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 UPS09654638Floorboard · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED FS 694. REPAIRED PER SRM 53-00-50-2R.Feb 8, 2009 · N314UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654637Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK POS 2R MOST O/B PANEL 40 INCHES AFT OF RED LINE AND APPROX 4 INCHES I/B OF O/B SEAT TRACK. GOUGED 2.1" LONG X 1" WIDE. REPAIRED PER EO B767-5320-31355-A.Feb 8, 2009 · N329UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654499Doubler · debondedINSPECTION TYPE:N/A RT WING - I/B AFT FLAP, TRAILING EDGE WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W4-02. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.Jan 30, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654522Stringer · damagedINSPECTION TYPE:7C FX - STA 1353-1366 STR - 14R FOUND A DRILLED HOLE AT THE RADIUS. FX - STA 1353-1366 STR - 14R REPAIRED AS PER SRM 53-00-03-2R1 FIG 201, SUBSEQUENCE INSPECTION REQUIRED AS PER SRM 53-00-03-2R1, FIG 201, SHEET 10 TABLE V. THIS IS CLASSIFIED Jan 28, 2009 · N304UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR UPS09654454Compressor · stalledINSPECTION TYPE:ETOP RTO LT ENG COMPRESSOR STALLED. PULLED HARD LEFT AT 80 KTS. TOWER REPORTED FLAMES FROM LEFT ENGINE AFTER ABORT. A/C OOS. ***SDR FILED OPEN***Jan 27, 2009 · N302UP · Boeing 76734AF · Turbine Engine Compressor SectionSDR IPXA10658276Coupler · leakingCREW REPORTED CRT HYD QTY EICAS MSG, CRT HYD SYS PRESSURE EICAS MSG, A ND WHILE ON SHORT FINAL RECEIVED A LT YAW DAMPER EICAS MSG. EMERGENCY DECLARED CTR LCCA LEAKING IN RT WHEEL WELL, REMOVED R LCCA TO SET D-5 MM 27-11 -14-4. COMPLETE INSTALLATION OF RT LCCAJan 26, 2009 · N307UP · Boeing 76734AF · Hydraulic System, MainSDR UPS09654541Stiffener · crackedINSPECTION TYPE:C M/DECK - STA 796, WL 196, LBL 33 FUEL TANK FWD UPPER CHORD FOUND CRACK 2.25 INCHES. FUEL TANK FRONT SPAR STIFFENER REPAIRED AS PER HX RS R57-11-36259 JUST AT STA 786, LBL 33, BETWEEN WL 173 AND 196. THIS IS CLASSIFIED AS A MAJOR REPAIR WITHJan 25, 2009 · N304UP · Boeing 76734AF · Wing, Center BoxSDR UPS09654523Frame · crackedINSPECTION TYPE:7C M/DECK STA 676 STR R5-R6 FRAME WEB FOUND CRACK. M/DECK STA 676 STR R5-R6 FRAME WEB REPAIRED AS PER SRM 53-00-07-2R1 FIG 201.Jan 25, 2009 · N304UP · Boeing 76734AF · Fuselage Main, FrameSDR UPS09654558Support Bracket · crackedINSPECTION TYPE:C RT WING- L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET FOUND CRACKED (1 INCH LENGTH). RT WING - L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 25, 2009 · N304UP · Boeing 76734AF · Wing SparSDR UPS09654557Support Bracket · crackedINSPECTION TYPE:C RT WING - L/E LES 732 FIXED L/E SUPPORT UPPER AFT SUPPORT BRACKET FOUND CRACKED (1.2 INCH). RT WING - L/E LES 732 FIXED L/E SUPPORT UPPER AFT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 25, 2009 · N304UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS09654551Floor Panel · dentedINSPECTION TYPE:7C MCD - STA 760 LBL 5 FLOOR PANEL FOUND DENT MARK. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.Jan 25, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654509Access Panel · debondedINSPECTION TYPE:C LT WING - I/B MAIN FLAP LOWER ACCESS PNL, FOUND DISBOND. SRM 51-70-10 REPAIR 4 FIG 203 REV 43.Jan 25, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654427Static Inverter · malfunctionedINSPECTION TYPE:ETOP DURING PS-CHECK, STARTING APU MECHANIC NOTICED SMOKE IN COCKPIT. FURTHER INVESTIGATION FOUND STATIC INVERTER IN E3 RACK CAUGHT FIRE. REMOVED STATIC INVERTER AND FIRE HAD BEEN EXTINGUISHED BY FIRE FIGHTER, NO DAMAGED ADJACENT COMPONENT.Jan 25, 2009 · N312UP · Boeing 76734AF · AC InverterSDR UPS09654538Attach Fitting · crackedINSPECTION TYPE:7C FX - MEC COMPT STA 246 RBL 10 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK. FX - MEC COMPT STA 246 RBL 10 MAIN DECK FLOORBEAM ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 24, 2009 · N304UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS09654507Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-08. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.Jan 24, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654647Hinge Fitting · crackedINSPECTION TYPE:C RT WING MAIN FLAP SUPPORT HINGE FITTING FOUND CRACK. RT WING MAIN FLAP SUPPORT HINGE FITTING REPAIRED PER SRM 57-53-02-2R1 FIG 201.Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654520Doubler · debondedINSPECTION TYPE:C RT WING - O/B FLAP LOWER FWD ACCESS PNL DOUBLER DISBOND FOUND, REF SURVEY SEQ 304-W4-05. SRM REV 43, 51-70-10, REPAIR 4 FIG 201.Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654519Skin · delaminatedINSPECTION TYPE:C LT WING O/B FLAP T/E WEDGE LOWER SKIN EXISTING REPAIR FOUND DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1).Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654555Floor Panel · damagedINSPECTION TYPE:7C MCD - POSITION 7, FLOOR PANEL FOUND HOLE 1 X .25 INCH APPROX. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.Jan 23, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654508Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND TOO CLOSE AND DISBOND, REF SURVEY SEQ 304-W3-06 TO 07. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654506Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND REF SURVEY SEQ 304-W3-04. SRM 51-70-10, REPAIR 4 FIG 202 REV 43.Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654505Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-09. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.Jan 23, 2009 · N304UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654540Skin · misrepairedINSPECTION TYPE:C FX - BS 365 TO 393 BETWEEN STR 32R AND 33R EXISTING REPAIR DOUBLER FOUND BLIND FASTENERS INSTALLED REFER TO SURVEY SEQUENCE 304-F1-01. FX - BS 365 TO 393 BETWEEN STR 32R AND 33R SKIN REPAIRED AS PER SRM 53-00-01-2R1 FIG 201, SUBSEQUENT INSPEJan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654539Skin · damagedINSPECTION TYPE:C FX - BS 654 TO 654+22 BETWEEN STR 25L AND 26L EXISTING REPAIR CAN'T DETERMINE THE REPAIR CONFIGURATION AS PER SRM REFER TO SURVEY SEQ 304-F1-03. FX - BS 654 TO 654+22 BETWEEN STR 25L AND 26L SKIN REPAIRED AS PER HX RS R53-30-36256. THIS IS Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS09654518Floor Support · crackedINSPECTION TYPE:C FX MEC STA 246 LBL 25 MAIN DECK FLOOR SUPPORT CLIP FOUND CRACK (1 INCH LENGTH). FX MEC STA 246 LBL 25 MAIN DECK FLOOR SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654517Floor Support · crackedINSPECTION TYPE:C FX MEC STA 246 LBL 50 MAIN DECK FLOOR SUPPORT CLIP FOUND CRACK (1 INCH LENGTH). FX MEC STA 246 LBL 50 MAIN DECK FLOOR SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654554Floor Panel · damagedINSPECTION TYPE:7C MCD - POSITION 2R, FLOOR PANEL FOUND HOLED. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654553Floor Panel · damagedINSPECTION TYPE:7C MCD - POSITION 5, FLOOR PANEL FOUND DAMAGE. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654552Floorboard · puncturedINSPECTION TYPE:7C MCD - POSITION 2L, CENTER FLOOR BOARD HAS 1 INCH HOLE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654463Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT - STA 1087 RBL 25 BELOW FLOOR CLIP FOUND CRACK (CRACK .8750 INCH LENGTH). AFT CARGO COMPT - STA 1087 RBL 25 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654462Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT - STA 1087 LBL 25 BELOW FLOOR CLIP FOUND CRACK. (.8750 INCH LENGTH). AFT CARGO COMPT - STA 1087 LBL 25 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Jan 22, 2009 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS09654550Floor Panel · damagedINSPECTION TYPE:7C MCD - POSITION 6, LEFT AND LEFT OF CENTER FLOOR PANEL FOUND HOLE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.Jan 21, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654549Floor Panel · damagedINSPECTION TYPE:7C DMI D390721, MCD POSITION 5C HAS A .5 INCH HOLE IN THE CENTER (STA 700 RBL 5) FLOOR PANEL. REPAIRED AS PER SRM 53-00-50-2R.Jan 21, 2009 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS09654389Panel · delaminatedINSPECTION TYPE:N/A, NR 9 SLAT AT CLOSE OUT PANEL DELAMINATED. DELAM 1.3 BY .30 INCH. THE TEAR IS LOCATED AT THE CENTER OF THE DELAM. REPAIRED PER EO B767-5750-30957-A.Jan 18, 2009 · N332UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654398Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL SURVEY SEQ 305-S1-12 TO 16 EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654397Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654396Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654395Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654394Skin Panel · debondedINSPECTION TYPE:C EMP - RT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH DISBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.Jan 17, 2009 · N305UP · Boeing 76734AF · Horizontal Stabilizer, Plate/SkinSDR UPS09654387Skin · misrepairedINSPECTION TYPE:C RT WING NR 10 SPOILER T/E UPPER SURFACE EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1) FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654386Skin · misrepairedINSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654385Skin · misrepairedINSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.Jan 11, 2009 · N305UP · Boeing 76734AF · SpoilersSDR UPS09654352Skin · misrepairedINSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-55, -56, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511194-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654351Skin · misrepairedINSPECTION TYPE: C RT WING NR 9 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR REF SURVEY SEQ NR 305-W4-30, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511210-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654350Skin · misrepairedINSPECTION TYPE: C RT WING NR 10 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-38, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511178-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654349Skin · misrepairedINSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W3-31, -32, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511244-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654348Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-23, -24, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511145-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654347Skin · misrepairedINSPECTION TYPE: C RT WING NR 7 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-5, -6, -7, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511160-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654346Skin · misrepairedINSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-16, -17. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511129-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR UPS09654345Skin · misrepairedINSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-53, -54. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511228-1.Jan 8, 2009 · N305UP · Boeing 76734AF · Leading Edge Devices
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