# Service difficulty reports: N14840, cancelled Apr 17, 2006

A list on [N14840, cancelled Apr 17, 2006](https://openairdocs.org/deregistered/N14840-2006-04-17.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 · 88 reports

- [SDR CALA0400490](https://openairdocs.org/sdr/CALA0400490.md): Seat Track · corroded · May 13, 2004 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT GALLEY MOUNTS, STA 1174 AND 1212. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-05.
- [SDR CALA0300134](https://openairdocs.org/sdr/CALA0300134.md): Frame · cracked · Mar 21, 2003 · N14840 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1/2 INCH CRACK IN CANTED FRAME CAP AT STA 1446, L3R. REMOVED AND REPLACED CAP IAW SRM 51-30-2.
- [SDR CALA0300119](https://openairdocs.org/sdr/CALA0300119.md): Longeron · cracked · Mar 19, 2003 · N14840 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT STA 1410. A REPAIR SECTION AND SPLICE WERE INSTALLED IAW ECRA 5311-01132.
- [SDR CALA0200243](https://openairdocs.org/sdr/CALA0200243.md): Torque Link · cracked · Apr 26, 2002 · N14840 · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > INSPECTION FOUND A 1.5" CRACK IN NLG UPPER TORQUE LINK. THE UPPER TORQUE LINK WAS REMOVED AND REPLACED IAW MM 32-21-04.
- [SDR CALA0100152](https://openairdocs.org/sdr/CALA0100152.md): Light · inoperative · Feb 22, 2001 · N14840 · Doug DC982 · Emergency Lighting
  > THE FORWARD ENTRY PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EMERGENCY LIGHT WAS REMOVED AND REPLACED IAW MM 33-53-01.
- [SDR CALA0001815](https://openairdocs.org/sdr/CALA0001815.md): Seat Track · corroded · Nov 21, 2000 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT FS 200 - 243. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-10-3.
- [SDR CALA0001799](https://openairdocs.org/sdr/CALA0001799.md): Doubler · corroded · Nov 17, 2000 · N14840 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND NR 1 RAD ALT ANTENNA DOUBLER CORRODED. THE ANTENNA DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR CALA0001798](https://openairdocs.org/sdr/CALA0001798.md): Bracket · cracked · Nov 17, 2000 · N14840 · Doug DC982 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND A 1 INCH CRACK IN NR 1 ENGINE PYLON O/B TRAILING EDGE BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.
- [SDR CALA0001784](https://openairdocs.org/sdr/CALA0001784.md): Skin · damaged · Nov 17, 2000 · N14840 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CREASED AT FS 133, LONGERON 18L. A DOUBLER AND SKIN FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-34, FIGURE 1.
- [SDR CALA0001783](https://openairdocs.org/sdr/CALA0001783.md): Support Bracket · cracked · Nov 16, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN AFT END OF TAIL COMPARTMENT LT SIDE WALL SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 51-10-1.
- [SDR CALA0001779](https://openairdocs.org/sdr/CALA0001779.md): Door Frame · corroded · Nov 16, 2000 · N14840 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO DOOR JAMB CORRODED AROUND RIVET NUTS. THE DOOR JAMB WAS REMOVED AND A NEW DOOR JAMB WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4.
- [SDR CALA0001778](https://openairdocs.org/sdr/CALA0001778.md): Seat Track · corroded · Nov 16, 2000 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 788 - 1258. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3, AND 53-05, FIGURE 4F.
- [SDR CALA0001775](https://openairdocs.org/sdr/CALA0001775.md): Skin · chafed · Nov 15, 2000 · N14840 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR OUTER SKIN CHAFED AT BOTTOM FORWARD CORNER. THE DOUBLER WAS REMOVED IAW SRM 51-30-2 AND 51-10-4. A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0001774](https://openairdocs.org/sdr/CALA0001774.md): Skin · dented · Nov 15, 2000 · N14840 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND LT WING 0 SLAT DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-06, FIGURE 1. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-7.
- [SDR CALA0001763](https://openairdocs.org/sdr/CALA0001763.md): Web · corroded · Nov 14, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED ON O/B EDGE AT STA 389 - 427, LONGERON 18R. THE CORRODED SECTION OF WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 53-01, FIGURE 1.
- [SDR CALA0001762](https://openairdocs.org/sdr/CALA0001762.md): Skin · dented · Nov 14, 2000 · N14840 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 280 BETWEEN LONGERON 23L AND 24L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0001751](https://openairdocs.org/sdr/CALA0001751.md): Angle · cracked · Nov 13, 2000 · N14840 · Doug DC982 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RIGHT PYLON PANEL 8212C L-ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.
- [SDR CALA0001750](https://openairdocs.org/sdr/CALA0001750.md): Fitting · cracked · Nov 13, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN EXTERNAL FUSELAGE LOWER FILLET FAIRING T-FITTING AT FS 880. THE T-FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0001748](https://openairdocs.org/sdr/CALA0001748.md): Web · corroded · Nov 13, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT CUSP WEB CORRODED AT STA 503 - 598. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-14-2.
- [SDR CALA0001747](https://openairdocs.org/sdr/CALA0001747.md): Pan · gouged · Nov 13, 2000 · N14840 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR LOWER EDGE PAN CHAFED AND GOUGE AROUND ALL DOOR STOPS. DOUBLERS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-30-2, AND 51-30-3.
- [SDR CALA0001743](https://openairdocs.org/sdr/CALA0001743.md): Rib · cracked · Nov 13, 2000 · N14840 · Doug DC982 · Aerodynamic Fairings
  > INSPECTION FOUND A 1 INCH CRACK IN AFT MOST LEFT RIB AT FASTENER HOLE OF VERTICAL STABILIZER SADDLE FAIRING. THE RIB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 55-01. A DOUBLER AND RIB WERE INSTALLED IAW SRM 55-01, 51-30-2, AND 51-30-5.
- [SDR CALA0001742](https://openairdocs.org/sdr/CALA0001742.md): Web · corroded · Nov 12, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED IN LT AFT BAG PIT AT FS 1174 - 1193, S18L. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.
- [SDR CALA0001741](https://openairdocs.org/sdr/CALA0001741.md): Strap · corroded · Nov 12, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO DOOR CUTOUT REPAIR STRAP CORRODED. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-5, 53-05, FIGURE B, AND 51-10-4.
- [SDR CALA0001740](https://openairdocs.org/sdr/CALA0001740.md): Fitting · cracked · Nov 12, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM FITTING AT FS 294, BL 0. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0001739](https://openairdocs.org/sdr/CALA0001739.md): Intercostal · cracked · Nov 12, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK AT AFT UPPER CORNER OF INTERCOSTAL BETWEEN FS 1022 AND 1041, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0001738](https://openairdocs.org/sdr/CALA0001738.md): Pan · dented · Nov 12, 2000 · N14840 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND RIGHT MLG DOOR UPPER DOOR PAN DENTED AT DOOR HINGE. THE PAN WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0001737](https://openairdocs.org/sdr/CALA0001737.md): Pan · gouged · Nov 12, 2000 · N14840 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR PAN AFT EDGE CHAFED AND GOUGED AROUND DOOR STOPS NR 6, 9 AND 10. REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0001733](https://openairdocs.org/sdr/CALA0001733.md): Support Bracket · cracked · Nov 11, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AN 8 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT BELOW RT WATER SEPARATOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-3, AND 51-30-1.
- [SDR CALA0001732](https://openairdocs.org/sdr/CALA0001732.md): Fitting · cracked · Nov 11, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND EXTERNAL FUSELAGE LOWER FILLET FAIRING STRUCTURE T-FITTINGS CRACKED AT FS 850 AND 865. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, 51-10-4, AND 51-30-5.
- [SDR CALA0001731](https://openairdocs.org/sdr/CALA0001731.md): Web · corroded · Nov 11, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT CUSP WEB CORRODED AT FS 598 - 712. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-10-4.
- [SDR CALA0001728](https://openairdocs.org/sdr/CALA0001728.md): Spacer · corroded · Nov 10, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO LOWER DOOR JAMB SPACER CORRODED. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-4.
- [SDR CALA0001727](https://openairdocs.org/sdr/CALA0001727.md): Panel · cracked · Nov 10, 2000 · N14840 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK AT FASTENER HOLE IN RT WING L/E PANEL 1222C. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 57-01, FIGURE 3, AND 51-30-2.
- [SDR CALA0001726](https://openairdocs.org/sdr/CALA0001726.md): Seat Track · corroded · Nov 10, 2000 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA0001725](https://openairdocs.org/sdr/CALA0001725.md): Skin · chipped · Nov 10, 2000 · N14840 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND THE L-1 DOOR SKIN CHIPPED IN FORWARD LOWER CORNER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA0001724](https://openairdocs.org/sdr/CALA0001724.md): Web · corroded · Nov 10, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON I/B EDGE OF CUSP WEB AT FS 1222 AT SEAT TRACK SPLICE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-02.
- [SDR CALA0001722](https://openairdocs.org/sdr/CALA0001722.md): Pan · gouged · Nov 10, 2000 · N14840 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR PAN CHAFED AND GOUGED AT DOOR STOPS NR 1, 2, AND 5. REPAIR DOUBLERS AND SHIMS WERE INSTALLED AT EACH DOOR STOP LOCATION IAW ECRA 5330-02819 AND SRM 51-10-5.
- [SDR CALA0001720](https://openairdocs.org/sdr/CALA0001720.md): Fitting · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND BOTH R-1 DOOR GIRT BAR MOUNT FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-3, 51-10-4, 51-10-3, AND 51-30-1.
- [SDR CALA0001719](https://openairdocs.org/sdr/CALA0001719.md): Plate · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 146 - 200, RBL 55. THE COVER PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-30-2.
- [SDR CALA0001718](https://openairdocs.org/sdr/CALA0001718.md): Web · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP WEBS CORRODED AT FS 503 - 598 AND FS 598 - 712. THE CUSP WEBS WERE REMOVED AND NEW CUSP WEBS WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA0001717](https://openairdocs.org/sdr/CALA0001717.md): Pan · gouged · Nov 9, 2000 · N14840 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR PAN GOUGED AT DOOR STOP NR 5. THE GOUGED AREA WAS REMOVED AND A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-3.
- [SDR CALA0001716](https://openairdocs.org/sdr/CALA0001716.md): Doubler · worn · Nov 9, 2000 · N14840 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND LT MLG DOOR AFT EDGE LOWER CHAFE STRIP WORN. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 52-05, FIGURE 28.
- [SDR CALA0001715](https://openairdocs.org/sdr/CALA0001715.md): Floorbeam · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND NUT PLATE AND FASTENER HOLE OF LT AFT CABIN FLOORBEAM CORRODED AT STA 1309, LBL 24. REPAIR ANGLES AND FILLER WERE INSTALLED IAW SRM 53-05, FIGURE 20A.
- [SDR CALA0001714](https://openairdocs.org/sdr/CALA0001714.md): Web · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP WEB CORRODED IN MID CARGO COMPARTMENT AT FS 737 - 756. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-2, 51-30-3, AND 51-30-4.
- [SDR CALA0001713](https://openairdocs.org/sdr/CALA0001713.md): Floorbeam · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT FASTENER HOLE, STA 1322, LBL 40. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-3 AND 53-05, FIGURE 20A.
- [SDR CALA0001712](https://openairdocs.org/sdr/CALA0001712.md): Bracket · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LT SERVICE DOOR THRESHOLD PAN MOUNTING BRACKET CORRODED. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-30-2.
- [SDR CALA0001711](https://openairdocs.org/sdr/CALA0001711.md): Seat Track · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1109. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4.
- [SDR CALA0001710](https://openairdocs.org/sdr/CALA0001710.md): Floor Support · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 140 - 200, LBL 7. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0001709](https://openairdocs.org/sdr/CALA0001709.md): Fitting · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND G-4 GALLEY ATTACH FITTING CORRODED AT FS 1174, LBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-5, AND 51-10-4.
- [SDR CALA0001708](https://openairdocs.org/sdr/CALA0001708.md): Seat Track · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1079 - 1271. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-5, 51-10-3, AND 53-05, FIGURE 4F.
- [SDR CALA0001707](https://openairdocs.org/sdr/CALA0001707.md): Floor Support · corroded · Nov 9, 2000 · N14840 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT FS 146 - 200, LBL 44 AND AT FS 200, LBL 55. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-10-4, 51-30-05, AND 51-30-08.

Next page: https://openairdocs.org/deregistered/N14840-2006-04-17/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 = 'N14840' AND deregistration_id = 'N14840-2006-04-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14840-2006-04-17/reports

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