Boeing 767-34AF

Service difficulty reports · 6,321

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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"

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SDR IPXA09657867Floorboard · damagedFLOORBOARD ON MCD CENTER POS 9 DAMAGED. FABRICATED FLOORBOARD PER EO B767-5320-9693-F.Nov 2, 2009 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657853Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT OTBD AREA AT OSS641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063IN CRACK LENGTH IS 0.090 INCH DAMAGED CUTOUT IS 7.7Nov 1, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657852Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063 IN CRACK LENGTH IS 0.125IN DAMAGED CUTOUT IS 7.25 INov 1, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657851Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 ORG MAT'L IS CLAD7075T6-0063IN, CRACK LENGTH IS 0.125 INCH DAMAGED CUTOUT IS 7.735 INCNov 1, 2009 · N324UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA09657850Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01 2R2 FIG 201 REV45 ORG MAT'L IS CLAD 7075T6-0063 IN, CRACK LENGTH IS 0.090IN. DAMAGED CUTOUT IS 7.Nov 1, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657884Support Angle · crackedINSPECTION TYPE:C NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP CRACKED AT NAC STA 285.45 (CRACK LENGTH 1 INCH). NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 Oct 26, 2009 · N324UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA09657859Floor Support · crackedINSPECTION TYPE:C BULK CARGO COMPT STA 1439 LBL 24 INCH FLOOR PANEL SUPPORT FOUND CRACK (CRACK LENGTH 1.75 INCH), BULK CARGO STA 1439 LBL 22.33 INCH FLOOR SUPPORT REPAIRED AS PER SRM 51-70-11-0G FIG 1 REV 45 ORG, MATERIAL IS 7075T6-0.040IN, CRACK LENGTH 1.75 IOct 26, 2009 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657801Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL POS 5R. REPAIRED PER SRM 53-00-50-2R.Oct 26, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657800Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL 5R DAMAGED. REPAIRED PER SRM 53-00-50-2R.Oct 26, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657799Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL POS 5R DAMAGED. REPAIRED PER SRM 53-00-50-2R.Oct 26, 2009 · N302UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657876Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 25, 2009 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657875Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER REPLACE AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 25, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657874Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 25, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657873Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 25, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657866Frame · crackedINSPECTION TYPE:C NR 1 PYLON INTERNAL FRAME CRACKED AT NAC STA 285.45 RT SIDE, (CRACK LENGTH 2 INCHES) NR 1 PYLON INTERNAL FRAME REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT NAC STA 285.45 RT SIDE.Oct 25, 2009 · N324UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/RibSDR IPXA09657863Stiffener · deformedINSPECTION TYPE:C BULK CARGO COMPT STA 1502 LBL 16 INCH FLOOR PANEL STIFFENER FOUND DEFORM. STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Oct 25, 2009 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657883Panel · damagedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.Oct 24, 2009 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657882Panel · damagedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.Oct 24, 2009 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657878Fairing · delaminatedINSPECTION TYPE:C LT WING O/B FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.Oct 24, 2009 · N324UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA09657865Slat · chafedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4, FIG 202 SHEET 8.Oct 24, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657881Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-02 PAR 5C FIG 2 REV 45.Oct 23, 2009 · N324UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09657880Bracket · crackedINSPECTION TYPE:C LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (1.125 INCH). LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 23, 2009 · N324UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09657879Panel · delaminatedINSPECTION TYPE:C LEFT I/B ELEVATOR UPPER SURFACE O/B T/E AREA DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PAR 4A FIG 10 REV 45.Oct 23, 2009 · N324UP · Boeing 76734AF · Elevator, Plate/SkinSDR IPXA09657877Angle · crackedINSPECTION TYPE:6C AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP FOUND CRACK. AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657864Doubler · delaminatedINSPECTION TYPE:C LHW INBD AFT FLAP UPPER SURFACE OTBD T/E AREA DELAMINATED FOUND ON EXISTING REPAIR PATCH. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4 FIG 201 SHEET 1.Oct 23, 2009 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657837Slat · chafedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REV 45 REPAIR 4 FIG 202 SHEET 8 AND SHEET 9 NOTES.Oct 23, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657833Fitting · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP FOUND CRACK (CRACK LENGTH 0.75 INCH). AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657827Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657826Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657825Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1197+108 TO 1263, RBL 77 TO RBL 88. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657824Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 283 TO 412, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657823Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1425 TO 1540, LBL 55 TO LBL 77. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657822Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 833 TO 930, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657821Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGE AT STA 654+22 TO 690 RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.Oct 23, 2009 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657860Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 RBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.25 I NCH), AFT BULK CARGO STA 1562-1582 RBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45Oct 22, 2009 · N324UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657858Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.5 INCH), AFT BULK CARGO STA 1562-1582 LBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 22, 2009 · N324UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657857Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 1.375 INCH), AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 22, 2009 · N324UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657836Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT O/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). LEFT WING NR 3 SLAT O/B AREA AT OSS792.3 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH Oct 22, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657835Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK .0625 INCH). LEFT WING NR 3 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH Oct 22, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657834Web · crackedINSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). RIGHT WING NR 10 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201 REV 45 ORG. MATERIAL IS CLAD 7075T6-0.063IN, CRACK LOct 22, 2009 · N324UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657820Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP FOUND CRACK (CRACK LENGTH 1.5 INCH). MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 22, 2009 · N324UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657816Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP FOUND CRACKED CRACK 0.875 INCH. MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 22, 2009 · N324UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657746Floor Panel · damagedMCD FLOOR PANEL DAMAGED POS 9. REPAIRED PER EO B767-5320-9693-F.Oct 19, 2009 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657666Panel · delaminatedRT WING INBD MAIN FLAP UPPER SURFACE OTBD EDGE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657665Panel · delaminatedVERTICAL STAB L/E AREA LT UPPER PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-70 PAR 5C FIG 10 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA09657664Stiffener · crackedFWD CARGO COMPT STA 785.9 LBL10.94 CENTER FRONT SPAR STIFFENER FOUND CRACK. FWD CGO COMPT STA785.9 LBL10.94 CTR TANK FRONT SPAR STIFFENER REPAIRED AS PER RS R57-10-36448 AND EO B767-5710-35177. ORG MAT'L BAC1518-912 2024T3511 DAMAGED SECTION CUT LENGTH 18.75Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657663Stiffener · crackedFWD CARGO STA 785.9 LBL32.94 CENTER TANK FWD B/H STIFFENER CRACK. FWD CARGO STA 785.9 LBL 32.94 CTR TANK FWD B/H STIFFENER REPAIRED AS PER HX RS R57-10-36449 & EO B767-5710-35176. ORG MAT'L BAC1518-749 2024-T3511, DAMAGED SECTION CUT LENGTH 16.5 INCH THIS REOct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657662Stiffener · crackedBULK CARGO COMPT STA 1480 RBL 8 FLOOR PANEL SUPPORT VERTICAL STIFFENER CRACK. REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657660Floor Support · crackedBULK CARGO COMPT STA 1417 LBL15 FLOOR PNL SUPPORT FOUND CRACKED. BULK CARGO COMPT STA 1417 LBL 15 FLOOR PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657658Floor Support · crackedBULK CARGO COMPT STA 1417 LBL9 FLR PNL SUPPORT FOUND CRACK. BULK CARGO COMPT STA 1417 LBL9 FLOOR PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous Structure
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