# Service difficulty reports: N553AS

A list on [N553AS](https://openairdocs.org/aircraft/N553AS.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 2 · 93 reports

- [SDR ASAA2026091068717](https://openairdocs.org/sdr/ASAA2026091068717.md): Lens · detached · Sep 10, 2026 · N553AS · Boeing 737890 · Emergency Lighting
  > EXIT SIGN LENS AT ROW 16A FELL OFF. GROUNDED - YES. REPLACED EXIT SIGN LENS ASSY AT ROW 16A IAW CMM 33-51-01. OPS CHKD GOOD.
- [SDR ASAA2026010263560](https://openairdocs.org/sdr/ASAA2026010263560.md): Battery Pack · inoperative · Jan 2, 2026 · N553AS · Boeing 737890 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST. FOUND LT SIDE BOTH OVERWING LIGHTT & OVERWING ESCAPE GROUND ILLUMINATION LIGHT & RT SIDE FWD OVERWING LIGHT INOPERATIVE. GROUNDED - YES. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK (M1670) THEN LT SIDE AFT OVERWING LIGHT & OVERWING
- [SDR ASAA2025041557461](https://openairdocs.org/sdr/ASAA2025041557461.md): Floorbeam · damaged · Apr 15, 2025 · N553AS · Boeing 737890 · Fuselage Main, Floor Beam
  > PANEL BREAK AT STA 540 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED 2EA PANEL BREAKS IAW B737-800 SRM 51-40-02-0G-0.
- [SDR ASAA2025041557460](https://openairdocs.org/sdr/ASAA2025041557460.md): Floorbeam · damaged · Apr 15, 2025 · N553AS · Boeing 737890 · Fuselage Main, Floor Beam
  > PANEL BREAK AT STA 540 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED 2EA PANEL BREAKS IAW B737-800 SRM 51-40-02-0G-0.
- [SDR ASAA2025041358443](https://openairdocs.org/sdr/ASAA2025041358443.md): Baffle · cracked · Apr 13, 2025 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > WHILE ACCOMPLISHMING NUT PLATE REPLACEMENT IN FWD CARGO FOUND BAFFLE CRACKED BETWEEN STA 500D AND 500E. GROUNDED - YES. REMOVED AND REPLACED BAFFEL IAW B737-800 SRM 51-40-02-OG-0.
- [SDR ASAA2025040657462](https://openairdocs.org/sdr/ASAA2025040657462.md): Doubler · cracked · Apr 6, 2025 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER RECEPTACLE DOOR LOWER LATCH WORN/WON'T CLOSE PROPERLY. GROUNDED - YES. UPON INVESTIGATION DETERMINED THAT LATCH NOT WORKING DUE TO LANDING CRACKED, REPAIRED DAMAGE IAW B737-800 SRM 53-10-15-2R-4.
- [SDR ASAA2024122354844](https://openairdocs.org/sdr/ASAA2024122354844.md): Door · binding · Dec 23, 2024 · N553AS · Boeing 737890 · Passenger/Crew Doors
  > FA REPORTS L1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. PERFORMED GVI OF L1 DOOR SURROUND AND DOOR. OPERATED L1 DOOR NUMEROUS CYCLES REF AMM TASK 52-11-00. CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY. OK FOR CONTINUED SERVICE.
- [SDR ASAA2024091653053](https://openairdocs.org/sdr/ASAA2024091653053.md): Skin Lap · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > R/H SEC 46 LWR LAP SEAM FROM STA 847 TO STA 887 STR 23R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON FUSELAGE SKIN P/N:146A3251-32/ 146A3231-23 AT R/H SEC 46 LWR LAP SEAM FROM STA 847 TO STA 887 STR 23R IAW EA800-53EA-27651
- [SDR ASAA2024091653052](https://openairdocs.org/sdr/ASAA2024091653052.md): Skin Lap · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > R/H SEC 43 LWR LAP SEAM AT STA 492.5 TO STA 500F AT STR 24R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON SKIN PANELS P/NS: 143A3252-29 AND 143A3232-28 IAW EA. NO. 800-53EA-27668 REV 00.
- [SDR ASAA2024091653051](https://openairdocs.org/sdr/ASAA2024091653051.md): Skin Buttjoint · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > L/H SIDE BUTT JOINT STA 887 TO BUTT JOINT STA 1016 STR 23L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON FUSELAGE SKIN P/N 147A3110-3 AT L/H SIDE BUTT JOINT STA 887 TO BUTT JOINT STA 1016 STGR 23L IAW EA 800-53EA-27677 REV 0
- [SDR ASAA2024091653050](https://openairdocs.org/sdr/ASAA2024091653050.md): Skin Lap · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > R/H SEC 47 LWR LAP SEAM FROM STA 887 TO STA 967 STR 23R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON R/H FUSELAGE SKIN P/N 147A3110-4 AT R/H SEC 47 LWR LAP SEAM FROM STA 887 TO STA 967 STR. 23R IAW EA 800-53EA-27666 REV 00.
- [SDR ASAA2024091653049](https://openairdocs.org/sdr/ASAA2024091653049.md): Skin · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > R/H LAP JOINT AT STA 1016 TO STA 1088 AT STR 16 SEC 48 HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON SKIN PANELS P/N 148A3331-1 AND P/N 148A3321-13 IAW EA 800-53EA-27640 REV. 00.
- [SDR ASAA2024091653048](https://openairdocs.org/sdr/ASAA2024091653048.md): Skin Panel · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > R1 DOOR FWD EDGE OF FRAME AT STR 14R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON SKIN PANEL 141A3312-2 AT R1 DOOR FWD CUTOUT EDGE IAW EA 800-53EA-27656 REV 00.
- [SDR ASAA2024091653028](https://openairdocs.org/sdr/ASAA2024091653028.md): Skin Lap · corroded · Sep 16, 2024 · N553AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > L/H SEC 46 LWR LAP SEAM AT STA 727E TO STA 887 AT STR 23L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON L/H FUSELAGE SKINS 146A3201-32 / 146A3231-23 SEC 46 LAP SEAM AT STA 727E TO STA 887 STGR 23L IAW EA 800-53EA-27669 REV 0
- [SDR ASAA2024082051961](https://openairdocs.org/sdr/ASAA2024082051961.md): Power Supply · inoperative · Aug 20, 2024 · N553AS · Boeing 737890 · Emergency Lighting
  > TC 78233008 - EMERGENCY EXIT LTS INOP @ FWD RT DOORWAY, FWD RT ESCAPE SLIDE LT, & FWD CEILING LT. GROUNDED - YES. REPLACED M1674 EMERGENCY EXIT PWR SUPPLY & BATTERY PACK, FWD RT DOORWAY, FWD RT ESCAPE SLIDE, & FWD CEILING EMERGENCY EXIT LTS OPS CHECKS OK. REF
- [SDR ASAA2024081351751](https://openairdocs.org/sdr/ASAA2024081351751.md): Sign · dislodged · Aug 13, 2024 · N553AS · Boeing 737890 · Emergency Lighting
  > MID CABIN OVERHEAD EXIT SIGN DISLODGED. GROUNDED - YES. REINSTALLED MID CABIN OVERHEAD EXIT SIGN PER AMM 33-51-01-960-802. OPS CHECK GOOD.
- [SDR ASAA2024032648658](https://openairdocs.org/sdr/ASAA2024032648658.md): Light · inoperative · Mar 26, 2024 · N553AS · Boeing 737890 · Emergency Lighting
  > REF T/C 78233001 EMERGENCY SLIDE LIGHT AFT OF L2 DOOR INOP. GROUNDED - YES. RELAMPED EMERGENCY SLIDE LIGHT AFT OF L2 DOOR REF AMM 33-51-04 OPS CHECK GOOD.
- [SDR ASAA2024032648657](https://openairdocs.org/sdr/ASAA2024032648657.md): Battery Pack · no test · Mar 26, 2024 · N553AS · Boeing 737890 · Emergency Lighting
  > REF T/C 78233001 BATTERY PACKS M1675, M1674, M1673, M1672 AND M1671 FAILED CAPACITANCE CHECK. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS M1671, M1672, M1673, M1674 AND M1675 REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR ASAA2023033042657](https://openairdocs.org/sdr/ASAA2023033042657.md): Rib · cracked · Mar 30, 2023 · N553AS · Boeing 737890 · Vertical Stabilizer
  > DURING OKAY TO CLOSE INSPECTION FOR THE LEFT HAND HORIZONTAL STABILIZER LEADING EDGE FOUND A CRACK IN RIB AT APPROX STAB STA 111.10. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED RIB IAW B737-800 SRM 55-10-09-2R-4.
- [SDR ASAA2023031442504](https://openairdocs.org/sdr/ASAA2023031442504.md): Skin · cracked · Mar 14, 2023 · N553AS · Boeing 737890 · Horizontal Stabilizer Structure
  > RIGHT HORIZ STAB LOWER SKIN IS CRACKED AT THE IB SIDE OF RIB STA 147.90 APPROX 16 INCHES FWD OF REAR SPAR. GROUNDED - YES. REMOVED DAMAGE AND REPLACED RH HORIZ STAB LOWER SKIN AT STA 147.9 THIS IS A CAT B REPAIR WITH A REPEAT INSPECTION OF 9,000 FLIGHT CYCLES
- [SDR ASAA2023030142147](https://openairdocs.org/sdr/ASAA2023030142147.md): Unknown · unknown · Mar 1, 2023 · N553AS · Boeing 737890 · Passenger/Crew Doors
  > FLIGHT DECK DOOR HAS TROUBLE CLOSING AND STAYING LOCKED. GROUNDED - YES. FLIGHT DECK DOOR OPS CKS NORMAL IAW B737-800 AMM 52-51-01.
- [SDR ASAA2021111336599](https://openairdocs.org/sdr/ASAA2021111336599.md): Lamp · inoperative · Nov 13, 2021 · N553AS · Boeing 737890 · Emergency Lighting
  > L/H FWD WING/SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED L/H FWD WING/SLIDE EMERGENCY LIGHT REF B737-800 AMM 33-51-04.OPS CHECK GOOD.
- [SDR ASAA2021051834948](https://openairdocs.org/sdr/ASAA2021051834948.md): Floor Panel · damaged · May 18, 2021 · N553AS · Boeing 737890 · Fuselage Floor Panel
  > PARTS RACK-DUE TO FLOOR STRUCTURE REPAIR PLUG ALL SCREW HOLES ON THE FORWARD EDGE OF 147A5810-27 AND 147A5810-28. GROUNDED - YES. REPAIRED PANELS 147A5810-27 AND 147A5810-28 HOLES ON THE FWD EDGE IAW B737-800 SRM 53-00-50-01-1, 53-00-50-2R-6.
- [SDR ASAA2021051634944](https://openairdocs.org/sdr/ASAA2021051634944.md): Floor Support · damaged · May 16, 2021 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > PARTS RACK- DUE TO FLOOR STRUCTURE REPAIR PLUG 8EA HOLES IN 147A5810-23, 4EA HOLES IN 147A5810-90. ALL HOLES MARKED IN RED. GROUNDED - YES. PLUGGED A TOTAL OF 12 INSERT HOLES. 8EA ON PNL PN 147A5810-23, 4EA ON PNLPN 147A5810-23 USING FACESHEET AND CORE REPAIR
- [SDR ASAA2021051134945](https://openairdocs.org/sdr/ASAA2021051134945.md): Web · corroded · May 11, 2021 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > PARTS RACK- AFT WET AREA, R/H GALLEY SUPPORT WEB IS CORRODED (P/N 147A5712-35). GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL THICKNESS IS.040, REMAINING IS.030,.010 WAS REMOVED. LOCATED ANDDRILLED NEW W
- [SDR ASAA2021050334950](https://openairdocs.org/sdr/ASAA2021050334950.md): Floorbeam · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Main, Floor Beam
  > SPOT OF CORROSION LOCATED AT MAIN CABIN FLOOR BEAM STA. 987 UPPER SURFACE AROUND FASTENER HOLE, APPROX. LBL 43. AREA MARKED IN RED. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL THICKNESS IS.150, REMAINING IS.141,.0
- [SDR ASAA2021050334949](https://openairdocs.org/sdr/ASAA2021050334949.md): Door Sill · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > SPOT OF CORROSION LOCATED AT L2 DOOR LOWER SILL WEBB UPPER SURFACE LOCATED AT LBL 47 APPROX. STA. 987. AREA CIRCLED IN RED. GROUNDED - YES. REMOVED AND REPLACED L/H INNER CHORD IAW BOEING DWG, 147A8501 REV B REMOVED DOT AND RED MARKS.
- [SDR ASAA2021050334904](https://openairdocs.org/sdr/ASAA2021050334904.md): Fitting · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > IN AFT WET AREA, CORROSION FOUND AROUND 2 EA. TOTAL LAVATORY FLOORSTRUCTURE FITTINGS, 1 EA. AT STA. 947, LBL 25, AND 1 EA. AT STA. 916, LBL 52. AREAS MARKED IN RED. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL MAT'L T
- [SDR ASAA2021050334903](https://openairdocs.org/sdr/ASAA2021050334903.md): Floorbeam · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT STRUCTURE LOCATED AT APPROX. STA. 950, APPROX. RBL45, 4 IN. FWD. OF R2 DOOR, HAS SPOT OF CORROSION ON UPPER SURFACE. AREA MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED SUPPORT REF BAC DWG 147A5650 SH 70 & 71 REV "A"CORROSION FOUND TO BE OUT
- [SDR ASAA2021050334902](https://openairdocs.org/sdr/ASAA2021050334902.md): Intercostal · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON BOTH UPPER AND LOWER SURFACES OF INTERCOSTAL LOCATED APPROX. 4 IN. FWD. OF R2 DOOR APPROX. STA. 950-956, RBL46. AREAS MARKED IN RED. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL IS.205, REMAINING I
- [SDR ASAA2021050334901](https://openairdocs.org/sdr/ASAA2021050334901.md): Intercostal · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON BOTH UPPER AND LOWER SURFACES OF INTERCOSTAL LOCATED APPROX. 9 IN. FWD. OF R2 DOOR STA. 947, RBL49. AREAS MARKED IN RED. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL THICKNESS IS.090, REMAINING IS
- [SDR ASAA2021050334786](https://openairdocs.org/sdr/ASAA2021050334786.md): Transition Panel · corroded · May 3, 2021 · N553AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT RIGHT SIDE TRANSITION PANEL SHOWS EVIDENCE OF CORROSION FROM STA:727 TO STA:767. GROUNDED - YES. REMOVED DAMGE ON R/H TRANSITION PNL FROM STA 727 - 767 ORIG. THICKNESS 0.040 PER BAC 1496-377, REMOVED 0.009, MATL REMAINING 0.031 AND FOUND
- [SDR ASAA2021050234951](https://openairdocs.org/sdr/ASAA2021050234951.md): Seat Track · corroded · May 2, 2021 · N553AS · Boeing 737890 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND INSIDE INBD. MAIN CABIN SEAT TRACK, LBL44, APPROX. STA. 368-380 IN MULTIPLE SPOTS. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-00-52.ORIGINAL THICKNESS IS.55, REMAINING IS.50,.05 WAS REMOVED.020 REMOV
- [SDR ASAA2021050134947](https://openairdocs.org/sdr/ASAA2021050134947.md): Floor Panel · damaged · May 1, 2021 · N553AS · Boeing 737890 · Fuselage Floor Panel
  > SECTION 41 FLOOR PANEL 141A5810-175 HAS MISSING INSERTS. GROUNDED - YES. INSTALLED SECTION 41 FLOOR PANEL 141A5810-175 MISSING INSERTS IAW B737-800-SRM-53-00-50-2R-4 AND 53-00-50-2R-0. AND ACCOMPLISHED PERMENANT F/G REPAIR IAW B737-SRM 53-00-50-2R-REP 2.
- [SDR ASAA2021043034946](https://openairdocs.org/sdr/ASAA2021043034946.md): Floor Panel · damaged · Apr 30, 2021 · N553AS · Boeing 737890 · Fuselage Floor Panel
  > PARTS RACK- SECTION 47 MAIN CABIN FLOOR PANEL 147A5810-267 HAS NUMEROUS BROKEN/CORRODED INSERTS. GROUNDED - YES. REMOVED THREE (3) CORRODED INSERTS AND REPLACED WITH NEW SLS5182A3 INSERTSON MAIN CABIN FLOOR PANEL 147A5810-267. REPAIRED DAMAGED FACE SHEET AND I
- [SDR ASAA2018112527091](https://openairdocs.org/sdr/ASAA2018112527091.md): Snubber · binding · Nov 25, 2018 · N553AS · Boeing 737890 · Passenger/Crew Doors
  > F/A REPORT L1 DOOR HARD TO CLOSE WHEN CLOSING SLOW. GROUNDED - YES. REMOVED AND REPLACED FWD ENTRY DOOR SNUBBER AND ADJUSTED L1 DOOR UPPER GUIDE ARM, OPS CHECK SATISFACTORY AT THIS TIME. AMM 52-11-51 AND 52-11-00/501, 52-11-00-802-801.
- [SDR ASAA2018092426225](https://openairdocs.org/sdr/ASAA2018092426225.md): Light · inoperative · Sep 19, 2018 · N553AS · Boeing 737890 · Emergency Lighting
  > AFT LAMP BURNED OUT IN LT FWD OVERWING EXIT SIGN. GROUNDED - YES. RELAMPED, OPS TEST GOOD REF AMM 33-51-01.
- [SDR ASAA2017051220781](https://openairdocs.org/sdr/ASAA2017051220781.md): Floor Support · corroded · May 12, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT AT BS 947 - 967, RBL 24 CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15. LOCATED, DRILLED, DEBURRED AND COUNTERSUNK IAW SRM 51-40-05, SRM 51-40-08, AND DRAWING 147A5650 REV-, SHEET 44.
- [SDR ASAA2017050320780](https://openairdocs.org/sdr/ASAA2017050320780.md): Baffle · cracked · May 3, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY, LT SIDE, BAFFLE IS CRACKED BS 500G - 500H, STRINGERS 25 - 26L. ACFT GROUNDED. REMOVED AND REPLACED THE BAFFLE IAW DWG 143A7505, REV B, AND SRM 51-40-02.
- [SDR ASAA2017042920778](https://openairdocs.org/sdr/ASAA2017042920778.md): Attach Angle · cracked · Apr 29, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT RIGHT SIDE INTERCOSTAL ATTACH ANGLE CRACK ATBS500G STR26R. GROUNDED - YES. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW B DWG 143A7505 REV B AND SRM 51-40-05. INSTALLED CLIP IAW B DWG 143A7505 REV B AND SRM 51-40-02.
- [SDR ASAA2017042920777](https://openairdocs.org/sdr/ASAA2017042920777.md): Attach Angle · cracked · Apr 29, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT RIGHT SIDE INTERCOSTAL ATTACH ANGLE CRACK ATBS500F STR26R. GROUNDED - YES. REMOVED INTERCOSTAL ATTACH ANGLE IAW B737-800 SRM 51-40-02. RECEIVED CLIP, LOCATED AND DRILLED IAW B DWG 143A7505 REV B AND SRM 51-40-05. INSTALLED CLIP IAW B DWG 143A7505 REV B
- [SDR ASAA2017042920776](https://openairdocs.org/sdr/ASAA2017042920776.md): Attach Angle · cracked · Apr 29, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT LT SIDE INTERCOSTAL ATTACH ANGLE CRACK AT BS 500G STR26L. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LT SIDE INTERCOSTAL ATTACH ANGLE (CLIP) 1EA AT STA 500G STR26L PER DWG 143A7505 REV B AND SRM 51-40-02.
- [SDR ASAA2017042920698](https://openairdocs.org/sdr/ASAA2017042920698.md): Attach Angle · cracked · Apr 29, 2017 · N553AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > FWD CARGO LT SIDE INTERCOSTAL ATTACH ANGLE CRACKED AT BS 500H STRINGER 26L. ACFT GROUNED. REMOVED AND REPLACED FWD CARGO ATTACH ANGLE IAW DWG 143A7505 REV: B AND SRM 51-40-02.
- [SDR ASAA2017042720796](https://openairdocs.org/sdr/ASAA2017042720796.md): Frame · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Main, Frame
  > MAIN CABIN FRAME CORRODED BS 951, RBL 51. ACFT GROUNDED. REMOVED CORROSION, PERFORMED HFEC INSPECTIONS, PERFORMED VISUAL INSPECTION OF ADJACENT STRUCTURE, FABRICATED, ALODINED, PRIMED, AND INSTALLED A REPAIR. APPLIED BMS 5-23 IAW EA 800-53EA-18800.
- [SDR ASAA2017042720754](https://openairdocs.org/sdr/ASAA2017042720754.md): Intercostal · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN INTERCOSTAL CORRODED AROUND FASTENER HOLES BS 951 - RBL 34, RBL 47. GROUNDED - YES. EVALUATED THE INTERCOSTAL AT BS 951.086, RBL 25 - RBL 47, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15. REMOVED AND REPLACED WITH NEW INTERCOSTAL IAW SRM 51-40-02 AND
- [SDR ASAA2017042720753](https://openairdocs.org/sdr/ASAA2017042720753.md): Structure · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > RIGHT HAND INNER CHORD HAS CORROSION FROM STA 943.5-STA 958. GROUNDED - YES. EVALUATED THE RIGHT-HAND INNER CHORD AT BS 973 - BS 958 FOR CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51. REMOVED AND REPLACED INNER CHORD IAW SRM 51-40-02 AND DWG 147A850
- [SDR ASAA2017042720749](https://openairdocs.org/sdr/ASAA2017042720749.md): Floorbeam · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 947.5 HAS CORROSION FROM RBL49-RBL54. GROUNDED - YES. EVALUATED CORROSION ON THE UPPER SURFACE OF THE T-CAP OF FLOORBEAM AT BS 947.5, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51. ACCOMPLISHED A CATEGORY "A" REPAIR TO THE FLOORBEAM AT BS 947.5 L
- [SDR ASAA2017042720709](https://openairdocs.org/sdr/ASAA2017042720709.md): Floor Support · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BS 947.5 - 967, RBL 50 HAS CORROSION. ACFT GROUNDED. EVALUATED CORROSION AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-70-51. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 147A5650, SHEET 44, REV -.
- [SDR ASAA2017042720697](https://openairdocs.org/sdr/ASAA2017042720697.md): Tee Fitting · corroded · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Main, Structure
  > MAIN CABIN T-CAP CORRODED AROUND FASTENER HOLE BS 986.5 - RBL 43. GROUNDED - YES. REPAIRED MAIN CABIN T-CAP BS 986.5 - RBL 43 IAW B737-800 SRM 53-70-51 FIG. 203 REPAIR 6. REMAINING FASTENERS TO BE INSTALLED ON ASA CARD G0859031. (ORIG THICKNESS.150, REMOVED.
- [SDR ASAA2017042720590](https://openairdocs.org/sdr/ASAA2017042720590.md): Floor Support · cracked · Apr 27, 2017 · N553AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT CRACKED BS 380 - 400. ACFT GROUNDED. REMOVED AND REPLACED IAW DWG 143A5400 AND SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N553AS/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 = 'N553AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N553AS/reports

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