# Service difficulty reports: N846AS, cancelled Jun 1, 2017

A list on [N846AS, cancelled Jun 1, 2017](https://openairdocs.org/deregistered/N846AS-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 4 · 198 reports

- [SDR ASOA2016032214637](https://openairdocs.org/sdr/ASOA2016032214637.md): Seal · dirty · Mar 22, 2016 · N846AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WOULD NOT OPEN FROM OUTSIDE. OPENED DOOR, CLEANED SEALS & OPS CK IAW AMM 52-41-00.
- [SDR ASOA2016020314438](https://openairdocs.org/sdr/ASOA2016020314438.md): Skin · damaged · Feb 3, 2016 · N846AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 3 BURNS IN SKIN EDGE AT FS 169.00. DAMAGE A IS BLEND OUT AT FS 169 JUST FWD OF ADG DOOR AND MEASURES.007" DEEP X.400" L X.300" W AND FOUND TO BE OUT OF LIMITS, TOO CLOSE TO NEAREST FASTENER, DAMAGE B IS EDGE DAMAGE AT FS 169 FWD OF ADG DOOR, EDGE TRIMMED
- [SDR ASOA2015101813932](https://openairdocs.org/sdr/ASOA2015101813932.md): Door · unknown · Oct 18, 2015 · N846AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR UNABLE TO BE OPENED FROM THE OUTSIDE. PERFORMED OPS TEST OF THE SERVICE DOOR IAW AMM 52-41-00. OPS CHECK GOOD ACFT OK FOR SERVICE.
- [SDR ASOA2015101313889](https://openairdocs.org/sdr/ASOA2015101313889.md): Light · damaged · Oct 13, 2015 · N846AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOODLIGHT AT SERVICE DOOR DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014072510979](https://openairdocs.org/sdr/ASOA2014072510979.md): Fairing · scratched · Jul 14, 2014 · N846AS · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > LT LOWER HORIZONTAL STABILIZER TO B-STABILIZER FAIRING SCRATCHED IN 3 LOCATIONS. REPAIRED IAW ECTC REO 601R-55-32-315 PERM REPAIR.
- [SDR ASOA2014072510978](https://openairdocs.org/sdr/ASOA2014072510978.md): Seat Track · corroded · Jul 13, 2014 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK SEGEMENT BS 364 - 399.5 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802 AND AMM TASK 53-01-11-400-802.
- [SDR ASOA2014072510977](https://openairdocs.org/sdr/ASOA2014072510977.md): Seat Track · corroded · Jul 13, 2014 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK SEGEMENT BS 399.5- 409+126 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2014072510976](https://openairdocs.org/sdr/ASOA2014072510976.md): Seat Track · corroded · Jul 13, 2014 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGEMENT 399.5 - 409+126 LBL 9, CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA2014072510975](https://openairdocs.org/sdr/ASOA2014072510975.md): Floor Support · corroded · Jul 12, 2014 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR SUPPORT AT BS 349 - 364 JUST AFT OF PAX DOOR REMOVED CORROSION IAW SRM 51-21-06-00. BLENDED AREA IS OUT OF LIMITS IAW REO 601R-53-00-530. REPAIRED IAW EC/TC REO 601R-53-21-2558.
- [SDR ASOA2014072510974](https://openairdocs.org/sdr/ASOA2014072510974.md): Skin · dented · Jul 12, 2014 · N846AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON LT SIDE FUSELAGE UNDER CABIN PRESSURE GROUND AIR SUPPLY DOOR. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-61-5309, PERMANENT REPAIR. RECEIVED AND COMPLIED WITH REO 601R-53-61-5309. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
- [SDR ASOA2014072510973](https://openairdocs.org/sdr/ASOA2014072510973.md): Seat Track · corroded · Jul 8, 2014 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK HAS CORROSION AT BS 424 - 559. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014072510972](https://openairdocs.org/sdr/ASOA2014072510972.md): Seat Track · corroded · Jul 8, 2014 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK HAS CORROSION AT BS 364 - 399.5. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014072510971](https://openairdocs.org/sdr/ASOA2014072510971.md): Floor Support · corroded · Jul 7, 2014 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CABIN FLOOR SUPPORT CORRODED FROM BS 310 - 320. R & R IAW SRM 51-42-13-00 AND DWG 601R38670.
- [SDR ASOA2014072510970](https://openairdocs.org/sdr/ASOA2014072510970.md): Light · failed · Jul 7, 2014 · N846AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT & RIGHT OVERWING EMERGENCY EXIT BETA LIGHT ON HANDLE FAILED FUNCTION TEST. R & R LT & RT OVERWING EMERGENCY EXIT BETA LIGHTS ON HANDLE IAW AMM 33-51-09-000-801.
- [SDR ASOA2014072510980](https://openairdocs.org/sdr/ASOA2014072510980.md): Skin · dented · Jul 5, 2014 · N846AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON LT SIDE FUSELAGE UNDER CABIN PRESSURE GROUND AIR SUPPLY DOOR. REPAIRED IAW REO 601R-53-61-5309. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR ASOA2014042510389](https://openairdocs.org/sdr/ASOA2014042510389.md): Door · binding · Apr 23, 2014 · N846AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WILL NOT STAY OPEN AND IS DIFFICULT TO CLOSE. RECYCLED SERVICE DOOR MECHANISM CLEARED JAMMED DOOR IAW AMM 52-41-03.
- [SDR ASOA2013121109612](https://openairdocs.org/sdr/ASOA2013121109612.md): Lamp · burned out · Dec 8, 2013 · N846AS · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA2013100709156](https://openairdocs.org/sdr/ASOA2013100709156.md): Light · broken · Oct 3, 2013 · N846AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ON FWD SIDE OF PAX DOOR OPENING, BROKEN. R & R EMERGENCY FLOODLIGHT ON WARDROBE IAW VCMM 25-20-52.
- [SDR ASOA2013080608833](https://openairdocs.org/sdr/ASOA2013080608833.md): Fairing · gouged · Aug 4, 2013 · N846AS · Cndair CL6002B19 · Vertical Stabilizer
  > FOUND VERTICAL STAB LT LOWER MIDDLE FAIRING HAS A GOUGE. CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3. REPAIRED IAW REO 601R-55-32-315.
- [SDR ASOA2013080108822](https://openairdocs.org/sdr/ASOA2013080108822.md): Door · unknown · Jul 29, 2013 · N846AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WOULD NOT OPEN. OPENED DOOR AS REQUIRED.
- [SDR ASOA2013062808531](https://openairdocs.org/sdr/ASOA2013062808531.md): Door · unknown · Jun 26, 2013 · N846AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN ENTRANCE DOOR WILL NOT CLOSE OR OPEN. TROUBLESHOT MAIN PAX DOOR - CYCLED DOOR - DOOR OPS CHECKED OK IAW AMM 52-11-00.
- [SDR ASOA2013042903457](https://openairdocs.org/sdr/ASOA2013042903457.md): Handle · fouled · Apr 25, 2013 · N846AS · Cndair CL6002B19 · Passenger/Crew Doors
  > RAMP REPORTS PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. FOUND INNER HANDLE RETENTION MECHANISM JAMMED AND LOCKED WITH DIRT AND DEBRIS. CLEANED AND LUBRICATED RETENTION MECHANISM. PERFORMED OPS CHECKED PAX DOOR IAW AMM 52-11-23.
- [SDR ASOA2013032203249](https://openairdocs.org/sdr/ASOA2013032203249.md): Actuator · unserviceable · Mar 20, 2013 · N846AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WILL NOT OPEN. R & R SERVICE DOOR HANDLE ACTUATOR IAW AMM 52-41-03. OPS TEST GOOD.
- [SDR ASOA2013030503100](https://openairdocs.org/sdr/ASOA2013030503100.md): Handle · binding · Mar 2, 2013 · N846AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR IS HARD TO OPEN. OPS CHECKED GOOD OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03, NO DEFECTS NOTED.
- [SDR ASOA2013020702966](https://openairdocs.org/sdr/ASOA2013020702966.md): Door · binding · Feb 3, 2013 · N846AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. DAMAGE TO AIRFRAME BOTH SIDES OF DOOR AT HANDLE LEVEL. PERFORM OPS CK OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03, BLENDED DAMAGE IAW REO 601R-53-21-024, AND 601R-53-21-160 FOUND TO BE WITHIN LIMITS, ALLODINED PRIMED
- [SDR ASOA2013011102774](https://openairdocs.org/sdr/ASOA2013011102774.md): Lamp · burned out · Jan 7, 2013 · N846AS · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-15, OPS CHECKED GOOD.
- [SDR ASOA2012090402163](https://openairdocs.org/sdr/ASOA2012090402163.md): Lamp · burned out · Aug 31, 2012 · N846AS · Cndair CL6002B19 · Emergency Equipment
  > F/A REPORTS CABIN FLASHLIGHT INOPERATIVE. RELAMPED F/A FLASHLIGHT IAW AMM 26-61-04. SDR CLOSED.
- [SDR ASOA2012083002151](https://openairdocs.org/sdr/ASOA2012083002151.md): Bulkhead Web · cracked · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX.3" IN LENGTH 100 PERCENT FSH. LOCATION TOP OF CARGO DOOR AFT TRACK. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-1541, REV D,
- [SDR ASOA2012083002150](https://openairdocs.org/sdr/ASOA2012083002150.md): Angle · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL ANGLE IS CORRODED. REMOVED PAX DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. RECEIVED NEW SERVICEABLE PAX DOOR SILL ANGLE PN 601R31527-221. LOCATED AND DRILLED FASTENER HOLES IN SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE
- [SDR ASOA2012083002148](https://openairdocs.org/sdr/ASOA2012083002148.md): Floor Support · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AT FS 349.00 AFT OF SERVICE DOOR BEYOND LIMITS. REMOVED DAMAGED SECTION OF SERVICE DOOR FLOOR SUPPORT FROM FS 349.00 TO FS 368.5 IAW REO 601R-53-21-326. COMPLIED WITH REO 601R-53-21-326 & 601R-53-21-2341.
- [SDR ASOA2012083002147](https://openairdocs.org/sdr/ASOA2012083002147.md): Sill · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL HAS 1 EA FASTENER HOLE WITH MINOR CORROSION AROUND RIVET THAT ATTACHES TO NUTPLATE AT FS 589.00+6 AT LBL 45. FOUND CARGO DOOR LOWER SILL CORRODED BEYOND LIMITS IAW SRM 53-00-00. REMOVED DAMAGED SILL IAW SRM 51-42-06, 51-42-10 AND 51-42-
- [SDR ASOA2012083002146](https://openairdocs.org/sdr/ASOA2012083002146.md): Floor Support · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY FLOOR SUPPORT AT LBL 27 HAS MULTIPLE FASTENER HOLES WITH PITTING CORROSION FROM FS 559.00+112 THROUGH 621.00. FOUND FLOOR SUPPORT BEYOND LIMITS IAW SRM 53-00-00. REMOVED DAMAGED CAP FROM LBL 27 FS 559+112 -621.00 IAW SRM 51-42-06 AND 51-42-21. DRI
- [SDR ASOA2012083002145](https://openairdocs.org/sdr/ASOA2012083002145.md): Cargo Track · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 9 FS 559.00+112 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED CARGO TRACK, INSTALLED NEW CARGO TRACK. WORK PERFORMED IAW AMM 53-01-11-000-802/53-01-11-400-802.
- [SDR ASOA2012083002144](https://openairdocs.org/sdr/ASOA2012083002144.md): Seat Track · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FS 559.00+85, RBL 9 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED FLOOR TRACK AT FS 559.00+85, RBL 9 IAW AMM TASK 53-01-11-000-802. FABRICATED NEW FLOOR TRACK IAW REO 601R-53-00-478. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2012083002143](https://openairdocs.org/sdr/ASOA2012083002143.md): Floor Support · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00+80 -559.00+96 HAS 4 EA FASTENER HOLES WITH CORROSION AT LBL 45 ON FLOOR SUPPORT. BLEND THE CORROSION IAW SRM 51-21-06. REMOVED.006" MATERIAL THICKNESS, LT.057". COMPLIED WITH REO 601R-53-51-196. FOUND TO BE SATISFACTORY.
- [SDR ASOA2012083002142](https://openairdocs.org/sdr/ASOA2012083002142.md): Floor Support · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT SERVICE DOOR ENTRANCE CORRODED BEYOND LIMITS BETWEEN FS 319 AND FS 349.0 AT WL 73.5 IAW TASK 000-53-900-509. REMOVED FLOOR SUPPORT ANGLE ASSY AT SERVICE DOOR ENTRANCE BETWEEN FS 319 AND FS 349 IAW SRM 51-42-21, 51-42-06 AND 51-42-13. I
- [SDR ASOA2012082902137](https://openairdocs.org/sdr/ASOA2012082902137.md): Floorbeam · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 349.0 WL 73.5 CORRODED BEYOND LIMITS FROM RBL 27 TO RBL 36 IAW TASK 000-53-900-509. REPAIRED IAW REO 601R-53-21-2342.
- [SDR ASOA2012082902136](https://openairdocs.org/sdr/ASOA2012082902136.md): Floor Support · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD FLOOR SUPPORT AND GALLEY SUPPORT PLATE LOCATED AT RBL 35 FROM FS 295 TO FS 319 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED CORRODED FLOOR SUPPORT & GALLEY SUPPORT PLATE FROM FS 310 TO FS 319, RBL 36 AND REPLACED WITH SERVICEABLE FLOOR SUPPO
- [SDR ASOA2012082902135](https://openairdocs.org/sdr/ASOA2012082902135.md): Tee Fitting · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FWD AND AFT TEE FITTINGS AT SERVICE DOOR ENTRANCE ARE CORRODED BEYOND LIMITS, LOCATED AT FS 319 AND FS 349 WL 73.5 IAW TASK 000-53-900-509. REMOVED CORRODED T FITTING AT FS 349, WL 73.5 IAW SRM 51-42-21. LOCATED AND DRILLED NEW T-FITTING AT FS 349, WL 73.5 I
- [SDR ASOA2012082902134](https://openairdocs.org/sdr/ASOA2012082902134.md): Attach Fitting · corroded · Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR LWR SILL ATTACHMENT CLIP LOCATED AT FS 349 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-42-06 & SRM 51-42-21. LOCATED & DRILLED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-40
- [SDR ASOA2012082902133](https://openairdocs.org/sdr/ASOA2012082902133.md): Floorbeam · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > IN PASSENGER COMPARTMENT BELOW FLOOR AT FS 280.00 ON RBL 9.00 AND LBL 9.00, INBD ATTACHMENT ANGLES ARE CRACKED. REMOVED THE CRACKED ATTACHMENT ANGLE AT FS 280.00 ON RBL 9.00 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ATTACHMENT ANGLE (PN 601R31113-58) AT F
- [SDR ASOA2012082902132](https://openairdocs.org/sdr/ASOA2012082902132.md): Isolator · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 REAR PRESSURE BULKHEAD HAS AN ISOLATOR BROKEN. REMOVED ISOLATOR, LOCATED HOLES IN NEW BRACKET AND INSTALLED USING MS20470AD5-5. ALL WORK PERFORMED IAW SRM 51-42-06.
- [SDR ASOA2012082902131](https://openairdocs.org/sdr/ASOA2012082902131.md): Angle · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 484.00 INTERCOSTAL ANGLE AT LBL 9 IS CRACKED.5" LONG IN UPPER RADIUS. INSTALLED A NEW ANGLE 601R31171-27 PO W17821 IAW AMM 51-42-21.
- [SDR ASOA2012082902130](https://openairdocs.org/sdr/ASOA2012082902130.md): Intercostal · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 460.00 INTERCOSTAL IS CRACKED AT LBL 9 SECOND RIVET DOWN.5" LONG. CUT AWAY DAMAGE ON INTERCOSTAL WEB AS SHOWN IN REO 601R-53-41-1600 FIG 2 SHEET 2 TO STEP 1 & 2. FABRICATED DOUBLER & FILLER IAW REO 601R-53-41-1600 IAW SRM 51-21-16 TO STEPS 4 OF REO.
- [SDR ASOA2012082902129](https://openairdocs.org/sdr/ASOA2012082902129.md): Angle · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IS CRACKED.5 INCHES LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT LBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-17 IAW SRM 51-42-21. PAINTED FASTENERS ON REPAIRED AREA IAW SRM 51-25-01, APPLIED WATER DISPLA
- [SDR ASOA2012082902128](https://openairdocs.org/sdr/ASOA2012082902128.md): Angle · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FS 484.00 INTERCOSTAL ANGLE AT RBL 27 IS CRACKED.5" LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT RBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-9 IAW SRM 51-42-21. TOUCHED UP REPAIR FASTENERS IAW SRM 51-25-01. APPLIED WATER DISPLACING CORRO
- [SDR ASOA2012082902127](https://openairdocs.org/sdr/ASOA2012082902127.md): Attach Angle · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 162EL VERTICAL ATTACHMENT ANGLE IS CRACKED FS 469.53. REMOVED DAMAGED RT UPPER WING VERTICAL ATTACHMENT ANGLE & REPLACED W/NEW SERVICEABLE ANGLE PN IAW SRM 51-42-13 & 51-42-06.
- [SDR ASOA2012082902126](https://openairdocs.org/sdr/ASOA2012082902126.md): Attach Angle · cracked · Aug 8, 2012 · N846AS · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 161EL VERTICAL ATTACHMENT ANGLE IS CRACKED. LOCATED & DRILLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET UNDER ACCESS PANEL 161EL ON L
- [SDR ASOA2012083002141](https://openairdocs.org/sdr/ASOA2012083002141.md): Skin · cracked · Aug 7, 2012 · N846AS · Cndair CL6002B19 · Wing, Plate/Skin
  > EXTERIOR SURFACE OF LOWER RT WING PLANK T/E AT WS 148.019 IS CRACKED APPROX 1.0 LONG. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131 REV A.
- [SDR ASOA2012083002140](https://openairdocs.org/sdr/ASOA2012083002140.md): Skin · cracked · Aug 7, 2012 · N846AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING LOWER PLANK IS CRACKED.235" LONG OTBD OF JACK PAD PLUG AT WS 148.019 T/E. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A DATED 08/29/2011 AS WRITTEN. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130 REV.J.

Next page: https://openairdocs.org/deregistered/N846AS-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 = 'N846AS' AND deregistration_id = 'N846AS-2017-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N846AS-2017-06-01/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
