Boeing 767-34AF

Service difficulty reports · 6,308

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2024021449080Door · warning messageL FWD ENTRY DOOR EICAS AND LIGHT ON AFTER BLOCK OUT PERFORMED DOOR WARNING SENSOR TEST AS PER AMM 52-71-00, SYST IS WORKING NORMAL.Feb 13, 2024 · N316UP · Boeing 76734AF · Door Warning SystemSDR IPXA2024020987073Warning Message · illuminated***EMERGENCY DECLARED *** TE FLAP DISAGREE EICAS ILLUMINATED WHEN SELECTING FLOPS FROM 1 TO 5 PERFORMED FIM TASK 27-51-FAULT TREE 808 AND 810. FOUND NO FAULTS IN FSEU. PERFORMED MULTIPLE OPS CHECKS OF TRAILING EDGE FLAP SYSTEM IAW AMM 27-51-00. SYSTEM OPERATEDFeb 9, 2024 · N301UP · Boeing 76734AF · Trailing Flap Position Indicating SystemSDR IPXA2024020267014Floor Panel · crackedFOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432-1520, LBL 55 - LBL 77.5, P/N: 146T5869-43 (REPAIR) IAW AMM 53-01-06-400-801 REV.141 INSTALL MAIN DECK CARGO FLOOR PANEL. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV 141 REFeb 2, 2024 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024020320072Floor Panel · crackedMAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432 ~ 1520, LBL55~ LBL77.5, P/N:146T5869-89 (REPLACE) REMOVE MAIN DECK CARGO FLOOR PANEL AREA SEALANT I.A.W AMM 53-01-06-000-801 REV 141 AND CONDITION CHECK NORMAL. ACCOMPLISHED ACCESS FLOOR PANELJan 31, 2024 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024022083876Hinge · deformedFOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. REPLACED HINGE ASSY I.A.W AMM 20-11-00-910-802 REV.141.Jan 29, 2024 · N315UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024022083857Spline · brokenFOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED DOORWAY SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141.Jan 29, 2024 · N315UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024020284515Skin Panel · dentedMAJOR REPAIR, DENT, FUSELAGE SKIN BETWEEN STA 360 - STA 384, S-16L - S-17L (REPAIR). ACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-12 REV.88 AND EO-89370-REQ 1 REV. 1. JOB COMPLISHED. REVIEW COMPLETEJan 29, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2024012983876Hinge · deformedFAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE)Jan 29, 2024 · N315UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024012983857Trim Panel · brokenFAULT - FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN (REPLACE)Jan 29, 2024 · N315UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024020571729None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR.Jan 28, 2024 · N348UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2024012971729None · none**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR.Jan 28, 2024 · N348UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2024013038949Support · brokenFOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY) REMOVED THE BROKEN INBD LE SUPPORT LINK DOORS AND REPLACED NEW INBD LESUPPORT LINK DOORS PER AMM 57-41-59-401 AND OPS CHK OKJan 26, 2024 · N324UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2024012638949Support · broken*SDR FILED OPEN* FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY)Jan 26, 2024 · N324UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024020523240Adapter · brokenFOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALJan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024020512998Angle · crackedCRACKED ANGLE IN BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALJan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024020222506Window · hazeDURING PRE-FLIGHT, FOUND FIRST OFFICERS FORWARD WINDOW TO BE HAZY AND OPAQUE. VISION OUT OF WINDOW IS IMPAIRED R/R #1 WINDOW ON FO SIDE IAW B767 AMM 56-11-01/401Jan 25, 2024 · N359UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA2024012622506Window · haze*SDR FILED OPEN* DURING PRE-FLIGHT, FOUND FIRST OFFICERS FORWARD WINDOW TO BE HAZY AND OPAQUE. VISION OUT OF WINDOW IS IMPAIRED REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT IAW 767 AMM30-41-01-004-001 AND 30-41-01-404-007. WINDOW HEAT OPERATES NORMAL. WINDOW Jan 25, 2024 · N359UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA2024012522998Angle · crackedFAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.141 REMOVED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALJan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024012523240Fitting · brokenFAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) 1. I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.141 REMOVED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALJan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA2024012521784Altimeter · warning messageABOVE 2 HRS INTO FLT AT 38K WE HAD AN ALT DISAGREE CAUGHTION MSG. WE DETERMINED THE F.O.'S WAS INCORRECT. IT WAS ABOUT 250-260 FT ABOVE THE CAPT'S AND ABOUT .01 DIFFERENCE IN MACH NUMBER ++ REMOVED AND REPLACED R/H ADC IAW MM CHT 34-12-01 OPS CKS GOOD QD'S WERJan 25, 2024 · N313UP · Boeing 76734AF · Altimeter, Barometric/EncoderSDR IPXA2024020506229Fire Detector · crackedCRACKED BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) I.A.W AMM 26-18-01-424-014-001 REV.141 INSTALLED DUCT LEAK DETECTOR CLAMPS AT STA 1562 LBL 66 & CONDITION CHECK NORMAL.Jan 24, 2024 · N348UP · Boeing 76734AF · Fire DetectionSDR IPXA2024012406229Strip · crackedFAULT - CRACK - BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) OK TO WORKJan 24, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA2024041680192Skin · damaged*SUPPLEMENTAL SDR* DURING PDC .FOUND DAMAGE ON RT WING INBD AFT FLAP. INSTALLED SERVICEABLE RH WING INBD AFT FLAP IAW AMM 27-51€“06/201. OPS CHECK GOOD. THIS CLEARS DMI.Jan 22, 2024 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024012580764Window · cloudy*SUPPLEMENTAL SDR* R1 WINDOW VERY CLOUDY. RR R1 WINDOW IAW AMM 55-11-01. OPS CHECK GOOD.Jan 22, 2024 · N359UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA2024012380764Window · damagedR1 WINDOW VERY CLOUDY. REMOVED R1 WINDOW IAW 767 AMM 56-11-01-004-039Jan 22, 2024 · N359UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA2024012380192Flap · damaged*SDR FILED OPEN* DURING PDC .FOUND DAMAGE ON RT WING INBD AFT FLAP. ASSIGNED EO-89280-REQ1 TO FAULT.Jan 22, 2024 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024012052414Cabin Pressure · faulted*ETOPS FILED OPEN* STATUS MSG CABIN ALT AUTO 2 APPEARED ENROUTE AT CRUISE ALTITUDE WHILE SWITCH WAS IN AUTO 2 DEFERRED CABIN ALT AUTO 2 INOP PER MEL 21-31-1A. PLACARD INST.Jan 20, 2024 · N322UP · Boeing 76734AF · Cabin Pressure Control SystemSDR IPXA2024013128494Skin · debondedFAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) C/W REVIEW. ADJUSTMENT AND OPERATIONAL TEST OF THE LH WING NO.4 SLAT. I.A.W AMM 27-88-01-722-028 REV.141 STEP G(16) TO STEP H COMPLETED LE SLAT SYSTEM OPERATIONAL TEST, RESULT WAS SATISFIED.Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2024013128280Rib · crackedFAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) C/W REVIEW REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV.88Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2024013128251Access Panel · crackedFAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) REVIEWED REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2024013128068Panel · crackedFAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) REVIEWED REMOVED CLOSURE PANEL AT NO.4 SLAT I.A.W SRM 51-40-02-0G REV.88Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2024012228068Panel · damaged*SDR FILED OPEN* FAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) PER B767 NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-02, REV.136 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL Jan 19, 2024 · N339UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2024012228251Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) OK TO WORKJan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2024012228494Skin · debonded*SDR FILED OPEN* *MAJOR REPAIR* FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) 1.OK TO INSTALL CHECK SATISFIED.<BR>2.I.A.W. AMM 27-81-02-424-099 REV.141 STEP 1.A TO 1.H(15) INSTALL NO.4 SLAT OF THE LH WING LEADING EDGE.Jan 19, 2024 · N339UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2024012228280Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) OK TO WORKJan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2024012227720Cap · crackedFAULT - CRACK, LH WING OUTBD FLAP END CAP. (REPAIR). PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W. 767 NTM PART1 51-01-01 REV:136. RESULT:NO DEFECT FOUND. 1.REMOVE THE DAMAGE MATERIALS (L:0.3", W:0.05", AT LEFT HAND OUTBOARD FLAP INBOARJan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024012227663Skin · damagedFAULT - CHIP SKIN, LH WING INBD MAIN FLAP OUTBD UPR SEAL LE AREA. (REPAIR). 1. REMOVE THE UNWANTED MATERIALS AND CLEAN AT LEFT HAND WING INBOARD MAIN FLAP OUTBOARD UPPER SEAL LEADING EDGE AREA. AND TRIM OUT THE DAMAGE AS REQUIRED, KEEP A MINIMUM 0.5 IN CORNER Jan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024013145304Liner · missing**SUPPLEMENTAL SDR**FAULT - FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) C/W REVIEW INSTALLED NEW DOOR LINING I.A.W AMM 52-12-02-004-001Jan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024011745304Liner · unknownFOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) OK TO WORKJan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024013037780Cover · inoperative**SUPPLEMENTAL SDR**COVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION REMOVED DEBRIS FROM HINGE REF IPC 52-11-02-10A ITEM 170. OPS CHK THE CREW ENTRY DOOR IAW AMM 52-12-00. DEFERRAL CLEARED PLACARD REMOVEDJan 15, 2024 · N337UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024011636099Stiffener · crackedFAULT - CRACK WING CENTER TANK FRONT SPAR STIFFENER AT STA 785.9 RBL 11 (REPAIR) THIS REPAIR IS CLASSIFIED AS MAJOR. ACCOMPLISH THE REPAIR PER SRM 57-10-10-2R-2 AND SUBTASK T3F18E003SH3X. MARK THE FAULT WITH FLIGHT SAFETY IMPACT. ACCOMPLISHED REPAIR I.A.W SRMJan 15, 2024 · N339UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024011637780Unknown · unknownCOVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION DEFERRED DOOR ARMING LEVER HINGE COVER REF MEL 52-11-2, PLACARDS INSTALLED.Jan 15, 2024 · N337UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024013124637Trim Panel · broken**SUPPLEMENTAL SDR**TRIM BROKEN L1 DOOR SIDE WALL PANEL INSTALLED NEW SPLINE TRIM PIECE I/A/W INDUSTRY STANDARD PRACTICES AND IPC 52-11-02-10A. NO DEFECTS NOTED AT THIS TIME.Jan 13, 2024 · N322UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024011424637Unknown · unknownRIM BROKEN L1 DOOR SIDE WALL PANEL ASSIGNED EO-89173-REQ1 TO FAULT.Jan 13, 2024 · N322UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024012302696Angle · brokenFAULT - FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 141T8310 SH. 4 REV. H. REVIEWEDJan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024012301393Scuff Plate · crackedFAULT - FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE). 1.I.A.W AMM 53-13-01-424-005 REV.141 INSTALLED THE SCUFF PLATE. 2.ACCOMPLISHED THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST I.A.W AMM 05-51-24-782-001 REV.141, NO LEAKAGE WAS FOUND. 3.JOBJan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024011202696Unknown · unknownFOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE)Jan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024011201393Unknown · unknownFOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE) OK TO WORKJan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024012382386Pawl · wornFAULT - FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.141 AND AMM 52-11-26-404-003 REV.141 REPLACED PAWL, OPERATION CHECK NORMAL. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWEDJan 11, 2024 · N326UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024012382163Cap · crackedFAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR). REMOVE THE DAMAGE AREA (L:0.2", W:0.1 , 5" FROM AFTER EDGE AT LOWER EDGE) AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURE AT 200°F FOR 220 MINUTES KEEP A MINIMUM VACUUM OF 22 IN/HG I.A.W. UPSJan 11, 2024 · N326UP · Boeing 76734AF · Trailing Edge Flaps
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