# Service difficulty reports: N839AS, cancelled Jun 8, 2017

A list on [N839AS, cancelled Jun 8, 2017](https://openairdocs.org/deregistered/N839AS-2017-06-08.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 · 185 reports

- [SDR ASOA2015060513053](https://openairdocs.org/sdr/ASOA2015060513053.md): Door · lack of lube · Jun 4, 2015 · N839AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DIFFICULT TO OPEN. LUBED AND CLEANED PAX DOOR IAW AMM 12-20-52. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED, ACFT OK FOR RETURN TO SERVICE. OK FOR SERVICE.
- [SDR ASOA2015060513051](https://openairdocs.org/sdr/ASOA2015060513051.md): Handle · lack of lube · Jun 1, 2015 · N839AS · Cndair CL6002B19 · Passenger/Crew Doors
  > UNABLE TO CLOSE DOOR, PASSENGER DOOR STOW CAUTION APPEARS AND UNABLE TO OPEN FROM INSIDE. LUBRICATED PASSENGER DOOR STOW HANDLE, CYCLED DOOR OPEN AND CLOSE IAW AMM 52-11-00. DOOR OPEN AND CLOSES NORMAL.
- [SDR ASOA2015021912250](https://openairdocs.org/sdr/ASOA2015021912250.md): Lamp · burned out · Feb 16, 2015 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > INTERIOR CABIN EMERGENCY EXIT SIGN WILL NOT LIGHT UP. REPLACED THE LAMP IAW AMM 33-51-14.
- [SDR ASOA2013101109209](https://openairdocs.org/sdr/ASOA2013101109209.md): Skin · cracked · Sep 29, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT LT TRU DOOR AFT LATCH. R & R SKIN IAW SRM 51-40-11, 51-42-06-00, 51-42-10-00 AND REO 601R-53-11-2563, REO 601R-53-11-2572 AND DWG 600-33052. CLASSIFIED A MAJOR REPAIR.
- [SDR ASOA2013101109208](https://openairdocs.org/sdr/ASOA2013101109208.md): Fitting · cracked · Sep 27, 2013 · N839AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LEFT MLG TRUNNION FITTING HAS TWO LOWER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-21-2002.
- [SDR ASOA2013100809185](https://openairdocs.org/sdr/ASOA2013100809185.md): Hinge · gouged · Sep 25, 2013 · N839AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > FOUND GOUGE DAMAGE ON DOOR SIDE OF ASD HINGE. BLENDED OUT GOUGE DAMAGE IAW SRM 51-12-00. MAJOR REPAIR.
- [SDR ASOA2013101109207](https://openairdocs.org/sdr/ASOA2013101109207.md): Fitting · cracked · Sep 22, 2013 · N839AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LEFT MLG TRUNNION FITTING HAS TWO LOWER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-57-21-2002 IAW NDTM PT6, 53-00-97.
- [SDR ASOA2013101109205](https://openairdocs.org/sdr/ASOA2013101109205.md): Skin · damaged · Sep 21, 2013 · N839AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK HAS TWO OVERSIZED HOLES. REPAIRED IAW REO 601R-57-21-2002 REV.P1.
- [SDR ASOA2013101109204](https://openairdocs.org/sdr/ASOA2013101109204.md): Skin · damaged · Sep 20, 2013 · N839AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK HAS ONE OVERSIZED HOLE. REPAIRED IAW REO 601R-52-21-2002, REV P1.
- [SDR ASOA2013100809184](https://openairdocs.org/sdr/ASOA2013100809184.md): Bulkhead · cracked · Sep 18, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB FWD FACE CRACKED ABOVE AFT CARGO DOOR TRACK AREA IS MARKED. COMPLIED WITH REO 601R-53-61-1541, REV D, DATED OCT 31, 2011 IAW NDTM PART 1 51-20-06 FOR BULKHEAD WEB.
- [SDR ASOA2013101109203](https://openairdocs.org/sdr/ASOA2013101109203.md): Floor Support · corroded · Sep 17, 2013 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CABIN FLOOR SUPPORT CORRODED BS 349 TO 364. REPAIRED IAW SRM 51-21-06-00 AND REO 601R-53-00-530. MAJOR REPAIR.
- [SDR ASOA2013100809183](https://openairdocs.org/sdr/ASOA2013100809183.md): Sign · inoperative · Sep 17, 2013 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR FAILED FUNCTIONAL TEST OF THE EXIT SIGN BETA LIGHT. REMOVED AND INSTALLED SERVICEABLE EXIT SIGN BETA LIGHT ON SERVICE DOOR IAW AMM 33-61-09-000-802, 33-51-09-400-802. FUNCTIONAL TEST GOOD OF SERVICE DOOR EXIT SIGN BETA LIGHT REF AMM TASK 33-51-0
- [SDR ASOA2013100809182](https://openairdocs.org/sdr/ASOA2013100809182.md): Light · failed · Sep 17, 2013 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR FAILED FUNCTIONAL TEST OF THE EXIT SIGN BETA LIGHT. REMOVED AND INSTALLED SERVICEABLE BETA LIGHT EXIT SIGN ON PAX DOOR IAW AMM 33-51-09-000-801, 33-51-09-400-801.
- [SDR ASOA2013101109202](https://openairdocs.org/sdr/ASOA2013101109202.md): Crossbeam · corroded · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON END OF CROSSBEAM AT BS 349.00, RBL 45. REMOVED CORROSION IAW SRM 51-21-06-00.
- [SDR ASOA2013100809181](https://openairdocs.org/sdr/ASOA2013100809181.md): Floor Support · corroded · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-01 AND INSTALLED IAW SRM 51-42-06 AND DWG 601R 31527. MAJOR REPAIR.
- [SDR ASOA2013100809180](https://openairdocs.org/sdr/ASOA2013100809180.md): Bracket · corroded · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT BRACKET IAW SRM 51-42-06-01. INSTALLED BRACKET IAW SRM 51-42-06, SRM 51-40-11 AND DWG 601R 31527. MAJOR REPAIR.
- [SDR ASOA2013100809179](https://openairdocs.org/sdr/ASOA2013100809179.md): Hinge · gouged · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE ON FUSELAGE HAS SEVERAL NICKS AND GOUGED. BLENDED OUT NICKS AND GOUGES ON PAX DOOR HINGE FUSELAGE SIDE AND ADDITIONAL GOUGE DAMAGE ON DOOR HINGE SIDE IAW SRM 51-12-00. RECEIVED AND COMPLIED WITH REO 601R-53-21-2464. MAJOR REPAIR
- [SDR ASOA2013100809178](https://openairdocs.org/sdr/ASOA2013100809178.md): Floor Support · corroded · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AROUND NUT PLATES AT RBL 45 FS 310 TO 319. REMOVED CORROSION IAW SRM 51-21-06-00. COMPLIED WITH REO 601R-53-00-530.
- [SDR ASOA2013100809177](https://openairdocs.org/sdr/ASOA2013100809177.md): Floorbeam · cracked · Sep 16, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ON LBL9 OTBD ANGLE CRACKED ON BS 280 FLOORBEAM, REMOVED CRACKED ANGLE IAW SRM 51-42-21-00. COMPLIED WITH REO 601R-53-11-926, REV B. IAW NDTM PART 1, 51-20-06. INSTALLED NEW ANGLE IAW SRM 51-42-21-00. COMPLIED WITH EC/TC REO 601R-53-11-926 01.
- [SDR ASOA2013101109201](https://openairdocs.org/sdr/ASOA2013101109201.md): Frame · corroded · Sep 15, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 394 CORRODED ON FWD FACE APPROX RBL 3. REMOVED CORROSION IAW SRM 51-21-06.
- [SDR ASOA2013100809176](https://openairdocs.org/sdr/ASOA2013100809176.md): Seat Track · damaged · Sep 14, 2013 · N839AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HOLES ELONGATED. REMOVED INBD SEAT TRACK IAW SB601R-53-22, PART A. REWORKED SEAT TRACK FIG 1(1)(A)-(R). SEAT TRACK REMOVED IAW SB 60R-12-022, FIG 1 (1A) THRU (R AND INSTALLED IAW SB 601R-53-022. MAJOR REPAIR.
- [SDR ASOA2013101109212](https://openairdocs.org/sdr/ASOA2013101109212.md): Skin · cracked · Sep 13, 2013 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND CRACK IN SKIN AT LT TRU DOOR AFT LATCH. R & R SKIN IAW SRM 51-42-06.
- [SDR ASOA2012112602510](https://openairdocs.org/sdr/ASOA2012112602510.md): Skin · cracked · Nov 22, 2012 · N839AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK.325" LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. REPAIRED IAW EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J.
- [SDR ASOA2012112602509](https://openairdocs.org/sdr/ASOA2012112602509.md): Skin · cracked · Nov 22, 2012 · N839AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK.325 LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. STOP DRILLED CRACK TO.250" IAW REO 601R-57-21-138, REV A.
- [SDR ASOA2012110902454](https://openairdocs.org/sdr/ASOA2012110902454.md): Light · unknown · Nov 5, 2012 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST. DISCREPANCY NO LONGER EXISTS. IAW MCC, NO FURTHER ACTION IS REQUIRED.
- [SDR ASOA2012102602401](https://openairdocs.org/sdr/ASOA2012102602401.md): Light · inoperative · Oct 24, 2012 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT EMERGENCY LIGHT INOPERATIVE. R & R LT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA201200024](https://openairdocs.org/sdr/ASOA201200024.md): Flashlight · inoperative · Jan 3, 2012 · N839AS · Cndair CL6002B19 · Emergency Equipment
  > F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 25-61-02 CHECKED GOOD.
- [SDR ASOA201101967](https://openairdocs.org/sdr/ASOA201101967.md): Light · miswired · Oct 14, 2011 · N839AS · Cndair CL6002B19 · Light System Wiring
  > LOWER OTBD EMERGENCY LIGHT ON F/A STATION DOES NOT WORK. FOUND WIRES SWAPPED BETWEEN EMERGENCY LIGHT DS9LY AND DS10LY PUT INPUT WIRES BACK TO THEIR CORRECT LOCATION IAW WDM 33-51-00. OPS TESTED GOOD.
- [SDR ASOA201101884](https://openairdocs.org/sdr/ASOA201101884.md): Seat Track · corroded · Oct 8, 2011 · N839AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. TRIMMED, FITTED AND INSRALLED SEAT TRACK IAW SRM 51-40-11 AND AMM 53-01-11-400-802 AT FS 574, RBL9.
- [SDR ASOA201101857](https://openairdocs.org/sdr/ASOA201101857.md): Pressure Blkhd · cracked · Oct 5, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LENTEL ATTACH POINT AREA. REPAIRED IAW REO 601R-53-61-1230 AND GREO 601R-53-61-1230 REV E.
- [SDR ASOA201101848](https://openairdocs.org/sdr/ASOA201101848.md): Floorbeam · corroded · Oct 3, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM JUST AFT OF SERVICE DOOR CORRODED. HAND SANDED MINOR SURFACE CORROSION. REMOVED.001 OUT.053 THK IAW SRM 51-21-06 AND RESTORED FINISH IAW SRM 51-21-16. R & R FLOORBEAM ANGLE IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS MINOR.
- [SDR ASOA201101941](https://openairdocs.org/sdr/ASOA201101941.md): Skin · dented · Sep 30, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTS BELOW CARGO DOOR AT FS 589 S21-22L. INSTALLED REPAIR DOUBLER. SEALED, PAINTED & APPLIES CORROSION INHIBITER IAW SRM 53-00-31.
- [SDR ASOA201101881](https://openairdocs.org/sdr/ASOA201101881.md): Bracket · corroded · Sep 26, 2011 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION FOUND AT SERVICE DOOR SILL FRAME BRACKETS AT FS 320.0, 345.0 AND 348.0. REMOVED CORROSION AT SERVICE DOOR SILL FRAMES BRACKET IAW SRM 51-21-6. PERFORMED UT THICKNESS INSP OF BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING
- [SDR ASOA201101816](https://openairdocs.org/sdr/ASOA201101816.md): Floor Panel · corroded · Sep 26, 2011 · N839AS · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION FOUND AT PRESSURE FLOOR LT LBL 36, STR 17 OVERWING EXIT AND AFT AT FOLLOWING FS 424-559. REPAIRED IAW REO 601R-53-41-666.
- [SDR ASOA201101792](https://openairdocs.org/sdr/ASOA201101792.md): Stiffener · cracked · Sep 23, 2011 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > POSSIBLE CRACK ON STIFFENER LBL18.00 AT FS409.00+128 INDICATION IS AT THE VERY BOTTOM ON THE OTBD. COMPLY WITH EC/TC REO 601R-53-41-056. RT 161728 09/23/11 (LT) COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-51-056, REV-E. RII FOUND TO BE SATISFACTOR
- [SDR ASOA201101781](https://openairdocs.org/sdr/ASOA201101781.md): Pressure Blkhd · cracked · Sep 21, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT. REPAIRED IAW REO 601R-53-61-1230 AND REO 601R-53-61-4218.
- [SDR ASOA201101796](https://openairdocs.org/sdr/ASOA201101796.md): Pressure Blkhd · cracked · Sep 20, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD HAS A CRACK ABOVE LINTEL. REPAIRED.
- [SDR ASOA201101763](https://openairdocs.org/sdr/ASOA201101763.md): Light · cracked · Sep 20, 2011 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT AISLE EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED IAW AMM 33-51-01-01, REV A 161954 10-7-11.
- [SDR ASOA201101762](https://openairdocs.org/sdr/ASOA201101762.md): Pressure Deck · corroded · Sep 20, 2011 · N839AS · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION FOUND AT PRESSURE FLOOR FS 424-559 LBL 36, STR 17. REMOVED COSSOSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSP PROCEDURE UT-3 MIN. MATERIAL REMAINING IS.071" WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666.
- [SDR ASOA201101761](https://openairdocs.org/sdr/ASOA201101761.md): Web · corroded · Sep 20, 2011 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB ON OTBD SIDE OF LBL 27 CORRODED BETWEEN FS 585-605. BLENDED IAW 51-12-00 AND FOUND TO BE OUT LIMITS IAW 53-00-00. REMOVED AND REPLACED WEB IAW SRM 51-40-06, 51-40-11, 51-42-06 AND SRM 51-42-21.
- [SDR ASOA201101747](https://openairdocs.org/sdr/ASOA201101747.md): Bulkhead · cracked · Sep 16, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT AREA. REPAIRED IAW 601R-53-61-1230.
- [SDR ASOA201101746](https://openairdocs.org/sdr/ASOA201101746.md): Stiffener · cracked · Sep 16, 2011 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > POSSIBLE CRACK ON STIFFENER, LBL 18.00 AT FS 409.00+128 INDICATION IS AT THE VERY BOTTOM ON THE OTBD. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSP PROCEDURE ET-2. STIFFENER CONFIRMED CRACKED AT BOTTOM, AFT, OTBD END OF POST. REPAIRED IAW REO 601R-53-4
- [SDR ASOA201101889](https://openairdocs.org/sdr/ASOA201101889.md): Floorbeam · corroded · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED. REMOVED FLOORBEAM CAP IAW SRM 51-42-21. DRILL AND INSTALL NEW CAP IAW SRM 51-42-06 AND REO 601R-53-61-3778.
- [SDR ASOA201101740](https://openairdocs.org/sdr/ASOA201101740.md): Seat Track · corroded · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. CORROSION REMOVAL WITHIN LIMITS IAW SRM 53-61-49.
- [SDR ASOA201101739](https://openairdocs.org/sdr/ASOA201101739.md): Skin · corroded · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT EXTERIOR SKIN PANEL AT FS 559.00 + 64 AND BETWEEN STR 14A AND 15A HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06. TREATED, PRIMED AND PAINTED REPAIR AREA IAW SRM 51-21-11.
- [SDR ASOA201101738](https://openairdocs.org/sdr/ASOA201101738.md): Support Bracket · cracked · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT WINDSHIELD SIDE POST LOWER OTBD SUPPORT BRACKET CRACKED. REMOVED OLD SUPPORT BRACKET. LOCATED, DRILLED AND INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21.
- [SDR ASOA201101737](https://openairdocs.org/sdr/ASOA201101737.md): Isolator · cracked · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CARGO COMPARTMENT AFT PRESSURE BULKHEAD MOUNTING ISOLATOR CRACKED. R & R CRACKED ISOLATOR IAW SRM 51-40-11. MINOR REPAIR.
- [SDR ASOA201101736](https://openairdocs.org/sdr/ASOA201101736.md): Placard · missing · Sep 14, 2011 · N839AS · Cndair CL6002B19 · Placards and Markings
  > COCKPIT EMERGENCY EXIT MISSING PLACARD. R & R PLACARD IAW AMM'S 11-20-00-000-801 & 11-10-03-400-801.
- [SDR ASOA201101394](https://openairdocs.org/sdr/ASOA201101394.md): Flashlight · inoperative · Jul 28, 2011 · N839AS · Cndair CL6002B19 · Emergency Equipment
  > COPILOT FLASHLIGHT DOES NOT WORK. R & R F/O'S FLASHLIGHT IAW AMM 25-60-01.
- [SDR ASOA201100621](https://openairdocs.org/sdr/ASOA201100621.md): Lamp · burned out · Mar 26, 2011 · N839AS · Cndair CL6002B19 · Emergency Lighting
  > CABIN CEILING EMERGENCY LIGHT 3 FROM FRONT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT 3RD FROM THE FRONT IAW CMM 33-22-89. OPS CK GOOD. RELAMPED CABIN CEILING EMERGENCY LIGHT 3RD FROM THE FRONT IAW CMM 33-22-89. OPS CHK GOOD.

Next page: https://openairdocs.org/deregistered/N839AS-2017-06-08/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 = 'N839AS' AND deregistration_id = 'N839AS-2017-06-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N839AS-2017-06-08/reports

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