N1709A
Service difficulty reports · 455
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N1709A' AND registry_match = 'registration' 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 n_number = 'N1709A' AND registry_match = 'registration' 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 UIEA2020060701230Warning System · false activationLT FWD WINDOW EICAS IN FLIGHT, REPEAT WRITE UP. PERFORMED FC WH ANTI-ICE OPS TEST AND WH ELEMENT LOOP RESISTANCE TEST IAW AMM 30-41-00-715-001 AND 30-41-00-765-046. OPS TEST NORMAL. PERFORMED FIM 30-41 TASK 801, NO DEFECTS FOUND AT THIS TIME.SDR UIEA2020060801220Warning System · false activationHI FLOW INHIBIT STATUS MESSAGE TRANSFERRED TO MDDR #129339 IAW MEL 21-51-02-02. PLACARDS INSTALLED. MCC NOTIFIED. PERFORMED FIM 21-51 FT 813 - PERFORMED SYSTEM FAULT RESET AND OPERATED BOTH PACKS, ALL NORMAL. NO FAULTS PRESENT. THIS CLOSES MDDR 129339. PLACARDSDR UIEA2020060801229Warning System · false activationL FWD FUEL PUMP EICAS MESSAGE. PERFORMED OPS CHECK IAW AMM 28-22-00/501. NO FAULTS NOTED. ALL OPS NORMAL.SDR UIEA2020060801237Warning System · false activationLT FORWARD WINDOW HEAT EICAS MSG. PERFORMED BITE TEST OF LT WINDOW HEAT. NO DEFECTS NOTED AT THIS TIME PER FIM 30-41-00.SDR UIEA2020060801213Unknown · malfunctionedTHRUST LEVER MOVEMENT STICKY. NOT SMOOTH. INSPECTED AND WORKED BOTH THRUST LEVERS, NO DISCREPANCY NOTED. LOAD TEST LESS THEN 6LBS IAW AMM 76-11-00-735-100-600.SDR UIEA2020060101169Coupler · leakingUPON PDSC IDG OIL LEVEL CHECK FOUND OVERFLOW SERVICE COUPLER LEAKING. TIGHTENED OVERFLOW SERVICE COUPLER IAW AMM 20-11-00/201. PERFORMED ENGINE RUN IAW AMM 71-00-00 AND LEAK CHECKED IAW AMM 71-71-00 AND 24-11-01. NO LEAKS NOTED AT THIS TIME.SDR UIEA2020052701139Isolation Valve · faultyDURING START, RIGHT ISOLATION VALVE DID NOT OPEN. TRANSFERRED TO MDDR 128880 AS PER MEL 36-11-06, CAT 'C'. DISP: GTC 09:27Z, ITEM M1: REMOVED AND REPLACED RIGHT ISO VALVE IAW AMM 36-11-04, OPS CHECK NORMAL. PLACARDS REMOVED. THIS CLEARS MDDR 128880.SDR UIEA2020052631116Seal · missingOIL QTY WENT TO ZERO AFTER LEVEL OFF. OIL PRESSURE STEADY DROPPED FROM 30PSI TO 12PSI AT LANDING. PERFORMED TEST OF THE NR 3 IDLE LEAK TEST IAW AMM 71-00-00-795. NR 3 FOUND LEAK FROM STARTER WITNESS CHAMBER. REMOVED STARTER IAW AMM 80-11-04. FOUND STARTER SSDR UIEA2020052201083Starter · failedDURING L ENG START WHEN STARTER MOVED TO "GND" DUCT PRESS DROPPED TO ALMOST NOTHING, N2 NEVER SPOOLED UP TO MORE THAN 15%. DUCT PRESS WAS 30 PSI PRIOR TO THIS.(<P>SWAPPED ECU WITH KNOWN GOOD PART, OPS CHECK BAD. RETURNED AIRCRAFT TO ORIGINAL CONFIG. TRANSFERRESDR UIEA2020052001083Pneumatic System · inoperativeDURING L ENG START WHEN STARTER MOVED TO "GND" DUCT PRESS DROPPED TO ALMOST NOTHING, N2 NEVER SPOOLED UP TO MORE THAN 15%. DUCT PRESS WAS 30 PSI PRIOR TO THIS.(<P>SWAPPED ECU WITH KNOWN GOOD PART, OPS CHECK BAD. RETURNED AIRCRAFT TO ORIGINAL CONFIG. TRANSFERRESDR UIEA2020051301030Skin · gougedGOUGE DAMAGE WAS FOUND ON FUSELAGE SKIN BETWEEN STA 1417 / STA 1430 AND STRINGERS S-19L / S-20L. DAMAGE REPAIRED IN ACCORDANCE WITH B767-300 SRM 53-00-01-2R-14.SDR UIEA2020052101025Strap · crackedCRACK INDICATION WAS FOUND ON THE LH & RH FAIL SAFE STRAPS DURING ACCOMPLISHMENT OF EO 6753A070 PARTS 1 AND 2(<P ><SPAN>CRACK DAMAGES WERE REPAIRED / IN ACCORDANCE WITH EO 6753A070 PARTS 3 AND 4</SPAN></P>)SDR UIEA2020052101026Skin · corrodedCORROSION OVER PREVIOUS REWORKS WAS FOUND ON THE RH HORIZONTAL STABILIZER TOP SKIN AT REAR SPAR AND BETWEEN RS STA 128.605 - RS STA 251.105(<P ><SPAN>DAMAGES REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6755033.</SPAN></P>)SDR UIEA2020052101027Skin · corrodedCORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER TOP SKIN, BETWEEN FRONT SPAR AND RIB 3.(<P ><SPAN>CORROSION WAS REWORKED AND / THE SKIN WAS REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6755032.</SPAN></P>)SDR UIEA2020052101029Skin · dentedDENT WITH CREASE WAS FOUND ON FUSELAGE TAIL CONE SKIN BETWEEN STA 1832 / STA 1843 RH SIDE(<P ><SPAN>DAMAGE REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6753348.</SPAN></P>)SDR UIEA2020052101031Splice Plate · corrodedCORROSION DAMAGE WAS FOUND ON THE SPLICE PLATE AT STA 977 AND STRINGER S-23L(<P ><SPAN>CORROSION DAMAGE WAS REMOVED / AND REPAIRED IN ACCORDANCE WITH MEXICANA MRO TRE6753347</SPAN></P>)SDR UIEA2020052101032Structure · corrodedPREVIOUS REWORK WITH CORROSION DAMAGE WAS FOUND AROUND STATIC PORT BETWEEN STA 1285 / STA 1307 AND STRINGERS S-28L / S-29L.(<P ><SPAN>DAMAGE WAS REPAIRED IN ACCORDANCE / WITH MEXICANA MRO TRE6753350 AND IAI CS-24086-015</SPAN></P><P ><SPAN></SPAN></P>)SDR UIEA2020052101033Support Beam · corrodedCORROSION WAS FOUND ON THE RH WING FIXED TRAILING EDGE SUPPORT BEAM BETWEEN AT BL 97.42, BETWEEN STA 957.80 / STA 1000.10.(<P ><SPAN>DAMAGE WAS REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6757157.</SPAN></P>)SDR UIEA2020040600695Warning System · false activationL ENGINE BLEED DISCREET LIGHT ILLUMINATED BETWEEN 8000-15000 WITH 102.0 N2 AND 103.6 N1 RESPECTIVELY.(<P>PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST IAW B767AMM TASK 36-23-00 715-001. NO FAULTS NOTED.</P>)SDR UIEA2020040200679Bleed Air Sys · malfunctionedDUCT PRESSURE FOR BOTH ENGINE STARTS WAS 15 PSI, MAX MOTORING TO BOTH STARTS WAS 18% N2, BOTH ENGINE STARTS NORMAL BUT TOOK LONGER THAN USUAL.(<P>DEFERRED APU BLEED AIR SYSTEM IAW ATLAS DDG 49-11-01-01, MDDR 126571, CAT "C".</P>)SDR UIEA2020033100580Oxygen Bottle · unserviceableGALLEY PORTABLE O2 BOTTLE PRESSURE OUT OF LIMITS.(<P>TRANSFERRED TO MDDR 126397, MEL 35-31-01, CAT 'D', DUE DATE: 27JUL20, TI: TS @ 0247Z. 2 SERVICEABLE PORTABLE O2 BOTTLES STILL ON BOARD, STOWED UNSERVICEABLE BOTTLE IN OVERHEAD BIN PER AMM 35-00-00.</P><P>30MSDR UIEA2020032600557Oil System · lowAPU OIL QUANTITY LOW, APU SHUT DOWN ON DESCENT.(<P>SERVICED APU OIL I/A/W AMM 12-13-04, APU OPS CHECK NORMAL.</P>)SDR UIEA2020032300535Ecu · faultyAPU AUTO SHUTDOWN AFTER MINUTES, ECU WON'T TEST.(<P>REMOVED AND REPLACED ECU IAW AMM 49-61-05, OPS CHECK NORMAL.</P>)SDR UIEA2020031700474Fuel Filter · faultedL ENG FUEL FILT ADVISORY SG AND STATUS MSG ILLUMINATED IN FLIGHT. NO ABNORMAL ENGINE INDICATIONS NOTED.(<P>REMOVED AND REPLACED L ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECK GOOD.<BR /></P>)SDR UIEA2020030300366Unknown · malfunctionedDURING ENGINE START, APU AIR DROPPED TO 15 PSI, FLUCTUATING 2-3 PSI. MAX MOTORING ACHIEVED WAS 16% N2 ON RIGHT ENGINE.(<P>PERFORMED T/S PER FIM 36-10 FAULT TREE 840 AND BITE AIR SUPPLY MODULE PERFORMED AND FOUND NO FAULTS AT THIS TIME.</P>)SDR UIEA2020030200364Battery · dischargedDURING DAILY CHK FOUND EMERGENCY FLASH LIGHT INOP.(<P>REMOVED AND REPLACED EMER FLASH LIGHT BATTERY, OPS CHK GOOD IAW 25-64-00.<BR /></P>)SDR UIEA2020030200362Filter · dirtyINFO & DUCT PRESSURE BELOW OPTIMUM 21 PSI UNTIL START VALVE OPEN DURING RIGHT ENGINE START.(<P>PERFORMED DRY MOTORIZED R/H ENG IAW AMM 71-00-00, VERIFIED PNEUMATIC PRESS I.A.W. AMM 36-11-00 PRESSURE WITHIN LIMITS, 30 PSI. SEE LOG PAGE #1197014.<BR /></P><P>LP SDR UIEA2020022800346Elt · inoperativePORTABLE ELT INOP IN GALLEY. ONE SERVICEABLE UNIT REMAINS (EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS).(<P>TRANSFERRED TO MDDR 125108, CAT 'D', MEL 25-63-10-01, DUE DATE 25JUN20. NOTIFIED MCC.</P><P>LP 1197029 - ITEM M6: REMOVED & REPLACED PORTABLSDR UIEA2020022630311Ecu · malfunctionedON INITIAL ENGINE START (R-CVG) (L-DEN), APU BLEED AIR PRESSURE IS FLUCTUATING BETWEEN 15 AND 25 PSI, RESULTING IN MAX MOTORING OF 19.5 N2 ONLY.(<P>TRANSFERRED TO DMI 124990, CAT C, DUE 04MAR20 IAW MEL 49-11-01-01.</P><P>LP 1196990: PERFORMED APU BITE IAW FIM SDR UIEA2020022100299Eec · malfunctionedLEFT ENGINE CONTROL ON EICAS AND STATUS MESSAGE.(<P>PERFORMED FIM 73-21 FAULT TREE 878 AND 71-01 TASK 936. REMOVED AND REPLACED LEFT ENGINE EEC, TESTED AND FOUND OK AS PER AMM 73-21-15. PERFORMED ENGINE RUN UP AS PER AMM 71-00-00. NO FAULT FOUND AT THIS TIME.<SDR UIEA2020020600198Sensor · inoperativeAPU PNEUMATICS INOP (AUXILIARY POWER UNIT, PNEUMATIC FUNCTION)(C/W DDG PROCEDURE 36-11-04)(<P>TRANSFERRED TO MDDR #124303 IAW DDG 49-11-01-01. MX ACTION C/W, CAT 'C', DUE 14FEB20. MCC GLEN NOTIFIED. PLACARDS INSTALLED.</P><P>LOG PAGE 1190476: REMOVED AND REPLSDR UIEA2020020400184Unknown · unknownREPEAT WRITE UP (1ST WRITE UP ON LP #1182887), ON BOTH ENGINE STARTS DUCT PRESSURE DROPPED TO AROUND 20 PSI AND N2 MAX MOTORED TO 12%-19% N2 BEFORE RUN SWITCHES ENGAGED (BOTH PACKS OFF).(<P>PERFORMED BITE TEST OF APU CONT. UNIT, NO FAULTS. APU DUCT PRESS NORMASDR UIEA2020020310162Warning Message · false activationON BOTH ENG STARTS, DUCT PRESS DROPPED TO AROUND 20 PSI AND N2 MAXED AT 19% BEFORE RUN SWITCHES ENGAGED.(<P>PERFORMED FAULT ISOLATION MANUAL 49-11 FAULT TREE 982 FOR LOW DUCT PRESSURE IN MAIN ENGINE START MODE ONLY. FOUND NO LOW PRESSURE OR SURGING. FOUND NO FSDR UIEA2020012870132Cap · unsecure1000 FT PRIOR TO LEVEL OFF AT FL 370, WE NOTICED R ENG OIL PRESS INDICATION AMBER AT 28. IT REMAINED AMBER FOR DURATION OF FLIGHT. ALL OTHER INDICATIONS NORMAL. AFTER FURTHER INSPECTION, FOUND OIL TANK FILLER CAP NOT SECURED. SERVICED ENG OIL TO PROPER LEVEL SDR UIEA2020012400116Unknown · unknownRIGHT ENG GENERATOR INOPERATIVE. RT IDG DISCONNECTED. PERFORMED ENGINE IDLE RUNS TWICE IAW AMM 71-00-00 AND COMPLETED OPERATIONAL TESTS OF RT IDG IAW AMM 24-11-00, NO DEFECTS NOTED. IDG OPS CHECKED GOOD.SDR UIEA2020012400119Warning Message · false activationON INITIAL CLIMB, LEFT BLEED LIGHT ILLUMINATED FOR SEVERAL SECONDS, NO EICAS MSG. REPEAT WRITE UP.(<P>PERFORMED BITE TEST ON AIR SUPPLY CONTROL UNIT IAW AMM 36-23-00. OPS TEST OK, NO FAULTS NOTED.</P>)SDR UIEA2020011500075Relay · failedLEFT FUEL OVERRIDE PUMP CB FOUND POPPED. TRANSFERRED TO MDDR 123426 IAW MEL 28-22-02A, CAT 'C', DUE 25JAN2020. PERFORMED FIM 28-22 FT 812, TO STEP 21, R&R RELAY K329 L FUEL OVERRIDE PUMP CONT. RELAY IAW WDM 28-22-12. OPS CHECK OF L CTR PUMP GOOD AT THIS TIME. SDR UIEA2020011500065Warning System · false activationON CLIMB OUT, LEFT BLEED LIGHT ILLUMINATED. NO EICAS MSG. LIGHT STAYED ON FOR SEVERAL MINUTES, NO EICAS MSG, THEN IT WENT OUT. WRITTEN UP BEFORE. PERFORMED AIR SUPPLY BITE TEST, NO FAULTS, REF AMM 36-20 FT 805 AND 36-23-00. REMOVED AND RE-RACKED AIR SUPPLY CONSDR UIEA2020011300055Warning System · false activationON CLIMB OUT, THE LEFT BLEED WAS ILLUMINATED MOMENTARILY.(<P>PERFORMED PUSH TO TEST, OPS CHECK GOOD ON LIGHT. PERFORMED BITE TEST TO AIR SUPPLY CONTROL. NO FAULTS NOTED ON BOX. PERFORMED AIR SUPPLY PRESSURE INDICATION TEST IAW AMM 36-21-00. OPS CHECK GOOD. NO SDR UIEA2020011300059Unknown · malfunctionedDURING PRE-FLIGHT FMC PROMPT ON UPPER EICAS STAYS DISPLAYED WITH IRU'S ALIGNED AND ALL FMC DATA ENTERED.(<P>CYCLED APU POWER I.A.W AMM 49-11-00. FMC MESSAGE WENT AWAY. OPS CHECK GOOD.</P>)SDR UIEA2020011300050Sensor · faultyMX MSG L ENG EEC C2, PER THE COMPANY REQUEST REPLACE #1 ENG CIT SENSOR T2.5.(<P>REMOVED AND REPLACED #1 ENGINE CIT SENSOR I.A.W AMM 73-21-02 AND ECM 20-20D-018. OPS CHECK GOOD.</P>)SDR UIEA2019123096164Controller · malfunctionedLT BLEED LIGHT CAME ON DURING CLIMBOUT FROM 7,000 TO 15,000, NO BLEED EICAS MSG PRESENT. LIGHT EXTINGUISHED AFTER LEVEL OFF @15,000 AND BEFORE QRH WAS ACCOMPLISHED. PERFORMED AIR SUPPLY BITE TEST, FAULTING HIGH PRESSURE CONTROLLER ON LEFT SIDE, IAW AMM 36-23-0SDR UIEA2019123096166Processing Unit · malfunctionedSUSPECT FUEL LEAK LT ENG. FUEL IMBALANCE AS MUCH AS 1.0K AND TOTALIZER /CALCULATED TO DIFF AS MUCH AS 2.5K. FUEL WAS BALANCED 2HR INTO FLIGHT, ALSO FUEL XFEED VALVE CHECKED SUCCESSFUL. PERFORMED A BIT PROCEDURES IAW AMM 28-41-00, WAS FAULTING PROCESSOR. REPLASDR UIEA2019121606083Warning Message · false activation"CTR R FUEL PUMP" EICAS MSG PRIOR TO ADVANCING THRUST LEVERS FOR TAKEOFF. 4000 LBS FUEL IN CTR TANK. CYCLED FUEL PUMP SWITCH PER MX CONTROL, OPERATED NORMALLY.(<P>C/W OPERATIONAL TEST OF CTR R BOOST PUMP IAW B767 AMM 28-22-00, PUMP OPS CHECK NORMAL.</P>)SDR UIEA2019120506002Warning Message · false activationIN FLIGHT, CTR LEFT FUEL AND CENTER RIGHT FUEL PUMP EICAS MESSAGES DO NOT DISPLAY WHEN CTR TANK QTY REACHES ZERO.(<P>PERFORMED TEST OF BOOST PUMPS, ALL OK IAW B767 AMM 28-00-00. FOUND SYSTEM TO OPERATE NORMAL AT THIS TIME.</P>)SDR UIEA2019120405993Warning Message · false activationCENTER R FUEL PUMP AND CENTER L FUEL PUMP EICAS MESSAGES. DOES NOT DISPLAY WHEN CENTER FUEL TANK QUANTITY REACHES ZERO.(<P>PERFORMED OPERATIONAL TEST OF THE CENTER L/R FUEL PUMPS ON EICAS, OPS CHECK GOOD IAW AMM 28-42-00, AMM 28-42-01, AND AMM 28-22-01. </P>)SDR UIEA2019112705960Relay · failedAFTER START, R FWD FUEL PUMP EICAS ILLUMINATED. PERFORMED FIM 28-22 ON GROUND POWER, APU POWER, AND ENGINE BLEED PRESSURE SENSE LINE RT IAW FIM IAW AMM 28-42-01. OPS CHECKED GOOD. MX PROCEDURE COMPLIED WITH. REMOVED AND REPLACED RELAY K10704 IAW WDM 28-22-SDR UIEA2019112655956Fire Warning · false activationEICAS MSG ON SHORT FINAL, FIRE/OVERHEAT SYSTEM.(<P>PERFORMED SYSTEM TEST OF THE FIRE/OVERHEAT SYSTEM IAW AMM 26-10-00, COULD NOT DUPLICATE. OPS CHECKS OKAY AND NO FURTHER FAULTS NOTED.</P>)SDR UIEA2019112545953Circuit Card · malfunctionedDURING CREW PRE-FLIGHT, STATUS MESSAGE "APU FIRE LOOP 1". (<P>TRANSFERRED TO DMI 121097 IAW MEL 26-15-01-01, CAT 'C', DUE DATE: 04-DEC-19.</P><P>LP 1223654 - M6: REMOVED AND REPLACED APU LOOP 1 PRINTED CIRCUIT CARD 685T, OPS CHECK GOOD. THIS CLEARS DMI 121097SDR UIEA2019112535948Overheat Loop · out of adjustEICAS FIRE/OVHT SYS.(<P>PERFORMED ADJUSTMENT TEST OF FIRE OVHT SYS IAW AMM 26-11-00, OPERATIONAL TEST NORMAL.</P>)
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