# Service difficulty reports: N833AS, cancelled Apr 25, 2017 A list on [N833AS, cancelled Apr 25, 2017](https://openairdocs.org/deregistered/N833AS-2017-04-25.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 · 169 reports - [SDR ASOA2015072813396](https://openairdocs.org/sdr/ASOA2015072813396.md): Battery Pack · inoperative · Jul 28, 2015 · N833AS · Cndair CL6002B19 · Emergency Lighting > OVERWING EMERGENCY LIGHTS ON LT AND RT SIDES INOPERATIVE. R & R THE NR 3 BATTERY PACK IAW AMM 33-51-04. REF IPC 33-51-04, ITEM 137. OPS CHECKED GOOD. - [SDR ASOA2013121109609](https://openairdocs.org/sdr/ASOA2013121109609.md): Lamp · burned out · Dec 7, 2013 · N833AS · Cndair CL6002B19 · Emergency Lighting > RT SIDE FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD. - [SDR ASOA2013103009315](https://openairdocs.org/sdr/ASOA2013103009315.md): Smoke Warning · illuminated · Oct 29, 2013 · N833AS · Cndair CL6002B19 · Smoke Detection > SMOKE INDICATION, CARGO SMOKE WARNING, BLEW CARGO BOTTLE, AND DIVERTED. - [SDR ASOA2013091209000](https://openairdocs.org/sdr/ASOA2013091209000.md): Light · inoperative · Sep 8, 2013 · N833AS · Cndair CL6002B19 · Emergency Lighting > THE EXTERIOR EMERGENCY FLOODLIGHT AFT OF THE RT WING EMERGENCY EXIT IS INOPERATIVE. R & R THE FLOODLIGHT IAW AMM 33-51-21-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801. - [SDR ASOA2013091208999](https://openairdocs.org/sdr/ASOA2013091208999.md): Skin · cracked · Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT INBD SIDE APPROX 8" LT 60 PERCENT SCREEN HEIGHT (X.250). REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K. - [SDR ASOA2013091208998](https://openairdocs.org/sdr/ASOA2013091208998.md): Skin · cracked · Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT AROUND ENTIRE HOLE. REPAIRED IAW REO 601R-57-21-1992, ECTC EO 600-57-81 AND REO 601R-57-21-030, REV K. - [SDR ASOA2013091208997](https://openairdocs.org/sdr/ASOA2013091208997.md): Skin · cracked · Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT MULTIPLE INDICATIONS INBD SIDE OF HOLE 50 PERCENT SCREEN HEIGHT. 1" L X.250. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K. - [SDR ASOA2013091208996](https://openairdocs.org/sdr/ASOA2013091208996.md): Skin · cracked · Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT INBD SIDE 50 PERCENT SCREEN HEIGHT.200 X.200. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K. - [SDR ASOA2013091208995](https://openairdocs.org/sdr/ASOA2013091208995.md): Skin · cracked · Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT WITH INDICATION ON INBD SIDE OF HOLE 2" L X.200 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K. - [SDR ASOA2013091208994](https://openairdocs.org/sdr/ASOA2013091208994.md): Skin · cracked · Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT AFT SIDE OF HOLE.200 X.200, 60 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K. - [SDR ASOA2013091208993](https://openairdocs.org/sdr/ASOA2013091208993.md): Skin · cracked · Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SKIN FAILS NDT INDICATIONS INBD & OTBD SIDE OF HOLE.500 X.250 70 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K. - [SDR ASOA2013091208992](https://openairdocs.org/sdr/ASOA2013091208992.md): Angle · cracked · Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing Miscellaneous Structure > LT WING HAS A CRACKED ANGLE JUST FWD & INBD OF MLG. REMOVED 601R10213-11, ANGLE TO REPLACE WITH NEW ANGLE IAW SRM. INSTALLED ANGLE, PN 601R10213-11 IAW SRM 51-42-06, COUNTERSUNK & ALODINED SRM 51-21-00 & 51-40-11. - [SDR ASOA2013091208991](https://openairdocs.org/sdr/ASOA2013091208991.md): Structure · cracked · Aug 21, 2013 · N833AS · Cndair CL6002B19 · Wing, Attach Fittings > RIGHT BOOST PUMP CUTOUT HOLE FAILS NDT WITH INDICATIONS ON AFT SIDE OF HOLE ON LANDING, GREATER THAN 50 PERCENT SCREEN HEIGHT, APROX 1. ALSO, HAS SMALLER INDICATIONS AROUND ENTIRE HOLE LANDING 10-20 PERCENT SCREEN HEIGHT APROX.1. REPAIRED IAW REO 601R-57-21- - [SDR ASOA2013091208990](https://openairdocs.org/sdr/ASOA2013091208990.md): Skin · cracked · Aug 21, 2013 · N833AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FOUND CARGO DOOR LOWER AFT CORNER FUSELAGE SKIN HAS INDICATION NOTED APRPOX.1" IN LENGTH 90 PERCENT FSH AT THIS LOCATION. IT ALSO, HAS PROTRUDING DENT.2" L X.2 W. FAILED NDT INSPECTION. REPAIRED IAW EO NR: CL 600-2B19-53-I00396 AND REO 601R-53-61-5011, - [SDR ASOA2013083008937](https://openairdocs.org/sdr/ASOA2013083008937.md): Trunnion · cracked · Aug 19, 2013 · N833AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings > INDICATION NOTED IN RT SIDE TURNNION FITTING FASTENER HOLE, 6TH HOLE AFT 9 INDICATION NOTED IN TRUNNION FITTING. 60 PERCENT FULL SCREEN HEIGHT AT OTBD SIDE OF HOLE APPROX.20 IN LENGTH, HOLE FAILS NDT. REPAIRED IAW REO NR 601R-57-21-1988. - [SDR ASOA2013082808923](https://openairdocs.org/sdr/ASOA2013082808923.md): Post · cracked · Aug 19, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 409.128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69, REPAIRED IAW REO 601R-53-41-889. - [SDR ASOA2013091208989](https://openairdocs.org/sdr/ASOA2013091208989.md): Skin · cracked · Aug 16, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/Skin > SUSPECT CRACK AT RT WING WS 148.019, EXTENDING OUT FROM A FASTENER. SUSPECTED CRACK IS LOCATED AFT OF THE AFT WING SPAR BESIDE THE PIE PANEL AND DIRECTLY BELOW THE FLAP FLEX SHAFT. ITEM REQUIRES FURTHER INVESTIGATION. REPAIRED IAW SRM 51-42-06, SRM 51-42-2 - [SDR ASOA2013082808922](https://openairdocs.org/sdr/ASOA2013082808922.md): Post · cracked · Aug 15, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 409+128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06 AND 51-42-22. - [SDR ASOA2013082208898](https://openairdocs.org/sdr/ASOA2013082208898.md): Post · cracked · Aug 15, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LBL 18 FS 409+128 OTBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX.250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED OTBD & INBD VERT POST AT FS 409+128 LBL 18 IAW SRM 51-42-06. LOCATED AND DRILLED NEW POSTS AND 601R - [SDR ASOA2013091208988](https://openairdocs.org/sdr/ASOA2013091208988.md): Hinge · gouged · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Door Hinge > PAX DOOR HINGE HALF ON FUSELAGE HAS ONE GOUGED LUG. LUG IS NEXT TO LAST LUG ON AFT END APPROX.025" L X.004" DEEP. REPAIRED IAW REO 601R-53-21-814, TYPE 1. MAJOR REPAIR. - [SDR ASOA2013091208987](https://openairdocs.org/sdr/ASOA2013091208987.md): Skin · dented · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Spoilers > LT WING INBD GROUND SPOILER LOWER INBD SKIN HAS 2 EA DENTS APPROX.100 L X.100 W X.030 D. REPAIRED IAW REO 601R-57-71-382, REV "A". - [SDR ASOA2013083008936](https://openairdocs.org/sdr/ASOA2013083008936.md): Skin · chafed · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Ailerons > LEFT AILERON UPPER FIXED L/E IS CHAFED AT THREE LOCATIONS APPROX 6.0 INCHES LONG,.400 INCHES WIDE AND.012 INCHES DEEP. REPAIRED IAW REO 601R-57-60-013. - [SDR ASOA2013082208897](https://openairdocs.org/sdr/ASOA2013082208897.md): Seat Track · corroded · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK FS 409 AND 409+128 CORRODED IN SEVERAL AREAS. REMOVED CABIN SEAT TRACK IAW AMM 53-01-11-00-802. LOCATED & INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802 AND SRM 51-40-11. - [SDR ASOA2013082208896](https://openairdocs.org/sdr/ASOA2013082208896.md): Seat Track · corroded · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK FS 349 AND FS 409 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW 53-01-11-000-802. DRILLED DEBURRED IAW AMM 53-01-11-400-802. INSTALLED NEW SEAT TRACK IAW 53-01-11-400-802. INSTALLED RT SEAT TRACK IAW AMM 53-01-11-400-802. - [SDR ASOA2013082208895](https://openairdocs.org/sdr/ASOA2013082208895.md): Angle · corroded · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 280.00 FWD J ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21. - [SDR ASOA2013082208894](https://openairdocs.org/sdr/ASOA2013082208894.md): Angle · cracked · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > BS 484 ANGLE AT RBL 27 IS CRACKED. R & R CRACKED CLIP WITH NEW IAW SRM 51-42-21 AND 51-40-11. - [SDR ASOA2013082208893](https://openairdocs.org/sdr/ASOA2013082208893.md): Angle · cracked · Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT BS 484 ANGLE AT LBL 27 IS CRACKED. R & R CRACKED ANGLE WITH NEW IAW SRM 51-42-21 AND 51-40-11. - [SDR ASOA2013062103863](https://openairdocs.org/sdr/ASOA2013062103863.md): Flashlight · intermittent · Jun 17, 2013 · N833AS · Cndair CL6002B19 · Emergency Equipment > PILOT FLASHLIGHT WORKS INTERMITTENTLY. R & R CAPTAIN'S FLASHLIGHT IAW AMM 25-61-04, OPS CHECKED GOOD. - [SDR ASOA2012091202190](https://openairdocs.org/sdr/ASOA2012091202190.md): Inverter · unserviceable · Sep 8, 2012 · N833AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8A HALF LIGHT. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD. - [SDR ASOA2012091202189](https://openairdocs.org/sdr/ASOA2012091202189.md): Lamp · burned out · Sep 8, 2012 · N833AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8D INOPERATIVE. R & R LAMP IAW AMM 33-51-13. OPS CHECKED GOOD. - [SDR ASOA2011121702377](https://openairdocs.org/sdr/ASOA2011121702377.md): Relay · failed · Dec 17, 2011 · N833AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS FLICKERING. R & R ACCESS BUSS UNDER VOLTAGE RELAY (K1XD) IAW AMM 24-51-27. OPS CHECKED GOOD. OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-01. OPS CHECKED GOOD. - [SDR ASOA201101517](https://openairdocs.org/sdr/ASOA201101517.md): Wire · misinstalled · Aug 8, 2011 · N833AS · Cndair CL6002B19 · Light System Wiring > LOWER EMERGENCY LIGHT AT LT OVERWING EXIT IS INOPERATIVE. TROUBLESHOOT AND FOUND SPLICES ON WIRES MISSING. INSTALLED 2 NEW QUICK DISCONNECT SPLICES ON THE EMERGENCY LIGHT WIRES IAW ESPM CH 20-11-00 AND 20-16-00. PERFORMED OPS TEST OF LIGHTS IAW AMM 33-51-00 - [SDR ASOA201101486](https://openairdocs.org/sdr/ASOA201101486.md): Crossbeam · corroded · Aug 8, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Structure > CORROSION FOUND ON FS 349 CROSSBEAM AT SERVICE DOOR. REPAIRED IAW REO 601R-53-61-1541. - [SDR ASOA201101480](https://openairdocs.org/sdr/ASOA201101480.md): Sign · inoperative · Aug 5, 2011 · N833AS · Cndair CL6002B19 · Emergency Lighting > RT SERVICE DOOR EXIT SIGN BETA LIGHTS HAS AN LIGHT INTENSITY LESS THAN 100. REMOVED AND REPLACED IAW AMM 33-51-09-400-802. FUNCTIONAL TESTED GOOD IAW AMM TASK 33-51-09-720-801. - [SDR ASOA201101460](https://openairdocs.org/sdr/ASOA201101460.md): Pressure Blkhd · cracked · Aug 5, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > REAR PRESSURE BULKHEAD IS CRACKED ABOVE CARGO DOOR, OVER AFT TRACK. PRESSURE BULKHEAD REPAIRED IAW ARM 51-52-06. - [SDR ASOA201101459](https://openairdocs.org/sdr/ASOA201101459.md): Pressure Panel · misrepaired · Aug 5, 2011 · N833AS · Cndair CL6002B19 · Fuselage Floor Panel > PRESSURE FLOOR DOUBLER CORRODED AFT OF FS 439.00 RBL43. APPEARS TO BE 10F6 UNDOCUMENTED DOUBLERS INSTALLED ON PRESSURE FLOOR. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3, MINIMUM MATERIAL RE - [SDR ASOA201101467](https://openairdocs.org/sdr/ASOA201101467.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > 3 INCH SEAT RAIL FWD OF FS 621.00 AT LBL 9.00 HAS CORROSION ON SURFACE IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AM - [SDR ASOA201101466](https://openairdocs.org/sdr/ASOA201101466.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK - [SDR ASOA201101465](https://openairdocs.org/sdr/ASOA201101465.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK R - [SDR ASOA201101464](https://openairdocs.org/sdr/ASOA201101464.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK R - [SDR ASOA201101463](https://openairdocs.org/sdr/ASOA201101463.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-40 - [SDR ASOA201101462](https://openairdocs.org/sdr/ASOA201101462.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+112-572.00 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL - [SDR ASOA201101457](https://openairdocs.org/sdr/ASOA201101457.md): Seat Track · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT RAIL BETWEEN FS 559.00+112-FS572.00 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001. - [SDR ASOA201101451](https://openairdocs.org/sdr/ASOA201101451.md): Angle · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Structure > CORROSION FOUND ANGLE AT FS 349 AT SERVICE DOOR UNDER TEFLON CAP. REMOVED ANGLE & FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06. INSTALLED SERVICABLE ANGLE IAW SRM 51-42-06. - [SDR ASOA201101450](https://openairdocs.org/sdr/ASOA201101450.md): Structure · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Structure > CORROSION FOUND AT FS 349 AT PAX DOOR UNDER TEFLON CAP. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. - [SDR ASOA201101449](https://openairdocs.org/sdr/ASOA201101449.md): Nut Plate · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PASSENGER DOOR SILL PLATE ANGLE CORRODED. UPON FURTHER INSPECTION FOUND 5 NUT CLIPS ONLY TO BE CORRODED. R & R IAW MINOR REPAIR. - [SDR ASOA201101448](https://openairdocs.org/sdr/ASOA201101448.md): Floorbeam · cracked · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > INBD AND OTBD CLIPS CRACKED AT FS280 LBL9. REMOVED CRACKED CLIPS INBD AND OTBD AT FS 280, LBL9 IAW SRM 51-42-00. INSTALLED NEW CLIPS AT FS 280, LBL9, INBD AND OTBD IAW SRM 51-42-00, PN 601R3113-57. THIS IS A MINOR REPAIR. CAMLOCK AT FS 280 CROSS BEAM REQUI - [SDR ASOA201101447](https://openairdocs.org/sdr/ASOA201101447.md): Floorbeam · cracked · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > INBD AND OTBD CLIPS CRACKED AT FS 280 RBL 9. REMOVED AND INSTALLED IAW SRM 51-42-00. - [SDR ASOA201101446](https://openairdocs.org/sdr/ASOA201101446.md): Frame · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Frame > FRAME CORRODED AT FS319.70, STR 26R. REMOVED FRAME LOWER SECTION IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SECTION OF FRAME & INSTALLED IAW SRM 51-42-06. - [SDR ASOA201101445](https://openairdocs.org/sdr/ASOA201101445.md): Frame · corroded · Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION AT FRAME FS 333 STR 26 & 27R. REMOVED CORROSION, FRAME FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-00-00. Next page: https://openairdocs.org/deregistered/N833AS-2017-04-25/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 = 'N833AS' AND deregistration_id = 'N833AS-2017-04-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N833AS-2017-04-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.