# Service difficulty reports: N834AS, cancelled Jul 7, 2015 A list on [N834AS, cancelled Jul 7, 2015](https://openairdocs.org/deregistered/N834AS-2015-07-07.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 · 170 reports - [SDR ASOA2014070310803](https://openairdocs.org/sdr/ASOA2014070310803.md): Structure · damaged · Jun 30, 2014 · N834AS · Cndair CL6002B19 · Rudder Structure > RT SIDE OF RUDDER HAS DAMAGE. COMPLIED WITH ALL STEPS OF EA 25-2014-193, JOB COMPLETE. MAJOR REPAIR IAW GMM 5-3. - [SDR ASOA2013101009198](https://openairdocs.org/sdr/ASOA2013101009198.md): Skin · cracked · Sep 27, 2013 · N834AS · Cndair CL6002B19 · Wing, Plate/Skin > SMALL CRACK IN LT LOWER WING PLANK STA 148. REPAIRED IAW REO 601R-57-51-660 AND REO 601R-57-21-130. - [SDR ASOA2013101009197](https://openairdocs.org/sdr/ASOA2013101009197.md): Bulkhead · cracked · Sep 25, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BULKHEAD AT FS 280, LBL 28, WL 85.50 HAS STANDOFF, BROKEN OFF WITH RIVET PULLED THROUGH AND HAS A CRACK EXTENDING 1" FROM HOLE. REMOVED DAMAGE IAW REO 601R-53-11-2566. FABRICATED AND INSTALLED REPAIR PARTS IAW REO 601R-53-11-2566. - [SDR ASOA2013100809174](https://openairdocs.org/sdr/ASOA2013100809174.md): Angle · cracked · Sep 23, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > ANGLE LBL 45 AT BS 605 ANGLE CRACKED AT FRAME. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. LOCATED AND DRILLED FRAME ANGLE SECTION IAW SRM 51-42-21. LOCATED AND DRILLED ANGLE IAW SRM 51-40-06 AND SRM 51-40-11. - [SDR ASOA2013101009196](https://openairdocs.org/sdr/ASOA2013101009196.md): Skin · cracked · Sep 20, 2013 · N834AS · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT LOWER WING PLANK BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORZ AND VERT SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-57-21-2003. - [SDR ASOA2013101009195](https://openairdocs.org/sdr/ASOA2013101009195.md): Bulkhead Web · cracked · Sep 18, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT LBL 36.20 APPROX WL 79 TO WL 81 2" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-5030. - [SDR ASOA2013101009194](https://openairdocs.org/sdr/ASOA2013101009194.md): Bulkhead Web · corroded · Sep 18, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0 APPROX WL 89 TO WL 113 24" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM CH 51-42-06 AND REO 601R-53-61-5034, REV 2013-09-27. - [SDR ASOA2013100809173](https://openairdocs.org/sdr/ASOA2013100809173.md): Skin · dented · Sep 18, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN AT FWD LOWER CORNER OF PAX DOOR SURROUND IS DENTED APPROX 1 L X.50 W X.30 D. CUT AWAY DAMAGED SKIN AT PAX DOOR CUTOUT OF FWD LWR CORNER IAW SRM 53-21-31, REPAIR NR 1, STEP 5, A1. COMPLIED WITH EC/TC SRM 53-21-31-01. FABRICATED DOUBLER AND FI - [SDR ASOA2013101109200](https://openairdocs.org/sdr/ASOA2013101109200.md): Hinge · chafed · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage, Door Hinge > PASSENGER DOOR HINGE ON FUSELAGE SIDE HAS (1 EA) LUG CHAFED APPROXIMATELY.003" DEEP ON LUG NR 13 COUNTING FROM FRONT TO BACK AND HINGE IS CHAFED APPROXIMATELY.045" DEEP AFT OF LUG NR 27 FROM CONTACT WITH HINGE PIN SPRING PIN. COMPLIED WITH REO 601R-53-21-81 - [SDR ASOA2013101109199](https://openairdocs.org/sdr/ASOA2013101109199.md): Bulkhead Web · gouged · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > REAR PRESSURE BULKHEAD FWD FACE ABOVE FLOOR HAS SEVERAL GOUGES RANGING FROM.003 TO.010 DEEP. BLENDED GOUGES IAW STEP NR 1 OF REO 601R-53-61-2155. - [SDR ASOA2013101009193](https://openairdocs.org/sdr/ASOA2013101009193.md): Angle · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN PASSENGER COMPARTMENT AT FS 280.00 BETWEEN LBL 9.00 TO RBL 9.00 THE TRANSVERSE BEAM TOP ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06. LOCATED AND INSTALLED NEW FS 280 FILLER BETWEEN LBL 9 AND RBL 9 IAW REO 601R-53-11-136. COMPLIED WITH EC/T - [SDR ASOA2013101009192](https://openairdocs.org/sdr/ASOA2013101009192.md): Seat Track · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > IN PASSENGER COMPARTMENT BETWEEN FS 348.00 TO 409.00+116 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED CORRODED SEAT TRACK FROM RBL 9.00 BETWEEN FS 398.00-FS 409.00+116 IAW SRM 51-41-02. INSTALLED FABBED SEAT TRACK AT RBL 9.0 BETWEEN F - [SDR ASOA2013101009191](https://openairdocs.org/sdr/ASOA2013101009191.md): Floorbeam · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > IN PASSENGER COMPARTMENT BETWEEN FS 409.00 RBL 9.00 THE FLOORBEAM ATTACHMENT HOLES FOR THE FLOORBOARD ARE CORRODED. REMOVED FLOORBEAM CAP IAW SRM'S 51-42-06 AND 51-42-34 AND 51-42-21. LOCATED, TRIMMED, DRILLED REPLACEMENT FLOORBEAM SECTION IAW SRM 51-40-11, - [SDR ASOA2013101009190](https://openairdocs.org/sdr/ASOA2013101009190.md): Attach Angle · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings > IN PASSENGER COMPARTMENT AT FS 280.00 ON RBL 9.00 THE ATTACHMENT ANGLE IS CRACKED (RT). REMOVED DAMAGED CLIP FROM FS 280 ON RBL 9 OTBD PREVIOUSLY INSTALLED IAW REO 601R-53-11-640. FABRICATED CLIP, PN 601R-53-11-640-2, REF REO 601R-53-11-640 FOR MAT SPEC. L - [SDR ASOA2013100809172](https://openairdocs.org/sdr/ASOA2013100809172.md): Post · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FOUND FS 409+128, VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX.2 INCHES IN LENGTH 50 PERCENT AND 100 PERCENT FSH. FAILED NDT INSPECTION AT AFT FLANGE RADIUS. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW POST IAW - [SDR ASOA2013100809171](https://openairdocs.org/sdr/ASOA2013100809171.md): Post · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FOUND FS 409+128 VERTICAL POST LBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX.2 INCHES IN LENGTH 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW VERTICAL POST IAW SRM 51-42 - [SDR ASOA2013100809170](https://openairdocs.org/sdr/ASOA2013100809170.md): Floorbeam · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > IN PASSENGER CABIN FS 349 BETWEEN LBL 27 TO 36, FLOORBEAM TOP CAP IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06, 51-42-21 AND AMM 51-23-00-390-802. - [SDR ASOA2013100709167](https://openairdocs.org/sdr/ASOA2013100709167.md): Floor Support · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN PASSENGER COMPARTMENT BETWEEN FS 280 TO 319.7 ON RBL 36.00 FLOOR SUPPORT AT SEVERAL LOCATIONS IS CORRODED. REPAIRED IAW REO 601R-53-00-530. - [SDR ASOA2013100709166](https://openairdocs.org/sdr/ASOA2013100709166.md): Floor Support · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN PASSENGER COMPARTMENT AT FS 319.00 ON RBL 36 THE SERVICE DOOR CUTOUT FLOORBOARD ATTACHMENT ANGLE IS CORRODED. RT FLOOR SILL SUPPORT BETWEN FS 310 AND FS 319 CORRODED BEYOND LIMITS. REPLACEMENT REQUIRED. INSTALLED NEW FWD RT SUPPORT ANGLE, PN 601R31148-79 - [SDR ASOA2013100709165](https://openairdocs.org/sdr/ASOA2013100709165.md): Seat Track · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > IN PASSENGER COMPARTMENT BETWEEN FS 364 - 398 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK FS 364.00 TO FS 398.00, RBL 9 IAW AMM 53-01-11-000-812. INSTALLED NEW SERVICEABLE PASSENGER SEAT TRACK FROM FS 364.00 -FS 398.00, RB - [SDR ASOA2013100709164](https://openairdocs.org/sdr/ASOA2013100709164.md): Seat Track · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > IN PASSENGER COMPARTMENT BETWEEN FS 364 TO 398 ON LBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK. LOCATED & DRILLED SERVICEABLE SEAT TRACK, PN N126-2075, PO W/12366 IAW SRM 51-40-11 & SRM 51-40-06. SEAT TRACK INSTALLED AS REQUI - [SDR ASOA2013100709163](https://openairdocs.org/sdr/ASOA2013100709163.md): Seat Track · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > IN PASSENGER COMPARTMENT BETWEEN FS 409.00+116 TO FS 559.00+5 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK 3X RING HARDWARE. INSTALLED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW AMM 53-01-11-900-802. DRILLED NEW SEAT TRA - [SDR ASOA2013100709162](https://openairdocs.org/sdr/ASOA2013100709162.md): Floor Support · corroded · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN PASSENGER COMPARTMENT AT FS 449.85 ON LBL 36.00 THE FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. - [SDR ASOA2013100709161](https://openairdocs.org/sdr/ASOA2013100709161.md): Angle · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN AFT EQUIPMENT COMPARTMENT AT FS 625.00, BL 45.00, STRINGER 14L AND AT WL 97.5 THE LT INTERCOSTAL, OBLIQUE, ANGLE IS CRACKED APPROX 1.1 LONG. REMOVED DAMAGED CLIP FROM FS 625, STR 14L AND INSTALLED NEW CLIP, PN 601-35012-1 IAW SRM 51-42-21. - [SDR ASOA2013100709160](https://openairdocs.org/sdr/ASOA2013100709160.md): Angle · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN PASSENGER COMPARTMENT AT FS 484.00 RBL 27.00 THE INTERCOSTAL REPAIR ANGLE IS CRACKED. R & R INTERCOSTAL ANGLE, PN 601R31171-9 FS 484.00, RBL 27.00 IAW SRM 51-42-06 & 51-42-21. - [SDR ASOA2013100709159](https://openairdocs.org/sdr/ASOA2013100709159.md): Isolator · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PNL 281FLW. R & R BROKEN ISOLATOR WITH SERVICEABLE ISOLATOR IAW SRM 51-42-10 AND SRM 51-42-13. - [SDR ASOA2013100709158](https://openairdocs.org/sdr/ASOA2013100709158.md): Isolator · cracked · Sep 17, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PANEL 281GLW. R & R BROKEN ISOLATOR WITH A SERVICEABLE ISOLATOR IAW SRM 51-42-13 AND SRM 51-42-10. - [SDR ASOA2013101009189](https://openairdocs.org/sdr/ASOA2013101009189.md): Floorbeam · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > IN CARGO COMPARTMENT AT FS 605.00 ON RBL 9.00 THE FLOORBEAM AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED FLOORBEAM UPPER CAP AT RBL 9 BETWEEN 569 & FS 621 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED, DRILLED NEW SERVICEABLE CARGO COMPARTMENT FLOORB - [SDR ASOA2013101009188](https://openairdocs.org/sdr/ASOA2013101009188.md): Floor Support · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN CARGO BAY BETWEEN FS 574.00 TO 621.00 ON LBL 36.00 THE CARGO DOOR CUTOUT FLOOR SUPPORT AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED CORRODED CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW CARGO COMPARTMENT FLOOR SU - [SDR ASOA2013101009187](https://openairdocs.org/sdr/ASOA2013101009187.md): Skin · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Wing, Plate/Skin > RT WING PLANK ACCESS HOLE 640AB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030. - [SDR ASOA2013101009186](https://openairdocs.org/sdr/ASOA2013101009186.md): Skin · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Wing, Plate/Skin > RT WING PLANK ACCESS HOLE 640BB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030 AND REO 601R-57-21-2004. - [SDR ASOA2013100309147](https://openairdocs.org/sdr/ASOA2013100309147.md): Floor Support · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX CABIN BS 449.85 RBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. - [SDR ASOA2013100309146](https://openairdocs.org/sdr/ASOA2013100309146.md): Floor Support · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX CABIN BS 559+32 LBL 36.00 THE FLOOR SUPPORT CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV. - [SDR ASOA2013100309145](https://openairdocs.org/sdr/ASOA2013100309145.md): Floor Support · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX CABIN FS 559+57 LBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV. - [SDR ASOA2013100309144](https://openairdocs.org/sdr/ASOA2013100309144.md): Floorbeam · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > IN CARGO BAY BS 598 LBL 9 FLOORBEAM CORRODED. REPAIRED IAW REO 601R-53-61-5029 AND REO 601R-53-00-005. - [SDR ASOA2013100309143](https://openairdocs.org/sdr/ASOA2013100309143.md): Floor Support · corroded · Sep 16, 2013 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > IN CARGO BAY BETWEEN BS 574 - 621 LBL 27 FLOOR SUPPORT AROUND ATTACHMENT HOLES CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW REO 601R-53-61- - [SDR ASOA2013042603455](https://openairdocs.org/sdr/ASOA2013042603455.md): Battery · inoperative · Apr 24, 2013 · N834AS · Cndair CL6002B19 · Emergency Equipment > CAPTAIN`S FLASHLIGHT NOT WORKING. REPLACED BATTERIES IAW AMM 52-61-00. - [SDR ASOA2012083102156](https://openairdocs.org/sdr/ASOA2012083102156.md): Battery Pack · inoperative · Aug 28, 2012 · N834AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHT AFT OF GALLEY INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD. - [SDR ASOA2012061501801](https://openairdocs.org/sdr/ASOA2012061501801.md): Door Frame · cracked · Jun 11, 2012 · N834AS · Cndair CL6002B19 · Fuselage Main, Structure > FOUND CRACK ON SERVICE DOOR FRAME. ON FWD DOOR SEAL STRIKER. REMOVED AND INSTALLED NEW SEAL STRIKER, IAW SRM 51-42-06, 51-23-00. - [SDR ASOA201102021](https://openairdocs.org/sdr/ASOA201102021.md): Battery · discharged · Oct 21, 2011 · N834AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS INOPERATIVE WITH SWITCH ON. CHARGED BATTERY PACK. - [SDR ASOA201101845](https://openairdocs.org/sdr/ASOA201101845.md): Floor Support · corroded · Oct 3, 2011 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PRESSURE FLOOR SKIN ANGLES HAVE CORROSION BETWEEN FS 409.00 +128 AND FS 559.00 RT SIDE. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-66. - [SDR ASOA201101840](https://openairdocs.org/sdr/ASOA201101840.md): Battery Pack · inoperative · Oct 2, 2011 · N834AS · Cndair CL6002B19 · Emergency Lighting > FLOOR LEVEL EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. REPLACE EMERGENCY LIGHT ASSY AT SVC DOOR, FLOOR LEVER REF AMM 33-51-10-000-801 (ASSY BROKEN) REPLACED EMERGENCY LIGHT FLOOR ASSY IAW AMM 33-51-10-400-801 FAILS OPS TEST. REPLACED EMERGENCY LIGHTS BA - [SDR ASOA201101839](https://openairdocs.org/sdr/ASOA201101839.md): Battery Pack · inoperative · Oct 2, 2011 · N834AS · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHT OVERWING THE LAST ONE AFT OF EMERGENCY EXIT ON LT AND RT INOPERATIVE. REPLACE BATTERY PACK NR4 IAW AMM 33-51-04-000-801. REPLACED NR 4 BATTERY PACK IAW AMM 33-51-04-400-801, OPS TEST GOOD. CEILING PANEL BETWEEN FS559+48R AND FS 559, OR REMOVE - [SDR ASOA201101809](https://openairdocs.org/sdr/ASOA201101809.md): Placard · wrong part · Sep 26, 2011 · N834AS · Cndair CL6002B19 · Placards and Markings > LEFT EMERGENCY EXIT HAS WRONG PLACARD INSTALLED. REMOVED INCORRECT PLACARD IAW AMM 11-30-00-000-801 AND INSTALLED CORRECT PLACARD, IAW AMM 11-30-00-400-801, - [SDR ASOA201101748](https://openairdocs.org/sdr/ASOA201101748.md): Floorbeam · corroded · Sep 16, 2011 · N834AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > FLOORBEAM HAS CORROSION AT FS 349.00. REPAIRED IAW REO 601R-53-21-1361. - [SDR ASOA201101795](https://openairdocs.org/sdr/ASOA201101795.md): Frame · cracked · Sep 15, 2011 · N834AS · Cndair CL6002B19 · Fuselage Main, Frame > BS 280 FRAME APPEARS TO BE CRACKED AFT LOWER SIDE NEAR LBL9.00. COMPLIED WITH ECTC REO 601R-53-11-171. - [SDR ASOA201101732](https://openairdocs.org/sdr/ASOA201101732.md): Drag Angle · cracked · Sep 14, 2011 · N834AS · Cndair CL6002B19 · Passenger/Crew Doors > POSSIBLE CRACK FOUND AT FASTNER LOCATION ON PAX DOOR UNDER AFT DRAG ANGLE. REPAIRED IAW REO 601R-52-11-1991. - [SDR ASOA201101706](https://openairdocs.org/sdr/ASOA201101706.md): Support · corroded · Sep 12, 2011 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT SIDE WINDSCREEN SUPPORT STRUCTURE AT FS 349 CORRODED. REMOVED AND REPLACED WINDSCREEN SUPPORT ANGLE & FITTING IAW SRM 51-42-06 & SRM 51-42-21. - [SDR ASOA201101705](https://openairdocs.org/sdr/ASOA201101705.md): Bracket · cracked · Sep 12, 2011 · N834AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PILOTS WINDSHIELD SIDE POST LOWER BRACKET CRACKED. R & R BRACKET IAW SRM 51-47-21. - [SDR ASOA201101688](https://openairdocs.org/sdr/ASOA201101688.md): Seat Track · corroded · Sep 9, 2011 · N834AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CORRODED AT RBL 9 AND FS 364.00. CLEANED CORROSION IAW SRM 51-21-11. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 5140-11 AND AMM 52-01 Next page: https://openairdocs.org/deregistered/N834AS-2015-07-07/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 = 'N834AS' AND deregistration_id = 'N834AS-2015-07-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N834AS-2015-07-07/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.