Boeing 767-322
Service difficulty reports · 11,764
Newest first. General aviation reporting is voluntary.
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 = '767322' 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.
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 = '767322' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UALA2012101705921Skin · damagedUNDER PAINT TOOLING BLENDOUT AT STR 2 RIGHT NEXT TO THE TCAS ANTENNA. EVALUATED DAMAGE & FOUND MATERIAL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE & ACP HFEC REF NDT MAN 51-00-19. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS REPAIR REF SRM 53-0SDR UALA2012101805974Skin · damagedUNDER PAINT TOOLING BLENDOUT AT STR 2 RIGHT NEXT TO THE TCAS ANTENNA. EVALUATED DAMAGE & FOUND MATERIAL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE & ACP HFEC REF NDT MAN 51-00-19. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS REPAIR REF SRM 53-0SDR UALA2012101705923Skin · dentedBULK CARGO DOOR DENTED ON EXTERNAL SKIN. DENT IS ON A PREVIOUS REPAIR DOUBLER. FABRICATED AND REPLACED THE REPAIR DOUBLER PER SRM 52-30-01, REPAIR 6.SDR UALA2012101705920Skin · crackedEXTERIOR FUSELAGE LOWER SKIN LEFT SIDE DENTED, BS 610 - BS 632, STR 32L - STR 33L. EVALUATED DENT & FOUND CRACKED OUTER SKIN. CUT OUT DAMAGE & ACP NDT OF CUT-OUT REF NDT MAN 51-00-19. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF SRM 53-00-01.SDR UALA2012101605911Computer · failedAUTOLAND AP PUMPED THE YOKE WHEN FLARE MODE ENGAGED. MCDP TEST 40 SHOW TLA R FAIL. REPLACE TMC. OP CHECK GOOD CAT 3 CHECK REF AMM. AC RETURNED TO CAT 3.SDR UALA2012101505826Shutoff Valve · faultyUNWANTED FUEL XFER.DUE TO CHRONIC HISTORY OF UNWANTED FUEL TRANSFER FROM CENTER TANK TO LEFT MAIN TANK, ACCOMPLISH FIM TASK PER MM. WITH FUEL IN CENTER TANK AND OVERRIDE PUMPS OPERATING, CHECK CENTER TANK AREA FOR EXTERNAL LEAKS. RAN OVERRIDE PUMPS WITH 2500SDR UALA2012101605910Yaw Damper · faultyLEFT YAW DAMPER INOPERATIVE. TROUBLESHOT TO BAD LEFT YAW DAMP MODUAL REPLACE SAME AS PER AMM. OPS CHECKS NORMAL. AC REMAINS CAT FULL CAPABLE. INSTALLED BORROWED PART PN 99-222 1-9-0001 SN 0937 MG PN 285T0013-123.SDR UALA2012101805950Processor · faultyAFTER 2 HOURS LEFT FUEL GAUGE 40.3 RT 39.3 WITH CNTR PUMPS ON FUEL FLOWS WITHIN 100 LBS. AS PER TOMC REQUEST REPLACED FUEL QTY PROCESSOR PER MM 28-41-08, NO FAULTS NOTED. PERFORMED SELF TEST ALL TESTS PASSED. OPS CHECKS GOOD AT THIS TIME.SDR UALA2012101805949Processor · faultyCONTINUED AFTER REBALANCING DOWN 1000 LBS ON RIGHT SIDE AFTER 2HRS WITH CNTR PUMPS OFF. AS PER TOMC REQUEST REPLACED FUEL PROCCESSOR UNIT PER MM 28-41-08. NO FAULTS NOTED. PERFORMED SELF TEST. ALL TESTS PASSED, OPS CHECKS GOOD AT THIS TIME.SDR UALA2012101605903Control Rod · brokenNR 7 LEADING EDGE SLAT CONTROL ROD BROKEN AND PROTRUDING OUT WITH SLAT IN THE UP POSITION, FOUND ON ARRIVAL. REPLACED NR 7 L/E SLAT CONTROL ROD AND OPS CHECKED GOOD.SDR UALA2012101505842Unknown · odorELECTRICAL ODOR IN COCKPIT, FLIGHT DIVERTED. LEFT SIDE OF FLT DECK IN FLT AND NO ODOR PRESENT ON GROUND, WITH NO DEFECTS FOUND AFTER EXTENSIVE INSPECTION. ACCOMPLISHED TEST FLT WITH EG CREW TO DIAGNOSE SOURCE OR CONFIRM NO ODOR PRESENT. OPERATE ACFT FOR 1 HSDR UALA2012101505873Battery · dischargedON WALKAROUND FOUND MAIN AIRCRAFT BATTERY DEAD. REMOVED AND REPLACED MAIN AIRCRAFT BATTERY PER AMM AND BATTERY CHARGER PER AMM, OPS CHECK GOOD.SDR UALA2012101505863Line · leakingLEFT HYD QTY EICAS INFLIGHT WITH RF 0.48. FOUND HYD LINE IN LEFT SAIL TAIL LEAKING. INSTALLED NEW LINE AND OPS CHECKED. NO LEAKS.SDR UALA2012101605885Smoke Goggles · damagedFIRST OFFICER GOGGLES ELASTIC STRAP IS STRETCHED OUT NEEDS REPLACING. REPLACED GOGGLES.SDR UALA2012101205821Fuel Line · leakingNR 2 ENGINE FUEL LEAK. DISCONNECTED THE NR 2 ENGINE FUEL LINE BETWEEN THE FUEL PUMP AND THE FUEL-OIL HEAT EXCHANGER DUE TO LEAK. REPLACED FUEL LINE BETWEEN FUEL PUMP PAD AND FUEL OIL HEAT EXCHANGER AS PER MM. ACCOMPLISHED LEAK CHECK AND REPAIRED LEAKING FUESDR UALA2012101205822Symbol Generator · faultyWITH F/O EFI PUSHED IN ALT, THE COMPARATOR FLAG ON F/O EADI BLINKING ON AND OFF AND GPWS EICAS AND TERRAIN SYSTEM STATUS MSG WAS BLINKING ALSO. THEN F/O EADI AND EHS I WENT BLANK AND STAYED BLANKED, UNTIL THE EFI SW WAS PUT BACK TO NORMAL. FOUND CTR SYMBOL GSDR UALA2012101105790Probe · faultyA-C RETURNED TO BLOCKS FOR :L AUX PITOT EICAS MSG AND ANNUNCIATOR LT FOR SAME. VERIFIED CB NOT POPPED AND L AUX PITOT DOES NOT OPERATE WHEN TEST SW ACTUATED. REPLACED LEFT AUX PITOT PROBE, OP CHECKS NORMAL, LEAK CHECKS WITHIN LIMITS PER MM.SDR UALA2012101205816Pressure Switch · faultyCREW REPORTED RUDDER RATIO LIGHT AND EICAS MESSAGE. TROUBLESHOT IAW FIM TASK 27-21-00 FIG 104. REPLACED LEFT ELECTRICAL HYD PUMP CONTROL PRESSURE SWITCH S27 IAW AMM. 'HYD SWITCH' FAULT CLEARED ON RIGHT YAW DAMP MODULE. 'RUDDER RATIO' LIGHT AND EICAS MESSAGSDR UALA2012101105799Pressure Switch · no testLEFT CENTER FUEL TANK PUMP DOES NOT TEST PROPERLY. TROUBLESHOT PROBLEM TO S424 PRESSURE SWITCH. REPLACED SWITCH AND TESTED PER AMM. TESTED NORMAL.SDR UALA2012101105798Light · damagedEMERGENCY EXIT LIGHT ON SEAT 6AB DAMAGED. REPLACED LIGHT, OPS CHECKED OKAY.SDR UALA2012100905725Connector · burnedC/B POPPED LAV SYSTEM LIGHTS. T/S LAV LIGHT AND SMOKE DETECTOR POPPING OF C/B. REPLACED CONN D7652P AND J SIDE DUE TO BURNT PINS IAW WDM. VERIFIED WIRES TO BE IN GOOD CONDITION PER SWP 20. REPLACED CR1 DIODES AT TB2 FOR FWD RIGHT LAV AND AFT RIGHT LAV. ALSDR UALA2012100905727Light · defectiveF/O INST PANEL FLOOD LIGHTS WON`T LIGHT OR DIM WITH CONT KNOB. LIGHTS DO NOT ILLUM BRT WITH LGT OVRD SWITCH ON. REPLACED ASSY PER WS WD 33-11-11 AND OPS NORMAL.SDR UALA2012101005743Floorbeam · corrodedMAIN CABIN FLOORBEAM AT STA 852 AT RBL 74.81 UPPER SURFACE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: CORROSION IS OUT LIMITS IAW SRM 53-00-51, PG 102. FABRICATED & INSTALLED T-CHORD, FILLER & SPLICE ANGLE IAW SRM 53-00-51, REPAIR 3.SDR UALA2012101005742Shear Tie · corrodedAFT CARGO COMPARTMENT BILGE, SHEAR TIE CORRODED BS 1395 - 1396, STR 39L - 39R. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.SDR UALA2012101005741Shear Tie · corrodedAFT FUSELAGE LOWER INTERNAL BILGE AREA WEB TIES CORRODED AT SEVERAL AREAS BS 1540, STR 36R - STR 39R. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION ON SHEAR TIE STA 1540 BETWEEN STR 39R-38R, ARE OUT OF LIMITS. INST 3EA NEW SHEAR TIES STA 1540, STR 36R-39R IASDR UALA2012101005740Structure · dentedBULK CARGO DOOR FWD LOWER CORNER HAS 6 EA DENTS 1" TO 5.5" FROM FWD EDGE, 1.5" TO 6.25" FROM BOTTOM EDGE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01, DET VI NOTE J. REPAIRED IAW SRM 52-30 -01, FIG 201. THIS REPAIR IS CATEGORY A.SDR UALA2012100905719Printer · inoperativeACARS PRINTER INOP. REPLACED COCKPIT PRINTER, OPS CHECKED NORMAL.SDR UALA2012100805665Idg · lowNR 1 ENG GEN EICAS MSG, DISCONNECTED IDG PER FM PROCEDURES. SERVICED LESS THAN 1 QRT IN 1 IDG. RECONNECTED IDG AND OPERATED 1 ENG. PUT FULL ELEC LOAD ON 1 GEN. GEN CHECKS GOOD. PERFORMED LEAK CHECK OF IDG. NO LEAKS NOTED. PERFORMED PBCU BITE. NO FAULTS FSDR UALA2012100805701Slide · faultyCHECK RIGHT OFF WING SLIDE OP. ACCOMPLISH OPERATIONAL CHECK OF THE RIGHT OFF WING ESCAPE SLIDE, PCN 649-9124 MR25722, PER MM. SLIDE DID NOT DEPLOY PROPERLY.SDR UALA2012100805674Skin · corrodedRIGHT WING INBOARD AFT FLAP, UPPER SKIN TRAILING EDGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED RT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 2EA AREAS BY BONDING FILLER SKINS & DOUBLERS IAW SRM 57-53-01 & 57-70-10. SEALED DOUBLERS IAW SRM 51-20-05 & BAC SDR UALA2012100805673Skin · corrodedLEFT WING INBOARD AFT FLAP UPPER TRAILING EDGE SURFACE HAS CORROSION. REPAIRED LEFT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 7EA AREAS BY BONDING SKIN FILLERS & DOUBLERS IAW SRM. SEALED DOUBLERS IAW BAC DRG 113T2320 & SRM 51-20-05, PREPPED AND PAINTED AREASSDR UALA2012100805672Skin · corrodedRIGHT WING INBOARD AFT FLAP, UPPER SKIN O/B TRAILING EDGE CORRODED IN SEVERAL AREAS. REPAIRED RT WING INBOARD AFT FLAP TRAILING EDGE 2EA AREAS UPPER SKIN BY BONDING FILLER SKIN & DOUBLERS IAW SRM 57-53-01 & 51-70-10. SEALED DOUBLERS IAW SRM 51-20-05 & BAC DSDR UALA2012100805676Skin · damagedRIGHT WING INBOARD AFT FLAP, LOWER TRAILING EDGE SKIN HAS 5 INCH CREASE. RECEIVED DAMAGE AT RIGHT WING INBOARD AFT FLAP LOWER T/E SKIN 83 INCHES FROM OTBD END IAW SRM 57-53-01 & 51-70 -10 REPAIR BY BONDING SKIN & DOUBLER IAW SRM 57-53-01 & 51-70-10. REPAIR RSDR UALA2012100805675Skin · damagedRIGHT WING INBOARD AFT FLAP, LOWER SKIN INBOARD SIDE DENTED IN SEVERAL AREAS. REMOVED DAMAGE ON DENTS, FABRICATED REPAIR PARTS, BONDED REPAIRS AND CURED, AND APPLIED CONDUCTIVE COATING IAW SRM 57-53-01 & 51-70-10 & 57-70-05, PREP AND PAINTED AREAS IAW GPM 5-0SDR UALA2012100505645Lug · defectiveGROUND LUG FOR NR 2 ENGINE IDG SHOW BROKEN STRANDS OF WIRE BEFORE LUG CRIMP. INSTALLED AND CRIMPED NEW LUG, HARNESS NEEDS TO BE SECURED. SECURED HARNESS.SDR UALA2012100405631Pump · faultyAS PREVIOUS MRM FUEL CONFIG LIGHT ON 3 HOURS INTO FLIGHT WITH 1400LBS MORE FUEL IN LEFT WING TANK. REMOVED AND REPLACED CENTER RIGHT OVERRIDE PUMP IAW AMM, NO LEAKS NOTED.SDR UALA2012100305616Engine · vibrationNR 1 ENGINE VIBRATION. REPLACED NR 1 ENGINE MAIN OIL SCREEN. NO METAL FOUND.SDR UALA2012100405629Drive Unit · failedWX FAIL DISPLAYED ON NO. HSI(S). WXR TEST INOP. (1=CAPT, 2=1ST OFF, 3=BOTH). WX RADAR FAILED DISPLAY ONLY COLOR TEST BAND ARC TESTED OK ON GROUND. ACCOMPLISH CHRONIC REVIEW. REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE AS PER MM, OPS CHECK GOOD.SDR UALA2012100405630Drain · leakingPUSH CREW REPORTS FUEL LEAK NR 2 ENGINE AFTER PUMPS TURNED ON. FOUND FUEL LEAKING FROM DRAIN NR 4. CREW RAN ENGINE FOR THREE MINUTES. INSPECTED DRAIN, NO FURTHER LEAK EVIDENT OK TO CONTINUE.SDR UALA2012100405628Drive Assy · failedWXR FAIL DISPLAYED ON HSI. WXR FAIL ANT DISPLAYED ON HSI IN WXR TEST POS. REMOVED AND REPLACED WX ANT DRIVE ASSY, OPS CHECK GOOD.SDR UALA2012100405637Light · out of positionEMERGENCY EXIT LIGHT STRIP PULLED OFF SEAT 1B. REPLACED EEL STRIP ON SEAT 1B, LIGHT OPS CHECKS OKAY.SDR UALA2012100305613Indicator · out of limitsL-4 DOOR LOAD LIMITER INDICATOR NUT OUT OF LIMITS, MORE THAN 1-8TH INCH FROM HOUSING. REMOVED AND REPLACED LOAD LIMITER PER B767 AMM 52-11-21 TASK 52-11-21-002-005 & TASK 52-1 1-21-402-003 REF NR 20028.SDR UALA2012100305612Indicator · out of limitsL-1 DOOR LOAD LIMITER INDICATOR NUT OUT OF LIMITS, MORE THAN 1-8TH INCH FROM HOUSING. REPLACE L1 DOOR LOAD LIMITER IAW MM, NR 20027.SDR UALA2012100205581Engine · malfunctionedEICAS MSG RIGHT GEN OFF DISPLAYED. DURING NR 2 ENGINE RUN, AFTER STARTER CUTOUT OIL PRESSURE BEGAN DROPPING AND RIGHT OIL PRESS LIGHT CAME ON. EGT RISES, FUEL FLOW NORMAL. FOUND METAL IN TAILPIPE AND OIL LEAKING. CREW COMMENTS: LOST ON TAKEOFF AT 110 KIAS.SDR UALA2012100405632Actuator · failed"AIL LOCK" LT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - UNLOCKED, BOTH. CREW COMMENTS: 290 KNOTS AT 13,000FT,TEMP -8, THE RT SAM HAD AN ADC AND A LT AILERON LOCKOUT ACTUATOR FAULTBALL. BOTH DID RESET. SDR UALA2012100305607Light · brokenEEL LIGHT ASSY BROKEN OFF AT SEATS 01H AND 02H. REPLACED LIGHT ASSY, OPS OK.SDR UALA2012100205573Starter · faultyAPU WILL NOT START EGT 715 & RPM 25 THEN SHUT DOWN PERFORMED BITE CHECK AND SHOWS NO ACCELL LAST 2 START ATTEMPTS WITH PT SENSOR. SEE 49-11-00 FOR T/S INFO. TESTED HYD GEN PER MM. REPLACED STARTER AND APU STARTED NORMAL.SDR UALA2012100305599Light · missingCABIN FIRST CLASS SEAT 1B EEL LIGHT ASSY MISSING. REPLACED LIGHT, CHECKS OK.SDR UALA2012100205587Connector · unsecureCABIN EEL LIGHTS INOP FROM ROWS 25H TO 31. SECURED CONNECTOR UNDER SEAT 31HJ, CHECKS OKAY.SDR UALA2012100205578Sensor · faultyFUEL TEMP INDICATION ON FUEL PANEL BLANK. REPLACED FUEL TEMP SENSOR TS168, OPS NORMAL.
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