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 IPXA2672604Stiffener · crackedINSPECTION TYPE: C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9, RBL 10.94. REPAIRED IAW SRM 57-10-10-2R2, REPAIR 2, FIG 201, REV 52 AT STA 785.9, RBL 10.94, ORG MATL IS BAC1518-912-2024T3511, CRACK LENGTH IS 2.5", CUMar 18, 2012 · N317UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2672410Floor Panel · damagedFLOOR PANEL 4/5 HAS A 1" HOLE. REPAIRED IAW SRM 53-00-50 2R.Mar 18, 2012 · N336UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672455Wedge · chafedINSPECTION TYPE:C, LT WING INBD T/E AFT FLAP CHAFED ON UPPER SKIN AT IFS 105.750. APPROX LT X W=1" X 1.25" ON UPPER SKIN CUT OUT THE CHAFED SIZE L X W=1" X 1.25". PERFORM THE REPAIR IAW REV: 52, SRM 57-53-01, REPAIR 1, FIG 201, SHEET 4 OF 6 AND 51-70-10 REPAMar 17, 2012 · N340UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2672453Wedge · chafedINSPECTION TYPE:C, RT WING INBD T/E AFT FLAP CHAFED ON UPPER SKIN AT IFS 105.750 APPROX L X W=1.1" X 1.24" ON UPPER SKIN CUT OUT THE CHAFED SIZE L X W=1.1" X 1.24". PERFORM THE REPAIR IAW REV:52, SRM 57-53-01. REPAIR 1, FIG 201 SHEET 4 OF 6 AND 51-70-10, REPMar 17, 2012 · N340UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2672408Wire · chafedON TAKE OFF, THE RT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CHECKED AND REPLACED THE RT ENGINE OIL FILTER, IT WAS CLEAN. FOUND CHAFED WIRE FOR FILTER PRESSURE SWITCH. REPAIRED WIRE.Mar 17, 2012 · N301UP · Boeing 76734AF · Engine Oil System WiringSDR IPXA2672256Floor Panel · brokenINSPECTION TYPE: C, MAIN DECK FLOOR PANEL NR 241AFF BROKEN AT BS 761, RBL 1. L X W=1"X1" ON UPPER SKIN AND CORE;L X W=1.2"X1" ON LOWER SKIN CUT OUT THE DAMAGE AREA WITH L X W=1.25"X1.25". REPAIR IAW REV:52, SRM 53-00-50 REPAIR GENERAL, FIG 201 PARA 4 E.Mar 12, 2012 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672221Floor Panel · damagedFLOOR PANEL POS 6R HAS HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Mar 11, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672220Floor Panel · damagedTWO HOLES IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Mar 11, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672219Floor Panel · damagedFLOOR PANEL HAS TWO HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Mar 11, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672218Floor Panel · damagedTWO HOLES FLOOR PANEL. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H.Mar 10, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672213Floor Panel · damagedHOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW B767-5320-9693-H.Mar 10, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672212Floor Panel · damagedDAMAGE IN FLOOR PANEL 145T5876-73 FWD CTR PANEL 6" LEFT OF CTR, FABRICATED PANEL REF EO B767-5020-9693-H.Mar 10, 2012 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672211Eadi · shortedAIR TURNBACK, SMOKE IN COCKPIT ON ARRIVAL AFTER CREW DEBRIEFING, FOUND EADI BLANK WITH ASSOCIATED CIRCUIT BREAKER POPPED. PERFORMED WIRING CHECKED FROM EADI TO SYMBOL GENERATOR, & FROM EADI TO EFIS CONTROL PANEL AND FROM EADI TO EHSI, NOT ABNORMAL, NOTED REF Mar 10, 2012 · N331UP · Boeing 76734AF · Attitude and Direction Data SystemSDR IPXA2672231Wedge · damagedINSPECTION TYPE: C, LEFT WING OTBD T/E FLAP HAS PUNCTURE (2"X1")ON L/E. LOCATED 2' OTBD OF INBD EDGE ON THE L/E. REMOVE THE EXISTING INTERIM REPAIR FOR SIZE L X W=5.1"X2.5". PERFORM THE REPAIR IAW REV:52,767-300F, SRM 57-53-01, REPAIR 1, TABLE I AND SRM 51-Mar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2672230Skin · dentedINSPECTION TYPE: C, DENTED SKIN, LT WING OTBD FLAP LOWER SKIN DENTS AT OTEF STA 250 AND OTEF STA 263.5. DENT WITH DELAMINATION DIMENSION L X W X D=2.2"X2.1"X0.020" AT OTEF STA 250 AND THE OTHER DENT WITH DELAMINATION DIMENSION L X W X D=2.0"X1.54"X0.020" AT OMar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2672252Wedge · chafedINSPECTION TYPE: 9C, LEFT WING NR 5 SLAT WEDGE LOWER SURFACE FOUND CHAFING. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8, REV 52.Mar 6, 2012 · N303UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2672227Floor Panel · dentedINSPECTION TYPE: 9C FLOOR PANEL FOUND WITH TWO PUNCTURES AND NINE DENTS AT BS 732 TO 825, LBL 55 TO 77. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.Mar 6, 2012 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12672177Fairing · delaminatedINSPECTION TYPE: 9C, RIGHT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1), FIG 5, REV 52.Mar 6, 2012 · N303UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA12672035Floor Panel · delaminatedMAIN CARGO DECK FLOOR PANEL DAMAGED POS 3R CENTER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Mar 5, 2012 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672028Floor Panel · puncturedMAIN CARGO DOOR FLOOR PANEL 4R HAS A PUNCTURE, DELAM, PN 143T5876-85. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Mar 5, 2012 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672017Floor Panel · damagedMAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320--9693-H.Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672016Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693 H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 &Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672015Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL HAS A .5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693H, FABRICATED A REPL PANEL FROM A402H ACCOMPLISHED PARA B STEP 5&6 REF EOMar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672229Stiffener · crackedINSPECTION TYPE: 9C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 LBL 10.94. REPAIRED IAW 57-10-10-2R2, REPAIR 2, FIG 201, REV 52, JUST AT STA 785.9, LBL 10.94, ORIG MATL: BAC1518-912-2024T3511, CRACK LENGTH: 3", CUTOFMar 3, 2012 · N303UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA2672228Stiffener · crackedINSPECTION TYPE:9C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94. REPAIRED IAW SRM 57-10-10-2R2, REPAIR2, FIG 201, REV 52 JUST AT STA 785.9 RBL10.94, ORIG MATL: BAC1518-912-2024T3511, CRACK LENGTH: 2.5",CUTOFMar 3, 2012 · N303UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA2672365Skin · damagedINSPECTION TYPE:9C, LEFT WING NR 5 SLAT T/E WEDGE SKIN REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 52.Mar 2, 2012 · N303UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2672012Skin · gougedINSPECTION TYPE: C, MAIN DECK CARGO EXTERNAL SKIN, 2 GOUGES BETWEEN STA 632 AND 636, WL 220,GOUGE NR 1,L X W X D=0.5" X 0.3" X 0.001", GOUGE NR 2 L X W X D= 0.3" X 0.3" X 0.012". REPAIR IAW EO NO B767-5330-46220-A.Feb 28, 2012 · N338UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2671984Skin · gougedINSPECTION TYPE:C, MAIN DECK CARGO EXTERNAL SKIN 2 GOUGES BETWEEN STA 632, WL 220,GOUGE NR1 L X W X D=0.5"X 0.3" X 0.001", GOUGE NR 2 L X W X D=0.3"X 0.3 X 0.012". REPAIR IAW EO NR B767-5330-46220-A.Feb 28, 2012 · N338UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2671896Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 9L DAMAGED. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671895Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED POS 6L. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671894Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED POS 5R. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671893Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED POS 10L. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671892Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED, POS 14 CTR, REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671891Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED POS 12 RT. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671890Floor Panel · damagedMAIN CARGO DECK FLOOR DAMAGED, POS 2L. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671889Floor Panel · damagedMAIN CARGO DECK FLOOR DAMAGE, POS 1 RT. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671888Floor Panel · damagedMAIN CARGO DECK FLOOR DAMAGED POS 1 LT. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671887Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED, POS 1. REPAIRED IAW SRM 53-00-50.Feb 26, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671876Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED BS 834-930, LBL 5- 8. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Feb 25, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2671908Slat System · malfunctionedL/E SLAT DISAGREE ILLUMINATED AFTER T/O IN 1500 ON RETRACTION. RAN CHECKLIST AND DIVERTED. LANDED REF 30 & 30/ FLAPS 20 AT 174 KTS, HOT BRAKES AFTER LANDING AND ONE RT TIRE. HAD TO USE ALTERNATE SYS TO RETRACT L/E OTBD FLAPS. VISUALLY INSP OTBD FLAP DRIVE SFeb 24, 2012 · N309UP · Boeing 76734AF · Leading Edge Slat Control SystemSDR IPXA12671782Floor Panel · damagedMAIN DECK FLOOR PANEL 8/9M LT DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Feb 20, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12671781Floor Panel · damagedMAIN DECK FLOOR PANEL 9L DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Feb 20, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12671780Floor Panel · damagedMAIN DECK FLOOR PANEL 10/11 LT DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Feb 20, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12671779Floor Panel · gougedMAIN CARGO DECK FLOOR PANEL 4L GOUGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Feb 20, 2012 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA12671783Buss · inoperativeINSPECTION TYPE: E TOP, DURING APPROACH WITH FLAPS & GEAR UP, AUOPILOT AUTO THROTTLE ENGAGED, PASSING THRU HEAVY RAIN, MULTIPLE SIMULTANEOUS EICAS MESSAGES OCCURED INCLUDING STBY PWR, L/E FLAP DISAGREE, EQUIP COOLING, APU BOTTLE, AIR GRND SYS, AUTO BRAKE, AUTOFeb 16, 2012 · N347UP · Boeing 76734AF · Electrical Power System WiringSDR IPXA12671851Web · chafedINSPECTION TYPE:C, WEB CHAFED AT RT WING INBD AILERON OTBD SIDE AT WS 533, REPAIRED IAW EO NR B767-5750-46114-A.Feb 13, 2012 · N313UP · Boeing 76734AF · AileronsSDR IPXA12671843Skin · chafedINSPECTION TYPE: C, WEB CHAFED AT RT WING INBD AILERON OTBD SIDE AT WS 533, REPAIRED IAW EO B767-5750-46114-A.Feb 13, 2012 · N313UP · Boeing 76734AF · AileronsSDR IPXA12671835Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROED AT BS 1540, RBL 76. CORROSION: 1.7 INCH (LENGTH) X 0.6 INCH (WIDTH). REPAIRED IAW EO B767-5310-46116-A.Feb 13, 2012 · N313UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA12671834Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROED AT BS 1540, RBL 63. REPAIRED IAW EO B767-5310-46118-A.Feb 13, 2012 · N313UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA12671833Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROSION AT STA 1540, LBL 68. REPAIRED IAW EO B767-5310-46117-A.Feb 13, 2012 · N313UP · Boeing 76734AF · Fuselage Main, Floor Beam
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