# Service difficulty reports: N824AS, cancelled Nov 13, 2017

A list on [N824AS, cancelled Nov 13, 2017](https://openairdocs.org/deregistered/N824AS-2017-11-13.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 5 · 226 reports

- [SDR SWIA201540909](https://openairdocs.org/sdr/SWIA201540909.md): Skin · dented · Mar 11, 2015 · N824AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN IS DENTED AT 2 LOCATIONS, APPROXIMATELY WS 56.30. AND WS64.30. REQUIRING SKIN REPLACEMENT. C-CHECK, RO 3/23/15, REPAIRED LT INBD FLAP LOWER INBD SKIN HALF FOR STS EA,ALL STEPS 1 THRU 7 COMPLIED WITH.THIS IS A PERMANENT REPAIR.
- [SDR SWIA201540913](https://openairdocs.org/sdr/SWIA201540913.md): Floor Panel · corroded · Mar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT OTBD PRESSURE FLOOR PANEL FS 473.15 TO 559 RBL 43 HAS CORROSION AROUND FASTENER HOLES. C-CHECK RO 3/23/15, REPAIRED CORROSION DAMAGE ON RT OTBD PRESSURE FLOOR PANEL FS 473.15 TO FS 559.0 RBL 43. ORIGINAL THICKNESS.055", IN CHEM-MILL POSKET, REMAININ
- [SDR SWIA201540910](https://openairdocs.org/sdr/SWIA201540910.md): Floor Panel · corroded · Mar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT OTBD PESSURE FLOOR PANEL FS 484 TO 559 LBL43 HAS CORROSION AROUND FASTENER HOLES. C-CHECK RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT OTBD PRESSURE FLOOR PANEL FS 484.0 TO FS 559.0 LBL 43. ORIGINAL THICKNESS.055", IN CHEM-MILL POCKET, REMAINING THICKN
- [SDR SWIA201540903](https://openairdocs.org/sdr/SWIA201540903.md): Skin · cracked · Mar 4, 2015 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SUSPECTED CRACK IN LOWER FUSELAGE SKIN AT AFT LT CORNER OF NLG AFT DOOR CUT-OUT. C-CHECK, RO 3/23/15, REPAIRED CRACK IN LOWER FUSELAGE AT AFT LT CORNER OF NLG DOOR CUTOUT REF PRESSURE CHECK GOOD. COMPLIED WITH ST 51-900-1003.
- [SDR SWIA201540912](https://openairdocs.org/sdr/SWIA201540912.md): Floor Support · corroded · Mar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SILL STRUCTURE FLOOR ANGLE FS 473.15 TO 513 HAS CORROSION. C-CHECK, RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT SILL STRUCTURE FLOOR ANGLE FS 473.15 TO FS 513.0. ORIGINAL THICKNESS.080", REMAINING THICKNESS.074", MATERIAL LOSS.006", WITHIN LIMIT REF R
- [SDR SWIA201540911](https://openairdocs.org/sdr/SWIA201540911.md): Floor Support · corroded · Mar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SILL STRUCTURE FLOOR ANGLE FS 409+128 TO 473.15 HAS CORROSION. C-CHECK, RO 3/23/15, REPAIRED CORROSION DAMAGE ON LT SILL STRUCTURE FLOOR ANGLE FS 409+128 TO FS 473.15. ORIGINAL THICKNESS.080", REMAINING THICKNESS.069", MATERIAL LOSS.011", WITHIN LIMI
- [SDR SWIA201540902](https://openairdocs.org/sdr/SWIA201540902.md): Seat Track · corroded · Mar 3, 2015 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT RAIL FS 349 TO 409+128, RBL 9 HAS CORROSION AND GOUGE DAMAGE. C-CHECK, RO 3/23, BLENDED GOUGE DAMAGE AT RBL 9, FS409+42, IAW SRM, LOCATION, ORIGINAL WIDTH IS.420?, REMOVED MATERIAL IS.080"?, REMAINING WIDTH IS.500"?, SEAT TRACK RAIL IS OUT OF
- [SDR SWIA201540918](https://openairdocs.org/sdr/SWIA201540918.md): Skin · corroded · Mar 2, 2015 · N824AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION AROUND FASTENER ON FUSELAGE BELLY SKIN FS 559+16, STR 26R APPROXIMATELY AS MARKED, C-CHECK, RO 3/23/15. REMOVED CORROSION FROM EXTERIOR FUSLEAGE BELLY SKIN FS 559+16, STR 26R, AND BLENDED SMOOTH IAW STS EA. BEGINNING MATERIAL THICKNESS IN DAMAGE AR
- [SDR SWIA201540914](https://openairdocs.org/sdr/SWIA201540914.md): Hinge · gouged · Mar 1, 2015 · N824AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RT OTBD FLAP AFT HINGE BOX-ATTACH FITTING AT WS 264.00 HAS 2 EA, GOUGES. C-CHECK, RO 3/23/15, BLENDED OUT GOUGES AND FOUND WITHIN LIMITS OF STS EA.
- [SDR SWIA201540908](https://openairdocs.org/sdr/SWIA201540908.md): Skin · chafed · Mar 1, 2015 · N824AS · Cndair CL6002B19 · Ailerons
  > LT AILERON LOWER L/E SKIN CHAFED INBD OF CENTER HINGES, C-CHECK, RO 3/23/15. COMPLIED WITH REPAIR OF THE LT AILERON LOWER L/E INBD OF THE CENTER HINGES REF REO.
- [SDR SWIA201439264](https://openairdocs.org/sdr/SWIA201439264.md): Charger · failed · Sep 10, 2014 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS STAY ILLUMINATED AT OVERWING EXITS. R & R THE AFT BATTERY CHARGER IN THE CABIN.
- [SDR ASOA2014051510493](https://openairdocs.org/sdr/ASOA2014051510493.md): Battery Pack · discharged · May 11, 2014 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AFTER CHARGING, OPS CHECKED GOOD IAW AMM 33-51-00, ACFT OK FOR SERVICE.
- [SDR ASOA2014050910482](https://openairdocs.org/sdr/ASOA2014050910482.md): Frame · cracked · May 2, 2014 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FRAME CRACKED AT BS 338 TOP OF DOOR. REPAIRED IAW REO 601R-52-11-402.
- [SDR ASOA2014050910481](https://openairdocs.org/sdr/ASOA2014050910481.md): Door Frame · cracked · May 2, 2014 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FRAME CRACKED AT BS 320.1, TOP OF DOOR. REPAIRED IAW 52-11-04-000-808 AND 52-11-04-000-810 AND SRM 51-42-13-00. COMPLIED WITH OPS TEST F/O ASD IAW AMM 52-11-00-710-801, OPS TESTED GOOD. MAJOR REPAIR.
- [SDR ASOA2014050910480](https://openairdocs.org/sdr/ASOA2014050910480.md): Floor Support · cracked · Apr 26, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED & CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21 AND REO: 601R-53-61-593.
- [SDR ASOA2014050910479](https://openairdocs.org/sdr/ASOA2014050910479.md): Floor Support · corroded · Apr 23, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED BETWEEN BS 559+112 TO 521 LT SIDE. FLOOR SUPPORT REPLACED IAW REO 601R-53-61-593.
- [SDR ASOA2014050910478](https://openairdocs.org/sdr/ASOA2014050910478.md): Floor Support · corroded · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 574 - 621, LBL 27 OTBD SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-21 AND 51-42-22.
- [SDR ASOA2014050910477](https://openairdocs.org/sdr/ASOA2014050910477.md): Floor Support · corroded · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO LT FLOOR SUPPORT HAS CORROSION BETWEEN BS 559+80-FS 559+96, LBL 47. REPAIRED IAW EC/TC REO 601R-53-00-526 AND REO 601R-53-00-526.
- [SDR ASOA2014050910476](https://openairdocs.org/sdr/ASOA2014050910476.md): Isolator · broken · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUR ISOLATORS BROKEN ON FWD FACE OF FS 621 BULKHEAD IN CARGO BAY. REMOVED BROKEN ISOLATORS FROM MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA). INSTALLED NEW SERVICEABLE ISOLATORS ON MOUNTING BRACKETS IAW SRM 51-42-06 (4 EA).
- [SDR ASOA2014050910475](https://openairdocs.org/sdr/ASOA2014050910475.md): Floor Support · cracked · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, FLOOR SUPPORT CRACKED AT RBL 27.0. REMOVED D & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-21.
- [SDR ASOA2014050910474](https://openairdocs.org/sdr/ASOA2014050910474.md): Floor Skin · cracked · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN CRACKED APPROX 3 INCH AT FS 460 BETWEEN BL 0 AND RBL 9. COMPLIED WITH REO:601R-53-41-1808.
- [SDR ASOA2014050910473](https://openairdocs.org/sdr/ASOA2014050910473.md): Rub Strip · worn · Apr 21, 2014 · N824AS · Cndair CL6002B19 · Vertical Stabilizer
  > VERTICAL STABILIZER LT UPPER VISOR ASSY FWD RUB STRIP IS WORN AND DETACHED. RECEIVED AND COMPLIED WITH ECTC OF REO 601R-52-11-2219 FOR DEVIATION OF GENERIC REO 601R-52-11-402. EC/TC REO 601R-52-11-2216 HAS BEEN COMPLETED AND ALL STEPS HAVE BEEN DOCUMENTED A
- [SDR ASOA2013082308902](https://openairdocs.org/sdr/ASOA2013082308902.md): Lamp · burned out · Aug 19, 2013 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013062103862](https://openairdocs.org/sdr/ASOA2013062103862.md): Fuse · blown · Jun 17, 2013 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > NR 2 AND 4 CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE ON NR 4 BATTERY POWER SUPPLY IAW CMM 33-21-70. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR ASOA2013062103861](https://openairdocs.org/sdr/ASOA2013062103861.md): Lamp · burned out · Jun 17, 2013 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT REAR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013051703598](https://openairdocs.org/sdr/ASOA2013051703598.md): Structure · cracked · May 14, 2013 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAS A CRACK. REPAIRED IAW REO 601R-52-11-1359-01.
- [SDR ASOA2013041203368](https://openairdocs.org/sdr/ASOA2013041203368.md): Door · binding · Apr 9, 2013 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR IS HARD TO OPEN, F/A CANNOT GET THE HANDLE TO STOW,.2500" GAP AT THE TOP OF THE DOOR. PREFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00, PRESSURIZED ACFT, OPS CHECKED GOOD.
- [SDR ASOA2013032503251](https://openairdocs.org/sdr/ASOA2013032503251.md): Rib · cracked · Mar 21, 2013 · N824AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STAB RIB 9 IS CRACKED. REMOVED THE RT HORIZONTAL STAB RIB AND DRILLED NEW RIB AND TRANSFERED ALL ANGLES AND BRACKETS IAW SRM 51-42-13 AND IAW SRM 51-42-06. INSTALLED NEW RIB 9 IAW SRM 51-42-13, 51-45-00.
- [SDR ASOA2013021203004](https://openairdocs.org/sdr/ASOA2013021203004.md): Unknown · odor · Feb 8, 2013 · N824AS · Cndair CL6002B19 · Air Distribution System
  > STRONG BURNING ODOR THROUGH COCKPIT GASPERS. F/A CALLED AND REPORTED THE SAME. ELECTRICAL COMPONENT BURNING ODOR. F/A REPORTED NO SMOKE BUT ODOR WAS STRONG. HAD F/A PULL GALLEY C/B'S AND ODOR WENT AWAY AFTER 1-2 MINUTES. ( GALLEY HEATING SYSTEM: FAN) EME
- [SDR ASOA2012102902402](https://openairdocs.org/sdr/ASOA2012102902402.md): Latch · jammed · Oct 24, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR LATCH HARD TO CLOSE AND OPEN. LOWER LATCH ESPCIALLY. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-03. OPS CHECKED GOOD. SDR CLOSED.
- [SDR ASOA2012101202349](https://openairdocs.org/sdr/ASOA2012101202349.md): Handle · inoperative · Oct 10, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM THE INSIDE OR OUTSIDE. R & R HANDLE. OPS CHECKED GOOD. ACFT OK FOR FURTHER SERVICE.
- [SDR ASOA2012091402217](https://openairdocs.org/sdr/ASOA2012091402217.md): Door · lack of lube · Sep 11, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED PAX DOOR, OPS CHECKED GOOD IAW AMM 52-11-00.
- [SDR ASOA2012081002054](https://openairdocs.org/sdr/ASOA2012081002054.md): Counterbalance · out of adjust · Aug 7, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > F/O UNABLE TO OPEN PAX DOOR ( DOORS AND OVERWING EMERGENCY EXITS) ADJUSTED PAX DOOR COUNTERBALANCE IAW AMM 52-11-17, OPS CK GOOD DEFER CLEARED PLACARD REMOVED.
- [SDR ASOA2012081002053](https://openairdocs.org/sdr/ASOA2012081002053.md): Latch · contaminated · Aug 7, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > F/A UNABLE TO OPEN MAIN PAX DOOR. FOUND DEBRIS IN LATCH ON MECHANISM CLEANED OUT AND LUBRICATED IAW AMM 52-11-03. ALL ROLL FITTINGS ACFT OK FOR SERVICE.
- [SDR ASOA2012080302035](https://openairdocs.org/sdr/ASOA2012080302035.md): Handle · lack of lube · Aug 1, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX OUTER HANDLE HARD TO PUSH OPEN. PAX OUTER HANDLE LUBRICATED IAW AMM 52-11-03. OPS CHECKED GOOD.
- [SDR ASOA2012072701996](https://openairdocs.org/sdr/ASOA2012072701996.md): Handle · obstructed · Jul 24, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. FOUND EXCESSIVE DEBRIS AND GREASE ON DOOR LOCKING HANDLE MECHANISM, CLEANED AND PERFORMED OPS TEST IAW AMM 52-11-00. OPS TESTED GOOD ACFT OK FOR SERVICE.
- [SDR ASOA2012070301854](https://openairdocs.org/sdr/ASOA2012070301854.md): Floor Support · corroded · Jun 11, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT BEHIND FS 349 IS CORRODED. INSTALLED NEW FLOOR SUPPORT SECTION IAW REO 601R-53-21-425.
- [SDR ASOA2012062001813](https://openairdocs.org/sdr/ASOA2012062001813.md): Strap · corroded · Jun 11, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP AT FS 559 AT RBL 36-45 CORRODED. APPLIED FINISH TO REWORKED AREA IAW SRM 51-21-11.
- [SDR ASOA2012070301853](https://openairdocs.org/sdr/ASOA2012070301853.md): Floorbeam · corroded · Jun 7, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF SERVICE DOOR SILL, FOUND CORROSION ON FS 349 FLOORBEAM LATERAL FRAME AT RBL 42. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06. CUT AWAY DAMAGE ON FLOORBEAM IAW REO 601R-53-21-2320, STEP 1 & 3. COMPLIED WITH STEP 2 OF REO 601R-53-21-2320 IAW N
- [SDR ASOA201201778](https://openairdocs.org/sdr/ASOA201201778.md): Seat Track · corroded · Jun 7, 2012 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9.0 BETWEEN FS 559+4 - 559+86 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA201201766](https://openairdocs.org/sdr/ASOA201201766.md): Support Bracket · corroded · Jun 4, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER AND LOWER SURFACE OF TOP FLANGE ON WINDSCREEN SUPPORT BRACKET. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06-00 & 51-42-21-00.
- [SDR ASOA201201765](https://openairdocs.org/sdr/ASOA201201765.md): Light · broken · Jun 4, 2012 · N824AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ASSY AT GALLEY/SERVICE DOOR BROKE. REMOVED UNSERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM TASK 25-31-01-000-802 SUBTASK 25-31-01-000-011. INSTALLED SERVICEABLE GALLEY 1 EMERGENCY EXIT LIGHT ASSY IAW AMM 25-31-01-400-802.
- [SDR ASOA2012071701910](https://openairdocs.org/sdr/ASOA2012071701910.md): Sill · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL IS CORRODED BETWEEN FS 319-349. R & R SERVICE DOOR SILL IAW EO 600-53-0724.
- [SDR ASOA201201759](https://openairdocs.org/sdr/ASOA201201759.md): Strap · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP AT FS 559 RBL 36-45 CORRODED. BLEND CORROSION ON STRAP AT FS559.0 AT RBL 36-45 AND EVALUATE. BLENDED CORROSION IAW SRM 53-00-00, FIG 101. PERFORMED UT THICKNESS INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-41-1584.
- [SDR ASOA201201758](https://openairdocs.org/sdr/ASOA201201758.md): Floorbeam · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM AT FS 349 BETWEEN LBL 27 - LBL 42 IS CORRODED ON UNDERSIDE. REPAIRED IAW SRM 51-42-06, 51-42-21.
- [SDR ASOA201201757](https://openairdocs.org/sdr/ASOA201201757.md): Floorbeam · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM AT FS 589 BETWEEN RBL 27 - RBL 41 IS CORRODED. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-321-06 & SRM 53-00-00. PERFORMED UT INSPECTION OF BLEND AREA IAW MWC NDT INSPECTION PROCEDURE UT-3. REPAIRED IAW REO 601R-53-61-4557.
- [SDR ASOA201201756](https://openairdocs.org/sdr/ASOA201201756.md): Floorbeam · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM AT FS 574 BETWEEN LBL 9.0 - RBL 9.0 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED CAP STRIP IAW SRM 51-42-06 AND 51-45-00, 51-42-15 AND DWG NR 601R35031.
- [SDR ASOA201201755](https://openairdocs.org/sdr/ASOA201201755.md): Floor Support · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO RT FLOOR SILL IS CORRODED BETWEEN FS 559+80 - 621. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. WITHIN LIMITS OF SRM 53-00-00.
- [SDR ASOA201201754](https://openairdocs.org/sdr/ASOA201201754.md): Floorbeam · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOORBEAM AT FS 621 BETWEEN LBL 9 - 27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. BEYOND LIMITS IAW SRM 53-61-49.
- [SDR ASOA201201753](https://openairdocs.org/sdr/ASOA201201753.md): Cargo Track · corroded · Jun 1, 2012 · N824AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 9 BETWEEN FS 612 - 616 IS CORRODED. CARGO TRACK FOUND TO BE UNSERVICEABLE IAW SRM 53-61-49. R & R CARGO TRACK IAW AMM 53-01-11-000-802.

Next page: https://openairdocs.org/deregistered/N824AS-2017-11-13/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 = 'N824AS' AND deregistration_id = 'N824AS-2017-11-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N824AS-2017-11-13/reports

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