# Service difficulty reports: N849AS, cancelled Dec 9, 2025

A list on [N849AS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N849AS-2025-12-09.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 · 162 reports

- [SDR ASOA2016081615271](https://openairdocs.org/sdr/ASOA2016081615271.md): Battery · discharged · Aug 16, 2016 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHTS ARE NOT ILLUMINATING IN THE CEILING AND AT THE FWD EXITS AND GALLEY. CHARGED & OPS CHECKED OK IAW AMM 33-51-04.
- [SDR ASOA2016041214701](https://openairdocs.org/sdr/ASOA2016041214701.md): Roller · stuck · Apr 12, 2016 · N849AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. FREED ROLLER ON INNER HANDLE AND PERFORMED OPS CHECK. NO FURTHER DEFECTS NOTED AMM 52-11-00.
- [SDR ASOA2016040714695](https://openairdocs.org/sdr/ASOA2016040714695.md): Roller · failed · Apr 7, 2016 · N849AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. R & R PASSENGER DOOR ROLLER ASSY IAW AMM 52-11-02. LUBED AND PERFORMED OPS CHECK OF PASSENGER DOOR OUTER HANDLE ASSY IAW AMM 52-11-03.
- [SDR ASOA2016040314683](https://openairdocs.org/sdr/ASOA2016040314683.md): Handle · lack of lube · Apr 3, 2016 · N849AS · Cndair CL6002B19 · Passenger/Crew Doors
  > COULD NOT OPEN PAX DOOR FROM OUTSIDE ACFT. HAD TO ENTER ACFT FROM SERVICE DOOR. WAS ABLE TO OPEN FROM INSIDE. TESTED DOOR AGAIN FROM OUTSIDE W/ NO SUCCESS. FOUND OUTER HANDLE NOT COMING OUT FAR ENOUGH. CLEANED AND LUBED AND OPS CHECKED PASSENGER DOOR OUTER
- [SDR ASOA2016012114374](https://openairdocs.org/sdr/ASOA2016012114374.md): Lens · missing · Jan 21, 2016 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > MISSING LENS ON OVERHEAD EMERGENCY EXIT LIGHT. INSTALLED MISSING LENS ON OVERHEAD EMERGENCY EXIT LIGHT IAW AMM 33-51-14.
- [SDR ASOA2015102313949](https://openairdocs.org/sdr/ASOA2015102313949.md): Apu · odor · Oct 23, 2015 · N849AS · Cndair CL6002B19 · APU Core Engine
  > DURING APPROACH STRONG AROMA OF FUEL/OIL FILLED CABIN COMING FROM APU IN AFT EQUIPMENT BAY. AUXILIARY POWER UNIT, APU, DOOR POSITION VERIFIED CLOSED. DEFER CLEARED, PLACARD REMOVED. COMPLIED WITH "APU CHANGE", ACFT RETURNED TO SERVICE.
- [SDR ASOA2015081313480](https://openairdocs.org/sdr/ASOA2015081313480.md): Actuator · failed · Aug 13, 2015 · N849AS · Cndair CL6002B19 · Auto Flight System
  > UNCOMMENDED YAW DAMPER IN MOTION WAS DETECTED IN THE CLIMB AROUND 290 KNOTS WITH AP OFF C/W QRH AND IN DESCENT MOTION WAS DETECTED 2 TIMES AT 250 KNOTS SEVERAL NOSE TRIM REQUIRED. ENROUTE TO DTW ACFT DIVERTED DUE TO MAINTENANCE. EMERGENCY DECLARED AS A PREC
- [SDR ASOA2015071013315](https://openairdocs.org/sdr/ASOA2015071013315.md): Structure · damaged · Jul 6, 2015 · N849AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING L/E NR 1 AND NR 2 HAS 1 EACH SHEAR RIVET LOCATED AT TRANSITION PANEL. COMPLIED WITH EC/TC REO 601R-57-41-001, PERMANENT REPAIR.
- [SDR ASOA2015041012600](https://openairdocs.org/sdr/ASOA2015041012600.md): Seat Track · corroded · Mar 20, 2015 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR BEAM CORRODED INBD SIDE OF SEAT RAIL AT FS94.00-409.00+112. RECEIVED REO 601R-53-31-841, DATED 2015-03-24. REMOVED EXTRUDED FLOORBEAM CAP FS394.00-409.00+112 IAW REO 601R-53-31-841. COMPLIED WITH REO 601R-53-31-841. COMPLIED WITH EC/TC REO 601R-53-31
- [SDR ASOA2015041012599](https://openairdocs.org/sdr/ASOA2015041012599.md): Floor Support · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL AFT OF THE SERVICE DOOR AT FS 349-364 CORRODED. REMOVED CORROSION IAW EC/TC REO 601R-53-00-530 DAMAGE OUT OF LIMITS IAW REO 601R-53-00-530. COMPLIED WITH ALL STEPS OF REV 601R-53-21-2603. COMPLIED WITH REO 601R-53-21-2601. COMPLIED WITH EC
- [SDR ASOA2015041012598](https://openairdocs.org/sdr/ASOA2015041012598.md): Seat Track · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL CORRODED AT FS 559.00 TO 559.00 + 80, RBL 9. SEAT RAIL AT RBL 9.0, FS 559.00 TO 559+80 HAS EXFOLIATING CORROSION AROUND SEVERAL FASTENER HEADS OUT OF LIMITS IAW SRM 51-21-49, FIG 101. REMOVED SEAT RAIL AT RBL 9.0, STA 559.00 TO 559+80 IAW SRM
- [SDR ASOA2015041012597](https://openairdocs.org/sdr/ASOA2015041012597.md): Door Frame · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FWD OF AVIONICS BAY DOOR ACCESS AT FS 364.00 FWD SIDE CORRODED, BETWEEN STR 25L-25R. REMOVED CORROSION ON FS 364 BETWEEN 26L & 27 STR IAW SRM 51-21-01-00 UPON FURTHER INVESTIGATION FOUND NO CORROSION ON BETWEEN 25L AND 26L STR ON FS 364. REMOVED CORROSION ON
- [SDR ASOA2015041012596](https://openairdocs.org/sdr/ASOA2015041012596.md): Seat Track · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT FS 694.00- 409.00+12 AND RBL 27 CORRODED. FLOOR SEAT RAIL RBL9, FS 394.00 TO 409+112 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT RAIL RBL 9.0, FS 394.00 TO 409+112 IAW AMM 53-01-11-000-802. DRILLED AND COUNTERSUNK A
- [SDR ASOA2015041012595](https://openairdocs.org/sdr/ASOA2015041012595.md): Floor Support · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 484.00 - FS 559.00+21. COMPLIED WITH ECTC REO 601R-53 -41-666, REV C.
- [SDR ASOA2015041012594](https://openairdocs.org/sdr/ASOA2015041012594.md): Floor Support · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 484.00 - FS 559+21. COMPLIED WITH ECTC REO 601R-53 -41-666-01.
- [SDR ASOA2015041012593](https://openairdocs.org/sdr/ASOA2015041012593.md): Floor Support · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT OVERWING PRESSURE FLOOR SUPPORT CORRODED BETWEEN FS 409+128-484.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01, REO 601R 53-41-666, REV C.
- [SDR ASOA2015041012592](https://openairdocs.org/sdr/ASOA2015041012592.md): Floor Support · corroded · Mar 19, 2015 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OVERWING PRESSURE FLOOR SILL CORRODED BETWEEN FS 409+128-FS 484.00. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C, DATED 11/06/2012 AS WRITTEN.
- [SDR ASOA2015041012591](https://openairdocs.org/sdr/ASOA2015041012591.md): Skin · cracked · Mar 18, 2015 · N849AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT SIDE WING, AT 148.019 IS CRACKED ON AFT PLANK, PROXIMITY.102. COMPLIED WITH ECTC REO 601R-57-21-130-01 AND REO 601R-57-21-130-01, REV K DATED 11/27/2013 AS WRITTEN. INSTALLED RT WING -9 REPAIR STRAP AT WS148.019, REF SRM 51-42-21 AND REO 601R-57-21-13
- [SDR ASOA2015041012590](https://openairdocs.org/sdr/ASOA2015041012590.md): Door · lack of lube · Mar 16, 2015 · N849AS · Cndair CL6002B19 · Emergency Exits
  > LEFT OVERWING EMERGENCY EXIT EXCEEDS MAX FORCE TO OPERATE HANDLE. LUBED LT OVERWING EMERGENCY EXIT DOOR AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-710-801 AND 12-20-52-340-802.
- [SDR ASOA2015041012589](https://openairdocs.org/sdr/ASOA2015041012589.md): Door · lack of lube · Mar 16, 2015 · N849AS · Cndair CL6002B19 · Emergency Exits
  > RIGHT OVERWING EMERGENCY EXIT EXCEEDS MAX FORCE TO OPERATE HANDLE. LUBED RT OVERWING EMERGENCY EXIT DOOR AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-710-801 AND 12-20-52-340-802, FUNCTIONAL CHECK GOOD.
- [SDR ASOA2015041012588](https://openairdocs.org/sdr/ASOA2015041012588.md): Light · weak · Mar 16, 2015 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXITS AND SERVICE DOOR BETA LIGHTS WEAK. R & R EMERGENCY EXIT BETA LIGHTS.
- [SDR ASOA2014121111860](https://openairdocs.org/sdr/ASOA2014121111860.md): Light · inoperative · Dec 7, 2014 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT IN GALLEY AND MAIN PASSENGER ENTRY ARE INOPERATIVE. REPLACED LIGHT IAW AMM 33-51-19.
- [SDR ASOA2014121011859](https://openairdocs.org/sdr/ASOA2014121011859.md): Light · inoperative · Dec 6, 2014 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT AT PASSENGER DOOR INOPERATIVE. R & R THE LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.
- [SDR ASOA2014100811387](https://openairdocs.org/sdr/ASOA2014100811387.md): Skin · cracked · Sep 4, 2014 · N849AS · Cndair CL6002B19 · Wing, Plate/Skin
  > WING SKIN FOUND TO HAVE CRACK INDICATION WHILE PERFORMING LOW FREQUENCY INSPECTION AT WS 65.75 SECOND ROW OF FASTENERS BETWEEN STR8 AND STR9, SECOND FASTENER INBD FROM WS 65.75.
- [SDR ASOA2014081511069](https://openairdocs.org/sdr/ASOA2014081511069.md): Blanking Plate · leaking · Aug 11, 2014 · N849AS · Cndair CL6002B19 · Turbine Engine Oil System
  > SLOWLY LOST OIL PRESSURE DURING FLIGHT, SHUTDOWN NR 1 ENGINE, OIL PULL NEVER GOT BELOW 25 PSI, EMERGENCY DECLARED. FOUND OIL LEAK AT BLANKING PLATE FOR EDP.
- [SDR ASOA2014042810392](https://openairdocs.org/sdr/ASOA2014042810392.md): Skin · burned · Apr 23, 2014 · N849AS · Cndair CL6002B19 · Wing, Plate/Skin
  > BURNS ON LT WINGLET TIP FAIRING. REMOVED DAMAGED LT WINGLET TIP IAW SRM 51-42-13. REMOVED AND REPLACED.
- [SDR ASOA2013110809372](https://openairdocs.org/sdr/ASOA2013110809372.md): Lamp · burned out · Nov 4, 2013 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA2013100209142](https://openairdocs.org/sdr/ASOA2013100209142.md): Lens · missing · Oct 1, 2013 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 CEILING EMERGENCY LIGHT COVER MISSING. INSTALLED NEW COVER IAW AMM 35-51-16, OPS CHECKED GOOD.
- [SDR ASOA2013042203418](https://openairdocs.org/sdr/ASOA2013042203418.md): Light · broken · Apr 16, 2013 · N849AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT AT LOWER BULKHEAD PAX DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY LIGHT OPS CHECKED GOOD REF MM 33-51-10.
- [SDR ASOA2013041003344](https://openairdocs.org/sdr/ASOA2013041003344.md): Access Panel · cracked · Mar 26, 2013 · N849AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT BOOST PUMP HOLE FAILS NDT WITH AN INDICATION ON AFT SIDE OF HOLE WITH MULTIPLE INDICATING, SOME 50 PERCENT SCREEN HEIGHT (ON LANDING). REPAIRED IAW REO 601R-57-21-1900. MAJOR REPAIR.
- [SDR ASOA2013041003338](https://openairdocs.org/sdr/ASOA2013041003338.md): Post · cracked · Mar 22, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND FS 409+128 VERTICAL POSTS AT LBL18.0 INBD SIDES HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX.2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED AND INSTALLED VERTICAL POST IAW REO 601R-53-41-889 REV A AND SRM 51-42-06.
- [SDR ASOA2013041003337](https://openairdocs.org/sdr/ASOA2013041003337.md): Post · cracked · Mar 22, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND FS 409+128 VERTICAL POSTS AT BL0.0 LT & RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS WL 69.0 BOTH APPROX.3" IN LENGTH 70 PERCENT AND 80 PERCENT FSH. BOTH FAILED NDT INSPECTION. INSTALLED NEW SERVICEABLE POST ASSY IAW REO 601R-53-41-889 REV A AN
- [SDR ASOA2013041003343](https://openairdocs.org/sdr/ASOA2013041003343.md): Hinge · gouged · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR PIANO HINGE ON PAX DOOR SIDE 1ST AND 6TH LUG FROM AFT SIDE CHAFED. DEEPEST APPROX.015. REMOVED PASSENGER DOOR IAW AMM 52-11-000-801. INSTALLED PASSENGER DOOR IAW AMM 52-11-00-400-801. REPAIRED IAW REO 601R-52-11-2152, REO 601R-52-11-1347 AND AMM
- [SDR ASOA2013041003342](https://openairdocs.org/sdr/ASOA2013041003342.md): Access Panel · damaged · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT FWD FUSELAGE ACCESS PANEL 132AL DOOR SURROUND FASTENER HOLE DAMAGED AT 7 0'CLOCK POSITION. REPAIRED IAW REO 601R-53-11-2477. MAJOR REPAIR.
- [SDR ASOA2013041003341](https://openairdocs.org/sdr/ASOA2013041003341.md): Fitting · chafed · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RT WING T/E OTBD FLAP ALIGNMENT RECEPTACLE IS CHAFED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.
- [SDR ASOA2013041003340](https://openairdocs.org/sdr/ASOA2013041003340.md): Fitting · chafed · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LT WING T/E FLAP ALIGNMENT RECEPTACLE IS CHAFED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.
- [SDR ASOA2013041003339](https://openairdocs.org/sdr/ASOA2013041003339.md): Skin · chafed · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > TOP CENTER OF CARGO DOOR EXTERIOR SKIN IS CHAFED 1.5" LONG,.350" WIDE,.018" DEEP. REPAIRED CARGO DOOR IAW REO 601R-52-31-198 REV A, MAJOR REPAIR.
- [SDR ASOA2013041003336](https://openairdocs.org/sdr/ASOA2013041003336.md): Bulkhead · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 621 REAR PRESSURE BULKHEAD TO HAVE AN INDICATION NOTED AT LBL 27.50 AND WL 130 (TOP OF CARGO DOOR TRACK) APPROX.500" LONG X 70 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541, REV D, DATED 10/31/11.
- [SDR ASOA2013041003335](https://openairdocs.org/sdr/ASOA2013041003335.md): Bulkhead · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 621 REAR PRESS BULKHEAD TO HAVE AN INDICATION NOTED AT LBL 36.2 AND APPROX WL 80 APPROX.500" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. R & R APU FUEL FEED LINE WITH A SERVICEABLE SHROUD ASY PN CA447 IAW AMM 28-20-01-400-801; AND COMPLIED WITH S
- [SDR ASOA2013041003334](https://openairdocs.org/sdr/ASOA2013041003334.md): Structure · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT VERTICAL MEMBER IS CRACKED INSIDE OF DOOR AT LOWER AFT DOOR STOP FITTING. INSTALLED NEW SERVICEABLE AFT VERTICAL MEMBER, IAW SRM 51-42-06.
- [SDR ASOA2013041003333](https://openairdocs.org/sdr/ASOA2013041003333.md): Seat Track · corroded · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 349, RBL 9 SEAT TRACK HAS CORROSION. R & R SEAT TRACK SEGMENT FS 349 TO FS 395.0 IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2013041003332](https://openairdocs.org/sdr/ASOA2013041003332.md): Support Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 INBD SIDE OF RBL 9.0 1 EA SUPPORT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-11-926, STEP 11 AND 12.
- [SDR ASOA2013041003331](https://openairdocs.org/sdr/ASOA2013041003331.md): Fitting · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT'S WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. R & R WITH NEW FITTING PN 601R33245-45 IAW SRM 51-42-21.
- [SDR ASOA2013041003330](https://openairdocs.org/sdr/ASOA2013041003330.md): Isolator · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD FACE OF THE FS 621 REAR PRESSURE BULKHEAD BETWEEN WL 74.00 AND WL 110.00 HAS 9 ISOLATORS EITHER CRACKED OR MISSING. 4 AT RBL 45, 1 AT RBL 36.2, 1 AT RBL 27.5, 1 AT RBL 9.5, 1 AT LBL 9.5 AND 1 AT LBL 27. ALL ISOLATORS ARE MARKED WITH RED TAPE. REPLACE
- [SDR ASOA2013041003329](https://openairdocs.org/sdr/ASOA2013041003329.md): Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.0 INBD SIDE OF LBL 9.0 1 EA SUPPORT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-11-926 STEP 11 AND 12.
- [SDR ASOA2013041003328](https://openairdocs.org/sdr/ASOA2013041003328.md): Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484.0 TWO SUPPORT ANGLES CRACKED AT LBL 27.0 AND LBL 36.0. INSTALLED NEW SUPPORT ANGLES IAW SRM 51-42-21.
- [SDR ASOA2013041003327](https://openairdocs.org/sdr/ASOA2013041003327.md): Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484.00 TWO SUPPORT ANGLES CRACKED AT RBL 27.0 AND RBL 36.0. R & R ANGLES IAW SRM 51-42-21.
- [SDR ASOA2013041003326](https://openairdocs.org/sdr/ASOA2013041003326.md): Attach Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING CENTER LEADING EDGE INBD ATTACHING ANGLE CRACKED IN RADIUS. INSTALLED NEW ANGLE IAW AMM 20-21-00-910-801.
- [SDR ASOA2013041003325](https://openairdocs.org/sdr/ASOA2013041003325.md): Drag Angle · cracked · Mar 21, 2013 · N849AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIR. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-517.
- [SDR ASOA201201060](https://openairdocs.org/sdr/ASOA201201060.md): Idg · failed · Mar 27, 2012 · N849AS · Cndair CL6002B19 · AC Generator-Alternator
  > NR 1 GENERATOR FAILED ENROUTE, ACFT DIVERTED. R & R NR 1 IDG ASSY IAW AMM 24-11-01, PERFORMED IDG ENGINE RUN LEAK AND OPS CHECK, OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N849AS-2025-12-09/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 = 'N849AS' AND deregistration_id = 'N849AS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N849AS-2025-12-09/reports

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