N14880, cancelled Mar 21, 2013

Service difficulty reports · 36

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA0100767Cylinder · inoperativeTHE 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 WITAug 22, 2001 · N14880 · Doug DC981 · Landing Gear ActuatorSDR CALA0000045Angle · crackedINSPECTION FOUND RT DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012.Jan 19, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA0000044Frame · crackedINSPECTION 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.Jan 19, 2000 · N14880 · Doug DC981 · Fuselage Main, FrameSDR CALA0000042Frame · crackedINSPECTION FOUND A 1 CRACK IN LT BELTFRAME AT STA101 BELOW PULLEY BRACKET. THE BELTFRAME WAS REPAIRED IAW SRM 51-30-2 AND 53-03.Jan 18, 2000 · N14880 · Doug DC981 · Fuselage Main, FrameSDR CALA0000041Fitting · crackedINSPECTION 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.Jan 18, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA0000033Fitting · crackedINSPECTION 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.Jan 17, 2000 · N14880 · Doug DC981 · Passenger/Crew DoorsSDR CALA0000032Retainer · crackedINSPECTION 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.Jan 17, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA0000030Jamb · crackedINSPECTION 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.Jan 16, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA0000027Floorbeam · dentedINSPECTION 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.Jan 14, 2000 · N14880 · Doug DC981 · Fuselage Main, Floor BeamSDR CALA0000023Stringer · crackedINSPECTION 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.Jan 11, 2000 · N14880 · Doug DC981 · Fuselage Main, Longeron/StringerSDR CALA0000022Skin · crackedINSPECTION 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.Jan 11, 2000 · N14880 · Doug DC981 · Fuselage Main, Plate/SkinSDR CALA0000016Pan · crackedINSPECTION 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.Jan 11, 2000 · N14880 · Doug DC981 · Cargo/Baggage DoorsSDR CALA0000014Longeron · corrodedINSPECTION FOUND LONGERON 22R CORRODED IN E/E COMPARTMENT AT STA 155-160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jan 8, 2000 · N14880 · Doug DC981 · Fuselage Main, Longeron/StringerSDR CALA0000009Seat Track · corrodedINSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA1098-1140. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0.Jan 4, 2000 · N14880 · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000008Cusp · crackedINSPECTION 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.Jan 4, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA0000004Cusp · crackedINSPECTION FOUND A 3 CRACK IN RT CUSP MEMBRAME ATSTA 1309. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96.Jan 2, 2000 · N14880 · Doug DC981 · Fuselage Miscellaneous StructureSDR CALA9901707Strut · dischargedTHE 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 SERVICDec 22, 1999 · N14880 · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR CALA9901532Strut · dischargedTHE 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. Nov 24, 1999 · N14880 · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR CALA9701714Skin · crackedINSPECTION 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.Dec 4, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/SkinSDR CALA9701706Skin · bentINSPECTION 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.Dec 2, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/SkinSDR CALA9701705Angle · crackedINSPECTION 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.Dec 1, 1997 · N14880 · Doug DC981 · Vertical StabilizerSDR CALA9701704Bracket · crackedINSPECTION 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.Dec 1, 1997 · N14880 · Doug DC981 · SpoilersSDR CALA9701437Spar Tang · crackedAFT 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.Oct 13, 1997 · N14880 · Doug DC981 · Wing SparSDR CALA9701338Hyd Line · leakingTHE 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 WSep 8, 1997 · N14880 · Doug DC981 · Hydraulic System, MainSDR CALA9700979Compressor Blade · failedTHE 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 OPERATIONJun 30, 1997 · N14880 · Doug DC981 · Turbine Engine Compressor SectionSDR CALA9700821Starter · failedENGINE 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 WERJun 4, 1997 · N14880 · Doug DC981 · Engine StarterSDR CALA9700302Skin · crackedINSPECTION 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,Mar 2, 1997 · N14880 · Doug DC981 · Fuselage Main, Plate/SkinSDR CALA9600962Hyd Pump · leakingTHE 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 WJul 4, 1996 · N14880 · Doug DC981 · Hydraulic Pump (Electric/Engine), MainSDR CAL960442Skin · damagedEWR - 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)Apr 6, 1996 · N14880 · Doug DC981 · Fuselage Main, Plate/SkinSDR CAL960326Dfg Computer · inoperativeEWR - 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 INCIDENTMar 16, 1996 · N14880 · Doug DC981 · Flight Management Computing Hardware SystemSDR CAL960290Actuator · iced upEWR - 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 NMar 10, 1996 · N14880 · Doug DC981 · Landing Gear Door ActuatorSDR CAL960055Bracket · crackedHOU - 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)Jan 11, 1996 · N14880 · Doug DC981 · Wing Miscellaneous StructureSDR CAL960054Bracket · brokenHOU - 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)Jan 11, 1996 · N14880 · Doug DC981 · Wing Miscellaneous StructureSDR CAL960053Rib · crackedHOU - 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)Jan 11, 1996 · N14880 · Doug DC981 · Wing, Rib/BulkheadSDR CAL960056Rib · crackedHOU - INSPECTION FOUND A 1.5 INCH CRACK IN RIB OF MAIN CABIN DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-05. (M)Jan 10, 1996 · N14880 · Doug DC981 · Passenger/Crew DoorsSDR CAL950324Steering · unsecuredKUL - DURING TAXI OUT STEERING HAD TO MUCH PLAY. REPLACED NLG TIRES AND SECURED STEERING PER MM 32-21-04. NO FURTHER INCIDENT. (W)Apr 18, 1995 · N14880 · Doug DC981 · Landing Gear Steering System
Back to N14880, cancelled Mar 21, 2013