# Service difficulty reports: N870AS, cancelled Jul 30, 2023

A list on [N870AS, cancelled Jul 30, 2023](https://openairdocs.org/deregistered/N870AS-2023-07-30.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 3 · 146 reports

- [SDR SWIA2019102246555](https://openairdocs.org/sdr/SWIA2019102246555.md): Warning Message · false activation · Oct 21, 2019 · N870AS · Cndair CL6002B19 · Engine Vibration Analyzer
  > N2 VIB MESSAGE CAME UP ON TAKE OFF ROLL. ABORTED TAKE OFF 80 KNOTS. BTMS WITHIN LIMITS FLT # 5946 CLOSED. NO DAMAGE NOTED. PERFORMED HIGH POWER ENGINE RUNS AND DID NOT GET VIBE INDICATION FOR N2. OPS CHECKS GOOD.
- [SDR ASOA2019040864012](https://openairdocs.org/sdr/ASOA2019040864012.md): Battery Pack · discharged · Apr 6, 2019 · N870AS · Cndair CL6002B19 · Emergency Lighting
  > IAH - FLIGHT 4306, THE CREW REPORTED EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOT AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE.
- [SDR ASOA2019040173021](https://openairdocs.org/sdr/ASOA2019040173021.md): Seal · faulty · Mar 27, 2019 · N870AS · Cndair CL6002B19 · Service Doors
  > THE CREW REPORTED AT 35,000 FEET LOST ALL PRESSURIZATION. MAINTENANCE INSPECTED AND REPLACED SERVICE DOOR SEAL. OPERATIONAL CHECK WERE GOOD.
- [SDR ASOA2016030514551](https://openairdocs.org/sdr/ASOA2016030514551.md): Bulb · missing · Mar 5, 2016 · N870AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY RT COVER AND LIGHT BULB MISSING ON NR 1 GALLEY WALL, ENTRANCE LT SIDE. REPLACED EMERGENCY LIGHT ASSY ON IAW AMM 33-5119, GOOD. OK FOR SERVICE.
- [SDR ASOA2016012614402](https://openairdocs.org/sdr/ASOA2016012614402.md): Skin · damaged · Jan 26, 2016 · N870AS · Cndair CL6002B19 · Rudder, Plate/Skin
  > DURING FLIGHT CONTROL TEST AFTER PUSHBACK, THE RT RUDDER PEDDAL WILL NOT REACH FULL DEFLECTION. DAMAGE TO RUDDAR, CAUSING OBSTRUCTION, SHEETMETAL REMOVED IAW REO 601R-55-41-197 PERFORMED OPS TEST OF RUDDAR IAW AMM 27-21-00.
- [SDR ASOA2015081013475](https://openairdocs.org/sdr/ASOA2015081013475.md): Skin · damaged · Aug 10, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AROUND LOW PRESSURE GROUND CONNECTION DOOR. THE REPAIR HAS BEEN DETERMINED AND CLASSIFIED TO BE MAJOR REAPAIR. RECEIVED AND COMPLIED IAW EA 25-2015-237.
- [SDR ASOA2015042912729](https://openairdocs.org/sdr/ASOA2015042912729.md): Angle · cracked · Apr 25, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CROSSMEMBER ANGLE CRACKED AT FS 621.00 BULKHEAD. R & R ANGLE AT FS 621.00 CARGO DOOR CROSSMEMBER WITH NEW SERVICEABLE PART IAW SRM 51-42-21.
- [SDR ASOA2015050412751](https://openairdocs.org/sdr/ASOA2015050412751.md): Skin · cracked · Apr 15, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED ON AFT OTBD SIDE APPROXIMATELY 1.5" LONG, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015050412750](https://openairdocs.org/sdr/ASOA2015050412750.md): Frame · corroded · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 605.00, STR 27. REMOVED CORROSION ON FS 605. FRAME BETWEEN STR 25L AND 25R IAW SRM 51-21-06. FS 605.00 FRAME FOPUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TRR 53-29. REMOVED OLD FS 605.00 FRAME SECTOR, PN:601R36026-27 BETWEEN FACTORY
- [SDR ASOA2015050412749](https://openairdocs.org/sdr/ASOA2015050412749.md): Skin · corroded · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK AT 640BB HAS CORROSION IN SEVERAL AREAS. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015050412748](https://openairdocs.org/sdr/ASOA2015050412748.md): Skin · corroded · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK AT 540BB HAS CORROSION AT INBD SIDE IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2015050412747](https://openairdocs.org/sdr/ASOA2015050412747.md): Floorbeam · cracked · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 621, LT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. REO:601R-53-61-5473, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.
- [SDR ASOA2015042912728](https://openairdocs.org/sdr/ASOA2015042912728.md): Door Sill · corroded · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON CARGO DOOR SILL FROM FS 621.00 TO FS 574.00. 2 AREAS 0.003 IN. OUT OF LIMITS AT FS 589.00+13 AND FS 605.00+6.25 ENGINEERING REQUIREDD. DAMAGE WAS BLENDED OUT TO SMOOTH CONTOUR IAW REO 601R-53-61-5472. COMPLIED WITH REO 601R-53-61-5472.
- [SDR ASOA2015042912727](https://openairdocs.org/sdr/ASOA2015042912727.md): Floorbeam · corroded · Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT FS 589.00 BETWEEN LBL 18 AND LBL 27. FOUND TO BE OUT OF LIMITS IAW TR 53-27, REQUIRES REPLACEMENT. REMOVED CORRODED FLOORBEAM CAP AT FS 589.00 BETWEEN LBL 18 AND LBL 27 IAW SRM 51-42-06, 51-42-21 AND 51-42-15. LOCATED AND INSTALLED
- [SDR ASOA2015042912726](https://openairdocs.org/sdr/ASOA2015042912726.md): Seat Track · corroded · Apr 12, 2015 · N870AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAILS FROM FS 454 - FS 559+54 HAS SEVERAL AREAS OF CORROSION AROUND THE LOWER EDGE OF THE COIN HOLES; WORST IS AT FS 474, MARKED WITH ORANGE TAPE. REMOVED RT SIDE SEAT RAIL AT FS 449.85 TO FS 495.98 IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SE
- [SDR ASOA2015050412746](https://openairdocs.org/sdr/ASOA2015050412746.md): Retainer · corroded · Apr 10, 2015 · N870AS · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVI BAY DOOR SEAL RETAINER IS CORRODED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPLACED SEAL RETAINERS IAW SRM 51-42-06. PERFORMED OPS TEST OF THE MAIN AVIONICS COMPARTMENT DOOR SEAL IAW AMM 52-42-07-710-801. OPS TESTED GOOD.
- [SDR ASOA2015050412745](https://openairdocs.org/sdr/ASOA2015050412745.md): Floor Support · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL AFT OF PAX DOOR AT FS 349.00. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.
- [SDR ASOA2015042912725](https://openairdocs.org/sdr/ASOA2015042912725.md): Floorbeam · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON AVIONICS BAY FLOORBOARD SUPPORT ANGLE AT FS 333.00. REMOVED FLOORBOARD SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED FS 333.00 AVIONICS BAY FLOORBOARD SUPPORT BRACKET IAW SRM 51-40-11 AND SRM 51-42-06.
- [SDR ASOA2015042912724](https://openairdocs.org/sdr/ASOA2015042912724.md): Door Sill · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL, LOWER, ANGLE HAS CORROSION IN SEVERAL AREAS. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LOWER SILL IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-40-11. INSTALLED NEW S
- [SDR ASOA2015042912723](https://openairdocs.org/sdr/ASOA2015042912723.md): Door Sill · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR SILL AT FS 319.70 AND FS 349.00. BLENDED AREA REMOVING CORROSION IAW REO 601R-53-00-530. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.
- [SDR ASOA2015042912722](https://openairdocs.org/sdr/ASOA2015042912722.md): Floor Support · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AROUND 3 FASTENER HOLES BETWEEN FS 310.00 AND FS 349.00 LBL 27. COMPLIED WITH EC/TC REO 601R-53-00-005.
- [SDR ASOA2015042912721](https://openairdocs.org/sdr/ASOA2015042912721.md): Floor Support · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SURFACE OF RT FLOOR SILL STRUCTURE FROM FS 409.00+128 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN.
- [SDR ASOA2015042912720](https://openairdocs.org/sdr/ASOA2015042912720.md): Frame · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 364.00 BETWEEN LBL 24 & RBL 24. COMPLIED WITH EA 32-2015-138.
- [SDR ASOA2015042912719](https://openairdocs.org/sdr/ASOA2015042912719.md): Frame · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 330.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION TO BE LOCATED ON FRAME SECTOR AT FS 333.00 NOT FS 330.00. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED CORRODED FRAME IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW
- [SDR ASOA2015042912718](https://openairdocs.org/sdr/ASOA2015042912718.md): Frame · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 319.70 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FS 319.70 FRAME OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 319.70 LOWER FRAME SECTOR FOR REPLACEMENT IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FS 319.70 LOWE
- [SDR ASOA2015042912717](https://openairdocs.org/sdr/ASOA2015042912717.md): Frame · corroded · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 310.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. COMPLIED WITH REO 601R-53-21-2612 P1.
- [SDR ASOA2015042912716](https://openairdocs.org/sdr/ASOA2015042912716.md): Floorbeam · cracked · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 FLOORBEAM ANGLE AT RBL 9 OTBD & RBL 27 INBD ARE CRACKED. FABRICATED NEW FS 280, RBL 9 CLIP FROM S6144-13, PERFORMED ANGLE 2024T42.050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED CLIP AT FS 280, RBL 9.0, OTBD IAW SRM CH 51-42-21. COMPLIED WI
- [SDR ASOA2015042912715](https://openairdocs.org/sdr/ASOA2015042912715.md): Floorbeam · cracked · Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 FLOORBEAM ANGLE AT LBL 9 INBD & OTBD ARE CRACKED. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD CLIPS FROM S6144-13, PREFORMED ANGLE 2024T42.050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED LBL 9 INBD AND OTBD CLIPS AT FS 280 IAW SRM CH 51-42-21
- [SDR ASOA2014041010306](https://openairdocs.org/sdr/ASOA2014041010306.md): Lamp · burned out · Apr 6, 2014 · N870AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD, IAW AMM 33-51-00.
- [SDR ASOA2013121909663](https://openairdocs.org/sdr/ASOA2013121909663.md): Priority Valve · failed · Nov 28, 2013 · N870AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR UP DISAGREE WARNING AFTER DEPARTURE. LT AND RT GEAR WERE IN DISAGREEMENT (RED). COMPLIED WITH QRH. MANUAL GEAR HANDLE WAS PULLED IAW QRH. EMERGENCY DECLARED. RETURNED TO DEPARTURE AND LANDED AT 46500 LBS. R & R MLG PRIORITY VALVE IAW AMM 32-32-15.
- [SDR ASOA2013100109138](https://openairdocs.org/sdr/ASOA2013100109138.md): Lamp · burned out · Sep 27, 2013 · N870AS · Cndair CL6002B19 · Emergency Lighting
  > CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OP'S CHECKED GOOD IAW AMM 33-51-16.
- [SDR ASOA2013053003737](https://openairdocs.org/sdr/ASOA2013053003737.md): Skin · cracked · May 10, 2013 · N870AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING SKIN IS CRACKED.25" LONG AT WS 148.09 - REINFORCING ANGLE IN T/E ABOVE SKIN IS CRACKED.75" LONG. C/W ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J, DATED 03/08/2011 AS WRITTEN. C/W ECTC REO 601R-57-21-131 AND REO 601R-57-21-131,
- [SDR ASOA2013053003736](https://openairdocs.org/sdr/ASOA2013053003736.md): Angle · cracked · May 8, 2013 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621, BULKHEAD AFT SIDE FS 621-625 ANGLES CRACKED. REMOVED CRACKED LT & RT FS 621-625 ANGLES AND INSTALLED SERVICEABLE ANGLES IAW SRM 51-40-11 AND SRM 51-42-06.
- [SDR ASOA2013053003735](https://openairdocs.org/sdr/ASOA2013053003735.md): Attach Bracket · cracked · May 8, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR UPPER SILL ATTACHMENT BRACKET CRACKED AT FS 280. REMOVED CRACKED BRACKET AT FS 280, STR 3 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE, PN 600-31057-19 IAW SRM 51-40-11. UPON FURTHER INVESTIGATION ANGLE, PN 600-31057-20, FS 280, STR 3
- [SDR ASOA2013053003734](https://openairdocs.org/sdr/ASOA2013053003734.md): Bulkhead · cracked · May 7, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621, BULKHEAD FAILS NDT WITH AN INDICATION FSH AT LBL 27.50, WL 130). REPAIRED IAW REO 601R-53-61-1541, REV D.
- [SDR ASOA2013053003733](https://openairdocs.org/sdr/ASOA2013053003733.md): Cargo Track · corroded · May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACKS CORRODED AROUND FASTENER HOLES AT LBL 27 AND LBL 9. R & R CARGO TRACKS IAW AMM 20-21-00-910-801.
- [SDR ASOA2013053003732](https://openairdocs.org/sdr/ASOA2013053003732.md): Isolator · cracked · May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD FWD FACE HAS FIVE CRACKED ISOLATORS. R & R ISOLATORS ON FS 621 BULKHEAD IAW SRM 51-42-06.
- [SDR ASOA2013053003731](https://openairdocs.org/sdr/ASOA2013053003731.md): Floor Support · corroded · May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CABIN FLOOR SUPPORT IS CORRODED AT FOUR NUTPLATE LOCATIONS. DAMAGE IS APPROX BETWEEN FS 409+128 AND FS 559. REPAIRED IAW TASK 51-26-0-110-801, SRM 51-21-11, 51-27-19, 51-21-06, 51-26-00 AND REO 601R-53-41-666.
- [SDR ASOA2013053003730](https://openairdocs.org/sdr/ASOA2013053003730.md): Skin · cracked · Apr 30, 2013 · N870AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING SKIN CRACKED.25" LONG AT WS 148.019. C/W EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J. C/W EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A. REPAIRED IAW REO 601R-57-51-639, SRM 51-42-06, 51-42-21 & REO 601R-57-21-6
- [SDR ASOA2013053003729](https://openairdocs.org/sdr/ASOA2013053003729.md): Drag Angle · cracked · Apr 30, 2013 · N870AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAW SRM 51-42-06 AND 51-42-10 AND REO 601R-52-11-513, REV A.
- [SDR ASOA2012100202318](https://openairdocs.org/sdr/ASOA2012100202318.md): Control Lever · failed · Sep 28, 2012 · N870AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON SELECTING FLAPS FROM 8 TO 20 DEGREES, FLAPS FAIL CAUTION MESSAGE DISPLAYED. VERIFIED FLAPS STUCK AT 8 DEGREES ON EICAS FLIGHT CONTROL PAGE. COMPLIED WITH QRH. EMERGENCY DECLARED. COMPLIED WITH AD 2009-06-12 TROUBLESHOOTING FOR FLAP FAILURES. R & R FLAP C
- [SDR ASOA2012091702224](https://openairdocs.org/sdr/ASOA2012091702224.md): Motor · malfunctioned · Sep 13, 2012 · N870AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR DOES NOT OPEN FULLY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. PERFORMED OPS CHECKS OF THE PWR DOOR ASSIST IAW AMM 52-11-08-720-802. NO DEFECTS NOTED DEFER CLEARED PLACARD REMOVED. SDR CLOSED.
- [SDR ASOA201201454](https://openairdocs.org/sdr/ASOA201201454.md): Detection Sys · malfunctioned · Apr 28, 2012 · N870AS · Cndair CL6002B19 · Fire Detection
  > DURING FIRE WARNING TEST, DID NOT GET LEFT ENGINE FIRE LOOP-B WARNING MESSAGE AND LEFT FIRE PUSH SWITCH DOES NOT ILLUMINATE. INSPECTED LT ENGINE FIRE LOOPS, NO PROBLEMS NOTED. FOUND LT FIRE PUSH SWITCH LIGHT LOOSE IN ITS SOCKET. RESECURED THE FIRE PUSH S
- [SDR ASOA201201315](https://openairdocs.org/sdr/ASOA201201315.md): Pin · missing · Apr 20, 2012 · N870AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR RELEASE HANDLE NOT FUNTIONAL. PIN MISSING. REPLACE MISSING PIN ON SERVICE DOOR RELEASE HANDLE. OPS CHECKED GOOD IAW AMM 52-41-02. (SDR CLOSED)
- [SDR ASOA201100887](https://openairdocs.org/sdr/ASOA201100887.md): Isolator · broken · May 4, 2011 · N870AS · Cndair CL6002B19 · Fuselage Floor Panel
  > APPROX RBL 36, WL 92 ON AFT BULKHEAD, ISOLATER BROKEN RT SIDE. R & R RT OTBD ISOLATOR AT WATER LINE 92 ON FS 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA
- [SDR ASOA201100878](https://openairdocs.org/sdr/ASOA201100878.md): Connector · malfunctioned · May 4, 2011 · N870AS · Cndair CL6002B19 · Light System Wiring
  > FWD LEFT EMERGENCY LIGHTS ARE INOP ON TEST. FOUND CONNECTORS J11LY AND P10LY SWAPPED WITH CONNECTORS J20LY AND P21LY. INSTALLED TO ORIGINAL CONFIG AND RESEATED CONNECTORS IAW ESPM 20-17-10. PERFORMED OPS CHECK IAW AMM 33-51-00-710-801. SYS CHECKS GOOD. OK
- [SDR ASOA201100783](https://openairdocs.org/sdr/ASOA201100783.md): Floorbeam · cracked · Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 AFT FLOOR ANGLE IS CRACKED OTBD OF RBL9 AND OTBD LBL9, REPAIRED IAW REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100777](https://openairdocs.org/sdr/ASOA201100777.md): Post · cracked · Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INDICATION NOTED AT FS 409+128 BL 0.00 WK 69.0 RADIUS OF RT CHANNEL APPROX.10" LENGTH, 55 PERCENT. REMOVED POST ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE POST ASSY IAW REO 601R-53-41-889.
- [SDR ASOA201100776](https://openairdocs.org/sdr/ASOA201100776.md): Floor Support · corroded · Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED FS 349 AT SERVICE DOOR SURROUND LOWER AFT FRAME BRACKET. REMOVED CORROSION, FOUND WITHIN LIMITS IAW SRM 53-21-15 AND SRM 53-00-00.
- [SDR ASOA201100775](https://openairdocs.org/sdr/ASOA201100775.md): Floor Support · corroded · Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, FWD FLOOR SUPPORT ANGLE IS CORRODED. R & R FWD FLOOR SUPPORT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06. REPAIR CLASSIFIED AS A MINOR.

Next page: https://openairdocs.org/deregistered/N870AS-2023-07-30/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 = 'N870AS' AND deregistration_id = 'N870AS-2023-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N870AS-2023-07-30/reports

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