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 IPXA10661010Stringer · crackedINSPECTION TYPE:C, M/DECK STA 1552 TO 1556 S20R CRACKED. STA 1542.3 TO STA 1579.3, S20R REPAIRED IAW RS R53-61-36765 AND EO B767-5310-38675. ORG MATL IS BAC1506-3122-7075T62, CRACK LENGTH IS 4" APPROX, CUT OFF LENGTH IS 37" THIS REPAIR IS CLASSIFIED AS A MAJun 24, 2010 · N301UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA10660985Skin · inoperativeINSPECTION TYPE:C, LT WING NR 4 SLAT UPPER SURFACE OTBD T/E WEDGE AREA NON-STANDARD REPAIR PATCH FOUND. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 1, REV 47.Jun 24, 2010 · N301UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660933Failsafe · crackedINSPECTION TYPE:C, FUS LT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRIP CRACK FOUND AT OTBD SURFACE 2 O'CLOCK POSITION .1875" DEPTH APPROX VIEW LOOKING OTBD FUSELAGE STA955 LT SIDE REAR SPAR BULKHEAD FAIL SAFE STRAP REPAIRED AS IAW EO B767-5350-17922-F, APPENDIX Jun 24, 2010 · N301UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10660931Failsafe · crackedINSPECTION TYPE:C, FUS RT BS 955 REAR SPAR BULKHEAD FAIL SAFE STRAP CRACK FOUND AT 5 O'CLOCK AND 11 O'CLOCK POSITION .1875" DEPTH APPROX & CORROSION FOUND AT INBD SURFACE 6 O'CLOCK & 9 O'CLOCK POSITION VIEW LOOKING OTBD FUSELAGE STA955 RT SIDE REAR SPAR BULJun 24, 2010 · N301UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10660926Skin · dentedINSPECTION TYPE:C, LT WING NR3 SLAT UPPER INBD AREA FOUND DENT MARK METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1.Jun 24, 2010 · N301UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660759Window · out of adjustF/O SLIDING WINDOW HANDLE REQUIRES EXCESSIVE FORCE TO OPERATE. ADJUSTED F/O SLIDING WINDOW IAW 56-11-02-5. OPS NORMAL. NOTE: WINDOW HEAT TERMINAL WAS NOT DISTURBED.Jun 24, 2010 · N305UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10660984Panel · delaminatedINSPECTION TYPE:C, EMP - VERTICAL STABILIZER RT L/E FIXED PANEL (FSS49 TO FSS59) FOUND DELAMINATION. METAL HOT BOND REPAIR CARRIED OUT IAW EO B767-5530-38665-A REFER RS R-55-30-36766, REV A.Jun 23, 2010 · N301UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA10660976Floor Panel · damagedINSPECTION TYPE:C, STA 1429 TO 1540 LBL 55 TO LBL 80 FLOOR PANEL FOUND 3 DAMAGED AND 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.Jun 22, 2010 · N301UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660867Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE ARM FLANGE AREA FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 1.5" & OTBD FLANGE IS 1.25", DAJun 22, 2010 · N301UP · Boeing 76734AF · Wing, Control Surface Attach FittingsSDR IPXA10660866Hinge Fitting · crackedINSPECTION TYPE:C, RT WING INBD MAIN FLAP INBD HINGE ARM FLANGE AREA FOUND CRACKED. RT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T3 FORGING, CRK LENGTH AT INBD FLANGE IS 1.25" & OTBD FLANGE IS 1.375", DJun 22, 2010 · N301UP · Boeing 76734AF · Wing, Control Surface Attach FittingsSDR IPXA10660983Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER FOUND CRACKED AT STA 785.9, RBL10.94. WING CTR SECTION AT STA785.9 RBL10.94 VERT STIFFENER REPAIRED IAW RS R57-10-36758 & EO B767-5710-38467, ORG MATL IS BAC1518-749-2024T 3511, CJun 21, 2010 · N301UP · Boeing 76734AF · Wing, Center BoxSDR IPXA10660982Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER FOUND CRACKED AT STA785.9 LBL10.94. WING CTR SECTION AT STA 785.9 LBL10.94 VERT STIFFENER REPAIRED IAW RS R57-10-36757 & EO B767-5710-38466, ORG MATL IS BAC1518-749-2024T 3511, CRJun 21, 2010 · N301UP · Boeing 76734AF · Wing, Center BoxSDR IPXA10660981Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER FOUND CRACK AT STA785.9 LBL32.94. WING CTR SECTION AT STA 785.9 LBL 32.94 VERT STIFFENER REPAIRED IAW RS R57-10-36759 & EO B767-5710-38468, ORG MATL IS BAC1518-749-2024T 3511, CRAJun 21, 2010 · N301UP · Boeing 76734AF · Wing, Center BoxSDR IPXA0660660Skin · damagedRT OTBD AILERON HAS 4 OTHER AREAS OF LIGHTNING STRIKE DAMAGE ON UPPER SURFACE OF WEDGE MARKED. STARTED SANDING AREA, FWD LIMITS TO ENGR. FINISHED DAMAGE REMOVAL REF SRM 57-60-02-2R. STARTED NR 346819. REPAIR COMPLETE SEE NRC 346819 AND ECA 020462. THIS REPAIJun 21, 2010 · N302UP · Boeing 76734AF · AileronsSDR IPXA0660654Wedge · damagedRT OTBD AILERON T/E WEDGE LIGHTNING DAMAGE. REPAIRED IAW EO B767-5750-38137-B.Jun 21, 2010 · N302UP · Boeing 76734AF · AileronsSDR IPXA0660659Switch · looseEMERGENCY EXIT LIGHT SWITCH IS LOOSE. SECURED SWITCH AS REQUIRED.Jun 19, 2010 · N324UP · Boeing 76734AF · Emergency LightingSDR IPXA0660636Pneumatic System · inoperativeINSPECTION TYPE:ETOP, APU PNEUMATIC INOP; REF 427849 AND WAN NR 1631215. T/S IAW FIM 49-11-00 AND ECU TEST PASS IAW AMM 49-11-00-5, ITEM CLOSED. BOW COMPLETED.Jun 18, 2010 · N309UP · Boeing 76734AF · Pneumatic SystemSDR IPXA10660544Bracket · inoperativeF/O WINDOW BRACKET BROKEN WHEN WINDOW WAS CLOSED. R & R F/O'S SLIDING WINDOW BEWTWEEN BRACKET IAW AMM 56-11-04-4. ALL SATISFACTORY.Jun 15, 2010 · N305UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10660572Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 1114 TO 1197+22 LBL 11" TO 33" FLOOR PANEL 3 PUNCTURE AND TOGETHER WITH 7 DENT MARKS. MCD FLOOR PANEL FABRICTED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 14, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660490Strip · wornREF WAN 1628319 AND DMI D427307 NR2 ENG OTBD THRUST REVERSER BLOCKER DOORS NR 2 AND NR 3 HAVE WORN TEFLON WEAR STRIPS. REPLACED TEFLON WEAR STRIPS ON OTBD T/R BLOCKER DOORS NR 2 AND NR3 IAW MM 78-31-14-8. CHECKED SATIS. THIS CLOSES DMI.Jun 13, 2010 · N304UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA10660488Strip · wornREF WAN 1628320 AND DMI D427308 NR 2 ENG INBD THRUST REVERSER BLOCKER DOOR NR 3 AND NR 4 WORN TEFLON WEAR STRIPS. REPLACED TEFLON WEAR STRIPS ON INBD T/R BLOCKER DOORS IAW MM 78-31-14- 8. CHECKED SATIS. THIS CLOSES DMI.Jun 13, 2010 · N304UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA10660604Fairing · 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 47.Jun 9, 2010 · N320UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10660600Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD AREA LWR SURFACE CRACKED. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 14, REV 47.Jun 9, 2010 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660383Hmu · malfunctionedINSPECTION TYPE:E, TOP IFSD - DIVERSION - AT CRUISE NR1 ENG LOST POWER. NO PRIOR INDICATION OR WARNINGS. COMPLETED ALL CHECKLISTS, DECLARED EMERGENCY AND DIVERTED TO RFD. MADE A SINGLE ENG LANDING WITH NO PROBLEMS. T/S PER FIM 71-05-00 FIG 104. OPS TEST OF FUJun 9, 2010 · N339UP · Boeing 76734AF · Fuel Controlling SystemSDR IPXA10660607Floor Panel · puncturedINSPECTION TYPE:C, MCD STA412 TO 544 LBL 77 TO LBL 88 FLOOR PANEL FOUND 4 PUNCTURE HOLES TOGETHER WITH 6 DENT. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660606Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 54.5" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660601Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 127" FROM OTBD EDGE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660599Floor Panel · puncturedINSPECTION TYPE:C, MCD STA1425 TO 1522, RBL55 TO RBL77, FLOOR PANEL FND 2 PUNCTURE HOLES AND 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660598Floor Panel · puncturedINSPECTION TYPE:C, STA412 TO 544 LBL55 TO 77 MCD FLOOR PANEL FND PUNCTURE HOLES AND 5 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B77-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660577Floor Panel · damagedINSPECTION TYPE:C, MCD STA540 TO 654+22 LBL11 TO RBL11 FLOOR PANEL FND 6 DAMAGED AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660576Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 972 TO 1112, LBL 11 TO RBL 11, FLOOR PANEL FOUND 3 PUNCTURE HOLES AND TOGETHER WITH 6 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660575Floor Panel · damagedINSPECTION TYPE:C, STA1207 TO 1351 RBL11 TO LBL11 FLOOR PANEL FND 3 DAMAGE AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660574Floor Panel · puncturedINSPECTION TYPE:C, MCD STA 1197+22 TO 1207 LBL11 TO RBL11 FLOOR PANEL FND 5 PUNCTURE HOLES AND 5 DENTS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660573Floor Panel · damagedINSPECTION TYPE:C, MCD STA833 TO 930 RBL11 TO LBL11 FLOOR PANEL FND 6 DAMAGE AND TOGETHER WITH 5 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.Jun 8, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660605Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/B OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-22R FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH 0.244", DAMAGED CUTOUT IS 8.875" X 7.25"Jun 7, 2010 · N320UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660579Skin · delaminatedINSPECTION TYPE:C RUDDER SKIN SIDE UPPER AREA DELAMINATION. GRAPHITE FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-04, PAR 5K, REV 47.Jun 7, 2010 · N320UP · Boeing 76734AF · Rudder, Plate/SkinSDR IPXA10660162Seat Track · damagedSEAT TRACK DAMAGED STA 1415, RBL 77.5. REPAIRED IAW EO B767-5310-37995-A.May 31, 2010 · N304UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA10660160Floor Panel · puncturedREF D425460 MAIN CARGO DECK, POSITION 2, OTBD FLOOR PANEL PUNCTURED. STA 434, RBL 83. ACCOMPLISHED MAJOR REPAIR IAW EO B767-5320-9693-G.May 30, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660384Bracket · crackedINSPECTION TYPE:C RT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. RT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 57-10-02 AND 51-40-02 REV 47.May 26, 2010 · N317UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA10660174Rib · crackedINSPECTION TYPE:C, LT WING L/E LES 160 FIXED FAIRING UPPER SUPPORT RIB FRONT SPAR SUPPORT ANGLE FOUND CRACKED CRACK .2500" IN LENGTH. LT WING L/E LES 160 FIXED FAIRING UPPER SUPPORT RIB FRONT SPAR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-May 25, 2010 · N317UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA10660207Skin · crackedINSPECTION TYPE:C, RT WIING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1440, DAMAGED CUTOUT IS 0.500" May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660206Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD AT OSS723.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1625", DAMAGED CUTOUT IS 0.500" May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660205Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1460", DAMAGED CUTOUT IS 0.500" DIA,May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660204Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1845", DAMAGED CUTOUT IS 0.500" DIAMay 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660203Skin · crackedINSP TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1530", DAMAGED CUTOUT IS 0.500" DIA. THIMay 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660202Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1455", DAMAGED CUTOUT IS 0.500" DIA. May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660201Skin · crackedINSPECTION TYPE:C, LT WING NR3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739, EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1255", DAMAGED CUTOUT IS 0.468" DIA, THMay 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660200Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR3 SLAT INBD AT OSS723.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1375 DAMAGED CUTOUT IS 0.468" DIA THIS IS CMay 24, 2010 · N317UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA10660176Hinge Fitting · crackedINSPECTION TYPE:7C, RT WING INBD MAIN FLAP INBD HINGE FITTING FLANGE FOUND CRACKED. RT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG 201, REV 47. ORG MAT'L IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 0.6" AND OTBD FLANMay 24, 2010 · N317UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660175Hinge Fitting · crackedINSPECTION TYPE:7C, LT WING INBD MAIN FLAP INBD HINGE FITTING FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG 201, REV 47. ORG MAT'L IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 1.5" AND OTBD FLANGMay 24, 2010 · N317UP · Boeing 76734AF · Trailing Edge Flaps
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