N590CA, cancelled Jan 25, 2018

Service difficulty reports · 39

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 = 'N590CA' AND deregistration_id = 'N590CA-2018-01-25'
  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 P9IA97009Battery Pack · dischargedRIGHT AFT OVERWING EMERGENCY LIGHT FAILED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD PER MM 33-50-11. (M)Apr 3, 1997 · N590CA · Boeing 727231 · Emergency LightingSDR P9IA97007Connector · looseFAA ITEM ON RAMP CHECK IN MCO, AFT SECTION OF EMERGENCY PATH LIGHTING DIM. INSPECTED AFT SECTION OF PATH LIGHTING AND FOUND END CONNECTOR PINS HAD MISSED FEMALE END. CLEANED AND CONNECTED AND OPS CHECKED PER MM 33-21-27. OPS CHECK GOOD. (M)Feb 18, 1997 · N590CA · Boeing 727231 · Emergency LightingSDR P9IA97006Connector · corrodedAFT EMERGENCY ESCAPE PATH LIGHTING VERY DIM. FOUND AFT FLOOR PATH LGIHT STRIP CENTER CONNECTION CORRODED. CLEANED CONTACTS SYSTEM OPS CHECKS GOOD IAW MM 33-21-27. (M)Feb 17, 1997 · N590CA · Boeing 727231 · Emergency LightingSDR P9IA97005Battery · dischargedAFT PATH LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IN CENTER CEILING BETWEEN STATION 1030-1050 IAW MM 33-50. OPS CHECKS NORMAL. (M)Feb 6, 1997 · N590CA · Boeing 727231 · Emergency LightingSDR P9IA97002Sensing Loop · shortedNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE STRUT SENSING LOOP IAW BOEING MM 26-14-1. PERFORMED ENGINE RUN-UP WITH BLEED AIR ON. OPS CHECKS GOOD ON GROUND IAW BOEING MM 71-00. (M)Jan 6, 1997 · N590CA · Boeing 727231 · Overheat DetectionSDR P9IA97001Bleed Valve · stuckNR 1 ENGINE LIGHT ON DURING CLIMB AT TAKEOFF POWER. POWER REDUCTION LIGHT 'OUT'. REMOVED AND REPLACED NR 1 ENGINE BLEED VALVE AND REROUTED STRUT OVERHEAT LOOP. PERFORMED LEAK CHECK, LEAK CHECKED OK. NO OVERHEAT LIGHT IAW 727 MM 36-10-00. (M)Jan 3, 1997 · N590CA · Boeing 727231 · Compressor Bleed ValveSDR N3VR96154T-Chord · corrodedLEFT NOSE WHEEL WELL T-CHORD CORRODED BEYOND LIMITS. CUT OUT SKIN APPROX 14 INCHES AT STATION 280 LEFT FOR REPLACEMENT OF LT NOSE WHEEL WELL T-CHORD. REPLACED T-CHORD AND SPLICED NEW SKIN IAW DWG 96-0804 DATED AUGUST 19, 1996. REF SRM 51-10-6, 51-10-2 AND 5Dec 4, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous StructureSDR N3VR96153Retainer · crackedLEFT HORIZ STABILIZER LOWR T/E SEAL RETAINER HAS SEAL RIVETS LOOSE AND LIGHT SURFACE CORROSION BETWEEN ELEVATOR HINGES NR 3 THROUGH NR 6 POSITION. CRACKS FOUND RUNNING FROM LOOSE RIVET HOLES. BLENDED OUT DAMAGED AREA, REMOVED CORROSION, RELOCATED FASTENERS IDec 4, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer StructureSDR N3VR96157Igv Case · crackedINLET GUIDE VANE CASE WAS CRACKED AT A PREVIOUS WELD REPAIR. THE INLET GUIDE VALVE (I/G/V) CASE WAS REPLACED IAW MM 72-00 AND THE NR 1 BEARING WAS REPLACED IAW MM 72-00-23. (M)Dec 2, 1996 · N590CA · Boeing 727231 · Turbine Engine Compressor SectionSDR N3VR96152Retainer · corrodedRIGHT HORIZ STAB T/E SEAL RETAINER, SEAL LOOSE AT ELEVATOR HINGES NR 2, NR 5 AND NR 7 POSITIONS, CRACKS FOUND RUNNING FROM LOOSE RIVET HEADS. BLENDED OUT DAMAGED AREAS, REMOVED CORROSION, RELOCATED FASTENERS IAW EO 96-1031, REF SRM 51-10-2, 51-30-2 AND 51-10-Sep 13, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer StructureSDR P91A096022Fire Loop · shortedFOUR MINUTES AFTER TAKEOFF STX AT 2145, HAD A FIRE WARNING, NR 3 ENGINE MADE SHUTDOWN PER PROCEDURES. RETURNED TO STX. TROUBLE-SHOT SYSTEM, NR 3 FOUND FIRE DETECTION LOOP BAD. REMOVED AND REPLACED FIRE DETECTION LOOP. CHECKS GOOD MM 26-12-00 A AND B SYSTEM.Jun 25, 1996 · N590CA · Boeing 727231 · Fire DetectionSDR N3VR96016Floor Beam · corrosionREF N/R 3691, FS 312, 37 INCHES RIGHT OF C/L FLOOR BEAM HAS CORROSION BEYOND BLEND LIMITS. REMOVED DAMAGED SECTION OF FLOOR BEAM IAW SRM 51-30-2. FABRICATED MATERIAL FROM TM 560-23934 PICKED UP HOLES IAW SRM 51-10-1, TREATED AND PRIMED IAW SRM 51-10-2, INSTAFeb 29, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96015Chord · corrosionREF N/R 3699, FS 1030, 20 INCHES LT OF C/L FLOOR BEAM CORROSION BEYOND BLEND OUT LIMITS UPPER CHORD. REMOVED CORRODED SECTION OF FLOOR BEAM, FABRICTED REPAIR PARTS IAW SRM 53-10-8 USING MATERIAL BAC 1505-100617, 7075-T73 TREATED AND PRIMED BEAM AND REPAIRED PFeb 29, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96020Floor Beam · corrosionREF N/R 3626, CORROSION STATION 344 AT CLIP NUT HOLE FLOOR BEAM PANEL NR 2 FORWARD EDGE BOTH SURFACES. REMOVED CORROSION IAW SRM 51-10-6. INSPECTION FOUND OUT OF LIMITS, CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS IAW SRM 53-10-8-8-2A USING BAC 1505-10Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96017Stringer · corrosionREF N/R 3600, STRINGER 22 LT AT FS 1166 HAS CORROSION. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3, FABRICATED REPAIR PART USING STRINGER MATERIAL BAC 1498-142 AND BAC 1498-132 IAW SRM 53-10-3, TREATED ADN PRIMED IAW SRM 51-10-2 INSTALLED PARTS IAW SRFeb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/StringerSDR N3VR96014Beam · corrosionREF N/R 3658, SURFACE CORROSION ON FLOOR BEAM STATION 312 AT CLIP NUT HOLES FT OF COCKPIT DOOR (BOTH SURFACES). REMOVED CORROSION IAW SRM 51-10-6 AT 3 INCHES LT OF C/L AND AT 19 INCHES OF C/L MAX MATERIAL REMOVED .050, TREATED AND PRIMED IAW SRM 51-10-2. FABFeb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96013Angle · corrosionREF N/R 3629, FORWARD LAV AISLE SIDE WALL SUPPORT ANGLE CORRODED FORWARD SECTION. FABRICATED FLOOR SUPPORT FROM EXTRUSION 60-357 7075-T6 PRIMED IAW 51-10-2. INSTALLED IAW SRM 51-30-2. (M)Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous StructureSDR N3VR96012Chord · corrosionREF N/R 3642, RIGHT HORIZONTAL STABILIZER FRONT UPPER CHORD CORRODED STATION 170, 188, 195, 205 (INTERNAL). REMOVED CORROSION IAW SRM 51-10-6, FORWARD INFORMATION TO ENGINEERING MATERIAL. REMOVED DETERMINED TO BE ACCEPTABLE PER ENGINEERING, PREPARED AREA PERFeb 28, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer StructureSDR N3VR96011Seat Track · corrosionREF N/R 3591, SEAT TRACK NR 3 FS 344 TO 400 CORRODED. REMOVED NR 3 SEAT TRACK PICKED UP HOLES IN NEW SEAT TRACK P/N BAC 1520-792, TREATED AND PRIMED IAW 51-10-2. INSTALLED IAW SRM 51-30-2 AND 51-10-1. (M)Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach FittingsSDR N3VR96010Blkhd Fitting · corrosionREF N/R 3592, FS 1183 BULKHEAD TO FLOOR ATTACH FITTING IS BLOWN IN CORNER LEFT SIDE STRINGER 17 LEFT. REMOVED AND REPLACED FITTING IAW SRM 51-30-2. (M)Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, BulkheadSDR N3VR96005Seat Track · corrosionREF N/R 3589 - SEAT TRACK CORROSION LEFT OUTBOARD TRACK F/S 990. TRANSFERRED FASTENER HOLES TO NEW SEAT TRACK SECTION P/N BAC 1520-792, TREATED AND PRIMED, INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. (M)Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach FittingsSDR N3VR96019Intercostal · corrosionREF N/R 3572, INTERCOSTAL FORWARD OF STATION 420 CORROSION BETWEEN SEAT TRACK NR 3 AND NR 4. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-10-4 AND 51-30-2 USING EXTRUSION 1506-3418, 7075-T6. INSTALLED INTERCOSTAL IAW SRM 51-30-2. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous StructureSDR N3VR96018Floor Beam · corrosionREF N/R 3559, FLOOR BEAM HAS CORROSION STATION 344 C/L LT AND RT 10 INCHES. FABRICATED T-CAP IAW SRM 51-40-4 USING T-EXTRUSION 60-23934 TREATED AND PRIMED, INSTALLED IAW SRM 51-40-4. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96009Seat Track · corrosionREF N/R 3561, SEAT TRACK HAS CORROSION STATION 344 TO 440 TRACK NR 4. REMOVED SEAT TRACK, DRILLED OUT NEW SEAT TRACK SECTION P/N BAC 1520-792, TREATED AND PRIMED IAW 51-10-2, INSTALLED IAW SRM 51-30-2 AND 51-10-1. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach FittingsSDR N3VR96008Seat Track · corrosionREF N/R 3562, SEAT TRACK NR 5 HAS CORROSION STATION 420 TO 460. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 TREATED AND PRIMED, INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach FittingsSDR N3VR96007Skin · crackREF N/R 3563, FUSELAGE SKIN CRACK STATION 430 RIGHT BETWEEN STRINGER 16 AND 17 RT. REMOVED DAMAGED SKIN IAW SRM 53-30-3, FABRICATED INTERNAL DOUBLER FROM 7575-T6 .090 8 INCHES BY 12 INCHES IAW SRM 53-30-3, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIRFeb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Plate/SkinSDR N3VR96006Floor Beam · corrosionREF N/R 3560, FLOOR BEAM CORROSION STATION 380 LEFT OF SEAT TRACK NR 4 APPROXIMATELY 12 INCHES AREA. REMOVED CORROSION IAW SRM 51-10-6 NEG MATERIAL REMOVED, TREATED AND PRIMED IAW SRM 51-10-2. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor BeamSDR N3VR96001Stringer · corrosionREF N/R 3498, STRINGER 21LT AT BS 1050 HAS CORROSION BLOWOUT. CORRODED STRINGER REMOVED FABRICATED REPAIR PARTS FROM 12 FEET BAC-1498-132, .063 EXTRUSION AND 12 FEET BAC 1498-143, .050 EXTRUSION IAW SRM 53-10-3. INSTALLED REPAIR PARTS IAW SRM 53-10-3. (M)Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/StringerSDR N3VR96002Intercostal · corrosionREF N/R 3465, FLOOR INTERCOSTAL BLOWN OUT CORROSION AT BS 1020 APPROXIMATELY 30 INCHES LEFT OF CENTER LINE. FABRICATED NEW PART, 21 INCHES PIECE OF 130188-1-1 7075-T6511 T-EXTRUSION AND 12 INCH BY 21 INCH 7075-T6 .125 IAW SRM 51-10-1, ALODINE AND PRIMED AND PFeb 26, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous StructureSDR N3VR96004Stringer · crackedREF N/R 3268, STRINGER CRACKED AFT OF B/S 720B, RT STRINGER 15 RT AT WING FLOOD LIGHT HOUSING. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS FROM 7075-T6 IAW SRM 53-10-3. INSTALLED PARTS IAW SRM 53-10-3. (M)Feb 17, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/StringerSDR N3VR96003Fitting · crackedREF N/R 3269, FITTING CRACKED UNDER RIGHT FORWARD EMERGENCY EXIT DOOR FRAME AFT OF B/S 760, FRAME. FABRICATED FITTING FROM 7078-T6 LOCATED AND DRILLED TO AIRCRAFT, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED IAW SRM 51-30-2. (M)Feb 17, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous StructureSDR 95ZZZX1943Life Raft · low pressureDURING AN INSPECTION OF LIFE RAFT BOTTLE PRESSURES, THE RAFT LOCATED IN THE OVERHEAD AT RIGHT OVERWING EXIT WAS FOUND TO HAVE ONE BOTTLE WITH LOW PRESSURE. THE RAFT WAS REMOVED AND A SERVICEABLE RAFT WAS INSTALLED.Apr 5, 1995 · N590CA · Boeing 727231 · Life RaftSDR YAUA9502Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 1 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR 95ZZZX1046Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 8 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR 95ZZZX1045Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 5 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR 95ZZZX1044Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 4 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR 95ZZZX1043Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 3 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR 95ZZZX1042Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 2 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231 · Leading Edge DevicesSDR YAUA9501Window Post · crackedTYPE SERVICE '2B' CHECK. X-RAY OF WINDOW POST N-F, AD 93-05-17, REF. SB 737-53-0086. FOUND CRACK AT 6TH FASTENER DOWN TO EDGE OF POST N-F, RIGHT HAND. EDDY CURRENT USED TO VERIFY CRACK. MODIFICATION/REPAIR DONE IAW SB 727-53-0086, REV 2, PART II, PAGE 24, Jan 20, 1995 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
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