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 IPXA09657189Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657188Fairing · delaminatedINSPECTION TYPE:C RT WING O/B FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT O/B PLACE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5.Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657187Fairing · delaminatedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT I/B PLACE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44.Aug 20, 2009 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657168Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 20, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657250Panel · crackedINSPECTION TYPE:C LT WING NR 6 SLAT LWR CLOSURE PANEL CRACKED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 44. REPAIR PATCH SIZE 12 X 6 INCHES.Aug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657241Support Fitting · crackedINSPECTION TYPE:7C LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP FOUND CRACKED. LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657238Skin · misrepairedINSPECTION TYPE:C SURVEY SEQUENCE 307-F1-07 BULK CARGO DOOR BETWEEN BS 1434-1447 & STR 25L - 28L AREA SKIN REPAIR DOES NOT CORRELATE TO THE SRM. REPAIR SIZE 12.5 X 14.5 INCHES. BULK CARGO DOOR BETWEEN BS 1434 - BS 1447 & STR 25L - 28L AREA SKIN REPAIRED PER Aug 19, 2009 · N307UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA09657175Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657174Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657173Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO 690, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657165Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657164Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1207 TO 1344, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657162Floor Panel · crackedINSPECTION TYPE:C MCD FLOOR PANEL FOUND CRACK AT STA 977 TO 1043, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 19, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657151Skin · crackedINSPECTION TYPE:C LT WING NR 4 SLAT I/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT I/B AREA OSS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01- 2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPAug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657150Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT O/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT O/B AREA OSS 641.49 NOSE SKIN REPAIRED AS PER SRM 57-43- 01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIAug 19, 2009 · N307UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657252Skin · misrepairedINSPECTION TYPE:C SURVEY SEQUENCE 307-F1-01 FUSELAGE BETWEEN BS 289 TO BS 303 AND STR 24L - 26L AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. FX BETWEEN BS 289-303 & STR 24L-27L AREA SKIN REPAIRED WITHOUT ZERO TIMING AS PER SRM 53-00-01-2R12 REV 44 & BOEIAug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657172Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657171Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657170Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657169Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657167Floor Panel · delaminatedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DELAMINATION AT STA 930 TO 975, LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657166Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO 1598, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657163Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, RBL 77 RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657149Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 40 FLOORBEAM ATT STIFFENER FOUND CRACKED (CRACK LENGTH 1.25 INCH). MEC COMPT STA 246 LBL 40 FLOORBEAM ATTACH STIFFENER REPAIRED REF SRM 53-10-51-2R4 REV 44. THIS IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0.063Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657124Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 50 CLIP FOUND CRACK LENGTH 0.75 INCH. MEC COMPT STA 246 LBL 50 CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657111Attach Angle · crackedINSPECTION TYPE:ETOP MEC COMPT STA 246 LBL 25 FLOORBEAM ATT ANGLE FOUND CRACK. MEC COMPT STA 246 LBL 25 FLOORBEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AN INSTALLED AS PER SRM 51-40-02 REV 44.Aug 18, 2009 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657082Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD POS 8R HAS DAMAGE. REPAIRED IAW EO B767-5320-34623-A.Aug 17, 2009 · N316UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657073Floor Panel · damagedINSPECTION TYPE:N/A D-403978 MAIN CARGO DECK POS 2R FLOOR PANEL INTERIM REPAIR. REPLACED PANEL PER EO767-5320-9693-F.Aug 15, 2009 · N323UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656992Support · crackedINSPECTION TYPE:C LEFT WING L/E LES 675 FIXED FAIRING SUPPORT AFT UPPER FRONT SPAR ANGLE FOUND CRACKED. CRACK LENGTH 0.75 INCH. LEFT WING L/E LES 675 FIXED FAIRING SUPPORT AFT UPPER FRONT SPAR ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REVAug 4, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656986Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 731 TO 833, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 4, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656974Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 690 TO 731, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 4, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656973Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 654+22 TO 690, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53- 01-01.Aug 4, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657019Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 4 SLAT O/B AREA OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657018Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT O/B AREA OSS792.25 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657017Skin · crackedINSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. RIGHT WING NR 10 SLAT I/B AREA OSS 724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657016Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT I/B AREA OOS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657015Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 4 SLAT I/B AREA OSS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657006Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT I/B AREA OSS 724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201, REV 44. THIS REPAIR CLASSIFIED AS MAAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657005Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT O/B AREA OSS 641.5 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJAug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657004Hinge Fitting · crackedINSPECTION TYPE:C RIGHT WING I/B AILERON I/B SUPPORT HINGE FITTING UPPER & O/B FLANGE CRACKED AT FASTENER AREA. CRACK LENGTH 0.312 INCH. RIGHT WING I/B AILERON I/B SUPPORT HINGE FITTING UPPER AND O/B FLANGE CRACKED AREA REPAIRED AS PER HX RS R57-55-36392 REVAug 3, 2009 · N328UP · Boeing 76734AF · AileronsSDR IPXA09656991Attach Angle · crackedINSPECTION TYPE:C AFT OF BULK CARGO COMPT STA 1582 LBL 80 TO LBL 81 FLOOR SUPPORT BEAM ATT ANGLE CRACK. CRACK LENGTH 1.5 INCH. AFT OF BULK CARGO COMPT STA 1582 LBL 80 TO LBL 81 FLOOR SUPPORT BEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRAug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656989Panel · misrepairedINSPECTION TYPE:C RIGHT WING NR 7 SLAT CLOSURE PANEL I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 44.Aug 3, 2009 · N328UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656988Wedge · delaminatedINSPECTION TYPE:C RIGHT WING O/B FLAP TRAILING EDGE O/B LWR SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-06 PAR 5A (1) FIG 9 REV 44.Aug 3, 2009 · N328UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656987Attach Angle · crackedINSPECTION TYPE:C AFT OF BULK CARGO COMPT STA 1582 LBL 81 TO LBL 82 FLOOR SUPPORT BEAM ATT ANGLE CRACK. CRACK LENGTH 1.5 INCH. AFT OF BULK CARGO COMPT STA 1582 LBL 81 TO LBL 82 FLOOR SUPPORT BEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRAug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656983Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 654+22 TO 690, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656982Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 690 TO 731, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656981Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 1114 TO 1197+22 RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656980Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 833 TO 930, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656979Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 833 TO 930 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656978Floor Panel · gougedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SCRATCH AND GOUGE AT STA 1197+22 TO 1207 RBL 11 TO RBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED AS PER MM 53-01-01.Aug 3, 2009 · N328UP · Boeing 76734AF · Fuselage Floor Panel
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