N13067, cancelled Apr 27, 2005

Service difficulty reports · 62

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 = 'N13067' AND deregistration_id = 'N13067-2005-04-27'
  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 CALA0000846Web · crackedINSPECTION FOUND A 3 INCH CRACK ON VERTICAL WEB IN AFT CARGO COMPARTMENT AT STA 1841 ABOVE LONGERON 43-44, LBL 65. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH A NEW WEB AND DOUBLER IAW SRM 53-00-01, FIGURE 4 & 5 AND 51-31-01.Jun 8, 2000 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0000845Channel · crackedTHE FORWARD CARGO COMPARTMENT LEFT LOWER SIDEWALL Z-CHANNEL FORWARD OF LOAD BAR HAD A 12 INCH CRACK AND PUNCTURE ON LT LOWER SIDEWALL TRIM PLATE. AN INTERIM REPAIR HAD PREVIOUSLY BEEN INSTALLED IAW ECRA 5320-00164 AND PLACED ON A DIP. A PERMANENT REPAIR WAS Jun 8, 2000 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0000844Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN CENTER CARGO COMPARTMENT AT STA 1740, LONGERON 45R. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 8 AND 51-31-01.Jun 7, 2000 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0000843Fitting · corrodedINSPECTION FOUND FORWARD CARGO DOOR JAMB FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 53-50-00, FIGURE 1, 51-21-01, AND 51-31-01.Jun 7, 2000 · N13067 · Doug DC1030 · Fuselage Main, StructureSDR CALA0000837Stringer · crackedINSPECTION FOUND STRINGERS NR 4, 5, AND 7 CRACKED IN RT MAIN GEAR WHEEL WELL AT O/B LOWER WALL AFT OF OUTER DOOR CUTOUT. THE CRACKS WERE 1, 4, AND 5 INCHES LONG. THE CRACKED AREAS WERE REMOVED AND REINFORCED WITH ANGLES IAW SRM 53-00-01, FIGURE 2 AND 51-31-0Jun 7, 2000 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA0000836Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ANGLE ON OUTER DOOR CUTOUT AFT SIDE FORWARD EDGE, LT MLG WHEEL WELL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01 AND 57-53-01.Jun 7, 2000 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0000835Skin · corrodedINSPECTION FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA 900 BETWEEN LONGERON 37L AND 38L. THE CORRODED AREA OF SKIN WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER AND FINGER DOUBLER USING RIVETS IAW SRM 53-20-00 AND 51-31-01.Jun 7, 2000 · N13067 · Doug DC1030 · Fuselage Main, Plate/SkinSDR CALA0000834Skin · crackedINSPECTION FOUND A 6 INCH CRACK IN LT WING LOWER SURFACE ON I/B CORNER OF FUELING BAY DOOR CUTOUT. THE AREA WAS REINFORCED WITH A DOUBLER USING RIVETS IAW SRM 57-10-00, FIGURE 68 AND 51-31-01.Jun 7, 2000 · N13067 · Doug DC1030 · Wing, Plate/SkinSDR CALA0000814Light · inoperativeINSPECTION FOUND CABIN EMERGENCY LIGHT ASSEMBLY AT SEAT 9B INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.Jun 2, 2000 · N13067 · Doug DC1030 · Emergency LightingSDR CALA9901719Oven · inoperativeSMOKE BEGAN COMING OUT OF THE AFT GALLEY OVEN CONTROL PANEL WHILE EN ROUTE TO EWR. THE SMOKE STOPPED WHEN OVEN WAS TURNED OFF. THE FLIGHT CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE AFT GALLEY OVEN WAS REMOVED AND REPLACEDDec 23, 1999 · N13067 · Doug DC1030 · Buffet/GalleysSDR CALA9901498Wire · brokenINSPECTION FOUND FORWARD EMERGENCY LIGHT AT SEAT 2KL INOPERATIVE. INSPECTION REPAIRED BROKEN WIRE AT SEAT 2KL AND OPERATION CHECKED GOOD.Nov 14, 1999 · N13067 · Doug DC1030 · Light System WiringSDR CALA9900779Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN ATTACH ANGLE AT STA 1120, STRINGER 33-34R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900778Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 899, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900777Support · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 755 BETWEEN RBL 65 AND 85. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900776Liner · tornINSPECTION FOUND A 2 INCH TEAR ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841, RBL 10. THE TORN AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 53-00-01, FIGURE 4, 51-21-01, AND 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900775Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME OF CENTER CARGO COMPARTMENT VERTICAL WALL AT STA 1841, RBL 20. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 53-00-01, FIGURE 4 AND 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Main, FrameSDR CALA9900774Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, LBL 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900773Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED UNDER LAV/GALLEY FLOOR AREA AT STA 420 BETWEEN BL 0 TO LBL 27. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-21-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900772Skin · crackedINSPECTION FOUND A 1 INCH CRACK WITH SHEARED RIVETS IN RT WING NR 2 LEADING EDGE SLAT INBOARD SKIN. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-00-01, FIGURE 4. THE RIVETS WERE REPLACED WITH NEW RIVETS IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Leading Edge DevicesSDR CALA9900771Angle · crackedINSPECTION FOUND TWO VERTICAL STIFFENER ANGLES ON LT WHEEL WELL AFT SIDE WEB CRACKED. THE CRACKS WERE .5 INCH LONG. THE TWO ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-31-01.Jul 5, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900770Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN STIFFENER VERTICAL ANGLE AT RT MLG WHEEL WELL REAR BULKHEAD LOWER O/B CORNER JOINT TO LONGERON TO BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-35-02 AND 51-33-01, FIGURE 1.Jul 4, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900759Stringer · corrodedINSPECTION FOUND FRAME CORRODED IN LOWER LOBE AFT CARGO BILGE AREA AT STA 1851 BETWEEN STRINGER 51L AND 51R WITH CORROSION ON STRINGERS 52L AND 51L. THE CORRODED AREA ON FRAME WAS CLEANED AND TREATED IAW SRM 51-21-00. THE CORRODED SECTIONS OF STRINGERS WERE Jun 30, 1999 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9900736Stringer · corrodedINSPECTION FOUND STRINGER 50 CORRODED BETWEEN STA 1851 AND 1868. THE CORRODED SECTION WAS REMOVED, A NEW SECTION OF STRINGER WAS INSTALLED WITH REINFORCEMENT IAW SRM 51-31-01 AND 53-10-00, FIGURE 2.Jun 28, 1999 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9900735Frame · corrodedINSPECTION FOUND CORROSION ON BOTH LOWER SIDES OF FRAME AT STA 1741 AND 1761 BETWEEN STRINGER 47L AND 50R. THE CORRODED AREAS WERE REMOVED, NEW ANGLES WERE INSTALLED IAW SRM 51-31-01.Jun 28, 1999 · N13067 · Doug DC1030 · Fuselage Main, FrameSDR CALA9900734Wall · tornINSPECTION FOUND TEARS ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841 BETWEEN LBL 40 & 60. THE TORN AREAS WERE TRIMMED OUT AND DEBURRED. REINFORCED AREAS WITH DOUBLER IAW SRM 53-00-01, FIGURE 4 AND INSTALLED RIVETS IAW SRM 51-33-01.Jun 28, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900733Angle · crackedINSPECTION FOUND A 2 INCH CRACK ON VERTICAL ANGLE IN CENTER CARGO COMPARTMENT AT STA 1841, LBL 10. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01.Jun 28, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900715Support · corrodedINSPECTION FOUND FLOOR SUPPORT UNDER LAV/GALLEY AREA CORRODED AT STA 755-899, LBL 44. THE CORRODED FLOOR SUPPORT SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED AND REINFORCED IAW SRM 53-70-00, FIGURE 13.Jun 22, 1999 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801941Apu · leakingOIL SMELL IN COCKPIT. APU INTERNAL OIL LEAK CONFIRMED. CLEANED AIRCRAFT PACKS. PLACARD APU PER MEL.Oct 11, 1998 · N13067 · Doug DC1030 · APU Oil SystemSDR CALA9800900Computer · inoperativeTHE CAPTAIN'S STICK SHAKER ACTIVATED, THE SLAT DISAGREE LIGHT ILLUMINATED, AND SLAT RESET ILLUMINATED DURING TAKEOFF FROM IAH. CONFIRMED SLAT RETRACTION PER CHECKLIST AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THEMay 24, 1998 · N13067 · Doug DC1030 · Auto Throttle SystemSDR CALA9800810Wire · brokenNUMBER 3 ENGINE NUMBER 1 AGENT FIRE BOTTLE LOW PRESSURE SWITCH FAILED. WIRE FOUND BROKEN AT EARTH POINT 6015D. WIRE RETERMINATED WITH A NEW TAG PER MM20-00-00.May 7, 1998 · N13067 · Doug DC1030 · Extinguishing SystemSDR CALA9800789Wire · brokenCARGO FIRE BOTTLE NR 2 LOW PRESSURE SWITCH ELECTRICAL CONNECTOR WIRE FOUND BROKEN. WIRE W277B24 FOUND BROKEN AT PIN B OF CONECTOR P1-2189. NEW PIN FITTED AND TESTED.May 6, 1998 · N13067 · Doug DC1030 · Fire Bottle, FixedSDR CALA9800788Fire Bottle · damagedNUMBER 2 ENGINE AND APU FIRE BOTTLE LOW PRESSURE CONNECTOR P1-1264 SOCKET B FOUND PUSHED BACK. ELECTRICAL CONNECTOR REPLACED PER MM 20-00-00.May 6, 1998 · N13067 · Doug DC1030 · Fire Bottle, FixedSDR CALA9800787Cartridge · open circuitNUMBER 1 ENGINE FIRE BOTTLE AGENT ONE FILAMENT A NOT LIGHTING ON TEST BOX DURING TEST. CARTRIDGE FOUND U/S. INSTALLED NEW CARTRIDGE.May 6, 1998 · N13067 · Doug DC1030 · Extinguishing SystemSDR CALA9700636Compressor · damagedTHE NR 3 ENGINE EXPERIENCED COMPRESSOR STALLS WHILE ENROUTE. THE AIRCRAFT WAS RETURNED TO LGW. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND OPERATION CHECKED GOOD. *S/D* INSPECTION OF THE ENGINE FOUND THAT THE ENTIRE COMPRESSOR HAD SUFMay 3, 1997 · N13067 · Doug DC1030 · Turbine Engine Compressor SectionSDR CALA9700666Longeron · corrodedDIP NR 017105 WAS COMPLIED WITH BY INSTALLING A PERMANENT REPAIR AT LONGERON 46L, STA 1811. THE OLD REPAIR WAS REMOVED. A PERMANENT REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03467.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9700665Skin · crackedINSPECTION FOUND A 1 CRACK IN SKIN WITH CORROSION AT FASTENER ON RIGHT HAND SIDE OF NR 2 ENGINE COWL, STA 2120 UPPER SURFACE AT BASE OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5530-01179. THE CORROSApr 25, 1997 · N13067 · Doug DC1030 · Engine Cowling SystemSDR CALA9700664Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED BELOW CENTER PIT DOOR AT STA 1681-1701, L48L TO L48R. THE CORRODED AREA OF SKIN WAS CUT OUT IAW SRM 53-20-00. SKIN FILLER, DOUBLER, TRIPLER, AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6, 5Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Main, Plate/SkinSDR CALA9700662Longeron · corrodedINSPECTION FOUND LONGERON 50L CORRODED AT BS 1708. THE CORRODED SECTION WAS CUTOUT. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE 1, AND SRM 51-33-01.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9700661Longeron · corrodedINSPECTION FOUND LONGERON 51R CORRODED AT STA 1708. THE CORRODED AREA WAS CUTOUT. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE 1, TYPE III, AND SRM 51-33-01.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9700660Panel · crackedINSPECTION FOUND NR 3 ENGINE ACCESS PANEL 487 FRAME CRACKED AT ATTACHMENT HOLE, A BROKEN NUTPLATE, AND CORROSION AT MATING SURFACE. THE CRACK WAS 1 INCH LONG. THE CRACKED AREA WAS REMOVED. DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01,Apr 25, 1997 · N13067 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9700659Angle · crackedINSPECTION FOUND A 5.5 INCH CRACK IN LT WING INBOARD ATTACH ANGLE AT WS XCW 118. THE ANGLE WAS REMOVED IAW SRM 51-33-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-00.Apr 25, 1997 · N13067 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9700658Skin · buckledINSPECTION FOUND FUSELAGE SKIN BUCKLED AT STA 335 JUST UNDER PILOT'S SLIDING WINDOW. THE AREA WAS REFORMED TO WITHIN LIMITS IAW SRM 53-20-00. A FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-20-00 AND 51-31-01.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Main, Plate/SkinSDR CALA9700657Shear Tie · corrodedINSPECTION FOUND FRAME SHEAR TIE CORRODED AT STA 1721, BETWEEN LONGERON 49L AND 47L. THE CORRODED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE SECTION WAS INSTALLED IAW SRM 51-33-01 AND 51-35-01.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700656Shear Tie · corrodedINSPECTION FOUND FRAME SHEAR TIE CORRODED AT STA 1821, BETWEEN LONGERON 48L AND 49L. THE CORRODED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 51-33-01 AND 51-35-01.Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700655Skin · dentedINSPECTION FOUND FIVE DENTS IN UPPER SKIN OF RT DETACHABLE ELEVATOR. THE DENTED SKIN WAS REMOVED IAW SRM 55-00-01, FIG. 1, VOL I AND 55-00-01, FIG. 2, VOL I. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-00-01, FIG. 3, VOL I AND 51-35-02, VOL II.Apr 25, 1997 · N13067 · Doug DC1030 · Elevator, Plate/SkinSDR CALA9700654Angle · crackedINSPECTION FOUND A 2 CRACK IN FORMED ANGLE AT FUSELAGE SKIN, STA 1421, LONGERON 31L TO 32L, AT LT WING INBOARD TOP FILLET AREA. THE ANGLE WAS REMOVED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, VOL II, 51-31-01, VOL II, AND 51-33-01, VOL 1Apr 25, 1997 · N13067 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9601725Control Cable · brokenTHE AIRCRAFT ARRIVED IN EWR WITH THE RT MLG DOOR HANGING DOWN. MAINTENANCE FOUND THE RT MLG DOOR FOLLOW-UP CABLE BROKEN. THE CABLE WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.Dec 3, 1996 · N13067 · Doug DC1030 · Landing Gear Door Retract SectionSDR CAL960217Longeron · corrodedKUL - INSPECTION FOUND CORROSION ON LONGERON 31L AT STATION 1405. THE CORROSION WAS REMOVED AND A DOUBLE ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03217 AND SRM 53-14-01. (M)Jan 28, 1996 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CAL960216Longeron · corrodedKUL - INSPECTION FOUND LONGERON 30L CORRODED AT STATION 1436. THE LONGERON WAS REPAIRED IAW ECRA 5310-03218 AND SRM 53-14-01. (M)Jan 28, 1996 · N13067 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CAL960219Stiffener · corrodedKUL - INSPECTION FOUND LATERAL STIFFENER CORRODED AT FS 1841 RBL 42 AND LBL 28. THE LATERAL STIFFENERS WERE REPLACED IAW SRM 53-16-01. (M)Jan 26, 1996 · N13067 · Doug DC1030 · Fuselage Miscellaneous Structure
Back to N13067, cancelled Apr 27, 2005