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 IPXA09657655Skin · damagedLIGHTNING STRIKE DMG TO FASTENER AT STA 325 STR 24R. DMI D363083 LIGHTNING STRIKE AT STA 325 STR 24R DAMAGE FASTENER REPLACED AS PER SRM 53-00-01-2R8 FIG 201 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657654Skin · crackedRHW NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 RHW NR 10 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIR AS SRM 57-43-01-2R2 FIG 201 REV45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.25 INCH BY 9 INCH Oct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657653Skin · crackedRT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS724.24 RHW NR 10 SLAT AT OSS724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01 -2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.125 INOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657652Skin · crackedLT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS572.9. LHW NR 4 SLAT AT OSS572.9 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 SIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.5 I NCH BY 8.Oct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657651Skin · crackedLHW NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 LHW NR 3 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T-600631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCHOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657650Skin · crackedLHW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK JUST AT OSS724.24. LHW NR 3 SLAT AT OSS 724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-00631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCH TOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657649Skin · crackedLHW NR 2 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK AT OSS872, LHW NR 2 SLAT OSS872 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L 7075T6-00631N CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 6.875 INCH BY 9.125 INCH THIS REPAIR IS CLASOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657690Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT INBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 LBL 75 INCH CRACK LENGTH 1.75 INCH. BULK CARGO STA 1578 LBL 75 INCH FLOOR SUPPORT INBD ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657689Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT ATT INBD SPLICE ANGLE FOUND CRACK JUST AT STA 1578 RBL 75 INCH CRACK LENGTH 1.75 I NCH. BULK CARGO STA 1578 RBL 75" FLOOR SUPPORT I/B ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV.45Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657688Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 RBL 76 INCH CRACK LENGTH 1 INCH. CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE REPLACED AS PER 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657687Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 LBL 76 INCH CRACK LENGTH 0.75 INCH. BULK CARGO STA 1578 LBL 76 INCH FLOOR SUPPORT OTBD ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657646Floorbeam · crackedMEC COMPT STA246 FLOORBEAM CLIP AT RBL 25 FOUND CRACK. MEC COMPT STA 246 RBL 25 FLOORBEAM ATTACH CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657645Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 873 TO 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657644Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657643Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO 930 RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657642Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 985 TO 1090 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657641Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1114 TO 1197+22 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657640Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO 930 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657639Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 690 TO 730 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657638Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO 654+22 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657637Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO 654+22 LBL11 TO RBL11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657636Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657635Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 690 TO 764 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657634Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1425 TO 1540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657633Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA1344 TO 1480 LBL77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657632Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657631Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657630Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1197+22 TO 1207 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657629Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1207 TO 1344 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657628Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 283 TO 412 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657627Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657626Floorbeam · crackedMEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT RBL 10 INCHES. MEC COMPT STA 246 FLOORBEAM RBL 10 INCHES STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-2 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657617Floor Panel · damagedINSPECTION TYPE:N/A REF D407584 CENTER CARGO FLOOR POS 6 HAS FOUR HOLES MCD. FABRICATED 2 FLOOR PANELS PER B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657616Floorboard · dentedINSPECTION TYPE:N/A D407591: MCD POS 11L FLOOR HAS 2 DENTS. FABRICATED NEW FLOORBOARDS PER B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657615Floorboard · dentedINSPECTION TYPE:N/A REF D407590: TWO DENTS IN MAIN CARGO DECK FLOORBOARDS POS 4R TRANSFERRED FROM LOG PG 297108 ITEM 3. FABRICATED 2 NEW FLOOR PANELS PER EO B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657686Support · crackedINSPECTION TYPE:6C RT WING L/E LES 675 FIXED FAIRING SUPPORT WEB UPPER AFT MOUNT SPAR CLIP FOUND CRACK. RHW L/E LES 675 FIXED FAIRING SUPPORT WEB UPPER AFT FRONT SPAR CLIP REPLACE AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 6, 2009 · N325UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA09657679Rib · crackedRHW - L/E LES 252 FIXED FAIRING LWR SUPPORT RIB FW AREA FOUND CRACKED CRACK LENGTH 0.75 INCH. RHW L/E LES252 FIX FAIRING LWR SUPPORT RIB FWD AREA REPAIRED AS PER HX RS R57-00-36458 AND EO B767-5710-35230-A ORG MAT'L 7050-T7451 BARE ALUMINUM PLATE PER AMS4050 Oct 6, 2009 · N325UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA09657680Panel · delaminatedINSPECTION TYPE:C RT WING NR 7 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657668Skin · crackedNR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS 572.77 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS572.77 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MATERIAL CLAD 7075T6-0.063 IN ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUOct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657667Skin · crackedNR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS641.62 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS641.62 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43 -01-2R2 FIG 201 REV45. ORG MATERIAL CLAD 7075T6-0.063 IN ORG, CRACK LENGTH .125 INCH DAMAGED SKIN Oct 5, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657614Stiffener · crackedINSPECTION TYPE:C AFT CARGO STA 1087 RBL 25 STIFFENER FOUND CRACK, CRACK .375 INCH LENGTH. AFT CARGO STA 1087 RBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657613Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 50, CRACK .375 INCH LENGTH. MEC COMPT STA 246 FLOORBEAM AT LBL 50 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657612Stiffener · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 25 STIFFENER FOUND CRACK, CRACK .25 INCH LENGTH. AFT CARGO STA 1087 LBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657611Stiffener · crackedINSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM STIFFENER FOUND CRACK AT LBL 25, CRACK .5 INCH LENGTH. MEC COMPT STA 246 FLOORBEAM AT LBL 25 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 5, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657446Sliding Window · malfunctionedINSPECTION TYPE:N/A F/O SLIDING WINDOW WILL NOT LOCK. ADJ WINDOW PER 56-11-02-5. OPS CHECKS GOOD.Sep 24, 2009 · N307UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA09657448A/C Pack · odorINSPECTION TYPE:N/A IDENTIFIED MUSTY SMELL ON LEVEL OFF AT FL 330. TURNED OFF RIGHT PACK, SMELL DISAPPEARED. OPERATED RT PACK FOR ONE HOUR, COULD NOT SMELL ANYTHING BAD. OK FOR SERVICE.Sep 23, 2009 · N313UP · Boeing 76734AF · Cabin Cooling SystemSDR IPXA09657525Skin Panel · damagedINSPECTION TYPE:C SURVEY SEQ 312-F1-07 FX BETWEEN BS 1197+72 TO BS 1197+88 AND STR 19L - 21L EXISTING REPAIR FASTENER HOLES 3EA DRILLED & INSTALLED AT MACHINED RADIUS AREA. FX BETWEEN BS 1197+72 - 1197+88 & STR 19L-21L, ORG MAT'L 202473-0.200IN MACHINED SKIN Sep 22, 2009 · N312UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657513Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657512Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657511Slat · damagedINSPECTION TYPE:C RT WING NR 9 SLAT O/B EDGE FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 SHT 8 REV 45.Sep 22, 2009 · N312UP · Boeing 76734AF · Leading Edge Devices
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