L ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.Mar 30, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655194Floor Panel · damagedINSPECTION TYPE:N/A POS 9 RBL 5 STATION 1134 DAMAGED 1.7 X 1.2 PUNCTURE. REPAIRED PER EO B767-5320-32928-A.Mar 30, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655193Floor Panel · damagedINSPECTION TYPE:N/A POS 9R RBL 8 STATION 1160 DAMAGED 1 INCH CUTOUT. REPAIRED PER EO B767-5320-32929-A.Mar 30, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655481Mount · crackedINSPECTION TYPE:C AFT CARGO DOOR MANUAL DRIVE SYS CHK FOUND FWD PDU EXCESSIVE MOVEMENT CAUSED THE PDU MOUNTING UPR STRUCTURE CRACKED. (CRACK 1.25 INCH LENGTH). AFT CARGO DOOR PDU MOUNTING UPPER WEB AND DOUBLER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PEMar 29, 2009 · N323UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655149Seat Track · damagedINSPECTION TYPE:N/A SEAT TRACK DAMAGED AT STA 1518 RBL 33. REPAIRED PER EO B767-5310-32616-B.Mar 24, 2009 · N323UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA09655145Engine · bird ingestionINSPECTION TYPE: ETOP ATB - AFTER DEPARTURE THE CAPTAIN REPORTED TO FLIGHT CONTROL VIA ACARS A BIRD STRIKE WITH POSSIBLE ENGINE AND/OR AIRFRAME DAMAGE. VIBRATION WAS REPORTED ON THE RIGHT ENGINE. REMOVED AND REPLACED RT ENGINE PER TC 6002. ENG TEST C/W PERMar 24, 2009 · N309UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR IPXA09655167Panel · crackedINSPECTION TYPE:N/A LEADING EDGE FIBERGLASS STRIP LOWER I/B HAS CRACK NEAR WING ROOT. CLASSIFIED AS A MAJOR REPAIR. TRANSFERRED TO NRC 354826. REPAIRED LT WING I/B SLAT CLOSEOUT PANEL IAW EO B767-5730-32829A (TEMP REPAIR). PERMANENT REPAIR OR REPLACEMENT NMar 23, 2009 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09655128Panel · crackedINSPECTION TYPE:N/A NR 6 SLAT LT SIDE CLOSURE PANEL CRACKED. INSTALLED INTERIM REPAIR PER SRM 57-43-01.Mar 23, 2009 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09655124Circuit Card · damagedINSPECTION TYPE:ETOP ATB - WHILE CLIMBING OUT, CREW RECEIVED RIGHT BLEED DUCT EICAS MESSAGE. NO EMERGENCY WAS DECLARED. ACFT OOS T/S IN PROGRESS. REMOVED AND REPLACED DETECTOR CARD PER AMM 26-10-01-4. T/S RT BLEED DUCT LEAK CAUTION EICAS MESSAGE. FOUND ELMar 23, 2009 · N309UP · Boeing 76734AF · Overheat DetectionSDR IPXA09655142Fairing · delaminatedINSPECTION TYPE:C LT 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.Mar 19, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655175Stiffener · crackedINSPECTION TYPE:C WING CENTER SECTION FWD BULKHEAD VERTICAL STIFFENER FOUND CRACKED JUST AT RBL 10, WL 195. CRACK 3.75 INCH LENGTH. WING CTR SECTION FWD BULKHEAD STA 785.9 WL 195 RBL 10 VERTICAL STIFFENER REPAIRED AS PER HX RS R57-11-36287 REV B AND UPS EO BMar 18, 2009 · N319UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA09655150Stiffener · crackedINSPECTION TYPE:6C MEC - MAIN DECK FLOOR SUPPORT ATT STIFFENER FOUND CRACKED JUST AT STA 246 RBL 10 - RBL 11. MEC - MAIN DECK FLOOR SUPPORT ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT STA 246 RBL 10 - RBL 11.Mar 18, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655138Panel · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP LWR PNL 555EB FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.Mar 18, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655136Stiffener · deformedINSPECTION TYPE:C BULK CARGO - STA 1480 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT LBL 9. BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT LBL 9.Mar 18, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655135Stiffener · deformedINSPECTION TYPE:C BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1480 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.Mar 18, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655134Stiffener · deformedINSPECTION TYPE:C BULK CARGO STA 1461 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1461 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.Mar 18, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655133Stiffener · deformedINSPECTION TYPE:C BULK CARGO - STA 1502 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1502 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9.Mar 18, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655159Attach Fitting · crackedINSPECTION TYPE:C MEC - BS 246 CABIN FLOORBEAM AFT FACE ATT CLIP CRACKED AT LBL 50 (CRACK 1 INCH LENGTH). MEC - BS 246 CABIN FLOORBEAM AFT FACE ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT LBL 50.Mar 17, 2009 · N319UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09655120Floorbeam · crackedINSPECTION TYPE:C MEC STA 246 CABIN FLOORBEAM FWD FACE ALTERNATE L/G ELECT ACT SUPPORT ANGLE CRACKED AT LBL 25 (CRACK 0.625 INCH LENGTH). MEC STA 246 CABIN FLOORBEAM FWD FACE ALTERNATE L/G ELECT ACT SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS Mar 17, 2009 · N319UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09655176Fitting · crackedINSPECTION TYPE:C LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP FOUND CRACK. CRACK 0.75 INCH LENGTH. LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09655158Hinge Fitting · crackedINSPECTION TYPE:C LT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FITTING FOUND CRACKED. CRACK 1.25 INCH AND 1.5 INCH LENGTH. LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 SHT 1 TO 5 REV 43. THIS IS CLASSIFIED AS A MAJMar 16, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655157Support · crackedINSPECTION TYPE:C FWD CARGO COMPT STA 480.75 DOOR SILL BALLMAT PANEL FOUND CRACKED. CRACK 3.75 INCH LENGTH. FWD CARGO COMPT STA 480.75 DOOR SILL BALLMAT PANEL SUPPORT REPAIRED AS PER HX RS R53-00-36286 REV B AND UPS EO B767-5300-32787-A.Mar 16, 2009 · N319UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09655141Panel · delaminatedINSPECTION TYPE:C RT WING NR 7 SLAT LWR CLOSURE PANEL I/B AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W4-01) DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09655140Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE MID AREA THE EXISTING REPAIR PATCH (REF SURVEY SEQ 319-W3-03) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655139Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE I/B AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-04) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655137Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER T/E MID AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-02) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.Mar 16, 2009 · N319UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655039Skin · damagedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGED AT STA 654+58 STR 32R. REMOVED DAMAGE AND REPAIRED IAW EO B767-5330-32729-A.Mar 16, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09655038Skin · damagedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGE DUE TO LIGHTNING STRIKE AT STA 654 AND STRINGER 32R. REMOVED DAMAGE AND REPAIRED IAW EO B757-5330-32682-B.Mar 16, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09655939Floor Panel · crackedINSPECTION TYPE:6C DMI NR D395403, MAIN CARGO AFTER CENTER OF POS 4 HAS 2 EACH 2 INCH CRACK IN FL FLOOR PANEL. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.Mar 14, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655122Floor Panel · puncturedINSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2, FWD RIGHT CORNER OF RIGHT O/B PANEL AT STN 412 (PUNCTURE ABOUT .75 INCH). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.Mar 14, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655121Floor Panel · puncturedINSPECTION TYPE:C FLOOR PANEL DAMAGED POS 2 SECOND FLOORBOARD FROM RIGHT STATION 412 .5 INCH PUNCTURE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43.Mar 14, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655002Shunt · inoperativeINSPECTION TYPE:ETOP ATB - LT ENG PRI AND STBY EGT INOP. EPER FIM 77-21-00 PIMU BITE SHOWS 352 16A EGT SENSOR AND 352 16B EGT SEN PER PIMU MESS INDEX. REMOVED AND REPLACED SHUNT JUNCTION BOX IAW 77-21-53-4 UP TO OPS CK. SHUNT BOX CKS J131 PIN B TO J3 PIN E Mar 12, 2009 · N306UP · Boeing 76734AF · Engine Temperature Indicating SystemSDR IPXA09654996Floor Panel · crackedINSPECTION TYPE:N/A CENTERLINE FLOOR PANEL CRACKED AT POSITION 8. REMOVED PANEL AND ROUTED TO SHEET METAL FOR REPAIR. INSTALLED CENTERLINE FLOORBOARD PANEL AT POS NR 8 ON MCD PER EO B767-5320-9693E.Mar 9, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654995Floorboard · damagedINSPECTION TYPE:N/A MAIN CARGO DOOR FLOORBOARD PANEL DAMAGED AT POS 13 REF D 392745. REMOVED FLOOR PANEL FOR REPAIR/REPLACEMENT. REMOVED AND REPLACED POS 13 FLOOR PANEL PER EO B767-5330-9693 APPX B. THIS CLEARS D 392745.Mar 9, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654967Floor Panel · crackedINSPECTION TYPE:N/A MCD POS NR 8 PANEL CRACKED. CRACK RUNS FROM EDGE TO EDGE. REPAIRED PER EO B767-5320-9693-E.Mar 9, 2009 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655000Skin · misrepairedINSPECTION TYPE:6C SURVEY SEQUENCE NR 316-F1-03 BETWEEN BS 440 - 462.5 AND STR 22R TO STR 25R REPAIR PATCH IS NOT CORRELATED TO SRM. SURVEY SEQUENCE NR 316-F1-03 A SINGLE REPAIR COVERING BOTH DAMAGES AT SURVEY SEQUENCE NR 316-F1-03 AND 316-F1-04 AT BS 439.5 TMar 4, 2009 · N316UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09654897Structure · dentedINSPECTION TYPE:N/A MAIN CARGO FLOOR DENTED BETWEEN POS 5 AND 6L. REPAIR COMPLETED WITH EO B767-5320-9693. THIS CLEARS DEFERRAL 388589. NO FURTHER ACTION REQUIRED.Mar 2, 2009 · N311UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09654883Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL POSITION 8R IS DAMAGED AT EDGE. REPAIRED IAW EO B767-5320-32520-A.Mar 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654882Floor Panel · dentedINSPECTION TYPE:N/A MCD FLOOR PANEL POSITION 4L HAS 5 INCH DENT. REPAIRED IAW EO B767-5320-32520-A.Mar 2, 2009 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654975Bracket · crackedINSPECTION TYPE:C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (CRACK 1.125 INCH LENGTH). RT WING LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40Mar 1, 2009 · N316UP · Boeing 76734AF · Wing SparSDR IPXA09654974Bracket · crackedINSPECTION TYPE:C LT WING - L/E LES 580 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (CRACK 1.75 INCH LENGTH). LT WING LES 580 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-Mar 1, 2009 · N316UP · Boeing 76734AF · Wing SparSDR IPXA09654972Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B MAIN FLAP AFT FLAP SUPPORT HINGE ARM UPPER MOUNT. LWR FLANGE CRACKED (CRACK 1 INCH LENGTH). RT WING I/B MAIN FLAP SUPPORT HINGE ARM UPPER MOUNT LWR FLANGE REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 SHT 1-5 REV 43. THIS IS CLASSIFMar 1, 2009 · N316UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09654971Hinge Fitting · crackedINSPECTION TYPE:C LT WING - I/B MAIN FLAP AFT SUPPORT HINGE ARM UPPER MOUNT LWR FLANGE CRACKED (CRACK 1.5 INCH LENGTH). LT WING - I/B MAIN FLAP AFT SUPPORT HINGE ARM UPPER MOUNT LWR FLANGE REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 SHT 1-5 REV 43, THIS IS CLASSMar 1, 2009 · N316UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09655922Floor Panel · dentedMCD CENTER FLOOR PANEL HAS LONG DENT IN PANELS. ACCOMPLISHED PERMANENT REPAIR PER EO B767-5320-9693-F. PERMANENT REPAIR ACCOMPLISHED AT NEXT C CHECK.Feb 28, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654993Skin · dentedINSPECTION TYPE:6C FX BS 1417 - 1439 STR 33L TO STR 36L SKIN DENT. FUSELAGE BS 1417 TO 1439 BETWEEN STR 33L - 36L 4EA SCRATCHES SMOOTHED OUT AND REPROTECTED AS PER RS R53-60-36281 REV A. NO CRACK AFTER HFEC INSP PER NTM PART 6 51-00-01.Feb 28, 2009 · N316UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09654836Floor Panel · damagedPOSITION 10 L HAS A HOLE 1 INCH IN DIA IN THE FWD O/B CORNER (DEFERRAL 390713). TRANSFERRED TO NRC 353656. VERIFIED FABRICATION OF NEW PANEL PER EO B767-5320-9693-E, APPX B, STEPS 3-6. OK TO INSTALL FLOORBOARD. INSTALLED PANEL ON L/P 012206 THIS CLEARS D390Feb 24, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654816Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED. REPLACED FLOORBOARD IAW EO B767-5320-9693-E.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09654814Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGE. FABRICATED NEW PANEL IAW EO B767-5320-9693-E.Feb 23, 2009 · N319UP · Boeing 76734AF · Fuselage Floor Panel
Back to Boeing 767-34AF