# Service difficulty reports: N506AS

A list on [N506AS](https://openairdocs.org/aircraft/N506AS.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 10 · 490 reports

- [SDR ASAA2026062867053](https://openairdocs.org/sdr/ASAA2026062867053.md): Battery Pack · inoperative · Jun 28, 2026 · N506AS · Boeing 737890 · Emergency Lighting
  > REF TASK CARD 78233001 FOUND LH AFT EMERGENCY LIGHTS DID NOT PASS TEST. GROUNDED - YES. REMOVED AND REPLACED AFT LT EMERGENCY BATTERY M1672 REF AMM 33-51-06, NEW BATTERY PASSED TEST.
- [SDR ASAA2026051666171](https://openairdocs.org/sdr/ASAA2026051666171.md): Gcu · faulted · May 16, 2026 · N506AS · Boeing 737890 · AC Generator-Alternator
  > GEN CONTROL UNIT A/C LEFT IN E+E BAY HAS BTB FAULT LIGHT ILLUMINATED. GROUNDED - YES. RESET GCU REF AMM 24-21-81-400-801 NO FAULTS NOTED.
- [SDR ASAA2026051166100](https://openairdocs.org/sdr/ASAA2026051166100.md): Skin · cracked · May 11, 2026 · N506AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > FOUND 1 EA CRACK INDICATION LOWER SKIN L/H STAB 138.70 AND S147.90 16 INCH LENGTH APROX AS MARK. GROUNDED - YES. REPAIRED THE L/H HORIZ. STAB LOWER SKIN STA 138.70 AND 147.90 USING MAT.071 2024-T3 AND.100 2024-T3 PER B737-80 SRM 55-10-01-2R-11. REPAIR IS A C
- [SDR ASAA2026020164080](https://openairdocs.org/sdr/ASAA2026020164080.md): Battery Pack · failed · Feb 1, 2026 · N506AS · Boeing 737890 · Emergency Lighting
  > LEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES, LT & RT ROW 23 & LT SEAT ROW 7. PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.
- [SDR ASAA2026020164079](https://openairdocs.org/sdr/ASAA2026020164079.md): Battery Pack · failed · Feb 1, 2026 · N506AS · Boeing 737890 · Emergency Lighting
  > LEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES LT & RT ROW 23 & LT SEAT ROW 7 & PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.
- [SDR ASAA2026020164078](https://openairdocs.org/sdr/ASAA2026020164078.md): Battery Pack · failed · Feb 1, 2026 · N506AS · Boeing 737890 · Emergency Lighting
  > LEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES LT & RT ROW 23 AND LT SEAT ROW 7 & PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.
- [SDR ASAA2024090452430](https://openairdocs.org/sdr/ASAA2024090452430.md): Skin · corroded · Sep 4, 2024 · N506AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > REF DEFECT # 300011333 N/R-00004 LAV WASTE VENT SKIN IS OUT OF LIMITS AND REQUIRES REPAIR. GROUNDED - YES. REPAIRED LAV WASTE VENT SKIN IAW 737-800 SRM 53-70-01-2R-3W=.5" O=.125" R=.096" L= 1" D=.029".
- [SDR ASAA2024062750724](https://openairdocs.org/sdr/ASAA2024062750724.md): Power Supply · inoperative · Jun 27, 2024 · N506AS · Boeing 737890 · Emergency Lighting
  > LIGHTS ASSOCIATED WITH M1674 POWER SUPPLY ARE INOP. GROUNDED - YES. REMOVED AND REPLACED M1674 POWER SUPPLY IAW B737-800 AMM 33-51-06-960-806 TEST GOOD.
- [SDR ASAA2024060350503](https://openairdocs.org/sdr/ASAA2024060350503.md): Floor Support · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN SUPPORT P/N 147A5676-16 STA 927 - STA 947 LBL16 CORRODED. GROUNDED - YES. BLENDED CORROSION SUPPORT HAS 100% MAT LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC D
- [SDR ASAA2024060350502](https://openairdocs.org/sdr/ASAA2024060350502.md): Floorbeam · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor Beam
  > MAIN CABIN SUPPORT P/N 147A5676-5 STA 947 LBL 25 - LBL 50 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1 100% MATERIAL LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05
- [SDR ASAA2024060350501](https://openairdocs.org/sdr/ASAA2024060350501.md): Floor Support · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN INTERCOSTAL P/N 147A5676-13 STA 947.5 TO 967 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1, 100% MAT LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05 AN BA
- [SDR ASAA2024060350431](https://openairdocs.org/sdr/ASAA2024060350431.md): Floorbeam · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor Beam
  > MAIN CABIN STA 990 RBL 32-43 CORRODED SUPPORT. GROUNDED - YES. CORROSION AT FASTENER HOLES 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INSTALLED ON N/
- [SDR ASAA2024060350430](https://openairdocs.org/sdr/ASAA2024060350430.md): Sidewall Support · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN WALL SUPPORT STA 990 - 1016 LBL 32 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENER HOLES, 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.
- [SDR ASAA2024060350429](https://openairdocs.org/sdr/ASAA2024060350429.md): Support · corroded · Jun 3, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN SUPPORT STA 990 - 1016 RBL 32 CORRODED. GROUNDED - YES. BLENDED OUT CORROSION. SUPPORT HAS 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INST
- [SDR ASAA2024060250427](https://openairdocs.org/sdr/ASAA2024060250427.md): Floorbeam · corroded · Jun 2, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FLOOR STRUCTURE AT STA 951 R/H HAS CORROSION AT FASTENER HOLES UNDERSIDE. GROUNDED - YES. REMOVED AND REPLACED SUPPORT FRAME IAW B737-800 SRM 51-40-02 AND IAW REF'S AIPC 53-42-51.
- [SDR ASAA2024053150499](https://openairdocs.org/sdr/ASAA2024053150499.md): Rib · cracked · May 31, 2024 · N506AS · Boeing 737890 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORZ. STAB INTERNAL APPROX. SS 120 BETWEEN FRONT SPAR AND REAR RIB CRACKED. GROUNDED - YES. REPAIRED THE RIGHT HORIZ. STAB RIB AT APPROX SS 120 USING MAT BAC1505-100962 T-SECTION, BAC1490-2793 ANGLE, 0.12 7075-T6 SHIMS PER B737-800 SRM 55-10-09-2R-4.
- [SDR ASAA2024052950500](https://openairdocs.org/sdr/ASAA2024052950500.md): Floor Support · corroded · May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT INTERCOSTAL AT STA 947 CORRODED. GROUNDED - YES. BLENDED CORROSION INTERCOSTAL HAS 100% MATERIAL LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 STM 53-70-51-1A-1 AT STA 242.5 LBL 24.5, DRILLED FIT NEW INTERCOSTAL IAW B737-800 S
- [SDR ASAA2024052950418](https://openairdocs.org/sdr/ASAA2024052950418.md): Angle · cracked · May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT, L/H BAFFLE CLIP AT STA 500H FWD SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT L/H BAFFLE CLIP AT STA 500H PN:143A7502-155 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.
- [SDR ASAA2024052950230](https://openairdocs.org/sdr/ASAA2024052950230.md): Baffle · cracked · May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT, L/H BAFFLE CLIP AT STA 500G AFT SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT, L/H BAFFLE CLIP AT AT STA 500G WITH PN: 143A 7502-159 PO: 1092414.1 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.
- [SDR ASAA2024052950090](https://openairdocs.org/sdr/ASAA2024052950090.md): Transition Panel · corroded · May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD PIT R/H TRANSITION PANEL STA 500E+10 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS.040" IAW B737-800 SRM 53-30-53-01-2 TABLE
- [SDR ASAA2024052950089](https://openairdocs.org/sdr/ASAA2024052950089.md): Transition Panel · corroded · May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO LT TRANSITION PANEL STA 500G+2 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500G+2 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS.040 IAW B737-800 SRM 53-30-53-01-2 TABLE 2. REMO
- [SDR ASAA2024052850723](https://openairdocs.org/sdr/ASAA2024052850723.md): Bracket · worn · May 28, 2024 · N506AS · Boeing 737890 · Electrical/Electronic Compartment Doors
  > E/E COMPT. AFT DOOR PIN RECEPTICLE BRACKET IS WORN. GROUNDED - YES. REMOVED AND REPLACED RECEPTICLE BRACKET IAW B737-800 SRM 51-40-02 AND BOEING DWG # 141A3501 REV: - ADJUSTMENT CHECK GOOD.
- [SDR ASAA2024052850504](https://openairdocs.org/sdr/ASAA2024052850504.md): Floorbeam · corroded · May 28, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor Beam
  > AFT WET AREA STA 947 T-CAP HAS CORROSION AT MOUNT FITTING. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICK 0.1800 IAW B737-800 SRM 53-70-51-1A-1 AND FLOOR BEAM BAC 1518-1212 REMAINING THICK 0.154 AT RBL 53, 0.026" REMOVE MAT, REMAINING THICK 0.158 AT LBL 4,
- [SDR ASAA2024052850428](https://openairdocs.org/sdr/ASAA2024052850428.md): Floorbeam · corroded · May 28, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor Beam
  > AFT WET STA 986 HAS CORRODED FASTENER HOLES FLOOR BEAM. GROUNDED - YES. REMOVED CORROSION. ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1 AND BAC 1518-1211. REMAINING THICKNESS AT RBL 34- 0.100, REMOVED 0.050. REMAINING THICK AT LBL43 0.095, REMOVED 0
- [SDR ASAA2024052850426](https://openairdocs.org/sdr/ASAA2024052850426.md): Floor Support · corroded · May 28, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD WET AREA STA 328 - 344 LBL11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 328-344, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-0I-2. TABLE 3. ITEM 8 PER. B737-800 SRM 53-10-51-1A-A. PAR 4.F,(2) O
- [SDR ASAA2024052850425](https://openairdocs.org/sdr/ASAA2024052850425.md): Floor Support · corroded · May 28, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD WET AREA STA 312 - 328 LBL 11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 312-328, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-OI-2, TABLE 3 ITEM (8)PER B737-800 SRM 53-10-51-1A-1, PAR. 4.F (2)
- [SDR ASAA2024052550417](https://openairdocs.org/sdr/ASAA2024052550417.md): Skin · dented · May 25, 2024 · N506AS · Boeing 737890 · Service Doors
  > R2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN, REFERENCE BAC DWG#147A6502 REV B, UPON FURTHER INSPECTION FOUND DENT & FOUND HANDLE PAN TO BE OUT OF LIMITS, REFERENCE B737-800 SRM 52-10-02-1A-4
- [SDR ASAA2024052550416](https://openairdocs.org/sdr/ASAA2024052550416.md): Skin · dented · May 25, 2024 · N506AS · Boeing 737890 · Service Doors
  > R1 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED DAMAGED PAN ASSY & INSTALLED NEW 141A6554Y1 PAN ASSY IAW B737-800 SRM 51-40-2 & BAC DWG 141A6516 REV.A UPON FURTHER INSPECTION FOUND DENT AND HANDLE PAN TO BE OUT OF LIMITS IAW B737-800 SRM
- [SDR ASAA2024052550232](https://openairdocs.org/sdr/ASAA2024052550232.md): Pan · dented · May 25, 2024 · N506AS · Boeing 737890 · Passenger/Crew Doors
  > L2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN REFERANCE BACDWG #147A6116 REV-, UPON FURTHER INSPECTION FOUND DENT & FOUND TO BE OUT OF LIMITS, REFERENCE B737-80 SRM 52-10-02-1A-3.
- [SDR ASAA2024052450721](https://openairdocs.org/sdr/ASAA2024052450721.md): Floor Support · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 794-807 RBL 13.84. GROUNDED - YES. REMOVED THE CORROSION FROM THE AFT PIT FLOOR SUPPORT AT STA 794-807, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.2.0 ORIG THICKNESS IS.070" IAW B737-800 SRM 53-60-53-01-2 TABLE 2.
- [SDR ASAA2024052450424](https://openairdocs.org/sdr/ASAA2024052450424.md): Shield · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT, DOOR SURROUND FWD SHIELD IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT DOOR SURROUND FWD SHIELD IAW B737-800 SRM 53-60-15-1A-1, ORIGIN'L MATERIAL WAS.050 IAW B737-800 SRM 53-60-15-01-1 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW B737
- [SDR ASAA2024052450423](https://openairdocs.org/sdr/ASAA2024052450423.md): Floor Support · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 727 AND 727B RBL 13.84. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FLOOR SUPPORT BETWEEN STA 727 TO 727B RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2 ORIG. THICKNESS IS.070" IAW B737-800 SRM 53-60-53-01-2 TABLE
- [SDR ASAA2024052450422](https://openairdocs.org/sdr/ASAA2024052450422.md): Transition Panel · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT R/H TRANSITION PANEL HAS CORROSION BETWEEN STA 727 AND 727F+11. 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 53-60-53-10-2 TABLE 2. RE
- [SDR ASAA2024052450421](https://openairdocs.org/sdr/ASAA2024052450421.md): Transition Panel · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT L/H TRANSITION PANEL CORROSION BETWEEN STA 727 AND 727F+11 GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727 TO 727 F+11 IAW B737-800 SRM 53-00-53-1A-2-0, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-0
- [SDR ASAA2024052450420](https://openairdocs.org/sdr/ASAA2024052450420.md): Web · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT DOOR THRESHOLD WEB IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT THRESHOLD WEB IAW ASA B737-800 SRM 53-60-15-1A-1 ORIGINAL MATL THKS.050 PER ASA B737-800 SRM 53-60-15-OI-1 TABLE ITEM 2 REMOVED.009 MATL.041 REMAINING MATL FOUND TO BE OUT O
- [SDR ASAA2024052450231](https://openairdocs.org/sdr/ASAA2024052450231.md): Strap · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT, DOOR SURROUND LOWER MAIN SILL STRAP IS CORRODED BETWEEN STA 767 AND 787. GROUNDED - YES. REMOVED DAMAGE FROM LOWER MAIN SILL STRAP IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS.080 PER B737-800 SRM 53-60-15-0I-1.REMOVED.037. REMAINING THICKNESS IS
- [SDR ASAA2024052450225](https://openairdocs.org/sdr/ASAA2024052450225.md): Attach Angle · corroded · May 24, 2024 · N506AS · Boeing 737890 · Fuselage Main, Structure
  > AFT PIT, DOOR SURROUND FWD SHIELD ATTACH ANGLE IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT FWD SHIELD ATTACH ANGLE IAW B737-800 SRM 53-60-15-1A-1. ORIGN'L MATERIAL WAS.050 IAW B737-800 SRM 53-60-15-01-1. REMOVED.020, REMAINING IS.030. FOUND TO
- [SDR ASAA2024052350419](https://openairdocs.org/sdr/ASAA2024052350419.md): Floor Support · cracked · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > MAIN CABIN UNDER FLOOR STA 540 PANEL SUPPORT CRACKED AT RBL 0 - RBL 10. GROUNDED - YES. REMOVED PANEL SUPPORT IAW B737-800 SRM 51-40-02. NEW PLATE PART. DRILLED TO FIT IAW B737-800 SRM 51-40-05. INSTALLED PANEL SUPPORT IAW B737-800 SRM 51-40-02 REF AIPC. 53-
- [SDR ASAA2024052350415](https://openairdocs.org/sdr/ASAA2024052350415.md): Floor Panel · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-136. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-136 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052350410](https://openairdocs.org/sdr/ASAA2024052350410.md): Floor Panel · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-28. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-28 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052350409](https://openairdocs.org/sdr/ASAA2024052350409.md): Floor Panel · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-27. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-27 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052350395](https://openairdocs.org/sdr/ASAA2024052350395.md): Floor Panel · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-23. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-23 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052350394](https://openairdocs.org/sdr/ASAA2024052350394.md): Floor Panel · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-137. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOORBOARD DELAMINATION PN 147A5810-137 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052350086](https://openairdocs.org/sdr/ASAA2024052350086.md): Floorboard · delaminated · May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-90. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-0, 53-00-50-2R-1.
- [SDR ASAA2024052150393](https://openairdocs.org/sdr/ASAA2024052150393.md): Floor Panel · delaminated · May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > FLOOR PANEL DELAME FWD WET AREA P/N 141A5810-763. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF FLOOR PANEL DELAMINATION ON FWD WET AREA PANEL PN 141A5810-763 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.
- [SDR ASAA2024052150085](https://openairdocs.org/sdr/ASAA2024052150085.md): Floor Panel · delaminated · May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL DELAME P/N 141A5810-236. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-236 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.
- [SDR ASAA2024052150080](https://openairdocs.org/sdr/ASAA2024052150080.md): Floor Panel · delaminated · May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor Panel
  > FLOOR PANEL DELAME FWD WET AREA P/N 141A5810-728. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-728 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.
- [SDR ASAA2024042249193](https://openairdocs.org/sdr/ASAA2024042249193.md): Lens · broken · Apr 22, 2024 · N506AS · Boeing 737890 · Emergency Lighting
  > F.A. REPORTS: L-1 FLOOR LEVEL EMERGENCY LIGHT COVER FELL OFF. GLASS BROKEN. GROUNDED - YES. REMOVED & REPLACED LOWER THRESHOLD LIGHT ASSEMBLY COVER IAW AMM 33-14-00.
- [SDR ASAA2024041549080](https://openairdocs.org/sdr/ASAA2024041549080.md): Lamp · inoperative · Apr 15, 2024 · N506AS · Boeing 737890 · Emergency Lighting
  > ROW 17 EXIT LIGHTING DIM. GROUNDED - YES. RE-LAMPED ROW 17 EXIT LIGHT, OPS GOOD.
- [SDR ASAA2024033048710](https://openairdocs.org/sdr/ASAA2024033048710.md): Door · noisy · Mar 30, 2024 · N506AS · Boeing 737890 · Passenger/Crew Doors
  > FA REPORTS L1 DOOR MAKES UNUSUAL NOISE AND HAS GREATER THAN NORMAL RESISTANCE DURING OPENING AND CLOSING. GROUNDED - YES. LUBRICATED L1 DOOR UPPER AND LOWER HINGES, GUST LOCK, AND OPS CK NORMAL. DOOR OPENS AND CLOSES NORMALLY.

Next page: https://openairdocs.org/aircraft/N506AS/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 = 'N506AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N506AS/reports

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