# Service difficulty reports: N872AS, cancelled Jul 3, 2017

A list on [N872AS, cancelled Jul 3, 2017](https://openairdocs.org/deregistered/N872AS-2017-07-03.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 · 102 reports

- [SDR ASOA2016060814917](https://openairdocs.org/sdr/ASOA2016060814917.md): Lamp · burned out · Jun 8, 2016 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 EXTERIOR EMERGENCY INOPERATIVE. REPLACED THE LAMP NR 1 EXIT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.
- [SDR ASOA2016041114697](https://openairdocs.org/sdr/ASOA2016041114697.md): Bulb · burned out · Apr 11, 2016 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT SIDE CENTER EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2014111711689](https://openairdocs.org/sdr/ASOA2014111711689.md): Isolator · cracked · Nov 12, 2014 · N872AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621, BULKHEAD, ISOLATOR CRACKED. R & R ISOLATION MOUNTS IAW SRM 51-42-06.
- [SDR ASOA2014012109782](https://openairdocs.org/sdr/ASOA2014012109782.md): Skin · damaged · Jan 12, 2014 · N872AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DAMAGE ON FUSELAGE SKIN BETWEEN FS 509-605, S25-26R. EC/TC REO 601R-53-61-4388, REV A HAS BEEN ACCOMPLISHED.
- [SDR ASOA2014012109781](https://openairdocs.org/sdr/ASOA2014012109781.md): Attach Bracket · cracked · Jan 11, 2014 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO TRACK UPPER CROSSBEAM AFT LOWER ATTACH BRACKET CRACKED. R & R ATTACH BRACKET IAW SRM 51-42-21 AND 51-40-11.
- [SDR ASOA2014011709772](https://openairdocs.org/sdr/ASOA2014011709772.md): Bulkhead · cracked · Jan 2, 2014 · N872AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED ABOVE CARGO DOOR. COMPLIED WITH ECTC REO 601R-53-61-1541. CLASSIFIED AS A MAJOR REPAIR.
- [SDR ASOA2014012209791](https://openairdocs.org/sdr/ASOA2014012209791.md): Bulkhead · gouged · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE AFT PRESSURE BULKHEAD FWD FACE AT BS 621 GOUGED. REPAIRED IAW EC/TC REO 601R-53-61-5152. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2014011509763](https://openairdocs.org/sdr/ASOA2014011509763.md): Seat Track · corroded · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST SEGMENT OF SEAT TRACK AT RBL 9.0 FROM BS 364-409 HAS CORROSION AT MULTIPLE LOCATIONS. COMPLIED WITH ECTC REO 601R-53-00-482 FABRICATED SEAT RAILS IAW GREO 601R-53-00-485. REMOVED SEAT TRACK AT RBL 9.0 FROM FS364-409 IAW AMM 53-01-11, TASK 53-01-11-000-
- [SDR ASOA2014011509762](https://openairdocs.org/sdr/ASOA2014011509762.md): Seat Track · corroded · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SECOND SEGMENT OF SEAT TRACK AT RBL 9.0 FROM BS 409-409+112 HAS CORROSION AT MULTIPLE LOCATIONS. COMPLIED WITH ECTC REO 601R-53-00-485. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, AT RBL9 FROM 409-409+112. INSTALLED SEAT TRACK IAW ECTC REO 601R-53-00-485.
- [SDR ASOA2014011509761](https://openairdocs.org/sdr/ASOA2014011509761.md): Seat Track · corroded · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST SEGMENT OF SEAT TRACK LBL 9, BS 364-409 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. REMOVED SEAT TRACK BS 364 - 399 IAW SRM 51-41-02-00 AND AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2014011509760](https://openairdocs.org/sdr/ASOA2014011509760.md): Seat Track · corroded · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SECOND SEGMENT OF SEAT TRACK AT LBL 9.0 BS 409 - 409+112 CORRODED. REMOVED SEGEMENT OF SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEGMENT OF SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2014011509759](https://openairdocs.org/sdr/ASOA2014011509759.md): Intercostal · cracked · Dec 30, 2013 · N872AS · Cndair CL6002B19 · Passenger/Crew Doors
  > INTERCOSTAL CRACKED INSIDE PAX DOOR ACCESS PANEL 832BR, UPPER FLANGE. REMOVED INTERCOSTAL IAW SRM 51-40-11 AND 51-42-06. INSTALLED INTERCOSTAL IAW SRM 51-40-11 & 51-42-06.
- [SDR ASOA2014012209790](https://openairdocs.org/sdr/ASOA2014012209790.md): Attach Bracket · cracked · Dec 29, 2013 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH BRACKET BENEATH CARGO DOOR CUTOUT LOWER SILL AT FS 589 FRAME. REMOVED AND REPLACED ATTACH BRACKET IAW SRM 51-42-06-00.
- [SDR ASOA2014011509758](https://openairdocs.org/sdr/ASOA2014011509758.md): Frame · corroded · Dec 28, 2013 · N872AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BETWEEN STRINGERS 26-27L, MINOR CORROSION FOUND AROUND FASTENERS. REMOVED LIGHT CORROSION IAW SRM AND TR 53-27, FOUND OUT OF LIMITS IAW SRM TR 53-27. COMPLIED WITH EA 25-2014-004.
- [SDR ASOA2014011509757](https://openairdocs.org/sdr/ASOA2014011509757.md): Intercostal · cracked · Dec 28, 2013 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING INSPECTION OF THE REAR PRESSURE BULKHEAD WEB AFT SIDE, FOUND INTERCOSTAL AT BS 630, STRINGER 14R TO BE CRACKED. R & R INTERCOSTAL IAW SRM 51-42-11.
- [SDR ASOA2014012209789](https://openairdocs.org/sdr/ASOA2014012209789.md): Skin · cracked · Dec 27, 2013 · N872AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK T/E CRACKED AT WS 148.019. COMPLIED WITH EC/TC REO 601R-57-21-131 AND 601R-57-21-131, REV A. COMPLIED WITH EC/TC REO 601R-57-21-130, REV K. REPAIR CLASSIFIED A MAJOR.
- [SDR ASOA2014011509756](https://openairdocs.org/sdr/ASOA2014011509756.md): Bracket · broken · Dec 27, 2013 · N872AS · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING STUB FAIRING FWD MOUNT BRACKET BROKEN ON T/E. R & R MOUNT BRACKET IAW SRM 51-42-20-00.
- [SDR ASOA2014011509755](https://openairdocs.org/sdr/ASOA2014011509755.md): Door · damaged · Dec 26, 2013 · N872AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR HAS A GROOVE WORN INTO IT, TOP/CENTER AREA. COMPLIED WITH GREO 601R-52-31-198. MAJOR REPAIR. COMPLIED WITH REO 601R-52-31-198 REV A DATED JAN 30,2013.
- [SDR ASOA2014011509754](https://openairdocs.org/sdr/ASOA2014011509754.md): Handle · lack of lube · Dec 26, 2013 · N872AS · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING FUNCTIONAL CHECK OF THE PAX DOOR, FOUND INNER HANDLE FORCE TO UNLATCH OUT OF LIMITS. CLEANED AND LUBRICATED PAX DOOR IAW AMM 12-20-52-640-810. PERFORMED FUNCTIONAL TEST OF PAX DOOR IAW AMM 52-11-00-720-802, FOUND WITHIN LIMITS. TESTED GOOD.
- [SDR ASOA2014012209792](https://openairdocs.org/sdr/ASOA2014012209792.md): Structure · cracked · Dec 24, 2013 · N872AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING CRACKED AT WS 149. REPAIRED IAW EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV R. REPAIR CLASSIFIED AS MAJOR.
- [SDR ASOA2013092309072](https://openairdocs.org/sdr/ASOA2013092309072.md): Skin · cracked · Sep 20, 2013 · N872AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING CRACKED AT WS 149. REPAIRED IAW GREO 601R-57-21-138, REV A AND NDTM 51-20-08. REPAIR CLASSIFED AS MAJOR IAW GMM 5-3.
- [SDR ASOA2013092309071](https://openairdocs.org/sdr/ASOA2013092309071.md): Drag Angle · cracked · Sep 20, 2013 · N872AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DRAG ANGLE CRACKED. ORIGINATING FROM RIVET HOLE AND CRACK IN RADIUS, MID-POINT OF ANGLE. REPAIRED IAW REO 601R-52-11-2184, REV A.
- [SDR ASOA2013052803673](https://openairdocs.org/sdr/ASOA2013052803673.md): Lens · broken · May 21, 2013 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOD LIGHT AT PAX DOOR LENS COMING OFF DUE TO BASE BEING BROKEN. R & LENS ASSY IAW AMM 33-23-02.
- [SDR ASOA2012083102157](https://openairdocs.org/sdr/ASOA2012083102157.md): Flashlight · inoperative · Aug 28, 2012 · N872AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. REPAIRED F/A FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR ASOA201201162](https://openairdocs.org/sdr/ASOA201201162.md): Battery · discharged · Apr 3, 2012 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY INOPERATIVE. EMREGENCY LIGHT SWITCH WAS LEFT IN ARM POSITION, CHARGED EMERGENCY LIGHT BATTERY IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR ASOA201102256](https://openairdocs.org/sdr/ASOA201102256.md): Beam · corroded · Nov 23, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Structure
  > TRANSVERSE BEAM HAS CORROSION BEYOND ALLOWABLE LIMITS AT OTBD END RBL 42, WL 73, MEASURES APPROX 2" LONG X 1" WIDE AND.012 DEEP WITH MATERIAL LOSS AT FWD OTBD CORNER OF UPPER LIP. REO 601R-53-21-2231, REV A HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOC
- [SDR ASOA201102241](https://openairdocs.org/sdr/ASOA201102241.md): Seat Track · corroded · Nov 21, 2011 · N872AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK FROM FS 439.00 TO FS 499.00 HAS AREAS OF CORROSION AROUND SCREW REO 601R-53-00-055 AND REO 601R-53-00-055, REV NL. REO 610R-53-00-055 DOES NOT ALLOW FOR FABRICATION OF WHOLE SEAT TRACK PN 601R38312-115, ITEM 3 OF MWC 8754211/106. RECEIVED
- [SDR ASOA201102228](https://openairdocs.org/sdr/ASOA201102228.md): Bracket · cracked · Nov 21, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS BENT ISOLATOR BRACKETS. REMOVED ISOLATOR MOUNT BRACKETS & ISOLATORS. INSTALLED NEW ISOLATORS IAW SRM 51-42-06.
- [SDR ASOA201102227](https://openairdocs.org/sdr/ASOA201102227.md): Floor Support · corroded · Nov 21, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INBD AND OTBD FLANGES OF FLOOR SUPPORT LBL 27 ARE CORRODED AROUND THE NUTPLATE HOLES FS 574 TO 621.
- [SDR ASOA201102226](https://openairdocs.org/sdr/ASOA201102226.md): Floor Support · corroded · Nov 21, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INBD AND OTBD FLANGES OF FLOOR SUPPORT AT LBL 27 ARE CORRODED AROUND THE NUTPLATE HOLES FS 574 TO 621. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, 51-42-10. INSTALLED, APPLIED PAINT, AND CORROSION INHIBITOR IAW SRM 51-25-16 & 51-21-11.
- [SDR ASOA201102239](https://openairdocs.org/sdr/ASOA201102239.md): Fitting · cracked · Nov 18, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Structure
  > LT/RT WINDSHIELD CENTER POST LOWER FITTINGS ARE CRACKED. DRILLED & LOCATED NEW LT & RT WINDSHIELD CENTER POST LOWER FITTINGS IAW SRM 51-40-06 & 51-40-11.
- [SDR ASOA201102203](https://openairdocs.org/sdr/ASOA201102203.md): Support Angle · corroded · Nov 16, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUTOUT LOWER SUPPORT ANGLE CORRODED AT SEVERAL LOCATIONS BETWEEN FS 319 AND FS 349. SERVICE DOOR CUTOUT LOWER SUPPORT ANGLE PN 601R38303-105 IS CORRODED AT SEVERAL LOCATIONS BETWEEN FS 319 AND FS 349. (CLOSED)
- [SDR ASOA201102202](https://openairdocs.org/sdr/ASOA201102202.md): Post · damaged · Nov 16, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH AN INDICATION IN RT AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST IAW SRM 51-42-06. REPAIRED IAW REO 601R-53-41-889 AND SRM 51-42-06.
- [SDR ASOA201102201](https://openairdocs.org/sdr/ASOA201102201.md): Post · damaged · Nov 16, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERT POST RBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE POST IAW SRM 51-42-06 & REO 601R-53-41-889.
- [SDR ASOA201102200](https://openairdocs.org/sdr/ASOA201102200.md): Post · damaged · Nov 16, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERT POST LBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST ASSY IAW SRM 51-42-06. LOCATED AND DRILLED NEW POST IAW SRM 51-40-06. INSTALLED NEW SERVICABLE POST IAW SRM 51-42-06 AND R
- [SDR ASOA201102199](https://openairdocs.org/sdr/ASOA201102199.md): Beam · corroded · Nov 16, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 349, TRANSVERSE BEAM HAS CORROSION BEYOND ALLOWABLE LIMITS AT OTBD END RBL 42, WL 73, MEASURES APPROX 2" LONG X 1" WIDE X.012" DEEP WITH MATERIAL LOSS AT FWD OTBD CORNER OF UPPER LIP. REPAIRED IAW SRM 51-42-06, 51-42-21, 51-40-11 AND REO 601R-53-21-2231.
- [SDR ASOA201102194](https://openairdocs.org/sdr/ASOA201102194.md): Attach Fitting · corroded · Nov 15, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FOUR FRAME ATTACH FITTINGS ON PAX DOOR LWR SECTION UNDER CMS 532-02 ARE CORRODED. REMOVED ATTACH FITTINGS IAW SRM 51-42-06. FOUND BEYOND LIMITS. INSTALLED FITTINGS IAW SRM 51-42-06.
- [SDR ASOA201102193](https://openairdocs.org/sdr/ASOA201102193.md): Floor Support · cracked · Nov 15, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED THE DAMAGED IAW REO 601R-53-61-117
- [SDR ASOA201102237](https://openairdocs.org/sdr/ASOA201102237.md): Bracket · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOT WINDSHIELD SIDE POST LOWER AFT SUPPORT BRACKET CRACKED. RECONNECTED LT WINDSHIELD HEATER POWER TERMINAL BLOCK WIRES IAW AMM 56-11-01-400-801. DISLODGED PILOT'S SIDE INSTRUMENT PANEL FOR ACCESS IAW SRM 51-44-00 AND 51-44-06. INSTALLED INSTRUMENT PANEL
- [SDR ASOA201102186](https://openairdocs.org/sdr/ASOA201102186.md): Seat Track · corroded · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT SIDE SEAT TRACK FS 439 TO 499 CORRODED. REMOVED SEAT TRACK SEGMENT IAW AMM 53-1-11-000-802. DRILLED, COUNTERSUNK NEW SEAT TRACK IAW REO 601R-53-00-055. INSTALLED SEAT TRACK IAW REO 601R-53-00-055.
- [SDR ASOA201102185](https://openairdocs.org/sdr/ASOA201102185.md): Attach Fitting · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 484 INTERCOSTAL INBD AND OTBD CLIPS ARE CRACKED BETWEEN RBL 27 AND RBL 36 PRESSURE FLOORBEAMS. R & R IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA201102184](https://openairdocs.org/sdr/ASOA201102184.md): Attach Fitting · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 484 INTERCOSTAL INBD CLIP CRACKED ON OTBD SIDE OF LBL 27 PRESSURE FLOORBEAM. R & R INBD CLIP IAW SRM 51-42-06 & 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR
- [SDR ASOA201102183](https://openairdocs.org/sdr/ASOA201102183.md): Floorbeam · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 460 SUPPORT ON OTBD SIDE OF RBL 9 PRESSURE FLOORBEAM IS CRACKED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-42-06, 51-42-21 & 51-40-11. INSTALLED NEW SUPPORT IAW SRM 51-42-06 & 51-42-21.
- [SDR ASOA201102182](https://openairdocs.org/sdr/ASOA201102182.md): Floorbeam · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM ANGLE CRACKED AT LBL 10 FROM MLG ALT EXT PULLEY BRACKET UPPER OTBD BOLT. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-20. INSTALLED ANGLE IAW REO 601R-53-11-926.
- [SDR ASOA201102181](https://openairdocs.org/sdr/ASOA201102181.md): Floorbeam · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, LBL 9 OTBD FLOORBEAM CLIP IS CRACKED IN UPPER PANELS. REPAIRED.
- [SDR ASOA201102180](https://openairdocs.org/sdr/ASOA201102180.md): Angle · cracked · Nov 14, 2011 · N872AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT UPPER FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-21 AND 51-25-16.
- [SDR ASOA201100542](https://openairdocs.org/sdr/ASOA201100542.md): Cover · missing · Mar 21, 2011 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY FLOOD LIGHT MISSING COVER. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-19, OP CK'S GOOD NO DEFECTS NOTED.
- [SDR ASOA201001783](https://openairdocs.org/sdr/ASOA201001783.md): Light · inoperative · Nov 14, 2010 · N872AS · Cndair CL6002B19 · Emergency Lighting
  > LT EXT EMERGENCY LIGHT (NR 7) WILL NOT ILLUMINATE WHEN COMMANDED. RESOLVED ON W/O: 179683 TASKCARD: N/R-00007. REMOVED AND REPLACED LT EXT EMERGENCY LIGHT (NR 7) LAMP IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. REMOVED AND REPLACED LT EXT EMERGENCY LIGHT (NR
- [SDR ASOA201001614](https://openairdocs.org/sdr/ASOA201001614.md): Wire · damaged · Oct 18, 2010 · N872AS · Cndair CL6002B19 · Light System Wiring
  > RT EMERGENCY EXIT SIGN AT ROW 8CD INOP. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. (CLOSE
- [SDR ASOA201000543](https://openairdocs.org/sdr/ASOA201000543.md): Fire Bottle · low · Apr 12, 2010 · N872AS · Cndair CL6002B19 · Fire Bottle, Fixed
  > CARGO BOTTLE LOW ILLUMINATED. REMAINED ON 10 TO 15 MIN. AND THEN EXTINGUISHED. (EMERGENCY DECLARED) (CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM) R & R LRD CARGO FIRE BOTTLE IAW AMM 26-25-01. OPS CHK GOOD. (CLOSED)

Next page: https://openairdocs.org/deregistered/N872AS-2017-07-03/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 = 'N872AS' AND deregistration_id = 'N872AS-2017-07-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N872AS-2017-07-03/reports

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