N596AS
Service difficulty reports · 549
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 = 'N596AS' 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 = 'N596AS' 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 ASAA2026040665524Stop Fitting · gougedWHILE PERFORMING AFT ENTRY DOOR HEALTH CHECK FOUND STOP PIN FITTING GAUGED AT TOP FWD CORNER. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO AFT ENTRY DOOR P/N 147A6116-26 S/N 002595 UPPRER FWD DOOR STOP FITTING P/N 147A6128-53 IAW EA 800-SDR ASAA2026040565340Battery Pack · inoperativeEMERGENCY LIGHT AT RIGHT HAND SIDE BETWEEN ROWS 19-24 AND OVERWING AFT AND BEHIND WING FAILED CAPACITY TEST. SRXR430X. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK EMERGENCY LIGHT AT RIGHT HAND SIDE BETWEEN ROWS 19-24 AND OVERWING AFT AND BEHIND WING (M16SDR ASAA2025053158386Power Supply · inoperativeEMERGENCY EXIT LIGHT BY L1 DOOR DAMAGED AND INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY ASSY M1670 AND M1675 REF BOEING AMM TASK 33-51-06-960-806. OP TEST GOOD WITH EMERGENCY LIGHTS ILLUMINATING AS REQUIRED. NO FURTHER DEFECTS.SDR ASAA2025020955894Roller · brokenR1 DOOR DIFFICULT TO CLOSE AND SEAL PROPERLY. GROUNDED - YES. REMOVED BOLT & WASHER ON THE DOOR LOCK CHANNEL REF AMM 52-41-00 STEP I STEPS 1-5 FOUND CENTER ROLLER BROKEN. ADJUSTED GUIDE ARM (TWO FLATS EXTENDED) REF AMM 52-41-00-820-801 STEP I. ADJUSTED CENTERISDR ASAA2024080351555Door · leakingL1 DOOR VERY DIFFICULT TO CLOSE AND MAKES HIGH PITCH WHISTLE NOISE AT CRUISE. GROUNDED - YES. PERFORMED CLOSING DOOR(L1) HANDLE TORQUE TEST REF AMM 52-11-00-700-804 FOUND CLOSING TORQUE OUT OF LIMITS. VERBAL FROM CREW, THROUGH SEAMC PETER L1 DOOR WHISTLE DOES SDR ASAA2024071751187Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH M1674 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1674 IAW B737-800 AMM 33-51-06-960-806 TEST GOOD.SDR ASAA2024062650844Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ZEE ANGLE IS CORRODED. STA 987-1006 RBL 32. GROUNDED - YES. REMOVED AND REPLACED, AFT WET AREA FLOOR SUPPORTS ZEE ANGLE STA 987-1006 RBL 32 IAW B737-800, DOCUMENT NUMBER: 147A5700, TYPE: DWG ID: 0063 REV:-, SRM 51-40-05, SUPPORT INSTSDR ASAA2024062650842Floor Support · corrodedAFT WET AREA FLOOR SUPPORT ZEE ANGLE IS CORRODED AT STA 98-1006 LBL 32. GROUNDED - YES. CORROSION FOUND OUT OF LIMITS, 100% MATERIAL LOSS IAW B737-800 SRM 53-70-51-1A-1, DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05, DOCUMENT NUMBER: 147A5700 TYPE: DWG SDR ASAA2024061951206Skin · puncturedL-1 DOOR DURING REMOVAL OF AFT FRAME FOUND INNER MIDDLE SKIN DAMAGED NEAR PRISM CUTOUT. GROUNDED - YES. REPAIRED INNER MIDDLE SKIN DAMAGE IAW EA CMPT-52EA-27220 REV: 00 DATED 07/10/2024.SDR ASAA2024061251204Door Frame · wornL-1 DOOR AFT FRAME IS GOUGED AT CENTERING GUIDE PLATE. GROUNDED - YES. CHECKED LIMITS, ORIGINAL FRAME OUT OF LIMITS IAW B-737-800 SRM 52-10-02-1A-1. ORIGINAL FRAME THICKNESS .071,MAT REMAINING .050,REMOVED .021 LIMIT OF REMOVED MAT.IS .007. RECEIVED NEW FRAME,SDR ASAA2024061150725Floor Panel · delaminatedPASSENGER FLOOR PANEL P/N 141A5810-755 HAS DELAM/CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF MAIN CABIN FLOOR PANEL 141A5810-755 DELAMINATED SKIN AND CORRODED INSERTS IAW ASA B737-800 SRM 53-00-50-2R-0G AND REPAIRS 1 AND 4.SDR ASAA2024060750912Shield · corrodedFWD PIT DOOR SURROUND AFT SHIELD CORRODED. GROUNDED - YES. REMOVED CORR. FROM FWD PIT DOOR SURROUND AFT SHIELD ORIG. THICKNESS .032 I.A.W B737-800 SRM 53-30-15. MAT. LOSSED .025 REMAINING THICKNESS .007 FOUND TO BE OUT OF LIMITS I.A.W. B737-800 SRM 53-30-15. TSDR ASAA2024060750852Floor Support · corrodedAFT WET AREA INTERCOSTAL STA 947-967 LBL 24 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .080,REMAINING .030,MATERIAL REMOVED .050 AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. TOO#T8493J DUE 12/26/2024. REMOVED AND REPLASDR ASAA2024060750848Floor Support · corrodedAFT WET AREA INTERCOSTAL STA 947-967 LBL 48 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .080,REMAINING .045, MATERIAL REMOVED .035 AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 TOOL# T8493J DUE 12/26/2024. REMOVED AND REPSDR ASAA2024060750846Floorbeam · corrodedFWD WET AREA STA 294 T-CAP HAS AREA OF CORROSION BL0. GROUNDED - YES. REMOVED CORROSION ORIG.094 REMOVED .023 REMAINING .071 FOUND OUT OF LIMITS PER B737-800 SRM 53-10-51-1A-1,PERFORMED DVI NO FUTHER CORROSION OR DAMAGE FOUND PER B737-800 SRM 53-10-51-2R-14,FLSDR ASAA2024060750843Sill Drain · corrodedFWD WET AREA R1 DOOR MOP SEAL HAS AREAS OF CORROSION STA 294-360. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-10-15-1A-2 FIG 103 DETAIL D. ORIG. MAT .080, REMAINING MAT .069 MAT LOSS OF .011 IS BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED INNER CHORSDR ASAA2024060750841Floorbeam · corrodedAFT WET AREA STA 987 T-CAP HAS CORROSION AT LH GIRT BAR MOUNT AREA LBL50. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-70-51-1A-1. ORIG MAT .150, REMAINING MAT .076. MAT. LOSS OF .074 IS BEYOND ALLOWABLE LIMITS. T-CAP WAS REMOVED AND REPLACED OR CUST SDR ASAA2024060750839Shield · corrodedFWD PIT DOOR SURROUND AFT SHIELD CORRODED. GROUNDED - YES. REMOVED CORR. FROM FWD PIT DOOR SURROUND AFT SHIELD ORIG. THICKNESS .032 I.A.W B737-800 SRM 53-30-15. MAT. LOSSED .025 REMAINING THICKNESS .007 FOUND TO BE OUT OF LIMITS I.A.W. B737-800 SRM 53-30-15. TSDR ASAA2024060750838Floorbeam · corrodedAFT WET AREA STA 987 T-CAP HAS CORROSION FROM RBL 0 TO RBL 50. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-70-51-1A-1. ORIG. MAT .150, REMAINING MAT AT LOWEST POINT .037. MAT LOSS OF .113 IS BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED UPPER CHORD ISDR ASAA2024060750837Floorbeam · corrodedAFT WET AREA FLOOR SUPPORT STA 952 RBL 50 HAS AREA OF CORROSION. GROUNDED - YES. REMOVED CORRODED FLOOR SUPPOR AND INSTALLED NEW FLOOR SUPPORT PER B737-800 SRM 51-40-02 REF: IPC 53-42-51-25E AND DWG# 147A5676 REV:M.SDR ASAA2024060750737Floor Panel · delaminatedFWD WET AREA FLOOR PANEL 141A5810-728 HAS DELAM/CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED FWD WET AREA FLOOR PANEL 141A5810-728 IAW ASA B737-NG SRM 53-00-50-2R-0.SDR ASAA2024060750736Floor Panel · delaminatedFWD WET AREA FLOOR PANEL 141A5810-155 HAS DELAM/CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-155 DELAM AND CORRODED INSERTS WITH A FIBERGLASS DOUBLER REPAIR AND REPLACING ALL DAMAGED INSERTS I.A.W B737-800 SRM 53-00-50-2R-1, 53-00-50-2R-SDR ASAA2024060750735Floorboard · delaminatedFWD WET AREA FLOOR PANEL 141A5810-454 HAS DELAM/CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-454 DELAM AND CORRODED INSERTS WITH FIBERGLASS DOUBLER REPAIR AND REPLACING ALL DAMAGED INSERTS I.A.W B737-800 SRM 53-00-50.SDR ASAA2024060750734Floorboard · delaminatedFWD WET AREA FLOOR PANEL 141A5810-763 HAS DELAM/BROKEN CORNER. GROUNDED - YES. REPAIRED FLOOR PANEL 141A5810-763 IAW B737-800 SRM 53-00-50-2R-06,53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024060750733Floorboard · delaminatedOVER WING BOX FLOOR PANEL 144A5810-127 HAS DELAMINATED SKIN. GROUNDED - YES. REPAIRED OVER WING BOX FLOOR PANEL 144A5810-127 IAW B737-800 SRM 53-00-50-2R-0 AND 53-00-50-2R-1.SDR ASAA2024060750732Floorboard · delaminatedOVER WING BOX FLOOR PANEL 144A5810-126 HAS DELAMINATED SKIN. GROUNDED - YES. REPAIRED OVER WING FLOOR PANEL 144A5810-126 IAW B737-800 SRM 53-00-50-2R-0 AND 53-00-50-2R-1.SDR ASAA2024060750731Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 147A5810-28 HAS CORRODED/MISSING INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED 62EA INSERTS ON AFT WET FLOOR PANEL 147A5810-28 IAW ASA B737-800 SRM 53-00-50-2R-0.SDR ASAA2024060750730Floor Panel · delaminatedAFT WET FLOOR PANEL 147A5810-27 HAS CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED 19EA INSERTS ON AFT WET AREA FLOOR PANEL 147A5810-27 IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2024060750729Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 147A5810-137 HAS CORRODED/MISSING INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED 55EA INSERTS ON AFT WET AREA FLOOR PANEL 147A5810-137 IAW ASA B737-800 SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024060750728Floor Panel · delaminatedFWD WET AREA FLOOR PANEL 141A5810-236 HAS DELAM/CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED IAW B737NG SRM 53-00-50-2R-0 FWD WET AREA FLOOR PANEL 141A5810-236.SDR ASAA2024060750727Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 147A5810-136 HAS CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED 13EA INSERTS ON AFT WET AREA FLOOR PANEL 147A5810-136 IAW ASA B737-800 SRM 53-00-50-2R-0.SDR ASAA2024060750726Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 147A5810-267 HAS CRACKED SKIN BETWEEN SEATTRACK CUTOUT AND DRAIN LINE CUTOUT. GROUNDED - YES. EVALUATED AND REPAIRED 27EA INSERTS AND CRACKED IAW ASA B737-800SRM 53-00-50-0I-01, SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024060650840Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL CORRODED @STA 727F+11 - 727I+10. GROUNDED - YES. REMOVED & EVALUATED DAMAGE FROM AFT PIT L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-1A-2. ORIG THICKNESS : .040 IAW B737-800 SRM 53-60-53-0I-2. REMOVED : .008 REMAINING : .032 ANDSDR ASAA2024060650738Shield · corrodedAFT PIT FWD SHIELD CORRODED. GROUNDED - YES. REMOVED CORROSION & EVALUATED AFT PIT FWD SHIELD ORIG THICKNESS .050 IAW B737-800 SRM 53-60-15-0I-1.REMOVED .007 REMAINING .043 AND IS FOUND TO BE OUT LIMITS IAW B737-800 SRM 53-60-15-1A-1.TOOL# T8224W DUE DATE:27/MSDR ASAA2024040348831Light · malfunctionedFLOOR EMERGENCY STRIP LOOSE BY FWD GALLEY. GROUNDED - YES. (RESOLVED ON W/O: 1996250 TASKCARD: N/R-00001 ) REMOVED & REPLACED THE FIRST SECTION OF STRIP - PHOTOLUMINESCENT AT ROW 1AB REF AMM 33-51-15, GOOD FOR SERVICES. THIS CLEARS MEL 33-19B, PLACARDS REMOVEDSDR ASAA2024031048565Housing · inoperativeFA ADVICES: EXIT PLACARD SIGN R2 DOOR CAME OFF. GROUNDED - YES. (RESOLVED ON W/O: 1992750 TASKCARD: N/R-00002 ) REMOVED AND REPLACED LOWER AFT R2 DOOR EMERGENCY EXIT LIGHT AND SIGN ASSEMBLY REF AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS PLT DEFERRAL. SEAMC AAROSDR ASAA2023102645905Lens · missingEXIT LENS COVER OVER R1 DOOR FELL OFF. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR EXIT SIGN LIGHT ASSY REF AMM 33-51-01. OPS CHK GOOD.SDR ASAA2023101845745Unknown · unknownVTK ANNUNCIATION FO SIDE, LNAV DISENGAGE NO OTHER INDICATIONS VTK WENT AWAY IN APPROX. 10-15 SEC. GROUNDED - YES. REBOOTED RT FMC - SYS OPS OK.SDR ASAA2023072544229Power Supply · inoperativePOWER SUPPLY M1671 FOR RH MID CABIN EMERGENCY LIGHTS FOUND TO FAIL TO CHARGE BATTERY. FAULT IN POWER SUPPLY FOUND WHILE WORKING TC 78233001. GROUNDED - YES. POWER SUPPLY M1671 REMOVED AND REPLACED PER AMM 33-51-06-960-806. ONE MIG-51A INSTALLED AND REMOVED. OPSDR ASAA2023071944174Sensor · faultedBEFORE T/O A SPLIT WAS NOTED IN THE COMMANDED N1 FOR T/O POWER. L 87.8, R 87.2. L DUCT PRESSURE INDICATED 3 PSI, RIGHT INDICATED 20 PSI. CYCLING PACKS AND BLEEDS CAUSED SAME RESULT. OPENING THE ISOLATION VALVE SHOWED DUCT PRESSURS BOTH AT 16PSI. GROUNDED - YESSDR ASAA2023060243431Unknown · unknownZONE TEMP LIGHT FOR CONT CABIN ON MASTER RECALL. GROUNDED - YES. PERFORMED B737-800 FIM 21-62 TASK 801 PACK TEMP CONTROL BITE PROCEDURE. ON THE RIGHT PZTC FOUND FAULT PACK/ZN CON-L FLT DECK TRIM VALVE. PERFORMED FIM 21-62 TASK 833 CIRCUIT BREAKER RESET PROCEDUSDR ASAA2023052243327Unknown · unknownL-FMC FAIL IN FLT. SWITCHED #2 AP AND THEN L-FMC FIXED ITSELF. GROUNDED - YES. R FMC LOGGED DATE RATE FAULT AGAINST L-FMC. ACCOMPLISHED STRING RESET. BOTH FMC'S OP CK NORMAL. REF B737-800 FIM 34-61 TASKS 801 & 837.SDR ASAA2023051543258Panel · crackedREF ASA T/C # 78472000 #1 ENGINE INLET AND FAN BLADES - DETAILED INSP FOUND 12 O'CLOCK STRUT PROFILE PANEL CRACK ON R/H SIDE, AFT END, AT FWD FASTENER HOLE CRACKED, NEXT TO 1 O'CLOCK AFT ACOUSTICAL PANEL. GROUNDED - YES. REPLACED #1 ENG 12 O'CLOCK STRUT PROFILSDR ASAA2023051543240Panel · delaminatedREF ASA T/C #78472000 #1 ENG. INLET AND FAN BLADES-DETAILED INSPT. FOUND #5 STRUT PANEL AT 5 O'CLOCK POS. HAS 1 EACH FASTENER INSERT DELAMINATED FROM PANEL, AFT I/B FASTENER. GROUNDED - YES. REMOVED AND REPLACED #5 STRUT PANEL. REF B737-800 AMM 72-23-07.SDR ASAA2023042343001Window · faultyL1 WINDOW OVERHEAT ILLUMINATED AFTER ENGINE START/PUSHBACK. GROUNDED - YES. REMOVED AND REPLACED L1 WINDOW IAW B737-800 AMM 56-11-11-401. PERFORMED OPERATIONAL CHECK. CABIN PRESSURE LEAK TEST IAW AMM 05-51-91-790-801. NO LEAK FOUND, CHECK OKAY. WINDOW HEAT SYSSDR ASAA2023040842801Unknown · unknown#1 HF RADIO "FAIL". GROUNDED - YES. REF B737-800 FIM 23-11 TASK 801, NO FAULTS FOUND ON HF TRANSCEIVER BIITE TEST. REF B737-800 FIM 23-11 TASK 806, INITIAL EVALUATION TESTS NORMALLY, NO FAULTS NOTED. TRANSMIT AND RECEIVE COMMUNICATION WITH RADIO TOWER. NO HISTSDR ASAA2023032942630Unknown · unknownSAT PHONE 1 AND 2 ABLE TO RECEIVE, WILL NOT TRANSMIT. GROUNDED - YES. CYCLED SAT COM C/B AT P18-2, D14. SATCOM GROUND VERIFICATION FOR 1 AND 2 OPS NML. REF B737-800 FIM 23-15 TASK 801.SDR ASAA2023032842652Indicator · faulty#2 FUEL INDICATOR @ FUELING PANEL SHOWS ARINC MESSAGE. GROUNDED - YES. REMOVED AND REPLACED #2 FUEL INDICATOR IAW REF B737-800 AMM 28-41-61.SDR ASAA2023032742601Unknown · unknownREFUEL PANEL #2 TANK GAUGE SHOWS ARINC MESSAGE. GROUNDED - YES. PERFORMED B737-800 FIM 28-41, NO FAULTS FOUND GROUND TEST PASSED. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2023031942427Servo Motor · faultedAUTO-THROTTLES WILL NOT REMAIN ENGAGED. GROUNDED - YES. CONFIRMED FAULT, A/T FAULT HISTORY SHOWS NUMEROUS ASM-2 FAULT MSG #22-31781 ASM 2 LIMIT FAIL. REMOVED & REPLACED ASM-2 REF B737-800 AMM 22-31-91, OPS CK NML. ACCOMPLISHED DFCS LAND VERIFY TEST REF AMM 22-
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