# Service difficulty reports: N840AS, cancelled Mar 20, 2018

A list on [N840AS, cancelled Mar 20, 2018](https://openairdocs.org/deregistered/N840AS-2018-03-20.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 · 186 reports

- [SDR ASOA2015051912855](https://openairdocs.org/sdr/ASOA2015051912855.md): Light · intermittent · May 15, 2015 · N840AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INTERMITTENT, F/A'S SWITCH WAS IN THE ON POSITION. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS TEST GOOD.
- [SDR ASOA2014111311639](https://openairdocs.org/sdr/ASOA2014111311639.md): Isolator · cracked · Nov 8, 2014 · N840AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD, INSOLATORS ARE CRACKED. R & R THE DAMAGED ISOLATORS IAW SRM 51-42-06.
- [SDR ASOA2014090311176](https://openairdocs.org/sdr/ASOA2014090311176.md): Fitting · worn · Aug 29, 2014 · N840AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP ALIGNMENT FITTING, HAS WEAR DAMAGE DUE TO ROLLER FITTING ASSY CONTACT. AFTER ATTEMPT TO APPLY GREO 601R-57-51-143 REPAIRS, IT WAS FOUND THAT FURTHER EVALUATION OF DAMAGE IS REQUIRED. BLENDED OUT DAMAGE ON LT FLAP ALIGNMENT FITTING IAW REO 60
- [SDR ASOA2013122709708](https://openairdocs.org/sdr/ASOA2013122709708.md): Charger · inoperative · Dec 19, 2013 · N840AS · Cndair CL6002B19 · Emergency Lighting
  > DURING OPS CHECK OF EMERGENCY LIGHTS FOUND NR 1 CEILING FLOOD LIGHT INOPERATIVE. R & R NR 1 CHARGER ASSY IAW AMM 33-51-05-000-801, 33-51-05-400-801. OPS CHECKED GOOD IAW AMM 33-51-04-740-801.
- [SDR ASOA2013122709707](https://openairdocs.org/sdr/ASOA2013122709707.md): Wire · broken · Dec 18, 2013 · N840AS · Cndair CL6002B19 · Light System Wiring
  > DURING OPS TEST OF THE EMERGENCY EXIT LIGHTS THE FLOOR PROXIMITY LIGHT ON THE WARDROBE WOULD NOT ILLUMINATE. FOUND BROKEN WIRE ON CONNECTOR P13LY. INSTALLED NEW CONNECTOR IAW ESPM 20-17-31. OPS CHECK GOOD IAW AMM 33-51-00-710-801.
- [SDR ASOA2013122709706](https://openairdocs.org/sdr/ASOA2013122709706.md): Bulkhead Web · cracked · Dec 11, 2013 · N840AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED AT BL 0 APPROX 8 INCHES BELOW WL 120.43. COMPLIED WITH ECTC REO 601R-53-61-1274 AND MET ALL REQUIREMENTS OF REO 601R-53-61-1285 REV D. MAJOR REPAIR.
- [SDR ASOA2013122709705](https://openairdocs.org/sdr/ASOA2013122709705.md): Floorbeam · corroded · Dec 7, 2013 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON RBL 9 FLOORBEAM AT BS 409. FOUND OUT OF LIMITS IAW SRM TR 53-27. REPAIRED IAW REO 601R-53-31-807 AND SRM 51-42-06, 51-42-15 51-42-20 AND 51-42-34.
- [SDR ASOA2013122709709](https://openairdocs.org/sdr/ASOA2013122709709.md): Angle · cracked · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD PAX DOOR ANCHOR FITTING FWD ANGLE CRACKED. REPLACED ANCHOR FITTING ASSY IAW AMM 52-11-17-400-801 AND AMM SUPPLEMENT 52-11-17, REV C.
- [SDR ASOA2013122709704](https://openairdocs.org/sdr/ASOA2013122709704.md): Sill · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MINOR CORROSION AROUND THE FASTENER HOLES ON THE RT SILL PLATE BETWEEN BS 559+80 - 521. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526 REV. MAJOR REPAIR.
- [SDR ASOA2013122709703](https://openairdocs.org/sdr/ASOA2013122709703.md): Sill · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MINOR CORROSION AROUND THE SCREW HOLES BETWEEN FS 559+64 - 559+80 ON SILL PLATE RT SIDE. COMPLIED WITH ECTC REO 601R-55-00-526-01 AND GREO 601R-53-00-526 REV. MAJOR REPAIR
- [SDR ASOA2013122709702](https://openairdocs.org/sdr/ASOA2013122709702.md): Seat Track · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 394-409 + 128. COMPLIED IAW REO 601R-53-00-485.
- [SDR ASOA2013122709701](https://openairdocs.org/sdr/ASOA2013122709701.md): Floor Support · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT HAS CORROSION RBL 45. BLENDED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM TR 53-27. REPAIRED IAW EA 20-2013-144.
- [SDR ASOA2013122709700](https://openairdocs.org/sdr/ASOA2013122709700.md): Retainer · bent · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ASD SEAL AT DOOR HINGE AFT SEAL RETAINER IS BENT OVER ON TOP OF THE SEAL. REMOVED SEAL RETAINER IAW SRM 51-42-13. COMPLIED WITH ECTC REO 601R-52-11-915 IAW REO 601R-52-11-915. MAJOR REPAIR.
- [SDR ASOA2013121309631](https://openairdocs.org/sdr/ASOA2013121309631.md): Cargo Track · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 9 BS 574 TO 559+112 HAS MINOR CORROSION. REMOVED AND INSTALLED NEW SERVCIABLE CARGO TRACK IAW SRM 51-41-02.
- [SDR ASOA2013121309630](https://openairdocs.org/sdr/ASOA2013121309630.md): Seat Track · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 364-394. REPAIRED IAW REO 601R-53-00-485.
- [SDR ASOA2013121309629](https://openairdocs.org/sdr/ASOA2013121309629.md): Seat Track · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 394-409 + 128 REPAIRED IAW REO 601R-53-00-485.
- [SDR ASOA2013121309628](https://openairdocs.org/sdr/ASOA2013121309628.md): Seat Track · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION FROM BS 364-394. REPAIRED IAW REO 601R-53-00-482 AND 601R-53-00-485.
- [SDR ASOA2013121309627](https://openairdocs.org/sdr/ASOA2013121309627.md): Pressure Panel · corroded · Dec 3, 2013 · N840AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT SIDE PRESSURE FLOOR OVER WING BOX HAS CORROSION BS 439-529. REPAIRED IAW EC/TC REO 601R-53-41-660-01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.
- [SDR ASOA2013122709699](https://openairdocs.org/sdr/ASOA2013122709699.md): Skin · dented · Dec 1, 2013 · N840AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THERE IS A DENT ABOVE THE AFT EQUIPMENT BAY AT FS 654.5 - 672.5, S0 TO S1R. APPEARS TO HAVE BEEN PREVIOUSLY FILLED WITH FILLER. ACCOMPLISHED REPAIR PROCEDURES 4A1 THRU 3.5 AND 8 (7 IS N/A) OF SRM 53-00-31, REPAIR NR 3. MAJOR REPAIR
- [SDR ASOA2013072408764](https://openairdocs.org/sdr/ASOA2013072408764.md): Glowstrip · missing · Jul 21, 2013 · N840AS · Cndair CL6002B19 · Emergency Equipment
  > PHOTOLUMINSCENT STRIP, ROW 1AB HAS COME OFF. INSTALLED NEW 2 WAY TAPE ON PHOTOLUMINACENT STRIP IAW AMM 25-60-01. OK FOR SVC.
- [SDR ASOA2013031503204](https://openairdocs.org/sdr/ASOA2013031503204.md): Flashlight · inoperative · Mar 11, 2013 · N840AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-61-00.
- [SDR ASOA2012113002588](https://openairdocs.org/sdr/ASOA2012113002588.md): Fire Loop · malfunctioned · Nov 29, 2012 · N840AS · Cndair CL6002B19 · Fire Detection
  > RECEIVED LT 14TH DUCT WARNING MESSAGE AT FL 280. RAN QRH PROCEDURE AND MESSAGE DID NOT EXTINGUISH. EMERGENCY DECLARED, LANDED AND MESSAGE FINALLY WENT OUT PRIOR TO LANDING AT AROUND 10000 MFL. R & R LT PYLON LOOP A59WK ASSY IAW AMM-36-21-04. PERFORMED OPS
- [SDR ASOA2012071601907](https://openairdocs.org/sdr/ASOA2012071601907.md): Sensor · broken · Jul 11, 2012 · N840AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE ON TAKEOFF. ASSOCIATED MESSAGE: WOW INPUT CAUTION, WOW OUTPUT FAIL STATUS, NOSE DOOR POEN WARNING. A/C RETURNED TO DEPARTURE AFTER TAKEOFF, EMERGENCY DECLARED. TROUBLESHOOTING FOUND BOTH NLG DOWNLOCK PROXIMITY SENSORS BROKEN.
- [SDR ASOA2012071801928](https://openairdocs.org/sdr/ASOA2012071801928.md): Priority Valve · failed · Jul 10, 2012 · N840AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF AND AFTER SELECTING LANDING GEAR HANDLE UP, MLG CAME UP NOSE DID NOT EICAS MESSAGE POSTED ON ED1 TOP TO BOTTOM. NOSE DOOR OPEN WARNING, GEAR DISAGREE WOW INPUT CAUTION, STEERING INOPERATIVE CAUTION ON ED2, WOW OUTPUT FAIL STATUS QRH FOLLOWED TO
- [SDR ASOA201201772](https://openairdocs.org/sdr/ASOA201201772.md): Ballast · overheated · Jun 6, 2012 · N840AS · Cndair CL6002B19 · Passenger Compartment Lighting
  > COCKPIT FILLED WITH ELECTRICAL FUMES IN FLIGHT. CONSISTENT DISPERSION INCREASE AND DECREASE WITH THRUST LEVERS, EMERGENCY DECLARED, DIVERTED. FOUND GALLEY LIGHT BALLAST OVERHEATED. R & R LIGHT BALLAST IAW AMM 33-26-05.
- [SDR ASOA201200263](https://openairdocs.org/sdr/ASOA201200263.md): Floorbeam · corroded · Jan 24, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RT SIDE FS 349 FLOORBEAM CORRODED ON OTBD END. REPAIRED IAW REO 601R-53-21-2255.
- [SDR ASOA201200216](https://openairdocs.org/sdr/ASOA201200216.md): Frame · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FACE OF FRAME, UNDER AVIONICS FLOORBOARD AT FS 319.70 APPEARS TO HAVE CORROSION UNDER PAINT.
- [SDR ASOA201200214](https://openairdocs.org/sdr/ASOA201200214.md): Seat Track · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK CORRODED BETWEEN FS 399.5 & FS 409+32.
- [SDR ASOA201200212](https://openairdocs.org/sdr/ASOA201200212.md): Seat Track · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK CORRODED FROM FS 364 TO FS 399.50.
- [SDR ASOA201200210](https://openairdocs.org/sdr/ASOA201200210.md): Frame · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE OF FRAME, UNDER AVIONICS FLOORBOARD AT FS 349.0. APPEARS TO HAVE CORROSION UNDER PAINT. (CLOSED)
- [SDR ASOA201200208](https://openairdocs.org/sdr/ASOA201200208.md): Angle · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SUPPORT SILL ANGLE CORRODED.
- [SDR ASOA201200206](https://openairdocs.org/sdr/ASOA201200206.md): Angle · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE IS CORRODED BEYOND LIMITS AT FWD END. (SDR CLOSED)
- [SDR ASOA201200204](https://openairdocs.org/sdr/ASOA201200204.md): Floorbeam · corroded · Jan 18, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RT SIDE FS 349 FLOORBEAM IS CORRODED ON OTBD END.
- [SDR ASOA201200184](https://openairdocs.org/sdr/ASOA201200184.md): Structure · cracked · Jan 17, 2012 · N840AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR EDGE MEMBER CRACKED AFT SIDE. REPAIRED IAW REO 601R-52-11-279.
- [SDR ASOA201200183](https://openairdocs.org/sdr/ASOA201200183.md): Floorbeam · corroded · Jan 17, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 FLOORBEAM IS CORRODED ON OTBD END. REPAIRED IAW REO 601R-53-21-2250.
- [SDR ASOA201200173](https://openairdocs.org/sdr/ASOA201200173.md): Angle · cracked · Jan 16, 2012 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 621-625 OBLIQUE ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-21.
- [SDR ASOA201200172](https://openairdocs.org/sdr/ASOA201200172.md): Isolator · cracked · Jan 16, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ISOLATOR ON FS 621 BULKHEAD BROKEN. R & R ISOLATOR IAW SRM 521-42-06.
- [SDR ASOA201200171](https://openairdocs.org/sdr/ASOA201200171.md): Frame · corroded · Jan 16, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE OF FRAME UNDER AVIONICS FLOORBOARD AT FS 349.00, APPEARS TO HAVE CORROSION UNDER PAINT.
- [SDR ASOA201200158](https://openairdocs.org/sdr/ASOA201200158.md): Frame · corroded · Jan 13, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE OF FRAME, UNDER AVIONICS FLOORBOARD, AT FS 349.00 BY DRAIN TUBE APPEARS TO HAVE UNDERLYING CORROSION UNDER PAINT. REPAIRED IAW SRM 51-42-06.
- [SDR ASOA201200154](https://openairdocs.org/sdr/ASOA201200154.md): Frame · corroded · Jan 13, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE OF FRAME, UNDER AVIONICS FLOORBOARD, AT FS 349.00 BY DRAIN TUBE APPEARS TO HAVE UNDERLYING CORROSION UNDER PAINT. REPAIRED IAW SRM 51-42-06.
- [SDR ASOA201200149](https://openairdocs.org/sdr/ASOA201200149.md): Bulkhead Web · cracked · Jan 12, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB LBL 27.50, WL 130 HAS A CRACK INDICATION APPROX.2" IN LENGTH 100 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.
- [SDR ASOA201200148](https://openairdocs.org/sdr/ASOA201200148.md): Floorbeam · corroded · Jan 12, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RT SIDE FS 349 FLOORBEAM IS CORRODED ON OTBD END. REMOVED CORROSION IAW SRM 51-21-06, STEP 3. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW REO 601R-53-21-2250, STEPS 1 AND 2. PERFORMED EDDY CURRENT IAW NDTM 51-20-06. NO INDICATIONS NOTED.
- [SDR ASOA201200147](https://openairdocs.org/sdr/ASOA201200147.md): Seat Track · corroded · Jan 12, 2012 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR SEAT TRACK CORRODED BETWEEN FS 399.50 AND FS 409.00+32. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-420-001.
- [SDR ASOA201200146](https://openairdocs.org/sdr/ASOA201200146.md): Seat Track · corroded · Jan 12, 2012 · N840AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR SEAT TRACK CORRODED FROM FS 364 TO FS 399.50. BLENDED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED UNSERVICEABLE SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA201200266](https://openairdocs.org/sdr/ASOA201200266.md): Frame · corroded · Jan 10, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT SIDE OF FRAME (UNDER AVIONICS FLOORBOARD) AT FS 333.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-00, 51-21-06 AND 53-00-00N, FIG 101, FOUND TO BE OUT OF LIMITS. DAMAGE 2.4"W - 3.0"L.017" DEPTH ABOVE STR 26R. REMOVED OLD FRAME SECTOR FS 333.00 BETWEEN S
- [SDR ASOA201200072](https://openairdocs.org/sdr/ASOA201200072.md): Frame · corroded · Jan 10, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE OF FRAME AT FS 349.0 BY DRAIN TUBE APPEARS TO HAVE CORROSION UNDER PAINT. REMOVED CORROSION IAW SRM 51-21-00, 51-21-06 AND 53-00-00, FIG 101 AND FOUND TO BE OUT OF LIMITS. REMOVED OLD FRAME SECTOR, LOCATED, DRILLED, ALODINED AND INSTALLED NEW FRAME
- [SDR ASOA201200071](https://openairdocs.org/sdr/ASOA201200071.md): Frame · corroded · Jan 10, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FACE OF FRAME UNDER AVIONICS FLOORBOARD AT FS 319.70 BY DRAIN TUBE APPEARS TO HAVE CORROSION UNDER PAINT. REMOVED CORROSION IAW SRM 51-21-00, 51-21-06 AND 53-00-00 FIGURE 101 AND FOUND TO BE OUT OF LIMITS. REPLACED FRAME IAW SRM 51-42-06
- [SDR ASOA201200070](https://openairdocs.org/sdr/ASOA201200070.md): Floorbeam · cracked · Jan 10, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, LBL 9 AND RBL 9 INBD FLOORBEAM ANGLE CRACKED. FABRICATED NEW FLOORBEAM SUPPORT ANGLE IAW REO 601R-53-11-926, REV B NOTE: 20. REMOVED OLD FLOORBEAM ANGLE IAW SRM 51-42-21. NEW FLOORBEAM ANGLE LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, PAINTED, INS
- [SDR ASOA201200069](https://openairdocs.org/sdr/ASOA201200069.md): Support Bracket · cracked · Jan 10, 2012 · N840AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT WINDSHIELD SIDE POST SUPPORT BRACKET CRACKED. R & R WINDSHIELD SUPPORT BRACKET IAW SRM 51-42-21.
- [SDR ASOA201200086](https://openairdocs.org/sdr/ASOA201200086.md): Isolator · broken · Jan 9, 2012 · N840AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > TWO ISOLATORS BROKEN ON AFT BULKHEAD. NEW MOUNT ISOLATORS INSTALLED ON AFT BULKHEAD IAW SRM 51-42-13.

Next page: https://openairdocs.org/deregistered/N840AS-2018-03-20/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 = 'N840AS' AND deregistration_id = 'N840AS-2018-03-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N840AS-2018-03-20/reports

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