N16894

Service difficulty reports not matched to an aircraft · 47

They name N16894, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N16894' AND registry_match IS NULL
  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 CALA0200221Bulkhead · corrodedINSPECTION FOUND BULKHEAD CORRODED FORWARD OF FIRST OFFICER'S I/B SEAT TRACK AT FS 120, LBL 30 TO RBL 58. THE BULKHEAD WAS REPAIRED IAW SRM 53-01, FIGURE 2.Apr 19, 2002 · N16894 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0200214Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED UNDER R/H RAIN GUTTER AT FS 1510. THE GUTTER WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-20-1.Apr 17, 2002 · N16894 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0200213Floor Panel · splitINSPECTION FOUND CHANNEL ON BACK OF MAIN CABIN DECK FLOOR PANEL AT FS 218-256, RBL 44-58, COMING LOOSE AND PANEL WAS SPLITTING AT THE END. THE PANEL AND CHANNEL WERE REPAIRED IAW SRM 51-70-2 AND 51-20-1.Apr 17, 2002 · N16894 · Doug DC982 · Fuselage Floor PanelSDR CALA0200204Wire · disconnectedINSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT 14R AND 15R. TROUBLESHOOTING FOUND CONNECTOR AT 15R HAD A PUSHED PIN. THE PIN WAS RESEATED IAW MM 20-50-01. SEAT 14R HAD GROUND WIRE PULLED FROM CONNECTOR SPLICE. THE GROUND WIRE AT CONNECTOR WAS RESEATED IApr 15, 2002 · N16894 · Doug DC982 · Emergency LightingSDR CALA0200203Skin · dentedINSPECTION FOUND VENTRAL STAIRS EXTERNAL SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 52-01, FIGURE 1 AND 51-10-3.Apr 13, 2002 · N16894 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0200202Wire · brokenINSPECTION FOUND L-2 DOOR EXIT LIGHT INOPERATIVE. CHECKED WIRING AT AFT DROP CEILING AND FOUND POWER WIRE BROKEN AT WIRE CONDUIT. THE POWER WIRE WAS RESPLICED. NO GROUND WIRE WAS FOUND GOING TO SIGN. CONNECTED GROUND WIRE AND OPERATIONAL CHECKS WERE GOOD IApr 13, 2002 · N16894 · Doug DC982 · Light System WiringSDR CALA0200201Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO AREA BETWEEN FS 769 AND 786, L27L-L28L. THE INTERCOSTAL WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.Apr 13, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200198Shear Tie · crackedINSPECTION FOUND A 1" CRACK IN SKIN TO FRAME SHEAR TIE AT STA 1307, LONGERON 15R LAV BULKHEAD. THE #2 ENGINE WAS REMOVED FOR ACCESS. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-04 AND 51-30-5. THE #2 ENGINE WAS REINSTALLED.Apr 13, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200199Fitting · corrodedINSPECTION FOUND GALLEY FITTING CORRODED AT STA 200-216, RBL 22, UPON REMOVAL OF SUBFLOOR WEB. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.Apr 12, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200195Skin · crackedINSPECTION FOUND A 1/2" CRACK IN THE R/H MLG I/B DOOR SKIN AT LOWER FORWARD EDGE. THE DOOR SKIN WAS REPAIRED IAW EA 9-5281-2-A0941 AND ECRA 5281-01020.Apr 11, 2002 · N16894 · Doug DC982 · Landing Gear DoorsSDR CALA0200191Web · corrodedINSPECTION FOUND FLOOR WEB CORRODED AT FS 120-133, LBL 28 TO RBL 84. THE O/B PILOT SEAT TRACK WAS REMOVED IAW SRM 51-30-1. THE FLOOR SUPPORT AND WEB WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.Apr 9, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200189Seat Track · corrodedINSPECTION FOUND COCKPIT SEAT TRACK CORRODED AT STA 110-120, RBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200188Seat Track · corrodedINSPECTION FOUND CAPTAIN'S I/B SEAT TRACK CORRODED AT STA 120-148, LBL 15. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200187Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 110-120, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200186Seat Track · corrodedINSPECTION FOUND R/H AND L/H FORWARD UPPER PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200185Seat Track · corrodedINSPECTION FOUND L/H AND R/H FORWARD UPPER CO-PILOT'S SEAT TRACKS CORRODED AND WORN. THE SEAT TRACKS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-05, FIGURE 92.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200184Floorbeam · corrodedINSPECTION FOUND UPPER CAP(ANGLE) OF FLOORBEAM CORRODED IN E&E COMPARTMENT OVERHEAD AT STA 120, RBL 15 TO RBL 30. THE ANGLE WAS REMOVED AND A NEW ANGLE AND REPAIR SPLICES WERE INSTALLED IAW SRM 51-10-4.Apr 6, 2002 · N16894 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0200183Angle · corrodedINSPECTION FOUND L-2 DOOR LOWER FORWARD DOOR JAMB L-ANGLE CORRODED AT STA 1138, 18L. THE SCUFF PLATE WAS REMOVED TO GAIN ACCESS IAW SRM 51-30-1. THE L-2 DOOR WAS REMOVED IAW MM 52-42-00. THE ANGLE AND FITTING WERE REMOVED AND A NEW ANGLE AND SPLICE WAS INSTALLApr 6, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200182Skin · dentedINSPECTION FOUND R/H I/B FLAP O/B VANE LOWER SKIN SURFACE DENTED. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-1.Apr 6, 2002 · N16894 · Doug DC982 · Wing, Plate/SkinSDR CALA0200180Seat Track · corrodedINSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT STA 237, RBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200179Longeron · crackedINSPECTION FOUND A 1.75" CRACK AT LOWER RADIUS OF LONGERON 20R EXTERNAL FITTING, FS 1003. THE CRACKED AREA WAS REMOVED IAW EA 9-5310-2-A0942 AND HFEC REVEALED NO FURTHER CRACKS IAW NTSPM 06-10-01. REPAIR PARTS WERE INSTALLED IAW EA 9-5310--2-A0942.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200177Support · crackedINSPECTION FOUND A 2" CRACK IN SUPPORT IN AFT ACCESSORY COMPARTMENT BETWEEN CANTED FRAMES STA 1485 AND 1497 AND BELOW LEFT AIRSTAIR TORQUE TUBE. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, AND 51-10-3.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200176Skin · gougedINSPECTION FOUND R/H WING I/B T/E FLAP PANEL #1613C SKIN NICKED AND GOUGED. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-3.Apr 4, 2002 · N16894 · Doug DC982 · Trailing Edge FlapsSDR CALA0200175Skin · crackedINSPECTION FOUND FORWARD EDGE OF FORWARD CARGO DOOR SKIN CRACKED AND BENT JUST ABOVE LOCK MECHANISM AND SEAL. THE CRACK MEASURED 0.4" LONG. THE EXISTING FASTENERS WERE REMOVED, THE CRACK WAS STOP DRILLED, AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 52-05, Apr 4, 2002 · N16894 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0200174Fitting · corrodedINSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 155, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-2.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200173Floor Panel · corrodedINSPECTION FOUND FLOOR PANEL CORRODED AT STA 180, LBL 10 - RBL 55. THE CORRODED DOUBLER WAS REMOVED FROM THE WEB AND A REPAIR DOUBLER WAS INSTALLED.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage Floor PanelSDR CALA0200172Seat Track · corrodedINSPECTION FOUND L/H I/B SEAT TRACK CORRODED FROM STA 1098-1174. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, 51-30-5, AND 53-05, FIGURE 4.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200171Floor Panel · crackedINSPECTION FOUND 1 INCH CRACKS AT FLOOR PANEL INSERTS, FS 1003. THE FLOOR PANEL WAS REPAIRED.Apr 4, 2002 · N16894 · Doug DC982 · Fuselage Floor PanelSDR CALA0200170Skin · dentedINSPECTION FOUND L/H WING #1 I/B FLAP VANE DENTED AND PUNCTURED. THE DAMAGED AREA OF SKIN WAS CUT OUT. FILLERS AND A DOUBLER WERE INSTALLED IAW SRM 57-03 AND 51-70-2.Apr 4, 2002 · N16894 · Doug DC982 · Wing, Plate/SkinSDR CALA0200156Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1146, LBL 40. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-10-3.Mar 27, 2002 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200154Support · corrodedINSPECTION FOUND FORWARD BULKHEAD LOWER CENTER SUPPORT FRAME HAD CLIP-NUTS AND ATTACH HOLES CORRODED IN MID CARGO COMPARTMENT AT STA 541. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.Mar 27, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200153Pan · corrodedINSPECTION FOUND PAN CORRODED AT FORWARD CARGO DOOR CUTOUT AREA, STA 370-420. THE CORROSION WAS BETWEEN SCUFF PLATE AND JAMB. THE PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44.Mar 27, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200151Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN MID CARGO COMPARTMENT AT FS 769-786 BETWEEN L27R AND 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Mar 27, 2002 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100452Wire Rope · frayedTHE TAIL CONE DID NOT RELEASE WHEN PULLED FROM AFT ENTRANCE DOOR. THE TAIL CONE CABLE WAS FOUND FRAYED. THE CABLE WAS REPLACED AND A TAIL CONE ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.May 9, 2001 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100444Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER FLANGE OF RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463 JUST FORWARD OF VERTICAL STABILIZER REAR SPAR PLANE. A REPAIR DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.May 5, 2001 · N16894 · Doug DC982 · Fuselage, Stabilizer Attach FittingsSDR CALA0100438Channel · corrodedMID BAG BIN DOOR JAMB Z CHANNEL HAS CORROSION AROUND HI-SHEARS. INSTALLED DOUBLER AND SPACER PER SRM 53-05 FIG 63.May 3, 2001 · N16894 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100040Strut · inoperativeTHE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED ACCOMPANIED BY NOISE AND BUFFETING AFTER TAKEOFF FROM ATL. THE AIRCRAFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NLG STRUT WAS REPACKED IAW MM 32-21-02. LEAK CHECKS WERE GOOD. A NOSE GEAR RETRAJan 16, 2001 · N16894 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA9900074Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR SKIN AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-05, FIGURE 32.Jan 23, 1999 · N16894 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900038Beltframe · corrodedHEAVY CORROSION ON LOWER FORWARD FLANGE AND FWD FACE OF BELT FRAME AT STA 1322 L28 TO R28. REPAIRED PER SRM 53-03.Jan 21, 1999 · N16894 · Doug DC982 · Fuselage Main, FrameSDR CALA9900030Seat Track · corrodedCORROSION ON LEFT INBOARD SEAT TRACK STA 1136 TO 1155. REPAIRED PER SRM 53-05.Jan 19, 1999 · N16894 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900027Skin · corrodedFWD WATER DRAIN MAST MOUNT STRUCTURE HAS CORROSION INSIDE E & E COMPARTMENT STA 198 RIGHT OF CENTER. REMOVED AND REPLACED INTERCOSTAL, DOUBLER AND DRAIN MAST PER SRM 51-30-2.Jan 19, 1999 · N16894 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900025Beam · crackedFORWARD SERVICE DOOR HORIZONTAL BEAM HAS 4 CRACKS IN RADIUS WHERE LOWER HINGE ATTACHES. REPLACED HORIZONTAL BEAM PER SRM 51-30-2.Jan 19, 1999 · N16894 · Doug DC982 · Service DoorsSDR CALA9900063Skin · dentedFORWARD FUSELAGE SKIN SCRATCHED AND DENTED STA 218 TO 225 BETWEEN LONG 15L AND 18L. REPAIRED PER EC/RA 5330-02445.Jan 16, 1999 · N16894 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9801588Hyd Line · leakedSMOKE APPEARED IN THE CABIN AFTER TAKEOFF AND BEGAN CLEARING WITHIN 2-3 MINUTES. THE SMOKE HAD COMPLETELY DISSIPATED WITHIN 10-15 MINUTES. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE IN THE AFT CARGO COAug 31, 1998 · N16894 · Doug DC982 · Hydraulic System, MainSDR CALA9801326Retract Mech · malfunctionedTHE NLG DID NOT RETRACT AFTER TAKEOFF. BOTH THE RED NOSE GEAR LIGHT AND YELLOW GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FAULT WAS ACCOMPANIED BY LOUD WIND NOISE AND VIBRATION. THE GEAR WAS CYCLED AND THE NOSE GEAR RETRACTED WITH GOOD INDICATIONS. THEJul 23, 1998 · N16894 · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CALA9601682Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN ABOVE AND BELOW HOLD OPEN HOOK. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01340 AND SRM 52-01.Nov 6, 1996 · N16894 · Doug DC982 · Service DoorsSDR CAL950027Latches · lack of lubeHOU - THE TAIL CONE INTERIOR RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE LATCHES WERE LUBRICATED AND THE INTERIOR RELEASE HANDLE PULL FORCE CHECKED GOOD PER MM 53-50-00. (X)Jan 8, 1995 · N16894 · Doug DC982 · Aerodynamic Fairings
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