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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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 INSTASDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR CALA0200304Intercostal · corrodedAFT PIT F/S 1136 TO 1155 LONGERON 30 INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-5.SDR 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.SDR CALA2000292IntercostalF/S 1212 LONGERON 28 RIGHT INTERCOATAL CORRODED 1"X1". INSTALLED NEW INTERCOSTAL IAW SRM 51-30-5.SDR CALA2000291IntercostalF/S 1193 LONGERON 28 RIGHT INTERCOSTAL CORRODED 20"X1". INSTALLED NEW INTERCOSTAL T & L ANGLES IAW SRM 51-30-5.SDR CALA2000290FrameAFT PIT, F/S 1041, LONGERON 30 FRAME ATTACH ANGLE CORRODED - 80". REPLACED FRAME ANGLE IAW SRM 51-30-5.SDR 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.SDR CALA2000284Skin · chafedMID CARGO DOOR LOWER AFT CORNER SKIN CHAFED. INSTALLED DOUBLER IAW SRM 51-30-1 AND 51-30-5.SDR 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.SDR CALA2000282Skin · dentedMID CARGO DOOR, OUTER SKIN HAS A SHARP DENT. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2, 52-05, FIG 1.SDR 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.SDR 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.SDR 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.SDR 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 IASDR 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.SDR CALA2000264SkinONE INCH DENT AT F/S 237, 17L-18L. REF. NON ROUTINE 4684047, REPAIRED DENT AT STA 229 PER ECRA 5330-03055.SDR 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.SDR CALA2000262Seat TrackCAPTAINS UPPER AND LOWER SEAT TRACKS WORN, REPAIRED AND REINSTALLED TRACKS IAW SRM 51-30-1 & 53-40-01.SDR 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.SDR 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.SDR 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.SDR 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 51-30-2SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR CALA0100490Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 2L TO 2R. REPAIRED IAW DRAWING SR09530003.SDR CALA0100488Battery Pack · dischargedINSPECTION FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.SDR 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.SDR 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.SDR 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.
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