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 IPXA1668640Shutoff Valve · dirtyINSPECTION TYPE: ETOP, LT ENGINE BLEED EICAS MSG AND SWITCH LIGHT ILLUMINATED. MANUALLY CYCLED PRSOV AND CLEANED C/P. ENG RAN BY CREW CHECK OK IAW AMM 36-11-00-5.Aug 15, 2011 · N337UP · Boeing 76734AF · Pneumatic Distribution SystemSDR IPXA1668634Floorboard · damagedFLOORBOARD DAMAGED FED OF MAIN CARGO DOOR. FABRICATED IAW EO B767-5320-9693-H.Aug 14, 2011 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668633Floorboard · damagedFLOORBOARD DAMAGED AFT OF MAIN CARGO DOOR LT SIDE. FABRICATED IAW EO.Aug 14, 2011 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668631Floorboard · crackedMCD POS 4R FLOORBOARD HAS A 5" CRACK. FABRICATED REPLACEMENT FLOORBOARD IAW EO B767-5320-9693-H. IDENTIFIED AS MAJOR REPAIR.Aug 13, 2011 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668630Floorboard · crackedMCD POS 4R FLOORBOARD HAS A 10" CRACK. FABRICATED REPLACEMENT FLOORBOARD IAW EO B767-5320-9693-H. IDENTIFIED AS A MAJOR REPAIR.Aug 13, 2011 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668525Indicator · failedON T/O AT 4000 FT CAPT EHSI BLANKING ON AND OFF THEN WENT BLANK. EADI CAPT DID THE SAME AT 6000 FT. THEN BOTH CAME BACK ON AT FLT 23000.CAPT EHSI WENT BLANK AND CB POPPED AND ELECTRICAL SMELL FOR LESS THAN 20 SEC. INSPECTED BOTH CONNECTOR AND REPLACED BOTH EAug 10, 2011 · N313UP · Boeing 76734AF · Attitude and Direction Data SystemSDR IPXA1668564Adi · failedAT FLT LEVEL 340, CAPTAINS ADI CRT CB POPPED. SCREEN WENT BLANK FOLLOWED BY AN ELECTRICAL BURNING ODOR. CHECKED EADI CONNECTOR FOR BURN, FOUND OK. REPLACED EADI LT SIDE IAW 34-22-03-4, OPS CHECK COMPLETE.Aug 9, 2011 · N306UP · Boeing 76734AF · Attitude Gyro and Indicating SystemSDR IPXA1668502Panel · delaminatedINSPECTION TYPE:C, RT WING OTBD FLAP UPPER SURFACE AFT INBD PNL OTBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 50.Aug 3, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668533Wedge · delaminatedINSPECTION TYPE:8C, RT WING OTBD T/E FLAP T/E WEDGE OTBD AREA UPPER SURFACE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG9, REV 50.Aug 2, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668497Tee Fitting · corrodedINSPECTION TYPE:C, FUSELAGE RT BS 955 'T' FTG FWD LOWER HOLE FOUND FRETTING AT MATTING SURFACE AREA. FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA 'T' FITTING. REPLACED AND REINSTALLED IAW EO B767-5350-17922-I APP D, FIG 6 ORG MAT'L IS 7075-T73 DIE FORGAug 2, 2011 · N311UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1668493Tee Fitting · corrodedINSPECTION TYPE:C, FUSELAGE LT BS 955 TEE FITTING FWD LOWER HOLE FOUND FRETTING AT MATING SURFACE AREA. FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA TEE FITTING. REPLACED AND INSTALLED IAW EO B767-5350-17922-I APP 'C' FIG 6, ORG MAT'L IS 7075-T73 DIE FORGING,Aug 2, 2011 · N311UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA11668666Floorbeam · corrodedINSPECTION TYPE:C, STA 1518, RBL 79 TO RBL 81 FLOORBEAM FOUND CORROSION. STA 1518, RBL 79 TO RBL 81 FLOORBEAM UPPER FLANGE REPAIRED IAW HX RS NR R53-65-37194, REV A AND EO NR B767-5310-43754-A, BLENDED OUT AREA AT FWD FLANGE LOWER SURFACE IS DEPTH 0.030" X WAug 1, 2011 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA1668535Floorbeam · corrodedINSPECTION TYPE:8C M/D, STA 1518 RBL 79 TO RBL 81 FLOORBEAM FOUND CORROSION. M/D STA 1518, RBL 79 TO RBL 81, FLOORBEAM UPPER FLANGE REPAIRED IAW HX RS NR R53-65-37194, REV A AND EO NR B767-5310-43754-A, BLENDED OUT AREA AT FWD FLANGE LOWER SURFACE IS DEPTH 0.Aug 1, 2011 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA1668534Floorbeam · crackedINSPECTION TYPE:8C, M/DECK STA 998, RBL 10 FLOOR SUPPORT LOWER FACE FOUND CRACKED. M/DECK STA 998, LBL10 TO RBL10 AREA FLOOR SUPPORT REPLACED AND INSTALLED IAW HX RS NR R-53-50-37193 REV A AND EO NR B767-5310-43780-A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAug 1, 2011 · N311UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA1668503Skin · dentedINSPECTION TYPE:C, RT WING NR 8 SLAT UPPER SURFACE FOUND DENTS. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 50.Aug 1, 2011 · N311UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA1668501Panel · delaminatedINSPECTION TYPE:C, RT WING OTBD FLAP INBD AFT UPPER PANEL FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 50.Aug 1, 2011 · N311UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA11668384Control Module · inoperativeCREW EXPERIENCED AUTOPILOT WARNING AND INABILITY TO OPERATE THE STABILIZER TRIM MANUALLY - AIR TURN BACK. TROUBLESHOOTING CARRIED OUT THROUGH AMM & FIM INDICATING STAB TRIM CONTROL MODULE FAILURE. BOTH STCM'S HAVE NOW BEEN REPLACED AND IN PROGRESS OF REPLACIJul 31, 2011 · N316UP · Boeing 76734AF · Flight Control SystemSDR IPXA1668318Indicator · inoperativeATB NR 2 CAPT EADI AND EHSI WENT BLANK WITH FAINT SMELL OF SMOKE. R & R CAPT EHSI CAPT EHSI, PN 622-7999-003, SN 4277.Jul 31, 2011 · N309UP · Boeing 76734AF · Flight Environment DataSDR IPXA1668317Eadi · inoperativeATB - CAPT EADI WENT BLANK WITH FAINT SMELL OF SMOKE. R & R CAPT EADI.Jul 31, 2011 · N309UP · Boeing 76734AF · Flight Environment DataSDR IPXA1668311Floor Panel · damagedMAIN CARGO FLOOR PANEL POS 5R HAS A HOLE. FABRICATED IAW B767-5320-9693-H.Jul 31, 2011 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA1668310Floor Panel · damagedMAIN CARGO DECK POS 4L 1/2 HOLE IN FLOOR PANEL, FABRICATED IAW EO 767-5320-9696-H.Jul 31, 2011 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668309Floor Panel · dentedFLOOR PANEL AT POS 4 LT OTBD DENTED. NEW FLOOR PANEL REF EO B767-5320-9693B.Jul 31, 2011 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668496Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FASTENER HOLE FOUND CRACK AT FAIL SAFE STRAP GREATER THAN 0.060" IN LENGTH. FUSELAGE RTS BS 955, REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-I APP D, ORG MAT'Jul 30, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1668492Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA FASTENER HOLE FOUND CRACK AT FAIL SAFE STRAP APP. 0.030" IN LENGTH. FUSELAGE LT SIDE BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP. REPAIRED IAW EO B767-5350-17922-I APP. 'C' ORG MAT'LJul 30, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1668302Controller · malfunctionedINSPECTION TYPE:ETOP, AUTO CABIN PRESS CONT SYS NR 2 (1 SYS INOP) REF TO WAN NR 1785042 AND DMI 458926. REF TO FIM 21-31-00 PERFORMED CABIN PRESS CONTROLLER BITE ON SYS NR2 FOUND SYS IS OK ALSO OPS CK OF OUTFLOW VALVE IAW AMM 21-31-00-5 SATIS NI O MORE MSG ATJul 30, 2011 · N322UP · Boeing 76734AF · Cabin Pressure ControllerSDR IPXA1668532Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 9 DENTS AND 7 PUNCTURES AT STA 654+22 TO STA 690 LBL11 TO RBL11. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668531Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 10 DENTS AND 6 PUNCTURES AT STA 1351 TO 1480, LBL 77 TO LBL 88. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668530Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 8 DENTS AND 9 PUNCTURES AT STA 654+22 TO STA 690, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668529Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 8 DENTS AND 6 PUNCTURES AT STA540 TO STA 654+22, RBL 33 TO RBL 55. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668528Floor Panel · dentedINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND 8 DENTS AND 7 PUNCTURES AT STA 1197+22 TO STA 1207 LBL11 TO RBL11. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM53-01-01.Jul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668505Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jul 29, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668504Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 50.Jul 29, 2011 · N311UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668495Failsafe · damagedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING, FAIL SAFE STRAP AREA, SUSPECT CRACK FOUND, REMOVED FASTENER FOR CRACK CONFIRMATION FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT REMOVED AND REIJul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1668491Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP AREA , SUSPECT CRACK FOUND, REMOVE FASTENER FOR CRACK CONFIRMATION. FUSELAGE LT BS 955, REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT. REMOVED AND REINSTALJul 29, 2011 · N311UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668270Hydraulic System · low pressureCENTER HYD SYS LOW PRESSURE LIGHT WITH ASSOSICATED ECIAS MSG. DEMAND PUMP IN AUTO AND LOW PRESSURE LIGHT ILLUMINATED, BOTH OCCURED WHEN SELECTING FLAPS TO 1. EMEREGENCY DECLARED AND LANDED WITHOUT INCIDENT. ACFT OUT OF SERVICE.Jul 29, 2011 · N308UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA1668295Controller · failedINSPECTION TYPE:ETOP, NR1 CABIN PERSSURE CONTROLLER STICKS IN VERIFY MODE CAUSING NR1 MOTOR TO FIGHT NR 2 MOTOR DURING TEST. R & R NR1 CABIN PRESSURE CONTROLLER IAW MM 21-31-02-4. OPS CHECKED GOO D IAW AMM 21-31-00-5.Jul 28, 2011 · N335UP · Boeing 76734AF · Cabin Pressure ControllerSDR IPXA1668280Flow Sensor · inoperativeINSPECTION TYPE:ETOP, DURING ETOPS PDC CK, FOUND APU INOP DEFERRED IAW MEL 49-11-1-0-2 AND ETOPS DOWNGRADED. R & R APU SURGE BLEED VALVE. NO HELP. R&R APU FLOW SENSOR MODULE. OPS CHECKED GOOD.Jul 28, 2011 · N316UP · Boeing 76734AF · APU Engine Fuel and ControlSDR IPXA11668279Indicator · inoperativeEHSI WENT BLANK SOON AFTER TAKEOFF. REPLACED CAPTAIN'S EHSI AND OPS TEST COND. NORMAL IAW AMM 34-22-04-4.Jul 27, 2011 · N307UP · Boeing 76734AF · Turn and Bank/Rate of Turn IndicatorSDR IPXA11668135Floor Panel · damagedFLOOR PANEL POS NR 3-4R HAS DAMAGED ON UPPER SKIN. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jul 23, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1668100Wedge · crackedINSPECTION TYPE:C 1 LT WING NR 4 SLAT T/E WEDGE ASSY LOWER SKIN BROKEN AT OSS 564. CRACK DIMENSION ABOUT 0.4" X 0.3" CUT THE LOWER SKIN 0.5" X 0.375" X 1", AND UPPER SKIN ABOUT 5.375" X 2". REPAIR IAW REV: 49 SRM 57-43-02 REPAIR 1, FIGURE 201 AND SRM 51-70-10 Jul 19, 2011 · N336UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA1667945Floor Panel · damagedPOS 6R HAS FLOOR PANEL DAMAGED. REPAIRED REF EO B767-5320-9693-H.Jul 17, 2011 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667944Floor Panel · damagedFLOOR PANEL DAMAGED AT POS 2R OTBD PANEL, REF LOG PAGE 712639-1. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jul 17, 2011 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11668219Failsafe · misinstalledINSPECTION TYPE:C, REMOVE FASTENERS / PARTS IDENTIFIED IN EO B767-5350-17922-I APPENDIX 'D', FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAIL SAFE STRAP. FASTENERS/ PARTS REMOVED AND REINSTALLED IAW EO NR B767-5350-17922-I APPENDIJul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668218Failsafe · misinstalledINSPECTION TYPE:C, REMOVE FASTENERS/ PARTS IDENTIFIED IN EO B767-5350-17922-I APP 'C' FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAIL SAFE STRAP. FASTENER / PARTS REMOVED AND REINSTALLED EO NR B767-5350-17922-I APP. 'C' FIG 6 AT Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668217Tee Fitting · corrodedINSPECTION TYPE:C, FUSELAGE RT BS 955 T-FITTING FRETTING FOUND JUST AT INTERNAL SURFACE AROUND THE MOST LOWER FASTENER HOLE. FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA 'T-FITTING REPLACED AND REINSTALL IAW EO NR B767-5350-17922-I APP 'D' FIG 6 ORG MATJul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11668181Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1518, LBL 80 FLOORBEAM FOUND CORROSION. REPAIRED IAW RS R-53-65-37175 REV A & EO B767-5310-43604-A ORIG MAT IS BAC1506-4177-0775T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.0150, CORROSION BLENDED AREA IS 0.063" DEPTH, 1" Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA11668179Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1540 LBL 75 FLOORBEAM FOUND CORROSION. REPAIRED IAW HX RS R-53-65-37170 REV A & EO B767-5310-43603-A. ORIG MAT IS BAC1506-4177-7075T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.150, CORROSION BLENDED AREA IS 0.050" DEPTH, 1Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA11668122Skin · dentedINSPECTION TYPE:C, LT WING INBD AFT FLAP LWR SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4 FIG 202, SHEET 1, REV 50.Jul 13, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668007Floor Support · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR, BS 1583-1597, LBL 54, CLIP FOUND CORROSION. M/D BELOW FLOOR AT BS 1583-1597, LBL 54 CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 & SRM 51-40-02, REV 50. ORG MAT'L THICKNESS 0.090" BLEND OUT DEPTH 0.065" WIDTH 0.5" LENGTH 0Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA11668216Tee Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD, CRACK FOUND AT T-FITTING 7 O'CLOCK POSITION APPROX .0625". FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA 'T' FITTING REPLACED AND REINSTALL IAW EO NR B767-5350-17922-I APP 'C' FIG 6 ORIGIANAL MATERIAL IS Jul 11, 2011 · N307UP · Boeing 76734AF · Fuselage Main, Bulkhead
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