# Service difficulty reports: N597AS

A list on [N597AS](https://openairdocs.org/aircraft/N597AS.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 9 · 401 reports

- [SDR ASAA2026062367063](https://openairdocs.org/sdr/ASAA2026062367063.md): Skin · cracked · Jun 23, 2026 · N597AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND, NR 1 RT HORZONTAL STAB LOWER SKIN STAB. STA.157.10.900"L INBD OF INBD ROW OF FASTENERS, 22.75" AFT OF FWD SPAR. GROUNDED - YES. REPLACED THE RT HORIZONTAL STAB LOWER SKIN STAB STA 157.10 IAW SRM 55-10-01-2R-11. REPAIR IS A CAT "B" IN
- [SDR ASAA2026062367062](https://openairdocs.org/sdr/ASAA2026062367062.md): Skin · cracked · Jun 23, 2026 · N597AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND, NR 3 RT HORZONTAL STAB LOWER SKIN STAB. STA.129.50.500"L INBD OF INBD ROW OF FASTENERS, 33.25" AFT OF FWD SPAR. GROUNDED - YES. REPAIRED THE RT HORIZONTAL STAB LOWER SKIN STAB STA 129.50 IAW SRM 55-10-01-2R-11. REPAIR IS A CAT "B" INS
- [SDR ASAA2026042165876](https://openairdocs.org/sdr/ASAA2026042165876.md): Mount · corroded · Apr 21, 2026 · N597AS · Boeing 737890 · Fuselage, Equipment Attach Fittings
  > PASSENGER CABIN STA 916.5 LBL 51.55 DUAL FLOOR MOUNT ATTACHING INTERCOSTAL HAS CORROSION AROUND MOUNT. GROUNDED - YES. REMOVED AND REPLACED 147A5690-8 INTERCOSTAL IAW BAC DWG 147A5680 REV - AND B737-800 SRM 51-40-02. ALLOWABLE LIMITS IN SRM FOUND DEEMED OUT OF
- [SDR ASAA2025110162010](https://openairdocs.org/sdr/ASAA2025110162010.md): Door · no discrepancy · Nov 1, 2025 · N597AS · Boeing 737890 · Passenger/Crew Doors
  > FA REPORTS L1 DOOR DIFFICULT TO CLOSE, REQUIRING MORE FORCE THAN NORMAL. ALSO REPORTED A TAPPING NOISE EMANATING FROM UPPER RIGHT SECTION OF L1 DURING DESCENT, LANDING. DURING TAXI-IN. GROUNDED - YES. INSPECTED FWD L1 DOOR FRAME/SILL AND DOOR ASSY IAW AMM 52-
- [SDR ASAA2025090260530](https://openairdocs.org/sdr/ASAA2025090260530.md): Elec Connector · unsecure · Sep 2, 2025 · N597AS · Boeing 737890 · Light System Wiring
  > EMERGENCY AISLE / AREA LIGHT ABOVE 6 ABC INOPERATIVE. GROUNDED - YES. SECURED D11344 CONNECTOR WDM 33-51-12-6, LIGHT L1065 NOW OPERATING NORMALLY.
- [SDR ASAA2025090260531](https://openairdocs.org/sdr/ASAA2025090260531.md): Battery Pack · inoperative · Sep 2, 2025 · N597AS · Boeing 737890 · Emergency Lighting
  > WHILE WORKING TC 78233001 THE FOLLOWING DEFECTS NOTED: 1) RH FWD OWE GROUND ILLUMINATION LIGHT INOP. 2) L2 OVERDOOR & ASSOCIATED LIGHTS INOP. 3) 21-24 DEF EMERGENCY AISLE LIGHTS INOP. 4) LH OWE GROUND ILLUMINATION & ESCAPE LT INOP. 5) 18-22 ABC EMERGENCY AISLE
- [SDR ASAA2024081952258](https://openairdocs.org/sdr/ASAA2024081952258.md): Rib · cracked · Aug 19, 2024 · N597AS · Boeing 737890 · Horizontal Stabilizer, Spar/Rib
  > (LATE FIND) WHILE INSPECTING FOR AN "OK TO INSTALL" L/H LEADING EDGE, FOUND TWO INTERNAL CRACKS AT STA LES 105.26 VERTICAL, SEGMENTS 3 AND 4. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB AT STA 92.70 3EA LOCATIONS USING MAT BAC1505-100962 T-SECTION, BAC 1490-2
- [SDR ASAA2024081952175](https://openairdocs.org/sdr/ASAA2024081952175.md): Rib · cracked · Aug 19, 2024 · N597AS · Boeing 737890 · Horizontal Stabilizer, Spar/Rib
  > (LATE FIND) WHILE INSPECTING FOR AN "OK TO INSTALL" R/H HORIZONTAL LEADING EDGE. FOUND INTERNAL CRACK AT STA LES 123.85 3 VERTICAL SEGMENTS AFT STREAMER ATTACHED AT OPENING. GROUNDED - YES. REPAIRED THE RIGHT HORIZ STAB RIB AT LE STA 123.85 USING MAT BAC 1505-
- [SDR ASAA2024071851458](https://openairdocs.org/sdr/ASAA2024071851458.md): Baffle · cracked · Jul 18, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT R/H BAFFLE BETWEEN STA 500E AND 500F CORNER BROKEN OFF. GROUNDED - YES. REMOVED AND REPLACED FWD PIT R/H BAFFLE BETWEEN STA 500E AND 500F PN:143A7510-22 PO: 1096771.4 IAW B737-800 SRM 51-40-02 AND SRM 51-40-05.
- [SDR ASAA2024071552006](https://openairdocs.org/sdr/ASAA2024071552006.md): Intercostal · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN INTERCOSTAL UPPER SURFACE HAS CORROSION AT BS307 LBL12 AS MARK. GROUNDED - YES. REMOVED CORROSION IAW B737-800 51-10-02. ORIG THICK 0.125, REMOVED 0.060, REMAINING THICK 0.065 OUT OF LIMITS IAW B737-800 SRM 53-10-51. REMOVED INTERCOSTAL IAW B737-800
- [SDR ASAA2024071551579](https://openairdocs.org/sdr/ASAA2024071551579.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APRROX. STA. 952, RBL 24-48 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES (2EA) AS MARKED. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02 AND BOEING DWG 147A5650 REV A. ORIG THICKNESS IS 0.075" REMOVED 0.
- [SDR ASAA2024071551513](https://openairdocs.org/sdr/ASAA2024071551513.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA FLOOR STRUCTURE BETWEEN GALLEY FITTINGS APPROX. STA. 1014 AND LBL 32,FLOOR PANEL LONGITUDINAL SUPPORT CORRODED AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02,100% MAT LOSS,NO LIMITS NOTED NO ORIG THICKNESS NOTED,FOUND
- [SDR ASAA2024071551193](https://openairdocs.org/sdr/ASAA2024071551193.md): Floorbeam · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBOARD SUPPORT HAS CORROSION AT BS270 BETWEEN RBL0 AND RBL7 AS MARK. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, ORIG THICKNESS FOR TOP SURFACE.100 REMOVED.007 REMAINING MAT.093 FOUND TO BE IN LIMITS IAW B737-800 SRM 53-10-51
- [SDR ASAA2024071551465](https://openairdocs.org/sdr/ASAA2024071551465.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN WET AFT AREA APPROX. STA. 952, LBL 16-24 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW B737-800 B737-800 SRM 53-42-51, NO LIMITS NOTED, ORIG THICKNE
- [SDR ASAA2024071551464](https://openairdocs.org/sdr/ASAA2024071551464.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APPROX. STA. 952,LBL 24-48 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MAT LOSS OUT OF LIMITS IAW B737-800 SRM 53-70-51, NO ORIG THICKNESS NOTED, NO LIMITS
- [SDR ASAA2024071551463](https://openairdocs.org/sdr/ASAA2024071551463.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APPROX. STA. 952,LBL 24 LONGITUDINAL FLOOR SUPPORT CORRODED AROUND (1EA)FASTENER HOLE AS MARKED. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS NO ORIG THICKNESS NOTED, NO LIMITS NOTED. REMOVED AND REPLAC
- [SDR ASAA2024071551462](https://openairdocs.org/sdr/ASAA2024071551462.md): Web · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APPROX. STA. 988, RBL 32 GALLEY FLOOR SUPPORT PLATE TOP SURFACE CORRODED AS MARKED. GROUNDED - YES. BLENDED OUT CORROSION IAW B737-800 SRM 51-10-02. WEB ORIGINAL THICKNESS 0.040 IAW BAC DWG 147A5712 REV B, REMAINING THICKNESS 0.028, REMOVED
- [SDR ASAA2024071551461](https://openairdocs.org/sdr/ASAA2024071551461.md): Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APPROX. STA. 993 AND RBL 34,GALLEY SUPPORT PLATE ATTACH ANGLE HAS DRILLED OUT ELONGATED HOLES(2EA) AS MARKED. GROUNDED - YES. SUPPORT HAS 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-8
- [SDR ASAA2024071551460](https://openairdocs.org/sdr/ASAA2024071551460.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA FLOOR STRUCTURE BETWEEN GALLEY FITTINGS APPROX. STA. 1015 AND RBL 32, FLOOR SUPPORT AFT END CORNER CORRODED AS MARKED. GROUNDED - YES. SUPPORT HAS 100% MATERIAL LOSS AND OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPO
- [SDR ASAA2024071551459](https://openairdocs.org/sdr/ASAA2024071551459.md): Floor Support · corroded · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN AFT WET AREA APPROX. STA. 958,LBL 48 LONGITUDUNAL FLOOR SUPPORT UPPER SURFACE CORRODED AROUND (2EA)FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MAT LOSS OUT OF LIMITS IAW B37-800 SRM 53-70-51. REMOVED AND R
- [SDR ASAA2024071551334](https://openairdocs.org/sdr/ASAA2024071551334.md): Floor Support · cracked · Jul 15, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACK AT BS312 RBL28 AS MARK. GROUNDED - YES. REMOVED AND REPLACED 1 CABIN FLOOR STRUCTURE INTERCOSTAL (P/N- 141A5410U12) P.O. 1096573.1 IAW B737-800- ETOP- SRM-51-40-02 AND BOEING DOCUMENT- 141A5400 REV:-
- [SDR ASAA2024071451400](https://openairdocs.org/sdr/ASAA2024071451400.md): Floorboard · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-136. GROUNDED - YES. EVALUATED AND REPAIRED MAIN CABIN AFT WET FLOORBOARD P/N 147A5810-136 AND REPLACED 55 INSERTS IAW B737-800 SRM 53-00-50-2R-0.
- [SDR ASAA2024071451399](https://openairdocs.org/sdr/ASAA2024071451399.md): Floorboard · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-28. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-28 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.
- [SDR ASAA2024071451398](https://openairdocs.org/sdr/ASAA2024071451398.md): Floorboard · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-27. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-27 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.
- [SDR ASAA2024071451333](https://openairdocs.org/sdr/ASAA2024071451333.md): Floorboard · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-23. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-23 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-7.
- [SDR ASAA2024071451332](https://openairdocs.org/sdr/ASAA2024071451332.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-454. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON MAIN CABIN FWD WET AREA FLOOR PANEL P/N: 141A5810-454 IAW ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-2R-1, ASA B737-800 SRM 53-00-50-2R-
- [SDR ASAA2024071451331](https://openairdocs.org/sdr/ASAA2024071451331.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-755. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON MAIN CABIN FWD WET AREA FLOOR PANEL P/N: 141A5810-755 IAW ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-2R-0. NO FURTHER ACTION REQUIRED.
- [SDR ASAA2024071451330](https://openairdocs.org/sdr/ASAA2024071451330.md): Floorboard · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-137. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-137 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.
- [SDR ASAA2024071451203](https://openairdocs.org/sdr/ASAA2024071451203.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-157. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.
- [SDR ASAA2024071451202](https://openairdocs.org/sdr/ASAA2024071451202.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-155. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.
- [SDR ASAA2024071451201](https://openairdocs.org/sdr/ASAA2024071451201.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-763. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.
- [SDR ASAA2024071451200](https://openairdocs.org/sdr/ASAA2024071451200.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-236. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-236 IAW B737-800 SRM 53-00-50-2R-1.
- [SDR ASAA2024071451199](https://openairdocs.org/sdr/ASAA2024071451199.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-728. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-728 IAW B737-800 SRM 53-00-50-2R-1.
- [SDR ASAA2024071451198](https://openairdocs.org/sdr/ASAA2024071451198.md): Floor Panel · delaminated · Jul 14, 2024 · N597AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-765. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-765 IAW B737-800 SRM 53-00-50-2R-1.
- [SDR ASAA2024071351514](https://openairdocs.org/sdr/ASAA2024071351514.md): Strap · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT LOWER DOOR SILL STRAP HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT LOWER DOOR SILL STRAP IAW B737-800 SRM 53-60-15-1A-1 ORIG THICKNESS IS.100" IAW B737-800 SRM 53-60-15-01-1. REMOVED.016". REMAINING THICKNESS IS.084" AND IS FOUND TO
- [SDR ASAA2024071351466](https://openairdocs.org/sdr/ASAA2024071351466.md): Shield · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Main, Structure
  > AFT PIT FWD SHIELD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FWD SHIELD IAW B737-800 SRM 53-60-15-1A-1 ORIG'L MATERIAL THICKNESS WAS.050 IAW B737-800 SRM 53-60-15-01-1,MAT REMOVED.025 REMAINING IS.025 FOUND TO BE OUT OF LIMITS IAW B737-8
- [SDR ASAA2024071351403](https://openairdocs.org/sdr/ASAA2024071351403.md): Attach Angle · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > AFT PIT,FWD SHIELD ATTACH ANGLE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FWD SHIELD ATTACH ANGLE IAW B737-800 SRM 53-60-15-1A-1 ORIGNL THICKNESS WAS.050 IAW B737-800 SRM 53-60-15-01-1.REMOVED.025 REMAINING THICKNESS IS.025 FOUND TO BE O
- [SDR ASAA2024071351402](https://openairdocs.org/sdr/ASAA2024071351402.md): Support · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Main, Bulkhead
  > FWD PIT,AFT BULKHEAD R/H SUPPORT IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT R/H AFT BULKHEAD SUPPORT IAW B737-800 SRM 53-30-08-1A-1.2.C. AND IS FOUND TO HAVE 100% MATERIAL LOSS IAW B737-800 SRM 53-30-08-1A-1.4.(2). REMOVED AND REPLACED FWD
- [SDR ASAA2024071351337](https://openairdocs.org/sdr/ASAA2024071351337.md): Transition Panel · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT L/H TRANSITION PANEL STA 727 TO 727E+12 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727 TO 727E+12 IAW B737-800 SRM 53-00-53-1A-2, ORIGNL MATERIAL WAS.040 IAW B757-800 SRM 53-60-53-01-2 100% MATERIAL LOST
- [SDR ASAA2024071351336](https://openairdocs.org/sdr/ASAA2024071351336.md): Transition Panel · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT L/H TRANSITION PANEL STA 727E+12 TO 738 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727E+12 TO 738 IAW B737-800 SRM 53-00-53-1A-2, ORIGN'L MATERIAL WAS.040 IAW B737-800 SRM 53-60-53-01-2 REMOVED.020. REMA
- [SDR ASAA2024071351335](https://openairdocs.org/sdr/ASAA2024071351335.md): Shield · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT, AFT SHIELD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT, AFT SHIELD IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS IS.050" IAW B737-800 SRM 53-60-15-01-1. REMOVED.025" REMAINING THICKNESS IS.025" AND IS FOUND TO BE OUT OF LIMITS I
- [SDR ASAA2024071351288](https://openairdocs.org/sdr/ASAA2024071351288.md): Support · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT, AFT BULKHEAD LOWER SUPPORT IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT, AFT BULKHEAD LOWER SUPPORT IAW B737-800 SRM 53-30-08-1A-1.2.C AND IS FOUND TO HAVE 100% MATERIAL LOSS IAW B737-800 SRM 53-30-08-1A-1.4.(2). REMOVED AND REPLACE
- [SDR ASAA2024071351287](https://openairdocs.org/sdr/ASAA2024071351287.md): Transition Panel · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT R/H TRANSITION PANEL STA 727 TO 727F+11 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727 TO 727F+11 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS.040" IAW B737-800 SRM 53-60-53-01-2. REMOVED.020" REMA
- [SDR ASAA2024071351286](https://openairdocs.org/sdr/ASAA2024071351286.md): Transition Panel · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT R/H TRANSISTION PANEL STA 727F+11 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727F+11 TO 767 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS.040" IAW B737-800 SRM 53-60-53-01-2. REMOVED.020" REM
- [SDR ASAA2024071351285](https://openairdocs.org/sdr/ASAA2024071351285.md): Transition Panel · corroded · Jul 13, 2024 · N597AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT R/H TRANSITION PANEL STA 500C+15 TO 500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500C+15 -500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS.040" IAW B737- 800 SRM 53-30-53-1A-2. TABLE 2.
- [SDR ASAA2024071051401](https://openairdocs.org/sdr/ASAA2024071051401.md): Stop Fitting · worn · Jul 10, 2024 · N597AS · Boeing 737890 · Passenger/Crew Doors
  > MAIN CABIN L1 DOOR, AFT LOWER STOP PIN FITTINGS IS WORN ON SIDE. GROUNDED - YES. CHECKED LIMITS ON WORN AREA ON STOP FITTING, OUT OF LIMITS IAW B737-800 SRM 52-10-90-1A-4. MAT. REMOVAL LIMITS.030 IN ZONE 2 LUG SURFACE.035 REMOVED USED TOOL E1555B DUE 25JAN25
- [SDR ASAA2024071051431](https://openairdocs.org/sdr/ASAA2024071051431.md): Stop Fitting · worn · Jul 10, 2024 · N597AS · Boeing 737890 · Passenger/Crew Doors
  > MAIN CABIN L1 DOOR, AFT LOWER STOP PIN FITTINGS IS WORN ON SIDE. GROUNDED - YES. CHECKED LIMITS ON WORN AREA ON STOP FITTING, OUT OF LIMITS IAW B737-800 SRM 52-10-90-1A-4. MAT. REMOVAL LIMITS.030 IN ZONE 2 LUG SURFACE.035 REMOVED USED TOOL E1555B DUE 25JAN25
- [SDR ASAA2024033048744](https://openairdocs.org/sdr/ASAA2024033048744.md): Lens · missing · Mar 30, 2024 · N597AS · Boeing 737890 · Emergency Lighting
  > FA REPORTS PLASTIC LIGHT COVER FOR EXIT ROW LIGHTING MISSING AT SEAT 16F. GROUNDED - YES. REPLACED L/H ROW 16F LOWER LIGHT COVER (EMERG). OPS GOOD.
- [SDR ASAA2023100645510](https://openairdocs.org/sdr/ASAA2023100645510.md): Unknown · unknown · Oct 6, 2023 · N597AS · Boeing 737890 · Flight Management Computing Hardware System
  > SINGLE FMC OPERATION MESSAGE ON CDU DURING TAXI IN. GROUNDED - YES. PERFORMED SYSTEM TEST OF FMC, NO FAULTS NOTED.
- [SDR ASAA2023092245472](https://openairdocs.org/sdr/ASAA2023092245472.md): Valve · malfunctioned · Sep 22, 2023 · N597AS · Boeing 737890 · Engine Bleed Air System
  > CFM DIAGNOSTICS REPORTS #2 ENGINE HAS INCREASE IN DELTA EGT, FUEL FLOW AND DECREASE IN CORE SPEED. HPTACC MALFUNCTION IS SUSPECTED. (#PRI2/ETOPS) CNR 20230922006. GROUNDED - YES. (RESOLVED ON W/O: 1970765 TASKCARD: N/R-00001) ACCOMPLISHED REMOVALOF HPTACC REF

Next page: https://openairdocs.org/aircraft/N597AS/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 = 'N597AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N597AS/reports

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