# Service difficulty reports: N514AS

A list on [N514AS](https://openairdocs.org/aircraft/N514AS.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 8 · 370 reports

- [SDR ASAA2025123163493](https://openairdocs.org/sdr/ASAA2025123163493.md): Door · binding · Dec 31, 2025 · N514AS · Boeing 737890 · Passenger/Crew Doors
  > FA REPORTS L1 VERY DIFFICULT TO OPEN. GROUNDED - YES. PERFORMED L1 DOOR FWD ENTRY DOOR SYSTEM TEST. DOOR IS WITHIN OPEN / CLOSE TORQUE SPECS. NO HISTORY PAST 90 DAYS.
- [SDR ASAA2025061658810](https://openairdocs.org/sdr/ASAA2025061658810.md): Light · detached · Jun 16, 2025 · N514AS · Boeing 737890 · Emergency Lighting
  > FA REPORTS EMERGENCY LIGHTING COVER CAME OFF NEAR ROW 16F. GROUNDED - YES. INSTALLED NEW EMERG/EXIT LIGHTING COVER @ ROW 16F.
- [SDR ASAA2025050757798](https://openairdocs.org/sdr/ASAA2025050757798.md): Sign · detached · May 7, 2025 · N514AS · Boeing 737890 · Emergency Lighting
  > F/A S REPORT LOWER EXIT SIDEWALL SIGN WILL NOT STAY ATTACHED AT 16A. GROUNDED - YES. REMOVED AND REPLACED EXIT LIGHT ASSY AT ROW 16A I/A/W AMM 33-51-01. OPS CHECK GOOD.
- [SDR ASAA2025012756002](https://openairdocs.org/sdr/ASAA2025012756002.md): Skin · corroded · Jan 27, 2025 · N514AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN BS.887 TO BS.1016 STR.23L UPPER LAP SHOWS SIGNS OF CORROSION 17 AREA. (MARKED IN RED). GROUNDED - YES. REMOVED CORROSION 17(EA) ON ZONE B. DAMAGE AREAS FROM STA 887-STA 1016 STR 23L UPPER LAP ORG MAT THICK 0.063, REMOVED 0.004 REMAINING 0.059 FOU
- [SDR ASAA2025012155907](https://openairdocs.org/sdr/ASAA2025012155907.md): Intercostal · corroded · Jan 21, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > (LATE FIND) AFT PIT BILGE INTERCOSTAL AT STA 867 TO 887 LBL 10 IS CORRODED. GROUNDED - YES. UPON FURTHER EVALUATION THE AFT PIT INTERCOSTAL AT STA 867-887, LBL 10 IS FOUND TO HAVE 100% MAT LOSS NO ALLOWABLE DAMAGE LIMITS ARE GIVEN IN B737-800 SRM. REMOVED DAMA
- [SDR ASAA2025011455731](https://openairdocs.org/sdr/ASAA2025011455731.md): Intercostal · corroded · Jan 14, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT BS.847 TO BS.867 BETWEEN STR.25L - STR.26L INTERCOSTAL CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT L/H INTERCOSTAL AT STA 847 TO 867, STR25L TO 26L IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS.045" IAW B737-800
- [SDR ASAA2025011355910](https://openairdocs.org/sdr/ASAA2025011355910.md): Web · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > R/H AFT CABIN AT STA 992 FLOOR SUPPORT WEB UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS 0.040. REMOVED 0.007, REMAINING 0.033. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED WEB IAW
- [SDR ASAA2025011355909](https://openairdocs.org/sdr/ASAA2025011355909.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > R/N AFT CABIN AT STA 1016 FLOOR SUPPORT ANGLE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. LOCATED,
- [SDR ASAA2025011355908](https://openairdocs.org/sdr/ASAA2025011355908.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE STRUCTURE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION, 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. DRILLED TO FIT NEW FLOOR S
- [SDR ASAA2025011355905](https://openairdocs.org/sdr/ASAA2025011355905.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > R/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-0.2. 100% MATERIAL LOSS-OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. DRILLED TO
- [SDR ASAA2025011355904](https://openairdocs.org/sdr/ASAA2025011355904.md): Web · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN AT STA 992 FLOOR SUPPORT WEB UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02 AND BOEING DWG 147A5700 REV B
- [SDR ASAA2025011355903](https://openairdocs.org/sdr/ASAA2025011355903.md): Support Angle · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > R2 GALLEY DOOR SILL PANEL SUPPORT ANGLE SURFASE CORRODED AT MULTIPLE SPOTS BETWEEN BS 951 AND 993. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. AREA FOUND TO BE 100% MAT LOSS OUT OF LIMITS. REMOVED AND REPLACED MOP SEAL INNER CHORD IAW B737-800
- [SDR ASAA2025011355802](https://openairdocs.org/sdr/ASAA2025011355802.md): Floorbeam · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Main, Floor Beam
  > R/H AFT CABIN AT STA 986 FLOOR BEAM UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, ORIG THICKNESS 0.150", REMOVED 0.045", REMAINING 0.105" OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1, REPAIRED DAMAGE IAW B737-800 S
- [SDR ASAA2025011355801](https://openairdocs.org/sdr/ASAA2025011355801.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE STRUCTURE UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT IAW B737-800 SRM 51-10-02. NO ALLOWABLE DAMAGE LIMITS STATED. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02 AN
- [SDR ASAA2025011355649](https://openairdocs.org/sdr/ASAA2025011355649.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CORROSION FOUND IN HOLES (3 EACH) ON PANEL BREAK BETWEEN STATION 328 AND STATION 344 BUTT LINE 10. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 328 TO 344 BUTT LINE 10 IAW B737-800 SRM 51-40-02.
- [SDR ASAA2025011355648](https://openairdocs.org/sdr/ASAA2025011355648.md): Floor Support · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN BETWEEN STA 907 AND STA 927 FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION AREAS IAW B737-800 SRM 51-10-02. PART FOUND TO BE OUT OF LIMITS 100% MAT LOSS. REMOVED AND REPLACED NEW FLOOR SUPPORT STRUCTURE IAW
- [SDR ASAA2025011355647](https://openairdocs.org/sdr/ASAA2025011355647.md): Transition Panel · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LEFT TRANSITION PANELS HAVE CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, L/H TRANSITION PANEL AT STA 727B+10 TO 797 IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS.040" IAW B737-800 SRM 53-60-53-01-2 TABLE 2 FOUND
- [SDR ASAA2025011355646](https://openairdocs.org/sdr/ASAA2025011355646.md): Floorbeam · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Main, Floor Beam
  > AFT CABIN AT STA 951 FLOOR BEAM UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS I.A.W. B737-800 SRM 53-70-51-1A-1 ORIGINAL THICKNESS.180, MAT REMAINING.142 IAW B737-800 SRM 53-70-51-01-1, FABRI
- [SDR ASAA2025011355643](https://openairdocs.org/sdr/ASAA2025011355643.md): Transition Panel · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RIGHT TRANSITION PANELS HAVE CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANELS FROM STA 727 TO 767 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS.040" IAW B737-800 SRM 53-60-53-01-2. FOUND TO HAVE 100% M
- [SDR ASAA2025011355642](https://openairdocs.org/sdr/ASAA2025011355642.md): Intercostal · corroded · Jan 13, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CORROSION FOUND IN HOLES (5 EACH) ON PANEL BREAK BETWEEN STATION 312 AND STATION 328 BUTT LINE 10. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 TO 328 BUTT LINE 10 IAW B737-800 SRM 51-40-02.
- [SDR ASAA2025011255644](https://openairdocs.org/sdr/ASAA2025011255644.md): Angle · corroded · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AFT MIX BAY ACCESS PANEL(A/C SIDE) NUT PLATE ANGLE L/H-R/H STA500I HAS SEVERAL AREAS OF CORROSION UPPER AND LOWER SURFACE. GROUNDED - YES. REMOVED AND REPLACED NEW RAIL P/N 143A9485Y35 P.O. 1111512.1, LOCATED AND DRILLED HOLES AT FWD CARG
- [SDR ASAA2025011255565](https://openairdocs.org/sdr/ASAA2025011255565.md): Floor Panel · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-136. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION 147A5810-136 IAW B737-800-SRM-53-00-50-2R-1 AND SRM-53-00-50-2R-0.
- [SDR ASAA2025011255564](https://openairdocs.org/sdr/ASAA2025011255564.md): Floor Panel · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-155. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF FORWARD WET AREA FLOOR BOARD DELAMINATION 141A5810-155 IAW B737-800-SRM-53-00-50-2R-1 AND SRM-53-00-50-2R-0.
- [SDR ASAA2025011255563](https://openairdocs.org/sdr/ASAA2025011255563.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-755. GROUNDED - YES. COMPLETED PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD 141A5810-755 IAW B737-800 SRM 53-00-50-2R-0.
- [SDR ASAA2025011255562](https://openairdocs.org/sdr/ASAA2025011255562.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-728. GROUNDED - YES. COMPLETED PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD 141A5810-728 IAW B737-800 SRM 53-00-50-2R-0.
- [SDR ASAA2025011255561](https://openairdocs.org/sdr/ASAA2025011255561.md): Floor Panel · damaged · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAMINATED 147A5810-137. GROUNDED - YES. PREFORMED PERMANT REPAIR TO MAIN CABIN AFT WET AREA FLOORBOARD 147A5810-137 IAW B737-800 SRM 53-00-50-2R-0.
- [SDR ASAA2025011255560](https://openairdocs.org/sdr/ASAA2025011255560.md): Floor Panel · damaged · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-28. GROUNDED - YES. PERFORMED PERMANT REPAIR TO MAIN CABIN AFT WET AREA FLOORBOARD 147A5810-28 IAW B737-800 SRM 53-00-50.
- [SDR ASAA2025011255559](https://openairdocs.org/sdr/ASAA2025011255559.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-454. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON FWD WET AREA FLOOR PANEL 141A5810-454 IAW B737 SRM 53-00-50-2R-0.
- [SDR ASAA2025011255558](https://openairdocs.org/sdr/ASAA2025011255558.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-90. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON MAIN CABIN AFT WET AREA FLOOR BOARD 147A5810-90 IAW B737 SRM 53-00-50-2R-0.
- [SDR ASAA2025011255557](https://openairdocs.org/sdr/ASAA2025011255557.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-27. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON MAIN CABIN AFT WET AREA FLOOR BOARD 147A5810-27 IAW B737 SRM 55-00-50-2R-0.
- [SDR ASAA2025011255503](https://openairdocs.org/sdr/ASAA2025011255503.md): Transition Panel · corroded · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT R/H TRANSITION PANEL HAS CORROSION AT SEVERAL AREAS STA500A-STA500I. GROUNDED - YES. REMOVED CORROSION FROM R/H TRANSITION PNL STA 500A-500I IAW B737-800 SRM 53-00-53-1A-2. ORIG. MATERIAL WAS.040" IAW B737-800 SRM 53-00-53-01-2. REMOVED
- [SDR ASAA2025011255497](https://openairdocs.org/sdr/ASAA2025011255497.md): Floorboard · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-765. GROUNDED - YES. REPAIRED FLOOR BOARD 141A5810-765 OF DELAM USING PERMANENT REPAIR IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-1, 53-00-50-2R-0.
- [SDR ASAA2025011255496](https://openairdocs.org/sdr/ASAA2025011255496.md): Floor Panel · delaminated · Jan 12, 2025 · N514AS · Boeing 737890 · Fuselage Floor Panel
  > FWD WET AREA FLOOR BOARD DELAME 141A5810-763. GROUNDED - YES. REPAIRED FLOOR BOARD 141A5810-763 OF DELAM USING PERMANENT REPAIR IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-1, 53-00-50-2R-0.
- [SDR ASAA2025011155906](https://openairdocs.org/sdr/ASAA2025011155906.md): Web · corroded · Jan 11, 2025 · N514AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT SILL WEB PLATE HAS CORROSION IN LARGE AREA. CIRCLED IN RED. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT DOOR SURROUND WEB IAW B737-800 SRM 53-60-15-1A-1. ORIG THICKNESS IS.050" IAW B737-800 SRM 53-60-15-01-1. FOUND TO BE 100% MATERIAL
- [SDR ASAA2025011155645](https://openairdocs.org/sdr/ASAA2025011155645.md): Strap · corroded · Jan 11, 2025 · N514AS · Boeing 737890 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT HAS CORROSION AROUND SCREW HOLES,AND OTHER SPOTS ON FLOOR STRUCTURE BEHIND THE SILL WEB PANEL. CIRCLED IN RED. GROUNDED - YES. AFTER FURTHER EVALUATION, CORROSION FOUND ON PREVIOUS REPAIR. NO ALLOWABLE DAMAGE LIMITS FOUND. REMOVED ADDITIO
- [SDR ASAA2025010955701](https://openairdocs.org/sdr/ASAA2025010955701.md): Pan · gouged · Jan 9, 2025 · N514AS · Boeing 737890 · Service Doors
  > R1 DOOR, EXTERIOR HANDLE PAN, INSIDE DIAMETER IS GOUGED. GROUNDED - YES. REMOVED GOUGED HANDLE PAN, RECIEVED & INSTALLED NEW HANDLE PAN IAW BAC DWG 141A6516 REV.B & B737-800 SRM 51-40-02-0G-0.
- [SDR ASAA2024121354568](https://openairdocs.org/sdr/ASAA2024121354568.md): Guide Arm · out of adjust · Dec 13, 2024 · N514AS · Boeing 737890 · Passenger/Crew Doors
  > AIRCRAFT WOULDN'T PRESSURIZED AFTER TAKEOFF. FA REPORTED L2 DOOR OPEN. NO DOOR INDICATION IN COCKPIT. RETURN TO JNU. GROUNDED - YES. AIR TURNBACK - ON ARRIVAL L2 DOOR FOUND SLIGHTLY OPEN. FWD ROLLERS FOUND TO BE OUT OF RECEIVERS. PERFORMED AFT ENTRY DOOR ADJUS
- [SDR ASAA2024072651372](https://openairdocs.org/sdr/ASAA2024072651372.md): Sign · detached · Jul 26, 2024 · N514AS · Boeing 737890 · Emergency Lighting
  > GALLEY 1 PLASTIC EXIT WALL SIGN FELL OFF. GROUNDED - YES. GALLEY 1 FWD OF R1 DOOR EXIT WALL LIGHT DAMAGED. REMOVED DAMAGED ASSEMBLY INSTALLED SERVICABLE ONE REF AMM 33-51-00 OPS CHECK GOOD.
- [SDR ASAA2024072051184](https://openairdocs.org/sdr/ASAA2024072051184.md): Sign · detached · Jul 20, 2024 · N514AS · Boeing 737890 · Emergency Lighting
  > R2 DOOR EXIT SIGN FELL OFF IN FLIGHT. GROUNDED - YES. (RESOLVED ON W/O: 2011019 TASKCARD: N/R-00001) R2 DOOR EXIT SIGN ASSY REPLACED REF AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS THE PLT ON LP 61008281.
- [SDR ASAA2024021847913](https://openairdocs.org/sdr/ASAA2024021847913.md): Battery Pack · no test · Feb 18, 2024 · N514AS · Boeing 737890 · Emergency Lighting
  > WHILE PERFORMING TC 78233001 FOUND 3 EMERGENCY LIGHT BATTERY PACKS FAILED. GROUNDED - YES. REPLACED BATTERY PACKS IAW AMM 33-51-06. OPS CHECKS GOOD.
- [SDR ASAA2023101745740](https://openairdocs.org/sdr/ASAA2023101745740.md): Packing · leaking · Oct 17, 2023 · N514AS · Boeing 737890 · AC Generator-Alternator
  > FOLLOW-UP TO #2 IDG FREQUENT SERVICING. (#PRI2/ETOPS). GROUNDED - YES. (RESOLVED ON W/O: 1973837 TASKCARD: N/R-00001) C/W LEAK CHECK WITH A TEN MINUTE IDLE RUN. FOUND PISTON COVER PLATE LEAKING. PLATE IS BELOW IDG RECONNECT RING & ABOVE AFT FILTER. NO EXTERN
- [SDR ASAA2023100645512](https://openairdocs.org/sdr/ASAA2023100645512.md): Unknown · unknown · Oct 6, 2023 · N514AS · Boeing 737890 · Flight Management Computing Hardware System
  > MAP FLAG ILLUMINATED ON CAPTAIN MFD FO SIDE NORMAL. GROUNDED - YES. PERF FMC BITE TEST REF B737-800 FIM 34-61 TASK 801. SYS TEST NORMAL, NO FAULTS LOGGED.
- [SDR ASAA2023092945384](https://openairdocs.org/sdr/ASAA2023092945384.md): Unknown · unknown · Sep 29, 2023 · N514AS · Boeing 737890 · Cabin Pressure Control System
  > "AUTOFAIL" ILLUMINATED ON PRESSURIZATION PANEL "ALTN" ALSO ILLUMINATED. GROUNDED - YES. PERFORMED B737-800 FIM 21-31 TASK 827. PER INITIAL EVALUATION FAULT IS TRANSITORY POSITION OF SWITCH, LIGHT EXTINGUISHED. PERFORMED REPAIR CONFIRMATION AT END OF FIM. NO FA
- [SDR ASAA2023092245268](https://openairdocs.org/sdr/ASAA2023092245268.md): Housing · broken · Sep 22, 2023 · N514AS · Boeing 737890 · Emergency Lighting
  > AFT EXIT SIGN BETWEEN L2 & R2 BROKEN & CROOKED. GROUNDED - YES. (ITEM RESOLVE UNDER MDDR: 60685168) (RESOLVED ON W/O: 1970745 TASKCARD: N/R-00001) REPLACED BROKEN EMERGENCY EXIT SIGN PER AMM 33-51-01. OP CHECKS NORMAL AT THIS TIME. THIS CLEARS MCT DEFERRAL AN
- [SDR ASAA2023090144934](https://openairdocs.org/sdr/ASAA2023090144934.md): Pressure Switch · faulty · Sep 1, 2023 · N514AS · Boeing 737890 · Aircraft Fuel System
  > CENTER TANK RIGHT FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE AFTER FUEL IS EXHAUSTED FROM THAT TANK. FUEL PUMP APPEARED TO OPERATE NORMALLY AND FUEL BURN WAS AS EXPECTED. GROUNDED - YES. PERFORMED INITIAL EVALUATION OF FIM 28-22 TASK 821, PUSH-TO-TEST LI
- [SDR ASAA2023073044328](https://openairdocs.org/sdr/ASAA2023073044328.md): Unknown · unknown · Jul 30, 2023 · N514AS · Boeing 737890 · APU Start/Ignition System
  > FAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL360. SUCCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED. GROUNDED - YES. RECIEVED ACARS MSSG AND PER SEAMC STEVE COLD SOACK APU PASSED. REMOVED MEL 49-99A. SEAMC STEVE NOTIFIED. A/C OK FOR SERVICE.
- [SDR ASAA2023071744086](https://openairdocs.org/sdr/ASAA2023071744086.md): Unknown · unknown · Jul 17, 2023 · N514AS · Boeing 737890 · Hydraulic System, Main
  > DRASTIC REDUCTION OF SYSTEM A AT ROTATION. FLT CONTROL AND HYD CAUTION LIGHTS ILLUMINATED. AIR RETURN AS PER FODO/MX CONTROL. GROUNDED - YES. AIR TURNBACK - PERFORMED SYS A LEAK CHK REF AMM 29-00-00-790-810. NO LEAKS NOTED. PER CAPT BRIEFING REFERENCE, ON LAND
- [SDR ASAA2023070543908](https://openairdocs.org/sdr/ASAA2023070543908.md): Unknown · unknown · Jul 5, 2023 · N514AS · Boeing 737890 · AC Generation System
  > APU GEN OFF LIGHT NOT ILLUMINATING WHEN APU IS OPERATIONAL. GROUNDED - YES. STARTED APU. APU GEN OFF LIGHT WORKS NORMAL. CYCLED APU GEN OFF AND ON SEVERAL TIMES WITH NO FAULTS. APU GCU BITE GOOD. REF FIM 24-21 TASK 801.
- [SDR ASAA2023060643478](https://openairdocs.org/sdr/ASAA2023060643478.md): Plate · worn · Jun 6, 2023 · N514AS · Boeing 737890 · Wing Main, Frame Structure
  > WHILE REPLACING OUTBOARD FWD STRIKER PLATE FOR ECS DOOR (192DR) FOUND DAMAGE UNDER STRIKER PLATE IN STRUCTURE MEASURING.093" DEEP,.281" LONG AND.156' WIDE. GROUNDED - YES. REF MIG-5 L/P 300010908 FOR PERMANENT REPAIR PER SRM 57-10-13-2R-3 REPAIR 3. ACC PERM
- [SDR ASAA2023052143329](https://openairdocs.org/sdr/ASAA2023052143329.md): Platform · damaged · May 21, 2023 · N514AS · Boeing 737890 · Turbine Engine Air Inlet Section
  > 1 PLATFORM ON #1 ENGINE DAMAGED. GROUNDED - YES. PLATFORM REPLACED PER ASA T/C 78472010 TEST 7 VIBE SURVEY B737-800 AMM 71-00-00 PB SO1 ACCOMPLISHED.

Next page: https://openairdocs.org/aircraft/N514AS/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N514AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N514AS/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.