# Service difficulty reports: N884AS, cancelled Nov 26, 2019

A list on [N884AS, cancelled Nov 26, 2019](https://openairdocs.org/deregistered/N884AS-2019-11-26.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 · 162 reports

- [SDR SWIA201743939](https://openairdocs.org/sdr/SWIA201743939.md): O-Ring · failed · Nov 1, 2017 · N884AS · Cndair CL6002B19 · Hydraulic System, Main
  > HYD SYSTEM 3 FAILED DURING CRUISE FLIGHT. ZERO PSI. COMPLIED WITH QRH. DECLARED EMERGENCY. PERFORMED A FREEFALL EXTENSION OF LANDING GEAR. R & R THE HYD PUMP 3A AND 3B IAW AMM. R & R THE O-RING BETWEEN THE PUMP AND THE BALL ATTENUATOR. LEAK CHECKED GOOD.
- [SDR SWIA2017101243860](https://openairdocs.org/sdr/SWIA2017101243860.md): Trunnion · damaged · Sep 13, 2017 · N884AS · Cndair CL6002B19 · Stabilizer Control System
  > UPPER LEFT TRUNNION STRUCTURE ATTACHMENT HOLES, ARE OVERSIZED. STEPPED UP TRUNNION HOLES TO FIRST OVER SIZE IAW REO.
- [SDR SWIA2017101243852](https://openairdocs.org/sdr/SWIA2017101243852.md): Floor Support · corroded · Sep 13, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FLOOR SUPPORT BRACKET AT BS 349 CORRODED. REMOVED AND REPLACED BRACKET IAW SRM.
- [SDR SWIA2017101243862](https://openairdocs.org/sdr/SWIA2017101243862.md): Angle · corroded · Sep 11, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SERVICE DOOR FLOOR SUPPORT ANGLE AT BS 319 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM.
- [SDR SWIA2017101243858](https://openairdocs.org/sdr/SWIA2017101243858.md): Floor Support · corroded · Sep 10, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT THE PASSENGER DOOR IS CORRODED BETWEEN BS 349 AND 359. REMOVED THE CORROSION IAW REO.
- [SDR SWIA2017101243864](https://openairdocs.org/sdr/SWIA2017101243864.md): Shear Tie · corroded · Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION ON LOWER FRAME SHEAR TIE AT BS 319. REMOVED AND REPLACED THE SHEAR TIE IAW SRM.
- [SDR SWIA2017101243863](https://openairdocs.org/sdr/SWIA2017101243863.md): Doubler · corroded · Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT GALLEY MOUNT DOUBLER FWD OF BS 319 IS CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM.
- [SDR SWIA2017101243857](https://openairdocs.org/sdr/SWIA2017101243857.md): Beam · corroded · Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT TRANSVERSE BEAM AT BS 349 IS CORRODED. REPAIRED DAMAGE AT IAW REO.
- [SDR SWIA201743855](https://openairdocs.org/sdr/SWIA201743855.md): Floor Support · damaged · Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT RBL 27 BETWEEN BS 574 - 621 DAMAGED. REPAIRED FLOOR SUPPORT IAW REO.
- [SDR SWIA2017101243853](https://openairdocs.org/sdr/SWIA2017101243853.md): Shear Tie · corroded · Sep 9, 2017 · N884AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION ON LOWER FRAME BRACKET AT BS 349. REMOVED AND REPLACED LOWER FRAME BRACKET IAW SRM.
- [SDR SWIA2017101243856](https://openairdocs.org/sdr/SWIA2017101243856.md): Floor Support · corroded · Sep 8, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON THE RT FLOOR SUPPORT FROM BS 349 - 364. REPAIRED THE DAMAGE IAW REO.
- [SDR SWIA2017101243851](https://openairdocs.org/sdr/SWIA2017101243851.md): Floor Support · corroded · Sep 3, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AROUND NUTPLATES BETWEEN BS 605.04 AND 574 CORRODED AT CARGO BAY DOOR. FURTHER INVESTIGATION FOUND CARGO DOOR FLOOR SUPPORT TO BE OUT OF LIMITS. IAW REO 601R-53-00-526 REV -.
- [SDR SWIA2017101243861](https://openairdocs.org/sdr/SWIA2017101243861.md): Frame · cracked · Aug 28, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 280 FRAME IS CRACKED AT STRINGER 3L. REPAIRED THE FRAME IAW REO.
- [SDR SWIA2017101243854](https://openairdocs.org/sdr/SWIA2017101243854.md): Channel · cracked · Aug 28, 2017 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK LOWER CHANNEL IS CRACKED. REMOVED AND INSTALLED A NEW CHANNEL IAW SRM.
- [SDR SWIA201743859](https://openairdocs.org/sdr/SWIA201743859.md): Skin · dented · Aug 24, 2017 · N884AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT BS 409+64, STRINGER 15R. REPAIRED IAW REO.
- [SDR ASOA2016060714916](https://openairdocs.org/sdr/ASOA2016060714916.md): Lamp · burned out · Jun 7, 2016 · N884AS · Cndair CL6002B19 · Emergency Lighting
  > NR 4 EXIT, EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2015121114209](https://openairdocs.org/sdr/ASOA2015121114209.md): Generator · shutdown · Dec 11, 2015 · N884AS · Cndair CL6002B19 · AC Generator-Alternator
  > ADG DEPLOYED IN FLIGHT DUE TO INADVERTENTLY SHUTTING DOWN OF GEN 1 AND GEN 2 EMERGENCY DECLARED. ACFT RETURNED TO DEPARTURE AFTER T/O. RETRACTED ADG IAW AMM 24-23-01 AND PERFORM IDLE ENGINE RUNS IAW AMM 71-00-00 WITH IDG'S AND APU GENERATOR ONLINE. NO ABN
- [SDR ASOA2015102313950](https://openairdocs.org/sdr/ASOA2015102313950.md): Spar · damaged · Oct 23, 2015 · N884AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > AFT SPAR ON RT HORIZONTAL STAB TIP FOUND TO BE DAMAGED DUE TO LIGHTNING STRIKE. CUT AWAY BURNED SECTION OF AFT SPAR AND CLEANED UP ALL SHARP EDGES ON MISDRILLED HOLE ON AFT SPAR TO THE RT OF BURN, WORK DONE REF EA EJ-CRJ255-00032. COMPLIED WITH EDDY CURRENT
- [SDR ASOA2015070213228](https://openairdocs.org/sdr/ASOA2015070213228.md): Angle · corroded · Jun 18, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 J-ANGLE CORRODED. REMOVED CORRODED J-ANGLE AT FS 280 PT 600-34017-351 IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW FS 280, J-ANGLE PT 600-34017-351S IAW SRM 51-42-06 & 51-40-11.
- [SDR ASOA2015070213227](https://openairdocs.org/sdr/ASOA2015070213227.md): Frame · cracked · Jun 10, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605, FRAME AND PREVIOUS USED DOUBLER STRAP CRACKED AT UPPER HOLE LOCATION WHERE STANDOFF SB INSTALLED AFTER INSTALLATION AT RT STR 26 AND RT STR 27. LOCATED AND DRILLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-40-11. INSTALL
- [SDR ASOA2015070213226](https://openairdocs.org/sdr/ASOA2015070213226.md): Floorbeam · corroded · Jun 8, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND AT NUTPLATE LOCATION AT LT FS 561.00, STR 17, BUTT LINE 36 TO 47. COMPLIED WITH EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C.
- [SDR ASOA2015070213225](https://openairdocs.org/sdr/ASOA2015070213225.md): Skin · cracked · Jun 5, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK ACCESS HOLE CUTOUT FOR PANEL 650CB HAS INDICATIONS AROUND CIRCUMFERENCE OF LANDING 55 PERCENT FSH, AREA MARKED ON ACFT, FAILED NDT. REMOVED RT WING FUEL ACCESS FUEL PANEL 650CB IAW AMM TASK 28-11-01-000-802. INSTALLED RT FUEL PANEL 650CB IAW
- [SDR ASOA2015070213224](https://openairdocs.org/sdr/ASOA2015070213224.md): Angle · cracked · Jun 5, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE CRACKED AT FS 622- FS 625, STR 14L ABOUT LBL 40. REMOVED OBLIQUE ANGLE IAW SRM 51-42-20. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE AT FS 622-FS 625, STR 14L, LBL 40 IAW SRM 51-42-20, SRM 51-40-11 AND SRM 51-42-06.
- [SDR ASOA2015070213223](https://openairdocs.org/sdr/ASOA2015070213223.md): Intercostal · cracked · Jun 5, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FS 621-625, STR 14L, ADJACENT TO SKIN, OTBD FLANGE IS CRACKED. REMOVED CRACKED INTERCOSTAL, PN:601R2350121-5 FROM INTERCOSTAL. IN STEP 3 IAW SRM 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL, PN:601R350121-5 IAW SRM 51-40-11. INSTALLED IT ON IN
- [SDR ASOA2015070213222](https://openairdocs.org/sdr/ASOA2015070213222.md): Intercostal · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 349-364, STRINGER 26L IS CORRODED. BLENDED CORROSION FROM INTERCOSTAL 26L AT FS 349-364 MAXIMUM MATERIAL REMOVED.002 IAW SRM 51-21-06, 53-00-00, FIG 102.
- [SDR ASOA2015070213221](https://openairdocs.org/sdr/ASOA2015070213221.md): Splice Plate · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > SPLICE PLATE AT FS 621 RH RBL 41 IS CORRODED. BLENDED CORROSION ON SPLICE PLATE AT FS 621, RBL 41 IAW REO 601R-53-61-4690. MAXIMUM MATERIAL REMOVED.009. REPAIRED FLOOR ANGLE AT FS 621.00 IAW REO 601R-53-61-4690.
- [SDR ASOA2015070213220](https://openairdocs.org/sdr/ASOA2015070213220.md): Skin · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION ON LOWER WING PLANK HOLE, 540BB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEENING REWORKED AREA IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015070213219](https://openairdocs.org/sdr/ASOA2015070213219.md): Skin · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION ON LOWER WING PLANK HOLE, 510AB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEEN OF THE REPAIR SURFACE IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015070113218](https://openairdocs.org/sdr/ASOA2015070113218.md): Skin · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CORRROSION ON LOWER WING PLANK HOLE, 610AB IN SEVERAL AREAS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L-ROTO PEEN OF REWORKED SURFACES IAW SRM 51-24-11. C/W REO 601R-57-21-030. LEAK CHECK GOOD. C/W ECTC EO 600-57-81, C/W IAW
- [SDR ASOA2015070113217](https://openairdocs.org/sdr/ASOA2015070113217.md): Skin · corroded · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION ON LOWER WING PLANK HOLE, 640BB, IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO-PEENING OF REWORK AREAS IAW SRM 51-24-11.
- [SDR ASOA2015070113216](https://openairdocs.org/sdr/ASOA2015070113216.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50, WL 130 APPROX 2.0" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. UPON MILLING OF CARGO DOOR TRACK IAW REO 601R-53-61-5498. REMOVED EXCESS MATERIAL CARGO DOOR TRACK REQUIRES REP
- [SDR ASOA2015070113215](https://openairdocs.org/sdr/ASOA2015070113215.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Structure (General)
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 JUST ABOVE WL 73.50 APPROXIMATELY 1.5 IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. C/W REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621, BULKHEAD LBL 36 IAW REO 60
- [SDR ASOA2015070113214](https://openairdocs.org/sdr/ASOA2015070113214.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 24" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEPS 1-3 OF REO 601R-53-61-5498, REV P1. C/W REO 601R-53-61-5498 P
- [SDR ASOA2015070113213](https://openairdocs.org/sdr/ASOA2015070113213.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 (
- [SDR ASOA2015070113212](https://openairdocs.org/sdr/ASOA2015070113212.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 9.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHAD WEB AT BL 0 IAW REO 601R-53-61-549
- [SDR ASOA2015070113211](https://openairdocs.org/sdr/ASOA2015070113211.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 9.5 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW SEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 9.5. C/W REO
- [SDR ASOA2015070113210](https://openairdocs.org/sdr/ASOA2015070113210.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 18. COMPLET
- [SDR ASOA2015070113209](https://openairdocs.org/sdr/ASOA2015070113209.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 121.43-WL 137.5 APPROXIMATELY 6.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-
- [SDR ASOA2015070113208](https://openairdocs.org/sdr/ASOA2015070113208.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-
- [SDR ASOA2015070113207](https://openairdocs.org/sdr/ASOA2015070113207.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498, P1 AT FS 621, RBL 18. C/W R
- [SDR ASOA2015070113206](https://openairdocs.org/sdr/ASOA2015070113206.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED POSITION OF THE REAR PRESSURE BULKHEAD WEB AT BL 0 IAW REO 601R-53-61-54
- [SDR ASOA2015070113205](https://openairdocs.org/sdr/ASOA2015070113205.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 9.50 BETWEEN WL 73.50-WL 120.43 APPROX 4.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGE PORTION OF THE REAR PRESSURE BULKHEAD WEB AT LBL 9.50 IAW REO 601R-53-61-5498.
- [SDR ASOA2015070113204](https://openairdocs.org/sdr/ASOA2015070113204.md): Bulkhead Web · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 73.50, WL 120.43 APPROXIMATELY 12" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW REO 601R-53-61-5498 P1. INSTALLED AL
- [SDR ASOA2015070113203](https://openairdocs.org/sdr/ASOA2015070113203.md): Post · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69.250", LONG BY 60 FSH. FAILED NDT. REMOVED INBD POST, PN:601R32208-32 AND OTBD POST, PN:601R32208-156 AT FS 409+128, RBL 18 IAW SRM 51-42-06. ASSEMBLED
- [SDR ASOA2015070113202](https://openairdocs.org/sdr/ASOA2015070113202.md): Attach Bracket · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BRACKET ATTACHING FROM STR 3L TO FS 280 IS CRACKED. REMOVED CLEAT IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32.
- [SDR ASOA2015063013198](https://openairdocs.org/sdr/ASOA2015063013198.md): Attach Angle · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STR 3L ATTACHING ANGLES ARE CRACKED JUST AFT OF FS 280. REMOVED ANGLE, PN 600-31057-19 FROM STR 3L AT FS 280 IAW SRM 51-42-06. DRILLED, LOCATED AND INSTALLED NEW ANGLE, PN 600-31057-19 ON STR 3L AT FS 280.0 IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32. REMOVE
- [SDR ASOA2015061213102](https://openairdocs.org/sdr/ASOA2015061213102.md): Post · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 APPROXIMATELY.250" LONG BY 50 PERCENT FSH. BOTH INDICATIONS FAILED NDT. NO OTHER INDICATIONS NOTED. REPAIRED IAW EC/TC, REO:601R-53-41-889.
- [SDR ASOA2015060813069](https://openairdocs.org/sdr/ASOA2015060813069.md): Post · cracked · Jun 3, 2015 · N884AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, BL 0 VERT POST LT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69.250", LONG Y 50 PERCENT FSH, FAILED NDT. REPAIRED IAW ECTC REO 601R-53-41-889.
- [SDR ASOA2015063013197](https://openairdocs.org/sdr/ASOA2015063013197.md): Frame · corroded · Jun 2, 2015 · N884AS · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION ON 605 FRAME FROM STR 27 TO STR 24L. FOUND CORROSION ON FS 605, FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-0
- [SDR ASOA2015063013196](https://openairdocs.org/sdr/ASOA2015063013196.md): Crossbeam · corroded · Jun 2, 2015 · N884AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON CROSSBEAM AT FS 589.00 BETWEEN RBL 9 & LBL 9. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00..021" MATERIAL REMOVED. REPLACEMENT REQUIRED. REMOVED DAMAGED CAP STRIP IAW SRM 51-42-06-00. FABRICATED, LOCATED AND DRILLED NEW SERVIC

Next page: https://openairdocs.org/deregistered/N884AS-2019-11-26/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 = 'N884AS' AND deregistration_id = 'N884AS-2019-11-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N884AS-2019-11-26/reports

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