# Service difficulty reports: N835AS, cancelled Aug 14, 2015

A list on [N835AS, cancelled Aug 14, 2015](https://openairdocs.org/deregistered/N835AS-2015-08-14.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 · 174 reports

- [SDR ASOA2015021112201](https://openairdocs.org/sdr/ASOA2015021112201.md): Angle · cracked · Feb 7, 2015 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT LBL 36.20, 6" ABOVE FLOOR SPLIT AT END. REMOVED CRACKED ANGLE AT LBL 36.20, 6" ABOVE FLOOR IAW SRM 51-42-06. INSTALLED IAW SRM 51-42-06.
- [SDR ASOA2015020912185](https://openairdocs.org/sdr/ASOA2015020912185.md): Bulkhead · cracked · Feb 5, 2015 · N835AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING AN EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD, FOUND AT LBL 36.2 ABOVE AND OTBD OF THE LOWEST ISOLATOR JUST ABOVE WL 73.50 CRACKED. FOUND A CRACK AT LBL 27.50 JUST ABOVE THE CARGO DOOR TRACK ABOVE WL 121.93, FOUND IS OUT OF LIMITS.
- [SDR ASOA2015020912184](https://openairdocs.org/sdr/ASOA2015020912184.md): Attach Angle · cracked · Feb 5, 2015 · N835AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > MAINTENANCE REPORTED A CRACK ON AN ATTACH ANGLE AT BS 621, LBL 36.2 BETWEEN WL 119.12 - 111.09.
- [SDR ASOA2015020912183](https://openairdocs.org/sdr/ASOA2015020912183.md): Bulkhead · cracked · Feb 5, 2015 · N835AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACK AT LBL 36.2 AND WL 73.5.
- [SDR ASOA2015020912182](https://openairdocs.org/sdr/ASOA2015020912182.md): Bulkhead · cracked · Feb 5, 2015 · N835AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESURE BULKHEAD CRACKED, LBL 27.50 ABOVE AFT CARGO DOOR TRACK.
- [SDR ASOA2014011709770](https://openairdocs.org/sdr/ASOA2014011709770.md): Bracket · bent · Jan 15, 2014 · N835AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE GEAR DISAGREE WARNING MESSAGE FOLLOWED BY NOSE DOOR OPEN WARNING RAN CHECKLIST FOR AND PULLED MANUAL GEAR RELEASE RETURNED FAR NORMAL LANDING. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY ACTIONS. FOUND NLG CENTERED, EXTENDED PROXIMITY SENSOR BRACK
- [SDR ASOA2013123109731](https://openairdocs.org/sdr/ASOA2013123109731.md): Light · damaged · Dec 29, 2013 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR FLOOR LEVEL FLOOD LIGHT ASSY DAMAGED. R & R PAX DOOR FLOOR LEVEL FLOOD LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR ASOA2013090408943](https://openairdocs.org/sdr/ASOA2013090408943.md): Bulb · burned out · Aug 31, 2013 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > AFT CABIN EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.
- [SDR ASOA2013041003360](https://openairdocs.org/sdr/ASOA2013041003360.md): Angle · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 BULKHEAD INTERCOSTAL CLIP AT S13L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD INTERCOSTAL CLIP AT STGR 13L IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-21 AND SRM 51-42-06.
- [SDR ASOA2013041003359](https://openairdocs.org/sdr/ASOA2013041003359.md): Angle · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 621 BULKHEAD INTERCOSTAL CLIP AT S14L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD INTERCOSTAL CLIP AT STGR 14L IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE 621 BULKHEAD INTERCOSTAL CLIP AT STR 14L IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013041003358](https://openairdocs.org/sdr/ASOA2013041003358.md): Angle · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 BULKHEAD INTERCOSTAL CLIP AT STGR 16L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD CLIP AT STGR 16L IAW SRM 5-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL CLIP IAW SRM 51-40-11. INSTALLED NEW CLIP AT FS 621 STGR 16L IAW SRM 51-42-06 AND 51
- [SDR ASOA2013041003357](https://openairdocs.org/sdr/ASOA2013041003357.md): Post · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Main, Structure
  > INDICATION NOTED AT FS 409+128 WL 69.0 LBL 18 OTBD CHANNEL IN RADIUS APPROX.10 L 50 PERCENT FULL SCREEN HEIGHT. LBL 18 OTBD CHANNEL FAILED NDT. REMOVED POST AT LBL 18 STA 409+128 IAW SRM 51-42-06. DRILLED UP AND INSTALLED NEW POSTS PN 601R32208-156 AND 601R
- [SDR ASOA2013041003356](https://openairdocs.org/sdr/ASOA2013041003356.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT JUST AFT OF FS 349 HAS CORROSION AROUND NUTPLATE HOLE. REPAIRED IAW EO CL600-2B19-53-I00186.
- [SDR ASOA2013041003355](https://openairdocs.org/sdr/ASOA2013041003355.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT FS 349 LBL 42 HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00191.
- [SDR ASOA2013041003354](https://openairdocs.org/sdr/ASOA2013041003354.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FS 310 LBL 42 HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00192.
- [SDR ASOA2013041003353](https://openairdocs.org/sdr/ASOA2013041003353.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT FS 559+116 - 599+32 HAS CORROSION. REPAIRED IAW CL600-2B19-53-I00193A.
- [SDR ASOA2013041003352](https://openairdocs.org/sdr/ASOA2013041003352.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559+132 - 559+48 LT FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW REO CL600-2B19-53-I00194.
- [SDR ASOA2013041003351](https://openairdocs.org/sdr/ASOA2013041003351.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559+48 - 559+80 LT FLOOR SUPPORT HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00194.
- [SDR ASOA2013041003350](https://openairdocs.org/sdr/ASOA2013041003350.md): Floorbeam · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 574 BETWEEN RBL 18 & RBL 27 IS CORRODED. R & R FLOORBEAM CAP IAW SRM 51-42-06.
- [SDR ASOA2013041003349](https://openairdocs.org/sdr/ASOA2013041003349.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CARGO FLOOR SUPPORT FROM FS 621 TO 559+180 HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW EO CL600-2B19-53-I00196.
- [SDR ASOA2013041003348](https://openairdocs.org/sdr/ASOA2013041003348.md): Floor Support · corroded · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT CARGO DOOR AREA IS CORRODED. REMOVED FLOOR SUPPORT AT LANDING FROM FS 579.5 TO 621 IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013041003347](https://openairdocs.org/sdr/ASOA2013041003347.md): Floorbeam · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280, LBL 9 INBD AND OTBD ANGLES CRACKED. REMOVED DAMAGED IAW SRM 51-42-21. FABRICATED AND INSTALLED ANGLES IAW REO 601R-53-11-926, REV B.
- [SDR ASOA2013041003346](https://openairdocs.org/sdr/ASOA2013041003346.md): Skin · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR INNER SKIN CRACKED AT THE UPPER FWD STOP BRACKET IN 2 PLACES. REMOVED DAMAGED DOOR FRAME SECTION AND CUT AWAY CHANNEL AND CAP ANGLE IAW BSC PRELIMINARY EO CL600-2B19-52-I00176. FABRICATED & INSTALLED REPAIR PARTS FOR CARGO DOOR FRAME REPAIR AND C
- [SDR ASOA2013041003345](https://openairdocs.org/sdr/ASOA2013041003345.md): Angle · cracked · Mar 20, 2013 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT 484, RBL 27 FLOOR SUPPORT CRACKED. R & R FLOOR SUPPORT ANGLE IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2013021203005](https://openairdocs.org/sdr/ASOA2013021203005.md): Glowstrip · missing · Feb 8, 2013 · N835AS · Cndair CL6002B19 · Emergency Equipment
  > FWD CABIN PHOTOLUMINESCENT ISLE END MARKERS ARE MISSING. INSTALLED FWD CABIN PHOTOLUMINESCENT AISLE END MARKERS IAW AMM 33-51-01.
- [SDR ASOA201102153](https://openairdocs.org/sdr/ASOA201102153.md): Light · malfunctioned · Nov 10, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ON REGARDLESS OF SWITCH POSITION. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IN REF WITH AMM 33-51-00. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR ASOA201101474](https://openairdocs.org/sdr/ASOA201101474.md): Battery Pack · unserviceable · Aug 6, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > REFER TO DMIL 767423 "EXTERIOR EMERGENCY LIGHT INOP". R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767423 IS CLEARED. PLACARD REMOVED.
- [SDR ASOA201101473](https://openairdocs.org/sdr/ASOA201101473.md): Battery Pack · unserviceable · Aug 6, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > REFER TO DMIL 767422 "MIDDLE EMERGENCY CABIN SIGN INOP." R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767422 IS CLEARED. PLACARD REMOVED.
- [SDR ASOA201101472](https://openairdocs.org/sdr/ASOA201101472.md): Battery Pack · unserviceable · Aug 6, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > NR2 EMERGENCY LIGHT OVER THE WING DOES NOT ILLUMINATE. EXTERIOR EMERGENCY LIGHTS - ACFT NOT OPERATED AT NIGHT. R & R NR3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767423 IS CLEARED. PLACARD REMOVED.
- [SDR ASOA201101471](https://openairdocs.org/sdr/ASOA201101471.md): Battery Pack · unserviceable · Aug 6, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN IN MIDDLE CABIN WILL NOT ILLUMINATE (CABIN EMERGENCY LIGHTS). R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767422 IS CLEARED. PLACARD REMOVED.
- [SDR ASOA201101400](https://openairdocs.org/sdr/ASOA201101400.md): Door · binding · Jul 29, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PASSENGER DOOR DIFFICULT TO OPEN. PERFORMED OPERATIONAL CHECK OF MAIN PASSENGER DOOR IAW AMM 52-11-02. OPS CHECKED GOOD.
- [SDR ASOA201101255](https://openairdocs.org/sdr/ASOA201101255.md): Handle · binding · Jul 1, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > HAD DIFFICULT STOWING DOOR OUTER HANDLE LEAVING GPS AND DOOR WAS DIFFICULT TO OPEN. PERFORMED OPS CHECK OF PASSANGER DOOR IAW AMM 52-10-00. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR ASOA201101230](https://openairdocs.org/sdr/ASOA201101230.md): Lens · broken · Jun 24, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT COVER BROKEN. REPLACED PAX ENTRY EMERGENCY LIGHT COVER AS REQUIRED.
- [SDR ASOA201101177](https://openairdocs.org/sdr/ASOA201101177.md): Door · binding · Jun 13, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR GET STUCK CLOSED. LUBRICATED DOOR STRIKERS AND ROLLERS, OPS CHECKED GOOD 5 TIMES WITHOUT FAULT IAW AMM 52-11-00.
- [SDR ASOA201101176](https://openairdocs.org/sdr/ASOA201101176.md): Door · binding · Jun 13, 2011 · N835AS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR HARD TO OPEN. FOUND EXCESSIVE AMOUNTS OF GREASE ON PAX DOOR SEAL, CLEANED AND RE-LUBBED AS REQUIRED. PERFORMED VISUAL AND FUNCTIONAL CHECK OF PAX DOOR, NO DEFECTS NOTED PAX DOOR OP CHECKS GOOD IAW AMM 52-11-00. DEFER CLEARED PLACARD REMOVED. (C
- [SDR ASOA201101159](https://openairdocs.org/sdr/ASOA201101159.md): Lens · broken · Jun 12, 2011 · N835AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT UNDER ARROW BY MAIN CABIN DOOR AND LENS BROKE BASE. REPLACED LIGHT COVER.
- [SDR ASOA201101158](https://openairdocs.org/sdr/ASOA201101158.md): Seal · contaminated · Jun 12, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > F/A STATES THAT DOOR HANDLE WILL NOT COME UP TO OPEN DOOR. (DOORS AND OVERWING EMERGENCY EXITS) FOUND EXCESSIVE AMOUNTS OF GREASE ON PAX DOOR SEAL, CLEANED AND RE-LUBED AS REQUIRED. PERFORMED VISUAL AND FUNCTIONAL CHECK OF PAX DOOR, NO DEFECTS NOTED. IAW A
- [SDR ASOA201101082](https://openairdocs.org/sdr/ASOA201101082.md): Door · binding · May 30, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CABIN DOOR WILL NOT OPEN FROM INSIDE ACFT, UNLESS ASSISTED BY GROUND CREW. SAW THE GROUND CREW PUSH THE VENT FLAP TO GET DOOR OPEN. OPS CHECK AND LUBRICATE CABIN DOOR WITH REF TO AMM 52-11-00. OPS CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA201100249](https://openairdocs.org/sdr/ASOA201100249.md): Structure · corroded · Feb 9, 2011 · N835AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FUSELAGE FS 364.00 HAS CORROSION FROM STGR 25L TO 25R.
- [SDR ASOA201100330](https://openairdocs.org/sdr/ASOA201100330.md): Frame · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 349.00 HAS CORROSION FROM STR 25L TO STR 25R. INSTALLED 6 EA SAME NUTPLATES ON DRAIN MAST NUTPLATES. INSPECTED AND FOUND TO BE IN SERVICEABLE CONDITION IAW SRM 51-42-06 AND 51-45-00. REINSTALLED SAME SERVICEABLE INTERCOSTAL AT STR 25L IAW SRM 51-42
- [SDR ASOA201100248](https://openairdocs.org/sdr/ASOA201100248.md): Wire · broken · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTING WIRE BROKE OFF ON PANEL 232BZ. REPLACED EMERGENCY LIGHT IAW 33-51-10-400-801. OPS TESTED GOOD.
- [SDR ASOA201100247](https://openairdocs.org/sdr/ASOA201100247.md): Structure · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FUSELAGE FS 333.00 HAS CORROSION FROM STR 25L TO STR 25R.
- [SDR ASOA201100246](https://openairdocs.org/sdr/ASOA201100246.md): Angle · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER ANGLE CORRODED AT LWR ENTRANCE SURROUND. REMOVED CORRODED ANGLE IAW SRM CH 51-42-06, 51-42-10 AND CH 51-42-21. LOCATED, DRILLED, SEALED, INSTALLED AND PAINTED NEW SILL ANGLE IAW SRM 51-40-11, 51-23-00, 51-42-11, 51-42-21 AND 51-25-21. REPAI
- [SDR ASOA201100245](https://openairdocs.org/sdr/ASOA201100245.md): Frame · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FS 364.00 HAS CORROSION FROM STR 25L TO 25R. REMOVED LIGHT CORROSION IAW SRM 51-21-06, STEPS 3B1 THROUGH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15 AND 53-00-00.
- [SDR ASOA201100244](https://openairdocs.org/sdr/ASOA201100244.md): Angle · cracked · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.090, RBL 9.0, OTBD ANGLE IS CRACKED. REMOVED CRACK ANGLE IAW SRM 51-42-21. FABRICATED AND INSTALLED ANGLE IAW REO 601R-53-11-638, REV A, STEP 4.
- [SDR ASOA201100243](https://openairdocs.org/sdr/ASOA201100243.md): Support Angle · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE ON FS 349.00, RBL 38.00 CORRODED. INSTALLED NEW SERVICEABLE SUPPORT ANGLE PN 601R38783-13 IAW SRM 51-42-06, 51-42-21 & 51-42-13. REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201100242](https://openairdocs.org/sdr/ASOA201100242.md): Floor Panel · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Floor Panel
  > UPPER SURFACE OF PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559 ON RBL 36 TO RBL 47. REPAIRED IAW REO 601R-53-41-1353.
- [SDR ASOA201100241](https://openairdocs.org/sdr/ASOA201100241.md): Floor Panel · corroded · Feb 8, 2011 · N835AS · Cndair CL6002B19 · Fuselage Floor Panel
  > UPPER SURFACE OF PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559 ON RBL 36 TO RBL 47. REPAIRED IAW REO 601R-53-41-1354.
- [SDR ASOA201100394](https://openairdocs.org/sdr/ASOA201100394.md): Sill · corroded · Feb 7, 2011 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL HAS CORROSION. INSTALLED FWD & AFT SERVICE DOOR SILL PLATE LATCHES IAW AMM 20-24-00-910-803 AND 20-24-00-910-806.
- [SDR ASOA201100238](https://openairdocs.org/sdr/ASOA201100238.md): Bracket · corroded · Feb 7, 2011 · N835AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE AFT BRACKET HAS CORROSION. LOCATED FASTENER HOLES IN NEW BRACKETS FOR AFT PAX DOOR SURROUND STRUCTURE IAW SRM CH 51-45-00 AND CH 51-40-11. INSTALL NEW BRACKET. INSTALLED THE PAX DOOR AFT CUP BRACKET IAW THE SRM 51-42-06 & 51-42-1

Next page: https://openairdocs.org/deregistered/N835AS-2015-08-14/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 = 'N835AS' AND deregistration_id = 'N835AS-2015-08-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N835AS-2015-08-14/reports

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