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 IPXA11669862Floor Panel · damagedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 2 DAMAGED AND 8 DENTS AT STA 1540 TO STA 1598 LBL 55 TO LBL 80. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.Oct 11, 2011 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11669861Floorbeam · corrodedINSPECTION TYPE: C, MAIN DECK BS 1540 RBL 71.25" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. FLOORBEAM REPAIRED IAW RS R53-65-37244, REV A & EO B767-5310-44764-A, ORG MATERIAL IS BAC1506-4177-7075T6511 EXTRUSION, ORG THICKNESS 0.150" CORROSION BLEND OUT Oct 11, 2011 · N314UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA11669821Wedge · delaminatedINSPECTION TYPE: 8C, LT WING OTBD T/E FLAP, T/E WEDGE MID AREA LWR SURFACE DELAMINATION. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR5 A (1), FIG 9, REV 50.Oct 11, 2011 · N314UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11669991Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE BS 955 LT REAR SPAR BULKHEAD FITTING AREA WAS FOUND 1 EA FASTENER HOLE CRACKED ON 6 O/C POSITION AT TEE FITTING APPROX .1250" IN LENGTH. TEE FITTING REPLACED IAW EO NR B767-5350-17922-J APPENDIX 'C', FIG 6, CRACK APPROX .1250" IN Oct 10, 2011 · N314UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11669989Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING WAS FOUND 1EA FASTENER HOLE CRACKED AT FAILSAFE STRAP ON 2 O/C AND 4 O/C POSITION THROUGH THICKNESS AND .1250" IN LENGTH. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'C', REPAIR IS CLASSIOct 10, 2011 · N314UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11669992Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'D'. REPAIR IS CLASSIFIED AS A MAJOR.Oct 9, 2011 · N314UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1669634Floor Panel · damagedREF D460011 MAIN CARGO DECK FLOOR PANEL POS 11R OTBD DAMAGED. IDENTIFIED FLOOR PANEL FROM 11R OTBD AS PN146T5869-50 IAW EO B767-5320-9693- FAB A REPLACEMENT FLOOR PANEL BY CUTTING OUT NEW FLOOR PANEL FROM A402H AND MARKED INSERT LOCATION USING EXISTING FLOOROct 9, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669633Floor Panel · damagedMCD FLOOR PANEL POS 14R OTBD PANEL 2EA HOLES IDENTIFIED PANEL FROM POS 14R OTBD AS PN 146T5869-88 IAW EO B767-5320-969 3 FAB A REPLACEMENT PANEL BY CUTTING OUT NEW PANEL FROM A402H AND MARKED INSERT LOCATION USING EXISTING PANEL AS TEMPLATE DRILLED AND CLEANEDOct 9, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11669990Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. R & R IAW EO B767-5350-17922-J APPENDIX 'D' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.Oct 8, 2011 · N314UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11669988Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA, CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. REMOVED AND REINSTALLED IAW EO NR B767-5350-17922-J APPENDIX 'C' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.Oct 8, 2011 · N314UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11669615Floor Panel · damagedPOS 7R HAS A DAMAGED MAIN DECK FLOOR PANEL ON 3RD PANEL FROM RT, 2" FROM AFT EDGE AND 9" FROM OTBD EDGE HOLE MEASURE .5 INCHES IN DIAMETER. INSTALLED TEMPORARY REPAIR REF EO B767-5320-27374-B. REPAIR BY NEXT C-CHECK. REINSPECT 81 DAYS 650 FLIGHT HOURS, 305 Oct 2, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669600Floor Panel · damagedPOSITION 7R DAMAGED MAIN DECK FLOOR PANEL. DAMAGE IS LOCATED ON 2ND FLOOR PANEL INBD FROM RT. 38 INCHES FROM AFT EDGE. DAMAGE IS 3" BY 1". MAJOR REPAIR. REMOVED FLOOR PANEL. INSTALLED FLOOR PANEL IAW MM 53-01-26-4 THRU PAR 4(8). INSTALLED TAPE TO PANEL IOct 2, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669599Floor Panel · damagedPOSITION 6C HAS A DAMAGED MAIN DECK FLOOR PANEL. DAMAGE LOCATED ON CENTER PANEL, 41 INCHES FROM FWD EDGE DAMAGE TO PANEL, 3 HOLES .5 INCHES IN DIAMETER. MAJOR REPAIR. REMOVED PANEL AND TRANSFERRED TO NRC 502193. INSTALLED TAPE AND COMPLETED INSTALLATION OOct 2, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669548Floor Panel · damagedHOLE IN FLOOR PANEL AT POS 4 ON MCD. REPAIRED FLOOR PANEL IAW SRM 53-00-50.Oct 2, 2011 · N343UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669546Floor Panel · damagedFLOOR PANEL DAMAGED AFT EDGE CTR OF THE PANEL. FABRICATED FLOOR PANEL IAW EOB767-5320-9693-H AND REPLACED.Oct 1, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669545Floor Panel · damagedFLOOR PANEL DAMAGED. FABLICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.Oct 1, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669540Floor Panel · puncturedMCD FLOOR PANEL DAMAGED AT STA 377.5, RBL 48, DAMAGE IS 1" X .500". REPAIRED IAW SRM 53-00-50-2R.Oct 1, 2011 · N322UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669521Escape Reel · damagedFOUND EMERGENCY ESCAPE INERTIAL DESCENT REEL WITH CABLE EXTENDED TOO FAR. R & R WITH SERVICEABLE UNIT PER AMM 25-61-03-2.Sep 29, 2011 · N334UP · Boeing 76734AF · Emergency EquipmentSDR IPXA1669582Skin · dented7C CHECK, RT WING OTBD FLAP, OTBD AFT LWR PANEL AT OTBD AREA FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED IAW SRM51-70-10-2R, REPAIR 4, FIG 202, SHEET.3, REV.50.Sep 26, 2011 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669581Rib · crackedC CHECK, RT WING NR 9 SLAT AT UP STOP FITTING INBD FLANGE FOUND CRACKED. RT WING- NR9 SLAT UP STOP SUPPORT RIB INBD FLANGE REPAIRED IAW HX RS R-57-41-37231 REV A & EO B767-5750-44540-A, ORG MAT'L 7075-T7351 PLATE, CRACK LENGTH 0.375" FINAL CUTOUT SIZE IS 0Sep 26, 2011 · N325UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA11669438Control Panel · inoperativeEMERGENCY LIGHTS DO NOT COME ON WHEN SWITCH PLACED TO ON POSITION. TROUBLESHOT IAW FIM 33-51-00, FIG 103, SHEET 1. SWITCH BAD E031979. R & R EMERGENCY LIGHTS CONTROL PANEL IAW MM 33-51-08. OPS CHECK GOOD.Sep 24, 2011 · N305UP · Boeing 76734AF · Emergency LightingSDR IPXA1669503Hinge Fitting · crackedINSPECTION TYPE: C, RT WING - INBD MAIN FLAP, INBD AFT FLAP HINGE ARM FOUND CRACKED RT WING - INBD MAIN FLAP HINGE ARM FITTING REPAIR IAW SRM 57-53-02-2R1, REPAIR 1, FIG 201, REV 50, ORG MAT'L 7075-T73 FORGING CRACK LENGTH AT INBD FLANGE IS 0.375" AND OTBD FLSep 23, 2011 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669556Floor Panel · gougedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DEEP GOUGES AND 10 DENTS AT STA 412 TO STA 540, LBL 11 TO LBL 33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Sep 22, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669555Floor Panel · puncturedINSPECTION TYPE:7C, FLOOR PANEL FOUND 8 PUNCTURES AND 15 DENTS AT STA 654+22 TO STA 690, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Sep 22, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11669213Fairing · delaminatedINSPECTION TYPE:8C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG5, REV50, 121 DEGREE/CURE.Sep 6, 2011 · N312UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11669212Fairing · delaminatedINSPECTION TYPE:8C, RT WING INBD MAIN FLAP OTBD L/E FAIRING. FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG5, REV50, 121 DEGREE/CURE.Sep 6, 2011 · N312UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669080Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPS CHECKED OK.Sep 6, 2011 · N319UP · Boeing 76734AF · Emergency LightingSDR IPXA1669070Floor Panel · damagedFLOOR PANEL MAIN DECK DAMAGED PANEL LOCATED APPROX STA 1210 TO 1270. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Sep 5, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669069Floor Panel · damagedFLOOR PANEL MAIN DECK DAMAGED LOCATED APPROX STA 680 TO 764. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.Sep 5, 2011 · N319UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669048Floor Panel · damagedFLOOR PANEL POS2 CTR HAS .5 INCH HOLE. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.Sep 4, 2011 · N349UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669044Floorboard · damagedINSPECTION TYPE:MX POS 4 FLOORBOARD MCD CENTER INTERIM REPAIR 2 INCH HOLES 16 INCHES AFT OF CENTERLINE IDENTIFIED PANEL FROM POSITION 4. PN 143T5876-98 IAW EO B767-5320-969 APPENDIX H. FABRICATED A REPLACEMENT PANEL BY CUTTING OUT A NEW PANEL FROM A402H ASep 4, 2011 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11669257Tee Fitting · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT TEE FITTING ON 9 O/C POSITION APPROX .1250" IN LENGTH. TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-I, APPENDIX 'D', FIG 6, ORG MAT'L IS 707Sep 3, 2011 · N312UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA11669256Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL SAFE STRAP ON 4 & 10 O/C POSITION THROUGH THICKNESS. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-ISep 3, 2011 · N312UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11669253Tee Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT 'T' FTG ON 3 O/C POSITION APPROX .1250" IN LENGTH FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG AREA 'T' FITTING REPLACED AND INSTALLED IAW EO NR B767Sep 3, 2011 · N312UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA11669252Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL STRAP ON 2 O/C POSITION THROUGH THICKNESS FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPLACED IAW EO NR B767-5350-17922-I, APPSep 3, 2011 · N312UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11669255Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FTG FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER REMOVED AND REINSTALLED IAWSep 2, 2011 · N312UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11669251Failsafe · crackedINSPECTION TYPE: C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER. R & R IAW EO NR B767-5Sep 2, 2011 · N312UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA20110901001ABattery Pack · failedINSPECTION TYPE:8C COCKPIT: EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAILED. COCKPIT EMERGENCY LIGHT BATTERY PACK REPLACED AND LIGHT OPS CHECKED NORMAL, REF AMM 33-51-07.Sep 1, 2011 · N312UP · Boeing 76734AF · Emergency LightingSDR IPXA11669249Floor Panel · damagedINSPECTION TYPE:8C, FLOOR PANEL FOUND 10 PUNCTURES AND 6 DENTS MARKS AT STA 764 TO 873, LBL 77 TO 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED AMM 53-01-01.Sep 1, 2011 · N312UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668985Spring · damagedEICAS MESSAGE EMERGENCY LIGHTS DISPLAYED & UNARMED LIGHT ILLUMINATED WITH EMERGENCY LIGHTS SWITCH ARMED. EMERGENCY LIGHT SWITCH GUARD SPRING CORRECTED AND EMERGENCY LIGHT CHECKED IAW AMM 33-51-00-5.Sep 1, 2011 · N345UP · Boeing 76734AF · Emergency LightingSDR IPXA1669015Sliding Window · inoperativeCAPT'S SLIDING WINDOW (L2) DOES NOT CLOSE PROPERLY. ADJUSTED WINDOW ER MM 56-11-02-5.Aug 31, 2011 · N329UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA11668944Wedge · delaminatedINSPECTION TYPE:C, LT WING NR 6 SLAT T/E WEDGE UPPER SURFACE REPAIR PATCH DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8, REV 50.Aug 22, 2011 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11668879Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Aug 22, 2011 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668797Floorboard · damagedPOS 5 RT FLOORBOARD DAMAGED REF DI 456109. FABRICATED NEW FLOORBOARD REF EO B767-5320-9693-H.Aug 21, 2011 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668790Floor Panel · damagedMAIN CARGO FLOOR PANEL DAMAGED, FABRICATED FLOOR PANEL BY CUTTING OUT A NEW PANEL FROM A402H AND MARKING INSERT LOCATION USING EXISTING PANEL AS A TIMPLATE, DRILLED AND CLEANED HOLES OF DEBRIS INSTALLED INSERTS IAW BMS5-107 AND CURED IAW MFG MARKED UNDERSIDEAug 20, 2011 · N332UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668788Floor Panel · damagedMAIN DECK FLOOR PANEL PN 146T5869-19 HAS INTERM REPAIR TO 1IN X 3IN HOLE PANEL LOCATED AT POS 10/11 LT MOST OTBD FLOOR PANEL. IDENTIFIED FLOOR PANEL FROM POS 10/11 LT PN146T5869-19 IAW EOB767-5320-9693. FABRICATED A REPLACMENT FLOOR PANEL BY CUTTING OUT A NEAug 20, 2011 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11668876Floor Panel · dentedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 6 DENTS AND 9 PUNCTURES AT STA 654+22 TO STA 690 LBL 55 TO LBL 77. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Aug 19, 2011 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11668877Floor Panel · dentedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 8 DENTS AND 5 PUNCTURES AT STA 654+22 TO STA 690 LBL 11 TO RBL 11. MCD FLOOR PANEL FABIRCATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Aug 18, 2011 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11668875Stiffener · crackedINSPECTION TYPE:C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94 STIFFENER REPAIRED IAW SRM 57-10-10-2R2, REPAIR 2, FIG 201, REV 50 AT STA 785.9 RBL 10.94 ORG MATERIAL BAC1518-912-2024T3511 CRACK LENGTH 1.2" CUAug 18, 2011 · N324UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA11668874Stiffener · crackedINSPECTION TYPE:C WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 LBL 10.94 WNG CTR TANK FRONT SPAR VERT STIFFENER REPAIRED PER SRM 57-10-10-2R2 REPAIR 2 FIG 201 REV 50 JUST AT STA 785.9 LBL 10.94 ORG MAT'L BAC1518-91Aug 18, 2011 · N324UP · Boeing 76734AF · Wing Miscellaneous Structure
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