N558AS

Service difficulty reports · 535

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 = 'N558AS' 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 ASAA2018122427565Lead · failed#2 ENG LH ING INOP DURING ENGINE RUN FOR OIL SVC. GROUNDED - YES. REF B737-800 FIM 74-21-TASK 806, PERFORMED AUDIBLE IGNITER TEST. LH IGN SOUNDED FAINT. RH TESTED NORMAL. REMOVED AND REPLACED LH IGNITION LEAD REF B737-800 AMM 74-21-01. AUDIBLE TESTED NORMALLY.Dec 24, 2018 · N558AS · Boeing 737890 · Ignition Harness (Distribution)SDR ASAA2018122637543Warning Message · abnormalLEFT PACK WILL NOT RESET WITH MASTER CAUTION "PUSH TO RESET" AS SPECIFIED BY MEL 21-32B. GROUNDED - YES. REF B737-800 FIM 21-62 TASK 801, PERFORMED PACK TEMP CONTROL BITE. RESET FAULTS AND PACK LIGHT NOW RESETS.Dec 23, 2018 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA201812247505Warning Light · false activationLEFT PACK LIGHT REMAINS ILLUMINATED AFTER MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED BITE CHECK PER B737-800 FIM TASK 21-62 TASK 801. PACK TEMP CONTROL BITE PROCEDURE ACCOMPLISHED RESET VERIFIED NO FAULTS VERIFY PACK LIGHT REMAINS OFF AT THIS TIME. A/CDec 22, 2018 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018122627502Duct · crackedDURING AFTER START CHECK UPON RECALL, THE LEFT PACK LIGHT ILLUMINATED. WE RAN QRH 2.12 AND AFTER PUSHING THE MASTER CAUTION LIGHT, THE PACK LIGHT EXTINGUISHED. GROUNDED - YES. RB211-535 E4Dec 21, 2018 · N558AS · Boeing 737890 · Air Distribution SystemSDR ASAA2018122197493Warning Light · false activationON DESCENT ON RECALL LEFT PACK LIGHT ILLUMINATED. EXTINGUISHED ON MASTER CAUTION RESET. GROUNDED - YES. REF B737-800 FIM 21-53 TASK 807, LEFT PZTC BITE VERIFY TEST GOOD, PREV FLT HAS NO FAULTS. VERIFIED NO OBSTRUCTION IN LEFT RAM AIR DUCT. VERIFIED LEFT PACK ODec 19, 2018 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018121967467Actuator · faultedLEFT PACK LIGHT ILLUMINATED ON CLIMB OUT AROUND FL290. GROUNDED - YES. DIVERSION TIME 52 MINUTES. ACCOMPLISHED PACK TEMP CONTROL BITE CHECK PER B737-800 FIM 21-62 TASK 801, FOUND LH RAM AIR ACTUATOR FAULTED. R/R RAM AIR ACTUATOR PER B737-800 AMM 21-51-21. R/R Dec 16, 2018 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018121957415Warning Message · false activationLEFT PACK ILLUMINATED ON MASTER CAUTION RECALL EXTINGUISHES WHEN PRESSING MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PACK/ZONE TEMPERATURE CONTROLLER BITE TEST ON BOTH CONTROLLERS REF. B737-800 AMM 21-51-00-700-803. OPS. NORMAL. NO FAULTS NOTED.Dec 15, 2018 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018121177273Exciter · inoperativeL IGNITION ON RT ENG INOP. GROUNDED - YES. REF B737-800 AMM TASK 74-11-01 FOR REMOVAL AND REPLACEMENT OF L/H IGNITION EXCITER BOX ON #2 ENG.Dec 7, 2018 · N558AS · Boeing 737890 · ExciterSDR ASAA2018112697064Probe · inoperativeMAIN FUEL TANK #1 QTY 8.16, CTR 8.00, MAIN TANK #2 8.62 - WITHIN 2 MINUTES #1 QTY 7.59, FUEL BURN AND FLOW NORMAL - XFEED FUEL AND IMBAL LIGHT ON. #1 TANK DID NOT GO OFF UNTIL MAIN TANKS WERE WITHIN 200 LBS. AFTER LANDING, #1 QTY INCREASED 500 LB. GROUNDED - YNov 19, 2018 · N558AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2018111526873Seal · damagedWHILE ACCOMP. FAN LUBE #2 ENG S/N 894151 FOUND PLATFORM SEAL DAMAGE TO ALL PLATFORMS TOTAL DAMAGE GREATER THAN 40". GROUNDED - YES. REPLACED ALL PLATFORM.Nov 15, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018111526872Shim · damagedWHILE ACCOMP FAN BLADE LUBE #2 ENG S/N 894151 FOUND ALL BLADE SHIMS WORN MISSING MOLY DAG COATING >25%. GROUNDED - YES. REPLACED ALL #2 ENG BLADE SHIMS.Nov 15, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018111526871Blade · damagedWHLE ACCOMP. T.C. SBCFM56-7B--72-1033-1 FAN BLADE ULTRASONIC INSP. FOUND BLADE #3 S/N DC980532-L ' 34% INDICATION .8" FROM T.E CONVEX SIDEBLADE #13 S/N DD281020-O ' 35% INDICATION 1.5" FROM L.E CONVEX SIDEBLADE #17 S/N DD281033-U ' 35% INDICATION 1.0" FROM L.ENov 15, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018111656870Blade · damagedWHILE ACC. FAN LUBE T.C. ESN - 894151 FOUND CU-NI DAMAGE TO BLADE POSN. #8 S/N DD280468-G #16 DD280056-8 #20 S/N DC975822-G. GROUNDED - YES. REPLACED BLADES ON #2 ENGINE, #8 & #20 AND #16 AND ITS PAIR #4 PER T/C 78472010. MAPPED BLADES PER BLAMAP V. 3.0, ENTERNov 15, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA201811086753Nut · looseDURING FLIGHT WITH RADAR CONTROL PANEL SETTINGS THE SAME FOR LEFT AND RIGHT AND IN AUTO, THE TWO RADAR PRESENTATIONS DO NOT MATCH. OBSERVED WEATHER SEEMS TO MATCH LEFT (CAPT) DISPLAY WHILE THE RIGHT IN AUTO SEEMS TO HAVE TILT TOO FAR DOWN DISPLAYING A LOT OF RNov 6, 2018 · N558AS · Boeing 737890 · Weather Radar SystemSDR ASAA2018102326596Fcu · faultyDURING INFLIGHT START FOR CSS WE RECEIVED A FAULT LIGHT AND THE APU SHUT DOWN TWICE AT FL380, APU STARTED SUCCESSFULLY AT FL350. GROUNDED - YES. ACCOMPLISHED BITE OF APU FOUND FAULTS IN FAULT HISTORY NO ACCELERATION SHUTDOWN MESSAGE 49-41010. OVERTEMP SHUTDOWNOct 23, 2018 · N558AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2018101726516Battery · lowAFT RIGHT EMERGENCY LIGHTS DO NOT REMAIN ON FOR 15 MINS. GROUNDED - YES. REMOVED AND REPLACED AFT RIGHT EMGR LIGHT BATT PACK OPS NML REQ ENDURANCE TEST. AFT RIGHT EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-06.Oct 17, 2018 · N558AS · Boeing 737890 · Emergency LightingSDR ASAA2018101526465Fmc · malfunctionedFMC R FAILED IN FLIGHT, RAN QRH, BOTH ON FMC L FOR REMAINDER OF FLIGHT. GROUNDED - YES. CYCLED FMC POWER & NORMAL OPS RESTORED. R FMC LOGGED GLITCH TIMER INTERMITTENT FAULT WITH SEVERAL ASSOCIATED DATA BASE MISMATCH FAULTS. VERIFIED CORRECT DATABASES LOADED INOct 12, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018101526464Fmc · inoperativeFMC R FAILED IN FLIGHT, RAN QRH, BOTH ON FMC "L" FOR REMAINDER OF FLIGHT. GROUNDED - YES. REMOVED AND REPLACED RT FMC COMPUTER REF AMM 34-61-02-400-801, OPS NML REF AMM 34-61-00-710-801. CROSS LOADED SOFTWARE AND ADJUSTED PERF FACTORS REF AMM 34-61-00-800-801.Oct 12, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018100926443Computer · malfunctionedRECEIVED SINGLE FMC INOP WARNING LIGHT AND A VTK FLAG ON F/O SIDE. FMC SWITCH ON "BOTH ON L". GROUNDED - YES. F/O FMC INOP. REPLACED FMCS COMPUTER, REF B737-800 AMM 34-61-02. CROSSLOADED SOFTWARE AND ADJUSTED PERF FACTORS PER SAME. FMCS OPS NML.Oct 9, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018100926425Igniter · failedRT ENGINE (NR 2) DURING ENGINE START, NO LIGHT OFF. GOOD FUEL FLOW AT START LEVER ON - BUT WOULD NOT LIGHT OFF (ZERO EGT). GROUNDED - YES. CONFIRMED NR 2 ENGINE LT IGNITION FAILED VIA AUDIBLE TEST REF AMM TASK 74-00-00-750-801-F00. REPLACED NR 2 ENG LT IGNITEROct 8, 2018 · N558AS · Boeing 737890 · Spark Plug/IgniterSDR ASAA2018091926194Panel · damagedDURING NR 1 ENG INLET AND FAN BLADES DETAILED INSP. FOUND NR 5 STRUT PANEL DAMAGED AT FWD LWR FASTENER BEING LOOSE. AFT LOOKING FWD (M) APPROX 5 O'CLOCK POS. GROUNDED - YES. REMOVED AND REPLACED FAN DUCT PANEL PER AMM 72-23-07/401. NO OTHER DEFECTS NOTED AT THSep 19, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018091026072Wire Harness · tornWHILE PERFORMING TASK CARD, FOUND CJ10 HARNESS OUTER SHEATH ON RT ENGINE TORN. GROUNDED - YES. PERFORMED TEMPORARY REPAIR ON CJ10 HARNESS OUTER SHEATH USING ALUMINUM TAPE AND LOCKWIRE. REF AMM 70-70-01. PLT CREATED DUE TO REPAIR BEING TEMPORARY UNTIL NEXT ENGISep 8, 2018 · N558AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA201808135746Fmc · lockedFMC LOCKED, WILL NOT ALLOW INPUT. ACFT GROUNDED. TROUBLESHOT TO A FAILED LEFT FMC BOX SWAPPED DURING TROUBLESHOOTING. REMOVED AND REPLACED THE LEFT FMC COMPUTER, CROSS LOADED SOFTWARE, BOTH FMC OPS CHECKED GOOD IAW AMM 34-61-02 PB400.Aug 11, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA201808135747Fmc · malfunctionedLEFT FMC FAILED. ACFT GROUNDED. PERFORMED FIM 34-61, TASK 807, FMC FAULT ISOLATION. RESET FMCS COMTR1 CIRCUIT BREAKER. FMC WORKING. WAS AN INTERMITTENT FAULT.Aug 10, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018081085732Display · malfunctionedMAP DISPLAYED ON FIRST OFFICER`S NAV DISPLAY. RAN QRH AND RETURNED TO NORMAL. ACFT GROUNDED. COMPLIED WITH FIM 34-61, TASK 801, AND 806 NO FAULTS FOUND. OK FOR SERVICE.Aug 8, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018071625411Circuit Breaker · openNR 2 ENGINE CONTROL CAUTION LIGHT ILLUMINATED AFTER ENGINE START. GROUNDED - YES. FOUND NR 2 ENGINE RUN/PWR C/B OPEN. ACCOMPLISHED C/B RESET PROCEDURE. REF MM 20-60-01-860-801. NR 2 EEC LOGGED 73-31352. APL VOLTAGE TO THE EEC OUT OF RANGE. BOTH EEC BITE CK NOJul 14, 2018 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2018062425197Unknown · malfunctionedFA REPORTS IN FLIGHT AFT CABIN IS VERY COLD EVEN WITH THE AFT CABIN CONTROL TURNED TO WARM AND INDICATES WARM AIR IN THE DUCT. ON THE GROUND APU RUNNING AND AFT CABIN CONTROLLER ON FULL WARM FA STILL REPORTS THE AIR IS LUKE WARM AT BEST. GROUNDED - YES. TEMP CJun 24, 2018 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA201806255175Spacer · debondedNR 1 ENGINE HAD EIGHT DEBONDED FAN BLADE SPACERS. ACFT GROUNDED. REPLACED THE FAN BLADE SPACERS IAW TC 78472002.Jun 22, 2018 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018041624260Wire Harness · damagedNR 1 ENGINE FIRE DETECTOR LOOP MW0326 HAS A BROKEN TERMINAL LUG. ACFT GROUNDED. REMOVED MW0326 HARNESS IAW AMM 26-11-02-000-802. INSTALLED A SERVICEABLE WIRE HARNESS IAW AMM 26-11-02-400-802, STEPS 5A-F(1A-1E). OPS CHECKED SATISFACTORY.Apr 16, 2018 · N558AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2018041624258Computer · malfunctionedSPEED TRIM FAILED AND MACH TRIM FAILED, COMES ON WITH M/C RECALL AND RESET. ACFT GROUNDED. FOUND FCC-A FAULTED DURING POWER TRANSFER. CYCLED POWER TO FCC-A & PERFORMED DFCS BITE CHECK, CURRENT STATUS & FLT DIRECTOR TEST GROUP 12 IAW FIM 22-11 TASK 801. PEApr 16, 2018 · N558AS · Boeing 737890 · Autopilot SystemSDR ASAA2018041624257Flight Dir · malfunctionedCAPTAIN`S FD ANNUNCIATED. ACFT GROUNDED. FOUND FCC-A FAULTED DURING POWER TRANSFER. CYCLED POWER TO FCC-A & PERFORMED DFCS BITE CHECK, CURRENT STATUS & FLT DIRECTOR TEST GROUP 12 IAW FIM 22-11 TASK 801. PERFORMED FCC LRU REPLACEMENT TEST IAW FIM 22-11 TASApr 16, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018022523682Lens · missingROW 16 ABC LOWER EMERGENCY EXIT LIGHT LENS MISSING. ACFT GROUNDED. INSTALLED A NEW LENS IAW AMM 33-51-01.Feb 25, 2018 · N558AS · Boeing 737890 · Emergency LightingSDR ASAA2018020423392Light · inoperativeR-2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. GROUNDED - YES. RELAMPED PER AMM 33-51-04-960-801. OPS CHECK GOOD.Feb 4, 2018 · N558AS · Boeing 737890 · Emergency LightingSDR ASAA2018012923321Fmc · malfunctionedLEFT FMC VTK AFTER LANDING, MAP RETURNED AFTER 10 SECONDS. ACFT GROUNDED, FIM 34-61 TASK 801 NO CURRENT FAULTS, FMC LEFT G LEG SHOWS PGM FAULT. PERFORMED FIM 34-61-00-810-836, AND FIM 34-61 TASK 807 FMC OPS TESTED NORMAL.Jan 29, 2018 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018012023232Hf Comm · malfunctionedUNABLE TO TUNE AND TRANSMIT HF NR 1 WHILE INFLIGHT BOTH HF RADIOS TESTED NORMAL ON GROUND. WE CAN HEAR STATIC ON HF NR 1 BUT CANNOT TRANSMIT DURING FLIGHT HF NR 2 WORKS NORMAL. GROUNDED - YES. PERFORMED BITE CHECK OF NR 1 HF COMM SYSTEM PER FIM 23-11 TASK 801 Jan 20, 2018 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA2018011323152Warning Light · false activationON RECALL, CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. DUCT TEMP NORMAL. LIGHT EXTINGUISHED ON RESET. ACFT GROUNDED. PERFORMED AMM 21-61-00, SHOWED THE NR 2 CONTROLLER FLT DECK LT ZONE TEMP. RESET AND REPERFORMED BITE, ALL PASSED, NO FAULTS AND NO HISTORYJan 13, 2018 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2018011123160Transceiver · failedGROUND CHECK OF THE NR 1 AND 2 HF SYSTEM, WAS OK. AIRBORNE NR 1 HF COULD NOT TRANSMIT. CAN HEAR SIDE TONE AND ATC BUT CANNOT TRANSMIT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 HF TRANSCEIVER. OPS CHECKED GOOD, NO DEFFECTS NOTED IAW AMM 23-11-21-000-801 Jan 11, 2018 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA2017123023063Start Valve · failedNR 1 ENGINE WILL NOT START. GOOD DUCT PRESSURE. CB IN, NO START VALVE OPEN LIGHT. GROUNDED - YES. REMOVED NR 1 ENGINE START VALVE PER AMM 80-11-03-000-801-F00. INSTALLED NEW START VALVE PER AMM 80-11-03-400-801-F00. GND VERIFICATION AND LEAK CHECK GOOD PER AMMDec 30, 2017 · N558AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2017122523026Warning Message · false activationNR 1 ENGINE ECONOMIC FAULT 73-11371, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. PERFORMED EEC BITE IAW FIM 73-00, TASK 801. FAULT 73-11371 IS NOT ACTIVE IN RECENT FAULTS. PERFORMED FIM 73-11, TASK 801 WITH ENGINE RUNNING, T49.5 PARAMETERS ARE S1 413,Dec 25, 2017 · N558AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017121522927Hf Comm · malfunctionedNR 1 HF TRANSMITTER INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED HF OPS TEST IAW AMM 23-11-00. OPS NORMAL. ACCOMPLISHED FIM 23-11 TASK 806, HF COMM SYSTEM TRANSMITTED AND RECEIVING PROBLEM. ABLE TO COMMUNICATE WITH SFO FREQ 5.547 BUT THE REPLY WAS UNCLEAR. COMMDec 15, 2017 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA2017112922739Exciter · failedAPU WILL NOT START, MAINT MESSAGE 49-41245 "APU START CONVERTER UNIT SHOWS UNDERVOLTAGE". NOTE: SCU CAN BE HEARD NORMALLY FOR APPROX 10 SECONDS UNTIL "NO ROTATION SHUTDOWN" OCCURS AND ASSOCIATED MAINT MESSAGE 49-41042. GROUNDED - YES. REMOVED AND REPLACED IGNINov 29, 2017 · N558AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2017112822722Eec · failedWHILE ACCOMPLISHING T/C 78273000, FOUND FAULTS ON THE NR 2 ENGINE, MULTIPLE FLIGHT LEGS: 75-10522, 75-10292, 73-10042, 73-21282, 73-10622, 75-10572, 75-10422, 75-10372, 73-10322, 73-10012, AND 73-10152. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED THE NR 2 EENov 28, 2017 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2017111222549Actuator · failedLEFT SPAR VALVE LIGHT ILLUMINATED BRIGHT ON LANDING, WENT OFF AFTER 20 SECONDS. ACFT GROUNDED. REMOVED AND REPLACED LEFT SPAR VALVE ACTUATOR IAW AMM 28-22-11. GROUND VERIFICATION ACCOMPLISHED OPS CHECK GOOD.Nov 12, 2017 · N558AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2017101422260Transition Panel · corrodedAFT CARGO BAY RIGHT SIDE TRANSITION PANEL CORRODED FROM BS 727D - 727J. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED IAW SRM 53-00-53-2R-S.Oct 14, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017101322362Bulkhead Web · corrodedAFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 13 CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS. REMVOED & REPLACED THE BULHEAD WEB IAW SRM 51-40-02 & DWG 147A5700, REV A.Oct 13, 2017 · N558AS · Boeing 737890 · Fuselage Main, BulkheadSDR ASAA2017101122361Web · corrodedMAIN CABIN AT BS 989, LBL 30 WEB CORRODED. GROUNDED - YES. REMOVED CORROSION FROM WEB REF SRM 51-10-02 (LENGTH -1.9" X .84" WIDE) BEYOND ALLOWABLE LIMITS MORE THAN 50% LOSS OF MATERIAL (ORIG.020, REMOVED .012, REMAINING .008 REF BAC DWG 147A5712) REMOVED & REPOct 11, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017101122285Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 380 - 400, LBL 3. ACFT GROUNDED. REMOVED THE FLOOR SUPPORT UPPER ANGLE IAW SRM 51-40-02. LOCATED, AND DRILLED IAW SRM 51-40-05, AND INSTALLED IAW SRM 51-40-02.Oct 11, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017101122284Floor Support · crackedFLOOR SUPPORT UPPER FLANGE CRACKED, BETWEEN BS 380 - 400, RBL 7. ACFT GROUNDED. REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02. LOCATED, AND DRILLED A NEW FLOOR SUPPORT IAW SRM 51-40-05, AND INSTALLED IAW SRM 51-40-02.Oct 11, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017101122249Web · corrodedAFT CARGO DOOR CUTOUT, LOWER SILL WEB CORRODED AND HAS LARGE AREAS OF BARE METAL AND PEELING PAINT. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED THE LOWER SILL WEB IAW SRM 51-40-02, DWG 146Oct 11, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017101122162Floor Support · corrodedBS 340, LBL 12 FLOOR SUPPORT CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 141A5400, AND SRM 51-40-02.Oct 11, 2017 · N558AS · Boeing 737890 · Fuselage Miscellaneous Structure
Back to N558AS