# Service difficulty reports: N611AS

A list on [N611AS](https://openairdocs.org/aircraft/N611AS.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 5 · 225 reports

- [SDR ASAA2026020564678](https://openairdocs.org/sdr/ASAA2026020564678.md): Stringer · corroded · Feb 5, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L, BS 540 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1. W=.650 O=.045 R=.005 L= 2.25 D=.040.
- [SDR ASAA2026020564676](https://openairdocs.org/sdr/ASAA2026020564676.md): Stringer · corroded · Feb 5, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/Stringer
  > STRINGER 26 LEFT F.S. 540 CORRDED. GROUNDED - YES. REPAIRED IAW BOEING 737-700 SRM 53-00-03-2R-1 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW BOEING 737-700 SRM 53-00-03-1A-1. W= 1" O=.045 R=.002 L= 2" D=.043.
- [SDR ASAA2026020464679](https://openairdocs.org/sdr/ASAA2026020464679.md): Stringer · corroded · Feb 4, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY, STRINGER 27L HAD CORROSION AT BS 540. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED STRINGER IAW SRM 53-00-03-2R-1W =.650 O=.045 R=.002 L= 2.25 D=.043.
- [SDR ASAA2026020464677](https://openairdocs.org/sdr/ASAA2026020464677.md): Stringer · corroded · Feb 4, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY STRINGER 27R CORRODED AT BS 540. GROUNDED - YES. REMOVED CORROSIONN, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED STRINGER IAW SRM 53-00-03-2R-1 W=.650 O=.045 R=.002 L= 1.25 D=.043.
- [SDR ASAA2026012964576](https://openairdocs.org/sdr/ASAA2026012964576.md): Frame Splice · corroded · Jan 29, 2026 · N611AS · Boeing 737790 · Fuselage Main, Frame
  > AFT CARGO BS 727D FRAME SPLICE CORRODED AT RBL-21. GROUNDED - YES. REMOVED & REPLACED NEW SPLICE PN 146A1300U8 ON AFT CARGO BS 727D, RBL 21 IAW SRM 51-40-02-0G-0. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1. W 1, O.07, R.054, L 1, D.
- [SDR ASAA2026011664292](https://openairdocs.org/sdr/ASAA2026011664292.md): Web · corroded · Jan 16, 2026 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT CARGO SCUFF PLATE SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SILL WEB IAW B737-700 SRM 51-40-02-0G-0, REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-60-15-1A-1 W= 1" O= 0.045" R= 0.036" L= 1" D= 0.009".
- [SDR ASAA2026011664173](https://openairdocs.org/sdr/ASAA2026011664173.md): Transition Panel · corroded · Jan 16, 2026 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT CARGO LT TRANSITION PANEL BS 727D+4 - 847 CORRODED. GROUNDED - YES. REMOVED AND REPAIRED THE LT TRANSITION PANEL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2026011664159](https://openairdocs.org/sdr/ASAA2026011664159.md): Transition Panel · corroded · Jan 16, 2026 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION AT STA 727+4 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED AND REPAIRED AFT CARGO R/H TRANSITION AT STA 727+4 TO 767, IAW B737-700 SRM 51-40-02-06-0. W= 1.25 O=.040 R=.030 L= 3.75 D=.010.
- [SDR ASAA2026011664158](https://openairdocs.org/sdr/ASAA2026011664158.md): Transition Panel · corroded · Jan 16, 2026 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT CARGO LT TRANSITION AT BS 727+4 TO 727D+2 HAS CORROSION. GROUNDED - YES. REMOVED AND REPAIRED AFT CARGO L/H TRANSITION AT STA 727+4 TO 727D+2 IAW B737-700 SRM 51-40-02-0G-0. W= 2" O= 0.040" R= 0.031" D= 0.009" L= 2".
- [SDR ASAA2026011664081](https://openairdocs.org/sdr/ASAA2026011664081.md): Support · corroded · Jan 16, 2026 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT BULKHEAD LOWER SUPPORT AT BS 500D WAS CORRODED. GROUNDED - YES. UPON FURTHER EVALUATION FOUND TO HAVE 100% MATERIAL LOSS. R & R THE SUPPORT IAW SRM 51-40-02-OG-OW: 1.25 O:.073 R: 0.00 L: 2.75 D:.073.
- [SDR ASAA2026011564730](https://openairdocs.org/sdr/ASAA2026011564730.md): Skin · corroded · Jan 15, 2026 · N611AS · Boeing 737790 · Fuselage Main, Plate/Skin
  > STA 520 TO STA 540 STR-27L TO STR-27R SKIN CORRODED. GROUNDED - YES. REMOVED CORROSION FOUN DTO HAVE 100% MATERIAL LOSS OUT OF LIMITS IAW B737-700 SRM 53-00-01-1A-5 REAPIRED IAW ASA EA# 700-53EA-29869. W= 6.50 O=.080 R= 0.00 L= 7.50 D=.080
- [SDR ASAA2025101761681](https://openairdocs.org/sdr/ASAA2025101761681.md): Lens · detached · Oct 17, 2025 · N611AS · Boeing 737790 · Emergency Lighting
  > FA REPORTS AFT GALLEY L2 DOOR EXIT SIGN FELL OFF. GROUNDED - YES. REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT SIGN LENS COVER AS REQUIRED. TAPE REMOVED. THIS CLEARS THIS PLT.
- [SDR ASAA2025091060806](https://openairdocs.org/sdr/ASAA2025091060806.md): Light · broken · Sep 10, 2025 · N611AS · Boeing 737790 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT HAS STRING STICKING OUT. GROUNDED - YES. REPAIRED BROKEN OVERWING ESCAPE HATCH LIGHT WIRING REF WDM 33-51-13-1. SECURED WIRE BUNDLE IN CLAMP. OPS NORMAL.
- [SDR ASAA2025080660901](https://openairdocs.org/sdr/ASAA2025080660901.md): Web · corroded · Aug 6, 2025 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT PASSENGER COMPARTMENT, BETWEEN STA 664 AND STA 685, AT STR17L, PANEL/RIVETS CORRODED. GROUNDED - YES. REMOVED AND REPLACED WEB BETWEEN STA 664 AND STA 685, AT STRINGER 17L IAW B737-700 SRM 51-40-02-0G-0W=1.2" O=.040 R=.020 L=1.6" D=.020.
- [SDR ASAA2025080560260](https://openairdocs.org/sdr/ASAA2025080560260.md): Skin · cracked · Aug 5, 2025 · N611AS · Boeing 737790 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED ON THE I/B SIDE OF RIB STA 129.5, APPROX 17" FROM FORWARD SPAR. GROUNDED - YES. REPAIRED RIGHT HAND HORIZONTAL STAB LOWER SKIN INBD OF HSS 129.5 IAW SRM 55-10-01-2R-11.
- [SDR ASAA2025060458483](https://openairdocs.org/sdr/ASAA2025060458483.md): Door · out of rig · Jun 4, 2025 · N611AS · Boeing 737790 · Passenger/Crew Doors
  > L1 DOOR EXTREMELY DIFFICULT TO OPEN FROM OUTSIDE. GROUNDED - YES. AFT MID STOP PIN (FIFTH FROM TOP) FOUND WITH MISSING LOCK SPRING. SCREWED IN FOR T/S, DOOR NEARLY IMPOSSIBLE TO CLOSE FROM OUTSIDE. DOOR HANDLE TORQUE TEST FAILED CLOSING TORQUE REF AMM 52-11-00
- [SDR ASAA2025050157702](https://openairdocs.org/sdr/ASAA2025050157702.md): Cover · loose · May 1, 2025 · N611AS · Boeing 737790 · Passenger/Crew Doors
  > FA REPORTS L1 DIFFICULT TO ROTATE OPEN AND CLOSE. GROUNDED - YES. FOUND L1 DOOR UPPER HINGE COVER CLIP LOOSE AND CAUSING BINDING. REMOVED UPPER HINGE COVER AND TIGHTENED CLIP. REINSTALLED HINGE COVER AND PERFORMED UPPER HINGE COVER ADJUSTMENT AMM REF 52-11-00-
- [SDR ASAA2025012555505](https://openairdocs.org/sdr/ASAA2025012555505.md): Light · malfunctioned · Jan 25, 2025 · N611AS · Boeing 737790 · Emergency Lighting
  > FWD MOST LED LIGHT FIXTURE IN CEILING CYCLES OFF AND ON UNCOMMANDED. GROUNDED - YES. RELAMPED FORWARD EMERGENCY AREA LIGHT REF AMM 33-51-03. OP CHECKS GOOD.
- [SDR ASAA2024062550528](https://openairdocs.org/sdr/ASAA2024062550528.md): Packing · leaking · Jun 25, 2024 · N611AS · Boeing 737790 · Hydraulic System, Main
  > TOTAL LOSS OFF SYSTEM B HYDRAULIC PRESSURE AND QUANTITY. USED ALTERNATE FLAP EXTENSION. STBY RUDDER SYSTEM B. GROUNDED - YES. CW HYD FLUID LOSS INFLIGHT CONDITIONAL INSP IAW AMM 05-51-88. NO OBVIOUS LEAK NOTED. FILLED SYS B RESERVOIR TO 38% WITH FLAPS AT 1 NO
- [SDR ASAA2023090645088](https://openairdocs.org/sdr/ASAA2023090645088.md): Rib · cracked · Sep 6, 2023 · N611AS · Boeing 737790 · Empennage Structure
  > UPON INSTALL OF SKIN REPAIR STAB RIB WAS FOUND CRACKED AT AFT MOST HOLE IN RADIUS AT R/H STAB STA 92. GROUNDED - YES. REMOVED AND REPLACED RIB AT STA 92 IAW B737-700 SRM 51-40-02-0G-0.
- [SDR ASAA2023090145141](https://openairdocs.org/sdr/ASAA2023090145141.md): Rib · loose · Sep 1, 2023 · N611AS · Boeing 737790 · Wing, Rib/Bulkhead
  > FIXED TRAILING EDGE DIRECTLY OVER PANEL 551GB IS LOOSE AND ATTACHING FASTENERS ARE SPINNING IN THE SERATED PLATE. GROUNDED - YES. REPAIRED DEFLECTION CONTROL RIB IAW B737-700 SRM 57-51-02-2R-1 AND B737-700 SRM 57-51-02-2R-4.
- [SDR ASAA2023082445099](https://openairdocs.org/sdr/ASAA2023082445099.md): Beam · cracked · Aug 24, 2023 · N611AS · Boeing 737790 · Service Doors
  > R1 DOOR BEAM 141A6535-4 IS CRACKED NEXT TO SHIM FOR HANDLE BOX (LOWER FORWARD HANDLE BOX ATTACH POINT) MARKED WITH DOT. GROUNDED - YES. REMOVED AND REPLACED BEAM IN THE R1 DOOR IAW B737-700 SRM 51-40-02-0G-0.
- [SDR ASAA2023082445093](https://openairdocs.org/sdr/ASAA2023082445093.md): Channel · corroded · Aug 24, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > L1 DOOR SILL HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE IN LIMITS IAW B737-700 SRM 53-10-15-1A-1.W= 1INCH O=.090 R=.087 L= 2INCH D=.003.
- [SDR ASAA2023082445092](https://openairdocs.org/sdr/ASAA2023082445092.md): Intercostal · corroded · Aug 24, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > RH STA 1040 RBL 3, COMMON TO THE PRESSURE SOME FLOOR STRUCTURE AS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FLOOR STRUCTURE FOUND IN LIMITS IAW B737-700 SRM 53-70-51-1A-1W= 1INCH O=.050 R=.048 L= 1INCH D=.002.
- [SDR ASAA2023082445091](https://openairdocs.org/sdr/ASAA2023082445091.md): Support · corroded · Aug 24, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT PIT TRANSITION L/H SIDE FROM 727-847 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2, FABRICATED NEW L/H TRANSITION FROM STA 727-847 IAW B737-700 SRM 51-40-05-0G-0.W= 1INCH ORG-.040 R= 0 L= 1INCH D=.040.
- [SDR ASAA2023082445090](https://openairdocs.org/sdr/ASAA2023082445090.md): Transition Panel · corroded · Aug 24, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT PIT TRANSITION R/H SIDE 727-767 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 FABRICATED NEW R/H TRANSITION FROM STA 727-767 IAW B737-700 SRM 51-40-05-0G-0.W= 1 INCH O=.040 R= 0 L= 1INCH D=.040.
- [SDR ASAA2023082445086](https://openairdocs.org/sdr/ASAA2023082445086.md): Intercostal · corroded · Aug 24, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > LH STA 1040 LBL 3 COMMON TO THE PRESSURE DOME FLOOR STRUCTURE HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FLOOR STRUCTURE IAW B737-700 SRM 53-70-51-1A-1 FOUND IN LIMITS W 2INCH O.050 R.049 L 1 INCH D.001.
- [SDR ASAA2023082245100](https://openairdocs.org/sdr/ASAA2023082245100.md): Web · corroded · Aug 22, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > WEB LOCATED IN AFT CARGO COPARTMETN SURROUND BETWEEN FRAME 787-794.37 AT STRINGER 25R IS CORRODED MARKED WITH DOT. GROUNDED - YES. REMOVED AND REPLACED WEB LOCATED IN AFT CARGO COMPARTMETN SURROUND BETWEEN FRAME 787-794.37 AT STRINGER 25R IAW B737-700 SRM 51-4
- [SDR ASAA2023082245089](https://openairdocs.org/sdr/ASAA2023082245089.md): Intercostal · corroded · Aug 22, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > LH STA 1040 LBL 20, COMMON TO THE PRESSURE DOME FLOOR STRUCTURE HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FLOOR STRUCTURE IAW B737-700 SRM 53-70-51-1A-1 FOUND IN LIMITS W= 1INCH O=.063 R=.060 L=.060 D=.003.
- [SDR ASAA2023082245087](https://openairdocs.org/sdr/ASAA2023082245087.md): Intercostal · corroded · Aug 22, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > RH STA 1040 RBL 20 COMMON TO THE PRESSURE DOME FLOOR STRUCTURE HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FORM FLOOR STRUCTURE IAW B737-700 SRM 53-70-51-1A-1 FOUND TO BE IN LIMITS W2" O.063" R=.061" L=1INCH D.002".
- [SDR ASAA2023082245085](https://openairdocs.org/sdr/ASAA2023082245085.md): Beam · corroded · Aug 22, 2023 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > RH LAV MOUNT STA 951 HAS CORROSION ON BEAM. GROUNDED - YES. REMOVED AND REPLACED BEAM CAP IAW B737-700 SRM 53-70-51-2R-5 W -1" O-.180" R-.130" L-1" D-050".
- [SDR ASAA2023082045094](https://openairdocs.org/sdr/ASAA2023082045094.md): Channel · corroded · Aug 20, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > R1 DOOR SILL HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE IN LIMITS IAW B737-700 SRM 53-10-15-1A-2.W= 2 INCH O=.3080 R=.074 L= 1INCH D=.006.
- [SDR ASAA2023081745098](https://openairdocs.org/sdr/ASAA2023081745098.md): Rib · cracked · Aug 17, 2023 · N611AS · Boeing 737790 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STAB RIB CRACKED ON FORWARD STIFFENER OF RIB 92.70. GROUNDED - YES. REPAIRED R/H HORIZONTAL STAB RIB IAW B737-700 SRM 55-10-09-2R-4.
- [SDR ASAA2023081645103](https://openairdocs.org/sdr/ASAA2023081645103.md): Cargo Track · cracked · Aug 16, 2023 · N611AS · Boeing 737790 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PIT L/H CARGO TRACK CRACKED AT STA 727C. GROUNDED - YES. REPAIR AFT PIT L/H CARGO TRACK AT STA 727C IAW B737-700 SRM 53-00-53-2R-3.
- [SDR ASAA2023081645102](https://openairdocs.org/sdr/ASAA2023081645102.md): Cargo Track · cracked · Aug 16, 2023 · N611AS · Boeing 737790 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PIT CARGO TRACK R/H SIDE CRACKED AT STA 727E AND 767. GROUNDED - YES. REMOVED AND REPLACED SECTION OF CARGO TRACK R/H STA 727E-767 IAW B737-700 SRM 53-00-53-2A-3.
- [SDR ASAA2023081645101](https://openairdocs.org/sdr/ASAA2023081645101.md): Shield · corroded · Aug 16, 2023 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT PIT SHIELD FWD OF THE DOOR HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SHIELD FWD OF THE DOOR IAW B737-700 SRM 51-40-02-0G-0.W= 1" O=.050 R= 0 L= 1" D=.050.
- [SDR ASAA2023081545097](https://openairdocs.org/sdr/ASAA2023081545097.md): Skin · cracked · Aug 15, 2023 · N611AS · Boeing 737790 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL LOWER SKIN CRACKED APROX STA 94 AND REAR SPAR. GROUNDED - YES. REPAIRED SKIN IAW B737-700 SRM 55-10-01-2R-11, THIS IS A CAT B REPAIR WITH AN INSPECTIN THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES, AND REPEAT INSPECTION. METHODS D.V.I AT 9000 FLIGHT C
- [SDR ASAA2023010441419](https://openairdocs.org/sdr/ASAA2023010441419.md): Door Latch · sticking · Jan 4, 2023 · N611AS · Boeing 737790 · Passenger/Crew Doors
  > FA RPTS L1 DOOR VERY DIFFICULT TO CLOSE SPECIFICALLY THE HANDLE HARD TO OPERATE. GROUNDED - YES. CLEANED, INSPECTED AND LUBRICATED L1 DOOR MULTIPLE OPERATIONAL CHECK GOOD. REF B737-700 AMM 12-25-11.
- [SDR ASAA2022021137420](https://openairdocs.org/sdr/ASAA2022021137420.md): Lens · detached · Feb 11, 2022 · N611AS · Boeing 737790 · Emergency Equipment
  > L1 DOOR EXIT SIGN COVER DOES NOT STAY PUT LOCATED AT FLOOR LEVEL R SIDE. GROUNDED - YES. REATTACHED TIGHTENED SET SCREW.
- [SDR ASAA2021103036467](https://openairdocs.org/sdr/ASAA2021103036467.md): Lens · detached · Oct 30, 2021 · N611AS · Boeing 737790 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENSE DOOR L-2 CAME OFF. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY REF B737-700 AMM 33-51-01.
- [SDR ASAA2021100636263](https://openairdocs.org/sdr/ASAA2021100636263.md): Unknown · unknown · Oct 6, 2021 · N611AS · Boeing 737790 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SWITCH COVER IN AFT GALLEY HAS A BROKEN RETURN SPRING. GROUNDED - YES. REATTACHED SPRING ON EMERGENCY EXIT LIGHT SWITCH COVER BY HAND.
- [SDR ASAA2021100636262](https://openairdocs.org/sdr/ASAA2021100636262.md): Lamp · inoperative · Oct 6, 2021 · N611AS · Boeing 737790 · Emergency Lighting
  > EMERGENCY EXIT BULB NEAR R2 DOOR BURNED OUT. GROUNDED - YES. RELAMPED R2 DOOR EMERGENCY EXIT LIGHT IAW B737-700 AMM 33-51-01-960-801.
- [SDR ASAA2021100636261](https://openairdocs.org/sdr/ASAA2021100636261.md): Lamp · inoperative · Oct 6, 2021 · N611AS · Boeing 737790 · Emergency Lighting
  > EMERGENCY EXIT BULB BURNED OUT OVER R1 DOOR. GROUNDED - YES. RELAMPED R1 DOOR EMERGENCY EXIT LIGHT IAW B737-700 AMM 33-51-01-960-801.
- [SDR ASAA2021091236036](https://openairdocs.org/sdr/ASAA2021091236036.md): Intercostal · cracked · Sep 12, 2021 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED @ BL0.0, STA 380-400. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPOR ANGLE IAW BOEING 737-700 SRM 51-40-02-0G-0.
- [SDR ASAA2021090936039](https://openairdocs.org/sdr/ASAA2021090936039.md): Beam · corroded · Sep 9, 2021 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > STA 986 FLOOR BEAM HAS CORROSION AROUND NUTPLATE AT APPROX RBL 40. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS, REPAIR STA 986 FLOOR BEAM IAW B737-700 SRM 53-70-51-2R-6.W= 1 O=.150 R=.111 L= 3 D=.039.
- [SDR ASAA2021090836037](https://openairdocs.org/sdr/ASAA2021090836037.md): Web · corroded · Sep 8, 2021 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER SILL WEB CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED LOWER SILL WEB IAW B737-700 SRM 51-40-02-0G-0W= 1 O=.045 R=.040 L= 10 D=.005.
- [SDR ASAA2021090736038](https://openairdocs.org/sdr/ASAA2021090736038.md): Beam · corroded · Sep 7, 2021 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > STA 986 LBL 40 CORROSION FOUND ON FLOOR BEAM. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED STA 986 FLOOR BEAM IAW B737-700 SRM 53-70-51-2R-6W= 1 O=.150 R=.114 L= 2 D=.036.
- [SDR ASAA2021090736035](https://openairdocs.org/sdr/ASAA2021090736035.md): None · corroded · Sep 7, 2021 · N611AS · Boeing 737790 · Fuselage Miscellaneous Structure
  > RBL 50 STA 947-980 CORROSION FOUND ON MOP SILL. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED MOP SILL IAW B737-700 SRM 51-40-02-0G-0W= 2 O=.080 R=.059 L= 20 D=.021.
- [SDR ASAA2021090436131](https://openairdocs.org/sdr/ASAA2021090436131.md): Frame · cracked · Sep 4, 2021 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > FRAME AT STA 440 IS CRACKED BELOW STRIGER 8R AT AIR CONDITIONING RAIL SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED FRAME IAW AD20090102-700-25-1R.
- [SDR ASAA2021090436130](https://openairdocs.org/sdr/ASAA2021090436130.md): Frame · cracked · Sep 4, 2021 · N611AS · Boeing 737790 · Fuselage Main, Structure
  > FRAME AT STA 500A IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING RAIL SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED FRAME IAW AD20090102-700-25-1R.

Next page: https://openairdocs.org/aircraft/N611AS/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 = 'N611AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N611AS/reports

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