# Service difficulty reports: N836AS, cancelled Jul 7, 2015

A list on [N836AS, cancelled Jul 7, 2015](https://openairdocs.org/deregistered/N836AS-2015-07-07.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 · 130 reports

- [SDR ASOA2013112509488](https://openairdocs.org/sdr/ASOA2013112509488.md): Battery Pack · discharged · Nov 24, 2013 · N836AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT DOESN'T WORK. REPLACED BATTERIES IAW AMM 25-00-00. OP CHECKED GOOD.
- [SDR ASOA2013061803830](https://openairdocs.org/sdr/ASOA2013061803830.md): Angle · corroded · May 21, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AT PAX DOOR ENTRANCE FS 349, LBL 45, WL 73. REPAIRED IAW REO 601R-53-21-2437.
- [SDR ASOA2013060703803](https://openairdocs.org/sdr/ASOA2013060703803.md): Floor Support · corroded · May 20, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ASSY, FS 409+128 - 599, HAS NUMEROUS AREAS OF SURFACE CORROSION ON SILL PANELS AND FLOOR ANGLES. REPAIRED IAW EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2013060703802](https://openairdocs.org/sdr/ASOA2013060703802.md): Floor Support · corroded · May 20, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ASSEMBLY, FS 409+128 - 559, HAS NUMEROUS AREAS OF SURFACE CORROSION ON SILL PANELS AND FLOOR ANGLES. REPAIRED IAW EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C, DATED 11/06/2012 AS WRITTEN.
- [SDR ASOA2013060703799](https://openairdocs.org/sdr/ASOA2013060703799.md): Post · cracked · May 15, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST LBL 18 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX.2" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889, REV A.
- [SDR ASOA2013060703796](https://openairdocs.org/sdr/ASOA2013060703796.md): Post · cracked · May 15, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX.2" IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889, REV A.
- [SDR ASOA2013061803829](https://openairdocs.org/sdr/ASOA2013061803829.md): Sill · corroded · May 13, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL PLATE UNDER 281LLF HAS MINOR CORROSION AROUND NUTPATE HOLES. R & R CARGO DOOR SILL PLATE IAW REO 601R-53-61-1574 AND SRM 51-42-06.
- [SDR ASOA2013061803828](https://openairdocs.org/sdr/ASOA2013061803828.md): Skin · cracked · May 13, 2013 · N836AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK IS CRACKED APPROX 0.75" LONG AT WS 148.019 AND REAR SPAR. REPAIRED IAW AMM 28-11-00-790-802.
- [SDR ASOA2013060703794](https://openairdocs.org/sdr/ASOA2013060703794.md): Frame · cracked · May 13, 2013 · N836AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL AFT VERTICAL MEMBER CRACKED AT FS 605, BELOW WL 82.58. REPLACED THE CARGO DOOR INTERNAL AFT VERTICAL MEMBER USING PN 601R35027-31, PO W/22253 IAW SRM 51-42-06 & SRM 51-42-21.
- [SDR ASOA2013060703792](https://openairdocs.org/sdr/ASOA2013060703792.md): Floorbeam · cracked · May 13, 2013 · N836AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, FLOORBEAM ANGLE ARE CRACKED AT THE INBD & OTBD SIDES OF RBL 9 AND LBL 9. REPAIRED IAW REO 601R-53-11-926, REV B.
- [SDR ASOA2013060703791](https://openairdocs.org/sdr/ASOA2013060703791.md): Floor Support · broken · May 13, 2013 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 HAS BROKEN FLOOR SUPPORT AT RBL 32. REPAIRED IAW REO 601R-53-41-059.
- [SDR ASOA2013060703789](https://openairdocs.org/sdr/ASOA2013060703789.md): Drag Angle · cracked · May 10, 2013 · N836AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513.
- [SDR ASOA2013060703787](https://openairdocs.org/sdr/ASOA2013060703787.md): Handle · lack of lube · May 9, 2013 · N836AS · Cndair CL6002B19 · Emergency Exits
  > RIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST FORCE TO OPERATE HANDLE IS OUT OF LIMITS 60+ POUNDS. MAX IS 40. LUBRICATED AND WORKED RT EMERGENCY OVERWING EXIT HANDLE MECHANISM AND LATCH PINS. PERFORMED FUNCTIONAL TEST OF RIGHT OVERWING EMERGENCY EXIT
- [SDR ASOA2012111602476](https://openairdocs.org/sdr/ASOA2012111602476.md): Lens · broken · Nov 12, 2012 · N836AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR, COVER IS BROKEN. INSTALLED COVER IAW AMM 33-50-00. OK FOR SERVICE.
- [SDR ASOA2012090402162](https://openairdocs.org/sdr/ASOA2012090402162.md): Rod · damaged · Aug 31, 2012 · N836AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR IS DIFFICULT TO OPEN ESPECIALLY FROM OUTSIDE THE ACFT. FOUND SERVICE DOOR INTERNAL STABILIZER ROD DAMAGED. REPLACED & RIGGED STABILIZER ROD IAW MM 52-41-00. SDR CLOSED.
- [SDR ASOA2012081702079](https://openairdocs.org/sdr/ASOA2012081702079.md): Latch · lack of lube · Aug 16, 2012 · N836AS · Cndair CL6002B19 · Service Doors
  > UNABLE TO OPEN GALLEY SERVICE DOOR FROM OUTSIDE - OPENS FINE FROM THE INSIDE. CLEANED SILL AND LUBED LATCHES AND HANDLE. CHECKED OPS IAW AMM 52-41-00. OPS CK OK. SDR CLOSED.
- [SDR ASOA2012080302028](https://openairdocs.org/sdr/ASOA2012080302028.md): Inverter · inoperative · Jul 30, 2012 · N836AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT EMERGENCY EXIT FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OP CHECKED GOOD.
- [SDR ASOA2012070301858](https://openairdocs.org/sdr/ASOA2012070301858.md): A/C Pack · odor · Jun 30, 2012 · N836AS · Cndair CL6002B19 · Cabin Cooling System
  > IN CRUISE FLT, AT 260, LEFT PACK HIGH TEMP MESSAGE. SMELLED OVERHEAT ODOR FROM LT PACK. PERFORMED OPS CHECK ON LT PACK IAW AMM 21-51-00. OPS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.
- [SDR ASOA201201760](https://openairdocs.org/sdr/ASOA201201760.md): Inverter · unserviceable · Jun 1, 2012 · N836AS · Cndair CL6002B19 · Emergency Lighting
  > RT EMERGENCY EXIT LOWER EMERGENCY LIGHT INOPERATIVE. R & R NR 3 EMERGENCY LIGHT INVERTER ASSY IAW AMM-33-51-07,OPS CHECKED GOOD ACFT OK FOR SERVICE.
- [SDR ASOA201102216](https://openairdocs.org/sdr/ASOA201102216.md): Landing Gear · malfunctioned · Nov 18, 2011 · N836AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MASTER WARNING, NLG WOULD NOT RETRACT. ACFT RETURNED AFTER T/O AND EMERGENCY DECLARED. PERFORMED LANDING GEAR EXTENSION AND RETRACTION FUNCTIONAL TEST IAW AMM 32-30-00. OP'S CHECKED GOOD.
- [SDR ASOA201102192](https://openairdocs.org/sdr/ASOA201102192.md): Battery · discharged · Nov 15, 2011 · N836AS · Cndair CL6002B19 · Emergency Equipment
  > FLASHLIGHT DIM. INSTALLED NEW BATTERIES IAW AMM 25-60-00.
- [SDR ASOA201102160](https://openairdocs.org/sdr/ASOA201102160.md): Proximity Switch · out of rig · Nov 11, 2011 · N836AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > ACFT RETURNED AFTER TAKE OFF DUE TO A GEAR DISAGREE WARNING MESSAGE FOR NOSE GEAR. DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED UNEVENTFUL. RIGGED NLG UPLOCK PROXIMITY SWITCH PS3GA IAW AMM 32-33-05. COMPLIED WITH SEVERAL GEAR SWINGS. OPS CHECKED GOOD.
- [SDR ASOA201102059](https://openairdocs.org/sdr/ASOA201102059.md): Proximity Sensor · out of adjust · Oct 29, 2011 · N836AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER T/O GEAR DISAGREE MASTER WARNING, QRH C/W EMERGENCY DECLARE DEVERSIONARY LAND, SYS WAS ABLE TO DOWN LOCK BUT NOT UP LOCK, SYS DID TURN GREEN FOR DOWNLOCK. ACFT DIVERTED, EMERGENCY DECLARED. ADJUSTED NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR BACK IN
- [SDR ASOA201102053](https://openairdocs.org/sdr/ASOA201102053.md): Landing Gear · malfunctioned · Oct 28, 2011 · N836AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MSG IN FLIGHT. NOSEWHEEL WOULD NOT RETRACT FOLLOWED QRH CHECKLIST. EMERGENCY RELEASE HANDLE PULLED. PERFORMED OPS TEST, SWUNG GEAR 10 TIMES, NO DEFECTS NOTED IAW AMM 32-30-00-720-801.
- [SDR ASOA201102027](https://openairdocs.org/sdr/ASOA201102027.md): Uplock · failed · Oct 22, 2011 · N836AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > UPON GEAR RETRACTION, RECEIVED A NOSE WHEEL DISAGREE & WOULD NOT RETRACT. ACFT RETURNED TO DEPARTURE & EMERGENCY DECLARED. R & R NLG UPLOCK ASSY IAW AMM 32-33-05 AND PERFORMED NLG SWING RETRACTION IAW AMM 32-33-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVIC
- [SDR ASOA201101966](https://openairdocs.org/sdr/ASOA201101966.md): Mechanism · lack of lube · Oct 14, 2011 · N836AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. LUBED SERVICE DOOR ROD AND BEARINGS IAW AMM 12-20-52. OPS CHECKED GOOD.
- [SDR ASOA201101810](https://openairdocs.org/sdr/ASOA201101810.md): Controller · failed · Sep 26, 2011 · N836AS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING OVERHEAT MESSAGE C/W QRH EMERGENCY PROCEDURES. MESAGE REMAINED ON. R & R WING ANTI ICE TEMP CONTROLER IAW AMM 30-12-19. RESEALED LT WING STAND BY THERMAL SWITCHES IAW AMM 30-12-16.
- [SDR ASOA201101346](https://openairdocs.org/sdr/ASOA201101346.md): Motor · failed · Jul 18, 2011 · N836AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WILL NOT OPEN. REMOVED AND REPLACED PAX DOOR MOTOR ASSY IAW AMM 52-11-08. OPS CHECKED GOOD NO FURTHER DEFECTS FOUND.
- [SDR ASOA201101061](https://openairdocs.org/sdr/ASOA201101061.md): Flashlight · inoperative · May 24, 2011 · N836AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED F/A FLASHLIGHT IAW AMM 25-61-00.
- [SDR ASOA201100995](https://openairdocs.org/sdr/ASOA201100995.md): Bulb · burned out · May 18, 2011 · N836AS · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT (7) SEVEN, LOCATED BELOW THE PASSENGER WINDOW AT FS 491.50L IS INOP. R & R THE BULB AT THE EXTERIOR EMERGENCY LIGHT (NR 7) IAW MM 33-51-21-000-801/400-801. PERFORMED THE OPS TEST OF THE EMERGENCY LIGHTS IAW MM 33-51-00-710-801. NO D
- [SDR ASOA201100888](https://openairdocs.org/sdr/ASOA201100888.md): Frame Splice · cracked · May 5, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SPLICE AT FS 718, STR 20R IS CRACKED. LOCATED AND INSTALLED SERVICEABLE FRAME SPLICE AT FS 718, STR 20R IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.
- [SDR ASOA201100877](https://openairdocs.org/sdr/ASOA201100877.md): Bulkhead · cracked · May 4, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT WL 130, LBL 27.50, APPROX.3" IN LENGTH 1005 FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.
- [SDR ASOA201100847](https://openairdocs.org/sdr/ASOA201100847.md): Seat Track · corroded · Apr 26, 2011 · N836AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT RAILS FORM FS 364.00 TO FS 409.00+128, RBL 9.0 ARE CORRODED. REPAIRED IAW REO 601R-53-00-412.
- [SDR ASOA201100799](https://openairdocs.org/sdr/ASOA201100799.md): Post · cracked · Apr 20, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Structure
  > VERTICAL POST AT FS 409+128, WL 69.00, RBL 18.00 HAS 2 INDICATIONS: (1) ON THE OTBD POST, (1) ON THE INBD POST. BOTH IN THE AFT RADIUS. FAILED NDT INSPECTION. REMOVED VERT POST IAW SRM 51-42-06. LOCATED, DRILLED AND ASSEMBLED VERT POST IAW SRM 51-42-06
- [SDR ASOA201100797](https://openairdocs.org/sdr/ASOA201100797.md): Floorbeam · corroded · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM AFT CAP ANGLE IS CORRODED BETWEEN RBL 9 AND LBL 9. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100796](https://openairdocs.org/sdr/ASOA201100796.md): Floor Support · corroded · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, FWD ANGLE BETWEEN LBL 9 AND RBL 9 IS CORRODED. REFER CO 7263111, REO 601R-53-11-926 W/O 198723 STEP 77 FOR INSTALLATION OF FS 280 FWD FLOOR SUPPORT ANGLE.
- [SDR ASOA201100795](https://openairdocs.org/sdr/ASOA201100795.md): Skin · corroded · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FS 559+93 STRG 23R HAS A SMALL AREA OF CORROSION AROUND A RIVET. REMOVED CORROSION IAW SRM 51-21-06. BLEND IS WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-31. TREAT, PRIME AND PAINT BLEND AREA.
- [SDR ASOA201100794](https://openairdocs.org/sdr/ASOA201100794.md): Attach Angle · cracked · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PILOTS WINDSHIELD POST LOWER ATTACHMENT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21.
- [SDR ASOA201100793](https://openairdocs.org/sdr/ASOA201100793.md): Attach Angle · cracked · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CO-PILOT WINDSHIELD POST LOWER ATTACHMENT ANGLE CRACKED. R & R WINDSHIELD POST LOWER ATTACHMENT ANGLE WITH NEW PART IAW SRM 51-40-11 AND SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.
- [SDR ASOA201100792](https://openairdocs.org/sdr/ASOA201100792.md): Floorbeam · cracked · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 OTBD OF LBL 9.0 CLIP IS CRACKED. REPAIRED IAW REO 601R-53-11-926 W/O 198723 STEP 82.
- [SDR ASOA201100791](https://openairdocs.org/sdr/ASOA201100791.md): Seat Track · corroded · Apr 19, 2011 · N836AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 AFT SEAT TRACK AT FS 621.00 CORRODED. R & R AT FS 621.00, LBL 9 SEAT RACK PN 601R31632-51 IAW AMM 20-21-00. (CLOSED)
- [SDR ASOA201100812](https://openairdocs.org/sdr/ASOA201100812.md): Placard · worn · Apr 15, 2011 · N836AS · Cndair CL6002B19 · Placards and Markings
  > EXIT INDICATORS AT THE OVERWING EXITS ARE WORN, ALL 4 PIECES. TO BE INSTALLED UNDER FLUSH COVER, NOT ON TOP. REMOVED AND INSTALLED SERVICEABLE MARKERS IAW AMM 11-30-00-000-801 & 11-30-00-400-801.
- [SDR ASOA201100772](https://openairdocs.org/sdr/ASOA201100772.md): Post · cracked · Apr 15, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Structure
  > LBL 27 INBD POST CRACKED AT FS 409+128 AT S20L. REPAIRED IAW REO 601R-53-41-056 IAW REO 601R-53-41-056
- [SDR ASOA201100886](https://openairdocs.org/sdr/ASOA201100886.md): Light · unserviceable · Apr 13, 2011 · N836AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED AND INSTALLED SERVICEABLE BETA EXIT LIGHT ON SERVICE DOOR IAW AMM 33-51-09-400-802. SERVICE DOOR BETA LIGHT REQ'S A FUNCTIONAL TEST IAW AMM 33-51-09-720-801. PERFORMED FUNC TEST OF SERVICE DOOR HANDLE
- [SDR ASOA201100859](https://openairdocs.org/sdr/ASOA201100859.md): Stiffener · chafed · Apr 13, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 621 BULKHEAD VERTICAL STIFFENER AT BL 0 IS CHAFED APPROX 1" L X.5" W X.005 ABOVE ESB. BLENDED AREA ON FS 621 BL 0.02 MEMBER IAW REO 601R-53-61-1523. PERFORMED EDDY CURRENT INSP ON THE NEWLY BLENDED AREA OF THE VERTICAL STIFFENER AT FS 621, BL0.0. NO INDI
- [SDR ASOA201100762](https://openairdocs.org/sdr/ASOA201100762.md): Structure · corroded · Apr 13, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 559.00+105 STR 23R HAS A SMALL AREA OF CORROSION AROUND RIVET" IN DIA. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06. WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-31.
- [SDR ASOA201100761](https://openairdocs.org/sdr/ASOA201100761.md): Seat Track · corroded · Apr 13, 2011 · N836AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FWD FLOOR SEAT TRACK FROM FS 364.00 TO FS 409.00+128 RBL 9.0 ARE CORRODED. R & R RT FWD FLOOR SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.
- [SDR ASOA201100760](https://openairdocs.org/sdr/ASOA201100760.md): Frame · cracked · Apr 13, 2011 · N836AS · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT BS 718 FRAME IS CRACKED AT S11-12L. REPLACED FRAME IAW SRM 51-42-06, 51-42-21.
- [SDR ASOA201100221](https://openairdocs.org/sdr/ASOA201100221.md): Landing Gear · smoke · Jan 27, 2011 · N836AS · Cndair CL6002B19 · Main Landing Gear
  > TOWER REPORTED SMOKE COMING FROM MLG AFTER LANDING, DURING TAXI IN. VISUALLY INSPECTED LT AND RT MLG, TIRES, AND BRAKE ASSY'S FOR DEFECTS AND LEAKS IAW AMM CH 32-10-00. NO DEFECTS FOUND.
- [SDR ASOA201001286](https://openairdocs.org/sdr/ASOA201001286.md): Battery Pack · inoperative · Sep 5, 2010 · N836AS · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS INOP. R & R NR 4 BATTERY PACK IAW AMM 33-51-04. OPS CK GOOD. R & R NR 4 BATTERY PACK IAW AMM 33-51-04, OPS CK GOOD.

Next page: https://openairdocs.org/deregistered/N836AS-2015-07-07/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 = 'N836AS' AND deregistration_id = 'N836AS-2015-07-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N836AS-2015-07-07/reports

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