# Service difficulty reports: N883AS, cancelled Dec 26, 2017

A list on [N883AS, cancelled Dec 26, 2017](https://openairdocs.org/deregistered/N883AS-2017-12-26.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 · 176 reports

- [SDR ASOA2016072915148](https://openairdocs.org/sdr/ASOA2016072915148.md): Battery Pack · discharged · Jul 25, 2016 · N883AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 EMERGENCY LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-04. FUNCTIONAL CHECKED GOOD IAW AMM 33-51-04.
- [SDR ASOA2016050814761](https://openairdocs.org/sdr/ASOA2016050814761.md): Lamp · burned out · May 8, 2016 · N883AS · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS OUT AT PASSENGER DOOR, FWD AND AFT LT EMERGENCY EXIT DOOR AND AFT OF SERVICE DOOR. RELAMPED BULBS AT FWD PAX DOOR AFT OF LT EMERGENCY EXIT DOOR, AND AFT OF SERVICE DOOR IAW AMM 33-51-21.
- [SDR ASOA2016030914571](https://openairdocs.org/sdr/ASOA2016030914571.md): Pseu · unserviceable · Mar 9, 2016 · N883AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON WARNING MESSAGE WITH ASSOCIATED AURAL MSG, GEAR SELECTED DOWN. SHOW BOTH MLG DOWN BUT NLG UP. RAN QRH CYCLED 2 TIMES AND CONDITION WORSEND ALL MML SHOWED UP AND WOULD NO COME DOWN. PERFORMED MANUAL GEAR EXTENSION. ENROUTE, ACFT DIVERTED DU
- [SDR ASOA2016011814383](https://openairdocs.org/sdr/ASOA2016011814383.md): Selector Valve · failed · Jan 18, 2016 · N883AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > MLG DID NOT EXTEND WHEN LANDING GEAR HANDLE EXTENDED. NOSE GEAR DID EXTEND. RAN QRH AND THE LANDING GEAR EXTENDED WHEN EMERGENCY EXTENTION USED. EMERGENCY ACTIONS, LANDING GEAR RETRACTION SYSTEM. R & R MLG SELECTOR VALVE IAW AMM 32-32-10. AIPC 32-32-10, FIG
- [SDR ASOA2015121514265](https://openairdocs.org/sdr/ASOA2015121514265.md): Frame · cracked · Dec 15, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Frame
  > PRIOR TO INSTALLING FASTENERS ON FLANGE OF FRAME 319.00 WHICH WERE REMOVED DUE TO CORROSION. MECHANIC FOUND CRACK AT VERY CORNER FASTENER HOLE. COMPLIED WITH EA 20-2015-363 P1. RECEIVED AND COMPLIED WITH FINAL EA 20-2015-363. RECEIVED AND COMPLIED WITH ECT
- [SDR ASOA2015121414264](https://openairdocs.org/sdr/ASOA2015121414264.md): Door Sill · cracked · Dec 14, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUTOUT LOWER SILL CRACKED AT BS 605. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B.
- [SDR ASOA2015121314263](https://openairdocs.org/sdr/ASOA2015121314263.md): Door Sill · cracked · Dec 13, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUTOUT LOWER SILL CRACKED AT FS 589.00, MARKED. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B, DATED 10/9/2009 AS WRITTEN.
- [SDR ASOA2015121014262](https://openairdocs.org/sdr/ASOA2015121014262.md): Seat Track · corroded · Dec 10, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL9, FS 405 TO 409.00+120. BLENDED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL IAW AMM TASK 53-01-11-000-802. COMPLIED WITH ECTC REO 601R-53-00-485. INSTALLED NEW SERVICEABLE SEAT TRACK
- [SDR ASOA2015120914274](https://openairdocs.org/sdr/ASOA2015120914274.md): Floorbeam · corroded · Dec 9, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UPON REMOVING UPPER COMPOSITE CAP FOR FROM ON JOB 8 OP 9 DISCOVERED ADDITIONAL CORROSION ON AFT LT-ANGLE ON 349 CROSSBEAM, RBL 40. REMOVED UPPER SUPPORT ANGLE FROM 349.00 CROSS BEAM REMOVED, 4 EA SOLID RIVETS AND 6 HILITES THROUGH ATTACHING MOUNT IAW SRM 51-4
- [SDR ASOA2015120914261](https://openairdocs.org/sdr/ASOA2015120914261.md): Skin · corroded · Dec 9, 2015 · N883AS · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK HOLE FUEL PANEL 640BB LAND SURROUND HAS CORROSION/PITTING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. COMPLIED WITH REO 601R-57-21-2392. RECEIVED AND COMPLIED WITH ECTC REO 601R-57-21-2392.
- [SDR ASOA2015120914260](https://openairdocs.org/sdr/ASOA2015120914260.md): Skin · corroded · Dec 9, 2015 · N883AS · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK ACCESS HOLE FOR FUEL PANEL 540BB LAND SURROUND HAS CORROSION PITTING. COMPLIED WITH ECTC EO 000-57-81.
- [SDR ASOA2015120714259](https://openairdocs.org/sdr/ASOA2015120714259.md): Frame · cracked · Dec 7, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333, CRACKED AT STR 1 RT. RECEIVED AND COMPLIED WITH 601R-53-21-2680 PI. REMOVED FRAME AND STARTED DRILLING NEW FRAME IAW SRM 51-42-06 & 51-42-21. DRILLED AND INSTALLED FRAME 333 AT SIGN RT IAW SRM 51-41-11 AND 51-42-06, & 51-42-21 AND DWL 601R 32004.
- [SDR ASOA2015120514258](https://openairdocs.org/sdr/ASOA2015120514258.md): Floor Support · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RT FLOOR SILL BETWEEN FS 559.00+16 & 559.00+32 NEED TO BE EVALUATED. COMPLIED WITH EC/TC REO 601R-53-00-526-01.
- [SDR ASOA2015120514257](https://openairdocs.org/sdr/ASOA2015120514257.md): Floor Support · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LT FLOOR SILL BETWEEN FS 559.00+32 & 559.00+80, NEED TO BE EVALUATED. COMPLIED WITH EC/TC REO 601R-53-00-526.
- [SDR ASOA2015120514256](https://openairdocs.org/sdr/ASOA2015120514256.md): Floor Support · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 & FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C, DATED 11/6/12 AS WRITTEN.
- [SDR ASOA2015120514255](https://openairdocs.org/sdr/ASOA2015120514255.md): Floor Support · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 & FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01, REV A, DATED OCT.23,2013.
- [SDR ASOA2015120514254](https://openairdocs.org/sdr/ASOA2015120514254.md): Angle · cracked · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT FS 280 AND RBL 9. R & R ANGLE WITH SRM 51-42-21-00.
- [SDR ASOA2015120514197](https://openairdocs.org/sdr/ASOA2015120514197.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 BETWEEN FS 559.00 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. R & R SEAT TRACK SECTION AT RBL9, FS 559 AND 559.00+86 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802 AND FABRI
- [SDR ASOA2015120514196](https://openairdocs.org/sdr/ASOA2015120514196.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 BETWEEN FS 559.00 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT LBL9 BETWEEN FS 559.00 AND 559.00+96 IAW AMM 53-01-11-000-802. COMPLIED WITH EC/TC REO
- [SDR ASOA2015120514195](https://openairdocs.org/sdr/ASOA2015120514195.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL BETWEEN FS 605.00 & 621.00 HAS CORROSION THAT NEED TO BE EVALUATED. REMOVED SEAT TRACK AT LBL BETWEEN FS 605.00 AND 621.00 IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK AT LBL BETWEEN FS 605.00 & 612.00 IAW AMM 53-01-11-400-802. COMPLIED
- [SDR ASOA2015120514194](https://openairdocs.org/sdr/ASOA2015120514194.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BETWEEN FS 574.00 & 559.00+112 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT RBL 9 BETWEEN FS 574.00 AND 559.00+112 IAW AMM 53-00-49-000-801. COMPLIED WITH EC/TC R
- [SDR ASOA2015120514193](https://openairdocs.org/sdr/ASOA2015120514193.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 BETWEEN FS 574.00 & 559.00+112 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT RAIL AT LBL9 BETWEEN FS 574.00 AND 559.00+112 IAW AMM 53-00-48-000-801. COMPLIED WITH EC/TC REO
- [SDR ASOA2015120514192](https://openairdocs.org/sdr/ASOA2015120514192.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DEFECT DESCRIPTION: SEAT TRACK AT RBL9 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT RBL9 BETWEEN FS 559.00 AND FS 559.00+96 IAW AMM 53-00-49-000-801.
- [SDR ASOA2015120514191](https://openairdocs.org/sdr/ASOA2015120514191.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01, REMOVED AND REPLACED. REMOVED SEAT RAIL AT LBL9 BETWEEN FS 559+80 AND 559+96 IAW AMM 53-00-48-000-801. COM
- [SDR ASOA2015120514190](https://openairdocs.org/sdr/ASOA2015120514190.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL18 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. R & R SEAT TRACK AT LBL 18 BETWEEN 559+80 AND 559+96 IAW AMM 53-01-11-000-802 AND 53-1-11-400-02 AND FABRI
- [SDR ASOA2015120514189](https://openairdocs.org/sdr/ASOA2015120514189.md): Seat Track · corroded · Dec 5, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT CORRODED ON RBL 9 FROM BS 409 TO 409+128 IN 6 SPOTS. COMPLIED WITH EC/TC REO 601R-53-00-485 FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACKIAW AMM 53-0
- [SDR ASOA2015120414253](https://openairdocs.org/sdr/ASOA2015120414253.md): Floor Support · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL CORRODED AT FS 319.70. R & R ANGLE DOUBLER ON RT FLOOR SILL AT FS 319.70 IAW SRM 31-42-06 AND SRM 51-42-13 AND SRM 51-42-15.
- [SDR ASOA2015120414252](https://openairdocs.org/sdr/ASOA2015120414252.md): Floor Support · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL9 FLOORBEAM FROM FS 405 TO 409.00+120 IS CORRODED AT FS 410 AND FS 409.00+120. AFTER EVALUATION ITS DISCOVERED THAT DAMAGE IS OUT OF LIMITS WITH SRM AND SPLICE REPAIRS ARE REQUIRED. REPAIRED FLOORBEAM AT LBL9, FWD SPLICE FS 409+26-409+5 AND AFT SPLICE FS
- [SDR ASOA2015120414251](https://openairdocs.org/sdr/ASOA2015120414251.md): Floor Support · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOORBEAM TOP CAP CORRODED BETWEEN FS 409 TO FS 409+96 IN 10 SPOTS MOSTLY AROUND SCREW HOLES. REMOVED SEAT RAIL FORM FS 409-FS 409+112. INSTALLED SEAT RAIL FS 409-40-+112 IAW AMM 53-01-11-40-802. BLENDED & REMOVED CORROSION SRM 51-123-00-00 IN 11 LOCA
- [SDR ASOA2015120414250](https://openairdocs.org/sdr/ASOA2015120414250.md): Attach Fitting · cracked · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BROKEN CLEAT AT FS 484.00 & RBL 28 INTERSECT NEED REPLACEMENT. REMOVED BROKEN CLEAT AT FS 484.00 & RBL 28 INTERSECT IAW SRM 51-42-21. INSTALLED SERVICEABLE CLEAT IAW SRM 51-42-21, DWG 601R31171.
- [SDR ASOA2015120414188](https://openairdocs.org/sdr/ASOA2015120414188.md): Seat Track · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG RT SIDE SEAT TRACK BETWEEN BS 449+85 TO 499, COMPLIED WITH EC/TC REO 601R 53-00-055. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2015120414187](https://openairdocs.org/sdr/ASOA2015120414187.md): Seat Track · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT TRACK FROM BS 409+128 - 461. COMPLIED WITH EC/TC REO 601R-53-00-055. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802.
- [SDR ASOA2015120414186](https://openairdocs.org/sdr/ASOA2015120414186.md): Seat Track · corroded · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 544.00 & 559.00+80. COMPLIED WITH EC/TC REO 601R-53-00-055. REMOVED SIDE SEAT TRACK IAW AMM TASK 53-01-11-000-802. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2015120414181](https://openairdocs.org/sdr/ASOA2015120414181.md): Isolator · broken · Dec 4, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD FACE, SEVEN BROKEN INSOLATORS. R & R ISOLATORS IAW SRM 51-42-10.
- [SDR ASOA2015120214249](https://openairdocs.org/sdr/ASOA2015120214249.md): Skin · cracked · Dec 2, 2015 · N883AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK FOUND IN WING PLANK ON LT SIDE AT 148.019, AFT SIDE LOWER PLANK, LENGTH.718. COMPLIED WITH EC/TC REO 601R-57-21-130 & GREO 601R-57-21-130, REV DATED 11/27/2013 AS WRITTEN. COMPLIED WITH EC/TC REO 601R-57-21-131 & GREO 601R-57-21-131, REV DATED 11/27/2
- [SDR ASOA2015120214248](https://openairdocs.org/sdr/ASOA2015120214248.md): Fitting · chafed · Dec 2, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FITTING CHAFED ON FS 364.00 FWD OF THE AVIONIC DOOR, 2EA. REMOVED CHAFE AT FS 364.00 FITTINGS FWD OF THE AVIONICS DOOR, 2EA IAW SRM 51-12-00-00, BLEND LENGTH 1.3" X.5". COMPLIED WITH STS EA 26-2015-203, REV A DATED 12/16/2015. RECEIVED AND COMPLIED WITH ECT
- [SDR ASOA2015120114266](https://openairdocs.org/sdr/ASOA2015120114266.md): Skin · dented · Dec 1, 2015 · N883AS · Cndair CL6002B19 · Wing, Plate/Skin
  > DENT ON RT WING L/E NEAR WING ROOT, REF AFDL FOR INTERM REPAIR IAW STS EA 25-2014-051, PERMANENT REPAIR REQUIRED. DENT ON RT WING L/E NEAR WINGROOT REPAIRED. NO DEFECTS NOTED. RECEIVED DISPOSITION AND COMPLIED WITH EA 26-2015-199. REMOVED L/E INNER SKIN
- [SDR ASOA2015110113989](https://openairdocs.org/sdr/ASOA2015110113989.md): Support Angle · damaged · Nov 1, 2015 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EXT POWER RECEPTACLE AFT SUPPORT ANGLE DAMAGED. REMOVED DAMAGE BRACKET. DRILLED UP NEW BRACKET IAW REO 601R-53-11-009. INSTALLED THE SUPPORT ANGLE IAW REO 601R-53-11-009. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3.
- [SDR ASOA2015110113988](https://openairdocs.org/sdr/ASOA2015110113988.md): Bracket · damaged · Nov 1, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > EXT POWER RECEPTACLE SUPPORT BRACKET DAMAGE. REMOVED DAMAGE BRACKET. DRILLED UP NEW BRACKET IAW REO 601R-53-11-009. INSTALLED THE BRACKET IAW REO 601R-53-11-009. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.
- [SDR ASOA2015110113987](https://openairdocs.org/sdr/ASOA2015110113987.md): Plate · damaged · Nov 1, 2015 · N883AS · Cndair CL6002B19 · Fuselage Main, Structure
  > EXT POWER RECEPTACLE DAMAGE. FABRICATED JOGGLE PLATE IAW REO 601R-53-11-009. INSTALLED IAW REO 601R-53-11-009. MAJOR REPAIR IAW GMM 5-3.
- [SDR ASOA2015062613178](https://openairdocs.org/sdr/ASOA2015062613178.md): Glowstrip · deteriorated · Jun 22, 2015 · N883AS · Cndair CL6002B19 · Emergency Equipment
  > PHOTOLUMINESCENT FROM ROW 1CD TO ROW 8CD WATER DAMAGED. R & R PHOTOLUMINESCENT INSERT FROM ROW 1CD TO ROW 8CD IAW STC ST02687AT.
- [SDR ASOA2015031812416](https://openairdocs.org/sdr/ASOA2015031812416.md): Wire · damaged · Mar 14, 2015 · N883AS · Cndair CL6002B19 · Light System Wiring
  > LIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE LT SIDE OF GALLEY. R & R WIRE SPLICE CONNECTOR IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014110711613](https://openairdocs.org/sdr/ASOA2014110711613.md): Windshield · failed · Nov 5, 2014 · N883AS · Cndair CL6002B19 · Flight Compartment Windows
  > F/O WINDSHIELD BEGAN ARCING AND SMALL CRACK, RAN QRH PROCEDURE 11-14, WINDSHIELD SHATTERED ONE MINUTE LATER. REMOVED AND REPLACED THE F/O'S WINDSHIELD IAW AMM 56-11-01. OPS AND LEAK CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2014081211037](https://openairdocs.org/sdr/ASOA2014081211037.md): Light · inoperative · Aug 8, 2014 · N883AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT BELOW F/A JUMPSEAT IS INOPERATIVE AND ITS WIRING HARNESS IS NOT TIED DOWN. R & R THE LIGHT IAW AMM 33-51-10.
- [SDR ASOA2014080611008](https://openairdocs.org/sdr/ASOA2014080611008.md): Bulb · burned out · Aug 2, 2014 · N883AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT FORWARD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R RT FWD EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013121709653](https://openairdocs.org/sdr/ASOA2013121709653.md): Fitting · damaged · Dec 7, 2013 · N883AS · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG FWD DOOR SPACER FITTING HAS ELONGATED HOLE ON FUSLAGE SIDE. REPAIRED IAW EC/TC REO 601R-57-21-2059. MAJOR REPAIR.
- [SDR ASOA2013121309626](https://openairdocs.org/sdr/ASOA2013121309626.md): Light · unserviceable · Nov 30, 2013 · N883AS · Cndair CL6002B19 · Emergency Lighting
  > NUMEROUS COMPONENTS OF THE EMERGENCY TRACK LIGHTS FOUND UNSERVICEABLE. INSTALLED SERVICEABLE COVERS IAW ASA 33-51-00 SUPPLEMENT AND SAFETGLO MM 41-10, 33-60-10.
- [SDR ASOA2013121309625](https://openairdocs.org/sdr/ASOA2013121309625.md): Floor Support · corroded · Nov 27, 2013 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MINOR CORROSION FOUND AROUND FASTENER HOLES ALONG RT FLOOR SUPPORT RBL 17 BETWEEN BS 559 + 48 TO FS 559 + 112. REPAIRED FLOOR SUPPORT IAW GREO 601R-53-00-526 AND EC/TC REO601R-53-00-526. MAJOR REPAIR.
- [SDR ASOA2013121309624](https://openairdocs.org/sdr/ASOA2013121309624.md): Seat Track · corroded · Nov 24, 2013 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 364 TO 394, RBL 9 CORRODED IN VARIOUS AREAS. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2013121309623](https://openairdocs.org/sdr/ASOA2013121309623.md): Seat Track · corroded · Nov 24, 2013 · N883AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 364 TO 394, LBL 9 IS CORRODED IN VARIOUS PLACES. R & R SEAT TRACK IAW AMM 53-01-11-946-003 AND 53-01-11-420-001.

Next page: https://openairdocs.org/deregistered/N883AS-2017-12-26/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 = 'N883AS' AND deregistration_id = 'N883AS-2017-12-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N883AS-2017-12-26/reports

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