N569AS

Service difficulty reports · 514

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 = 'N569AS' 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.

SDR ASAA2019011127760Transceiver · failedWX RADAR WILL NOT TEST IN "TEST" MODE. "WX STAB AND WXR RANGE DISAGREE MESSAGES APPEAR ON MAP DISPLAY. GROUNDED - YES. REMOVED & REPLACED WEATHER RADAR RECEIVER/TRANSMITTER IAW AMM 34-43-41-000-801 & 34-43-41-401-801. PERFORMED OPS CHECK IAW AMM 34-43-00-710-8Jan 11, 2019 · N569AS · Boeing 737890 · Weather Radar SystemSDR ASAA2019010227653Battery Pack · dischargedLT OVERWING EMERGENCY LIGHT DOES NOT COME ON. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1694 S/N 35160 AND OPS CK GOOD.Jan 2, 2019 · N569AS · Boeing 737890 · Emergency LightingSDR ASAA2019010227652Battery Pack · dischargedL1 DOOR EMERGENCY LIGHT DOES NOT COME ON. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1675 S/N 76392 AND OPS CK GOOD.Jan 2, 2019 · N569AS · Boeing 737890 · Emergency LightingSDR ASAA2018122837588Floorbeam · corrodedINTERNAL PAX COMPARTMENT AFT WET AREA FLOOR STRUCTURE HAS AN AREA OF CORR ON A FLOOR SUPPORT AT STA. 952. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM SUPPORT AT STA 952 FOR INTERVAL PAX COMPARTMENT AFT WET AREA IAW B737 800 SRM 51 40 2 W 4" O .063 R .055 LDec 13, 2018 · N569AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2018121227666Crease Beam · corrodedRT INTERNAL PAX COMPARTMENT FLOOR STRUCTURE HAS CORR AT STA 847 WHERE FLOOR MEETS SIDEWALL. GROUNDED - YES. REPAIRED INNER CREASE BEAM CHORD IAW EA 800 53EA 21103 REV 0 ISSUED 03JAN19.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2018121227664Intercostal · crackedINTERCOSTAL CRACKED BETWEEN STA 312-328 RBL 24. GROUNDED - YES. REMOVED AND REPLACED 1EA INTERCOSTAL AT RBL 24, STA 312-328 IAW SRM 51 42 02 06 0 PG 6 STEP D.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121227662Intercostal · crackedINTERCOSTAL CRACKED BETWEEN STA 312-328 AT LBL 36. GROUNDED - YES. REMOVED AND REPLACED 1EA. INTERCOSTAL AT LBL 36, STA 312-328 IAW SRM 51 40 02 0G 0 PG 6 STEP D.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121227642Fitting · crackedINTERNAL FWD CARGO COMPARTMENT R/H SIDE HAS A CRACKED BAFFLE CLIP ON FWD SIDE OF STA 500G. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW SRM 51 40 02 0G 0.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018122827589Floor Support · corrodedFLOOR SUPPORT AT STA 947 TO 967 HAS CORR @LBL24. GROUNDED - YES. REMOVED CORR AND FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 REMOVED AND REPLACED FLOOR SUPPORT AT STA 947 TO STA 967 AT LBL 24 IAW B737 800 SRM 51 40 02 0G 0 W 1.90 O .075 R .062 L Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018122827587Angle · corrodedANGLE ON R/H WEB AFT OF STA 986 HAS CORR. GROUNDED - YES. REMOVED CORR AND FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 REMOVED AND REPLACED ANGLE IAW B737 800 SRM 51 04 02 0G 0 W .090 O .052 R .032 L 2.20 D .020".Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018122827586Baffle · crackedINTERNAL FWD CARGTO COMPARTMENT L/H SIDE HAS A CRACKED BAFFLE CLIP ON FWD SIDE OF STA. 500G. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW B737 800 SRM 51 40 02 0G 0.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018122827585Angle · crackedINTERNAL FWD CARGO COMPARTMENT L/H SIDE HAS CRACKED BAFFLE CLIPS ON FWD AND AFT SIDES OF STA 500H. GROUNDED - YES. REMOVED AND REPLACED 2EA. BAFFLE CLIPS IAW B737 800 SRM 51 40 02 0G 0.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121227405Fitting · crackedINTERNAL FWD CARGO COMPARTMENT RT SIDE HAS CRACKED BAFFLE CLIPS ON FORWARD AND AFT SIDES OF STA 500H. GROUNDED - YES. REMOVED AND REPLACED 2EA CLIPS IAW SRM 51 40 02 0G 0.Dec 12, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121127665Floor Support · crackedCABIN FLOOR SUPPORT STA 540 BL0 RBL24 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED NEW CABIN FLOOR SUPPORT STA 540 BL0-RBL 24 IAW SRM 51 40 02 0G 0.Dec 11, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121127663Floor Support · crackedCABIN FLOOR SUPPORT STA 540 BL0-LBL24 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED NEW CABIN FLOOR SUPPORT STA 540 BL0-LBL24 IAW SRM 51 40 02 0G 0.Dec 11, 2018 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018121127661Seat Track · crackedCABIN SEAT TRACK STA 500H+10 RBL44 HAS BROKEN FLANGE. GROUNDED - YES. REPAIRED RBL44 SEAT TRACK IAW SRM 53 00 52 2R 4.Dec 11, 2018 · N569AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2018112527108Probe · failedMX CONTROL REQUEST A CHECK THE FQIS SYSTEM IN THE RT TANK TO PREVENT POTENTIAL INCORRECT FUEL QTY READINGS. GROUNDED - YES. FOUND COMP PROBE BAD. ALL OTHER PROBES WITHIN LIMITS. REMOVED AND REPLACED NR 2 TANK COMP PROBE F15R REF AMM 28-41-21/401. ALL PROBES WINov 25, 2018 · N569AS · Boeing 737890 · Fuel Quantity SensorSDR ASAA2018112527107Probe · failedDUE TO 2 FUEL QTY EVENTS ON THE NR 1 TANK, MX CONTROL REQUEST A CHECK THE FQIS SYSTEM IN THE LEFT TANK TO PREVENT POTENTIAL INCORRECT FUEL QTY READINGS. GROUNDED - YES. FOUND PROBES F4, F6, F7, F9, AND COMP PROBE BAD. ALL OTHER PROBES WITHIN LIMITS. WHILE CONFNov 25, 2018 · N569AS · Boeing 737890 · Fuel Quantity SensorSDR ASAA2018112427123Compensator · failedAFTER TAKEOFF AT 200 TO 300 FT THE NR 1 MAIN TANK FUEL QTY SHOWED AN IMBALANCE OF 1300 LBS RAN QRH. TOP AT CLIMB SHOWS 1000 LBS. ALL FUEL FLOWS AND ENGINE INDICATIONS ARE NORMAL. GROUNDED - YES. NR 1 TANK PROBES F4, F6, F7, F9 AND COMP PROBE REPLACED. NO LEAKSNov 24, 2018 · N569AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2018112427065Valve · failedREPLACE THE CROSSFEED VALVE AND SHAFT DUE TO FUEL IMBALANCE DURING FLIGHT. GROUNDED - YES. REMOVED AND REPLACED ENGINE FUEL CROSSFEED VALVE REF AMM 28-22-21-400-805. INSPECTED CROSSFEED VALVE SHAFT AND FOUND NO DEFECTS. INSTALLED ADAPTER PLATE REF AMM 28-22-21Nov 24, 2018 · N569AS · Boeing 737890 · Fuel Transfer ValveSDR ASAA2018101926528Plenum · delaminatedLT AFT HEAT EXCHANGER ACCESS PANEL DOOR OPENING DELAMINATED BEYOND LIMITS. COMMON TO THE PLENUM. GROUNDED - YES. MIG-2C 40-0009860 INIT. REPLACED LT AFT HEAT EXCHANGER PLENUM REF MM 21-51-03-400-804-002, MIG 2C 40-0009860 COMPLETED.Oct 17, 2018 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018101926527Plenum · damagedFURTHER DAMAGE NOTED ON RT AFT PRIMARY HEAT EXCHANGER PLENUM. GROUNDED - YES. REPLACED RT PRIMARY HEAT EXCHANGER PLENUM REF AMM 21-51-03-400-804-002. OPS, LEAK CK NORMAL.Oct 17, 2018 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018100326346Warning System · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL. GROUNDED - YES. BITE OF NR 2 CONTROLLER SHOWS TCV FAULT. FAULT CLEARS & OPS NORMAL REF FIM 21-61 TASK 801.Oct 3, 2018 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018091026078Sensor · dirtyFOUND FAUL 77-10851 BOTTOM RIGHT S2 EGT SENSOR OUT OF RANGE ECONOMIC FAULT ON NR 1 ENGINE. GROUNDED - YES. ACCOMPLISHED FIM 77-21 TASK 802. PERFORMED EGT CLEANING OF NR 1 ENGINE REF AMM 77-21-00. PERFORMED EEC TEST OF NR 1 ENGINE EEC TEST PASS REF AMM 73-21-00Sep 9, 2018 · N569AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2018090626077Warning System · false activationWHILE PERFORMING TASKCARD 78273000, FOUND FAULT CODE 77-20872, NR 2 ENG, THE TOP LEFT EGT SIGNAL IS OUT OF RANGE, ECONOMIC FAULT, DEFERRED PER TASK CARD 78273000. GROUNDED - YES. DEFERRED PER TASKCARD 78273000, DEFERRAL INTERVAL IS 500 FLT HRS. NR 2 ENGINE FAUSep 6, 2018 · N569AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2018090726039Warning System · false activationRIGHT PACK LIGHT ILLUMINATED WITH MASTER CAUTION RECALL EXTINGUISHED WITH RESET. GROUNDED - YES. PERF BITE PROCEDURE PER FIM 21-61 TASK 801 RESET CONT OPS NRML NO FAULTS.Sep 6, 2018 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018082025817Guide Arm · inoperativeR1 DOOR DOES NOT CLOSE PROPERLY WITHOUT ASSISTANCE. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE R1 DOOR GUIDE ARM AND ADJUSTED TO WITHIN LIMITS IAW AMM 52-41-21-400-801.Aug 16, 2018 · N569AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2018073025557Software · faultedVTK DISPLAYED ON BOTH NAVIGATION DISPLAYS AFTER LANDING DURING TAXI - IN TO OAK. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801, SYSTEM CHECKS GOOD. INFLIGHT FAULTS HAD ONE GROUND FAULT FOR RT FMC, CODE 3DD REVEALED IT WAS A PROGRAM FAULT, A SOFTWARE INSTRUCTIONJul 28, 2018 · N569AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018071625407Display · failedF/O FMC / CDU FAILED ON GROUND DURING POWER SWITCHING (APU TO GND). GROUNDED - YES. CYCLING FMCS 2 & FMC CDU C/B'S NO HELP. REPLACED F/O FMCS CDU REF AMM 34-61-00-000-802. OPS CK NORMAL.Jul 13, 2018 · N569AS · Boeing 737890 · Central DisplaySDR ASAA2018070825307Blade · damagedWHILE ACCOMPLISHING TC 78472002 NR 1 ENGINE S/N 894474 FOUND FAN BLADES NR 7, 14, 19, 20, 22, 23 CU-NI-IN COATING CHIPPED MEASURED & FOUND TO BE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED ENG 1 FAN BLADES 7, 14, 19, 20, 21, 22 AND 23 ON S/N 894474 REFJul 8, 2018 · N569AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2018070825306Blade · damagedWHILE ACCOMPLISHING TC 78472002 NR 1 ENGINE S/N 894474 FOUND FAN BLADES NR 1 (.006) AND 16 (.008) DAMAGE DUE SHIM CONTACT CONCAVE SIDE. GROUNDED - YES. REMOVED AND REPLACED ENG 1 S/N 894474 FAN BLADES 1, 16 REF T/C 78472002.Jul 8, 2018 · N569AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2018070825305Lubrication Unit · defectivePOP IT EXTENDED ON APU LUBE MODULE. TECH SERVICES REQUESTS REMOVE AND REPLACE. GROUNDED - YES. REMOVED AND REPLACED LUBE MODULE. NO LEAKS FOUND. OP CHECK GOOD. APU BITE TEST GOOD REF AMM 49-91-11.Jul 8, 2018 · N569AS · Boeing 737890 · APU Oil SystemSDR ASAA2018070225275Detector · inoperativeJUST PRIOR TO LEVEL OFF AT FL350 APU DET INOP ILLUMINATED. APU WAS OFF AT THE TIME AND REMAINED OFF FOR THE REMAINDER OF THE FLIGHT. GROUNDED - YES. DIVERSION TIME 10 MINUTES - REMOVED AND REPLACED APU LOWER HEAT DETECTOR ASSEMBLY REF AMM 26-15-01. WHEN ACCOMPJul 2, 2018 · N569AS · Boeing 737890 · Overheat DetectionSDR ASAA2018061725094Eec · unknownWHILE ACCOMPLISHING T/C#78273000, FOUND A FAULT ON THE NR 1 ENGINE. SHORT TIME FAULT, MESSAGE NUMBER 73-11271, THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. ACFT GROUNDED. PERFORMED FIM 73-27, TASK 804. NO FAULTS FOUND. REMOVED AND INSTALLED TJun 17, 2018 · N569AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2018060925009Unknown · malfunctionedWHILE ACCOMPLISHING T/C 78273000, FOUND FAULT ON NR 1 ENGINE. SHORT TIME FAULT, MSG NUMBER: 73-11271, THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. GROUNDED - YES. ACCOMPLISHED T/C 78273000, VERIFIED NR 1 ENG HAVE NO FAULTS MSG FOR THE LAST 5 FLT LEJun 9, 2018 · N569AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2018043024448Blade · damagedWHILE ACCOMPLISHING T/C 78472002, FOR NR 2 ENGINE FAN BLADE LUBE. FOUND THE NR 2 PLATFORM AREA B HAS SHIM WEAR IAW AMM 72-21-02. ACFT GROUNDED. REMOVED HIGH METAL FROM THE NR 2 PLATFORM AREA B IAW AMM 72-21-02-200-801-F00.Apr 30, 2018 · N569AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018040724160Hf Comm · malfunctionedNO AUDIO FROM HF 2. ACFT GROUNDED. SWITCHED FROM SAT TO HF, OPS NORMAL.Apr 7, 2018 · N569AS · Boeing 737890 · HF Communications SystemSDR ASAA2018040624166Warning System · false activationFOUND NR 1 ENGINE SHORT TIME FAULT MSG 73-10021 INTERNAL EEC FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. PERFORMED FIM 73-21 TASK 801. NO FAULTS NOTED ON ANY LEG. ACCOMPLISHED THE REPAIR CONFIRMATION (EEC TEST) PER AMM 73-21-00-700-804-F00. CHECKS GOOD. Apr 6, 2018 · N569AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA2018033024088Fmc · dirtyENROUTE, FMC WOULD NOT ACCEPT DIRECT ROUTING OR WOULD THE EXEC LIGHT ILLUMINATE FOR ANY FUNCTION OR INPUT. ACFT GROUNDED. FMC FAULT REVIEW SHOWS FIRST OFFICER`S FMC CDU FAULT ON THE INBOUND LEG. ACCOMPLISHED FMC OPERATIONAL TEST IAW AMM 34-61-00-710-801 AMar 30, 2018 · N569AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018032424033Wire Harness · faultedFAULT CODE: 73-11271 FOUND ON THE NR 1 ENGINE. THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. SHORT TIME FAULT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE J7 HARNESS IAW AMM 73-21-06-000-801-F00, AND AMM 73-21-06-400-801-F00. PERFORMED EMar 24, 2018 · N569AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2018032324024Circuit Breaker · malfunctionedNR 1 HF RADIO HAS A FAIL IN THE ACTIVE AND STANDBY FREQUENCY DISPLAYS. ACFT GROUNDED. CYCLED THE NR 1 HF CIRCUIT BREAKER. OP CHECKED NORMAL IAW FIM 23-11, TASK 801.Mar 23, 2018 · N569AS · Boeing 737890 · HF Communications SystemSDR ASAA2018031423886Fault Message · false indicationFOUND MAINTENANCE MESSAGE 73-11271, NR 1 ENGINE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE, SHORT TIME FAULT. ACFT GROUNDED. PERFORMED TASK CARD 78273000. NO FAULTS FOUND AND NO MAINTENANCE HISTORY FOUND WITHIN THE PAST 30 DAYS. ACFT RELEASED.Mar 14, 2018 · N569AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2018030523771Valve · intermittentDURING DESCENT, APPROACH AND AFTER ENGINE SHUTDOWN, THE LEFT COWL VALVE OPEN LIGHT FLASHED ON AND OFF INTERMITTENTLY. TAI DID NOT DISPLAY WITH BLUE CALL LIGHT. ACFT GROUNDED. PERFORMED FIM 30-21 / 806 INITIAL EVALUATION. OPS CHECKED GOOD. DUE TO HISTORY, REMar 5, 2018 · N569AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2018030423762Indicator · intermittentNR 1 ENGINE COWL VALVE OPEN LIGHT (BLUE) FLICKERS ON AND OFF IN TURBULENCE. VALVE FUNCTIONED NORMALLY WHEN IN THE ON OR OFF POSITION. ACFT GROUNDED. INSPECTED, CLEANED, & REPLACED THE BULBS IN COWL VALVE OPEN LIGHT. INSPECTED THE NR 1 ENGINE COWL VALVE & CLMar 4, 2018 · N569AS · Boeing 737890 · Central WarningSDR ASAA2018022823747Wire Harness · chafedFOUND RUBBING DAMAGE ON CJ9 HARNESS. FOUND DAMAGE ON DP1004 ON J10 HARNESS. THIS IS FOR THE NR 2 ENGINE ESN 894475. GROUNDED - YES. REMOVED AND REPLACED CJ9 HARNESS REF AMM 73-21-06/401. OPS TEST NORMAL. ACCOMPLISHED REPAIR ON DP1004 ON J10 HARNESS REF AMM 70-Feb 28, 2018 · N569AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2018021823603Fmc · malfunctionedLEFT FMC FAILED IN FLIGHT. VTK AND MAP FLAGS DISPLAYED. NORMAL OPERATION ACHIEVED FOLLOWING QRH PROCEDURE WITH FMC SWITCH BOTH ON RIGHT. ACFT GROUNDED. CYCLED THE POWER TO LEFT FMC OPS RESTORED NO FAULTS FIM 34-61-TASK 801.Feb 18, 2018 · N569AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018021223528Fmc · malfunctionedRIGHT FMC FAILED ENROUTE. VTK AND MAP FAILURE FLAGS ON FIRST OFFICER NAVIGATION DISPLAY. ACFT GROUNDED. CYCLED THE NR 2 FMC IAW FIM 34-61 TASK 836. RESTORED. OK FOR CONTINUED SERVICE.Feb 12, 2018 · N569AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018020423438Alternator · faultedNR 1 ENGINE FAULT FOUND AT FMC CDU, RECENT SHORT TIME MESSAGE CODE 73-11271. THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. ACFT GROUNDED. REMOVED & REPLACED THE NR 1 ENGINE EEC, ALTERNATOR, & ROTOR IAW AMM 73-21-08. OPS & LEAK CHECKED GOOD.Feb 4, 2018 · N569AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2018013123361Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL, RESETS WITH MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROLLER BITE IAW FIM 21-62 TASK 801. SHOWS NO FAULTS, PACK OPS CHECKED NORMAL.Jan 31, 2018 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018012223270Oil System · lowMAINT LIGHT ILLUMINATED AFTER START. GROUNDED - YES. APU OIL LOW, SERVICING ACCOMPLISHED PER AMM 12-13-31.Jan 22, 2018 · N569AS · Boeing 737890 · APU Oil System
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