# Service difficulty reports: N880AS

A list on [N880AS](https://openairdocs.org/aircraft/N880AS.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 · 192 reports

- [SDR SWIA2018092445090](https://openairdocs.org/sdr/SWIA2018092445090.md): Strut · failed · Sep 24, 2018 · N880AS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON DEPARTURE NOSE DOOR OPEN WARNING AND GEAR DISAGREE WARNING. COMPLETED QRH. WOW INPUT CAUTION MESSAGE. NO NOSE WHEEL STEERING ON LANDING. (FLT 5014) CLOSED PERFORMED FULL SERVICE ON NOSE LANDING GEAR STRUT IAW AMM. STRUT EXTENSION CHECK GOOD AT THIS TIME. PE
- [SDR SWIA2018073144944](https://openairdocs.org/sdr/SWIA2018073144944.md): Screw · loose · Jul 31, 2018 · N880AS · Cndair CL6002B19 · Wing, Plate/Skin
  > STRONG INTERMITTENT FUEL SMELL IN THE FLIGHT DECK IN FLIGHT AND ON GROUND. APU RAN ENTIRE FLIGHT. (FLT 5421) CLOSED SECURED LOOSE PANEL SCREWS ON RIGHT WING, NR 5 FUEL PANEL AS REQUIRED. NO LEAKS NOTED. RAN APU AND ENGINES, OPERATED BLEED AIR WITH NO FUEL SMEL
- [SDR SWIA201844655](https://openairdocs.org/sdr/SWIA201844655.md): Proximity Sensor · out of adjust · May 11, 2018 · N880AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > UPON SELECTING GEAR UP ON TAKE OFF, THE NOSE GEAR REMAINED DOWN. CYCLED THE GEAR TWO MORE FULL CYCLES AND ABOUT A MINUTE AFTER THE LAST ATTEMPT THE NOSE GEAR RETRACTED. (FLT 5645) CLOSED ADJUSTED PROX SENSORS S23, S11 AND S03 IAW AMM. OPS CHECK GOOD. PERFORME
- [SDR SWIA201743483](https://openairdocs.org/sdr/SWIA201743483.md): Sensor · out of adjust · Jul 10, 2017 · N880AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE, DECLARED EMERGENCY. PROXIMITY SENSOR WAS OUT OF ADJUSTMENT ON THE LT MAIN LANDING UPLOCK. OPS CHECKED GOOD.
- [SDR ASOA2016081815280](https://openairdocs.org/sdr/ASOA2016081815280.md): Battery Pack · discharged · Aug 18, 2016 · N880AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERY PACKS AND OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-05. OPS CHECKED GOOD.
- [SDR ASOA2016052814900](https://openairdocs.org/sdr/ASOA2016052814900.md): Pseu · failed · May 28, 2016 · N880AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > AT 31,000', ENROUTE, RECEIVED AMBER CAUTION PRIX SYSTEM CHANNEL MESSAGE, FOLLWED QRH MANNUALLY EXTENDED GEAR LANDED. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R PSEU IAW AMM 32-61-01, IPC REF32-61-00, ITEM 5, OPS TEST GOOD, IAW THE NATU
- [SDR ASOA2016050914833](https://openairdocs.org/sdr/ASOA2016050914833.md): Bushing · deteriorated · May 9, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RT MLG TRUNNION AFT BUSHING AUX BORE HOLE DIAMETER IS OUT OF LIMITS. REMOVED RT MLG AFT TRUNNION LUG TO TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN RT MLG AFT TRUNNION IAW ECTC REC 601R-57-21-003 AND GREO 601R-57-21-003,
- [SDR ASOA2016050714832](https://openairdocs.org/sdr/ASOA2016050714832.md): Bushing · deteriorated · May 7, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RT MLG TRUNNION FWD BUSHING BORE, AFT SPAR, HOLE DIAMETER IS OUT OF LIMITS. REMOVED AND REAMED THE TRUNNION, MLG TRUNNION FWD BUSHING BORE, AFT SPAR, TO 1ST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN THE RT MLG TRUNNION FWD BUSHI
- [SDR ASOA2016050714831](https://openairdocs.org/sdr/ASOA2016050714831.md): Bushing · deteriorated · May 7, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LT MLG TRUNNION AFT BUSHING BORE AUXILIARY HOLE DIAMETER IS OUT OF LIMITS. REAMED LT MLG AFT TRUNNION LUG TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVRSIZE BUSHING INLT MLG AFT TRUNNION IAW ECTC REO 601R-57-21-003.
- [SDR ASOA2016050614830](https://openairdocs.org/sdr/ASOA2016050614830.md): Seat Track · corroded · May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT CORRODED AND OUT OF LIMITS ON RBL9 AND BETWEEN FS 559 TO FS 559+86. REMOVED SEAT TRACK SEGEMENTS AT RBL9 BETWEEN FS559-FS559+86 IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK SEGMENT AT RBL9 BETWEEN FS 559-559+86 IN REF TO AMM 53-01-11-400
- [SDR ASOA2016050614829](https://openairdocs.org/sdr/ASOA2016050614829.md): Intercostal · cracked · May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED BETWEEN FS 621 AND FS 625.30 AT STR 15R. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS625.3, RBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.
- [SDR ASOA2016050614828](https://openairdocs.org/sdr/ASOA2016050614828.md): Intercostal · cracked · May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED BETWEEN BS 621 AND 625.30 AT STR 15L. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS 625.3, LBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.
- [SDR ASOA2016042914839](https://openairdocs.org/sdr/ASOA2016042914839.md): Floor Support · corroded · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOORSILL AT LBL 47 AND BETWEEN FS 349 TO FS 367. BLENDED CORROSION ON FLOOR SILL AT LBL47 BT FS 349 AND FS 367 IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW EC/TC REO 601R-53-00-530. PERFORMED UT THICKNESS INSP IAW BSC NDTM SEC 4.3 MIN REM
- [SDR ASOA2016042914827](https://openairdocs.org/sdr/ASOA2016042914827.md): Seat Track · corroded · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK SEGMENT BETWEEN FS 400 TO FS 409+128 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A.
- [SDR ASOA2016042914825](https://openairdocs.org/sdr/ASOA2016042914825.md): Seat Track · corroded · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION AROUND SEVERAL SCREW HEADS, MARKED. EVALUATED LBL9 FLOOR SEAT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED LBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-000-802. CO
- [SDR ASOA2016042914824](https://openairdocs.org/sdr/ASOA2016042914824.md): Seat Track · corroded · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION IN A FEW SPOTS. EVALUATED RBL9 FLOORS AT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED RBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRIC
- [SDR ASOA2016042914823](https://openairdocs.org/sdr/ASOA2016042914823.md): Seat Track · corroded · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9, FLOOR SEAT RAIL SEGMENT BETWEEN FS 400 TO FS 409+128 IS CORRODED OUT OF LIMITS. EVALUATED RBL9, FLOOR SEAT RAIL FS 400-FS 409+128 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVE SEAT RAIL. REMOVED RBL9, SEAT RAIL FS 400-FS 409+128 IAW AMM 53-01-11-
- [SDR ASOA2016042914822](https://openairdocs.org/sdr/ASOA2016042914822.md): Floorbeam · cracked · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE CLIP CRACKED AT FS 280 AND RBL9, INBD SIDE. RECEIVED REO 601R-53-11-2904 AND COMPLIED WITH ALL STEPS OF REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.
- [SDR ASOA2016042914821](https://openairdocs.org/sdr/ASOA2016042914821.md): Floorbeam · cracked · Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE CLIP CRACKED AT FS 280 AND LBL 9; OTBD SIDE. RECEIVED AND COMPLIED WITH REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.
- [SDR ASOA2016042614838](https://openairdocs.org/sdr/ASOA2016042614838.md): Skin · cracked · Apr 26, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AT FS 192.00 BELOW TRU DOOR LT IAW SRM 51-42-06 AND 51-42-13-00. LOCATED AND DRILLED NEW SERVICEABLE LT DOOR LAND BELOW AFT TRU DOOR AT APPROXIMATELY
- [SDR ASOA2016042614820](https://openairdocs.org/sdr/ASOA2016042614820.md): Door · lack of lube · Apr 26, 2016 · N880AS · Cndair CL6002B19 · Emergency Exits
  > RIGHT EMERGENCY DOOR FAILED PULL TEST 70 LBS. LUBRICATED RT EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-802. PERFORMED PULL TEST OF RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-801, STEPS 4.A, 1, 3. PULL TEST GOOD.
- [SDR ASOA2015110914005](https://openairdocs.org/sdr/ASOA2015110914005.md): Light · damaged · Nov 9, 2015 · N880AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR-LEVEL EMERGENCY FLOOD LIGHT AT MAIN ENTRANCE DOOR DAMAGED. R & R FLOOD LIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015072913402](https://openairdocs.org/sdr/ASOA2015072913402.md): Wire · misinstalled · Jul 29, 2015 · N880AS · Cndair CL6002B19 · Light System Wiring
  > REF DMIL A595210 FWD CABIN EMERGENCY CEILING LIGHT INOPERATIVE. TROUBLESHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00.
- [SDR ASOA2015072713391](https://openairdocs.org/sdr/ASOA2015072713391.md): Wire · misinstalled · Jul 27, 2015 · N880AS · Cndair CL6002B19 · Light System Wiring
  > FWD CABIN EMERGENCY CEILING LIGHT IS INOPERATIVE. TROUBLE SHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORRECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00. OPS CHECK GO
- [SDR ASOA2015031312377](https://openairdocs.org/sdr/ASOA2015031312377.md): Trunnion · damaged · Mar 3, 2015 · N880AS · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > RIGHT TOP AFT HOLE ON HORIZONTAL STABILIZER TRUNNION AND ACFT HORIZONTAL STABILIZER OVERSIZED TO.4125, MAX IS.380. REMOVED MOUNTING HARDWARE FROM HORIZONTAL STA IAW AMM 27-42-01-000-801. BOTTOM PINS AND TRUNNIONS TEMP INSTALLED. INSTALLED MOUNTING HARDWA
- [SDR ASOA2014111211631](https://openairdocs.org/sdr/ASOA2014111211631.md): Lamp · burned out · Nov 7, 2014 · N880AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2014071110849](https://openairdocs.org/sdr/ASOA2014071110849.md): Flashlight · inoperative · Jul 9, 2014 · N880AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2014052710602](https://openairdocs.org/sdr/ASOA2014052710602.md): Bulb · inoperative · May 19, 2014 · N880AS · Cndair CL6002B19 · Emergency Lighting
  > GALLEY FLOOR EMERGENCY LIGHT EXIT SIGN HAS FIVE BAD BULBS. REMOVED BULBS FROM THE GALLEY EMERGENCY LIGHT FLOOR EXIT SIGN AND REPLACED WITH SERVICEABLE BULBS IAW 33-51-10-400-801.
- [SDR ASOA2014052710601](https://openairdocs.org/sdr/ASOA2014052710601.md): Angle · corroded · May 16, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO ANGLES AT FS 364 LBL AND RBL 18 ARE CORRODED. REMOVED DAMAGED ANGLES IAW SRM 51-42-06. FABRICATED AND INSTALLED NEW ANGLES IAW SNIEO 601R31049-S02.
- [SDR ASOA2014052710600](https://openairdocs.org/sdr/ASOA2014052710600.md): Skin · buckled · May 8, 2014 · N880AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT SKIN ARE BUCKLED, COMPLIED WITH REO:601R-52-11-2227.
- [SDR ASOA2014052710599](https://openairdocs.org/sdr/ASOA2014052710599.md): Skin · damaged · May 7, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING VISUAL INSPECTION FOR LIGHTNING STRIKE DAMAGE, FOUND BURNED RIVETS. FOUND TO BE SATISFACTORY.
- [SDR ASOA2014052710598](https://openairdocs.org/sdr/ASOA2014052710598.md): Skin · cracked · May 7, 2014 · N880AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT FUEL ACCESS HOLE 550HB HAS MULTIPLE INDICATIONS ON INBD, FWD & AFT SIDE 50 PERCENT FSH, FAILED NDT. C/W ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014052710597](https://openairdocs.org/sdr/ASOA2014052710597.md): Beam · corroded · May 5, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 349.00 TRANSVERSE BEAM IS CORRODED OTBD OF RBL 27.00. REO 601R-53-21-2534 REV--HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD. RII'S HAVE BEEN ACCOMPLISHED IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNE
- [SDR ASOA2014052710596](https://openairdocs.org/sdr/ASOA2014052710596.md): Skin · cracked · May 5, 2014 · N880AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZONTAL LANDING 50 PERCENT FSH FAILED NDT. BLENDED RT WING LOWER SKIN PLANK AT BOOST PUMP LANDING IAW STS EA 26-2014-050.
- [SDR ASOA2014052710595](https://openairdocs.org/sdr/ASOA2014052710595.md): Bearing · worn · May 4, 2014 · N880AS · Cndair CL6002B19 · Rudder Structure
  > RUDDER UPPER AND LOWER CENTER HINGE BEARINGS HAVE EXCESSIVE PLAY. COMPLIED WITH EC/TC RIL 0602, REPAIR TYPE II: REPLACEMENT OF THE SWAGED BEARING IAW RIL 602, REV E.
- [SDR ASOA2014052710594](https://openairdocs.org/sdr/ASOA2014052710594.md): Bracket · corroded · May 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MAIN AVIONICS DOOR LATCH PIN RECEIVER SUPPORT BRACKET FS 364.00 FRAME SECTOR AT BL 0 TO BE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 T/R 53-27, FIG 102, SHEET 2. CORROSION IS ON OVERLAPPING ELEMENTS THRU RADIUS. LOCATED, DRILLED UP & INST
- [SDR ASOA2014052710593](https://openairdocs.org/sdr/ASOA2014052710593.md): Intercostal · cracked · May 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 625 CRACKED INTERCOSTAL AT STRINGERS 13 & 14L. REMOVED INTERCOSTAL IAW SRM 51-42-21 AND 51-42-06. LOCATED & DRILLED INTERCOSTAL IAW SRM 51-40-11 AND DWG 601-35012. LOCATED NEW FASTENER HOLES TO NEW SERVICEABLE INTERCOSTAL IAW REO 601R-53-61-5265. MAJOR
- [SDR ASOA2014052710592](https://openairdocs.org/sdr/ASOA2014052710592.md): Striker · dented · May 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR CUT-OUT SEAL STRIKER, UPPER, AT FS 310 IS DAMAGED. C/W BSC REO 601R-53-22-176 REV IAW SRM 51-42-06 AND 51-40-11.
- [SDR ASOA2014052710591](https://openairdocs.org/sdr/ASOA2014052710591.md): Door Sill · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL IS CORRODED. REMOVED SERVICE DOOR SILL ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICE DOOR SILL ANGLE, PN 601R38303-253 IAW SRM 51-40-11 AND DWG 601R38303. INSTALLED SILL ANGLE IAW SRM 51-42-06 AND SRM 51-42-11.
- [SDR ASOA2014052710590](https://openairdocs.org/sdr/ASOA2014052710590.md): Door Frame · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Structure
  > SERVICE DOOR SURROUND FWD FITTING AND FLOOR EDGE MEMBER ARE CORRODED AT BS 319. DAMAGE TO FLOOR EDGE MEMBER FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27 AND REQUIRES REPLACEMENT FROM FS 310-319. REMOVED AND LOCATED NEW PART, PN 601R31148-79 IAW SRM 5
- [SDR ASOA2014052710589](https://openairdocs.org/sdr/ASOA2014052710589.md): Intercostal · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 364 INTERCOSTAL BETWEEN 26L & 26R CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2014052710588](https://openairdocs.org/sdr/ASOA2014052710588.md): Frame · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 364 S23L - 23R IS CORRODED. R & R FRAME SUPPORT ANGLE FROM AFT SIDE OFFS 364.0 IAW SRM 51-42-06. R & R INTERCOSTALS AT LBL/RBL 18.0 BETWEEN FS 349.0-FS 364.0 IAW SRM 51-42-06. R & R FRAME SECTOR AND SPLICE ANGLE FROM FS 364.0 BETWEEN STRINGERS 2
- [SDR ASOA2014052710587](https://openairdocs.org/sdr/ASOA2014052710587.md): Door Sill · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES. REMOVED CORROSION IAW REO 601R-53-00-526. FOUND TO BE WITHIN LIMITS WITH MAX MATERIAL REMOVED.004, MAX ALLOWABLE.010. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.
- [SDR ASOA2014052710586](https://openairdocs.org/sdr/ASOA2014052710586.md): Stringer Clip · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280, STRINGER CLIP 3L CRACKED. REMOVED FS 280 STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2014052710585](https://openairdocs.org/sdr/ASOA2014052710585.md): Angle · cracked · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT 484, ANGLE AT RBL 27 IS CRACKED.250L. REMOVED CRACKED ANGLE AND LOCATED, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.
- [SDR ASOA2014052710584](https://openairdocs.org/sdr/ASOA2014052710584.md): Isolator · broken · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD FWD FACE HAS A BROKEN ISOLATOR. R & R BROKEN ISOLATOR IAW SRM 51-42-06.
- [SDR ASOA2014052710583](https://openairdocs.org/sdr/ASOA2014052710583.md): Fitting · cracked · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 460, FITTING ON OTBD SIDE OF RBL 9 IS CRACKED.5". REMOVED THE SUPPORT FITTING IAW SRM 51-42-21 AND 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SUPPORT FITTING IAW SRM 51-40-11, 51-42-06 AND 51-42-21. MAJOR REPAIR.
- [SDR ASOA2014052310582](https://openairdocs.org/sdr/ASOA2014052310582.md): Bearing · worn · May 2, 2014 · N880AS · Cndair CL6002B19 · Elevator Structure
  > RIGHT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS. REPLACED BEARINGS IAW AMM 20-26-00-910-807.
- [SDR ASOA2014052310581](https://openairdocs.org/sdr/ASOA2014052310581.md): Bearing · worn · May 2, 2014 · N880AS · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS REPLACED BEARING IAW EC/TC RIL 0183 AND RIL 0183, REV B.
- [SDR ASOA2014051210490](https://openairdocs.org/sdr/ASOA2014051210490.md): Cargo Track · corroded · May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED LBL 9. R & R CARGO TRACK IAW AMM 20-21-00-910-801 AND SRM 51-40-11.

Next page: https://openairdocs.org/aircraft/N880AS/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 = 'N880AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N880AS/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.