N529AS

Service difficulty reports · 344

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 = 'N529AS' 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 ASAA2017031420180Starter · failedSTART ABORTED ON NR 2 ENGINE NO ROTATION ON N2. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE STARTER, REF AMM 80-11-01. OPS CHECK GOOD.Mar 14, 2017 · N529AS · Boeing 737890 · Engine StarterSDR ASAA2017030620034Shim · wornALL 24 FAN BLADE SHIMS ON THE NR 1 ENGINE ARE WORN. ACFT GROUNDED. REMOVED AND REPLACED THE SHIMS IAW T/C 78472002.Mar 6, 2017 · N529AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017030420005Control Panel · malfunctionedWITH MAIN PANEL LIGHTS LESS THAN FULL BRIGHT, IAS & MACH DIGITS FLICKER. ACFT GROUNDED. REMOVED & REPLACED THE AUTOPILOT MODE CONTROL PANEL IAW AMM 22-11-34. SYSTEM OPS CHECKED NORMAL, LAND VERIFY & HGS SENSOR TEST IAW AMM 34-36-00 PASSED.Mar 4, 2017 · N529AS · Boeing 737890 · Autopilot SystemSDR ASAA2017021319803Wire Harness · damagedNR 1 ENGINE J9 HARNESS DAMAGED. PUNCTURED INTO HARNESS CORE NEAR CJ9 CONNECTION. ACFT GROUNDED. ALT DEACTIVATION USED IAW CH 5 TABLE 3 ITEM 1 AND 3 05-07-01. REMOVED AND REPLACED THE J9 HARNESS IAW AMM 73-21-06. ALL TESTS PASSED. OPS CHECKED GOOD.Feb 13, 2017 · N529AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2016123019213Battery Pack · failedBATTERY PACKS M1671, M1672, M1673, M1675, AND M1694 FAILED CAPACITY TEST REF T/C 78233001. GROUNDED - YES. REPLACED BATTERY PACKS AT M1671, M1672, M1675, AND M1694. REPLACED BATTERY AND CHARGER ASSEMBLY AT M1673. OPERATIONAL TEST OK, REF AMM 33-51-06/201.Dec 30, 2016 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2016110718587Valve · failedAFTER ENGINE START RECALL RECEIVED A PACK CAUTION LT LEFT PACK. ACFT GROUNDED. FOUND BAD AFT TRIM MOD VALVE. REMOVED AND REPLACED THE VALVE & OPS NORMAL & FAULT CLEARED IAW AMM 21-62-01.Nov 7, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016110218549Hmu · failedFOUND FAULT CODE 73-31161, THE MECHANICAL OVERSPEED PROTECTION SIGNAL IS OUT OF RANGE, A LONG TERM FAULT, ON THE NR 1 ENGINE BITE TEST FOR LEGS 1-7. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE HMU. TEST 3A & 12 PASS, NO LEAKS NOTED. BITE CHECK PASSEDNov 2, 2016 · N529AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016102718499Warning Flag · false activationDURING PRE-FLIGHT "FD" FLAG ON CAPTAIN`S PFD. ACFT GROUNDED. HAD TO CYCLE FCC A DC CIRCUIT BREAKER BEFORE DFCS WILL GO INTO BITE. CURRENT STATUS PASSED. ACCOMPLISHED DFCS LRU INTERFACE TEST ONLY FOR FCC A, TEST PASSED, IAW AMM 22-11-33.Oct 27, 2016 · N529AS · Boeing 737890 · Autopilot SystemSDR ASAA2016101018254Control Panel · failedHEADING SELECT KNOB ON MCP IS BROKEN. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34. ACCOMPLISHED LWMP TESTS, DFCS LRU INTERFACE TEST FOR MCP, LAND VERIFY TEST AND HGS SENSOR TEST FOR FCC/AT. ALL TESTED GOOD IAW AMM 22-11-34, AMM 22-11-00, AND SMM 34-36-00.Oct 10, 2016 · N529AS · Boeing 737890 · Autopilot SystemSDR ASAA2016100318201Engine · faultedWHILE ACCOMPLISHING T/C 78273000 FOUND ECONOMIC FAULT 77-10852 (THE BOTTOM RIGHT EGT SIGNAL IS OUT OF RANGE. ACFT GROUNDED. NO RECENT FAULTS ON NR 2 ENGINE IAW T/C 78273000.Oct 3, 2016 · N529AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2016082517816Fmc · malfunctionedFMC DISAGREE ON LANDING ROLL, VTK ON CAPTAIN'S ND, FMC PROMPT MISSING ON MCDU MENU PAGE. NO ACTION TAKEN. ALL RETURNED TO NORMAL DURING TAXI TO GATE. ACFT GROUNDED. FMC NUISANCE ERROR NOTED, NO MX REQUIRED, REF REQUIRED, IAW AMM 34-61-00-860-801.Aug 25, 2016 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016072917560Bleed Valve · failedWHILE ACCOMPLISHING BLEED AIR CROSSOVER TEST FOR REPAIR CONFIRMATION OF LT ENGINE LOW DUCT PRESSURE, NOTED RT ENGINE DUCT PRESSURE DID NOT RISE ABOVE 15 PSI UNTIL 50% N1, ALL OTHER PARAMETERS NORMAL. SUSPECT NR 2 ENGINE HIGH STAGE REGULATOR FAILURE. ACFT GROJul 29, 2016 · N529AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2016072917549Warning Message · false activationAUTO FAIL AND ALTERNATE LIGHTS ILLUMINATED ON PRESSURIZATION PANEL. DISCOVERED DURING PRE-FLIGHT. ACFT GROUNDED. FOUND FAULT DISPLAYED ON NR 1 DCPC. PERFORMED FIM 21-31 TASK 801. CLEARED FAULTS PER FIM PROCEDURE AND NO EXISTING FAULTS. BITE TESTS OK. GROUNJul 29, 2016 · N529AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2016072217473Valve · failedENROUTE, RIGHT PRESSURE SHOWS 45 PSI AND LEFT SHOWS 25 PSI (FL340). ACFT GROUNDED. R & R THE NR 1 ENGINE PRE-COOLER CONTROL VALVE, IAW AMM 36-12-02-000-801 AND 36-12-02-400-801. LEAK & OPS CHECKED GOOD. ACCOMPLISHED NR 1 ENGINE BLEED AIR SYS HEALTH CHECK Jul 22, 2016 · N529AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2016071517374Modulating Valve · malfunctionedA/C PACK LIGHT ILLUMINATED FOR NR 2 PACK. EXTINGUISHES WITH M/C RESET. ACFT GROUNDED. R & R ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-21, PERFORMED ZONE TRIM AIR MODULATING VALVE INSTALLATION BITE TEST, NO FAULT NOTED, AND LEAK CHECK FOUND NORMAL IN REF Jul 15, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016071417377Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED DURING RECALL AND EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE RT TEMP CONTROLLER BITE, OPS CHECKED NORMAL, NO FAULTS.Jul 14, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016070317225Lamp · failedEMERGENCY LIGHT AREA LIGHT (AISLE FLOODLIGHT) INOP AT ROW 20 LEFT. ACFT GROUNDED. REPLACED THE LAMP AND TESTED IAW AMM 33-51-03-960-801, OPS NORMAL.Jul 3, 2016 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2016070317224Bulb · failedEMERGENCY LIGHT EXTERIOR SLIDE LIGHT AT R-1 DOOR INOP. GROUNDED - YES. RELAMPED AND TESTED PER B737-800 AMM 33-51-04-960-801 - OPS NORMAL.Jul 3, 2016 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2016070217212Controller · faultedON PREFLIGHT AUTO FAIL ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. CYCLED MODE CONTROL ON PRESSURE PANEL AND AUTO FAIL LIGHT EXTINGUISHED. BITE CHECK OF PRESSURE CONTROLLER NR 1 & 2 NORMAL WITH NO FAULTS LOGGED IAW FIM 21-31 TASK 827.Jul 2, 2016 · N529AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2016060416942Fmc · malfunctionedENROUTE RECEIVED A SINGLE FMC OPERATION MESSAGE ON THE CDU SCRATCH PAD WITH VTK DISPLAYED ON THE F/O'S ND MAP DISPLAY. FOLLOWED THE QRH AND PLACED THE FMC SWITCH IN "BOTH ON L". CHECKED THE FMC INFO ON POS SHIFT PAGE 3/3 AND FOUND THE FMC -R IS BLANK. ACFT GRJun 4, 2016 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016052816863Sensor · dirtyCONTROLLER CABIN TEMP IS DIFFICULT TO CONTROL. SOME ROTATION OF TEMP MAKE IT TOO HOT OR TOO COLD. ACFT GROUNDED. CLEANED SENSORS IN COCKPIT, FWD CABIN. TEMP CONTROLLER NOT FAULTING. OPS CHECK GOOD IAW FIM 21-62, TASK 814.May 28, 2016 · N529AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016052616860Actuator · failedLT PACK LIGHT ILLUMINATED UPON RECALL AFTER ENGINE START. ACFT GROUNDED. ATTEMPTED TO DO BITE ON NR 1 IAW FIM 21-62, TASK 301 NR 1 PTC DID NOT OPERATE. FOUND RAM AIR MOD LT C/B P6-4 OUT, C/B WOULD NOT RESET. REF AMM 20-60-01, NO DEFECTS NOTED ON C/B. REMOVMay 26, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016040516246Actuator · failedRIGHT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED RT PACK TEMP CONTROL BITE, REF AMM 21-62, TASK 801, RAM AIR ACTUATOR LOGGED ON RECENT FLIGHTS. DUE TO REPEATED WRITE UPS, R & R RT RAM AIR INLET ACTUATOR, REF AMM 21-51-21. RAM AIR INLET ACTUAApr 5, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016040416234Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL AND EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED RT PACK/ ZONE TEMP CONTROLLER BITE TEST, REF AMM 21-61-00-700-806-002. FAULT LIGHT CLEARED ON VERIFY. CLEARED WITH RESET.Apr 4, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016032116044Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL DURING DESCENT CHECKLIST. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST, REF AMM TASK 21-61-00-700-806-002, ON RT PACK AND FOUND RAM AIR ACTUATOR LIGHT ILLUMINATED AFTER BIT BUTTON PUSHED, CONTINUED TEST AMar 21, 2016 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016031515943Fmc · malfunctionedFMC WOULD NOT SELECT TO POWER OR ALLOW MANUAL SELECTION OF TO POWER. ACFT GROUNDED. RESET FMCS COMPUTER 1 AND 2 CB'S, REF FIM TASK 34-61, TASK 836 AND ACARS CMU-1 AND CMU/ACARS DC C/B'S REF FIM TASK 23-27, TASK 815. NO HELP. FOUND TAT TEMP NOT DISPLAYING ANMar 15, 2016 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016022115604Warning Light · false activationON RECALL THE CONTROLLER CAB ZONE TEMP LIGHT ILLUMINATES. IT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. VERIFIED CONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON MASTER RECALL, EXTINGUISHING WITH MASTER RESET. PERFORMED PACK/ZONE TEMP CONTROL BITE TEFeb 21, 2016 · N529AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016022015595Hmu · failedSHORTLY BEFORE TAKEOFF, NR 1 ENGINE CONTROL LIGHT COME ON. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROL BITE REF 73-00, TASK 801 FOUND FAULT CODE 75-10581. REF FIM 75-23, TASK 801. PERFORMED TEST 12 ACTUATORS TEST. TEST PASSED: NO FAULTS, FAULT IS INTEFeb 20, 2016 · N529AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2016021115419Control Panel · failedWINDOW LIGHTED NUMERALS CONSTANTLY PULSING ON MCP. ACFT GROUNDED. CONFIRMED FAULT. R & R DFCS MCP REF AMM 22-11-34, OPS CHECK NORMAL. ACCOMPLISHED DFCS LRU INTERFACE TEST MCP, GP 32, REF AMM 22-11-34, DFCS LAND VERIFY TEST, GP 49, REF AMM 22-11-00 AND HGS SEFeb 11, 2016 · N529AS · Boeing 737890 · Autopilot SystemSDR ASAA2016020315237Connector · looseHISTORY OF FAULT CODE 75-10581, TBV DEMAND AND POSITION SIGNAL DISAGREE. ACFT GROUNDED. ACCOMPLISHED ELECTRIC ENGINE CONTROL TEST AND ACTUATORS TEST ON NR 1 ENGINE REF AMM 71-00-00-700-807-F00, NO FAULTS LOGGED. ACCOMPLISHED FIM 75-23, TASK 801, ALL RESISTAFeb 3, 2016 · N529AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2016012815195Warning Light · false activationNR 1 ENGINE CONTROL LIGHT ILLUMINATED ON TAXI OUT. ACFT GROUNDED. ACCOMPLISHED ELECTRONIC ENGINE CONTROL BITE IAW FIM AMM 73-00-TASK 801. ACCOMPLISHED FIM AMM 75-23-TASK 801. TEST PASSED NO FAULTS MESSAGE. OK FOR SERVICE.Jan 28, 2016 · N529AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2015122814512Fmc · malfunctionedIN FLIGHT MOMENTARY FMC (RIGHT) FAIL. RESTORED ITSELF. ACFT GROUNDED. VERIFIED LAST FLT RT FMC FAILED. ACCOMPLISHED FMC SYSTEM OPS TEST, TEST PASS REF MM 34-61-00-710-801.Dec 28, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015121714306Warning Light · false activationDURING AFTER START CHECK, ON MASTER CAUTION RECALL, THE CONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED. THE ZONE TEMP LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. FOLLOWED QRH NO FURTHER ACTION REQUIRED. ACFT GROUNDED. PERFORMED PACK/ZONE BITE TESDec 17, 2015 · N529AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015112113904Fmc · failedLEFT FMC FAILED DURING THE FLIGHT. ACFT GROUNDED. R & R LT FMCS COMPUTER IAW AMM 34-61-02. ACCOMPLISHED SOFTWARE LOAD IAW AMM 34-61-00 VIA CROSSLOAD. SYS OPS CHECKS NORMAL IAW AMM 34-61-00.Nov 21, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015102713541Fmc · failedLEFT FMC FAILURE UNABLE TO RESTORE AFTER QRH PROCEDURE. ACFT GROUNDED. VERIFIED DISCREPANCY, OPENED, CLOSED 2CBS FOR LT FMC, REF 34-61, TASK 836. FMC RETURNED TO NORMAL. ACCOMPLISHED LT FMC BITE 34-61, TASK 801. FOUND MMR, RT ILS FAULT. ACCOMPLISHED FIM Oct 27, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015101413499Warning Light · false activationLEFT PACK LIGHT ILLUMINATES WITH RECALL EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. VERIFIED AND RESET CONTROL BOXES 1 AND 2 REF PLAC ON FRONT OF CONTROL BOX, GROUND VERIFICATION NORMAL.Oct 14, 2015 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015100313305Fmc · malfunctionedON CAPT FMC THE EXEC LIGHT & THE OFFSET LIGHT FLASH BRIGHT THEN DIM AT APPROXIMATELY 1 TO 2 SECOND INTERVALS WHEN THE LIGHTS TEST SWITCH IS IN THE DIM POSITION. IN THE BRIGHT POSITION THE FMC LIGHTS OPERATE NORMAL, BRIGHT. AFTER 3 HRS OF FLIGHT THE LIGHTS SOct 3, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015092113159Fmc · failedFOLLOW INITIALIZATION TAKES ABOUT 30 MINS TO RECEIVE DATA TO FMC'S. DURING PROGRAMING PROCESS A MESSAGE SHOWS UP: "FMCS FILE SYSTEM DOWNLOAD UTILITY INSERT INTO DATA LEADER DISK FORMATTED BY THE PC UTILITY OR PRESS HERE TO EXIT". ACFT GROUNDED. NR 1 & NR 2 FSep 21, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015092113151Warning Message · false activationFMC DISAGREE DISPLAYED ON TAXI. ACFT GROUNDED. ACCOMPLISHED QRH, MESSAGE NO LONGER ILLUMINATED.Sep 21, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015090612948Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RAN CHECKLIST QRH, FMC DISAGREE NO LONGER DISPLAYED.Sep 6, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015090212917Lens · missingEXIT SIGN OVER THE L-2 DOOR IS MISSING ITS COVER. ACFT GROUNDED. INSTALLED A NEW EXIT SIGN LENS AT L-2 DOOR, OPS CHECKED NORMAL REF AMM 33-51-01.Sep 2, 2015 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2015081212860Lens · missingL-2 DOOR HAS MISSING EXIT PLASTIC SIGN. ACFT GROUNDED. REINSTALLED & SECURED A NEW LENS.Aug 12, 2015 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2015081212862Warning Message · false activationLEVEL FL380 IN CRUISE. RIGHT FMC MASTER. LEFT FMC P/RST LIGHT ILLUMINATED FOLLOWED BY LT MAP DISPLAY DATA REMOVED AND "VTK" ILLUMINATED ON NAV DISPLAY. LEFT CDU MENU DISPLAY WITH NO FMC ON MENU. AFTER 2 MIN ALL DATA AND INDICATIONS REBUILT ITSELF TO NORMALAug 12, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015080312706Fmc · failedLEFT FMC FAILURE ENROUTE. UNABLE TO RESTORE DUAL FMC OPS. RIGHT FMC NORMAL. ACFT GROUNDED. SUCCESSFULLY PERFORMED FMCS OPS TEST IAW AMM 34-61-00-710-801. NO FAULTS FOUND AND NO MAINTENANCE HISTORY WITHIN THE PAST 30 DAYS.Aug 3, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015062212188Eec · failedNR 2 ENGINE CONTROL LIGHT ILLUMINATED AFTER ENGINE START. ACFT GROUNDED. ENGINE CONTROL LIGHT OUT AFTER BLOCK IN. ACCOMPLISHED BITE IAW FIM 73-00, TASK 801- FOUND FAULT (3) CODES 73-21282, 73-10012, 73-10042 IN "RECENT FAULTS", FAULT HISTORY. AT THIS POINTJun 22, 2015 · N529AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015061112077Warning Message · false activationFMC DISAGREE, ACFT GROUNDED. RESOLVED IAW QRH.Jun 11, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015061112073Hf Comm · malfunctionedNR 1 HF RADIO WILL TRANSMIT BUT NOT RECEIVE. NR 2 HF RADIO WILL TRANSMIT BUT ONLY 2 X 2 RECEPTION. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. ACCOMPLISHED GOOD COMMUNICATION ON BOTH NR 1 & NR 2 HF SYSTEMS WITH FREQ 8.933. SELCAL ON BOTH HF SYSTEMS OPS NORJun 11, 2015 · N529AS · Boeing 737890 · HF Communications SystemSDR ASAA2015041511502Channel · corrodedIN THE AFT CARGO FLOOR AREA , LT TRANSITION PANEL CORRODED. BS 727C-BS 767, BL LBL24 -BL LBL30, STR 25L -STR 26L. ACFT GROUNDED. REMOVED CORROSION FROM TRANSITION PANEL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REPAIR TRANSITION PANEL IAW SRM 53-00-53,Apr 15, 2015 · N529AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015041511474Channel · crackedIN THE AFT PIT FLOOR AREA , RIGHT TRANSITION PNL CRACKED . DOT ATTACH, BS 727J - BS 727J, BL RBL24 - BL RBL30, STR 25R - STR 26R. GROUNDED - YES. REMOVED CRACKED TRANSITION PANEL FROM AFT PIT RH STA 727E+10 TO 767, FABRICATED NEW TRANSITION PANEL AND 2EA SPLIApr 15, 2015 · N529AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015041511473Channel · corrodedIN THE AFT PIT FLOOR AREA , LEFT TRANSITION PNL CORRODED. DOT ATTACH, BS 727C - BS 767, BL LBL24 - BL LBL30, STR 25L - STR 26L. GROUNDED - YES. REMOVED CORROSION FROM TRANSITIONPANEL FROM STA 727L TO 747+10 LBL 24, ORIGINAL THICKNESS .040 MAT REMOVED .003 REMAApr 15, 2015 · N529AS · Boeing 737890 · Fuselage Miscellaneous Structure
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