N16895

Service difficulty reports not matched to an aircraft · 65

They name N16895, 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 = 'N16895' 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 CALA0200321Battery Pack · dischargedTHE OVERHEAD EMERGENCY LIGHTS AT ROW 5-9 STAYED ON WHEN POWER WAS SECURED DURING TEST. THE EMERGENCY LIGHT B5-101 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.May 27, 2002 · N16895 · Doug DC982 · Emergency LightingSDR CALA0200320Wire · brokenINSPECTION FOUND THE L-2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE IAW STANDARD WIRING PRACTICES 20-10-03 AND OPEARTION CHECKED GOOD IAW MM 33-53-00.May 26, 2002 · N16895 · Doug DC982 · Emergency LightingSDR CALA0200319Skin · dentedINSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 1212, L29L TO L29R. THE AREA WAS REPAIRED IAW ECRA 5331-01114 AND EA 9-5330-2-A0954.May 24, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0200318Frame · corrodedINSPECTION FOUND FRAME CORRODED IN AFT PIT AT STA 1322, RBL 29-30. REMOVED TWO INTERCOSTALS AND TWO BULKHEAD ATTACH ANGLES TO GAIN ACCESS TO FRAME. INSTALLED NEW FRAME IAW SRM 51-30-2 AND 51-30-5. REINSTALLED INTERCOSTALS AND BULKHEAD ATTACH ANGLES. ALSO INSTAMay 24, 2002 · N16895 · Doug DC982 · Fuselage Main, FrameSDR CALA0200317Frame · corrodedAFT PIT STATION 1322 - 1309 AT L28 - L27 FRAME CORRODED. REMOVED FABRICATED AND REINSTALLED FRAME PER SRM 53-01 FIG1, 51-30-2, 51-30-5, AND 51-10-03.May 23, 2002 · N16895 · Doug DC982 · Fuselage Main, FrameSDR CALA0200316Web · corrodedL2 DOORWAY CUSP WEB CORRODED LBL 44 TO LBL 54 AT STATION FS 1168. REMOVED AND REPLACED WEB AND STIFFENER PER SRM 51-30-2 AND 51-30-5.May 23, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200315Web · corrodedAFT PIT WEB CORRODED AT STATION 1322 - 1309 R28 - R27. REMOVED, FABRICATED AND REINSTALLED INTERCOSTAL PER SRM 51-30-5 AND 51-30-2.May 23, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200312Trim Tab · gougedRIGHT AILERON CONTROL TAB UPPER SURFACE GOUGED. REMOVED, REPAIRED, AND BALANCED CONTROL TAB PER MM 27-10-02, SRM 51-70-1, AND SRM 57-50-1. REINSTALLED PER MM 27-10-02.May 21, 2002 · N16895 · Doug DC982 · Aileron TabsSDR CALA0200311Skin · dentedLEFT ELEVATOR LOWER SKIN DENTED. REMOVED ELEVATOR, REPAIRED AND BALANCED PER SRM 55-03 FIG 14, 55-20-2. REINSTALLED PER MM 27-30-02 AND 27-30-00.May 21, 2002 · N16895 · Doug DC982 · Elevator, Plate/SkinSDR CALA0200310Frame · chafedTAIL COMPARTMENT STATION 1401 AT LONGERON 21 R FRAME HAS DEEP CHAFE. BLENDED DAMAGE AND INSTALLED REPAIR PER SRM 51-30-2, 51-30-5, AND 53-03 FIG 4.May 20, 2002 · N16895 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200309Frame · chafedAFT ACCESSORY COMPARTMENT FRAME AT STATION 1380 LEFT SIDE HAS CHAFED FRAME WEB. CUT OUT DAMAGED AREA OF WEB, FABRICATED AND INSTALLED REPAIR PER SRM 53-01 FIG 94.May 20, 2002 · N16895 · Doug DC982 · Fuselage Main, FrameSDR CALA0200308Rib Doubler · crackedHORIZONTAL STABILIZER RIGHT INBOARD LEADING EDGE OF ELEVATOR INTERNAL RIB DOUBLER CRACKED BELOW DUCT COUPLING. REMOVED AND REPLACED RIB DOUBLER PER SRM 51-30-2.May 20, 2002 · N16895 · Doug DC982 · Horizontal Stabilizer, Spar/RibSDR CALA0200302Seat Track · corrodedLEFT OUTBOARD SEAT TRACK HAS EXFOLIATION CORROSION STATION 1174 TO 1309. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-5 AND 51-30-1.May 20, 2002 · N16895 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200304Intercostal · corrodedAFT PIT F/S 1136 TO 1155 LONGERON 30 INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-5.May 17, 2002 · N16895 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200303Seat Track · wornFIRST OFFICER UPPER AND LOWER SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-1, 51-30-2, AND 51-10-4.May 17, 2002 · N16895 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2000292IntercostalF/S 1212 LONGERON 28 RIGHT INTERCOATAL CORRODED 1"X1". INSTALLED NEW INTERCOSTAL IAW SRM 51-30-5.May 16, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000291IntercostalF/S 1193 LONGERON 28 RIGHT INTERCOSTAL CORRODED 20"X1". INSTALLED NEW INTERCOSTAL T & L ANGLES IAW SRM 51-30-5.May 15, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000290FrameAFT PIT, F/S 1041, LONGERON 30 FRAME ATTACH ANGLE CORRODED - 80". REPLACED FRAME ANGLE IAW SRM 51-30-5.May 15, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000289FrameTAIL COMPARTMENT RH SIDE STA 1446 AT LONGERON 18R FRAME HAS DEEP 1"X1" CHAFE. INSTALLED ANGLE AND FILLER IAW SRM 51-30-5, 51-30-2, 51-70-5, FIG 1.May 15, 2002 · N16895 · Doug DC982 · Fuselage Main, StructureSDR CALA2000284Skin · chafedMID CARGO DOOR LOWER AFT CORNER SKIN CHAFED. INSTALLED DOUBLER IAW SRM 51-30-1 AND 51-30-5.May 13, 2002 · N16895 · Doug DC982 · Cargo/Baggage DoorsSDR CALA2000283SkinSKIN DAMAGED AFT OF PITOT TUBE AT STA 76 R/S FWD OF COCKPIT WINDOW 3"X4". INSTALLED CLASS II REPAIR IAW SRM 53-04 FIG 12B.May 13, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA2000282Skin · dentedMID CARGO DOOR, OUTER SKIN HAS A SHARP DENT. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2, 52-05, FIG 1.May 13, 2002 · N16895 · Doug DC982 · Cargo/Baggage DoorsSDR CALA2000281Frame · chafedTAIL COMPARTMENT STA 1418 AT LONGERON 15R FRAME HAS DEEP CHAFE. INSTALLED REPAIR AND SHIMS IAW SRM 51-30-2, 51-30-5, 53-03, FIG 4.May 13, 2002 · N16895 · Doug DC982 · Fuselage Main, FrameSDR CALA2000270WebCUSP WEB L/S AFT OF L-2 DOOR IS CORRODED 20"X38". REMOVED WEB IAW SRM 53-01. INSTALLED WEB IAW SRM 51-30-2 & 51-30-5, 53-01 FIG 1.May 9, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000269Shear TieAFT PIT F/S 1193 LONGERON 30 SHEAR TIE IS CORRODED 0.5 INCHES. REMOVED AND REINSTALLED NEW SHEAR TIE IAW SRM 51-30-2.May 9, 2002 · N16895 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA2000268Seat TrackSEAT TRACK AT F/S 390 RH O/B IS HEAVILY CORRODED APPROXIMATELY 4"X19'. REMOVED AND REINSTALLED AIR GRILL F/S 200-484 RH O/B IAW SRM 51-30-1. REMOVED AND REINSTALLED FLOOR PANELS F/S 256-465 RH O/B IAW SRM 51-30-1. INSTALLED NEW SEAT TRACK, SPLICE, & FITTING IAMay 9, 2002 · N16895 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2000265Seat TrackCABIN FLOOR SEAT TRACK RBL 24 F/S 984 AND 1003 HAS SURFACE CORROSION. REMOVED SEAT RACK FROM STA 789-1032 RBL24 IAW SRM 51-30-5 AND INSTALLED NEW TRACK IAW SRM 53-05.May 7, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000264SkinONE INCH DENT AT F/S 237, 17L-18L. REF. NON ROUTINE 4684047, REPAIRED DENT AT STA 229 PER ECRA 5330-03055.May 7, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA2000263SkinRIGHT FORWARD FUSELAGE SKIN HAS 2" CREASE BETWEEN LONGERON 25 & LONGERON 26 AT APPROXIMATELY F/S 141. CUT OUT DAMAGE IAW SRM53-04 FIG 38, SHEET 34. INSTALLED REPAIR PARTS IAW SRM 53-04 FIG 38, SHEET 34.May 7, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA2000262Seat TrackCAPTAINS UPPER AND LOWER SEAT TRACKS WORN, REPAIRED AND REINSTALLED TRACKS IAW SRM 51-30-1 & 53-40-01.May 7, 2002 · N16895 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2000261IntercostalAFT PIT F/S 1146 TO 1155 BETWEEN LONGERON 30 & 29R INTERCOSTAL CORROSION 10 INCHES LONG. REMOVED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-5. REPLACED INTERCOSTAL IAW SRM 51-30-2 & 51-30-5.May 7, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000457Shear TieAFT PIT, F/S 1212 LONGERON 30 SHEAR TIE HAS 3 INCHES OF CORROSION. REMOVED SHEAR TIE IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2.May 6, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000259Shear TieF/S 1309 BETWEEN LONGERON 14R AND 15R SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD DOUBLER AND SHEAR TIE IAW SRM 51-30-4 AND 51-30-5. INSTALLLED SHEAR TIE, OUTER CHORD, DOUBLER AND STIFFER IAW SRM 51-30-5 AND 51-30-2.May 6, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA2000258Shear TieF/S 1309 BETWEEN LONGERON 41L AND 15L SHEAR TIE IS CRACKED 12 INCHES. REMOVED OUTER CHORD, DOUBLER AND SHEAR TIE IAW SRM 51-10-4 AND SRM 51-31-1. INSTALLED NEW SHEAR TIE IAW 51-10-4 AND 51-30-5. INSTALLED CHORD, DOUBLER AND STIFFNER IAW SRM 51-30-5 AND 51-30-2May 6, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200256Web · corrodedCUSP WEB IS CRACKED AND CORRODED AT STA 218 L18R RBL 56. CUT OUT CORRODED AREA IAW SRM 53-01, FIG 4. FABRICATED NEW DOUBLER IAW SRM 55-14-2 AND 53-01, FIG 4. INSTALLED DOUBLER IAW SRM 51-30-2.May 1, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200253Skin · damagedINSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 218 BETWEEN STRINGER 16R AND 17R. THE CREASED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 51-10-04 AND 53-04, FIGURE 38.Apr 29, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0200252Skin · damagedINSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 420 AND 446 BETWEEN STRINGER 22L AND 23L. THE CREASED AREAS WERE CUT OUT IAW SRM 53-04, FIGURE 38. A DOUBLER, FILLER, AND FINGER DOUBLER WERE INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38.Apr 29, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0200251Pan · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR PAN AT FORWARD AND AFT SIDE. THE CRACK WAS LOCATED AT RADIUS BELOW LATCH. THE CRACKS WERE STOP DRILLED IAW SRM 52-05, FIGURE 26A. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW SRM 52-05, FIGURE 26A.Apr 29, 2002 · N16895 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0200294Stiffener · corrodedVERTICAL STIFFENER FOR ATTACH ANGLE FOR FRAME CORRODED AT FS 1322 LONGERON 30. REMOVED AND REINSTALLED FABRICATED ANGLE PER SRM 51-30-2, 51-30-5, AND 53-01 FIG1.Apr 27, 2002 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200293Web · crackedFORWARD ENTRY DOOR JAMB INNER WEB CRACKED AT STATION 200 LONGERON 14L. INSTALLED REPAIR PER EC/RA 5314-01011 AND EA 9-5314-2-A0950.Apr 26, 2002 · N16895 · Doug DC982 · Fuselage Internal Mounting StructureSDR CALA0200238Skin · dentedINSPECTION FOUND TWO DENTS IN THE FUSELAGE SKIN AT STA 232, LONGERON 17R. THE DENTS WERE REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-30-2.Apr 24, 2002 · N16895 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100500Spar · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER LT FRONT SPAR AT CANTED FRAME STA 1388. THE CRACK WAS LOCATED NINE INCHES UP FROM BOTTOM END. THE SPAR WAS REPAIRED IAW ECRA 5510-01581.May 24, 2001 · N16895 · Doug DC982 · Vertical Stabilizer, Spar/RibSDR CALA0100498Clip · out of adjTHE CABIN AFT ENTRY DOOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982 · Aerodynamic FairingsSDR CALA0100497Clip · out of adjTHE EXTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982 · Aerodynamic FairingsSDR CALA0100496Clip · out of adjTHE INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982 · Aerodynamic FairingsSDR CALA0100490Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2L TO 2R. REPAIRED IAW DRAWING SR09530003.May 22, 2001 · N16895 · Doug DC982 · Fuselage Main, FrameSDR CALA0100488Battery Pack · dischargedINSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.May 21, 2001 · N16895 · Doug DC982 · Emergency LightingSDR CALA0100483Web · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN FORWARD LOWER SILL PLATE WEB AT AFT BAGGAGE BIN DOOR JAMB AREA. THE SILL PLATE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-0.May 20, 2001 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100478Pan · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN DOOR PAN CORRODED BETWEEN LOWER DOOR STOPS AT STA 389-408. SPLICES WERE INSTALLED ON FORWARD CARGO DOOR PAN IAW SRM 53-05, FIGURE 44.May 18, 2001 · N16895 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900006Cables · out of adjustTHE TAIL CONE RELEASE PULL WAS BELOW LIMITS WHEN USING INTERIOR OR EXTERIOR TAIL CONE HANDLE. THE CABLES, LATCHES AND CLIPS WERE ADJUSTED IAW MM 53-53-00.Jan 2, 1999 · N16895 · Doug DC982 · Aerodynamic Fairings
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