# Service difficulty reports: N851AS, cancelled Jul 30, 2018

A list on [N851AS, cancelled Jul 30, 2018](https://openairdocs.org/deregistered/N851AS-2018-07-30.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 · 154 reports

- [SDR ASOA2016080315154](https://openairdocs.org/sdr/ASOA2016080315154.md): Sensor · out of adjust · Jul 30, 2016 · N851AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > DURING DEPARTURE, SELECTED GEAR HANDLE UP AND RECEIVED GEAR DISAGREE FOLLOWED BY NOSE DOOR WARNING MESSAGE. NOSE GEAR WAS NOT UP. FOLLOWED QRH AND PULL EMERGENCY EXT. NOSE GEAR DOWN AND LOCKED. RETURNED TO DEPARTURE AND LANDED NORMALLY. FOUND NLG WEIGHT OFF W
- [SDR ASOA2016071715113](https://openairdocs.org/sdr/ASOA2016071715113.md): Door · unknown · Jul 17, 2016 · N851AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WOULD NOT OPEN FROM INSIDE. PERFORMED OPERATIONAL TEST OF THE MAIN PAX DOOR IAW AMM 52-11-02, OPS CHECK NORMAL, NO DEFECTS NOTED. OK FOR SERIVCE.
- [SDR ASOA2016040514693](https://openairdocs.org/sdr/ASOA2016040514693.md): Battery Pack · discharged · Apr 5, 2016 · N851AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT IS DEAD. REPLACED BATTERIES IN F/A`S FLASHLIGHT.
- [SDR ASOA2016010214302](https://openairdocs.org/sdr/ASOA2016010214302.md): Seat Track · corroded · Jan 2, 2016 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM FS559.00-FS559.00+80 AT LBL9 IS CORRODED AS REPORTED BY MAINTENANCE. REMOVED CORROSION IAW SRM 51-21-06-00, SEAT TRACK OUT OF LIMITS IAW SRM 53-51-49. REMOVED SEAT TRACK IAW SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802. COMP
- [SDR ASOA2015123014325](https://openairdocs.org/sdr/ASOA2015123014325.md): Skin · cracked · Dec 30, 2015 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING FASTENER HOLE INSPECTION OF RT LOWER WING PLANK 1EA HOLE HAS CRACK INDICATION. RECEIVED & COMPLIED WITH ADR JLEB-15-3626196, REF SRM 51-40-11. RECEIVED & COMPLIED WITH FINAL REO 601R-57-21-2394. RECEIVED & COMPLIED WITH ECTC REO 601R57-21-2394.
- [SDR ASOA2015123014301](https://openairdocs.org/sdr/ASOA2015123014301.md): Seat Track · corroded · Dec 30, 2015 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL BETWEEN FS 409.00+128 AND FS559.00 AT RBL 9 IS CORRODED. EVALUATED AND FOUND DAMAGE TO BE OUT OF LIMITS REF SRM 53-41-49. R & R SEAT RAIL BETWEEN FS 409.00+128 AND FS 559.00 AT RBL 9 REF COMPLIED WITH GREO 601R-53-00-485, REV A, AMM 53-01-11-
- [SDR ASOA2015123014300](https://openairdocs.org/sdr/ASOA2015123014300.md): Seat Track · corroded · Dec 30, 2015 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL BETWEEN FS 409.00+128 AND FS 559.00 AT LBL9 IS CORRODED. REMOVED SEAT RAIL BETWEEN FS 409 + 128 & FS 559.00, LBL 9 IAW AMM 53-01-11-000-802. INSTALLED SEAT RAIL BETWEEN FS 409+128-FS 559.00 IAW AMM 53-01-11-400 802. FINISHED COUNTERSINKING & INST
- [SDR ASOA2015122814320](https://openairdocs.org/sdr/ASOA2015122814320.md): Floor Support · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOORBEAM, OTBD SIDE, FS 589.00-605.00 AND LBL9. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00. REMOVED FLOOR SUPPORT BEAM CAP IAW SRM 51-42-21, 51-42-06. STARTED INSTALLATION OF LT SIDE OF NEW SERVICABLE FLOOR SUPPORT BEAM CA
- [SDR ASOA2015122814319](https://openairdocs.org/sdr/ASOA2015122814319.md): Structure · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND RBL4.0 SILL AT 559+80-559.00+96. BLENDED CORROSION IAW SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REC, DATED 05-22-2013 AS WRITTEN.
- [SDR ASOA2015122814318](https://openairdocs.org/sdr/ASOA2015122814318.md): Frame · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND AROUND SCREW HOLES AT FS 559.00+69 AND 559.00+80 RBL9 ON OTBD SIDE. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00 AT FS 559+69 AND 559+80 RBL9. REPAIRED FLOORBEAM AT FS 559.00+69 TO 559.00+80 RBL9 IAW SRM 53-00-43 FLOOR SUPPORT
- [SDR ASOA2015122814310](https://openairdocs.org/sdr/ASOA2015122814310.md): Seat Track · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK AT 559.00+ 559.00+96 AND RBL 27. EVLAUATED AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-51-49. R & R SEAT RAIL BETWEEN FS 559.00+80 AND 559.00+96, RBL 27, REF: AMM 53-01-11-000-802 AND 53-01-11-400-802. FABRICATED SEAT RAILS
- [SDR ASOA2015122814309](https://openairdocs.org/sdr/ASOA2015122814309.md): Seat Track · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK BETWEEN 559.00+80 TO 559.00+98 AND RBL 9. REMOVED SEAT TRACK FROM FS 559.+87 TO 559+96 RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK BETWEEN FS 559.+80 AND FS 559.00+96 AT RBL9 REF: AMM 53-01-11-400-802. REMOVED SEAT
- [SDR ASOA2015122814299](https://openairdocs.org/sdr/ASOA2015122814299.md): Seat Track · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND FOUND ON SEAT TRACK AT FS559.00+112-574.00, LBL9. REMOVED CORROSION IAW SRM 51-21-06-00. SEAT TRACK OUT OF LIMITS IAW SRM 53-61-49. REMOVED SEAT TRACK IAW SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC
- [SDR ASOA2015122814291](https://openairdocs.org/sdr/ASOA2015122814291.md): Plate · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND TIE DOWN BLOCK AT BS 574 - 589 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.
- [SDR ASOA2015122814290](https://openairdocs.org/sdr/ASOA2015122814290.md): Plate · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND TIE DOWN BLOCK AT BS 589 - 605 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.
- [SDR ASOA2015122814289](https://openairdocs.org/sdr/ASOA2015122814289.md): Plate · corroded · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON TIE DOWN LOCK AT FS559+96-559-.00+112 AND F, LBL27. R & R ANCHOR PLATE AT 559.00+96-559.00+112 AND LBL27 IAW SRM 51-41-02. UPON REPLACMENT OF ANCHOR PLATE AT 559.00+96-559.00+112, LBL27 FOUND ANCHOR PLATE FWD OF THAT TO BE CORRODED ALSO. R
- [SDR ASOA2015122814288](https://openairdocs.org/sdr/ASOA2015122814288.md): Door Sill · cracked · Dec 28, 2015 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKS FOUND ON CARGO DOOR SILL AT FS589.00 AND 605.00 AND LBL 4.0. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B, DATED 10/9/2009 AS WRITTEN.
- [SDR ASOA2015122114308](https://openairdocs.org/sdr/ASOA2015122114308.md): Skin · cracked · Dec 21, 2015 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK CRACKED AT WS 148.019. REMOVED RT INBD LOWER T/E INBD OF "PIE PANEL" IAW SRM 51-42-21, 51-42-06. INSTALLED INBD LOWER T/E INBD OF "PIE PANEL", REF SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R10225. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO
- [SDR ASOA2015121214212](https://openairdocs.org/sdr/ASOA2015121214212.md): Lamp · burned out · Dec 12, 2015 · N851AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT EXTERIOR EMERGENCY LIGHT NR 2 INOPERATIVE. RELAMPED RT EXTERIOR EMERGENCY LIGHT NR 2 IAW AMM 33-51-21. OPS CHECK GOOD.
- [SDR ASOA2015050412744](https://openairdocs.org/sdr/ASOA2015050412744.md): Battery Pack · inoperative · May 1, 2015 · N851AS · Cndair CL6002B19 · Emergency Lighting
  > AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-24-400-801. OPS CHECK GOOD IAW AMM 33-51-00-710-801. VERIFIED NR 2 EMERGENCY LIGHT BATTERY IS EFFECTIVE FOR INSTALLATION ON THIS ACFT IAW AMM SUPPLEMENT 33-
- [SDR ASOA2015050412743](https://openairdocs.org/sdr/ASOA2015050412743.md): Bulkhead · cracked · Apr 26, 2015 · N851AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 2 INDICATIONS NOTED AT 621 REAR PRESSURE BULKHEAD FWD FACE AT BL 0.0, WL 110 APPROXIMATELY 1.350" IN LENGTH VERTICALLY AND 90 PERCENT FULL SCREEN HEIGHT INDICATION AND WL 108 APPROXIMATELY.250 IN LENGTH VERTICALLY AT 20 PERCENT FULL SCREEN HEIGHT. FAILING NDT
- [SDR ASOA2015050412742](https://openairdocs.org/sdr/ASOA2015050412742.md): Stiffener · cracked · Apr 25, 2015 · N851AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT VERTICAL MEMBER, PN:601R35027-31, CRACKED APPROXIMATELY 5" LONG INSIDE OF DOOR FS 605. REMOVED AFT VERTICAL MEMBER IAW SRM 51-42-06. INSTALLED NEW AFT VERTICAL MEMBER IAW SRM 51-42-06. LOCATED AND DRILLED NEW AFT VERTICAL MEMBER IAW SRM 51-40
- [SDR ASOA2014101711438](https://openairdocs.org/sdr/ASOA2014101711438.md): Skin · burned · Oct 14, 2014 · N851AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ONE BURNED FASTENER ON BS 265 STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC REO 601R-53-00-115. WET INSTALLED TEMP FASTENER, CR3222 4-3 IAW REO 601R-53-00-115, REV E. RESTORED SURFACE FINI
- [SDR ASOA2014101711437](https://openairdocs.org/sdr/ASOA2014101711437.md): Skin · damaged · Oct 14, 2014 · N851AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ONE BURN LOCATED 1 INCH AFT OF BS 235 AND ON STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC REO 601R-53-00-115 WET INSTALLED TEMP FASTENER, CR3222 5-4 IAW REO 601R-53-00-115, REV E. RESTOR
- [SDR ASOA2014091811257](https://openairdocs.org/sdr/ASOA2014091811257.md): Flashlight · inoperative · Sep 14, 2014 · N851AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.
- [SDR ASOA2014091211217](https://openairdocs.org/sdr/ASOA2014091211217.md): Skin · damaged · Sep 11, 2014 · N851AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AND HOLE IN FUSELAGE SKIN BETWEEN BS 654-672 AND STRINGERS 26 - 27R. FOUND DAMAGE TO BE IN A NON-REPAIRABLE LOCATION IAW SRM 53-00-31. SUBMITTED DAMAGE REPORT TO STS IAW SRM TR 51-27. RECEIVED EA 12-2014-219, P1, 09/11/2014. CUT AWAY DAMAGED SECTION, PU
- [SDR ASOA2013122409687](https://openairdocs.org/sdr/ASOA2013122409687.md): Cable · loose · Dec 21, 2013 · N851AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PAX DOOR IS JAMMED, WILL ONLY OPEN ABOUT 1 FOOT. FOUND CABLE OFF OF PULLEY INSTALLED PAX DOOR ASSIST CABLE IAW AMM 52-11-08, OPS CHECK GOOD.
- [SDR ASOA2013080608834](https://openairdocs.org/sdr/ASOA2013080608834.md): Bulb · burned out · Aug 4, 2013 · N851AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. R & R BULB IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA2013071708716](https://openairdocs.org/sdr/ASOA2013071708716.md): Wire · broken · Jul 1, 2013 · N851AS · Cndair CL6002B19 · Light System Wiring
  > WIRE BROKEN AT CONNECTOR FOR EMERGENCY LIGHT ON SERVICE DOOR SURROUND PANEL 232BZ. REPAIRED WIRE IAW ECSPM 20-17-00. OPS CHECKED GOOD IAW AMM 31-51-00-710-801.
- [SDR ASOA2013071708715](https://openairdocs.org/sdr/ASOA2013071708715.md): Structure · misrepaired · Jun 21, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE WORKING SB 601R-25-187, FOUND REPAIR AT LBL 27 TO HAVE BEEN DONE INCORRECTLY. REPAIRED IAW SRM 51-42-21 AND REO 601R-53-61-4939.
- [SDR ASOA2013071708714](https://openairdocs.org/sdr/ASOA2013071708714.md): Angle · cracked · Jun 9, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL ANGLE AT LBL 27.50 ON FWD SIDE OF THE ENG BEAM IS CRACKED AT THE BOTTOM OF THE ANGLE APPROX 1"L. REMOVED CRACKED ANGLE AT LBL 27.50 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED SERVICEABLE ANGLE AT LBL 27.50 IAW SRM 51-40-11. INSTALLED
- [SDR ASOA2013071708713](https://openairdocs.org/sdr/ASOA2013071708713.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT FUEL ACCESS HOLE 540EB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708712](https://openairdocs.org/sdr/ASOA2013071708712.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS HOLE 650CB FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT ON FWD SIDE OF HOLE. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708711](https://openairdocs.org/sdr/ASOA2013071708711.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS HOLE 650DB FAILS NDT WITH INDICATIONS ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708710](https://openairdocs.org/sdr/ASOA2013071708710.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS HOLE 640DB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708709](https://openairdocs.org/sdr/ASOA2013071708709.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS HOLE 650BB FAILS NDT WITH AN INDICATION ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708708](https://openairdocs.org/sdr/ASOA2013071708708.md): Skin · cracked · Jun 5, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS HOLE 650AB FAILS NDT WITH AN INDICATION ON FWD INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.
- [SDR ASOA2013071708707](https://openairdocs.org/sdr/ASOA2013071708707.md): Skin · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK ACCESS HOLE AT WS 54.897, HOLE NR 1 AT PANEL LOCATION 540BB HAS PITTING CORROSION AT FORWARD AND AFT ENDS IN THE CRITICAL REGIONS. DEEPEST AREA IS APPROXIMATE.003" DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR ASOA2013071708706](https://openairdocs.org/sdr/ASOA2013071708706.md): Sill · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL IS CORRODED. REPAIRED IAW SRM 51-42-21, 51-40-11, 51-42-21, 51-42-10, 52-142-00.
- [SDR ASOA2013071708705](https://openairdocs.org/sdr/ASOA2013071708705.md): Mount · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > GALLEY FWD INBD AND AFT INBD FLOOR STRUCTURE MOUNT PLATES AT FS 295 AND 315 RBL 5 CORRODED AND FWD OTBD MOUNT PLATE AT FS 285 RBL 36 CORRODED. REPAIRED IAW EO 601R38669 AND 51-42-06 & 51-42-10.
- [SDR ASOA2013071708704](https://openairdocs.org/sdr/ASOA2013071708704.md): Intercostal · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER COMPARTMENT INTERCOSTAL AT FS 349 RBL 36.45 CORRODED. REPAIRED IAW REO 601R-53-21-2439.
- [SDR ASOA2013071708703](https://openairdocs.org/sdr/ASOA2013071708703.md): Angle · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER COMPARTMENT FLOOR SILL CORRODED AT RBL 45 FROM BS 310 - 364 TO INCLUDE SERVICE DOOR SILL ANGLE. REPAIRED IAW SRM 51-40-11, 51-42-06.
- [SDR ASOA2013071708702](https://openairdocs.org/sdr/ASOA2013071708702.md): Seat Track · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER COMPARTMENT SEAT TRACK AT RBL 9 CORRODED FROM FS 364 THRU 409+128. R & R SEAT TRACK IAW SRM 51-41-00/51-40-11.
- [SDR ASOA2013071708701](https://openairdocs.org/sdr/ASOA2013071708701.md): Seat Track · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER COMPARTMENT SEAT TRACK AT LBL 9 CORRODED FROM FS 364 THRU 409+128. REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802, SRM 51-40-11.
- [SDR ASOA2013071708700](https://openairdocs.org/sdr/ASOA2013071708700.md): Frame · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME BS 333 CORRODED ON FWD AND AFT SIDES BETWEEN STR 26L AND STR 26R. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013071708699](https://openairdocs.org/sdr/ASOA2013071708699.md): Frame · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME BS 319.7 CORRODED ON FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME SECTOR IAW SRM 51-42-06, 51-42-21. DRILL & LOCATED 319.70 FRAME SECTOR IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE FRAME IAW SRM 51-42-06 AND 51-42-
- [SDR ASOA2013071708698](https://openairdocs.org/sdr/ASOA2013071708698.md): Frame · corroded · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME BS 310 CORRODED ON THE FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FRAME SEGMENT.
- [SDR ASOA2013071708697](https://openairdocs.org/sdr/ASOA2013071708697.md): Intercostal · cracked · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED FROM FS 621-625 AT S13L. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 521-40-06 AND 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2013071708696](https://openairdocs.org/sdr/ASOA2013071708696.md): Angle · cracked · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE CRACKED AT FS 621-626 AT S14L. REMOVED OBLIQUE ANGLE IAW SRM 51-42-21. DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.
- [SDR ASOA2013071708695](https://openairdocs.org/sdr/ASOA2013071708695.md): Stringer · cracked · Jun 3, 2013 · N851AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STRINGER 3L IS CRACKED AT FS 280. R & R ONE STRINGER IAW 51-42-21-00 AND 51-42-06-00.

Next page: https://openairdocs.org/deregistered/N851AS-2018-07-30/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 = 'N851AS' AND deregistration_id = 'N851AS-2018-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N851AS-2018-07-30/reports

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