# Service difficulty reports: N14880, cancelled Mar 21, 2013

A list on [N14880, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N14880-2013-03-21.md).

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

- [SDR CALA0100767](https://openairdocs.org/sdr/CALA0100767.md): Cylinder · inoperative · Aug 22, 2001 · N14880 · Doug DC981 · Landing Gear Actuator
  > THE R/H MLG WOULD NOT RETRACT AND THE GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED.AFTER TAKEOFF FROM EWR. THE LEFT MAIN AND NOSE GEAR WERE SLOW TO RETRACT AND THE R/H MAIN REMAINED DOWN DURING GEAR RECYCLING. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WIT
- [SDR CALA0000045](https://openairdocs.org/sdr/CALA0000045.md): Angle · cracked · Jan 19, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012.
- [SDR CALA0000044](https://openairdocs.org/sdr/CALA0000044.md): Frame · cracked · Jan 19, 2000 · N14880 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND THREE CRACKS IN WEB THROUGH LOWER FASTENERS IN A RADIAL STIFFENER OF LT CANTED BELTFRAME AT STA 1463. THE LENGTH OF THE THREE CRACKS TOTALED FIVE INCHES. THE CRACKS WERE STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-14-04.
- [SDR CALA0000042](https://openairdocs.org/sdr/CALA0000042.md): Frame · cracked · Jan 18, 2000 · N14880 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 CRACK IN LT BELTFRAME AT STA101 BELOW PULLEY BRACKET. THE BELTFRAME WAS REPAIRED IAW SRM 51-30-2 AND 53-03.
- [SDR CALA0000041](https://openairdocs.org/sdr/CALA0000041.md): Fitting · cracked · Jan 18, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 CRACK IN SUPPORT FITTING ABOVE AND FORWARD OF RT MLG DOOR ACTUATOR UPPER ATTACH POINT IN WHEEL WELL. A NEW FITTING WAS INSTALLED IAW SRM 51-30.
- [SDR CALA0000033](https://openairdocs.org/sdr/CALA0000033.md): Fitting · cracked · Jan 17, 2000 · N14880 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND A 2 CRACK IN AFT ENTRANCE DOOR CENTER HORIZONTAL BEAM RT END FITTING FLANGE. ANGLES WERE INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA0000032](https://openairdocs.org/sdr/CALA0000032.md): Retainer · cracked · Jan 17, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 CRACK IN LT COCKPIT WINDOW RETAINER. THE RETAINER WAS REMOVED AND A NEW RETAINER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000030](https://openairdocs.org/sdr/CALA0000030.md): Jamb · cracked · Jan 16, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 10 INCH CRACK IN RT WHEEL WELL FORWARD O/B DOOR JAMB. THE RT WHEEL WELL FORWARD O/B DOOR JAMB WAS REMOVED AND A NEW JAMB WAS INSTALLED IAW SRM 53-03, FIGURE 26.
- [SDR CALA0000027](https://openairdocs.org/sdr/CALA0000027.md): Floorbeam · dented · Jan 14, 2000 · N14880 · Doug DC981 · Fuselage Main, Floor Beam
  > INSPECTION FOUND ABB LOWER SIDE OF MAIN CABIN FLOORBEAM DENTED AND CREASED FROM CARGO DOOR LOWER FLANGE AT STA 1174. REPAIRED IAW SRM 53-05, FIGURE 86.
- [SDR CALA0000023](https://openairdocs.org/sdr/CALA0000023.md): Stringer · cracked · Jan 11, 2000 · N14880 · Doug DC981 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.25 INCH CRACK IN STRINGER 1L BETWEEN STA 1088 AND 1117. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000022](https://openairdocs.org/sdr/CALA0000022.md): Skin · cracked · Jan 11, 2000 · N14880 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.15 CRACK IN FUSELAGE SKIN AT STA 1338, BELOW L5L. THE CRACK WAS CUT OUT. DOUBLERS AND FILLER PLUG WERE INSTALLED IAW DAC DRAWING J060138.
- [SDR CALA0000016](https://openairdocs.org/sdr/CALA0000016.md): Pan · cracked · Jan 11, 2000 · N14880 · Doug DC981 · Cargo/Baggage Doors
  > INSPECTION FOUND A.25 INCH CRACK IN FORWARD BAGGAGE BIN DOOR PAN AT FORWARD MIDDLE STOP PAD. THE AREA WAS REPAIRED IAW SRM 52-05, FIGURE 50, SHEET 1.
- [SDR CALA0000014](https://openairdocs.org/sdr/CALA0000014.md): Longeron · corroded · Jan 8, 2000 · N14880 · Doug DC981 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 22R CORRODED IN E/E COMPARTMENT AT STA 155-160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000009](https://openairdocs.org/sdr/CALA0000009.md): Seat Track · corroded · Jan 4, 2000 · N14880 · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA1098-1140. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0000008](https://openairdocs.org/sdr/CALA0000008.md): Cusp · cracked · Jan 4, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2.5 CRACK INCH LT CUSP MEMBRANE AT STA 1309. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96.
- [SDR CALA0000004](https://openairdocs.org/sdr/CALA0000004.md): Cusp · cracked · Jan 2, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 CRACK IN RT CUSP MEMBRAME ATSTA 1309. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96.
- [SDR CALA9901707](https://openairdocs.org/sdr/CALA9901707.md): Strut · discharged · Dec 22, 1999 · N14880 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. THE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS CYCLED AND RETRACTION WAS SUCCESSFUL WITH ALL GEAR INDICATION LIGHTS GREEN. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. A NOSE STRUT FULL SERVIC
- [SDR CALA9901532](https://openairdocs.org/sdr/CALA9901532.md): Strut · discharged · Nov 24, 1999 · N14880 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR WAS EXTENDED AND ALL THREE GEAR GREEN LIGHTS WERE INDICATED. THE AIRCRAFT WAS RETURNED TO EWR. CREW NOTICED GEAR HANDLE RELEASE BUTTON WAS IN. THE BUTTON POPPED OUT WITH NOSE GEAR TOUCHDOWN.
- [SDR CALA9701714](https://openairdocs.org/sdr/CALA9701714.md): Skin · cracked · Dec 4, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.25 AND.125 INCH CRACK IN FUSELAGE SKIN AT LONGERON 1R STA 1337.5. A REPAIR WAS INSTALLED IAW ECRA 5331-01009 AND SRM 53-04, FIGURE 38, VIEW H.
- [SDR CALA9701706](https://openairdocs.org/sdr/CALA9701706.md): Skin · bent · Dec 2, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN BENT AND FASTENERS FOR INTERCOSTAL SHEARED AT LOWER VHF ANTENNA, STA 484. A REPAIR WAS INSTALLED IAW EA 5330-01823, OPERATION 3.
- [SDR CALA9701705](https://openairdocs.org/sdr/CALA9701705.md): Angle · cracked · Dec 1, 1997 · N14880 · Doug DC981 · Vertical Stabilizer
  > INSPECTION FOUND A.75 INCH CRACK EXTENDING FROM FASTENER IN RT AFT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1474. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23.
- [SDR CALA9701704](https://openairdocs.org/sdr/CALA9701704.md): Bracket · cracked · Dec 1, 1997 · N14880 · Doug DC981 · Spoilers
  > INSPECTION FOUND A 1.75 INCH CRACK ON THE RT WING INBOARD FLIGHT SPOILER ACTUATOR BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9701437](https://openairdocs.org/sdr/CALA9701437.md): Spar Tang · cracked · Oct 13, 1997 · N14880 · Doug DC981 · Wing Spar
  > AFT SPAR LEFT SIDE AFT TANG CRACKED (.250) FROM BUTE DOOR ATTACH HOLE APPROXIMATELY 5 OUTBOARD OF STATION 164. CUT OUT 2 CRACK AREA. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH EC/RA 5710-01844 AND DRAWING J060271-503.
- [SDR CALA9701338](https://openairdocs.org/sdr/CALA9701338.md): Hyd Line · leaking · Sep 8, 1997 · N14880 · Doug DC981 · Hydraulic System, Main
  > THE RT HYDRAULIC SYSTEM QUANTITY DROPPED TO AS LOW AS THREE QUARTS WHILE EN ROUTE. THE AIRCRAFT LANDED AT BOS WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE FOR RUDDER CONTROL SYSTEM LEAKING. THE HYDRAULIC LINE WAS REPLACED USING FLEX LINE. A DIP W
- [SDR CALA9700979](https://openairdocs.org/sdr/CALA9700979.md): Compressor Blade · failed · Jun 30, 1997 · N14880 · Doug DC981 · Turbine Engine Compressor Section
  > THE TOWER REPORTED SPARKS COMING FROM THE NR 1 ENGINE AT START OF TAKEOFF ROLL. THE TAKEOFF WAS REJECTED AT LESS THAN 60 KNOTS. EQUIPMENT WAS DISPATCHED AND THERE NO VISIBLE SIGNS OF FIRE OR SMOKE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINE OPERATION
- [SDR CALA9700821](https://openairdocs.org/sdr/CALA9700821.md): Starter · failed · Jun 4, 1997 · N14880 · Doug DC981 · Engine Starter
  > ENGINE START WAS ABORTED AFTER PUSHBACK WHEN THE NR 2 ENGINE REACHED 500 DEGREES. THE NR 2 ENGINE COWLING WAS OPENED WHICH REVEALED AN UNCONTAINED STARTER FAILURE. THE STARTER HAD DAMAGED THE SECONDARY FUEL SUPPLY MANIFOLD. THE STARTER AND FUEL MANIFOLD WER
- [SDR CALA9700302](https://openairdocs.org/sdr/CALA9700302.md): Skin · cracked · Mar 2, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN ABOVE FORWARD SERVICE PANEL. THE CRACKED AREA OF SKIN WAS REMOVED. A CLASS III REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12B. A DIP WAS ISSUED TO REPLACE THE CLASS III REPAIR WITH A CLASS I OR II REPAIR WITHIN 8,
- [SDR CALA9600962](https://openairdocs.org/sdr/CALA9600962.md): Hyd Pump · leaking · Jul 4, 1996 · N14880 · Doug DC981 · Hydraulic Pump (Electric/Engine), Main
  > THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED SHORTLY AFTER TAKEOFF FROM EWR. WHILE COMPLYING WITH ABNORMAL PROCEDURES THE LT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE LEFT HYDRAULIC PUMP AND TRANSFER PUMP WERE SECURED. THE AIRCRAFT WAS RETURNED TO EWR W
- [SDR CAL960442](https://openairdocs.org/sdr/CAL960442.md): Skin · damaged · Apr 6, 1996 · N14880 · Doug DC981 · Fuselage Main, Plate/Skin
  > EWR - FLT 0611 - THE FUSELAGE SKIN WAS DAMAGED BY A BELT LOADER AT STA 427, FORWARD CARGO DOOR JAMB. THE AREA WAS REPAIRED BY INSTALLING AN EXTERNAL DOUBLER IAW ECRA 5330-02381. (X)
- [SDR CAL960326](https://openairdocs.org/sdr/CAL960326.md): Dfg Computer · inoperative · Mar 16, 1996 · N14880 · Doug DC981 · Flight Management Computing Hardware System
  > EWR - FLT 0554 - THE LANDING GEAR AURAL WARNING SOUNDED ON FINAL APPROACH TO DWR WITH 3 GREEN LANDING GEAR LIGHTS INDICATED. CHECK LIST PROCEDURES WERE C/W DURING A 'GO-AROUND' AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. ACFT LANDED WITHOUT INCIDENT
- [SDR CAL960290](https://openairdocs.org/sdr/CAL960290.md): Actuator · iced up · Mar 10, 1996 · N14880 · Doug DC981 · Landing Gear Door Actuator
  > EWR - FLT 0491 - A SEVERE AIRFRAME VIBRATION WAS FELT IN THE VICINITY OF THE NOSE GEAR AREA AFTER GEAR WAS RAISED. THE NOSE GEAR UNSAFE LIGHT WAS ALSO ILLUMINATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT N
- [SDR CAL960055](https://openairdocs.org/sdr/CAL960055.md): Bracket · cracked · Jan 11, 1996 · N14880 · Doug DC981 · Wing Miscellaneous Structure
  > HOU - INSPECTION FOUND A.75 INCH CRACK IN RIGHT WING LEADING EDGE RIB AFT BRACKET, LOCATED AT FORWARD SPAR UPPER CAP OUTBOARD OF NR 8 SLAT TRACK. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M)
- [SDR CAL960054](https://openairdocs.org/sdr/CAL960054.md): Bracket · broken · Jan 11, 1996 · N14880 · Doug DC981 · Wing Miscellaneous Structure
  > HOU - INSPECTION FOUND RIGHT WING LEADING EDGE RIB LOWER ATTACH BRACKET BROKEN OUTBOARD OF NR 2 SLAT TRACK. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M)
- [SDR CAL960053](https://openairdocs.org/sdr/CAL960053.md): Rib · cracked · Jan 11, 1996 · N14880 · Doug DC981 · Wing, Rib/Bulkhead
  > HOU - INSPECTION FOUND A.625 INCH CRACK IN LOWER RADIUS OF LEFT WING LEADING EDGE RIB, LOCATED OUTBOARD OF NR 8 SLAT TRACK. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-04. (M)
- [SDR CAL960056](https://openairdocs.org/sdr/CAL960056.md): Rib · cracked · Jan 10, 1996 · N14880 · Doug DC981 · Passenger/Crew Doors
  > HOU - INSPECTION FOUND A 1.5 INCH CRACK IN RIB OF MAIN CABIN DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-05. (M)
- [SDR CAL950324](https://openairdocs.org/sdr/CAL950324.md): Steering · unsecured · Apr 18, 1995 · N14880 · Doug DC981 · Landing Gear Steering System
  > KUL - DURING TAXI OUT STEERING HAD TO MUCH PLAY. REPLACED NLG TIRES AND SECURED STEERING PER MM 32-21-04. NO FURTHER INCIDENT. (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 = 'N14880' AND deregistration_id = 'N14880-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14880-2013-03-21/reports

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