# Service difficulty reports: N844AS, cancelled Jul 30, 2018

A list on [N844AS, cancelled Jul 30, 2018](https://openairdocs.org/deregistered/N844AS-2018-07-30.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 6 · 283 reports

- [SDR ASOA2016090415351](https://openairdocs.org/sdr/ASOA2016090415351.md): Light · inoperative · Sep 4, 2016 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT EXIT ROW EMERGENCY EXIT MARKER INOPERATIVE. R & R LT EXIT ROW EMERGENCY EXIT MARKER IAW AMM 33-51-13. OPS CHECK GOOD. SDR CLOSED.
- [SDR ASOA2016052714898](https://openairdocs.org/sdr/ASOA2016052714898.md): Sign · inoperative · May 27, 2016 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > ROW 8A EMERGENCY EXIT,EXIT SIGN INOPERATIVE. R & R ROW 8A LIGHTED EXIT SIGN IAW AMM 33-51-10. OPS CHECK GOOD.
- [SDR ASOA2016040414688](https://openairdocs.org/sdr/ASOA2016040414688.md): Door · unknown · Apr 4, 2016 · N844AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WILL NOT LOCK IN CLOSED POSITION AND WILL NOT OPEN. C/W OPS TEST GOOD IAW AMM 52-11-02, NO DEFECT NOTED.
- [SDR ASOA2016021714496](https://openairdocs.org/sdr/ASOA2016021714496.md): Door · binding · Feb 17, 2016 · N844AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM INSIDE. HAD TO GET RAMP TO OPEN FROM OUTSIDE. INSPECTED PASSENGER DOOR AND LATCH MECHANISM AND PAX DOOR HANDLE NO DEFECTS NOTED REF AMM 52-11-00.
- [SDR ASOA2016021614495](https://openairdocs.org/sdr/ASOA2016021614495.md): Door · binding · Feb 16, 2016 · N844AS · Cndair CL6002B19 · Passenger/Crew Doors
  > DOOR HANDLE STUCK COULD NOT OPEN DOOR FROM INSIDE MAIN DOOR. INSP DOOR NO DEFECT NOTED OPENED AND CLOSED DOOR IAW AMM 52-11-00 DOOR OPERATE NORMALLY. ACFT OK FOR SERVICE.
- [SDR ASOA2016021314456](https://openairdocs.org/sdr/ASOA2016021314456.md): Linkage · fouled · Feb 13, 2016 · N844AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. FOUND LANYARD CAUGHT UP IN LINKAGE. RESECURED LANYARD AND PERFORMED OPS TEST OF PASSENGER DOOR IAW AMM 52-11-00. OPS TESTED 10 TIMES. NO DEFECTS NOTED AT THIS TIME.
- [SDR ASOA2016020814447](https://openairdocs.org/sdr/ASOA2016020814447.md): Door · binding · Feb 8, 2016 · N844AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN PASSENGER DOOR WOOULD NOT OPEN FROM THE INSIDE. PERFORMED OPS TEST OF PASSENGER DOOR SEVERAL TIMES IAW AMM 52-11-00. FURTHER FAULTS FOUND AT THIS TIME, OK FOR SERVICE.
- [SDR ASOA2016010714363](https://openairdocs.org/sdr/ASOA2016010714363.md): Attach Angle · cracked · Jan 7, 2016 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INBD AND OTBD ANGLES ATTACHED TO STR3L BETWEEN FS 280 TO FS 295 ARE CRACKED. REMOVED INBD AND OTBD ANGLE AT STR 3L BETWEEN FS 280 AND FS 294 IAW SRM 51-42-06. LOCATED TRANSFERED DRILLED MOUNT HOLES AND INSTALLED SERVICABLE INBD AND ON ANGLES AT STR 3L BETWEEN
- [SDR ASOA2016010714349](https://openairdocs.org/sdr/ASOA2016010714349.md): Floor Support · corroded · Jan 7, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SUPPORT ANGLE OF FLOOR PANEL 221ALF. BLENDED AND REMOVED CORROSION IAW SRM 51-21-06-00. RECEIVED AND COMPLIED WITH EA 15-2016-002.
- [SDR ASOA2016010614348](https://openairdocs.org/sdr/ASOA2016010614348.md): Intercostal · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SIDE INTERCOSTAL CRACKED AT WL 84.00 BETWEEN FS 621.00 AND FS 625.30. R & R INTERCOSTAL AT WL 84, BS 621 IAW SRM 51-42-21, 51-42-02.
- [SDR ASOA2016010614347](https://openairdocs.org/sdr/ASOA2016010614347.md): Intercostal · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SIDE INTERCOSTAL CRACKED AT WL 80.00 BETWEEN FS 621.00 AND 625.30. REMOVED CRACKED INTERCOSTAL AT WS 80.00 BETWEEN FS 621.00 AND 625.30 THEN INSTALL NEW INTERCOSTAL AT SAME LOCATION IAW SRM 51-42-06, 51-42-21.
- [SDR ASOA2016010614346](https://openairdocs.org/sdr/ASOA2016010614346.md): Bracket · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT SUPPORT STRUCTURE RT FWD POST TIE PLATE CRACKED, FS 640.00 STR 24RH. REMOVED CRACKED BRACKET, INSTALLED NEW BRACKET AT AFT EQUIPMENT BY APU SUPPORT, RT AND LT FWD POST UPPER IB GUIDE IAW SRM 51-42-13.
- [SDR ASOA2016010614335](https://openairdocs.org/sdr/ASOA2016010614335.md): Intercostal · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SIDE INTERCOSTAL CRACKED AT WL 76.00 BETWEEN FS 621.00 AND 625.30. REMOVED CRACKED BRACKET, INSTALLED NEW BRACKET AT AFT EQUIPMENT BY APU SUPPORT, RT AND LT FWD POST UPPER INBD GUIDE IAW SRM 51-42-13.
- [SDR ASOA2016010614330](https://openairdocs.org/sdr/ASOA2016010614330.md): Intercostal · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE INTERCOSTAL CRACKED AT WL 90.00 BETWEEN FS 621.00 AND FS 625.30. REMOVED INTERCOSTAL LT SIDE & STIFFENER FORM WL 90.00 BTS. FS 621 & 625 REF SRM 42-21 & SRM 51-42-00. LOCATED AND DRILLED LT SIDE INTERCOSTAL AT WL 90.00 BTS FS 621 AND FS 625.30 IAW
- [SDR ASOA2016010614329](https://openairdocs.org/sdr/ASOA2016010614329.md): Angle · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT WL 80.00 RT SIDE BETWEEN FS 621.00 AND 625.30. REMOVED CLIP AT WL 80 RT SIDE AND REPLACED WITH SERVICEABLE CLIP WL 80 BETWEEN FS 621 & FS 625.30 REF SRM 51-42-21.
- [SDR ASOA2016010614328](https://openairdocs.org/sdr/ASOA2016010614328.md): Angle · cracked · Jan 6, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT WL 80.00 LT SIDE BETWEEN FS 621.00 AND 625.30. REMOVED CLIP AND WL 80 LT SIDE & REPLACED WITH SERVICEABLE CLIP WL80 BETWEEN FS 621 & FS 625.30 REF SRM 51-42-21.
- [SDR ASOA2016010514362](https://openairdocs.org/sdr/ASOA2016010514362.md): Floor Support · corroded · Jan 5, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RT FLOOR SILL BETWEEN FS559.00-559.00+16. REMOVED CORROSION IAW SRM 51-21-06, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01. REMOVED INTERCOSTAL FOR REPLACMENT. DRILLED UP NEW INTERCOSTAL. REF: SRM 51-42-06 AND 51-40-11. DWG: 601R38842,
- [SDR ASOA2016010514361](https://openairdocs.org/sdr/ASOA2016010514361.md): Angle · cracked · Jan 5, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ASD UPPER FWD SILL CLIP CRACKED AT FS 280.00 AND STR 3. REMOVED CLEAT AT FS 280.00 AND STR 3 IAW SRM 51-42-06. LOCATED, TRANSFERD DRILLED MOUNTING HOLES AND INSTALLED SERVICEABLE CLEAT AT ASD UPPER SILL FWD AT FS 280 AND STR 3 REF SRM 51-40-11 AND SRM 51-42-
- [SDR ASOA2016010514360](https://openairdocs.org/sdr/ASOA2016010514360.md): Bulkhead · cracked · Jan 5, 2016 · N844AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE ABOVE FLOOR IS CRACKED AT BL 0.00 BETWEEN WL 73.50 AND WL 120.43. COMPLIED WITH ECTC REO601R-53-61-1285 08 AND GREO 601R-53-61-1285, REV D DATED: 10/31/2011 AS WRITTEN.
- [SDR ASOA2016010514359](https://openairdocs.org/sdr/ASOA2016010514359.md): Bracket · cracked · Jan 5, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED BRACKETS FOUND ON LBL9 AND 280 CROSSBEAM, BOTH OTBD AND INBD CLIP. REMOVED 2 EA, L-ANGLE CLIPS AT FS280, LBL9, OTBD ABD INBD IAW COMPLY WITH REO 601R-53-11. COMPLIED WITH REO 601R-53-11. RECEIVED AND COMPLIED WITH ECTC REO601R-53-11-2849.
- [SDR ASOA2016010514358](https://openairdocs.org/sdr/ASOA2016010514358.md): Bracket · cracked · Jan 5, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED BRACKETS FOUND ON RBL9 AND 280 CROSSBEAM, BOTH OTBD & INBD CLIP. REMOVED 2 EA L-ANGLE CLIPS AT FS 280, RBL 9 OTBD ABD INBD IAW COMPLY WITH REO 601R-53-11. INSTALLED NEW L-ANGLE CLIP AT FS 280, RBL9 RT INBD IAW SRM 51-42-21. COMPLIED WITH REO 601R-53
- [SDR ASOA2016010414384](https://openairdocs.org/sdr/ASOA2016010414384.md): Floor Support · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND BETWEEN BS 621 - 605 AND LBL 27. AREA IS OUT OF LIMIT IAW RED 601R-53-00-005, REV B. DATED JAN. 6, 2011, FIGURE 2. PERFORMED EDDY CURRENT INSPECTION IAW SRM 51-12-00, IAW 51-20-06. NO INDICATIONS NOTED AT THIS TIME. EVALUATED BLEND AT LBL 27
- [SDR ASOA2016010414364](https://openairdocs.org/sdr/ASOA2016010414364.md): Frame · cracked · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK FOUND AT 621.00 AND LBL 40. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-61-5619, REV O, DATED 2016-01-10. REMOVED 2 EA INTERCOSTALS TO GAIN ACCESS TO REPAIR AREA IAW SRM 51-42-21 AND 51-42-00. INSTALLED 2 EA INTERCOSTALS BACK TO ORIGINAL LOCATION IAW
- [SDR ASOA2016010414334](https://openairdocs.org/sdr/ASOA2016010414334.md): Structure · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SILL AT AT FS 559.00-FS 559.00-559+32 LBL 40. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526.
- [SDR ASOA2016010414333](https://openairdocs.org/sdr/ASOA2016010414333.md): Structure · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SILL & AROUND HEATER VENT AT FS 559.00 -559.00+80, RBL 40-45. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526.
- [SDR ASOA2016010414332](https://openairdocs.org/sdr/ASOA2016010414332.md): Door Sill · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SILL AT FS 559.00+80-559.00+12 AND LBL 40. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV DATED: 05/26/2013 AS WRITTEN.
- [SDR ASOA2016010414331](https://openairdocs.org/sdr/ASOA2016010414331.md): Door Sill · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CARGO DOOR SILL AT 574.00- 621.00 AROUND SCREW HOLES LBL40-45 TO 27. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV DATED: 05/22/2013 AS WRITTEN.
- [SDR ASOA2016010414327](https://openairdocs.org/sdr/ASOA2016010414327.md): Seat Track · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT RAIL AT FS 559.00+80 & RBL 9. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAILS AT FS 559.00 TO 559.00+80, RBL 9 IAW SRM 51-41-00-00 51-41-04 & IAW AMM 53-01-11-000-802/400-802.
- [SDR ASOA2016010414326](https://openairdocs.org/sdr/ASOA2016010414326.md): Seat Track · corroded · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND SEAT RAIL AT FS 559.00+80-559.00+96 AND RBL 27. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAILS AT FS 559.00+80 TO +96 RBL27 IAW SRM 51-41-00-00 & 51-41-04 & AMM 53-01-11-000-802 & 53-01-11-400-802.
- [SDR ASOA2016010414307](https://openairdocs.org/sdr/ASOA2016010414307.md): Plate · cracked · Jan 4, 2016 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON SILL PLATE AT FS 589.00 & LBL40. COMPLIED WITH ECTC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B DATED 10/09/2009 AS WRITTEN.
- [SDR ASOA2015121614219](https://openairdocs.org/sdr/ASOA2015121614219.md): Fan · failed · Dec 16, 2015 · N844AS · Cndair CL6002B16 · Air Distribution Fan
  > STRONG ELECTRICAL SMELL IN FLIGHT DECK. C/W OPS CHECK FOR STRONG ELECTRICAL SMELL IN FLIGHT DECK IAW AMM 21-24-19. OPS CHECK OK. DEFECT CLEARED. PLACARD REMOVED. ACFT OK FOR SERVICE. R & R OF GALLEY EXHAUST FAN.
- [SDR ASOA2015052212891](https://openairdocs.org/sdr/ASOA2015052212891.md): Light · inoperative · May 21, 2015 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > ROW 8 A/B FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR ASOA2015012812094](https://openairdocs.org/sdr/ASOA2015012812094.md): Battery Pack · inoperative · Jan 27, 2015 · N844AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT IS INOPERATIVE. R & R BATTERIES. OPS CHECKED GOOD IAW AMM 25-60-00. ACFT OK FOR SERVICE.
- [SDR ASOA2014103011588](https://openairdocs.org/sdr/ASOA2014103011588.md): Isolator · cracked · Oct 26, 2014 · N844AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD, ISOLATORS ARE CRACKED. REMOVED AND REPLACED WITH NEW IAW SRM 51-42-06.
- [SDR ASOA2014103011587](https://openairdocs.org/sdr/ASOA2014103011587.md): Light · inoperative · Oct 25, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > LT EMERGENCY EXIT MARKER LIGHTS ON WALL JUST FWD OF DOOR IS INOPERATIVE. REMOVED LT EMERGENCY EXIT MARKER IAW AMM 33-51-10-000-801. INSTALLED SERVICEABLE EMERGENCY EXIT MARKER IAW 33-51-10-400-801, PN 6020-6. OPS TEST ID GOOD.
- [SDR ASOA2014082511135](https://openairdocs.org/sdr/ASOA2014082511135.md): Light · intermittent · Aug 22, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS CHECK OF SIDEWALL EMERGENCY LIGHT IAW AMM 33-51-01.
- [SDR ASOA2014082511134](https://openairdocs.org/sdr/ASOA2014082511134.md): Light · intermittent · Aug 19, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > ONE EMERGENCY LIGHT INOPERATIVE. CABIN EMERGENCY LIGHTS ILLUMINATED. PERFORMED OPS CHECK OF SIDEWALL EMERGENCY LIGHT IAW AMM 33-51-01 DEFER CLEARED PLACARD REMOVED.
- [SDR ASOA2014061010658](https://openairdocs.org/sdr/ASOA2014061010658.md): Lamp · burned out · Jun 6, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > CEILING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.
- [SDR ASOA2014052910603](https://openairdocs.org/sdr/ASOA2014052910603.md): Sign · inoperative · May 23, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT MARKER INOPERATIVE. R & R LT OVERWING EMERGENCY EXIT MARKER IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR ASOA2014040810304](https://openairdocs.org/sdr/ASOA2014040810304.md): Light · inoperative · Apr 5, 2014 · N844AS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY EXIT LIGHT AT SEAT 8A INOPERATIVE. PERFORMED OPS TEST OF THE EMERGENCY EXIT LIGHT AT SEAT 8A IAW AMM 33-51-00. NO DEFECTS NOTED AT THIS TIME.
- [SDR ASOA2014020509907](https://openairdocs.org/sdr/ASOA2014020509907.md): Trunnion · damaged · Jan 17, 2014 · N844AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > ONE HOLE AT LT FWD SIDE OF MLG TRUNNION STRAP NO GO SIDE OF COMBINATION GAGE GOES IN HOLE. REPAIRED IAW REO 601R-57-21-2087, REV P1. MAJOR REPAIR.
- [SDR ASOA2014020509906](https://openairdocs.org/sdr/ASOA2014020509906.md): Trunnion · damaged · Jan 17, 2014 · N844AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > ONE HOLE AT RT FWD SIDE OF MLG TRUNNION STRAP NO GO SIDE OF COMBINATION GAGE GOES IN HOLE. REPAIRED IAW REO 601R-57-21-2087, REV P1. MAJOR REPAIR.
- [SDR ASOA2014020509905](https://openairdocs.org/sdr/ASOA2014020509905.md): Skin · corroded · Jan 16, 2014 · N844AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER PLANK ACCESS HOLE FUEL PANEL 640BB HAS CORROSION. REPAIRED IAW REO 601R-57-21-030. MAJOR REPAIR.
- [SDR ASOA2014020509904](https://openairdocs.org/sdr/ASOA2014020509904.md): Skin · corroded · Jan 16, 2014 · N844AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING LOWER PLANK ACCESS HOLE FUEL PANEL 540BB HAS CORROSION. COMPLIED WITH REO 601R-57-21-030. MAJOR REPAIR.
- [SDR ASOA2014020509903](https://openairdocs.org/sdr/ASOA2014020509903.md): Bulkhead · cracked · Jan 14, 2014 · N844AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED IN 2 PLACED AT RBL 27.50 BETWEEN WL 73.50 AND WL 120.43 AREAS ARE MARKED. COMPLIED WITH REO 601R-53-61-1285, REV D. MAJOR REPAIR.
- [SDR ASOA2014020509902](https://openairdocs.org/sdr/ASOA2014020509902.md): Seat Track · corroded · Jan 13, 2014 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 CORRODED AFT OF BS 559+32. R & R SEAT TRACK IAW REO 601R-53-00-485.
- [SDR ASOA2014020509901](https://openairdocs.org/sdr/ASOA2014020509901.md): Seat Track · corroded · Jan 13, 2014 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 559+16 - FS 559+32. REMOVED AND INSTALLED NEW SEAT TRACK BS 495.98 - 535.02, IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014020509900](https://openairdocs.org/sdr/ASOA2014020509900.md): Seat Track · corroded · Jan 13, 2014 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK HAS CORROSION BETWEEN BS 529-544. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014020509899](https://openairdocs.org/sdr/ASOA2014020509899.md): Seat Track · corroded · Jan 13, 2014 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 BETWEEN FS 394 - 409+128 HAS NUMEROUS PLACES OF CORROSION. R & R SEAT TRACK IAW REO 601R-53-00-485 STEPS 1-3.
- [SDR ASOA2014020509898](https://openairdocs.org/sdr/ASOA2014020509898.md): Seat Track · corroded · Jan 13, 2014 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BETWEEN BS 394-409+128 HAS NUMEROUS PLACES OF CORROSION. R & R SEAT TRACK IAW REO 601R-53-00-485 UP TO STEP 6

Next page: https://openairdocs.org/deregistered/N844AS-2018-07-30/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 = 'N844AS' AND deregistration_id = 'N844AS-2018-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N844AS-2018-07-30/reports

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