# Service difficulty reports: N14890, cancelled Jul 14, 2003

A list on [N14890, cancelled Jul 14, 2003](https://openairdocs.org/deregistered/N14890-2003-07-14.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA0100468](https://openairdocs.org/sdr/CALA0100468.md): Megaphone · inoperative · May 17, 2001 · N14890 · Doug DC982 · Emergency Equipment
  > THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE DURING TEST. THE AFT CABIN MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-60-00.
- [SDR CALA0000181](https://openairdocs.org/sdr/CALA0000181.md): Cable · out of rig · Feb 22, 2000 · N14890 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO DROP TAILCONE USING EXTERIOR AND INTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE RIGGED AND DROP CHECK WAS GOOD IAW MM 53-53-00.
- [SDR CALA0000177](https://openairdocs.org/sdr/CALA0000177.md): Beltframe · cracked · Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 1380 BETWEEN LONGERONS 4L AND 5L. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.
- [SDR CALA0000176](https://openairdocs.org/sdr/CALA0000176.md): Skin · dented · Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 216 BETWEEN LONGERON 14R AND 15R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0000175](https://openairdocs.org/sdr/CALA0000175.md): Fitting · cracked · Feb 17, 2000 · N14890 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN DOOR LOWER AFT STOP AREA INTERNAL FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0000173](https://openairdocs.org/sdr/CALA0000173.md): Door Jamb · cracked · Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO 1.5 INCH CRACKS IN MAIN CABIN DOOR JAMB BOX GUSSET AT STA 207, LONGERONS 11L AND 15L. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-03985 AND ECRA 5310-03986.
- [SDR CALA0000161](https://openairdocs.org/sdr/CALA0000161.md): Beltframe · corroded · Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD FACE OF BELTFRAME IN AFT BAG BIN CORRODED AT STA 1322, LONGERON 23L TO 29R. THE BELTFRAME WAS REPLACED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 55-03, FIGURE 2A, 51-10-3, 51-30-2, 51-30-5.
- [SDR CALA0000159](https://openairdocs.org/sdr/CALA0000159.md): Floorbeam · worn · Feb 16, 2000 · N14890 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM LOWER FLANGE WORN AT STA 1193 IN AFT CARGO COMPARTMENT. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 86.
- [SDR CALA0000157](https://openairdocs.org/sdr/CALA0000157.md): Angle · cracked · Feb 14, 2000 · N14890 · Doug DC982 · Entrance Stairs
  > INSPECTION FOUND A 1 INCH CRACK IN AFT STAIR DOOR ANGLE AT UPPER HINGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000156](https://openairdocs.org/sdr/CALA0000156.md): Cargo Track · cracked · Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 3 INCH CRACK IN TIE DOWN RAIL IN AFT BAG BIN AT STA 1271, LT SIDE. THE TIE DOWN RAIL WAS REMOVED AND A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 51-30-01.
- [SDR CALA0000155](https://openairdocs.org/sdr/CALA0000155.md): Cargo Track · corroded · Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT TIE DOWN RAIL TRACK CORRODED IN MID CARGO COMPARTMENT AT STA 693 TO AFT BULKHEAD. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000154](https://openairdocs.org/sdr/CALA0000154.md): Cargo Track · corroded · Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TIE DOWN RAIL IN AFT CARGO COMPARTMENT CORRODED. THE TIE DOWN RAIL WAS REPLACED IAW SRM 51-10-3 AND 51-30-0.
- [SDR CALA0000150](https://openairdocs.org/sdr/CALA0000150.md): Intercostal · corroded · Feb 12, 2000 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER LEFT OF INTERCOSTAL CORRODED UNDER LEFT TIE DOWN RAIL AT STA 1309-1322, L28L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-20-02.
- [SDR CALA0000149](https://openairdocs.org/sdr/CALA0000149.md): Intercostal · cracked · Feb 11, 2000 · N14890 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND MAIN CABIN DOOR INTERCOSTAL CRACKED BETWEEN NR 4 AND NR 5 BEAMS AFT OF INSIDE DOOR HANDLE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000144](https://openairdocs.org/sdr/CALA0000144.md): Seat Track · corroded · Feb 10, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 200-280. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-3.
- [SDR CALA9900109](https://openairdocs.org/sdr/CALA9900109.md): Support · broken · Feb 5, 1999 · N14890 · Doug DC982 · Landing Gear Position and Warning
  > THE LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION BOUND FOR EWR. THE GEAR WAS CYCLED TWICE, BUT THE LIGHT WOULD NOT EXTINGUISH. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT PROBLEM. MAINTENANCE FOUND THE LT MAIN GEAR DOOR TAR
- [SDR CALA9800445](https://openairdocs.org/sdr/CALA9800445.md): Angle · cracked · Mar 14, 1998 · N14890 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND A.375 INCH CRACK IN VERTICAL STABILIZER FORWARD RIGHT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. THE ANGLE WAS REPAIRED IAW SRM 55-02, FIGURE 26.
- [SDR CALA9800224](https://openairdocs.org/sdr/CALA9800224.md): Beltframe · cracked · Feb 12, 1998 · N14890 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 CRACK IN BELTFRAME AT LONGERON 2R AND A 2 CRACK IN BELTFRAME AT LONGERON 2L, STA 1418. A DOUBLER WAS INSTALLED TO ENCOMPASS BOTH CRACKS IAW SRM 53-05, FIGURE 32 AND ECRA 5311-01039.
- [SDR CALA9800215](https://openairdocs.org/sdr/CALA9800215.md): Cables · out of adjust · Feb 11, 1998 · N14890 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE EXTERIOR RELEASE HANDLE PULLED AT 15 POUNDS. THE TAILCONE WAS RIGGED IAW WORK CARD 08-5350-1-0008.
- [SDR CALA9800213](https://openairdocs.org/sdr/CALA9800213.md): Angle · cracked · Feb 10, 1998 · N14890 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA9800212](https://openairdocs.org/sdr/CALA9800212.md): Longeron · cracked · Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18.
- [SDR CALA9800205](https://openairdocs.org/sdr/CALA9800205.md): Splice · corroded · Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON TIEDOWN RAIL SPLICE AT STA 1220, LONGERON 28L, IN AFT CARGO COMPARTMENT. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-05-4.
- [SDR CALA9800204](https://openairdocs.org/sdr/CALA9800204.md): Angle · corroded · Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION IN LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT AT STA 1155. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9800203](https://openairdocs.org/sdr/CALA9800203.md): Fitting · cracked · Feb 10, 1998 · N14890 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9800188](https://openairdocs.org/sdr/CALA9800188.md): Support · corroded · Feb 5, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 IN AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9800187](https://openairdocs.org/sdr/CALA9800187.md): Support · corroded · Feb 5, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON THRESHOLD SUPPORT TEE BETWEEN STA 1155 AND 1174 AT AFT CARGO DOOR CUTOUT. THE THRESHOLD SUPPORT WAS REPLACED IAW SRM 51-10-2.
- [SDR CALA9800186](https://openairdocs.org/sdr/CALA9800186.md): Clips · broken · Feb 5, 1998 · N14890 · Doug DC982 · Aerodynamic Fairings
  > INSPECTION FOUND AFT FUSELAGE TAIL CONE EXTERIOR RELEASE HANDLE CLIPS BENT AND BROKEN. NEW CLIPS WERE INSTALLED AND TESTED IAW MM 53-53-00.
- [SDR CALA9800185](https://openairdocs.org/sdr/CALA9800185.md): Angle · cracked · Feb 4, 1998 · N14890 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.4 INCH CRACK IN AFT CABIN DOOR ANGLE INSIDE DOOR AT CENTER RIGHT DOOR STOP. THE ANGLE WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9800003](https://openairdocs.org/sdr/CALA9800003.md): Skin · cracked · Jan 6, 1998 · N14890 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A.5 INCH CRACK ABOVE BUMPER PAD IN LT MLG DOOR. THE CRACKED SKIN WAS REMOVED AND REPLACED IAW SRM 52-05.
- [SDR CALA9601171](https://openairdocs.org/sdr/CALA9601171.md): Apu Compressor · damaged · Aug 15, 1996 · N14890 · Doug DC982 · APU Core Engine
  > THERE WAS A STRONG PUNGENT ODOR IN THE AIRCRAFT CABIN SHORTLY AFTER TAKEOFF. NO ODOR WAS NOTICED DURING CRUISE PORTION OF FLIGHT WITH BOTH PACKS OPERATING. MAINTENANCE FOUND THE APU COMPRESSOR DAMAGED AND SEAL LEAKING. THE APU WAS PLACARDED INOPERATIVE FOR
- [SDR CAL960620](https://openairdocs.org/sdr/CAL960620.md): Downlock Sensor · inoperative · May 17, 1996 · N14890 · Doug DC982 · Landing Gear Position and Warning
  > FLT 1105 - CLE - THE LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH TO CLE. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS MANUALLY EXTENDED, BUT THE LIGHT REMAINED ON. THE GEAR WAS VISUALLY VERIFIED DOWN THROUGH THE VIEW PORT. TH
- [SDR CAL960377](https://openairdocs.org/sdr/CAL960377.md): Bracket · corroded · Feb 14, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND BRACKET PLATE CORRODED AT INTERSECTION OF FUSELAGE RIGHT CUSP FITTING AND FLOORBEAM, STATION 1338. THE CORRODED PLATE WAS REMOVED AND A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-01. (M)
- [SDR CAL960376](https://openairdocs.org/sdr/CAL960376.md): Support Brackets · cracked · Feb 13, 1996 · N14890 · Doug DC982 · Wing Miscellaneous Structure
  > MIA - INSPECTION FOUND 3 SUPPORT BRACKETS CRACKED AT RT WING FIXED LEADING EDGE INNER RIB. TWENTY INCHES OUTBOARD OF SLAT TRACK NR 2. THE CRACKS WERE 2 INCHES,.50 INCH, AND.50 INCH LONG. THE BRACKETS WERE REMOVED. NEW BRACKETS WERE FABRICATED AND INSTALL
- [SDR CAL960378](https://openairdocs.org/sdr/CAL960378.md): Fasteners · broken · Feb 12, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND TWO FASTENER HEADS POPPED ON RIGHT SIDE OF FUSELAGE AT FS 1000 AND 1005 BETWEEN L18R AND L19R, BELOW CUSP LINE. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. (M)
- [SDR CAL960390](https://openairdocs.org/sdr/CAL960390.md): Support · cracked · Feb 11, 1996 · N14890 · Doug DC982 · Wing Miscellaneous Structure
  > MIA - INSPECTION FOUND A.75 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST INBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL960389](https://openairdocs.org/sdr/CAL960389.md): Support · cracked · Feb 11, 1996 · N14890 · Doug DC982 · Wing Miscellaneous Structure
  > MIA - INSPECTION FOUND A 1 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST OUTBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL960380](https://openairdocs.org/sdr/CAL960380.md): Angle · corroded · Feb 11, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND THREE FLOOR SUPPORT 'Z' ANGLES CORRODED UNDER FLOORBOARD AT FORWARD ENTRY DOOR SILL AREA. THE FLOOR SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4. (M)
- [SDR CAL960379](https://openairdocs.org/sdr/CAL960379.md): Web · corroded · Feb 11, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND HORIZONTAL WEB CORRODED AT THRESHOLD OF FORWARD ENTRY DOOR, 4 INCHES INBOARD OF AFT CORNER OF CUTOUT. THE CORROSION WAS REMOVED IAW SRM 53-01. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01. (M)
- [SDR CAL960388](https://openairdocs.org/sdr/CAL960388.md): Support · cracked · Feb 9, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND A.6250 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807 BETWEEN LONGERON 25L AND LONGERON 26L. (X)
- [SDR CAL960381](https://openairdocs.org/sdr/CAL960381.md): Angle · cracked · Feb 9, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous Structure
  > MIA - INSPECTION FOUND A.5625 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807, BETWEEN L26R AND L27R. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01. (M)
- [SDR CAL951033](https://openairdocs.org/sdr/CAL951033.md): Gear Handle · binding · Nov 12, 1995 · N14890 · Doug DC982 · Landing Gear Selector
  > EWR - FLT 0609 - ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHTS EXTINGUISHED. MAINTENANCE CLEANED AND LUBRICATED THE LANDING GEAR HANDLE AND SWITCH. GEAR OPERATION AND INDICATIONS TESTED GOOD. (X
- [SDR CAL950723](https://openairdocs.org/sdr/CAL950723.md): Fire Loop · inoperative · Aug 17, 1995 · N14890 · Doug DC982 · Fire Detection
  > FLT NR 0114 - IAH - THE NR 1 ENGINE LOOP 'A' AND FIRE DETECT LOOP LIGHT ILLUMINATED WHILE ON DESCENT INTO IAH AT 15,000 FEET. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND BOTH FIRE BOTTLES WERE DISCHARGED. THE NR 1 ENGINE WAS SHUT DOWN. THE RED HANDLE LIGHT
- [SDR CAL950151](https://openairdocs.org/sdr/CAL950151.md): Switch · failed · Feb 24, 1995 · N14890 · Doug DC982 · Landing Gear Position and Warning
  > FLT NR 0132 - EWR - ALL THREE GEAR INDICATORS REMAINED RED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND ONLY THE NOSE GEAR LIGHT AND DOOR LIGHT REMAINED ON. THE GEAR WAS CYCLED A SECOND TIME AND ALL INDICATIONS WERE NORMAL. THE THREE GEAR INDICATORS WENT
- [SDR CAL950015](https://openairdocs.org/sdr/CAL950015.md): Grd Shift Mech · frozen · Jan 7, 1995 · N14890 · Doug DC982 · Landing Gear Retraction/Extension System
  > FLT NR 0262 - CLE - THE THREE GEAR RED UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED LEAVING CLE. THE GEAR WAS EXTENDED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE G
- [SDR CAL950003](https://openairdocs.org/sdr/CAL950003.md): Duct · blown · Jan 3, 1995 · N14890 · Doug DC982 · Cabin Cooling System
  > SAT - FLT 0437 - A STRONG BURNING ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON FINAL APPROACH TO SAT WITH THE ICE PROTECTION ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LT AIR CONDITIONING SYSTEM DUCT BLOWN IN THE TAIL COMPARTMENT AFT OF W

## 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 = 'N14890' AND deregistration_id = 'N14890-2003-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14890-2003-07-14/reports

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