N407AS
Service difficulty reports · 273
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 = 'N407AS' 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 = 'N407AS' 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 ASAA2026022364512Lamp · inoperativeDURING PDC DISCOVERED LOWER EXIT SIGN LAMP AT ROW 17DEF BROKEN. GROUNDED - YES. REMOVED AND REPLACED LOWER EXIT SIGN LAMP IAW AMM 33-51-01. OPS CHECK GOOD. OK FOR SERVICE.SDR ASAA2025020355715Battery Pack · no testREF T/C 78233001: EMERGENCY LIGHT BATTERY PACK M1675 FAILS CAPACITY CHECK. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY - BATTERY PACK M1675 REF AMM 33-51-06-960-805. FOUR MIG-51A TAGS INSTALLED AND REMOVED. OPS CHECK GOOD.SDR ASAA2024021647911Power Supply · faultyAFTER LANDING EMERGENCY EXIT LIGHTS AROUND R1 AND 1ST CLASS CABIN CAME ON FOR APPROX 30 SECS TO 1 MINUTE. GROUNDED - YES. VERIFIED DISCREP. AS I WAS REMOVING M2816 EMERGENCY EXIT LIGHT BATTERY PACK, BUMPED BATTERY PACK AGAINST FRAME WORK, DISCREP. LIGHTS CAME SDR ASAA2024021247842Power Supply · malfunctionedREF PREVIOUS REPORTS ON VARIOUS EMERGENCY LIGHTS FLICKERED ON T/O AND CLIMB PRI#1. GROUNDED - YES. (RESOLVED ON W/O: 1989627 TASKCARD: N/R-00001 ) ACCOMPLISHED REPLACEMENT OF M1676 AND 1672 POWER SUPPLY AND BATTERY. PER TSR715602. SEAMC DAVE . REF AMM 33-51-06SDR ASAA2024021247841Power Supply · malfunctionedAT TAKE OFF AND FOR 1 MINUTE AFTER T/O THEEMERGENCY LIGHTS AT THE R1 DOOR AND A/C RIGHT SIDE FIRST CLASS CABIN CAME ON. NO ABNORMAL FLIGHT DECK INDICATIONS. GROUNDED - YES. REF TSR715602 FOR REPLACEMENT OF PWR SUPPLY AND BATTERY.SDR ASAA2024021247840Light · malfunctionedEMERGENCY EXIT LIGHTS LOCATED AT R2 DOOR AND INS FIRST CLASS ABOVE, RIGHT SIDE LIGHT , WHERE THE FORWARD LIFE RAFT IS LOCATED, ACTIVATED INTERMITTENTLY DURING TAKE OFF, AND CLIMB. GROUNDED - YES. PERFORMED EMERGENCY LIGHTS OPS CK PER AMM 33-51-00 OPS CK OK. NOSDR ASAA2024013147632Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH M1695 INOP. GROUNDED - YES. REMOVED, REPLACED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS POWER SUPPLY M1695 PER B737-900ER AMM 33-51-06-960-806, LIGHTS OPERATION GOOD.SDR ASAA2024013147631Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH M1694 INOP. GROUNDED - YES. REMOVED, REPLACED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS POWER SUPPLY M1694 PER B737-900ER AMM 33-51-06-960-806, LIGHTS OPERATION GOOD.SDR ASAA2024012347480Intercostal · crackedMAIN CABIN INTERCOSTAL P/N 141A5410-12 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-900ER SRM 51-40-02 AND BOEING DWG 1415400 REV.-.SDR ASAA2024011147479Floor Support · corrodedFWD PIT FLOOR STA 500L RBL 13.84 IS CORRODED. GROUNDED - YES. EVAL'D CORROSION ON FWD PIT FLOOR SUPPORT STA 500L RBL 13.84. HAS 100% MAT LOSS AND IS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2.4.B.(2). REMOVED & REPLACED WITH NEW FWD PIT FLOOR SSDR ASAA2024010547558Floorbeam · corrodedFLOOR BEAM STA. 328 RBL HAS CORROSION. FS 328, BL RBL 20, WL 208. GROUNDED - YES. BLENDED CORROSION. ORIG THICKNESS 0.125 IAW B737-900ER SRM 53-10-51-0I-2 AND BAC 1518-1210. REMOVED 0.085, REMAINING THICK 0.040. OUT OF LIMITS IAW B737-900ER SRM 53-10-51-1A-1. SDR ASAA2024010547478Floor Support · crackedINTERCOSTAL BETWEEN FLOOR BEAM STA 312 AND 328 LBL 45 HAS CRACK AT NUT PLATE. GROUNDED - YES. REMOVED INTERCOSTAL IAW B737-900ER SRM 51-4-02. LOCATED AND DRILLED NEW PART IAW B737-900ER SRM 51-40-02 AND IAW BAC DWG 141A5400 REV:-. INSTALLED NEW PART IAW B737-9SDR ASAA2024010547477Floor Support · crackedINTERCOSTAL BETWEEN FLOOR BEAM STA 344 AND 360 BL 0 HAS CRACK. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT STA 344-360 IAW B737-900ER SRM 51-40-02 AND IAW BAC DWG 141A5400 REV:-SDR ASAA2023123047372Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-443 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATION ON MAIN CABIN FLOOR PANEL 147A5810-443 IAW ASA B737-900ER SRM 53-00-50-2R-0 REPAIR 7, AND FIG 210.SDR ASAA2024011747354Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-155 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-155 IAW B737-900 SRM 53-00-50-1A-1 AND SRM 53-00-50-2R-0.SDR ASAA2024011747353Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-444. GROUNDED - YES. REPAIRED PANEL 147A5810-444 WITH CATEGORY A PERMANENT REPAIR IAW B737-900 SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.SDR ASAA2023122847227Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-421 DELAMINATED. GROUNDED - YES. COMPLETED WET LAY UP REPAIR ON FLOOR PANEL P/N 147A5810-421 IAW B737-900ER SRM 53-00-50-2R.SDR ASAA2023122747373Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2024011747352Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-109 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATED FACE SHEET ON MAIN CABIN FLOOR PANEL 147A5810-109 IAW ASA B737-900ER SRM 53-00-50-2R-0, REPAIR 7, AND FIG 210.SDR ASAA2024011747351Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-439 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 147A5810-439 IAW B737-900 SRM 53-00-51-1A-1 AND SRM 53-00-50-2R-0.SDR ASAA202011747350Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2023122747040Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-446 DELAMINATED. GROUNDED - YES. EVALUATED AND REPAIRED FLOOR PANEL 147A5810-446 DELAM AND 1 INSERT IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.SDR ASAA2023122747039Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-445 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATION ON FLOOR PANEL PN 147A5810-445 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2023122747038Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-440 DELAMINATED. GROUNDED - YES. EVALUATED FLOOR PANEL P/N 147A5810-440 AND FOUND MULTIPLE MISSING/PEELING UPPER SURFACE AND 4EA DAMAGED INSERTS REQUIRING REPAIR IAW ASA B737-900ER SRM 53-00-50-1A-1. REPAIRED IAW ASA B737-900ER SRM 53-SDR ASAA2023122747037Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-477 DELAMINATED. GROUNDED - YES. COMPLETED WET BY UP AND REMOVED AND REPLACED INSERTS 6EA ON FLOOR PANEL P/N 147A5810-477 IAW B737-900ER SRM 53-00-50-2R-0.SDR ASAA2023122347476Baffle · corrodedAFT PIT R/H BAFFLE STA 747 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM BAFFLE PER B737-900ER SRM 53-00-53-1A-2A. ORIG THICKNESS IS .032 PER B737-900ER SRM 53-30-15-0I-1 TABLE 2 REMOVED .009 REMAINING THICKNESS IS .023 AND FOUND TO BE OUT OF LISDR ASAA2023122347374Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727I+9 TO 727L+13 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727I+9 TO 727L+13 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG. THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS &SDR ASAA2024011747357Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727 TO 727E+12 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727-727E+12 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2 TABLE 2 100% MAT LOSS AND FOUND TO BESDR ASAA2024011747356Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727 TO 727D+15 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727 TO 727D=15 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIGINAL THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS & FOSDR ASAA2024011747355Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727D+15 TO 727I+9 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727D+15 TO 727I+9 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS & SDR ASAA2024011747340Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727E+12 TO727I+9 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727E TO 727I IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS " .040 IAW B737-900ER SRM 53-60-53-OI-7 TBALE 2 100% MAT LOSS AND FOUND SDR ASAA2024011747339Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727L+13 TO 809 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727L+13 TO 809 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIGINAL THICKNESS 0.04 IAW B737-900ER SRM 53-00-53-OI-2 100% MAT LOSS & FOUSDR ASAA2024011747338Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727I+9 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727+9-767 IAW B737-900ER SRM 2 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2 3 TABLE 2 100% MAT LOSS & FOUND TO BE SDR ASAA2024011747337Angle · corrodedAFT PIT DOOR SURROUND, FWD SHELD ATTACH ANGLE HAS CORROSION. GROUNDED - YES. EVAULATED THE SHEILD ATTACH ANGLE CORROSION NO ALLOWABLE DAMG LIMITS GIVEN IN B737-900ER SRM REMOVED AND REPLACED NEW PART IAW B737-900ER SRM 51-40-02 AND BOEING DWG #146A8123.SDR ASAA2023122347336Shield · corrodedAFT PIT DOOR SURROUND, FWD SHEILD HAS CORROSION. GROUNDED - YES. EVAULATED REMOVED CORROSION FROM SHEILD PER B737-900ER SRM 53-00-53-1H-2A ORIG THICKNESS IS .050 PER B737-900ER SRM 53-30-15-OI TABLE 4 REMOVED .007 REMAINING IS .043 AND FOUND TO BE OUT OF LIMITSDR ASAA2023122347335Transition Panel · corrodedFWD PIT L/H TRANSITION PANEL STA 500K+6 TO 500L HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500K+6 TO 500L IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040 IAW B737-900ER SRM 53-30-53-01-2 TABLE 2. RSDR ASAA2023122347334Transition Panel · corrodedFWD PIT R/H PANEL STA 500E+2 TO 500H+10 HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+2 TO 500HD+10 IAW B737-900ER SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-0I-2 TABLE 2.SDR ASAA2023122347333Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500H+10 TO 500L HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500H+10 TO 500L IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-01-2 TABLE 2SDR ASAA2023122347283Transition Panel · corrodedFWD PIT R/H PANEL STA 500A+17 TO 500D+7 HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500A+17 TO 500D+7 IAW B737-900ER SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-0I-2 TABLE 2. SDR ASAA2023130247582Power Supply · inoperativeEMERGENCY LIGHTS AT 25DEF AND 29DEF ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M2627 AND PERFORMED GOOD INSTALLATION TEST PER B737-900ER AMM 33-51-06-960-806, NO DEFECTS NOTED EMERGENCY LIGHTS AT 25DEF AND 29DEF OPERATION NORMAL.SDR ASAA2023121746798Unknown · unknownFOUND 2 EMERGENCY AISLE LIGHT INOP WHILE ACCOMPLISHING T/C 78233008 BOTH LIGHT LOCATED ON THE RIGHT ROWS 25 AND 29. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102845887Unknown · unknownAFT CABIN ZONE TEMP LIGHT ILLUMINATED IN FLIGHT, LIGHT EXTINGUISHED WHEN MASTER CAUTION IS RESET. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023102545837Unknown · unknownDURING DESCENT L FMC FAIL, QRH COMPLIED WITH, FMC REESTABLISHED. AFTER LANDING MULTIPLE FMC DISAGREE MESSAGE POSTED. GROUNDED - YES. PRM MSG PREVIOUS FLT FOR L-FMC, NO HISTORY PAST 30 DAYS. FMC OPERATIONAL TEST PASS REF B737-900 AMM 34-61 TASK 801.SDR ASAA2023100945526Control Unit · faultyELEC AMBER LIGHT ON OVERHEAD PANEL ILLUMINATED. GROUNDED - YES. PERFORMED TROUBLESHOOTING PER REF FIM 24-31 TASK 801 AND FIM 34-31 TASK 802 AND FOUND SPCU TO BE INOP. REMOVED AND REPLACED SPCU PER AMM 24-34-11-000-801 AND AMM 24-34-11-400-801. OPS CHECK GOODSDR ASAA2023100945525Unknown · unknownZONE TEMP LIGHT ILLUMINATED ON RECALL CONT CAB EXTINGUISHES ON RESET. GROUNDED - YES. (RESOLVED ON W/O: 1972560 TASKCARD: N/R-00004 ) PERFORMED FIM TASK 21-62 TASK 801. BITE PROCDURE. ZONE TEMP LIGHT EXTINGUIED. NO LIGHTS ON MASTER RECALL. THIS CLEARS MEL 21-2SDR ASAA2023100545459Sensor · faultyAPU FAULT CODE SHOWING - "49-94304 OIL LEVEL SENSOR SHOWS OPEN CIRCUIT FAILURE". GROUNDED - YES. REMOVED AND REPLACED APU OIL LEVEL SENSOR REF B737-900 AMM 49-94-11. LEAK CHECK AND OPC GOOD.SDR ASAA2023091445193Control Valve · faultyTECH SERVICES REQUEST FOLLOW-UP TO LEFT PACK LIGHT WITH PACK SELECTED OFF----(#PRI1)----ETOPS SIGNIFICANT SYSTEM----. GROUNDED - YES. (RESOLVED ON W/O: 1967218 TASKCARD: N/R-00002 ) OPENED AND TAGGED 1 CB. LT FLOW CONTROL AND SHUTOOF VALVE REMOVED REF MM TASK SDR ASAA2023091345132Unknown · unknownRIGHT PACK ILLUMINATED ON RECALL. RAN QRH AND PACK LIGHT EXTUINGUISHES ON MC RESET. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023091345106Unknown · unknownLEFT PACK LIGHT ILLUMINATED AFTER BLOCKOUT ( ON THE GROUND) AND PRIOR TO THE PACK SWITCH MOVED TO ON. RUN PACK ( TURNED ON ) AND ACCOMPLISHED QRH CHECKLIST, PACK LIGHT STILL ILUMINATED. RETURNED TO GATE FOR MAINTENANCE ACTION. GROUNDED - YES. PERFORMED PZTC BISDR ASAA2023080644430Unknown · unknownNO FUEL FLOW TO # 1 ENGINE DURING START ATTEMPT. GROUNDED - YES. #1 ENG, PERFORMED FUEL FLOW WAS NOT DETECTED DURING START ATTEMPT REF FIM 73-31 TASK 803. PERFORMED EEC BITE REF FIM 73-00 TASK 801. FOUND MESSAGE 73-31551 FF NOT DETECT AT START. IGN R IS FAILED
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