# Service difficulty reports: N590US, cancelled Sep 3, 2008

A list on [N590US, cancelled Sep 3, 2008](https://openairdocs.org/deregistered/N590US-2008-09-03.md).

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

- [SDR USAA920080718](https://openairdocs.org/sdr/USAA920080718.md): Stringer · corroded · Mar 28, 2008 · N590US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - MAJOR REPAIR-C-2-NR O3C21853002/10, CORROSION ON STRINGER 27L AT BS 962.2. REMOVED DAMAGED STRINGER & INSTALLED STRINGER SPLICE REPAIR IAW SRM 53-00-03 REPAIR 1.
- [SDR USAA920080720](https://openairdocs.org/sdr/USAA920080720.md): Skin · cracked · Mar 27, 2008 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 742, S24L. REPAIRED FUSELAGE SKIN, BS 742, S24L IAW USAIRWAYS TYPICAL REPAIR 53-33 REPAIR 31.
- [SDR USAA070285](https://openairdocs.org/sdr/USAA070285.md): Beam · chafed · Apr 18, 2007 · N590US · Boeing 737301 · Fuselage Main, Structure
  > FOUND CHAFED UPPER SURFACE BEAM CHORD IN LEFT A/C PACK BAY AT BS 548.85, 569.70, 637.50. FABRICATED AND INSTALLED REPAIR STRAPS PER EA 98602A, DEFECT SIZE:.6" BY.5" X.010" TO.025".
- [SDR USAA070284](https://openairdocs.org/sdr/USAA070284.md): Beam · chafed · Apr 18, 2007 · N590US · Boeing 737301 · Fuselage Main, Structure
  > FOUND BEAM CHAFED UPPER SURFACE OF RT AIR CONDITINING PACK PR BAC AT CHORD BS 614.90. INSTALLED REPAIR STRAP PER EA 98602A, DEFECT SIZE:.6" BY.5" BY.020"
- [SDR USAA070294](https://openairdocs.org/sdr/USAA070294.md): Access Panel · cracked · Apr 18, 2007 · N590US · Boeing 737301 · Nacelle/Pylon, Plate/Skin
  > LEFT PYLON ACCESS PANEL 5727L ON OUTER SKIN HAS CRACK. INSTALLED DOUBLER PER TR 54-30-07, DEFECT SIZE: 1 INCH.
- [SDR SB06091](https://openairdocs.org/sdr/SB06091.md): Splice · loose · Sep 14, 2006 · N590US · Boeing 737301 · Light System Wiring
  > CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON BOTTOM OF SEAT ROW 10 WILL NOT ILLUMINATE. MAINTENANCE TIGHTENED LOOSE SPLICE CONNECTION. OPERATIONAL CHECK GOOD.
- [SDR SB06039](https://openairdocs.org/sdr/SB06039.md): Light · broken · Apr 20, 2006 · N590US · Boeing 737301 · Emergency Lighting
  > ORF - THE SEAT MOUNTED EMERGENCY AISLE LIGHT WAS FOUND BROKEN ON SEAT 5C. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY AISLE LIGHT ASSEMBLY ON SEAT 5C. OPERATIONAL CHECK GOOD.
- [SDR USAA060449](https://openairdocs.org/sdr/USAA060449.md): Skin · cracked · Mar 13, 2006 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > LBS 727D, S-22L CRACK. INSTALLED FABRICATED DOUBLER IAW SRM 53-00-01, FIG 201 DETAIL XL, DEFECT SIZE: 2.750 INCH.
- [SDR USAA050886](https://openairdocs.org/sdr/USAA050886.md): Web · dented · Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > BFM - Q6 - WEB SKIN, 18 INCH X 2.0 INCH X.040 INCH DENT. BS 1016, BTW STR 24R-27R. FAB DOUBLER, FILLER, NEW SKIN SECTION, INSTALLED IAW EA AND SRM. (K)
- [SDR USAA050885](https://openairdocs.org/sdr/USAA050885.md): Vertical Support · cracked · Jul 18, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > BFM - Q6 - VERTICAL STIFFENER, 1.0 INCH RACK, CRACKED, WHEEL WELL FWD BULKHEAD 663 LBL 6.15. REPLACED STIFFENER IAW EA AND SRM. (K)
- [SDR USAA050799](https://openairdocs.org/sdr/USAA050799.md): Floorbeam · corroded · Jun 23, 2005 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED 48 INCHES LONG BY 2 INCHES WIDE BY.035 INCH DEEP, 2.5 INCHES LONG BY 2 INCHES WIDE BY.033, FLOORBEAM, BS 328, RBL 12 INCHES-50 INCHES AND LBL 50 INCHES. FABRICATED PARTS, INSTALLED NEW T-CHORD AND REPAIR ANGLE PER SRM 53-00-51, FIG
- [SDR USAA050798](https://openairdocs.org/sdr/USAA050798.md): Intercostal · cracked · Jun 23, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > BFM - FOUND WEB/INTERCOSTAL CRACKED.125 INCH, STATION 294.5 STRINGER 7L. INSTALLED ANGLE REPAIR OVER CRACKED AREA PER SRM 53-10-15, 51-70-13. (M)
- [SDR USAA050043](https://openairdocs.org/sdr/USAA050043.md): Reveal · cracked · Jan 4, 2005 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND REVEAL CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR REVEAL. REPLACED REVEAL PER EA 79744. (M)
- [SDR USAA040987](https://openairdocs.org/sdr/USAA040987.md): Skin · cracked · Dec 1, 2004 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01.
- [SDR SB04148](https://openairdocs.org/sdr/SB04148.md): Light · inoperative · Oct 24, 2004 · N590US · Boeing 737301 · Emergency Lighting
  > PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB04133](https://openairdocs.org/sdr/SB04133.md): Wire · faulty · Sep 26, 2004 · N590US · Boeing 737301 · Light System Wiring
  > CLT - MAINTENANCE REPORTED TWO EMERGENCY EXIT LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR USAA040400](https://openairdocs.org/sdr/USAA040400.md): Skin · cracked · Aug 9, 2004 · N590US · Boeing 737301 · Nacelle/Pylon, Plate/Skin
  > PIT - FOUND SKIN CRACKED.5 INCH, LEFT WING INBOARD OF PYLON L/E STATION 208. ROUTED CRACK OUT AND FILLED WITH SEALANT PER T/R 57-41-03. (M)
- [SDR USAA040401](https://openairdocs.org/sdr/USAA040401.md): Structure · torn · Aug 8, 2004 · N590US · Boeing 737301 · Cargo/Baggage Doors
  > PIT - FOUND CARGO DOOR WITH TORN LIGHTENING HOLE, FORWARD DOOR. FABRICATED DOUBLER PER TR 52-30-09. (M)
- [SDR USAA040399](https://openairdocs.org/sdr/USAA040399.md): Support Bracket · cracked · Aug 8, 2004 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND THREE BRACKETS CRACKED, FORWARD.1875 INCH, AFT 1 INCH AND 1.5 INCH, FORWARD ENTRANCE DOOR TOP LINER SUPPORT BRACKET NEAR TOPGATE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA040351](https://openairdocs.org/sdr/USAA040351.md): Stiffener · corroded · Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M)
- [SDR USAA040349](https://openairdocs.org/sdr/USAA040349.md): Frame · corroded · Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, Bulkhead
  > PIT - FOUND PRESSURE FRAME CORRODED.25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M)
- [SDR USAA040350](https://openairdocs.org/sdr/USAA040350.md): Bulkhead · corroded · Jul 21, 2004 · N590US · Boeing 737301 · Fuselage Main, Bulkhead
  > PIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED.5 INCH BY.5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M)
- [SDR USAASB03144](https://openairdocs.org/sdr/USAASB03144.md): Warning Light · illuminated · Aug 22, 2003 · N590US · Boeing 737301 · Landing Gear Position and Warning
  > AFTER DEPARTURE FROM MCI AND GEAR RETRACTION, CREW REPORTED VIA ACARS THAT THE NOSE GEAR RED LIGHT ILLUMINATED WITH THE MAIN GEAR INDICATION NORMAL. PER QUICK REF HANDBOOK PROCEDURES, CREW EXTENDED THE LANDING GEAR AND RECEIVED A NORMAL GEAR INDICATION OF THR
- [SDR USAA030137](https://openairdocs.org/sdr/USAA030137.md): Skin · cracked · Aug 9, 2003 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRAKED 3 INCHES, STATION 727E PLUS 2 INCHES S24R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB03103](https://openairdocs.org/sdr/USAASB03103.md): Switch · failed · Jul 6, 2003 · N590US · Boeing 737301 · Leading Edge Slat Control System
  > ON CLIMB-OUT FROM PHL, EN ROUTE TO ATL, CREW REPORTED THE LT WING INBOARD LEADING EDGE FLAP WOULD NOT RETRACT. CREW RECYCLED FLAPS TWICE WITH NO SUCCESS. FLIGHT RETURNED TO FIELD TO PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTE
- [SDR USAASB03095](https://openairdocs.org/sdr/USAASB03095.md): Battery Pack · inoperative · Jun 28, 2003 · N590US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERAITONAL CHECK GOOD. (M)
- [SDR USAASB02215](https://openairdocs.org/sdr/USAASB02215.md): Slide · binding · Nov 21, 2002 · N590US · Boeing 737301 · Escape Slide
  > PHL - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE HAD DIFFICULTY RELEASING FROM THE COMPARTMENT COVER. AFTER DEPLOYMENT, THE FORWARD UPPER CORNER WAS BOUND UP AGAINST THE DOOR. SLIDE WAS ROLLED AFT AND WOULD NOT
- [SDR USAA020388](https://openairdocs.org/sdr/USAA020388.md): Angle · cracked · Oct 4, 2002 · N590US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND VERT Z-ANGLE CRACKED IN HALF, FORWARD BULKHEAD LEFT SIDE W/W STATION 663 LBBL 6.15. INSTALLED TEMP SUPPORT ANGLE AND STRAPS PER EA 74968A. (M)
- [SDR USAA011070](https://openairdocs.org/sdr/USAA011070.md): Floorbeam · corroded · Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - FOUND BEAM CORRODED LBL 60 - RBL 18, STATION 344 CABIN FLOOR LBL 60 RBL 18. REPLACED UPPER CHORD PER SRM 53-10-51, FIG 205 AND EA 71720. (M)
- [SDR USAA011071](https://openairdocs.org/sdr/USAA011071.md): Beam · corroded · Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Structure (General)
  > PIT - FOUND BEAM CORRODED, LBL 48 INCHES-RBL 48 INCHES, STATION 986.5 CABIN FLOOR LBL 48 INCHES RBL 48 INCHES. REPLACED UPPER CHORD PER TYPICAL REPAIR 53-10-05. (M)
- [SDR USAA011072](https://openairdocs.org/sdr/USAA011072.md): Beam · corroded · Aug 12, 2001 · N590US · Boeing 737301 · Fuselage Structure (General)
  > PIT - FOUND BEAM CORRODED LBL 60 INCHES - RBL 60 INCHES, STATION 328 CABIN FLOOR LBL 60 INCHES, RBL 60 INCHES. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-51. (M)
- [SDR USAA010759](https://openairdocs.org/sdr/USAA010759.md): Skin · cracked · Jun 24, 2001 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED,INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 202. (M)
- [SDR USAASB01087](https://openairdocs.org/sdr/USAASB01087.md): Battery Pack · discharged · Mar 25, 2001 · N590US · Boeing 737301 · Emergency Lighting
  > CLT - PILOT REPORTED THAT NUMEROUS EMERGENCY EVACUATION LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCITED BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB0034](https://openairdocs.org/sdr/USAASB0034.md): Indicator · faulty · Nov 28, 2000 · N590US · Boeing 737301 · Trailing Flap Position Indicating System
  > PIT - FLT 1912 - ON DESCENT INTO PIT FROM PVD, CAPTAIN REPORTED A FLAP ASYMMETRY PROBLEM AS FLAPS WERE MOVED BETWEEN 1 AND 5 POSITION. LEFT FLAP POSITION INDICATED 1 AND RIGHT FLAP POSITION INDICATED 3. AFTER FOLLOWING QUICK REFERENCE HANDBOOK PROCEDURES, FL
- [SDR USAASB00316](https://openairdocs.org/sdr/USAASB00316.md): Transformer · malfunctioned · Nov 16, 2000 · N590US · Boeing 737301 · DC Rectifier/Converter
  > FLT 1514 - DEPARTING DCA EN ROUTE TO SYR, PILOT REPORTED ELECT SMELL IN COCKPIT AND CABIN WITH A/C ON THE GROUND AFTER ENG START AND THROUGHOUT T/O. AFTER 2,000 FT, MAIN ELECTRIC TRIM YOKE SWITCHES WERE INOP. CREW FOUND TRANSFORMER RECTIFIER NR 2 C/B POPPED.
- [SDR USAASB00076](https://openairdocs.org/sdr/USAASB00076.md): Battery Pack · discharged · Mar 21, 2000 · N590US · Boeing 737301 · Emergency Lighting
  > CLE - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHT ON THE RIGHT SIDE AISLE INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)
- [SDR USAA991209](https://openairdocs.org/sdr/USAA991209.md): Skin · cracked · Nov 1, 1999 · N590US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 380, DIRECTLY AFT OF EQUIPMENT COOLING DUCT OUTLET FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M)
- [SDR USAASB99197](https://openairdocs.org/sdr/USAASB99197.md): Battery Pack · discharged · Jul 25, 1999 · N590US · Boeing 737301 · Emergency Lighting
  > EWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERABLE OVER THE COCKPIT AND FORWARD ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)
- [SDR USAASB99143](https://openairdocs.org/sdr/USAASB99143.md): Connector · corroded · Jun 14, 1999 · N590US · Boeing 737301 · Overheat Detection
  > JAX - FLT 1469 - DURING CRUISE, AT APPROXIMATELY FL 350, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ELECTED TO DIVERT TO THE NEAREST STATION AT JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUTDOWN OCCURRED NOR WAS AN EMERGENCY DECLARED. MA
- [SDR USAASB98136](https://openairdocs.org/sdr/USAASB98136.md): Outflow Valve · failed · Jun 3, 1998 · N590US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND.
- [SDR 98ZZZM532](https://openairdocs.org/sdr/98ZZZM532.md): Press Controller · failed · Jun 3, 1998 · N590US · Boeing 737301 · Cabin Pressure Controller
  > PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND.
- [SDR 98ZZZM531](https://openairdocs.org/sdr/98ZZZM531.md): Outflow Valve · failed · Jun 3, 1998 · N590US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HORN BEGAN TO SOUND.
- [SDR USAASB98056](https://openairdocs.org/sdr/USAASB98056.md): Light · inoperative · Feb 24, 1998 · N590US · Boeing 737301 · Emergency Lighting
  > ORD - WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE FORWARD RIGHT EMERGENCY EVACUATION SLIDE LIGHT INOP. LIGHT ASSEMBLY WAS BADLY CORRODED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAA970281](https://openairdocs.org/sdr/USAA970281.md): Floor Beam · corrosion · Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 VISUAL INSPECTION FOUND A 2 INCH AREA OF CORROSION AT STA 967 FLOOR BEAM AT RBBL 18.0. CORROSION TASK NR C53-107-02. CUT OUT CORROSION, REPAIRED DOUBLER AND FILLER PER REPAIR DOCUMENT SRM 53-00-51. (X)
- [SDR USAA970280](https://openairdocs.org/sdr/USAA970280.md): Floor Beam · corrosion · Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 VISUAL INSPECTION, FOUND A.500 INCH AREA OF CORROSION STA 967 FLOOR BEAM AT LBBL 18.0. CORROSION TASK NR C53-107-02. REMOVED CORROSION, FABRICATED FILLER AND DOUBLERS PER REPAIR DOCUMENT SRM 53-00-51. (X)
- [SDR USAA970279](https://openairdocs.org/sdr/USAA970279.md): Floor Beam · corrosion · Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 VISUAL INSPECTION, FOUND CORROSION AROUND CLIP-NUT HOLES ON THE FLOOR BEAM, STA 987, BL ZERO TO RBBL 45.0. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP. REPAIRED ENTIRE LENGTH PER REPAIR DOCUMENT SRM 53-60-51. (X)
- [SDR USAA970278](https://openairdocs.org/sdr/USAA970278.md): Floor Beam · corrosion · Sep 15, 1997 · N590US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING VISUAL INSPECTION FOUND CORROSION AROUND CLIP-NUT HOLES ON FLOOR BEAM, STA 987, FLOOR BEAM BL ZERO TO LBBL 45.0. CORROSION TASK NR C53-107-02. REPAIRED ENTIRE T-CAP PER SRM 53-60-51. (X)
- [SDR USAASB97140](https://openairdocs.org/sdr/USAASB97140.md): Lock Actuator · failed · May 26, 1997 · N590US · Boeing 737301 · Landing Gear Retraction/Extension System
  > IAD - FLT 892 - DURING APPROACH AND EXTENSION OF THE LANDING GEAR, CREW RECEIVED AN UNSAFE INDICATION ON THE NOSE GEAR. CAPTAIN ACCOMPLISHED A GO-AROUND. A TOWER FLYBY ALSO ACCOMPLISHED WITH THE TOWER ADVISING THE NOSE GEAR APPEARED TO BE DOWN. CREW ACCOMPL
- [SDR USAASB96082](https://openairdocs.org/sdr/USAASB96082.md): Iru · failed · May 10, 1996 · N590US · Boeing 737301 · Inertial Guidance System
  > FLT 84 - SAN - NR 1 IRU FAULT LIGHT ILLUMINATED IN FLIGHT. IN ATT ADI WOULD NOT RECOVER AND HEADING SELECT WAS UNSUCCESSFUL, HEADING SLEWED TO MANUAL SETTING BUT IMMEDIATELY STARTED TO DRIFT. RETURNED TO SAN. MX REPLACED NR 1 IRU. BITE CHECK NORMAL. (M)

## 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 = 'N590US' AND deregistration_id = 'N590US-2008-09-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N590US-2008-09-03/reports

---
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