N618AS

Service difficulty reports · 229

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 = 'N618AS' 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 ASAA2016110518760Floor Support · corrodedCOCKPIT FLOOR BS 270 BL 0 ANGLE CORRODED. ACFT GROUNDED. REPAIRED BS 270 THE FLOOR SUPPORT IAW 700-53EA-18037 REV 00, AND REO-G20417 REV A.Nov 5, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016110518597Channel · corrodedAFT CARGO RT TRANSITION PANEL CHANNEL IS CORRODED AT BS 727D. ACFT GROUNDED. REMOVED CORROSION, FOUND BEYOND ALLOWABLE SRM LIMITS, IAW SRM 53-00-53. INSTALLED REPAIR IAW DWG 146A7500 REV C AND SRM 53-00-53. .Nov 5, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016110418716Floor Support · corrodedCOCKPIT FLOOR STA 270 BL0 FLOOR SUPPORT IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED SUPPORT CHANNEL IAW DWG 141A5210 REV- AND SRM 51-40-02.Nov 4, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016110218725Support Fitting · corrodedSUPPORT FITTING CORRODED BS 947-967 LBL 45. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT FITTING IAW DWG 147A5660. FITTING TO BE INST ON CARD G754113 N/R 26613.Nov 2, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016110218724Support Fitting · corrodedSUPPORT FITTING CORRODED BS 947-967 RBL 25 45. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5660. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.Nov 2, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016103118703Floor Support · crackedFLOOR SUPPORT CRACKED BS 986 - 1006 LBL 30. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND SRM 53-70-51 & DWG 147A5700 REV-.Oct 31, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016103118614Web · corrodedRIGHT CREASE BEAM WEB CORRODED BS 947 - 992. ACFT GROUNDED. REMOVED CORRODED WEB IAW SRM 51-10-2, FABRICATED NEW WEB IAW DWG 147A8510-51 REV E AND INSTALLED WEB IAW DWG 147A8501 REV-.Oct 31, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016103018704Web · corrodedCREASE BEAM WEB AT RT BS 992-1006 CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1 FIG 103. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, DWG 147A8510 REV A, SRM 51-20-01.Oct 30, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102918759Frame · corrodedFRAME AT LEFT SIDE WALL CORRODED . BS 559, STRINGERS 16 - 17L. ACFT GROUNDED. ACCOMPLISHED REPAIR IAW REO-G20407 REV A AND EA 700-53EA-18015 REV 00.Oct 29, 2016 · N618AS · Boeing 737790 · Fuselage Main, FrameSDR ASAA2016102918722Seat Track · corrodedSEAT TRACK CORRODED AT SEVERAL SPOTS. BS 540 - BS 706, RBL 45.57. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-40-52-1A-1, ORIGINAL MATERIAL THICKNESS IS 0.146 IN, REMAINING THICKNESS IS 0.080 IN, REMOVED 0.066 IN. REMOVED SEAOct 29, 2016 · N618AS · Boeing 737790 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2016102818758Frame · corrodedMAIN CABIN LT STUB FRAME BS 693.75 HAS CORROSION. ACFT GROUNDED. REPAIRED THE FRAME BETWEEN STRINGERS 16 -17L IAW 700-53EA-18018 REV 00, AND REO-G20401 REV A.Oct 28, 2016 · N618AS · Boeing 737790 · Fuselage Main, FrameSDR ASAA2016102818757Door Frame · corrodedMAIN CABIN L1 DOOR FRAME INBD FLANGE, CORRODED BS 303.9, STRINGERS 9 - 10L. ACFT GROUNDED. REMOVED CORROSION IAW 700-53EA-17989 REV 00, REO-G20402 REV A.Oct 28, 2016 · N618AS · Boeing 737790 · Fuselage Main, StructureSDR ASAA2016102818717Door Sill · corrodedMAIN CABIN AFT WET AREA DOOR SILL UPPER SURFACE HAS CORROSION BETWEEN BS 951 AND BS 992 LBL 47. GROUNDED - YES. REMOVED CORRODED WEB IAW SRM 51-40-02, FABRICATED NEW WEB [-50] IAW DWG 147A8510 REV B. LOCATED, DRILLED AND DEBURRED NEW WEB IAW DWG 147A8501 REV AOct 28, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102818706Support Angle · corrodedSUPPORT ANGLE AT BS 992 RBL 31-45 CORRODED. ACFT GROUNDED. REPLACED THE SUPPORT ANGLE IAW DWG 147A5700 REV- .Oct 28, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718729Floor Support · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 950 BETWEEN LBL 35 AND LBL 49. GROUNDED - YES. REMOVED CORR, LOSS OF 50% OF MAT. FOUND OUT OF LIMITS IAW SRM 53-70-51. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5676. SUPPORT WILL BE INST ON CARD G754113 N/R 26613Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718728Floor Support · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 957,LBL 51. GROUNDED - YES. REMOVED CORR. LOSS OF 50% MAT. FOUND OUT OF LIMITS IAW SRM 53-70-51. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5560. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718727Floorbeam · corrodedMAIN CABIN FLOORBEAM T-CAP HAS CORROSION AT BS 987, BETWEEN RBL 12 AND RBL 45. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-70-51-1A-1, ORIGINAL MATERIAL THICKNESS IS .150 IN. REMAINING IS .136 IN, REMOVED .014 IN REMOVED, EXIOct 27, 2016 · N618AS · Boeing 737790 · Fuselage Main, Floor BeamSDR ASAA2016102718726Support · corrodedMAIN CABIN L2 DOOR CUTOUT LOWER AREA SILL SUPPORT HAS CORROSION BETWEEN BS 947 AND BS 987 LBL 47. GROUNDED - YES. FOUND CORROSION TO BE BEYOND THE SRM LIMITS REPAIRS. FOUND OUT OF LIMITS IAW SRM 53-70-15 AND 57-10-02, REMOVED Z ANGLE SUPPORT AND ADJACENT ANGLEOct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718720Support · corrodedAFT MAIN CABIN R-2 DOOR SILL SUPPORT HAS CORROSION BETWEEN BS 947.05 AND BS 995 , RBL 60. GROUNDED - YES. EVALUATED DAMAGE CORROSION FOUND OUT OF LIMITS, ORIGINAL MATERIAL THICKNESS IS .080, REMOVED .026, REMAINING IS .054 IAW SRM 53-70-15 REMOVED AND REPLACEDOct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718719Floor Support · corrodedMAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 950 AND RBL 29. GROUNDED - YES. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW DWG 147A5650. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718718Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION AT BS 947.05 AND RBL 51. GROUNDED - YES. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. CORROSION REMOVAL BEYOND LIMITS IAW SRM 53-70-51-1A-1, ORIGINAL THICKNESS 0.180 WITH 0.149 REMAINING , 0.031. REMOVED FLOORBEAM UPPEROct 27, 2016 · N618AS · Boeing 737790 · Fuselage Main, Floor BeamSDR ASAA2016102718707Web · corrodedMAIN CABIN FLOOR WEB HAS CORROSION BETWEEN BS 987 AND 993. RBL 31 AND 45. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW DWG 147A5700 REV-.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718649Strap · corrodedMAIN CABIN WEB STRAP ANGLE HAS CORROSION AT BS 1018 , LBL 27. ACFT GROUNDED. CORROSION BEYOND REPAIRABLE LIMITS, REMOVED AND REPLACED MAIN CABIN WEB STRAP ANGLE AT BS 1018 LBL 27 IAW DWG 147A5714 REV A, 147A5700 REV-, AND SRM 51-40-02.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718574Floorbeam · corrodedMAIN CABIN FLOORBEAM TEE HAS CORROSION BS 967 BETWEEN LBL 10 AND RBL 04. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-70-51. REPAIRED IAW SRM 53-00-51-2R-1.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Main, Floor BeamSDR ASAA2016102718525Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED AT BS 318 RBL 30. ACFT GROUNDED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5400.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718524Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED AT BS 333, LBL 46. GROUNDED, YES. REMOVED AND REPLACED FLOOR SUPPORT AT BS 333 LBL 46 IAW SRM 51-40-02 AND DWG 141A3400.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102718523Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED AT BS 319, LBL 46. GROUNDED, YES. REMOVED AND REPLACED FLOOR SUPPORT AT BS 319, LBL 46 IAW SRM 51-40-02 AND DWG 141A5400.Oct 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102618527Transition Panel · corrodedAFT CARGO LEFT TRANSITION PANEL. BS 727 TO 727E+10 HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION PANEL IAW SRM 51-40-02 AND SPLICED IN NEW TRANSITION PANEL IAW SRM 53-00-53Oct 26, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102618526Transition Panel · corrodedAFT CARGO BAY LT TRANSITION PANEL. BS 727E+10 TO 847 HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REMOVED DAMAGE IAW SRM 51-40-02, FABRICATED A NEW TRANSITION PANEL IAW SRM 53-00-53 AND DWG 1Oct 26, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016102518702Doubler · crackedELECTRICAL GROUND POWER 304 RECEPTACLE SURROUND DOUBLER FWD LOWER END CRACKED. ACFT GROUNDED. REPAIRED IAW EA 700-53EA-17997 AND REO-G20385 REV B.Oct 25, 2016 · N618AS · Boeing 737790 · Fuselage Main, Plate/SkinSDR ASAA2016102518609Bulkhead · crackedBS 663 UPPER PRESSURE BULKHEAD CRACKED RBL 42.5. ACFT GROUNDED. REPAIRED THE BULKHEAD IAW SRM 57-10-10-2R-3.Oct 25, 2016 · N618AS · Boeing 737790 · Fuselage Main, BulkheadSDR ASAA2016102418560Floor Panel · damagedFWD CARGO FLOOR PANEL 120AF CORRODED AND GOUGED. ACFT GROUNDED. FOUND BEYOND SRM LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-13.Oct 24, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102418559Floor Panel · gougedFWD CARGO FLOOR PANEL 120CF GOUGED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-31 REV C.Oct 24, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102418558Floor Panel · gougedFWD CARGO FLOOR PANEL 120BF GOUGED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-43 REV B.Oct 24, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102318514Floor Panel · dentedAFT CARGO FLOOR PANEL 140BF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-31, ALODINED IAW SRM 57-20-01, PRIMED IAW SOPM 20-41-02.Oct 23, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102318513Floor Panel · damagedAFT CARGO FLOOR PANEL 140CF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610. ALODINED IAW SRM 51-20-01. AND PRIMED IAW SOPM 20-41-02.Oct 23, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102318512Floor Panel · dentedAFT CARGO FLOOR PANEL 140DF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW 53-00-53, FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-19 REV B. ALODINED IAW SRM 57-20-01, PRIMED IAW SOPM 20-41-02.Oct 23, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016102318511Floor Panel · dentedAFT CARGO FLOOR PANEL 140AF DENTED AND SCRATCHED ALL ARROUND. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-33, ALODINED IAW SRM 57-21-01, PRIMED IAW SOPM 20-41-02.Oct 23, 2016 · N618AS · Boeing 737790 · Fuselage Floor PanelSDR ASAA2016101818398Sign · brokenEMERGENCY EXIT SIGN ADJACENT TO LEFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE AND A BROKEN LENS. ACFT GROUNDED. REPLACED THE LAMPS, AND LENS, TESTED IAW AMM 33-51-01-960-801 - OPS NORMAL.Oct 18, 2016 · N618AS · Boeing 737790 · Emergency LightingSDR ASAA2016100918251Track · out of adjustOVERWING EMERGENCY EXIT AT SEAT 16F MAKES LOUD LEAKING NOISE IN FLIGHT. PRESSURIZATION OPERATES NORMAL ALL PHASES OF FLIGHT. FAULT CODES D223616F AND D224216F. ACFT GROUNDED. PRESSURIZED ACFT TO 2 PSI, FOUND RT OVERWING EXIT EXTERIOR HANDLE TO BE LEAKING. AOct 9, 2016 · N618AS · Boeing 737790 · Emergency ExitsSDR ASAA2016092718611Web · corrodedMAIN CABIN FLOOR WEB HAS CORROSION AT BS 1018, LBL 33. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, CORRODDED 20% OUT OF LIMITS IAW SRM 53-70-51, REMOVED AND REPLACED NEW WEB IAW DWG 147A5700, REV B.Sep 27, 2016 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2016052516888Stringer · damagedWHILE INSPECTING FWD ATG ANTENNA SUPPORT STRUCTURE, FOUND 2EA DOUBLE FLUSH RIVETS INSTALLED IN STR 27R BS 500+5 HAT SECTION ADJACENT TO PLUG RIVETS FROM PREVIOUS ANTENNA STRUCTURE REF GOGO DWG P19110-23906, FLAGNOTE 12. ACFT GROUNDED. REMOVED DAMAGE IN STR 27May 25, 2016 · N618AS · Boeing 737790 · Fuselage Main, Longeron/StringerSDR ASAA2016032116055Lamp · failedLAMPS INOPERATIVE RT OVERWING EMERGENCY EXIT SIGN, OVERWING CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN, L1 DOOR OVERHEAD EMERGENCY EXIT SIGN, R1 DOOR OVERHEAD EMERGENCY EXIT SIGN, L2 DOOR OVERHEAD EMERGENCY EXIT SIGN. REF LOG PAGES 11495051, 11495052, 11495053Mar 21, 2016 · N618AS · Boeing 737790 · Emergency LightingSDR ASAA2016031015883Latch · failedREPORTED BY F/A: L-1 DOOR SLIDE LATCH ASSY BROKEN. ACFT GROUNDED. R & R LATCH ASSY REF AMM 25-66-01-400-803, 25-66-01-00-801, 25-66-01-00-802, 25-66-01-400-801.Mar 10, 2016 · N618AS · Boeing 737790 · Escape SlideSDR ASAA2016030215736Fuel Cell · corrodedAFTER REMOVAL OF RT DRAG LINK ASSY. FOUND CENTER FUEL TANK SKIN CORRODED. ACFT GROUNDED. BLENDED CORRODED RT CENTER FUEL TANK SKIN, OUT OF LIMITS, IAW SRM 5710-01-1A-2, ACCOMPLISHED EA 700-57EA-16677, W-1.500, O-.304, R-.268, L-1.600, D-0.036.Mar 2, 2016 · N618AS · Boeing 737790 · Fuel StorageSDR ASAA2015122014361Sign · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 1 GALLEY ADJACENT TO R-1 DOOR HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REF WDM 33-51-21-2, FOUND LIGHT ASSY L1186 BROKEN. REMOVED, REPLACED, AND TESTED L1186 EMERGENCY LIGHT EXIT LOCATOR SIGN IAW AMM 33-51-01-960-Dec 20, 2015 · N618AS · Boeing 737790 · Emergency LightingSDR ASAA2015100618539Skin · damagedUPPER HINGE FWD UPPER SKIN CUTOUT DEFORMED AND APPEARS GOUGED ON L1 DOOR. ACFT GROUNDED. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-40-02, DWG S 141A8180, 141A3110, 141A3112, SRM 51-20-01 AND AMM 51-21-99.Oct 6, 2015 · N618AS · Boeing 737790 · Passenger/Crew DoorsSDR ASAA2014120510000Floor Support · corrodedAFT CARGO BAY RT OTBD FLOOR SUPPORT CORRODED FROM BS 787-827, RBL 13.8. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. R & R THE FLOOR SUPPORT IAW SRM 51-40-05, 51-40-02 AND DWG 146A7500.Dec 5, 2014 · N618AS · Boeing 737790 · Fuselage Miscellaneous StructureSDR ASAA2014120209894Window Frame · crackedRT WINDOW POST BETWEEN R1 AND R2 WINDOWS CRACKED IN UPPER FOWARD RADIUS. ACFT GROUNDED. ACCOMPLISHED HFEC INSPECTION OF R1 OTBD WINDOW POST IAW MM PART 6 51-00-00, PROC 23, FOUND TO BE CRACKED. REPAIR OF R1 WINDOW POST TO BE ACCOMPLISHED ON SB737-53-1336-NDec 2, 2014 · N618AS · Boeing 737790 · Fuselage Main, StructureSDR ASAA2014092209204Power Supply · failedEMERGENCY LIGHTS INOPERATIVE SEATS 10 & 17 LT SIDE AND BOTH OVERWING ESCAPE GROUND. GROUNDED. R & R REPLACED THE LAMPS AND POWER SUPPLY. OPS GOOD, IAW AMM 33-51-00.Sep 22, 2014 · N618AS · Boeing 737790 · Emergency Lighting
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