Boeing 767-33AER
Service difficulty reports · 288
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 = '76733AER' 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 = '76733AER' 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 UIEA2016062700506Screw · corrodedENGINE NR 2 ON THE UPPER IGNITION BOX, THE PLUGS SCREWS ARE CORRODED. ENGINE NR 2 ON THE UPPER IGNITION BOX THE PLUGS SCREWS WERE CLEANED FORM CORROSION IAW SWPM 20-60-01.SDR UIEA2016062700504Nut Plate · missingENGINE NR 2 RT C-DUCT UPPER SKIRT FAIRING NUT PLATE MISSING. INSTALLED NEW NUT PLATE IAW SRM 51-40-02.SDR UIEA2016062700503Seal · tornENGINE NR 2 IN THE INTERMEDIATE CASE ON THE BLADE, SEAL IS TORN. PERFORMED SEALANT ON THE ENGINE NR 2 IN THE INTERMEDIATE CASE BLADES IAW AMM 51-31-00.SDR UIEA2016062700502Seal · tornNR 2 ENGINE RT FAN UPPER SIDE SEAL TORN. REPLACED SEAL IAW AMM 51-40-02.SDR UIEA2016062700501Rivet · damagedENGINE NR 1 RT C-DUCT AFT INTERNAL PART, SUNK RIVETS. RIVETS REPLACED IAW SRM 51-40-02.SDR UIEA2016062700499Rivet · damagedENGINE NR 2 C-DUCT LT AND RT AFT INTERNAL PART, SUNK RIVETS. DRILLED OUT DAMAGED RIVETS AND INSTALLED NEW RIVETS IAW SRM 51-40-02.SDR UIEA2016062700498Plug · corrodedENGINE NR 1, NR 2 PLUGS ON THE IGNITION BOX ARE CORRODED. ENGINE NR 1, NR 2 PLUGS ON THE IGNITION BOX WERE CLEANED OF CORROSION IAW SWPM 20-60-01.SDR UIEA2016062700497Bracket · damagedENGINE NR 2 RT CORE COWL BRACKET. STOW PIN OF HOLD OPEN ROD DAMAGE BRACKET. ADAPTER REPLACED AMM 71-11-11.SDR UIEA2016062700496Cowling · damagedENGINE NR 2 LT CORE COWL SUPPORT ROD DAMAGED. LT CORE COWL REPLACED.SDR UIEA2016062700495Cowling · chafedENGINE NR 2 LT CORE COWL AFT BRACKET OF HOLD OPEN ROD CHAFING. ENGINE NR 2 REPLACE CORE COWL IAW AMM 71-11-06.SDR UIEA2016062700494Duct · dentedNR 1 ENGINE DENT FOUND IN THE TOP SIDE OF THE LT C-DUCT RAIL. C-DUCT REPLACED, NRC M0150 REPLACEMENT.SDR UIEA2016062700493Protector · peelingENGINE NR 2 RT FAN COWL-MID OTBD PART DIVISOR MATERIAL. CHECK FAN COWL FWD L/E FOUND EDGE PROTECTOR PEELING OFF, BONDED EDGE PROTECTOR USING EA 9394 ADHESIVE PASTE IAW CMM 71-13-22.SDR UIEA2016062700492Lock · corrodedENGINE NR 1 CORROSION FOUND ON THE RT C-DUCT LOCK. CORROSION CLEANED AND TREATED ACCY TO AMM 51-05-03.SDR UIEA2016062700491Cowling · damagedENGINE NR 2 RT FAN COWL FWD AND AFT PART MISSING MATERIAL. PERFORMED FILLER AND GRAPHITE AND FIBERGLASS PLIES REPAIR ON FAN COWL. INNER SURFACE BOTH CORNERS IAW SRM 54-22-01.SDR UIEA2016062700511Housing · corrodedAPU SURGE VALVE HOUSING CORRODED. REPLACED HOUSING IAW AMM 49-53-06.SDR UIEA2016062700507Wire Harness · contaminatedNR 2 ENGINE FAN AREA ELECTRICAL HARNESS DIRTY WITH OIL. CLEANED IAW AMM 72-00-00.SDR UIEA2016062700509Nut Plate · damagedPYLON NR 1 RIGHT CORE COWL AREA LOWER PART, NUT PLATE INSTALLED. REMOVED DAMAGED NUT PLATE AND INSTALLED NEW NUT PLATE IAW SRM 51-40-02.SDR UIEA2016062700510Strip · corrodedENGINE NR 1 RT CORE COWL UPPER STRIP STRUCTURE CORRODED. CORRODED PART REMOVED AND NEW WEAR STRIP, PN 224-2301-122 WAS INSTALLED USING RIVETS IAW SRM 51-40-02.SDR HALA2015052400097Warning Light · false activationDURING DESCENT, LT ENGINE EEC MODE EICAS ILLUMINATED, ADHERED TO QRH PROCEDURES AND CHECKLIST AND LT ALT ILLUMINATED, ALSO, LIGHT NOT ILLUMINATED AFTER QRH. ACCOMPLISHED FIM 73-21-826 AND NO FAULTS NOTED; RAN ENGINE IAW AMM71-00-00 AND NO EICAS MESSAGE.SDR HALA2015030700030Actuator · leakingETOPS SIGNIFICANT SYSTEM, CENTER HYD QTY LOW ON ARRIVAL .55 RF STARTED FLT WITH 1.05. FOUND UPPER RUDDER PCA LEAKING. R & R RUDDER PCA IAW AMM 27-21-02-001, AMM 27-21-02-422-038 LEAK, OPS CHECK OK.SDR HALA2015011800010Window · failedSHORTLY AFTER LEVEL OFF AT FL340 HEARD A LOUD "BOOM". NOTICED F/O WINDSHIELD SHATTERED. AN UNEVENTFUL LANDING WAS MADE. R & R RT FWD WINDOW IAW AMM 56-11-01-401, OPS CHECKED OK. R & R RT FWD & LT SIDE WINDOW HEAT CONTROLLER CHECKED GOOD.SDR HALA2015010700005Warning Message · false activationEICAS MESSAGE FWD EQPT VAL ILLUMINATED AFTER ENGINE START REMAINED ILLUMINATED FOR 3 MIN, OPS NORMAL REMAINDER OF FLIGHT. ACCOMPLISHED AMM TASK 21-58-00 TEST SUCCESSFUL, NOTED NORMAL OPERATIONS OF FWD EQUIPMENT COOLING SYS EICAS MSG EXTINGUISHED, OK TO CONTINSDR HALA2015010100001Warning Message · false activationAFTER START WITH APU OFF, WHEN ADVANCING ENGINE POWER FOR TAXI, RT PACK OFF EICAS MESSAGE DISPLAYED. UNABLE TO CLEAR WITH QRH PROCEDURE. BITE CHECK, FOUND NO FAULTS, RESET CONTROLLER, RAN ENGINE WITH PAX ON SYSTEM CHECKED OK.SDR RYNA2013012200002Pump · failedLEFT AFT BOOST PUMP FAILED INFLIGHT. PLACED ON MEL 28-22-1 CAT C DDD 1 FEB 2013. ISSUED DMI 3025. SUPPLEMENTAL REPORT TO FOLLOW.SDR RYNA2013012100001Scavenge Pump · leakingNR 1 ENGINE OIL SCAVENGE PUMP LEAKING. REPLACED OIL SCAVENGE PUMP IAW AMM 79-21-00 P 401. OPERATIONAL AND LEAK CHECK NORMAL. INSPECTED MASTER CHIP DETECTOR PER AMM 79-21-10.SDR HALA2012121000232Unknown · unknownFMC LIGHT ON, BUT NO MESSAGE IN SCRATCH PAD. DISCOVERED TOTALIZER QTY ON PROGRESS PAGE 2 MISSING FUEL PANEL TOTALIZER, OPS NORMAL. FURTHER INVESTIGATION SHOWED PERF INIT PAGE FUEL MANUAL. PERFORMED FMC SYS OPS CK ON LT AND RT FMC'S IAW AMM 34-61-00, BOTH PASSDR HALA2012120400234Channel · crackedNR 2 ENGINE STRUT HAS CRACKED CHANNEL ON AFT WEB OF LOWER FACED FAIRING. REPLACEMENT CHANNEL FABRICATED AND INSTALLED.SDR RYNA201211260040Door · bentON POSTFLIGHT NOTICED RIGHT MAIN GEAR TRUNNION PANEL (DOOR) BENT. ACCOMPLISHED TEMP (INTERIM) REPAIR IAW DER ENGINEERING DRAWING 52-12548-1, 8110-3 APPROVAL DATED 22 NOV 2012. REPETITIVE INSPECTIONS AT A CHECK INTERVALS AND PERMANENT REPAIR AT C CHECK.SDR RYNA201210280039Wire Harness · brokenWIRE HARNESS BROKEN FROM EMERGENCY TRACK LIGHTING TO BATTERY PACK AT SEAT ROW 21GH. REMOVED AND REPLACED LUMINESCENT SYSTEM WIRE HARNESS FROM EMERGENCY TRACK LIGHTING TO BATTERY PACK REF CMM 33-50-01. OPERATIONAL CHECKED NORMAL.SDR RYNA201210020038Adc · failedDUAL AIR DATA COMPUTER FAILURE. RETURNED TO LAND AT RFD. REMOVED AND REPLACED LEFT AND RIGHT AIR DATA COMPUTERS PER AMM 34-12-01. PERFORMED HIGH LEVEL LEAK CHECK PER AMM 34-11-00. BOTH LEFT AND RIGHT PITOT STATIC SYSTEMS CHECKED NORMAL AND VERIFIED ACCURACSDR HALA2012100100216Stringer Clip · misinstalledSTRINGER 8L CLIP BS 1678 ,FOUND WITH FOUR RIVETS NOT INSTALLED SINCE MFG, PILOT HOLES IN CLIP, NO HOLES IN STRINGER). FOUR NEW FASTENERS INSTALLED IAW SRM 51-40-02 D63T210, REV 90, REF S/O 52109681 SKIN CRACKS COULD BE RESULT OF THESE FASTENERS MISSING.SDR RYNA201208280034Hydraulic Line · chafedFOUND PRESSURE LINE IN NUMBER ONE PYLON THAT HAD CHAFED AGAINST AN CLAMP. INSTALLED TEMPORARY LINE PAR GMM VOL 6 , CHAPTER 29RY01. INSTALLED PERMANENT TUBE (LINE) PER SRM 20-10-09. LEAK CHECKED NORMAL. CLEARED EMI-2, REMOVED PLACARD.SDR RYNA201208210033Wire · damagedFLIGHT CREW CALLED MAINTENANCE CONTROL AND REPORTED THAT THE LEFT CENTER BOOST PUMP HAS FAILED RESULTING IN AIR TURNBACK TO CMN. REMOVED AND REPLACED WIRING TO LEFT CENTER FUEL PUMP FROM LEFT LANDING GEAR PLUG D5558J TO D2805 AT PUMP. OPS CHECK NORMAL PER ASDR HALA2012072900187Switch · looseAPU FAILED TO START ON GROUND. FOUND APU START SWITCH VERY LOOSE, CAN NOT SELECT PROPER START POSITION, SECURED START SWITCH. STARTED NORMAL IAW AMM 49-21-00.SDR HALA2012070900169Starter · failedDURING LT ENGINE START N2 ACCEL TO 18 PERCENT AND THEN ROLLED BACK TO ZERO PNEU PRESS WAS 30 PSI NEVER TURNED ON FUEL. R & R LT ENG STARTER IAW AMM 80-11-01. R & R LT ENG START VALVE IAW AMM 80-11-02. OPS AND LEAK CHECK GOOD.SDR RYNA201207070029Warning System · malfunctionedON A/C POWER UP STATUS MSG FWD CARGO FIRE DETECT 1 WILL NOT CLEAR. PLACED ON MEL 25-20-1. SUPPLEMENTAL REPORT TO FOLLOW.SDR HALA2012070200164Controller · malfunctionedLEFT PACK TEMP EICAS, LEFT PACK OFF. REMOVED, CLEANED AND INSTALLED COMPRESOR OVERHEAT SENSOR, RESET LEFT PACK CONTROLLER, PERFORMED OPS CHECKED NORMAL, OK FOR SERVICE IAW AMM 21-51-00.SDR RYNA201206260028Smoke Detector · defectiveAFT LEFT LAVATORY SMOKE DETECTOR DEFECTIVE. REMOVED AND REPLACED L-4 (AFT LEFT) LAVATORY SMOKE DETECTOR. REFERENCE AMM 26-13-01.SDR RYNA201205160025Housing · failedON CLIMBOUT 11,000 FT, NR 2 ENGINE OIL PRESSURE STARTED DECREASING, AT 74 PERCENT PER CPM SHUT DOWN ENGINE (PRECAUTIONARY) RETURNED TO LEJ. PERFORMED DETAILED VISUAL INSPECTION OF NR 2 ENGINE FOUND 2 STUDS ON MAIN ENGINE OIL FILTER HOUSING FAILED. INSPECTED SDR RYNA201202170009Slide · dislodgedL1 DOOR SLIDE ASSY DISENGAGED FROM DOOR WHEN DOOR OPENED BY CREW. INSPECTED AND INSTALLED L1 DOOR SLIDE IAW AMM 25-66-01. SLIDE DID NOT DEPLOY.SDR RYNA201201230007Skin · corrodedAFT CARGO COMPARTMENT, STA 1130 BL 0.0 SKIN CORROSION. REMOVED AREA OF CORROSION AT STA 1100 PER AMM 51-10-02, TYPICAL EXTERNAL DOUBLER REPAIR REQUIRED. CARRIED OUT EXTERNAL DOUBLER REPAIR IAW 767 SRM 53-00-01. APPLIED DECORATIVE FINISH ON EXTERNAL REPAIR DSDR HALA2011120600568Test Panel · failedSQUIB TEST 2 (AFT) CARGO 1 FAIL INTERMITTENT. REPLACED SQUIB TEST PANEL & OPS CHECKED OK IAW AMM 26-21-04.SDR HALA2011120600567Test Panel · failedETOPS SIGNIFICANT SYS - SQUIB TEST 2 (AFT) CARGO 1 FAILED INTERMITTENTLY. REPLACED SQUIB TEST PANEL & OPS CHECKED OK IAW AMM 26-21-04.SDR HALA2011120500569Unknown · unknownETOPS SIGNIFICANT SYSTEM - EICAS MESSAGE - LT AUX PITOT. RESECURED D1012 TO B29, OPS CHECKED OK IAW AMM 30-31-00.SDR HALA2011111700528Transducer · malfunctionedON SELECTING FLAPS TO 5 A T/E FLAP DISAGREE ICAS WARNING LIGHT ILLUMINATED. PERFORMED CHECKLIST AND LANDED WITH FLAP HANDLE IN 20 DEGS DETENT. LEFT CONFIGURATION AS IS NO T/E FLAP WERE OUT AT GATE ARRIVAL. FOUND NR 8 ROTARY ACTUATOR TORQUE LIMITER INDICATORSDR HALA2011111700529Radar · no testETOPS SIGNIFICANT SYS - RT WEATHER RADAR SYS FAILED DURING TEST. RESET WEATHER RADAR SYS. GROUND OPS CHECKED OK.SDR HALA2011111600530Controller · inoperativeETOPS SIGNIFICANT SYS - RT PACK INOPERATIVE LIGHT ON. REPLACED RT PACK TEMP CONTROLLER IAW AMM TASK 21-51-14 BITE CK OK.SDR HALA2011111500522Structure · damagedNR 2 ENGINE PYLON STRUCTURE FOUND CRACKED AND DAMAGED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500521Module · malfunctionedON APPROACH, FLAPS SELECTED FROM 1 TO 5, INDICATOR STAYED AT FLAPS 1 AND TE FLAP DISAGREE LIGHT CAME ON. CHECKED HANDLE IN DETENT AND MOVES HANDLE BACK TO FLAP 1 THEN FLAP 5 AGAIN - NO HELP. USED ALTERNATE FLAP SYS TO EXTEND FLAPS TO 20 FOR LANDING. OPS NORSDR HALA2011110600505A/C Pack · malfunctionedETOPS SIGNIFICANT SYS - PACK INOPERATIVE LIGHT WITH PACK WORKING. RESET PACK COULD FIND NO FAULT OPS CHECKED NORMAL IAW MM 21-00-00-862 AND FIM 21-51-00 1.
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