# Service difficulty reports: N825AS, cancelled Mar 29, 2016

A list on [N825AS, cancelled Mar 29, 2016](https://openairdocs.org/deregistered/N825AS-2016-03-29.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 · 154 reports

- [SDR ASOA2014090211175](https://openairdocs.org/sdr/ASOA2014090211175.md): Door · lack of lube · Aug 29, 2014 · N825AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WOULD NOT OPEN. LUBED PASSENGER DOOR AND OPS CHECK IAW AMM 52-11-00.
- [SDR ASOA2014030610089](https://openairdocs.org/sdr/ASOA2014030610089.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS PANEL HOLE 640EB HAS MULITPLE INDICATIONS ON THE AFT, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. REMOVED PANEL 640EB FOR INSPECTION IAW AMM 28-11-01-000-802. INSTALLED ACCESS PANEL 640EB IAW AMM 28-11-01-400-802. COMPLIED WITH EC/TC EO 60
- [SDR ASOA2014030610088](https://openairdocs.org/sdr/ASOA2014030610088.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT FUEL ACCESS PANEL HOLE 540EB HAS MULTIPLE INDICATIONS ON INBD, OTBD, FWD & AFT SIDES 60 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014030610087](https://openairdocs.org/sdr/ASOA2014030610087.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL ACCESS PANEL HOLE 650AB HAS MULTIPLE INDICATIONS ON THE FWD, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.
- [SDR ASOA2014030610086](https://openairdocs.org/sdr/ASOA2014030610086.md): Access Panel · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL ACCESS PANEL 640AB HAS MULTIPLE INDICATIONS ON THE AFT SIDE 80 PERCENT FCH. FAILED NDT. REMOVED PANEL 640AB FOR INSPECTION IAW AMM 25-11-01-000-802. INSTALLED PANEL 640AB IAW AMM 28-11-01-400-802.
- [SDR ASOA2014030610085](https://openairdocs.org/sdr/ASOA2014030610085.md): Skin · corroded · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL ACCESS PANEL HOLE 610AB HAS MULTIPLE INDICATIONS ON INBD 7 FWD SIDE 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014030610084](https://openairdocs.org/sdr/ASOA2014030610084.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT FUEL ACCESS PANEL HOLE 650CB HAS MULTIPLE INDICATIONS, GROUND THE ENTIRE CIRCUMFERENCE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81.
- [SDR ASOA2014030610083](https://openairdocs.org/sdr/ASOA2014030610083.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT FUEL ACCESS PANEL HOLE 550CB HAS MULTIPLE INDICATIONS ON INBD 78 FWD SIDE 5 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81.
- [SDR ASOA2014030610082](https://openairdocs.org/sdr/ASOA2014030610082.md): Skin · cracked · Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT FUEL ACCESS PANEL HOLE 650DB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014030610081](https://openairdocs.org/sdr/ASOA2014030610081.md): Strap · corroded · Feb 19, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR CUTOUT AT FS 349 BETWEEN STRINGERS 3-4L, THE UPPER INNER FRAME STRAP IS CORRODED. FABBED FRAME STRAP IAW EO DWG SNIEO 600-31153 FROM 7075-T6 PO 74097/1. C/W EO 600-31153 SNIEO S01. REMOVED FRAME STRAP AND REPLACED WITH NEW FRAME STRAP, PN 6
- [SDR ASOA2014030610080](https://openairdocs.org/sdr/ASOA2014030610080.md): Skin · cracked · Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING ACCESS PANEL HOLE 640CB HAS MULTIPLE INDICATIONS ON THE RT SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.
- [SDR ASOA2014030610079](https://openairdocs.org/sdr/ASOA2014030610079.md): Skin · cracked · Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL HOLE 640FB HAS MULTIPLE INDICATIONS ON THE INBD SIDE 60 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO600-57-81. C/W IAW REO:601R-57-21-030.
- [SDR ASOA2014030610078](https://openairdocs.org/sdr/ASOA2014030610078.md): Skin · cracked · Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING ACCESS PANEL HOLE 540FB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.
- [SDR ASOA2014030610077](https://openairdocs.org/sdr/ASOA2014030610077.md): Angle · cracked · Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27, BS 484 INBD ANGLE IS CRACKED. R & R IAW SRM 51-42-21 AND SRM 51-42-06.
- [SDR ASOA2014030610076](https://openairdocs.org/sdr/ASOA2014030610076.md): Angle · cracked · Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 27, BS 484 ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2014030510071](https://openairdocs.org/sdr/ASOA2014030510071.md): Angle · cracked · Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 36, BS 484.00, ANGLE CRACKED. R & R ANGLE IAW REO 601R-53-41-059 AND REO 601R-53-41-059, REV B.
- [SDR ASOA2014030510070](https://openairdocs.org/sdr/ASOA2014030510070.md): Skin · cracked · Feb 14, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZ LANDING, 50 PERCENT FSH FAILED NDT. COMPLIED WITH REO: 601R-57-21-2124.
- [SDR ASOA2014030510069](https://openairdocs.org/sdr/ASOA2014030510069.md): Floor Panel · corroded · Feb 12, 2014 · N825AS · Cndair CL6002B19 · Fuselage Floor Panel
  > TWO AREAS ON LT FLOOR PANEL ARE BEYOND MAXIMUM BLEND DEPTH LIMITS OF REO 601R-53-41-666, SUBSECTION 1.1 AND TABLE 1, REV.C 2012-11-06. C/W REO 601R-53-41-1777 FOR REPAIR OF DAMAGE TO LT PRESSURE FLOOR PANEL
- [SDR ASOA2014030510068](https://openairdocs.org/sdr/ASOA2014030510068.md): Post · cracked · Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX.300" LONG 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED, DRILLED, LOCATED AND REPLACED FS 409+128, RBL 18, POST ASSY IAW SRM 51-42-06, 51-42-22, REO 601R-
- [SDR ASOA2014030510067](https://openairdocs.org/sdr/ASOA2014030510067.md): Isolator · cracked · Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD ISOLATORS CRACKED AT LBL 27.50 AND LBL 9.50, WL 98. REMOVED UNSERVICEABLE ISOLATOR MOUNTS IAW SRM 51-42-13. INSTALLED 2 EA NEW ISOLATORS PN SL2337-3 IAW SRM 51-42-13.
- [SDR ASOA2014030510066](https://openairdocs.org/sdr/ASOA2014030510066.md): Angle · cracked · Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SUPPORT BEAM LOWER AFT ANGLE CRACKED APPROX 0.3" WIDE. R & R ANGLE ON CARGO DOOR SUPPORT BEAM IAW SRM 51-42-21.
- [SDR ASOA2014030510065](https://openairdocs.org/sdr/ASOA2014030510065.md): Bulkhead · cracked · Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 0, WL 91-48 APPROX 7 INCHES, AREA 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06. COMPLIED WITH REO:601R-53-61-1285, REV D.
- [SDR ASOA2014030510064](https://openairdocs.org/sdr/ASOA2014030510064.md): Bulkhead · cracked · Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 79.0 APPROX.6 INCHES IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-5186, REV.
- [SDR ASOA2014030510063](https://openairdocs.org/sdr/ASOA2014030510063.md): Stringer · cracked · Feb 10, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED APPROX 0.70" LONG AT BS 280.8. REPAIRED IAW SRM 51-42-06. REPAIRED IAW SNIEO 601R-31522.
- [SDR ASOA2014030510062](https://openairdocs.org/sdr/ASOA2014030510062.md): Finger Doubler · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FINGER DOUBLERS CORRODED IN MULTIPLE AREAS FS 409+128 - 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C. REPAIRED IAW REO 601R-53-5186, REV.
- [SDR ASOA2014030510061](https://openairdocs.org/sdr/ASOA2014030510061.md): Skin · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN & FINGER DOUBLERS HAVE CORROSION IN MULTIPLE AREAS BS 409+128-559. COMPLIED WITH EC/TC REO 601R-53-41-66601 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2014030510060](https://openairdocs.org/sdr/ASOA2014030510060.md): Cargo Track · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK RBL 9 BS 559+80-574 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AMM 53-01-11-400-802 AND REO 601R-53-00-485, REV.
- [SDR ASOA2014030510059](https://openairdocs.org/sdr/ASOA2014030510059.md): Cargo Track · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK LBL 9, BS 559+80-621 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802 AND REO NR 601R-53-00-485, REV.
- [SDR ASOA2014030510058](https://openairdocs.org/sdr/ASOA2014030510058.md): Floor Support · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL 27, BS 574-621 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-21, 51-42-20 & 51-42-06. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A.
- [SDR ASOA2014030510057](https://openairdocs.org/sdr/ASOA2014030510057.md): Floor Support · corroded · Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT RBL 45 IS CORRODED FROM BS 559+80 - 574. REPAIRED IAW SRM 51-42-06 & 51-42-21 AND IAW REO 601R-53-00-526.
- [SDR ASOA2013121309645](https://openairdocs.org/sdr/ASOA2013121309645.md): Light · missing · Dec 10, 2013 · N825AS · Cndair CL6002B19 · Emergency Lighting
  > SHORT PORTION OF EMERGENCY LIGHT AT 18B MISSING. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.
- [SDR ASOA201201095](https://openairdocs.org/sdr/ASOA201201095.md): Connector · loose · Mar 29, 2012 · N825AS · Cndair CL6002B19 · Engine Oil System Wiring
  > CLIMBING THROUGH FL 220, RECEIVED RT ENGINE OIL PRESSURE WARNING WITH OIL PRESSURE AT 15 PSI. OIL TEMPERATURE WAS NORMAL OIL PRESS READ NORMAL AFTER DESCENT. (ACFT RETURNED TO CAE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND RT ENGINE OIL TEMPERAT
- [SDR ASOA201201078](https://openairdocs.org/sdr/ASOA201201078.md): Scavenge Pump · failed · Mar 29, 2012 · N825AS · Cndair CL6002B19 · Turbine Engine Oil System
  > RIGHT ENGINE OIL PRESSURE MASTER CAUTION AT 18000 FT. EMERGENCY DECLARED. R & R RT LUBE AND SCAVENGE PUMP IAW AMM 79-21-01. LEAK AND OPS CHECKED GOOD.
- [SDR ASOA201200502](https://openairdocs.org/sdr/ASOA201200502.md): Floor Support · corroded · Feb 15, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW AMM 20-21-00-910-001 AND 20-24-00-910-802.
- [SDR ASOA201200436](https://openairdocs.org/sdr/ASOA201200436.md): Angle · cracked · Feb 8, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NLG CUTOUT CORNERS CRACKED AFT OF FOLLOW -UP DOOR HINGES (RADIUS). REPAIRED IAW REO 601R-53-11-0048 IAW 601R-53-11-0048, REV C.
- [SDR ASOA201200546](https://openairdocs.org/sdr/ASOA201200546.md): Angle · corroded · Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FWD UPPER ANGLE CORRODED. R & R CORRODED ANGLE IAW DWG NR 601R38303.
- [SDR ASOA201200412](https://openairdocs.org/sdr/ASOA201200412.md): Seat Track · corroded · Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FS 394 TO 409+128 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA201200410](https://openairdocs.org/sdr/ASOA201200410.md): Seat Track · corroded · Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FS 409+128 TO 559.0 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 51-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-807 AND AMM 53-01-11-400-802.
- [SDR ASOA201200408](https://openairdocs.org/sdr/ASOA201200408.md): Attach Angle · cracked · Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE CRACKED AFT EQUIPMENT BAY RT SIDE AT PRESSURE BULKHEAD ABOUT 12 INCHES BELOW ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.
- [SDR ASOA201200406](https://openairdocs.org/sdr/ASOA201200406.md): Attach Angle · cracked · Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH FITTING CRACKED AFT EQUIPMENT BAY LT SIDE AT PRESSURE BULKHEAD ABOVE ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. LOCATED SERVICEABLE ATTACH ANGLE IAW STM 51-40-11. INSTALLED ATTACH ANGLE IAW SRM 57-42-22.
- [SDR ASOA201200398](https://openairdocs.org/sdr/ASOA201200398.md): Seat Track · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FS 364 TO 396 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM TASK 53-01-11-400-802.
- [SDR ASOA201200396](https://openairdocs.org/sdr/ASOA201200396.md): Seat Track · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FS 364-396 AT LBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-420-001.
- [SDR ASOA201200394](https://openairdocs.org/sdr/ASOA201200394.md): Support Angle · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-26-00..031" OF MATERIAL REMOVED-.026" MATERIAL REMAINING. REMOVED SILL SUPPORT ANGLE IAW SRM'S 51-42-06, 51-42-21, AND 51-42-13. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND 51-42-
- [SDR ASOA201200392](https://openairdocs.org/sdr/ASOA201200392.md): Floorbeam · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FS 280 HAS CORROSION DAMAGE. REMOVED CORROSION IAW SRM 51-21-06. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06. DRILLED NEW ANGLE IAW SRM 51-40-11.
- [SDR ASOA201200390](https://openairdocs.org/sdr/ASOA201200390.md): Floorbeam · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND NUTPLATE ON FS 280.00 FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PRODCEDURES UT-3. MIN MATERIAL REMAINING IS.035".
- [SDR ASOA201200388](https://openairdocs.org/sdr/ASOA201200388.md): Seat Track · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SHORT SEAT TRACK BETWEEN FLOOR PANELS 281BLF AND 281FRF HAS CORROSION. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA201200386](https://openairdocs.org/sdr/ASOA201200386.md): Seat Track · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SHORT SEAT TRACK HAS CORROSION AT LBL9 BETWEEN FLOOR PANEL 281HLF AND 281BLF. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-40-802.
- [SDR ASOA201200384](https://openairdocs.org/sdr/ASOA201200384.md): Seat Track · corroded · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AT RBL 9 AT 9G BULKHEAD. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA201200382](https://openairdocs.org/sdr/ASOA201200382.md): Attach Fitting · cracked · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT RBL 27.0. REMOVED DAMAGED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM AND DWG NR 601R31171.
- [SDR ASOA201200380](https://openairdocs.org/sdr/ASOA201200380.md): Attach Fitting · cracked · Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT LBL 27.0. REMOVED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21.

Next page: https://openairdocs.org/deregistered/N825AS-2016-03-29/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 = 'N825AS' AND deregistration_id = 'N825AS-2016-03-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N825AS-2016-03-29/reports

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