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 IPXA11668215Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 B/H, CRACK FOUND AT FAIL SAFE STRAP 3 O'CLOCK POSITION APPROX 0.040". FUSELAGE LT SIDE BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIED EO NR B767-5350-17922-I APP 'C' ORIGINAL MAT'L IS 2024T351-0750" MACHINED STJul 11, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668150Fairing · delaminatedINSPECTION TYPE:C, RT 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 50.Jul 11, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667973Fairing · delaminatedINSPECTION TYPE:8C, LT 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.Jul 11, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11668214Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR B/H SIDE FTG FAIL SAFE STRAP ULTRASONIC INSP FOUND CRACK INDICATION , REMOVE FASTENER FOR CRACK CONFIRMATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT REMOVED AND REJul 9, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668213Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR B/H SIDE FTG FAILSAFE STRAP ULTRASONIC INSP FOUND CRACK INDICATION, REMOVE FASTENER FOR CRACK CONFIRMATION. FASTENER RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT REMOVED AND REINSTJul 9, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11667902Blade · damagedINSPECTION TYPE:E TOP, ATB - BIRD STRIKE ON TAKEOFF, LT FAN VIBRATION 5.0. ALL OTHER ENG INDICATIONS NORMAL. REPLACED 5 EA DAMAGED BLADES IAW EO80C2-7230-43438-A & AMM 72-31-02-4 VIB SURVEY W/I LIMITS IAW AMM 71-00-00-5.Jul 9, 2011 · N339UP · Boeing 76734AF · Turbine Engine Compressor SectionSDR IPXA1667723Instrument Panel · smokeAT 10000 FT ON ARRIVAL, A 3.5 SEC STREAM OF SMOKE BILLOWED UP FROM THE UPPER EICAS SCREEN DEFINITE ACRID ODOR LIKE IT MAY BE ELECTRIC BUT THEN IT DISAPPATED AND DID NOT RETURN. GAINED ACCESS TO AREA RWD OF INST PANEL THRU P1-3 P2, AND P3-1 PANELS FOUND NO INDJul 7, 2011 · N341UP · Boeing 76734AF · Central WarningSDR IPXA1667709Actuator · inoperativeRUDDER TRIM WOULD NOT MOVE RT WITH RUDDER TRIM KNOB. TRIM AT 1.5 LT FOR LANDING-AIR TURN BACK TO DEPARTURE T/S IAW FIM 27-21-00/101, FIG 100, FOUND RUDDER TRIM ACTUATOR WOULD NOT MOVE. R & R RUDDER TRIM ACTUATOR AND SYS OPS CHECK NORMAL IAW AMM 27-21-11-2.Jul 5, 2011 · N320UP · Boeing 76734AF · Rudder Tab Control SystemSDR IPXA1667649Bulb · inoperativeEXTERIOR EMERGENCY LIGHT INOP. R & R BULB IAW MM 33-51-16-2, SYS OPS CK'S NORMAL.Jul 3, 2011 · N341UP · Boeing 76734AF · Emergency LightingSDR IPXA11667582Pseu · inoperativeWHEN SETTING FLAP 5, CREW GOT "LE SLAT ASM" MESSAGE. EMERGENCY DECLARED. T/S C/O IAW FIM 27-81-00, FIG 107, SH1, SH2, BLOCK 1, 2 TO 20. FOUND ON PSEU BITE CARD NR 9 AT FAULT. R & R PSEU IAW AMM 32-09-04-4. OPS CHECK SATIS. PERFORMED ADJ/TEST OF L/E SLAT SJun 28, 2011 · N332UP · Boeing 76734AF · Leading Edge Slat Control SystemSDR IPXA11667573Skin · damagedFUSELAGE SKIN DAMAGE AT STA 1439. REPAIRED IAW EO B767-5330-43156.Jun 28, 2011 · N334UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA1668799Floor Panel · dentedINSPECTION TYPE:PS, MAIN CARGO FLOOR PANEL DENTED, FABRICATED A REPLACEMENT FLOOR PANEL BY CUTTING OUT A NEW FLOOR PANEL FROM A402H IAW EO B767-5-320-9693-G..Jun 26, 2011 · N332UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667535Floor Panel · damagedNUMEROUS HOLES IN MAIN CARGO FLOOR PANEL, POS 2L, JUST FWD OF MAIN CARGO DOOR OPENING. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Jun 26, 2011 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667618Floor Panel · dentedINSPECTION TYPE:7C, D455624 - MAIN CARGO COMPT FLOOR PANEL REPAIR POSITION 2 CENTER LINE PANEL. POSITION 2 CTR LINE FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Jun 23, 2011 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667617Floor Panel · dentedINSPECTION TYPE:7C D455632 - MAIN CARGO COMPT FLOOR PANEL REPAIR. POSITION 5 CENTER LINE PANEL. POSITION 5 CENTER LINE FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Jun 23, 2011 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667616Floor Panel · dentedINSPECTION TYPE:7C, D455622- MAIN CARGO COMPT FLOOR PANEL REPAIR POSITION 6, CENTER LINE PANEL. POSITION 6 CENTER LINE FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Jun 23, 2011 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667654Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jun 22, 2011 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11667443Unknown · odorETOP DIV - STRONG ODOR, EXHAUST METALLIC TYPE ODOR WHILE A TCR CRUISE SUSPECT RESIDUE FROM GROUND. PNUEMATIC START CART, SMOKE/STRONG ODOR INCREASED IN INTESITY WITH BOTH CONFIRMATIONS. INSP LT & RT ACFT SYS. RAN PACKS TO REMOVE ODOR WITH AIR START UNIT AJun 22, 2011 · N326UP · Boeing 76734AF · Air Distribution SystemSDR IPXA1667661Fitting · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H FITTING AREA 1EA FASTENER HOLE FOUND CRACK AT T-FITTING APPROX .1250" IN LENGTH ON 3 O/C POSITION. FUSE RT BS 955 REAR SPAR B/H FITTING AREA T-FITTING REPLACED AND INSTALL IAW EO B767-5350-17922-I APP D ORG MAT'Jun 21, 2011 · N308UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1667660Failsafe · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H FITTING AREA 1 EA FASTENER HOLE FOUND 2EA CRKS AT FAIL SAFE STRAP APPROX .1250" IN LENGTH ON 4 O/C POSITION AND THROUGH THICKNESS OM 10 O/C POSITION. FUSE RT BS 955 REAR SPAR B/H FITTING FAIL SAFE STRAP REPAIREDJun 21, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667659Failsafe · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H SIDE FITTING FAIL SAFE STRAP 1 EACH HOLE CRACK INDICATION. FUSE RT BS 955 REAR SPAR B/H SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT REMOVED AND REINSTALLED IAW EO B767-5350-17922-I, APPENDIX D FIG 6 FOR FURTHJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667657Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 B/H REAR SPAR FITTING AREA CRACK FOUND AT T-FITTING HAT 9 O'CLOCK POSITION APPROX 1250" . FUSE LT BS 955 REAR SPAR B/H AREA T-FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-I APP C, ORG MAT'L IS 7075-T73 DIE FORGINJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1667656Failsafe · crackedINSPECTION TYPE:C, FUSE LT BS 955 B REAR SPAR FITTING AREA 2EA CRACKS FOUND AT FAIL SAFE STRAP AT 3 O'CLOCK POSITION THROUGH THICKNESS AND 9 O'CLOCK POSITION APPROX. .1250" FUSE LT SIDE BS 955 REAR SPAR B/H FITTING FAIL SAFE STRAP REPAIRED AS IAW EO B767-5350Jun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667655Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP, 1 EACH HOLE CRACK INDICATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT. REMOVED & REINSTALLED IAW EO B767-5350-17922-I APP C, FJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA11667604Floor Panel · dentedINSPECTION TYPE:C, FLOOR PANEL FOUND 8 EA DENTS TOGETHER WITH DEEP GOUGE RUNNING THROUGH FROM FWD TO AFT AT BS 598 TO 654+22 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.Jun 19, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667603Floor Panel · dentedINSPECTION TYPE:C, FLOOR PANEL FOUND 9EA DENTS AND 2 TOGETHER WITH DEEP GOUGE RUNNING THROUGH FROM FWD TO AFT AT STN 654+22 TO STN 690 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.Jun 19, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667580Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9, LBL 10.94. ORIGINAL MATERIAL IS BAC1518-912-2024T3511, CRACK LENGTH IS 1.25", CUT OFF LENGTH IS 19.5". THIS REPAIR IS CLASSIFIED ASJun 19, 2011 · N308UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA11667578Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. ORIGINAL MATERIAL IS BAC1518-749-2024T3511, CRACK LENGTH IS 2.25", CUT OFF LENGTH IS 16.5", THIS REPAIR IS CLASSIFIED AS AJun 19, 2011 · N308UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA1667366Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 4, CENTER HAS 3 EA .2500" HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667363Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 4L HAS HOLE. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667362Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL, POS NR 6 CTR HAS 2 EA HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667361Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 6/7R HAS 2 EA .2500" HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667360Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS NR 5R HAS .2500" HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667348Floor Panel · damagedREF D431900, FLOOR PANEL 2L HAS 1" HOLE. FABRICATED & REPLACED PANEL IAW EO B767-5320-9693-H.Jun 18, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667347Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 2/3 HAS 1EA HOLE. REF D432191, FABRICATED & REPLACED FLOOR PANEL IAW EO B767-5320-9693-H.Jun 18, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667400Failsafe · corrodedINSPECTION TYPE:8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING - A SLIGHT CORROSION FOUND AFTER FAIL SAFE STRAP TRINNED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA OF THE SKIN IN THE AREA WHERE THE "T"FITTING TO THE FAIL SAFE STRAP. RT BS 955 BULKHEAD SJun 10, 2011 · N309UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1667394Failsafe · corrodedINSPECTION TYPE:8C, FUSELAGE LT BS 955 BULKHEAD SIDE FITTING - CORROSION FOUND AFTER FAIL SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE "T" FITTING TO THE FAIL SAFE STRAP. FUSELAGE LT BS955 BULKHEAD SIDE FITTING - SLIGHT CJun 10, 2011 · N309UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11667142Floor Panel · puncturedMAIN CARGO FLOOR PANEL REPAIR POS 4 R HAS A.75" HOLE & .5: IDENTIFIED FLOOR PANEL FROM POS 4, RT PN143-5876-50 IAW EO B767-5320-9693H FABRICATED A REPLACMENT FLOOR PANEL BY CUTTING OUT A NEW FLOOR PANEL FROM A402H AND MARKING INSERTS LOCATION USING EXISTING FJun 10, 2011 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667141Floor Panel · puncturedMAIN CARGO FLOOR PANEL REPAIR POS 4 R HAS .75" HOLE .5". IDENTIFIED FLOOR PANEL FROM POS 4 RT PN145T5876-50 IAW EO B767-5320-9693H FABRICATED A REPLACMENT FLOOR PANEL BY CUTTING OUT A NEW FLOOR PANEL FROM A402H AND MARKED INSERT LOCATION USING EXISTING FLOOR Jun 10, 2011 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667140Floorboard · puncturedMAIN DECK FLOORBOARD AT POS 14 LT HAS A 1" HOLE AND .5". IDENTIFIED FLOORBOARD FROM POS 14 LT PN145T5869-54 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT FLOORBOARD BY CUTTING OUT A NEW PANEL FROM A402H AND MARKED INSERT LOCATION USING EXSTING FLOORBOARDJun 10, 2011 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667139Floorboard · puncturedMAIN DECK FLOORBOARD AT POS 7 L HAS A .5" HOLE REF D446415. IDENTIFIED FLOORBOARD FROM POS 7, L PN145T5876-10 IAW EO B767-5320-9693H FABRICATED A REPLACEMENT FLOORBOARD BY CUTTING OUT A NEW FLOORBOARD FROM A402 HAND MARKING INSERT LOCATION USING EXISTING FLOOJun 10, 2011 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667138Floor Panel · puncturedPOSITION 5, CTR MAIN DECK FLOOR PANEL HAS A 3" DENT WITH A 2" HOLE. IDENTIFIED PANEL FROM POS 5 CTR PN145T5876-51 IAW EO B767-5320-9693 HAS REPLACEMENT FLOOR PANEL BY CUTTING OUT NEW PANEL FROM A402H AND MARKING INSERT LOC USING EXISTING FLOOR PANEL AS TEMPLAJun 10, 2011 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667335Fairing · delaminatedINSPECTION TYPE:8C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1), FIG 5, REV 50.Jun 9, 2011 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667398Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA, 3 EA CRACKS FOUND AT T-FITTING AT 5 O'CLOCK POSITION APPROX .0625", 6 O'CLOCK POSITION APPROX. .0625" AND 10 O'CLOCK POSITION APPROX .1250". FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA "T"Jun 8, 2011 · N309UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1667397Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA, 2 EA CRACKS FOUND AT FAIL-SAFE STRAP AT 3 O'CLOCK POSITION APPROX .1250" AND 7 O'CLOCK POSITION APPROX .1250". FUSELAGE LT SIDE BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED Jun 8, 2011 · N309UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1667337Fairing · delaminatedINSPECTION TYPE:8C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG5, REV 50.Jun 8, 2011 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667336Fairing · delaminatedINSPECTION TYPE:8C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG5, REV 50.Jun 8, 2011 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11667254Skin · bulgedINSPECTION TYPE:8C, LT WING NR3 SLAT WEDGE AREA UPPER SURFACE NEAR INBD EDGE FOUND BULGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 50.Jun 8, 2011 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA1667392Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT FAIL SAFE STRAP AT 8 O'CLOCK POSITION. THROUGH THICKNESS FUSELAGE BS955 RT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-H, APPENDIX "D". Jun 7, 2011 · N309UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1667391Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955, REAR SPAR BULKHEAD FITTING CRACK FOUND AT TEE FITTING AT 8 O'CLOCK POSITION APPROX .1250". TEE FITTING REPLACED IAW EO B767-5350-17922-H, APPENDIX "D". ORIGINAL MATERIAL IS 7075-T73 DIE FORGING, CRACK FOUND AT TEE FITTJun 7, 2011 · N309UP · Boeing 76734AF · Fuselage Main, Attach Fittings
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