# Service difficulty reports: N843AS, cancelled Jun 1, 2017

A list on [N843AS, cancelled Jun 1, 2017](https://openairdocs.org/deregistered/N843AS-2017-06-01.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 · 148 reports

- [SDR ASOA2016021014503](https://openairdocs.org/sdr/ASOA2016021014503.md): Floorbeam · corroded · Feb 10, 2016 · N843AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOORBEAM AT FS430.00 AND LBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH STEPS 1-14 OF REO PL 601R-53-41-19980 COMPLIED WITH STEP 15 OF REO PL 601R-53-41-1998. REPAIRED
- [SDR ASOA2016021014502](https://openairdocs.org/sdr/ASOA2016021014502.md): Floorbeam · corroded · Feb 10, 2016 · N843AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOORBEAM FS 461.00 AND LBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH REO PL 601R-53-41-19980. COMPLIED WITH REO PL 601R-53-41-1998. REPAIRED IAW ECTC 601R-53-41-1998
- [SDR ASOA2016021014501](https://openairdocs.org/sdr/ASOA2016021014501.md): Floor Support · corroded · Feb 10, 2016 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PRESSURE FLOOR SUPPORT BEAM IN MULTIPLE LOCATIONS BETWEEN FS409.00+128 AND FS559.00 AT RBL9. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. COMPLIED WITH REO PL 601R-53-41-19980. COMPLIED WITH REO
- [SDR ASOA2016020914511](https://openairdocs.org/sdr/ASOA2016020914511.md): Skin · dented · Feb 9, 2016 · N843AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ASD SURROUNDING STRUCTURE LOWER FWD CORNER HAS DAMAGE, DENT. REMOVED DAMAGE AT ASD SURROUNDING STRUCTURE LOWER FWD CORNER IAW REO 601R-53-21-160. BLENDED AREA IS OUT OF LIMITS IAW REO 601R-53-21-160. ECTC NOT REQUIRED FOR GREO 601R-53-21-160 DAMAGE IS OUT O
- [SDR ASOA2016020614500](https://openairdocs.org/sdr/ASOA2016020614500.md): Floor Panel · corroded · Feb 6, 2016 · N843AS · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION FOUND ON PRESSURE FLOOR JUST FWD OF FS 559 ON RT SIDE. BLENDED CORROSION FWD OF FS 559 ON CROSSBEAM ABOVE PRESSURE FLOOR IAW SRM 51-21-06-00. EVALUATED BLEND AREA FOUND TO BE ON STEP AT FS 559.00 BETWEEN RBL36-RBL45 OUT OF ALLOWABLE DAMAGE LIMITS I
- [SDR ASOA2016020514499](https://openairdocs.org/sdr/ASOA2016020514499.md): Door Sill · gouged · Feb 5, 2016 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL IS GOUGED CAUSED BY ANTI-MIGRATION PIN. EC/TC REO 601R-53-21-814 FOUND TO BE OUT OF LIMITS. DAMAGE MEASURED BY MECHANICAL MEANS.063" FOUND TO BE OUT LIMITS IAW REO 601R-53-21-814, TYPE IV STEP, 2. RECIEVED DEVIATION TO REO 601R-53-21-814 AND
- [SDR ASOA2016020214510](https://openairdocs.org/sdr/ASOA2016020214510.md): Inlet · eroded · Feb 2, 2016 · N843AS · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > LEFT ENGINE INLET ERODED. COMPLIED WITH PERMANENT REPAIR OF LT ENGINE INLET IAW CMM 71-61-01. REPAIRED LT ING INLET EROSION IAW CMM TASK 71-61-01-300-822-A01.
- [SDR ASOA2014102711491](https://openairdocs.org/sdr/ASOA2014102711491.md): Isolator · cracked · Oct 20, 2014 · N843AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 FWD FACE OF BULKHEAD NUMEROUS ISOLATOR MOUNTS CRACKED AND/OR BROKEN. REPLACED ISOLATORS WITH NEW IAW SRM 51-42-06.
- [SDR ASOA2014102711490](https://openairdocs.org/sdr/ASOA2014102711490.md): Support Angle · cracked · Oct 20, 2014 · N843AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD, CARGO DOOR SUPPORT MEMBER. LOWER ATTACHMENT ANGLE IS CRACKED. R & R SUPPORT ANGLE WITH NEW SERVICEABLE PART IAW SRM 51-42-21.
- [SDR ASOA2014082211133](https://openairdocs.org/sdr/ASOA2014082211133.md): Light · damaged · Aug 21, 2014 · N843AS · Cndair CL6002B19 · Emergency Lighting
  > PAX ENTRY FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY DAMAGED. R & R PAX ENTRY FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR ASOA2014021909989](https://openairdocs.org/sdr/ASOA2014021909989.md): Trunnion · cracked · Jan 31, 2014 · N843AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LEFT MLG TRUNNION HAS ONE CRACKED FASTENER HOLE. RECEIVED AND COMPLIED WITH REO 601R-57-21-2099 AND EC/TC REO 601R-57-21-2099. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909988](https://openairdocs.org/sdr/ASOA2014021909988.md): Skin · corroded · Jan 30, 2014 · N843AS · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS PANEL 540BB HAS PITTING AROUND THE FLANGE. COMPLIED WITH REO 601R-57-21-030 AND EC/TC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909987](https://openairdocs.org/sdr/ASOA2014021909987.md): Skin · corroded · Jan 30, 2014 · N843AS · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS PANEL RT WING 640BB HAS CORROSION AROUND LAND. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909986](https://openairdocs.org/sdr/ASOA2014021909986.md): Access Panel · corroded · Jan 30, 2014 · N843AS · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS PANEL 650CB CORRODED. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909985](https://openairdocs.org/sdr/ASOA2014021909985.md): Bulkhead · cracked · Jan 28, 2014 · N843AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON REAR PRESSURE BULKHEAD FORWARD FACE BELOW WL 120.43 AT BL 0. COMPLIED WITH ECTC REO601R-53-61-1285 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1285, REV D.
- [SDR ASOA2014021909984](https://openairdocs.org/sdr/ASOA2014021909984.md): Cargo Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED FS 559+80, LBL 27.5. REMOVED AND REPLACED CARGO TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802, & 53-01-11-400-802.
- [SDR ASOA2014021909983](https://openairdocs.org/sdr/ASOA2014021909983.md): Seat Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED FS 409+128-559, RBL 9. COMPLIED WITH REO 601R-53-00-485, REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND AMM 53-01-11-400-801.
- [SDR ASOA2014021909982](https://openairdocs.org/sdr/ASOA2014021909982.md): Seat Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED FS 394-409+128, RBL 9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014021909981](https://openairdocs.org/sdr/ASOA2014021909981.md): Seat Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED FS 394-409+128, LBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 01-11-400-802.
- [SDR ASOA2014021909980](https://openairdocs.org/sdr/ASOA2014021909980.md): Seat Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED FS 364-394, RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.
- [SDR ASOA2014021909979](https://openairdocs.org/sdr/ASOA2014021909979.md): Seat Track · corroded · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED, FS 364-394, LBL 9.0. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.
- [SDR ASOA2014021909978](https://openairdocs.org/sdr/ASOA2014021909978.md): Attach Angle · cracked · Jan 25, 2014 · N843AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 280 BULKHEAD TO LBL 9 FLOOR ATTACH ANGLE CRACKED OTBD SIDE. REMOVED ATTACH ANGLE IAW SRM 51-42-20. INSTALLED FABRICATED NEW ATTACH ANGLE IAW REO 601R-53-11-926. COMPLIED WITH REO 601R-53-11-926, REV B IAW NDTM PART 1, 51-20-06. REPAIR CLASSIFIED AS MAJO
- [SDR ASOA2014021909977](https://openairdocs.org/sdr/ASOA2014021909977.md): Hinge · dented · Jan 24, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE HALF DENTED BETWEEN RIVET 7 AND 11 AND INCLUDE DOOR FRAME UNDER SEAL RETAINER. REPAIRED IAW SRM 52-00-00 AND SRM 51-42-06. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909976](https://openairdocs.org/sdr/ASOA2014021909976.md): Hinge · gouged · Jan 23, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > HINGE SEGEMENT, PASSENGER DOOR LUGS HAS GOUGE DAMAGE. R & R HINGE IAW SUPPLEMENT ASA 52-11-26. COMPLIED WITH ECTC EO600-52-0146. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909975](https://openairdocs.org/sdr/ASOA2014021909975.md): Hinge · gouged · Jan 23, 2014 · N843AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > HINGE SEGEMENT HALF ON FUSELAGE SIDE HAS GOUGED LUGS. REPAIRED IAW REO 601R-53-21-814. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014021909974](https://openairdocs.org/sdr/ASOA2014021909974.md): Intercostal · cracked · Jan 23, 2014 · N843AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR LOWER AFT CORNER INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-06-000. INSTALLED INTERCOSTAL & FASTENERS IAW SRM DWG 601R3507. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2013101409213](https://openairdocs.org/sdr/ASOA2013101409213.md): Light · wrong part · Oct 8, 2013 · N843AS · Cndair CL6002B19 · Emergency Lighting
  > CABIN FLOOR EMERGENCY LIGHT INCORRECT FOR THIS ACFT. R & R PAX CABIN EMERGENCY LIGHT IAW AMM 33-51-01 01.
- [SDR ASOA2013092509099](https://openairdocs.org/sdr/ASOA2013092509099.md): Skin · dented · Sep 24, 2013 · N843AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE AT FS 310 AND STGR 16L CAUSED BY CONTACT WITH FWD LOWER PAX DOOR LATCH PIN. REPAIRED IAW GREO 601R-53-21-160, REV B. CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3.
- [SDR ASOA2012122102698](https://openairdocs.org/sdr/ASOA2012122102698.md): Sign · inoperative · Dec 19, 2012 · N843AS · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED EMERGENCY EXIT SIGN ON THE LOWER WARDROBE INOPERATIVE. R & R THE LIGHTED EMERGENCY EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR ASOA2012102902405](https://openairdocs.org/sdr/ASOA2012102902405.md): Pushrod · out of adjust · Oct 25, 2012 · N843AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SOMETIMES WILL NOT OPEN. ADJUSTED PUSH ROD ON LATCH CAM TORQUE-TUBE MECHANISM IAW AMM 52-11-23. SDR CLOSED.
- [SDR ASOA2012102602399](https://openairdocs.org/sdr/ASOA2012102602399.md): Wire · misrouted · Oct 22, 2012 · N843AS · Cndair CL6002B19 · Door System Wiring
  > ON GATE RETURN, COULD NOT OPEN PAX DOOR. WIRING ON P55MB AND P56MB WAS FOUND HOOKED OVER THE CAM ON PAX DOOR TORQUE TUBE. REPAIRED. PERFORMED OPS TEST OF PAX DOOR IAW AMM 52-11-00. NO DEFECT NOTED.
- [SDR ASOA201200539](https://openairdocs.org/sdr/ASOA201200539.md): Frame · corroded · Feb 20, 2012 · N843AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.00 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REPAIRED IAW REO 601R-53-21-2264.
- [SDR ASOA201200510](https://openairdocs.org/sdr/ASOA201200510.md): Skin · cracked · Feb 17, 2012 · N843AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK CRACKED OTBD OF RT JACK PAD. REWORKED AREA IAW REO 601R-57-21-130 REV J.
- [SDR ASOA201200492](https://openairdocs.org/sdr/ASOA201200492.md): Angle · corroded · Feb 13, 2012 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 CORRODED. REMOVED DAMAGE IAW REO 601R-53-21-2263. COMPLIED NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. INSTALLED NEW SERVICEABLE ANGLE AND FITTING AT FS 349.00 IAW SRM 51-42-06-00 AND 51-42-21-00.
- [SDR ASOA201200552](https://openairdocs.org/sdr/ASOA201200552.md): Sill · corroded · Feb 9, 2012 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL CORRODED AROUND BOTH FWD AND AFT STOP FITTINGS. REMOVED SERVICE DOOR SILL DUE TO CORROSION BE BEYOND LIMITS IAW SRM 31-42-21 AND 51-42-06. INSTALLED NEW SERVICEBLE SERVICE DOOR SILL IAW SRM 51-42-21 AND 51-42-06.
- [SDR ASOA201200455](https://openairdocs.org/sdr/ASOA201200455.md): Structure · corroded · Feb 9, 2012 · N843AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 ON CORRODED. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE BEYOND LIMITS. REMOVED FITTING AND ANGLE, IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA201200443](https://openairdocs.org/sdr/ASOA201200443.md): Frame · corroded · Feb 9, 2012 · N843AS · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REMOVED CORROSION IAW SRM 51-21-06-00. PERFORMED UT THICKINESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MIN MATERIAL REMAINING IS.045" ORIGINAL IS.050" MATERIAL REMOVED IS.005". ALODINED AREA, WET
- [SDR ASOA201200550](https://openairdocs.org/sdr/ASOA201200550.md): Bushing · corroded · Feb 8, 2012 · N843AS · Cndair CL6002B19 · Horizontal Stabilizer, Attach Fittings
  > LEFT SIDE HORIZONTAL TO VERTICAL ATTACHMENT POINT BUSHING CORRODED ON VERTICAL. REMOVED THE HORISONTAL STABLIZER IAW AMM 55-10-00-000-801. REPAIRED BUSHING, INSTALLED ORIGINAL HORIZONTAL STABLIZER IAW AMM 55-10-00-400-801.
- [SDR ASOA201200439](https://openairdocs.org/sdr/ASOA201200439.md): Rib · cracked · Feb 8, 2012 · N843AS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT WING AFT SPAR SUPPORT RIB AT WS 149.58 CRACKED. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2 AREA IS CONFIRMED CRACKED. REPAIRED IAW REO 601R-57-21-130, REV J, REPAIR OPTION 2.
- [SDR ASOA201200437](https://openairdocs.org/sdr/ASOA201200437.md): Housing · broken · Feb 8, 2012 · N843AS · Cndair CL6002B19 · Emergency Lighting
  > CEILING EMERGENCY LIGHT HOUSING BROKEN AT FLOOD LIGHT 1, FS 405.00. R & R EMERGENCY LIGHT ASSY WITH NEW LIGHT ASSY IAW AMM 33-51-16-000-801 & 33-51-16-400-801.
- [SDR ASOA201200548](https://openairdocs.org/sdr/ASOA201200548.md): Seat Belt · unserviceable · Feb 6, 2012 · N843AS · Cndair CL6002B19 · Passenger Compartment Equipment
  > SEATS 1A AND 1B SEAT BELT TAGS UNREADABLE. R & R SEAT BELTS FOR PAX SEATS 1A&1B IAW CMM 25-25-82.
- [SDR ASOA201200414](https://openairdocs.org/sdr/ASOA201200414.md): Light · damaged · Feb 6, 2012 · N843AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT STAINED BEYOND 10 PERCENT OF 48 INCH LENGTH. (4.75) AT SEATS 1&2 ABCD. R & R LIGHT IAW AMM SUPPLEMENT 33-51-00 AND 33-51-01-000-806, 33-51-01-400-806. OP CHECKED GOOD.
- [SDR ASOA201101500](https://openairdocs.org/sdr/ASOA201101500.md): Fitting · cracked · Aug 13, 2011 · N843AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LT MLG MAIN FITTING HAS A CRACK INDICATION ON OTBD SIDE OF AFT BOLT HOLE AREA. REMOVED LT MLG ASSY IAW AMM 32-11-00. R & R MAIN FITTING ASSY IAW CMM 32-10-15. REINSTALLED SERVICABLE LT MLG ASSY IAW AMM 32-11-00. OPS AND LEAK CHECK GOOD IAW AMM 32-11-00.
- [SDR ASOA201001831](https://openairdocs.org/sdr/ASOA201001831.md): Battery · discharged · Nov 24, 2010 · N843AS · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN'S FLASHLIGHT INOP. REPLACED BATTERIES IN FLASHLIGHT, OPS TEST GOOD IAW CRJ 200 AMM 25-61-00.
- [SDR ASOA201001511](https://openairdocs.org/sdr/ASOA201001511.md): Thrust Reverser · unknown · Oct 7, 2010 · N843AS · Cndair CL6002B19 · Engine Thrust Reverser
  > LT ENGINE THRUST REVERSER ECAIS MESSAGE AND REV N1 WARNING INFLIGHT. COMPLIED WITH QRH 1-12 NO OTHER ABNORMALITIES NOTED. (ACFT RETURNED TO DEPARTURE AFTER T/O -- TOWER DECLARED EMERGENCY) PERFORMED OPS TEST OF THE THRUST REVERSER SYS IAW AMM 78-30-00. OPS CK
- [SDR ASOA201001145](https://openairdocs.org/sdr/ASOA201001145.md): Door · binding · Aug 18, 2010 · N843AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HARD TO OPEN, OUTER HANDLE HARD TO DEPLOY. COMPLIED WITH OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.
- [SDR ASOA201000160](https://openairdocs.org/sdr/ASOA201000160.md): Skin · cracked · Feb 3, 2010 · N843AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING FUEL DRAIN HOLE AT APPROX WS 50.00 HAS A 60 PERCENT FSH HFEC INDICATION NOTED 0.100" LONG APPROX 0125" OTBD OF DRAIN HOLE. INDICATION MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-57-21-1230 AND REO 601R-57-21-1230.
- [SDR ASOA201000152](https://openairdocs.org/sdr/ASOA201000152.md): Sill · corroded · Feb 3, 2010 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL PLATE HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 621.00. REMOVED 5 OLD DAMAGED INSERTS. INSTALLED 5 NEW SERVICEABLE INSERTS FROM LAV THRESHOLD IAW CMM 53-10-04 PART D STEPS 1-13, USING EY3010A/B ADHESIVE PO W1011.
- [SDR ASOA201000151](https://openairdocs.org/sdr/ASOA201000151.md): Plate · cracked · Feb 3, 2010 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR LANDING PLATE IS CRACKED AT FS 589 AT INBD FLOORBEAM RIVET. C/W EC/TC REO 601R-53-61-433 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-433.
- [SDR ASOA201000141](https://openairdocs.org/sdr/ASOA201000141.md): Beam · cracked · Feb 1, 2010 · N843AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409+128 BULKHEAD LBL 18.00 VERTICAL BEAM CRACKED ON C/B SIDE BY LOWER ATTACH FASTENER. REMOVED VERT BEAM IAW SRM 51-42-06 ST 1 AND 11. INSTALLED NEW SERVICEABLE O/B VERTICAL BEAM TO THE BEAM ASSEMBLY IAW SRM 51-42-06 1 AND 9. INSTALLED VERT BEAM IAW RE

Next page: https://openairdocs.org/deregistered/N843AS-2017-06-01/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 = 'N843AS' AND deregistration_id = 'N843AS-2017-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N843AS-2017-06-01/reports

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