Boeing 767-32LF
Service difficulty reports · 74
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 = '76732LF' 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 = '76732LF' 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 FDEA202002080299Fault Message · false activationMDIS 297 34-61 3894 08FEB20 MEM FACT U. PER CREW VERBAL: DURING APPROACH A/C FULLY CONFIGURED FLAPS 30, VREF FOR THE LANDING WEIGHT OF 302.3 WAS COMPUTING 141 KTS. AT THIS AIRSPEED THE STALL ZIPPER WAS ABOVE THE VREF SPEED APPROXIMATELY 7-8 KNOTS. THE HUD SDR FDEA2020021080290Stick Shaker · inoperative"WARN ELEX" ON STATUS PAGE DURING PREFLIGHT TROUBLESHOOTING PER B767 FIM 27-32 FT803, WITH IRU'S ALIGNED THE WARN ELEX MSG CLEARS BUT PER BLK 2 WHEN THE LEFT STALL WARNING SWITCH IS TOGGLED THERE IS NO STICK SHACKER AND "WARN ELEX" APPEARS ON THE STATUSSDR FDEA201905261163Unknown · malfunctionedSPOILER DID NOT DEPLOY AT TOUCHDOWN AUTOMATICALLY. HAD TO MANUALLY DEPLOY. FACT 28MAY19 01:56 TPA PERFORMED AUTO SPEEDBRAKE OPERATIONAL TEST AND ALL FUNCTIONS PASSED. ALSO INTERROATED BOTH YSM'S (LEFT AND RIGHT) NO FAULTS OR HISTORY NOTED. PER FIM 27-62 00-SDR FDEA201903090563Window · arcedL SIDE NR 2 WINDOW OVERHEAT WITH ARCING DELAMINATION AND CRACKING. FACT 10MAR19 04:42 DEN REMOVED AND REPLACED LEFT WINDOW NR 2 REF AMM 56-11-02-4. WINDOW OPS CHECKS GOOD REF AMM 56-11-02 AND WINDOW ANTI-ICING OPS CHECKS GOOD REF AMM 30-41-00. A/C OK FOR SDR FDEA2019022870507Controller · failedPDIS 298 21-30 2907 26FEB19 LAX FACT U LOGPAGES:3042464 ON CLIMBOUT RECEIVED " CABIN ALTITUDE " WARNING LEVELED OFF ALERT WENT AWAY , AIRCRAFT PRESSURIZED TO BELOW SEA LEVEL AND BEYOND MAX DIFFERENTIAL PRESSURE . AIR TURN BACK FACT 26FEB1SDR FDEA201901020008Wheel · damagedNR 5 TIRE WORN. UPON REMOVAL FOUND INNER HALF OF WHEEL TO BE DAMAGED FROM CONTACTING BRAKE ASSEMBLY. REMOVED AND REPLACED NR 5 WHEEL AND TIRE ASSEMBLY. REFERENCE AMM 32-45-01-4. (NOTE NR 5 BRAKE WAS FOUND TO HAVE A LOOSE OUTER AXLE BUSHING.)SDR FDEA2019010113625Bushing · wornNOTED NR 5 WHEEL INNER SURFACE APPEARS TO BE CONTACTING OUTER BRAKE SURFACE. UPON REMOVAL OF TIRE AND BRAKE ASSEMBLY, FOUND BRAKE AXLE BUSHING WORN ALLOWING CONTACT BETWEEN WHEEL AND BRAKE. REMOVED AND REPLACED NR 5 BRAKE ASSEMBLY. REFERENCE AMM 32-41-08-4-4. SDR FDEA201812273612Proximity Sensor · failedAT CRUISE, FL 380 GOT MAIN CARGO DOOR MESSAGE. RAN QRH, SET LANDING ALT TO 9500'. THE AIRPLANE HELD PRESSURE ALL THROUGH DESCENT. DESCENDING THROUGH FL 185, LIGHT WENT OUT BUT IT CAME BACK ON AT 9100'. IMMEDIATLY UPON TOUCHDOWN THE LIGHT WENT OUT BUT THE ACARSSDR FDEA2018120653439Sensor · failedPDIS 298 21-30 2688 05DEC18 MEM OPEN U LOGPAGES:2932480 AT FL 340, CABIN PRESSURE ALTITUDE WARNING. WENT ON CREW DONNED O2 MASK. DID RED TAB CABIN ALTITUDE LOSS - DESCENDED TO 10,000 FT AS AUTO CONTROLLER IN AUTO 1 AND 2 WOULD NOT RESPOND ANDSDR FDEA201811093168Pseu · faultyLE SLAT DISAGREE MSG RECEIVED AFTER MOVING FLAP HANDLE TO 1 ON APPROACH. COMPLIED WITH QRH PROCEDURES. REPLACED PSEU REF AMM 32-09-04-4, NO DEFECTS NOTED. PERFORMED SENSORS S287, S299 AND S305 TARGET TEST AT SLATS RET, T/O AND LDG REF AMM 27-81-00-3, NO DEFECTSDR FDEA2018082322150Skin · dentedRIGHT INBD FLAP TOP SURFACE WAS DENTED APPROX 39 INCHES FROM INBD EDGE, AND 6 INCHES FROM AFT EDGE. ACCOMPLISHED A REPAIR ON THE RTFLAP TOP SURFACE IAW SRM 57-53-01-01, AND SRM 51-70-10, REPAIR 2.SDR FDEA201804070907Skin · damagedRT WING INBD AFT FLAP LOWER EDGE COMPOSITE SKIN HAS MINOR DAMAGE, 51 INCHES AWAY FROM INBD END. REPAIRED THE RT WING AFT FLAP IAW SRM 51-70-10-2R, AND EA TH-5750-T0339275. MAJOR REPAIR.SDR FDEA201803310814Skin · dentedLEFT WING NR 4 SLAT DENTED ON THE TE WEDGE UPPER SKIN FROM OTBD BETWEEN 5 AND 8 INCHES. REPAIRED IAW SRM 51-70-10-2R, REP 2, SRM 57-43-02-02R, AND EA T-5750-T0339155 ,P1. MAJOR REPAIR.SDR FDEA201803300806Skin · dentedLEFT WING L/E SLAT HAS DENT ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 57 & 60 INCHES. REPAIRED IAW SRM 51-70-10, REPAIR 2, SRM 57-43-02-2R, AND EA H-5750-T0339161, P1. MAJOR REPAIR.SDR FDEA201803270789Skin · dentedRIGHT WING L/E NR 10 SLAT HAS DENTS ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 62 INCHES & 71 INCHES. REPAIRED THE SLAT IAW SRM 51-70-10-2R, REPAIR 2, MAJOR REPAIR.SDR FDEA201709292797Control Valve · failedALTERNATE SLAT INBD POWER CIRCUIT BREAKER FOUND TRIPPED, DURING FLIGHT DECK INSPECTION. REPLACED CONTROL VALVE MODULE ASSY IAW AMM 27-81-12-4 3.SDR FDEA201709132534Smoke Detector · false activationDURING PUSH BACK, AND ENGINE START, THE LAVATOPRY SMOKE DETECTOR STARTED GOING OFF. THE LED SHOWED RED AS ALARM SOUNDED. ALARM STOPPED AFTER ABOUT THREE MINUTES & LED LIGHT WAS GREEN. NO EVIDENCE OF SMOKE BUT LAVATORY HAD A FOUL ODOR. REMOVED AND REPLACED SDR FDEA201704211300Connector · defectiveON DEPARTURE CLIMBING THROUGH APPROXIMATE 2000 FT EICAS MESSAGE "FWD CARGO DOOR" DECLARED EMERGENCY. ACCOMPLISH QRH. RETURNED TO KEWR LANDED UNEVENTFULLY. REPLACED D6266J ON CARGO DOOR AND REPLACED D6266P REF WDM 52-71-13 PG 1 SHEET 2, REMOVED PSEU REF AMM 32SDR FDEA201702110524Tire · out of roundDURING TAKEOFF ROLL, ENCOUNTERED VERY NOTICABLE SHUDDER OF UNKNOWN ORIGIN. ABORTED TAKEOFF AT 100 KTS. JACKED NOSE GEAR AND FOUND BOTH NOSE TIRES OUT OF ROUND. IAW FIM 32-51 FT 805 FIGURE 104.SDR FDEA201610013406Skin · chafedRT WING I/B FLAP O/B END UPPER SURFACE HAS DEEP CHAFING MARK JUST ABOVE UPPER SEAL. REPAIRED RT WING IB FLAP OB END UPPER SURFACE IAW SRM 57-53-01-2R FIG 201 AND 51-70-05.SDR FDEA201609263366Skin · dentedFUSELAGE SKIN DENTED AT BS 1398 BETWEEN STRINGERS 34-35L. COMPLIED WITH EA H-5330-T0328464 P1. FABRICATED A REPAIR DOUBLER AND FILLER. INSTALLED REPAIR.SDR FDEA201609013098Duct · loosePASSING FL 220 AT 330 IAS IN CLIMB, A SUDDEN AND EXTREMELY LOUD HORN, SIREN OR WHISTLE CAME ON. LEVELED AT FL 260 AND SLOWED TO 300 KTS IAS. SOUNDS CONTINUED FOR ABOUT 10 MIN AND THEN SLOWLY DECREASED TO ZERO. F/O AND CAPT BOTH REPORTED NOISE WAS LOUD CONTINSDR FDEA201608222948Skin · damagedBIRD STRIKE DENTED THE LT FORWARD FUSELAGE AT STA 148.5, WL 215. DENT MEASURES 6.4" X 3.5" X 0.336". REPAIRED DAMAGE IAW SRM 53-00-01, FIG 201, TABLE 5 WHICH REQUIRES REPETITIVE INSPECTION. CONTACT MOCC AFTER 30K FLT CYCLE INSPECTION TO SET UP 12K FLT CYCLESDR FDEA201608112880Skin · damagedBIRD STRIKE IMPACT CAUSED DENT IN STRUCTURE APPROXIMATELY 17" AFT OF RADOME AND 8" BELOW THE LT TAT PROBE. INSPECTED IAW EA H-5310-T0327414A PERFORMED HFEC OF EXTERNAL SKIN SURFACE OF DENT. ALSO BORESCOPE INSPECTED INTERNAL STRUCTURE AT DENT AREA. COMPLIED W
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