# Service difficulty reports: N848AS, cancelled Jul 30, 2018

A list on [N848AS, cancelled Jul 30, 2018](https://openairdocs.org/deregistered/N848AS-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 3 · 128 reports

- [SDR ASOA20160905001](https://openairdocs.org/sdr/ASOA20160905001.md): Bolt · broken · Sep 5, 2016 · N848AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CABIN WILL NOT RAISE. MX REPLACED BROKEN EYEBOLT AND OPS CHECKED PAX DOOR IAW 52-11-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2016071315087](https://openairdocs.org/sdr/ASOA2016071315087.md): Battery Pack · discharged · Jul 13, 2016 · N848AS · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERIES.
- [SDR ASOA2016071315086](https://openairdocs.org/sdr/ASOA2016071315086.md): Flashlight · inoperative · Jul 13, 2016 · N848AS · Cndair CL6002B19 · Emergency Equipment
  > F/O FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-61-04.
- [SDR ASOA2015060513054](https://openairdocs.org/sdr/ASOA2015060513054.md): Light · unserviceable · Jun 4, 2015 · N848AS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY LIGHT IN GALLEY UNSERVICEABLE. R & R GALLEY EMERGENCY LIGHT IAW AMM 33-51-10.
- [SDR ASOA2015020612167](https://openairdocs.org/sdr/ASOA2015020612167.md): Battery · disconnected · Feb 5, 2015 · N848AS · Cndair CL6002B19 · Emergency Lighting
  > NR 3 AND 4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND NR 2 EMERGENCY BATTERY PACK NOT INSTALLED IN CHARGER UNIT. INSTALLED BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.
- [SDR ASOA2015012212071](https://openairdocs.org/sdr/ASOA2015012212071.md): Connector · broken · Jan 19, 2015 · N848AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY EXIT INOPERATIVE ON SIDE PANEL OF GALLEY NR 1. REPLACED BROKEN CONNECTOR J122LY BY REMOVING IT AND INSTALLING A NEW ONE IAW ESPM 20-17-31. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, OPS TEST GOOD.
- [SDR ASOA2015012212070](https://openairdocs.org/sdr/ASOA2015012212070.md): Seat Track · corroded · Jan 18, 2015 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED OUT OF LIMITS IAW SRM 53-31-49 AND SRM 53-21-49. FABRICATED & INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.
- [SDR ASOA2015012212069](https://openairdocs.org/sdr/ASOA2015012212069.md): Attach Bracket · cracked · Dec 20, 2014 · N848AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR LINTEL AFT BRACKET ATTACHED TO PRESSURE BULKHEAD CRACKED, REMOVED THE BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-11, SRM 51-42-21.
- [SDR ASOA2014122911997](https://openairdocs.org/sdr/ASOA2014122911997.md): Seat Track · corroded · Dec 20, 2014 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRAC AT RBL9 BS 559-559+80 CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802, AND SRM 51-40-11.
- [SDR ASOA2014122911996](https://openairdocs.org/sdr/ASOA2014122911996.md): Isolator · broken · Dec 20, 2014 · N848AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 5 BROKEN ISOLATORS FOUND ON THE AFT PRESSURE BULKHEAD FWD FACE. REPLACED 5 BROKEN ISOLATORS ON AFT PRESSURE BULKHEAD FWD FACE IAW SRM 51-42-13.
- [SDR ASOA2014122911995](https://openairdocs.org/sdr/ASOA2014122911995.md): Frame · corroded · Dec 19, 2014 · N848AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION AROUND 2 NUTPLATES UNDER FLOORBOARD 251ALF ON RBL9 AND AT FS 409+16 AND FS 409+32. REMOVED CORROSION IAW SRM 51-21-06. REMOVED.023 MATERIAL THICKINESS.063" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. C/W REO 601R-53-21-064.
- [SDR ASOA2014080110987](https://openairdocs.org/sdr/ASOA2014080110987.md): Lens · missing · Jul 31, 2014 · N848AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT SIGN COVER MISSING BETWEEN GALLEY SERVICE DOOR AND SNACK BINS. REINSTALLED EMERGENCY LIGHT COVER IAW AMM 33-51-13.
- [SDR ASOA2013011502802](https://openairdocs.org/sdr/ASOA2013011502802.md): Wire · disconnected · Jan 10, 2013 · N848AS · Cndair CL6002B19 · Light System Wiring
  > AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AFT CEILING EMERGENCY LIGHT, FOUND WIRES TO BE DISCONNECTED. CONNECTED WIRES AND REINSTALLED LIGHT. OPS CHECKED GOOD, WORK DONE IAW MM 33-51-16-000-801 AND 33-51-16-400-801.
- [SDR ASOA2013011502801](https://openairdocs.org/sdr/ASOA2013011502801.md): Fitting · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR FITTING IS GOUGED AND CORRODED. REMOVED SERVICE DOOR FITTING BETWEEN FS 319 AND 349 IAW SRM 51-41-02. LOCATED AND DRILLED NEW SERVICE DOOR FITTING, IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SERVICE DOOR FITTING IAW AMM 20-21-00-910-801.
- [SDR ASOA2013011502800](https://openairdocs.org/sdr/ASOA2013011502800.md): Floorbeam · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOORBEAM STRUCTURE MOUNT IS CORRODED AT FS 310. REMOVED FLOORBEAM SUPPORT MOUNT IAW SRM 51-42-21. LOCATED & INSTALLED FLOORBEAM JOINT ANGLE IAW SRM 51-40-11 & 51-42-21, PN 601R38335-1.
- [SDR ASOA2013011502799](https://openairdocs.org/sdr/ASOA2013011502799.md): Floorbeam · cracked · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM CRACKED AND CORRODED. REMOVED DAMAGED AND REPAIRED IAW SRM CH 51-42-06, 51-42-10 & 51-42-21, & REO 601R-53-11-926.
- [SDR ASOA2013011502798](https://openairdocs.org/sdr/ASOA2013011502798.md): Floor Support · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FS 280.00 FLOOR SUPPORT. REMOVED DAMAGED FWD FLOOR SUPPORT IAW SRM CH 51-42-06 & 51-42-21. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT, IAW SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06.
- [SDR ASOA2013011502797](https://openairdocs.org/sdr/ASOA2013011502797.md): Sill · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR LOWER SILL. REMOVED SILL ANGLE (LOWER) IAW SRM 51-42-21 & 51-42-06. LOWER SILL ANGLE FOUND TO HAVE CORROSION EXCEEDING LIMITS IAW SRM 53-00-00-01, T/R-53-27. LOCATED & DRILLED NEW LOWER SILL ANGLE, IAW SRM 51-40-11-00. INSTALLED NEW
- [SDR ASOA2013011502796](https://openairdocs.org/sdr/ASOA2013011502796.md): Sill · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR LOWER SILL FWD AND AFT CUPS. REPAIRED IAW SRM CH 51-42-06 & 51-42-11.
- [SDR ASOA2013011502795](https://openairdocs.org/sdr/ASOA2013011502795.md): Beam · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON PAX DOOR AFT FRAME LOWER TRANSVERSE BEAM AT FS 349.00. REPAIRED IAW REO 601R-53-21-2392. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
- [SDR ASOA2013011502794](https://openairdocs.org/sdr/ASOA2013011502794.md): Frame · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 349 BETWEEN STR 26L AND 26R. REMOVED LOWER FRAME SECTION FS 349 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE LWR FRAME SECTION AT FS 349 AND INSTALLED FRAME IAW SRM 51-40-21, 51-42-06, 51-42-21.
- [SDR ASOA2013011502793](https://openairdocs.org/sdr/ASOA2013011502793.md): Frame · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 314.7 BETWEEN STR 26L AND STR 26R. REMOVED LOWER SECTION OF FRAME AT FS 319.00, STR 24L-24R IAW SRM 51-42-06 & 51-42-21. LOCATED & DRILLED HOLES COMMONT TO SKIN AND SPLICE & NEW SERVICEABLE FRAME SECTOR PN 601R32003-61 IAW SRM 51-40-
- [SDR ASOA2013011502792](https://openairdocs.org/sdr/ASOA2013011502792.md): Frame · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 310.00 BETWEEN S26L AND 26R. REPAIRED IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013011502791](https://openairdocs.org/sdr/ASOA2013011502791.md): Floor Support · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SUPPORT FWD OF SERVICE DOOR FROM FS 319.70 TO FS 310.00 AND AFT OF DOOR FROM FS 349.00 TO 364.00. REPAIRED IAW SRM 51-42-06, SRM 53-00-00 AND IAW REO 601R-53-21-2385.
- [SDR ASOA2013011502790](https://openairdocs.org/sdr/ASOA2013011502790.md): Beam · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON THE END OF THE TRANSVERSE BEAM FS 349.00, RBL 36 AT SERVICE DOOR AFT FRAME. COMPLIED WITH STEP 1 OF REO 601R-53-21-2391, REV P1 CUT AWAY DAMAGE.
- [SDR ASOA2013011502789](https://openairdocs.org/sdr/ASOA2013011502789.md): Sill · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR SILL FROM FS 319.70 TO FS 349.00. REMOVED SILL IAW SRM 51-42-06 AND SRM 51-42-21 AND SRM 51-42-10. DRILLED, LOCATED AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-21 AND 51-42-10.
- [SDR ASOA2013011402788](https://openairdocs.org/sdr/ASOA2013011402788.md): Sill · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL IS CORRODED AROUND ALL NUTPLATES. REMOVED CARGO DOOR SILL IAW SRM 51-42-06, 51-42-21 & 51-42-10. INSTALLED NEW SERVICEABLE SILL IAW REO 601R-53-61-1574, REV A.
- [SDR ASOA2013011402787](https://openairdocs.org/sdr/ASOA2013011402787.md): Floor Support · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SUPPORT IS CORRODED INBD OF EMERGENCY EXIT. REPAIRED IAW REO 601R-53-41-666, REV C.
- [SDR ASOA2013011402786](https://openairdocs.org/sdr/ASOA2013011402786.md): Stringer · corroded · Dec 19, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > AFT EQUIPMENT COMPARTMENT STRINGER 19R IS CORRODED BETWEEN FS 654.5 AND 672.2. STRINGER DAMAGED BEYOND REPAIR, REMOVED STRINGER IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW STRINGER IAW SRM 51-42-06.
- [SDR ASOA2013011402785](https://openairdocs.org/sdr/ASOA2013011402785.md): Post · cracked · Dec 17, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERTICAL POST LBL 18 INBOARD AFT UPPER RADIUS FAILED NDT WITH INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX.2 LONG. REMOVED INBD & OTBD VERTICAL POST AT LBL 18 FS 409+128 IAW SRM 51-42-22. LOCATED AND DRILLED NEW VERTICAL POST AT LBL 18
- [SDR ASOA2013011402784](https://openairdocs.org/sdr/ASOA2013011402784.md): Floorbeam · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLES AT FS 484.00, LBL 27 AND LBL 36 ARE CRACKED. FABRICATED AND INSTALLED NEW ANGLES IAW REO 601R-53-41-059.
- [SDR ASOA2013011402783](https://openairdocs.org/sdr/ASOA2013011402783.md): Floorbeam · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 484.00, RBL 27 AND RBL 36 CRACKED. FABRICATED AND INSTALLED FLOORBEAM ANGLE IAW REO 601R-53-41-059.
- [SDR ASOA2013011402782](https://openairdocs.org/sdr/ASOA2013011402782.md): Angle · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD AND OTBD ANGLES AT FS 280.00, RBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926.
- [SDR ASOA2013011402781](https://openairdocs.org/sdr/ASOA2013011402781.md): Angle · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD AND OTBD ANGLES AT FS 280.00 LBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926.
- [SDR ASOA2013011402780](https://openairdocs.org/sdr/ASOA2013011402780.md): Support Bracket · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WINDSHIELD LOWER SIDE POST SUPPORT BRACKET IS CRACKED, APPROX.500" LONG. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21.
- [SDR ASOA2013011402779](https://openairdocs.org/sdr/ASOA2013011402779.md): Connector · broken · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Light System Wiring
  > BROKEN QUICK DISCONNECT FOR EMERGENCY LIGHTS IN WARDROBE. INSTALLED QUICK DISC SPLICES FOR WARDROBE EMERGENCY LIGHT IAW ESPM 20-17-10 ON ACFT SIDE. OPS CHECKED, EMERGENCY LIGHTS REO 33-51-00-710-801.
- [SDR ASOA2013011102778](https://openairdocs.org/sdr/ASOA2013011102778.md): Bulkhead · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON RBL 27.50, WL 83-93 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-1285.
- [SDR ASOA2013011102777](https://openairdocs.org/sdr/ASOA2013011102777.md): Bulkhead · cracked · Dec 11, 2012 · N848AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621, BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON LBL 36.20, WL 80 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-4747.
- [SDR ASOA201200065](https://openairdocs.org/sdr/ASOA201200065.md): Pdu · failed · Jan 6, 2012 · N848AS · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER UNLOCKED MESSAGE DURING CLIMB, EMERGENCY DECLARED. PERFORMED CHECKLIST AND COMPLIED WITH QRH PROCEDURE. AIR RETURN TO DEPARTURE. R & R LT ENGINE PDU IAW AMM 78-32-03 AND 78-32-03, ITEM 5A. OPS CHECKED GOOD.
- [SDR ASOA201102315](https://openairdocs.org/sdr/ASOA201102315.md): Flashlight · inoperative · Dec 4, 2011 · N848AS · Cndair CL6002B19 · Emergency Equipment
  > F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.
- [SDR ASOA201100468](https://openairdocs.org/sdr/ASOA201100468.md): Battery · inoperative · Mar 11, 2011 · N848AS · Cndair CL6002B19 · Emergency Equipment
  > CA'S FLASHLIGHT INOP. REPLACED BATTERIES, CAPT FLASHLIGHT IAW AMM 25-60-00. OPS CHECK GOOD.
- [SDR ASOA201001943](https://openairdocs.org/sdr/ASOA201001943.md): Floorbeam · corroded · Dec 14, 2010 · N848AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND SEVERAL SCREW HOLES UNDER FLOORBOARD 251ALF AND ON FLOORBEAMS. BLENDED AREA AT RBL9 BETWEEN FS 409.00+48 AND FS 409.00+64 HAS A REMAINING THICKNESS OF.025 WITH MATERIAL THICKNESS IS.050 AND IS OUT OF ALLOWABLE LIMITS. IAW SRM 53-00-00, FIG
- [SDR ASOA201001905](https://openairdocs.org/sdr/ASOA201001905.md): Attach Fitting · cracked · Dec 9, 2010 · N848AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON RT SIDE. CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON RT SIDE RT.
- [SDR ASOA201001904](https://openairdocs.org/sdr/ASOA201001904.md): Attach Fitting · cracked · Dec 9, 2010 · N848AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON LT SIDE. CLIP CRACKED ON REAR BULKHEAD AFT FACE WAS FOUND TO BE AT FS 625 LT SIDE. R & R IAW SRM 51-40-11 AND 51-42-20 APPLIED SEALANT AND FINISH COAT IAW 51-25-00 AND 51-23-00.
- [SDR ASOA201002015](https://openairdocs.org/sdr/ASOA201002015.md): Seat Track · corroded · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT POSITION 3A (SIDE RAIL). REMOVED MINOR CORROSION ON LT SIDE SEAT RAIL AT SEAT POSITION 3A IAW SRM 51-21-06. MATERIAL REMOVAL FROM SIDE SEAT RAIL AT SEAT POSTION 3A WAS.006" AND.369". DAMAGE OUT OF LIMITS, BL
- [SDR ASOA201002003](https://openairdocs.org/sdr/ASOA201002003.md): Seat Track · corroded · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT LOCATION 12CD. REMOVED MINOR CORROSION ON RT SIDE SEAT RAIL. REMOVED.008" MATERIAL AT LOCATION 12CD. IAW SRM 51-21-06. CONTACT MFG FOR DAMAGE LIMITATIONS AND REPAIR PROCEDURE. REPLACE SEAT IAW STEP 3. REMOVE
- [SDR ASOA201001911](https://openairdocs.org/sdr/ASOA201001911.md): Nut Plate · broken · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT CARGO AFT PRESSURE BULKHEAD HAS NUTPLATE BROKEN AT CTR ROW, 2ND ROW UP FROM FLOOR (ISOLATOR). REMOVED BROKEN ISOLATOR MOUNT ON AFT PRESS BULKHEAD & INSTALLED NEW ISOLATOR MOUNT IAW SRM 51-42-13 THIS IS A MINOR REPAIR.
- [SDR ASOA201001892](https://openairdocs.org/sdr/ASOA201001892.md): Seat Track · corroded · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 9L SEAT TRACK SEGMENT FROM FS 559 + 32 TO 559 + 80 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS.5" WIDE X.5" LENGTH X.024" DEEP. OUT OF LIMITS IAW SRM 53-21-49. REMOVED 9L SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802.
- [SDR ASOA201001891](https://openairdocs.org/sdr/ASOA201001891.md): Seat Track · corroded · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 9R SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS.5" WIDE X.5" LONG X.022" DEEP. OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK SEGMENT IAW AMM 5.-01-11-000-802. FABRICATED SEAT
- [SDR ASOA201001890](https://openairdocs.org/sdr/ASOA201001890.md): Seat Track · corroded · Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 9L SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM LT PASSENGER SEAT TRACK. BLEND DIMENSION.5" LONG X.5" WIDE X.025" DEEP OUT OF LIMITS IAW SRM 53-41-29. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED S

Next page: https://openairdocs.org/deregistered/N848AS-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 = 'N848AS' AND deregistration_id = 'N848AS-2018-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N848AS-2018-07-30/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.