# Service difficulty reports: N590CA, cancelled Jan 25, 2018

A list on [N590CA, cancelled Jan 25, 2018](https://openairdocs.org/deregistered/N590CA-2018-01-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR P9IA97009](https://openairdocs.org/sdr/P9IA97009.md): Battery Pack · discharged · Apr 3, 1997 · N590CA · Boeing 727231 · Emergency Lighting
  > RIGHT AFT OVERWING EMERGENCY LIGHT FAILED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD PER MM 33-50-11. (M)
- [SDR P9IA97007](https://openairdocs.org/sdr/P9IA97007.md): Connector · loose · Feb 18, 1997 · N590CA · Boeing 727231 · Emergency Lighting
  > FAA 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)
- [SDR P9IA97006](https://openairdocs.org/sdr/P9IA97006.md): Connector · corroded · Feb 17, 1997 · N590CA · Boeing 727231 · Emergency Lighting
  > AFT 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)
- [SDR P9IA97005](https://openairdocs.org/sdr/P9IA97005.md): Battery · discharged · Feb 6, 1997 · N590CA · Boeing 727231 · Emergency Lighting
  > AFT PATH LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IN CENTER CEILING BETWEEN STATION 1030-1050 IAW MM 33-50. OPS CHECKS NORMAL. (M)
- [SDR P9IA97002](https://openairdocs.org/sdr/P9IA97002.md): Sensing Loop · shorted · Jan 6, 1997 · N590CA · Boeing 727231 · Overheat Detection
  > NR 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)
- [SDR P9IA97001](https://openairdocs.org/sdr/P9IA97001.md): Bleed Valve · stuck · Jan 3, 1997 · N590CA · Boeing 727231 · Compressor Bleed Valve
  > NR 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)
- [SDR N3VR96154](https://openairdocs.org/sdr/N3VR96154.md): T-Chord · corroded · Dec 4, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > LEFT 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 5
- [SDR N3VR96153](https://openairdocs.org/sdr/N3VR96153.md): Retainer · cracked · Dec 4, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer Structure
  > LEFT 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 I
- [SDR N3VR96157](https://openairdocs.org/sdr/N3VR96157.md): Igv Case · cracked · Dec 2, 1996 · N590CA · Boeing 727231 · Turbine Engine Compressor Section
  > INLET 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)
- [SDR N3VR96152](https://openairdocs.org/sdr/N3VR96152.md): Retainer · corroded · Sep 13, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer Structure
  > RIGHT 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-
- [SDR P91A096022](https://openairdocs.org/sdr/P91A096022.md): Fire Loop · shorted · Jun 25, 1996 · N590CA · Boeing 727231 · Fire Detection
  > FOUR 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.
- [SDR N3VR96016](https://openairdocs.org/sdr/N3VR96016.md): Floor Beam · corrosion · Feb 29, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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, INSTA
- [SDR N3VR96015](https://openairdocs.org/sdr/N3VR96015.md): Chord · corrosion · Feb 29, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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 P
- [SDR N3VR96020](https://openairdocs.org/sdr/N3VR96020.md): Floor Beam · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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 1505-10
- [SDR N3VR96017](https://openairdocs.org/sdr/N3VR96017.md): Stringer · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > REF 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 SR
- [SDR N3VR96014](https://openairdocs.org/sdr/N3VR96014.md): Beam · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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. FAB
- [SDR N3VR96013](https://openairdocs.org/sdr/N3VR96013.md): Angle · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > REF 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)
- [SDR N3VR96012](https://openairdocs.org/sdr/N3VR96012.md): Chord · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Horizontal Stabilizer Structure
  > REF 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 PER
- [SDR N3VR96011](https://openairdocs.org/sdr/N3VR96011.md): Seat Track · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > REF 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)
- [SDR N3VR96010](https://openairdocs.org/sdr/N3VR96010.md): Blkhd Fitting · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage Main, Bulkhead
  > REF 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)
- [SDR N3VR96005](https://openairdocs.org/sdr/N3VR96005.md): Seat Track · corrosion · Feb 28, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > REF 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)
- [SDR N3VR96019](https://openairdocs.org/sdr/N3VR96019.md): Intercostal · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > REF 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)
- [SDR N3VR96018](https://openairdocs.org/sdr/N3VR96018.md): Floor Beam · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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)
- [SDR N3VR96009](https://openairdocs.org/sdr/N3VR96009.md): Seat Track · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > REF 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)
- [SDR N3VR96008](https://openairdocs.org/sdr/N3VR96008.md): Seat Track · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > REF 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)
- [SDR N3VR96007](https://openairdocs.org/sdr/N3VR96007.md): Skin · crack · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Plate/Skin
  > REF 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 REPAIR
- [SDR N3VR96006](https://openairdocs.org/sdr/N3VR96006.md): Floor Beam · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Floor Beam
  > REF 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)
- [SDR N3VR96001](https://openairdocs.org/sdr/N3VR96001.md): Stringer · corrosion · Feb 27, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > REF 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)
- [SDR N3VR96002](https://openairdocs.org/sdr/N3VR96002.md): Intercostal · corrosion · Feb 26, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > REF 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 P
- [SDR N3VR96004](https://openairdocs.org/sdr/N3VR96004.md): Stringer · cracked · Feb 17, 1996 · N590CA · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > REF 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)
- [SDR N3VR96003](https://openairdocs.org/sdr/N3VR96003.md): Fitting · cracked · Feb 17, 1996 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > REF 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)
- [SDR 95ZZZX1943](https://openairdocs.org/sdr/95ZZZX1943.md): Life Raft · low pressure · Apr 5, 1995 · N590CA · Boeing 727231 · Life Raft
  > DURING 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.
- [SDR YAUA9502](https://openairdocs.org/sdr/YAUA9502.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR 95ZZZX1046](https://openairdocs.org/sdr/95ZZZX1046.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR 95ZZZX1045](https://openairdocs.org/sdr/95ZZZX1045.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR 95ZZZX1044](https://openairdocs.org/sdr/95ZZZX1044.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR 95ZZZX1043](https://openairdocs.org/sdr/95ZZZX1043.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR 95ZZZX1042](https://openairdocs.org/sdr/95ZZZX1042.md): Bolts · loose · Jan 25, 1995 · N590CA · Boeing 727231 · Leading Edge Devices
  > COMPLY 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 KIT
- [SDR YAUA9501](https://openairdocs.org/sdr/YAUA9501.md): Window Post · cracked · Jan 20, 1995 · N590CA · Boeing 727231 · Fuselage Miscellaneous Structure
  > TYPE 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,

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N590CA-2018-01-25/reports

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