# Service difficulty reports: N546AS

A list on [N546AS](https://openairdocs.org/aircraft/N546AS.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 3 · 126 reports

- [SDR ASAA2026032865639](https://openairdocs.org/sdr/ASAA2026032865639.md): Battery · inoperative · Mar 28, 2026 · N546AS · Boeing 737890 · Emergency Lighting
  > FWD AND AFT PASS CABIN EMERGENCY LIGHTS NOT WORKING. GROUNDED - YES. REMOVED AND INSTALLED SERVICABLE EMERGENCY LIGHTS BATTERY S/N 450416, OPS CHECKS GOOD IAW B737-800 AMM 33-57-0G-960-805.
- [SDR ASAA2026032365113](https://openairdocs.org/sdr/ASAA2026032365113.md): Plate · corroded · Mar 23, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO, RT SIDE PLATE CORRODED, BS 727C - 767. GROUNDED - YES. R & R THE SIDE PLATE IAW SRM 53-00-53-2R-5.
- [SDR ASAA2026031765186](https://openairdocs.org/sdr/ASAA2026031765186.md): Plate · corroded · Mar 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY SIDEPLATE HAS CORROSION FROM BS 500I TO 500E LT SIDE. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO BAY SIDEPLATE BS 500I TO 500E LT SIDE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2026022264925](https://openairdocs.org/sdr/ASAA2026022264925.md): Skin · cracked · Feb 22, 2026 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STA 129.50 (MARKED). GROUNDED - YES. REPARIED SKIN RIGHT HORIZONTAL SATAB LOWER AT STA 129.50 IAW B737-800 SRM 55-10-01-2R-11 THIS IS A CAT B REPAIR WITH INSPECTION THRESHOLD AT 56,000 FLIGHT CYCLES AND INTERVAL A
- [SDR ASAA2026022065116](https://openairdocs.org/sdr/ASAA2026022065116.md): Floorbeam · corroded · Feb 20, 2026 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
  > MAIN CABIN, AFT WET AREA, FLOORBEAM, BS 986.5 FOUND CORRODED AT MULTIPLE AREAS. GROUNDED - YES. REMOVED THE DAMAGE ON THE FLOORBEAM, BS 986, RBL 20 - LBL 20, FOUND TO BE IN LIMITS IAW SRM 53-70-51-1A-1, REPAIRED THE FLOORBEAM, BS 986.5, RBL20 - RBL30 &
- [SDR ASAA2026021965187](https://openairdocs.org/sdr/ASAA2026021965187.md): Rib · cracked · Feb 19, 2026 · N546AS · Boeing 737890 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB RIB 182A5302 AT APPROXIMATELY HSS 92.70 HAS MULTIPLE CRACKS. GROUNDED - YES. REPAIRED LT HORIZONTAL STAB RIB 182A5302, IAW SRM 55-10-09-2R-4.
- [SDR ASAA2026021765614](https://openairdocs.org/sdr/ASAA2026021765614.md): Frame · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Main, Frame
  > FWD PIT AFT BULKHEAD SUPPORT FRAME AT STA 500I BOTTOM MIDDLE HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACE FWD PIT AFT BULKHEAD SUPOPRT FRAME AT STA 5001 BOTTOM MIDDLE IAW B737-800 SRM 51-40-02-OG-OW: 1 O:.063 R:.040 L: 1/2 D:.023.
- [SDR ASAA2026021765613](https://openairdocs.org/sdr/ASAA2026021765613.md): Frame · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Main, Frame
  > FWD PIT AFT BULKHEAD SUPPORT FRAME L/H SIDE LOWER AT STA 500I HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT AFT BULKHEAD SUPPORT FRAME L/H SIDE LOWER AT STA 5001 IAW B737-800 SRM 51-70-02-OG-OW: 1 O:.063 R:.046 L: 3 D:.017.
- [SDR ASAA2026021765188](https://openairdocs.org/sdr/ASAA2026021765188.md): Plate · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEPLATE HAS CORROSION FROM BS 727D TO 827 LT SIDE. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SIDEPLATE IAW SRM 53-00-53-2R-5.
- [SDR ASAA2026021765185](https://openairdocs.org/sdr/ASAA2026021765185.md): Cargo Track · cracked · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK R/H SIDE IS CRACKED AT BS 727H-747. GROUNDED - YES. REPAIRED AFT CARGO BAY CARGO TRACK R/H SIDE AT BS 727H -747 IAW SRM 53-00-53-2R-3.
- [SDR ASAA2026021765115](https://openairdocs.org/sdr/ASAA2026021765115.md): Web · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO SILL WEB CORROED. GROUNDED - YES. R & R THE SILL WEB IAW SRM 51-40-02-0G-0.
- [SDR ASAA2026021765114](https://openairdocs.org/sdr/ASAA2026021765114.md): Plate · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO, RT SIDE PLATE CORRODED, BS 500C - 500D. GROUNDED - YES. R & R THE SIDE PLATE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2026021765112](https://openairdocs.org/sdr/ASAA2026021765112.md): Web · corroded · Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FOWARD CARGO SILL WEB CORRODED. GROUNDED - YES. R & R THE SILL WEB, IAW SRM 51-40-02-0G-0.
- [SDR ASAA2026020765638](https://openairdocs.org/sdr/ASAA2026020765638.md): Charger · inoperative · Feb 7, 2026 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY LIGHT INOP AT EXTERIOR L1 DOOR. GROUNDED - YES. REMOVED AND REPLACED BATTERY CHARGER S/N 120105 FOR EMERGENCY LIGHTS IAW AMM 33-51-04-960-801 AND LAMP IAW B737-800 AMM 33-51-06-960-806 OPS CHECK GOOD.
- [SDR ASAA2025122063242](https://openairdocs.org/sdr/ASAA2025122063242.md): Light · malfunctioned · Dec 20, 2025 · N546AS · Boeing 737890 · Emergency Lighting
  > 16 AND 17A EXIT ROW PLACARD LIGHT ARE FLICKERING AND DIMMER THAN NORMAL. GROUNDED - YES. AFTER POWER RECYCLE UNABLE TO DUPLICATE FAULT 16 AND 17A EXIST AND THE REST WORK NORMAL, NO HISTORY REF AMM 33-51-00.
- [SDR ASAA2025081760147](https://openairdocs.org/sdr/ASAA2025081760147.md): Sign · loose · Aug 17, 2025 · N546AS · Boeing 737890 · Emergency Lighting
  > FA REPORTS LOWER EXIT ROW SIGN SEATS 16 A-C LOOSE. GROUNDED - YES. REMOVED AND REPLACED LOWER EXIT ROW SIGN SEATS 16 A-C. OPS CHECK GOOD REF AMM 33-51-01.
- [SDR ASAA2025052758302](https://openairdocs.org/sdr/ASAA2025052758302.md): Guide Arm · binding · May 27, 2025 · N546AS · Boeing 737890 · Service Doors
  > FA REPORTS R1 DOOR WILL NOT CLOSE/SITS AJAR (CAN SEE DAYLIGHT THROUGH IT). GROUNDED - YES. FOUND R1 DOOR WONT CLOSE UNLESS APPLYING FORCE TO ASSIST HANDLE, INSPECTED R1 DOOR, FOUND CENTERING GUIDE & ROLLER DAMAGE ALSO FOUND DAMAGE TO CENTERING GUIDE TRACK BOD
- [SDR ASAA2025021355974](https://openairdocs.org/sdr/ASAA2025021355974.md): Battery Pack · faulted · Feb 13, 2025 · N546AS · Boeing 737890 · Emergency Lighting
  > WHILE PERFORMING T/C 78233001, FOUND EMERGENCY LIGHTS UNDER OVERHEAD BINS BETWEEN ROWS 17 THROUGHOUT 24 ABC & DEF DID NOT OPERATE LONGER THAN 15 MINUTES. GROUNDED - YES. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS FOR ROWS 17 - 24 ABC AND DEF PER AMM 33-51-06,
- [SDR ASAA2024070150709](https://openairdocs.org/sdr/ASAA2024070150709.md): Lens · broken · Jul 1, 2024 · N546AS · Boeing 737890 · Emergency Lighting
  > LIGHT UNDER L-1 EXIT PLACARD BROKEN. GROUNDED - YES. REMOVED AND REPLACED L-1 DOOR LIGHT COVER AND OPS NML. OK FOR SVC.
- [SDR ASAA2024021347885](https://openairdocs.org/sdr/ASAA2024021347885.md): Power Supply · inoperative · Feb 13, 2024 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY EXIT DOOR LIGHT INOP ON SEAT 16A INTERMITTENTLY. GROUNDED - YES. CHARGED BATTERY PACK AND POWER SUPPLY FOR SEAT 16A EMERGENCY EXIT LIGHT, OPS CHECK GOOD IAW B737-800 AMM 33-51-06-610-802.
- [SDR ASAA2024012247774](https://openairdocs.org/sdr/ASAA2024012247774.md): Panel · corroded · Jan 22, 2024 · N546AS · Boeing 737890 · Ailerons
  > L/H WING AILERON BALANCE BAY PANELS HAVE PITTED AND CORRODED BUTTON HEAD RIVETS. GROUNDED - YES. REMOVED AND REPLACED RIVETS IAW B737-800 SRM 51-40-02-0G-0 AND OPS TEST GOOD.
- [SDR ASAA2024012147773](https://openairdocs.org/sdr/ASAA2024012147773.md): Panel · corroded · Jan 21, 2024 · N546AS · Boeing 737890 · Ailerons
  > RIGHT WING AILERON #3 BALANCE PANEL BUTTON HEAD RIVETS PITTED/CORRODED. GROUNDED - YES. REMOVED AND REPLACED RIVETS AILERON BALANCE PANEL #3 IAW B737-800 SRM 51-40-02-0G-0, OPS CHECK GOOD AT THIS TIME IAW BOEING 737-800 AMM 27-11-00-700-809 19 C,D,E.
- [SDR ASAA2024012147772](https://openairdocs.org/sdr/ASAA2024012147772.md): Panel · corroded · Jan 21, 2024 · N546AS · Boeing 737890 · Ailerons
  > RIGHT WING AILERON #2 BALANCE PANEL BUTTON HEAD RIVETS PITTED/CORRODED. GROUNDED - YES. REMOVED AND REPLACED RIVETS AILERON BALANCE PANEL #2 IAW B737-800 SRM 51-40-02-0G-0, OPS CHECK GOOD AT THIS TIME IAW BOENG 737-800 AMM 27-11-00-700-809 19, C,D,E.
- [SDR ASAA2024012147770](https://openairdocs.org/sdr/ASAA2024012147770.md): Battery Pack · faulty · Jan 21, 2024 · N546AS · Boeing 737890 · Emergency Lighting
  > R2 EMERGENCY LIGHTS FAILED OP CHECK. GROUNDED - YES. REMOVED, REPLACED, AND OPS CHECKED GOOD THE R2 EMERGENCY LIGHT BATTERY PACK IAW B737-800 AMM 33-51-06-960-805 STEP 4.E & 4.F. (S/N 223209)
- [SDR ASAA2024011947769](https://openairdocs.org/sdr/ASAA2024011947769.md): Doubler · worn · Jan 19, 2024 · N546AS · Boeing 737890 · Fluid Service Doors
  > DOUBLER/PANEL LANDING FOR WATER SERVICE DOOR 146AR IS WORN ALMOST HALF WAY THROUGH THE DOUBLER MATERIAL. GROUNDED - YES. REMOVED AND REPLACED DOUBLER/PANEL LANDING FOR WATER SERVICE DOOR 146AR IAW B737-800 SRM 51-40-02-0G-0.
- [SDR ASAA2022030237709](https://openairdocs.org/sdr/ASAA2022030237709.md): Skin · cracked · Mar 2, 2022 · N546AS · Boeing 737890 · Horizontal Stabilizer Structure
  > RH HORIZ LWR SKIN IS CRACKED AT STA 138 APPROX 18 IN FWD OF REAR SPAR. GROUNDED - YES. REPAIRED RH STAB LWR SKIN IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11 REPAIR IS A CAT B REPAIR WITH SUPPLEMENTAL INSPECTIONS AS FOLLOWS: THRESHOLD 56,000 CYCLES & REPEAT INSPE
- [SDR ASAA2021090135843](https://openairdocs.org/sdr/ASAA2021090135843.md): Skin · corroded · Sep 1, 2021 · N546AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FOUND SKIN CORROSION JUST BELOW THE WASTE TANK VENT PORT. GROUNDED - YES. REPAIRED FUSELAGE SKIN IAW 737-800 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSPECTION INTERVAL OF 5,000 FLT CYCLES AND A THRESHOLD OF 50,000 FLT CYCLES A/C TOTAL FLT CYCLES AT T
- [SDR ASAA2020040232593](https://openairdocs.org/sdr/ASAA2020040232593.md): Power Supply · failed · Mar 31, 2020 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY LIGHTS FOR L1 DOOR FAILS CK. GROUNDED - YES. REMOVED,REPLACED AND OPS CK GOOD MIG 75 3 EMER LIGH PWR SUPPLY FOR L1 DOOR LIGHTS IAW B737 800 AMM 33 51 06 960 806.
- [SDR ASAA2020032532556](https://openairdocs.org/sdr/ASAA2020032532556.md): Floor Support · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT WET FLOOR SUPPORT STA 947 TO 967 LBL 45 HAS LIGHT COROSION. GROUNDED - YES. REMOVED & REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02-0G-0W=2" O=.080 R=.051 L=1" D=.029.
- [SDR ASAA2020032532553](https://openairdocs.org/sdr/ASAA2020032532553.md): Cargo Track · cracked · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PIT RH CARGO TRACK IS CRACKED AT RADIUS ATTACH POINT STA. 727E AND STA. 727G. GROUNDED - YES. REMOVED AND REPLACED CARGO TRACK IAW B737-800 SRM 53-00-53-2R-3.
- [SDR ASAA2020032532547](https://openairdocs.org/sdr/ASAA2020032532547.md): Floorbeam · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
  > FLOOR BEAM 947 HAS COROSION AT BL0. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1, REPAIRED DAMAGE TO FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-8W: 1 O:.190 R:.157 L: 2 D:.033.
- [SDR ASAA2020032532538](https://openairdocs.org/sdr/ASAA2020032532538.md): Floor Support · cracked · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT IS CRACKED STA 540 BETWEEN BL 0 AND LBL 24. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT IAW B737 800 SRM 51 40 02 0G 0.
- [SDR ASAA2020032432518](https://openairdocs.org/sdr/ASAA2020032432518.md): Transition Panel · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT LH TRANSITION PANEL IS CORRODED AND MISSING NUT PLATES FROM STA 727 TO 727E+10. GROUNDED - YES. REMOVED AND REPLACED AFT PIT L/H TRANSITION PNL AND MUT PLATES FROM STA 727 TO 727E+10 IAW B737 800 SRM 51 40 02 0G 0 W 2" O.040 R.024 L 2" D.016.
- [SDR ASAA2020032432517](https://openairdocs.org/sdr/ASAA2020032432517.md): Transition Panel · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT PIT LH TRANSITION PANEL HAS CORR FROM STA 747.5 TO STA 807. GROUNDED - YES. REMOVED AND REPLACED AFT PIT LH TRANSITION PANEL IAW B737 800 SRM 51 40 02 0G 0 W 8" O.040 R.022 L 3" D.018.
- [SDR ASAA2020032432516](https://openairdocs.org/sdr/ASAA2020032432516.md): Floorbeam · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
  > FLOOR BEAM STA 986.5 HAS CORR AROUND NUTPLATE HOLE AT RBL 10 AND RBL45. GROUNDED - YES. CORR FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 REMOVED AND REPLACED EXISTING UPPER T CAP REPAIR PART IAW B737 800 SRM 53 70 51 2R 4 W 1 O.150 R.140 L 2 D.
- [SDR ASAA2020032432515](https://openairdocs.org/sdr/ASAA2020032432515.md): Floorbeam · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
  > FLOOR BEAM STA 986.5 HAS CORR AROUND NUTPLATE HOLE LBL 45. GROUNDED - YES. CORR FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1, REMOVED AND REPLACED EXISTING UPPER T-CAP REPAIR PART IAW B737 800 SRM 53 70 51 2R 4 W 1 O.50 R.133 L 2 D.017.
- [SDR ASAA2020032432514](https://openairdocs.org/sdr/ASAA2020032432514.md): Floor Support · corroded · Mar 9, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT RBL 45 ST. 947 TO 967 HAS CORR. GROUNDED - YES. REMOVED DAMAGE BY BLENDING, ORIG T.080", LOSS OF.035, REMAINING T.045", FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 70 51 1A 1 REMOVED AND REPLACED DAMAGED AFT WET AREA FLOOR SUPPO
- [SDR ASAA2020040232590](https://openairdocs.org/sdr/ASAA2020040232590.md): Skin · cracked · Mar 4, 2020 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > LEFT LOWER HORIZ. STAB SKIN CRACKED AT STA. 138.70 O/B ROW OF FASTENERS. GROUNDED - YES. REPAIRED IAW B737 800 SRM 55 10 01 2R 11, THIS IS A CATEGORY B REPAIR REQUIRING DETAILED VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION EVERY 9,000 F
- [SDR ASAA2020040232589](https://openairdocs.org/sdr/ASAA2020040232589.md): Skin · cracked · Mar 4, 2020 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > LEFT LWR HORIZONTAL STAB SKIN IS CRACKED AT STA 129.50 I/B ROW OF FASTENERS. GROUNDED - YES. REPAIRED IAW B737 800 SRM 55 10 01 2R 11, THIS IS A CATEGORY B REPAIR REQUIRING DETAILED VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION EVERY 900
- [SDR ASAA2020040232588](https://openairdocs.org/sdr/ASAA2020040232588.md): Skin · cracked · Mar 4, 2020 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON BOTTOM OF RIGHT HORIZ STAB SKIN AT STATION 129.50 O/B ROW OF FASTENERS. GROUNDED - YES. REPAIRED IAW B737 800 SRM 55 10 01 2A 11, THIS IS A CATEGORY B REPAIR REQUIRING DETAILED VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION EVERY
- [SDR ASAA2020032532554](https://openairdocs.org/sdr/ASAA2020032532554.md): Door Sill · corroded · Mar 4, 2020 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUT OUT LOWER SILL WEB CORRODED. GROUNDED - YES. REMOVED & REPLACED AFT CARGO SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 2" O:.050" R:.010" L: 2.0" D:.040".
- [SDR ASAA2020032532552](https://openairdocs.org/sdr/ASAA2020032532552.md): Door Sill · corroded · Mar 4, 2020 · N546AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUTOUT LOWER SILL WEB IS CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02-0G-0W: 2 O:.056 R:.046 L: 8 D:.010.
- [SDR ASAA2019101591013](https://openairdocs.org/sdr/ASAA2019101591013.md): Fitting · gouged · Sep 13, 2019 · N546AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > WHILE ACCOMPLISHING T/C 78327000 FOUND GOUGE NEAR AFT O/B BOLT ON L/H JACKSCREW SUPPORT FITTING LOOKING AFT. GROUNDED - YES. LOCAL BLEND REPAIRED PER ASA EA 800-27EA-22071.
- [SDR ASAA2018082982948](https://openairdocs.org/sdr/ASAA2018082982948.md): Lens · missing · Aug 28, 2018 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY LIGHT EXIT SIGN FOR THE NR 4 GALLEY, ADJACENT TO THE L2 DOOR WAS MISSING THE LENS. ACFT GROUNDED. REPLACED THE LENS AND TESTED THE LIGHT IAW AMM 33-51-01-960-801. OPS NORMAL.
- [SDR ASAA2018032824055](https://openairdocs.org/sdr/ASAA2018032824055.md): Power Supply · inoperative · Mar 28, 2018 · N546AS · Boeing 737890 · Emergency Lighting
  > RIGHT FWD WING EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE POWER SUPPLY AND OPS CHECKED GOOD IAW AMM 33-51-06.
- [SDR ASAA2018030123794](https://openairdocs.org/sdr/ASAA2018030123794.md): Channel · corroded · Mar 1, 2018 · N546AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR PANEL LEFT SIDE ZEE CHANNEL HAS CORROSION AT 7 FASTENER HOLES. ACFT GROUNDED. BLENDED CORROSION ON THE CHANNEL BS 727J - 747 AND 727H + 9. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, FIG 103, SHEET 2. REMOVED THE CHANNEL IAW SRM 53-
- [SDR ASAA2018030123779](https://openairdocs.org/sdr/ASAA2018030123779.md): Floorbeam · cracked · Mar 1, 2018 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM ANGLE CRACKED BS 540, RBL 2. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02.
- [SDR ASAA2017120522792](https://openairdocs.org/sdr/ASAA2017120522792.md): Lens · broken · Dec 5, 2017 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY LIGHT EXIT LOCATOR SIGN AT R-2 DOOR HAS DAMAGED LENS. GROUNDED - YES. REMOVED AND REPLACED LENS AND TESTED LIGHT ASSY PER AMM 33-51-01-960-801 - OPS NORMAL.
- [SDR ASAA2017032320266](https://openairdocs.org/sdr/ASAA2017032320266.md): Cover · missing · Mar 23, 2017 · N546AS · Boeing 737890 · Emergency Lighting
  > EMERGENCY EXIT SIGN HOUSING AT MID CABIN CEILING IS MISSING COVER ON FWD SIDE. ACFT GROUNDED. REPLACED THE COVER.
- [SDR ASAA2017011519392](https://openairdocs.org/sdr/ASAA2017011519392.md): Light · missing · Jan 15, 2017 · N546AS · Boeing 737890 · Emergency Lighting
  > EXIT LIGHTING TRACK AT ROW 12DEF SIDE MISSING. GROUNDED - YES. INSTALLED NEW TRACK LT AT ROW 12DEF. OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N546AS/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 = 'N546AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N546AS/reports

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