# Service difficulty reports: N14839, cancelled Jul 16, 2008

A list on [N14839, cancelled Jul 16, 2008](https://openairdocs.org/deregistered/N14839-2008-07-16.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 2 · 74 reports

- [SDR CALA0300499](https://openairdocs.org/sdr/CALA0300499.md): Strut · low · Aug 26, 2003 · N14839 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM LAS. RECYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SHOCK STRUT INFLATION LOW. THE SHOCK STRUT WAS SERVICED IAW MM 32-31-02.
- [SDR CALA0200581](https://openairdocs.org/sdr/CALA0200581.md): Battery Pack · inoperative · Dec 11, 2002 · N14839 · Doug DC982 · Emergency Lighting
  > THE TAILCONE SLIDE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0200389](https://openairdocs.org/sdr/CALA0200389.md): Latch · out of rig · Jul 2, 2002 · N14839 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE INTERIOR RELEASE HANDLE PULL WAS EXCESSIVE. THE TAILCONE LATCH LOCKPINS WERE ADJUSTED AND OPERATION CHECKED GOOD IAW MM 53-53-00.
- [SDR CALA0200369](https://openairdocs.org/sdr/CALA0200369.md): Longeron · cracked · Jun 28, 2002 · N14839 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/4" CRACK IN LONGERON 2L AT BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18.
- [SDR CALA0000143](https://openairdocs.org/sdr/CALA0000143.md): Panel · cracked · Feb 8, 2000 · N14839 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN RT WING TRANSVERSE PANEL. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
- [SDR CALA0000142](https://openairdocs.org/sdr/CALA0000142.md): Cargo Track · corroded · Feb 8, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO RT TIEDOWN TRACK CORRODED AT FS 1003-1155. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-03, 51-30-01, AND 51-30-02.
- [SDR CALA0000140](https://openairdocs.org/sdr/CALA0000140.md): Cargo Track · corroded · Feb 7, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MID AND AFT CARGO LT TIE DOWN TRACKS CORRODED AT FS 636-736 AND FS 1003-1212, LBL 24. THE CORRODED SECTIONS OF TRACK WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-1, AND 51-30-5.
- [SDR CALA0000138](https://openairdocs.org/sdr/CALA0000138.md): Door Pan · gouged · Feb 5, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR AFT STOP POSITIONS ON FRAME GOUGED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA5230-01519.
- [SDR CALA0000137](https://openairdocs.org/sdr/CALA0000137.md): Web · corroded · Feb 5, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR WEB CORRODED AT SUPPORTS BETWEEN FS 1136 AND 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.
- [SDR CALA0000135](https://openairdocs.org/sdr/CALA0000135.md): Floorbeam · corroded · Feb 4, 2000 · N14839 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO FLOOR PANEL SUPPORT CORRODED AT FS 1155, LBL 16 TO RBL 8. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0000128](https://openairdocs.org/sdr/CALA0000128.md): Intercostal · cracked · Feb 2, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN INTERCOSTAL AT FS 1022-1041, BL 0. THE INTERCOSTAL WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0000127](https://openairdocs.org/sdr/CALA0000127.md): Stop Pad · chafed · Feb 2, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR FORWARD STOP PADS ON FRAME CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-03, AND EA 9-5233-A0988.
- [SDR CALA0000126](https://openairdocs.org/sdr/CALA0000126.md): Cargo Track · corroded · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CARGO TIEDOWN TRACK IN MID CARGO COMPARTMENT CORRODED AT STA 769-786. A NEW CARGO TIEDOWN TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-10-3.
- [SDR CALA0000125](https://openairdocs.org/sdr/CALA0000125.md): Fitting · corroded · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LEFT O/B GALLEY FITTING CORRODED AT FS 1140. THE GALLEY FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR CALA0000124](https://openairdocs.org/sdr/CALA0000124.md): Skin · chafed · Feb 1, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND LOWER EXTERNAL SKIN FORWARD AND AFT CORNERS OF FORWARD CARGO DOOR CHAFED. A TWO DOUBLER REPAIR WAS INSTALLED WITH SHIMS IAW SRM 52-05, FIGURE 4, PAGE 5 AND 51-30-2, FIGURE 4, PAGE 5.
- [SDR CALA0000123](https://openairdocs.org/sdr/CALA0000123.md): Skin · dented · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 636, LONGERON 30. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 53-01, FIGURE 1, 51-30-05, AND 51-30-02.
- [SDR CALA0000122](https://openairdocs.org/sdr/CALA0000122.md): Bracket · cracked · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT FORWARD ADF FAIRING SUPPORT BRACKET CRACKED AT L/E WING ROOT. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0000121](https://openairdocs.org/sdr/CALA0000121.md): Skin · cracked · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT SIDE TAIL COMPARTMENT SKIN CRACKED JUST FORWARD OF RUDDER TRIM ACTUATOR AT STA 1485. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-14-4 AND 51-30-1.
- [SDR CALA0000120](https://openairdocs.org/sdr/CALA0000120.md): Skin · dented · Feb 1, 2000 · N14839 · Doug DC982 · Elevator, Plate/Skin
  > INSPECTION FOUND LT ELEVATOR LOWER SKIN SURFACE DENTED. THE DENTED AREA WAS REMOVED AND REPAIRED IAW ECRA 5520-01231.
- [SDR CALA0000119](https://openairdocs.org/sdr/CALA0000119.md): Intercostal · gouged · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO COMPARTMENT INTERCOSTAL GOUGED ON TOP AND BOTTOM FLANGE AT STA 1007, LONGERON 22R. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01, FIGURE 2.
- [SDR CALA0000118](https://openairdocs.org/sdr/CALA0000118.md): Stop Pad · chafed · Feb 1, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR UPPER STOP AND FORWARD STOP PADS ON FRAME CHAFED. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, 52-03, FIGURE 8, AND ECRA 5230-01519.
- [SDR CALA0000116](https://openairdocs.org/sdr/CALA0000116.md): Skin · corroded · Feb 1, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR UPPER FORWARD WEB SKIN CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0000115](https://openairdocs.org/sdr/CALA0000115.md): Frame · chafed · Feb 1, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR UPPER FORWARD STOP AREA CHAFED. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 52-03, FIGURE 8 AND ECRA 5230-01518.
- [SDR CALA0000114](https://openairdocs.org/sdr/CALA0000114.md): Flange · chafed · Feb 1, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD PIT DOOR SEAL ATTACH FLANGE CHAFED UNDER STOP PADS AT ALL SIDES OF DOOR. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, 51-30-7, 52-03, FIGURE 8 AND ECRA 5230-01518.
- [SDR CALA0000105](https://openairdocs.org/sdr/CALA0000105.md): Cargo Track · corroded · Jan 27, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT TIEDOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 1212-1322, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4H AND 51-30-1.
- [SDR CALA0000089](https://openairdocs.org/sdr/CALA0000089.md): Rib · cracked · Jan 26, 2000 · N14839 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A 1 INCH CRACK IN I/B TOP END OF FORWARD RIB ON LT MLG I/B DOOR. THE SKIN WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-05. THE SKIN WAS CLOSED IAW SRM 51-30-1, 51-30-2,
- [SDR CALA0000088](https://openairdocs.org/sdr/CALA0000088.md): Seat Track · corroded · Jan 26, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED FROM STA 1098 TO 1231. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 5.
- [SDR CALA0000087](https://openairdocs.org/sdr/CALA0000087.md): Clip · cracked · Jan 26, 2000 · N14839 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.
- [SDR CALA0000082](https://openairdocs.org/sdr/CALA0000082.md): Cowl · cracked · Jan 25, 2000 · N14839 · Doug DC982 · Engine Cowling System
  > INSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.
- [SDR CALA0000081](https://openairdocs.org/sdr/CALA0000081.md): Beam · corroded · Jan 25, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED AROUND RIVETS. A DOUBLER AND SPACER WERE INSTALLED IAW SRM 51-30-5 AND ECRA 5310-03027.
- [SDR CALA0000075](https://openairdocs.org/sdr/CALA0000075.md): Seat Track · corroded · Jan 24, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT GALLEY FITTING FS 218. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F, 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.
- [SDR CALA0000074](https://openairdocs.org/sdr/CALA0000074.md): Seat Track · corroded · Jan 24, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1140 GALLEY FITTING. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-05, 51-10-4, AND 51-30-1.
- [SDR CALA0000073](https://openairdocs.org/sdr/CALA0000073.md): Seat Track · corroded · Jan 24, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT INBD AND RT CENTER SEAT TRACKS CORRODED AT STA 207. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.
- [SDR CALA0000072](https://openairdocs.org/sdr/CALA0000072.md): Skin · gouged · Jan 24, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR SKIN GOUGED. THE AREA WAS REPAIRED IAW SRM 52-05, FIGURE 1.
- [SDR CALA0000071](https://openairdocs.org/sdr/CALA0000071.md): Door Pan · cracked · Jan 24, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A.75 INCH CRACK IN FORWARD CARGO DOOR PAN AT T/E SEAL RETAINER HOLES FLANGE, LOWER FORWARD SECTION, 12 INCHES FROM BOTTOM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 26A. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A, 51-10
- [SDR CALA0000070](https://openairdocs.org/sdr/CALA0000070.md): Support · corroded · Jan 24, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 168-200, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 53-14-1.
- [SDR CALA0000069](https://openairdocs.org/sdr/CALA0000069.md): Door Pan · corroded · Jan 23, 2000 · N14839 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVETS. THE DOOR JAMB PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44.
- [SDR CALA0000068](https://openairdocs.org/sdr/CALA0000068.md): Skin · cracked · Jan 23, 2000 · N14839 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND.5 INCH CRACKS IN REPAIR DOUBLER AT LOWER AFT O/B CORNER OF LT MLG I/B DOOR. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000067](https://openairdocs.org/sdr/CALA0000067.md): Seat Track · corroded · Jan 23, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 218. THE SEAT TRACK WAS REMOVED AND REPLACED USING A SPLICE IAW SRM 51-30-2,53-05, AND 51-30-3.
- [SDR CALA0000066](https://openairdocs.org/sdr/CALA0000066.md): Seat Track · corroded · Jan 23, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 1079-1271. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, 53-05, AND 51-30-2.
- [SDR CALA0000065](https://openairdocs.org/sdr/CALA0000065.md): Skin · cracked · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND AFT ACCESSORY CATWALK SHROUD RT AND LT FWD END SKIN CRACKED AT FS 1345. THE CRACKS WERE 2 AND 1 LONG, RESPECTIVELY. THE CRACKS WERE STOP DRILLED AND REPAIRED IAW SRM 53-01, FIGURE 2.
- [SDR CALA0000064](https://openairdocs.org/sdr/CALA0000064.md): Fitting · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED ATSTA 157, RBL 4. A NEW GALLEY SUPPORT FITTING WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000063](https://openairdocs.org/sdr/CALA0000063.md): Web · cracked · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT AIRSTAIRS LEFT AND RIGHT LOWER WEB CRACKED ABOVE GROUND ROLLER. THE CRACKS WERE 2 AND 1 LONG RESPECTIVELY. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 1 AND 51-10-3.
- [SDR CALA0000062](https://openairdocs.org/sdr/CALA0000062.md): Seat Track · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT FS 157-200, LBL 14. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
- [SDR CALA0000061](https://openairdocs.org/sdr/CALA0000061.md): Support · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180-200, RBL 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-3, AND 51-30-5.
- [SDR CALA0000060](https://openairdocs.org/sdr/CALA0000060.md): Skin · creased · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 120-150 BETWEEN LONGERON 24 AND 25R. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-30-2, AND 51-30-5.
- [SDR CALA0000059](https://openairdocs.org/sdr/CALA0000059.md): Bracket · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Emergency Exits
  > INSPECTION FOUND CORROSION AROUND FASTENER HOLE AT RT LOWER CORNER OF RT AFT EMERGENCY EXIT DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND 51-30-2. A BRACKET WAS INSTALLED IAW SRM 51-10-4 AND 51-30-1.
- [SDR CALA0000053](https://openairdocs.org/sdr/CALA0000053.md): Support · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRANCE THRESHOLD CORRODED. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1 AND 51-3-0.
- [SDR CALA0000052](https://openairdocs.org/sdr/CALA0000052.md): Panel · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND FORWARD UPPER PANEL OF Rt MLG DOOR CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 52-84-0.
- [SDR CALA0000051](https://openairdocs.org/sdr/CALA0000051.md): Support · corroded · Jan 21, 2000 · N14839 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRY AREA, STA 180, LBL 25, CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-30-5, AND 51-20-00.

Next page: https://openairdocs.org/deregistered/N14839-2008-07-16/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 = 'N14839' AND deregistration_id = 'N14839-2008-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14839-2008-07-16/reports

---
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