N615AS
Service difficulty reports · 241
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 = 'N615AS' 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 = 'N615AS' 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 ASAA2015103113933Seat Track · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE, TRACK AT BS 792 AND RBL 13.84 HAS CORROSION. MARKED. ACFT GROUNDED. R & R WITH NEW AFT CARGO COMPARTMENT FLOOR STRUCTURE TRACK IAW SRM 53-00-53-2R-3 & BAC DWG 146A7501, REV:C REMOVED DOT U847.SDR ASAA2015103113856Floor Support · corrodedAFT CARGO COMPARTMENT, FLOOR SUPPORT/TRANSITION PANEL BETWEEN BS787 TO BS793 AND S26R & S25R HAS CORROSION ON UPPER AND LOWER SURFACE, MARKED. ACFT GROUNDED. REMOVED CORROSION FROM TOP AND BOTTOM FLOOR SUPPORT STRAPS AT BS 787-793, 526R-25R IAW SRM 53-00-83 -SDR ASAA2015103113854Bracket · corrodedFWD PIT AFT BILGE ANTENNA BRACKET IS CORR AT STA 500 TO STA 500A. ACFT GROUNDED. REMOVED NR 1 ANTENNA BLANKING PLATE IAW AMM 23-19-07. REMOVED ANTENNA BRACKETS IAW SRM 51-40-02, MATERIAL ID 7075-T6, .040, PO 804411.4 AND FABBED IAW DWG 143A3233, REV F LOCATESDR ASAA2015103113853Transition Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE LT TRANSITION PANEL FROM BS 736 TO BS 787 HAS CORROSION, MARKED. ACFT GROUNDED. CUTOUT DAMAGE PORTION OF AFT CARGO LT TRANSTION PANEL, FABRICATED, LOCATED & DRILLED NEW REPAIR PARTS USING BAC 1496-377 EXTRUSION PO 843790SDR ASAA2015103113852Bracket · corrodedFWD PIT AFT BILGE ANTENNA BRACKET IS CORRODED AT BS 500A TO 500B. ACFT GROUNDED. REMOVED NR 2 ANTENNA BLANKING PLATE IAW AMM 23-19-07. REMOVED ANTENNA BRACKETS IAW SRM 51-40-02, MATERIAL ID 7075-T6 .040, PO 804411.4 AND FABBED IAW BAC DWG 143A3233, REV F. LOSDR ASAA2015103113808Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE, TEE STRAP AT BS772 HAS CORROSION IN SEVERAL AREAS, MARKED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. BEYOND LIMITS IAW SRM 53-00-53, FIG 103. ORIGINAL THICKNESS WAS 0.070 WITH 0.040 REMAINING, 0.030 MATERIAL RSDR ASAA2015103113807Transition Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE RT TRANSITION PANEL FROM BS 767 TO BS 787 HAS CORROSION, MARKED. ACFT GROUNDED. REMOVED CORROSION ON SHIELD, TRANSITION PANEL FROM BS 767 TO BS 787 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .050. REMOVED DOT REMAINING THSDR ASAA2015103113748Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 727 AND BS 727A AND LBL 12.5 HAS CORROSION. MARKED. ACFT GROUNDED. BLEND OUT CORROSION AREA, ORIGINAL MATERIAL THICKNESS .063 IAW DWG 1509-100146, MAT REMOVED .004, MAT REMAINING .059, FOUND TO BE WITHIN LIMITS IASDR ASAA2015103113747Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 727 AND BS 727A AND RBL 13.84 HAS CORROSION. MARKED. ACFT GROUNDED. BLEND OUT AREA ORIGINAL MATERIAL THICKNESS, .063 IAW DWG 1509-100146, MAT REMOVED .001 MAT REMAINING .062 FOUND TO BE WITHIN LIMITS IAW SRM 53-00SDR ASAA2015103113700Transition Panel · corrodedFWD CARGO BAY LT SIDE TRANSITION PANEL CORRODED FROM LT BS 500B TO FWD PIT AFT BULKHEAD. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, WITHIN LIMITS IAW SRM 53-00-53, FIG 103. ORIGINAL THICKNESS 0.040 WITH 0.038, REMAINING 0.002 MATERIAL REMOVED MEASURESDR ASAA2015103113699Web · corrodedFWD CARGO THRESHOLD IS CORRODED. ACFT GROUNDED. ORIGINAL MATERIAL .045", REMOVED .001", REMAINING MATERIAL .044; FOUND TO BE WITHIN LIMITS IAW SRM 53-30-15-1A-1, PAGE 7, FIG 103. APPLIED ALODINE AND PRIMER IAW SRM 51-20-01-OG-0.SDR ASAA2015103014037Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 344, REPAIR HAS CORROSION, LBL 5. ACFT GROUNDED. REPAIRED FLOORBEAM REF: REO-G19363, REV B AND EA 700-53EA-16186, REV NEW, DOT REMOVED.SDR ASAA2015103013943Crease Beam · corrodedMAIN CABIN, FLOOR SUPPORT CORRODED BS 637-BS 641, RBL 62-RBL 65. ACFT GROUNDED. REPAIRED IAW EA 700-53, EA-16116 AND REO-G19342, REV A DOT REMOVED.SDR ASAA2015103013843Floorbeam · corrodedAFT FUSELAGE WET AREA STA 947.5 RBL 49 HAS CORROSION. ACFT GROUNDED. AFT FUSELAGE WET AREA BS 947.5 TOP OF THE FLOORBEAM CHORD CORRODED BEYOND LIMITS IAW SRM 53-70-51. REMOVED DAMAGE AND REPAIRED CHORD IAW SRM 53-70-51-2R-5, SRM 51-10-02, SRM 51-40-02, SRM 51SDR ASAA2015103013806Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CORRODED AT R-1 DOOR AREA. ACFT GROUNDED. R & R R-1 DOOR CHORD, PN 654A0004-134 IAW AND REF DWG'S 141A8310, 143A5900, 140A9810. DOT REMOVED.SDR ASAA2015103013744Fitting · corrodedMAIN CABIN GIRT BAR ATTACH FLOOR FITTING CORRODED BS 308-BS 310, LBL 58-LBL 60. ACFT GROUNDED. R & R 141A5220-2 TIE DOWN FITTING IAW SRM 51-40-02. DOT REMOVED.SDR ASAA2015103013743Girt Bar · corrodedMAIN CABIN GIRT BAR ATTACH FLOOR FITTING CORRODED BS 344-BS 346, LBL 58-LBL 60. GROUNDED. R & R 141A5220-4, TIE DOWN FITTING IAW SRM 51-40-02. DOT REMOVED.SDR ASAA2015103013705Floorbeam · corrodedMAIN CABIN RT FLOORBEAM BS 328 CORROSION ON UPPER SURFACE. ACFT GROUNDED. REPAIRED FLOORBEAM BS 328, RBL40-RBL65 IAW SRM 53-10-51-2R-7.SDR ASAA2015103013691Support · corrodedAFT FUSELAGE WET AREA, BS 1016, LBL 32 HAS CORROSION AND BENT. ACFT GROUNDED. REMOVED CORRODED AND BENT WALL SUPPORT, RECEIVED NEW WALL SUPPORT, PN 147A5710U16, LOCATED, DRILLED AND COUNTERSANK FASTENER HOLES ON NEW WALL BRACKET IAW SRM 51-40-08, INSTALLED NESDR ASAA2015103013690Floor Support · corrodedAFT FUSELAGE WET AREA, BS 987 +6, LBL 40 HAS CORROSION. ACFT GROUNDED. ORIGINAL MATERIAL THICKNESS .050", DAMAGED MATERIAL THICKNESS .007, REMAINING MATERIAL THICKNESS .043", FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51USING UT GAUGE TOOL T8225Z, REMOVED SUPPOSDR ASAA2015103013685Floor Support · corrodedAFT FUSELAGE WET AREA, BS 1006, RBL 31 HAS CORROSION. ACFT GROUNDED. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .050 MATERAIL LOSS .008, MATERIAL REMAINING .042" FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51, LOCATEDSDR ASAA2015103013652Floor Support · crackedMAIN CABIN RT FLOOR SUPPORT BETWEEN BS 312 - 328 IS CRACKED RBL 33. ACFT GROUNDED. REMOVED THE CRACKED INTERCOSTAL IAW SRM 51-40-02. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2015103013650Floor Support · crackedMAIN CABIN BELOW FLOOR SUPPORT CRACKED BS 320, LBL 46. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5910, REV U.SDR ASAA2015103013649Floor Support · crackedMAIN CABIN BELOW FLOOR SUPPORT CRACKED BS 334, LBL 46. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5410, REV U.SDR ASAA2015102913857Stringer · dentedMAIN CABIN BS 360 S9-R, STRINGER SPLICE IS BENT. ACFT GROUNDED. R & R STRINGER CHANNEL AND STRINGER CLIP REF: SRM 51-40-02 AND BAC DWG 140A9111, REV B. REMOVED DOT.SDR ASAA2015102913805Angle · chafedVERTICAL STABILIZER PANEL 323AL, LOWER SUPPORT ANGLE HAS CHAFING MARKS BETWEEN BS 1005 AND BS 1016 ,STR 2L AND 3L. ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02 & EA NG-55-EA-03820, REV NEW FOUND TO BE OUT LIMITS AT BS 1005 ORIGINAL .063 REMOVED .011 REMAININSDR ASAA2015102913651Support Angle · bentL2 DOOR SCUFF PLATE SUPPORT ANGLE BENT. ACFT GROUNDED. REMOVED BENT SUPPORT ANGLE IAW SRM 51-40-02. RECEIVED MATERIAL ID SUPPORT ZEE BAC 1517-2797-7075-T73511 EXTRUSION TO FABRICATE NEW SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE IAW DWG 147A8530 AND GPM 0SDR ASAA2015102713929Support · wornRIGHT WING T/E OTBD OF PYLON, SUPPORT ROD ATTACH BRACKET HOLES WORN. ACFT GROUNDED. R & R BRACKET IAW SRM 51-40-02 AND BAC DWG 115A6400, LEAK CHECK ACCOMPLISHED ON TASK CARD 74528002, DOT REMOVED.SDR ASAA2015102713812Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN JUST INBD OF STABILIZER BS 101.90. CRACK IS APPROXIMATELY .5" LONG AND APPROXIMATELY 10 AFT OF DRAIN HOLE AND IS MARKED. ACFT GROUNDED. REPAIRED LOWER SKIN OF RT HORIZONTAL STABILIZER AT BS 101.90 IAW SRM 55-SDR ASAA2015102713723Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN JUST INBD OF STABILIZER STATION 92.70. CRACK IS APPROXIMATELY .5" LONG AND APPROXIMATELY 10" FWD OF DRAIN HOLE AND IS MARKED. ACFT GROUNDED. REPAIRED LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT BS 92.70 IAW SSDR ASAA2015102613844Shim · migratedWING AFT SPAR LOWER ATTACH FITTING BL71.24 LT BS 663.75 HAS TORN SEALANT AND MIGRATING SHIMS. ACFT GROUNDED. REPAIRED IAW REO-G19315 A REQUIRES INSPECTION: "INSPECT THE JOINT FOR BOLT/NUT ROTATION OR ADDITIONAL SHIM MIGRATION WITH IN 200 CYCLES OR 12 MONTHSSDR ASAA2015102513722Floor Panel · corrodedAFT PIT FLOOR PANEL 140BF HAS CORROSION AND GOUGES ALL ARROUND. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 140BF IAW DWG 453A2610, REV E.SDR ASAA2015102513721Floor Panel · corrodedAFT PIT FLOOR PANEL 140CF HAS CORROSIN AND GOUGES ALL ARROUND. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 140 CF IAW DWG 453A2610, FLOOR PANEL 140CF HAS MULTIPLE GOUGES LINGER THAN 3", PN 453A2610, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1.SDR ASAA2015102513680Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 140DF HAS CORROSION AND GOUGES ALL ARROUND. ACFT GROUNDED. EVALUATED DAMAGE ON FLOOR PANEL 140DF, FOUND OUT OF LIMIT ACCORDING TO SRM 53-00-53, MATERIAL ID TO FABRICATE NEW PANEL 2024-T3 .071" IAW B-DWG 453A2610, PO:8406181.1. FABRSDR ASAA2015102513655Floor Panel · corrodedAFT PIT FLOOR PANEL 140AF HAS CORROSIN AND GOUGES ALL ARROUND. ACFT GROUNDED. EVALUATE DAMAGE ON AFT PIT FLOOR PANEL 140AF FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 REV 26, FABRICATED NEW FLOOR PANEL IAW DWG 453A2610, THE NEW PANEL WAS ALODINED AND PRIMED IAWSDR ASAA2015102413803Strip · corrodedAFT CARGO RT SIDEWALL CAPSTRIP NR 2 CORRODED. ACFT GROUNDED. RECEIVED NEW CAP STRIP PN 453A2611-11. INSTALLATION ACCOMPLISHED.SDR ASAA2015102413796Floor Panel · corrodedPARTS RACK, FWD PIT FLOOR PANEL 120BF CORRODED AND GOUGED IN SEVERAL AREAS. ACFT GROUNDED. FLOOR PANEL NR 120BF, PN 453A1610-44 HAS MULTIPLE GOUGES LONGER THAN 3". FOUNT TO BE OUT OF LIMITS PER ASA B737-700 SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL, PO 8SDR ASAA2015102413654Floor Panel · corrodedPARTS RACK, FWD PIT FLOOR PANEL 120AF CORRODED SEVERAL AREAS. ACFT GROUNDED. BLENDED OUT PANEL 120AF ORIGINAL MATERIAL .071, MATERIAL REMOVED IS .020 MATERIAL REMAINING IS .051 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL IAW DSDR ASAA2015051211714Track · gougedRT ZEE TRACK AT ST 749 TO HAVE A .2500" PUNCTURE. ACFT GROUNDED. REPAIRED RT TRANSITION PANEL IN AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-5 FROM STA 727-STA 767.SDR ASAA2015022410768Module · corrodedWHILE PERFORMING TC 78233008, EMERGENCY LIGHT CK FOUND LIGHT AT 20D DIM AND ALWAYS ON. ACFT GROUNDED. GROUND MODULE GD03806 CORRODED. REPLACED GROUND MODULE IAW SRM 51-40-02. RE-TERMINATED W4142-0455-20, W4146-0072-18, AND W4146-0073-18 AND INSTALLED WIRESSDR ASAA2015022210744Guide Arm · out of adjustFOUND L1 DOOR HARD TO LATCH WHILE INSIDE, END OF TRAVEL. ACFT GROUNDED. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED L-1 DOOR GUIDE ARM REF AMM 52-11-00-820-801 STEP H. ACCOMPLISHED FORWARD ENTRY DOOR SYS TEST & TESTED GOOD REF AMM 52-11-00-700-804.SDR ASAA2014123010112Power Supply · failedBULL NOSE EMERGENCY LIGHT AT ROW 20 FED & 21 FED WILL NOT GO OUT. ACFT GROUNDED. REPLACED BATTERY PACK/CHARGER M1672 AND RELAMPED L1065 AISLE LIGHT BETWEEN ROWS 20 AND 21 FED. OPS CHECK OK, REF AMM 33-51-06/201.SDR ASAA2014110209557Lamp · inoperativeEMERGENCY LIGHT OVERWING EXIT HANDLE, FLOODLIGHTS AT LT AND RT OVERWING EXITS EACH HAVE BOTH LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.SDR ASAA2014040507447Screw · looseCAPTAIN`S SLIDING WINDOW WILL NOT FULLY OPEN. ACFT GROUNDED. INSPECTED WINDOW IAW MM 56-12-11-710-803. TIGHTENED ONE SCREW ON AFT WINDOW SHADE SLIDE RAIL. OPS CHECKED NORMAL. NO REPAIRS, RIGGING OR ADJUSTMENTS WERE REQUIRED.SDR ASAA2013102496316Seat Track · crackedSEAT TRACK BS 727B, RBL 45.50 CRACKED. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G16843, REV B AND EA 700-53EA-11540, REV.SDR ASAA2013102496315Seat Track · crackedSEAT TRACK AT BS 727B, RBL 24.75 CRACKED. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G16843, REV B AND EA 700-53EA-11540, REV.SDR ASAA2013082795892Hmu · malfunctionedCLIMBING THOUGH 17,000 FT, NR 2 ENGINE SURGED CONTINUALLY. RAN SURGE CHECKLIST, THROTTLE ALMOST CLOSE WHEN ENGINE STALLED, ENGINE THEN FAILED. COMPLETED CHECKLIST AND RETURNED DEPARTURE. ACFT GROUNDED. ACCOMPLISHED EA 700-72EA-10951. NR 2 ENGINE HMU REPLSDR ASAA2012111893318Guide Arm · out of alignmentACFT L1 DOOR DID NOT CLOSE AND LOCK PROPERLY CAUSING AN AIR LEAK AND LACK OF PROPER PRESSURIZATION. NO LIGHT CAME ON IN FLIGHT OR GROUND. ACFT GROUNDED. FOUND L1 DOOR OUT OF ALIGNMENT WITH FUSELAGE SKIN. ADJUSTED GUIDE ARM IAW AMM 52-17-00-820-801, STEP 2 ASDR ASAA2012110909303Window Post · crackedCRACK ON LT NR 1 WINDOW OTBD POST. ACFT GROUNDED. REPAIRED IAW SB737-53-1336-NG-1.SDR ASAA2012110293320Window Frame · crackedPOSSIBLE CRACK ON LT NR 1 WINDOW OTBD POST. REPAIRED CRACK ON NR 1 WINDOW POST BY FABRICATING AND INSTALLING EXTERNAL DOUBLER IAW EA 700-53EA-09202.
Back to N615AS