# Service difficulty reports: N393US, cancelled Jul 5, 2013

A list on [N393US, cancelled Jul 5, 2013](https://openairdocs.org/deregistered/N393US-2013-07-05.md).

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

Page 1 of 2 · 60 reports

- [SDR SB06003](https://openairdocs.org/sdr/SB06003.md): Charger · faulty · Jan 10, 2006 · N393US · Boeing 7373B7 · Emergency Lighting
  > DCA - DURING FLIGHT, THE EMERGENCY EXIT LIGHTS AT THE SEATS AND AT THE BOTTOM OF THE FORWARD ENTRY AND SERVICE DOORS ILLUMINATED AND WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY AT STATION 400 PER MM 33-51-00. AL
- [SDR USAA050884](https://openairdocs.org/sdr/USAA050884.md): Skin · cracked · Jul 18, 2005 · N393US · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > CLT - C - SKIN,.75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)
- [SDR SB05075](https://openairdocs.org/sdr/SB05075.md): Shutoff Valve · leaking · Jun 28, 2005 · N393US · Boeing 7373B7 · Hydraulic System, Main
  > PHL FLT 1085 AFTER TAKEOFF AND GEAR RETRACTION, CREW REPORTED A SUBSTANTIAL DROP IN THE A-HYDRAULIC SYSTEM QUANTITY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLIGHT CONTROL SHUTO
- [SDR SB05044](https://openairdocs.org/sdr/SB05044.md): Wire · broken · Apr 5, 2005 · N393US · Boeing 7373B7 · Light System Wiring
  > BOS COCKPIT EMERGENCY LIGHT SWITCH NOT WORKING PROPERLY. MAINTENANCE REPAIRED A BROKEN WIRE ABOVE ROW 20ABC.
- [SDR SB05042](https://openairdocs.org/sdr/SB05042.md): Battery Pack · faulty · Mar 30, 2005 · N393US · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD.
- [SDR USAA050062](https://openairdocs.org/sdr/USAA050062.md): Skin · cracked · Jan 13, 2005 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2.5 INCHES, 1 INCH ABOVE S23L AT BS 745. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAA040386](https://openairdocs.org/sdr/USAA040386.md): Skin · delaminated · Jul 21, 2004 · N393US · Boeing 7373B7 · Leading Edge Devices
  > FOUND SKIN AND CORE BONDED 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED NEW CORE AND TOP SKIN PER BOEING SRM 51-70-10. (M)
- [SDR USAA040387](https://openairdocs.org/sdr/USAA040387.md): Skin · delaminated · Jul 21, 2004 · N393US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND SKIN AND CORE BOND DELAMINATED 3 INCH BY 4 INCH AREA, UPPER INBOARD END T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)
- [SDR USAASB04030](https://openairdocs.org/sdr/USAASB04030.md): Tube · leaking · Mar 15, 2004 · N393US · Boeing 7373B7 · Hydraulic System, Main
  > AFTER TAKEOFF FROM CLT, THE RIGHT MLG WOULD NOT RETRACT. THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESURE LIGHT WAS ALSO ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, SELECTED THE HYDRAULIC PUMP TO OFF AND DECLARED AN EMERGENCY. FLIGHT RETURN
- [SDR USAA040007](https://openairdocs.org/sdr/USAA040007.md): Frame · cracked · Jan 9, 2004 · N393US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED 1 INCH, BS 178 LEFT SIDE FRAME AT WL 207. SPLICED FRAME AT WL 212 EPR EO 5300V157 PART F. (M)
- [SDR USAA04000B](https://openairdocs.org/sdr/USAA04000B.md): Bulkhead · cracked · Jan 7, 2004 · N393US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > FOUND WEB CRACKED.5 INCH, BULKHEAD WEB BS 178, WL 218, RBBL 5.7. INSTALLED DOUBLER PER EO 5300V153. (M)
- [SDR USAASB03155](https://openairdocs.org/sdr/USAASB03155.md): Battery Pack · inoperative · Aug 27, 2003 · N393US · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE CABIN OVERHEAD BIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD. (M)
- [SDR USAA030154](https://openairdocs.org/sdr/USAA030154.md): Skin · cracked · Aug 19, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN PANEL CRACKED 10 INCHES AND SEVERAL.25 INCH THROUGH.5 INCH LONG CRACKS AND DISBONDED, LAPJOIJNT S-10L BS 360-540 ALONG 15 FT SECTION OF FUSELAGE SKIN. INSTALLED THREE NEW SKIN PANELS.080 INCH PER EA 76610A. (M)
- [SDR USAA030153](https://openairdocs.org/sdr/USAA030153.md): Skin · cracked · Aug 19, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2.4 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER SRM 53-60-01 FIG 207. (M)
- [SDR USAA030138](https://openairdocs.org/sdr/USAA030138.md): Skin · cracked · Aug 14, 2003 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.125 INCH BY.25 INCH CRACKING AT RIVET HEADS, APPROX 40, AND DISONDING, LEFT SIDE STATION 360-540 STRINGER 10 LEFT. REMOVED SKIN PANEL STATION 360-540, INSTALLED 3 SECTIONS WITH 2 SPLICE AT STATION 420 AND 480 PER EA 76610. (M)
- [SDR USAASB03010](https://openairdocs.org/sdr/USAASB03010.md): Pump · faulty · Jan 15, 2003 · N393US · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), Main
  > PHL - FLT 390 - EN ROUTE FROM CLT-DTW, THE 'A' HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED WITH THE PUMP CYCLING ON AND OFF. DECISION WAS MADE TO DIVERT TO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED
- [SDR USAA020329](https://openairdocs.org/sdr/USAA020329.md): Skin · cracked · Aug 1, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2.1 INCH, STATION 727E ABOVE STRINGER 24L IN AFT FUSELAGE SKIN. CRACKED AREA CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA020309](https://openairdocs.org/sdr/USAA020309.md): Stringer · corroded · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CORRODED ON ENDS OF STRINGER STATION 323.7 AND BL 0 TO S28R. (M)
- [SDR USAA020297](https://openairdocs.org/sdr/USAA020297.md): Door Frame · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Passenger/Crew Doors
  > PIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER FORWARD CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)
- [SDR USAA020298](https://openairdocs.org/sdr/USAA020298.md): Door Frame · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Passenger/Crew Doors
  > PIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER AFT CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)
- [SDR USAA020293](https://openairdocs.org/sdr/USAA020293.md): Attach Angle · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > PIT - FOUND ANGLE CRACKED.75 INCH, INT ATTACH ANGLE FORWARD STATION 291.5, S12R AND S13R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M)
- [SDR USAA020294](https://openairdocs.org/sdr/USAA020294.md): Angle · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ANGLE CRACKED.5 INCH, INT ATTACH ANGLE FORWARD OF STATION 291.5, S11R AND S12R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BOEING DWG 65-45807-31. (M)
- [SDR USAA020296](https://openairdocs.org/sdr/USAA020296.md): Frame · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25 INCH, INT DOOR FRAME ON FUSELAGE AT FORWARD UPPER CORNER. FABRICATED NEW ANGLE PER EA. (M)
- [SDR USAA020299](https://openairdocs.org/sdr/USAA020299.md): Stringer · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.125 INCH, AT RIVET STATION 927 AT STRINGER 8R AND 9R. REMOVED CRACK AND INSTALLED OVERSIZED FASTENER PER 51-40-05. (M)
- [SDR USAA020300](https://openairdocs.org/sdr/USAA020300.md): Stringer · cracked · Jul 30, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.25 INCH, STATION 907, STRINGER 8L-9L AT RIVET. REMOVED CRACKED AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAA020225](https://openairdocs.org/sdr/USAA020225.md): Skin · delaminated · Jul 2, 2002 · N393US · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER DELAMINATED SEVERAL PLACES FROM.25 INCHES TO 6 INCHES, 1 PLY DEEP, RIGHT/LEFT RUDDER, R STATION 121.64 TO 0.00. COMPLETED 200-230 DEGREE WET LAY UP PER SRM 51-70-17 PER EA 74241. (M)
- [SDR USAA020310](https://openairdocs.org/sdr/USAA020310.md): Skin · cracked · Jul 2, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 3 INCHES, ABOVE LEFT NLG DOOR JUST FORWARD OF STATION 259.5. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER EA 61654B. (M)
- [SDR USAA020295](https://openairdocs.org/sdr/USAA020295.md): Skin · cracked · Jun 19, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.5 INCHES LONG, FORWARD SERVICE DOOR AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01 FIG 202. (M)
- [SDR USAA020308](https://openairdocs.org/sdr/USAA020308.md): Skin · cracked · Jun 19, 2002 · N393US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1 INCH, CAPTAINS WINDSHIELD NR 1 UPPER LEFT CORNER OF WINDOW POST. INSTALLED EXTERIOR DOUBLER PER SRM 53-10-01 FIG 210 PAGE 233. (M)
- [SDR USAASB02017](https://openairdocs.org/sdr/USAASB02017.md): Regulator · failed · Jan 19, 2002 · N393US · Boeing 7373B7 · Pneumatic Distribution System
  > BOS - FLT 926 - CLIMBING-OUT FROM PHL, EN ROUTE TO PWM AT FL250, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CREW TRIED TO RESET BLEED WITH NO HELP. WITH NR 2 BLEED INOPERATIVE, PRESSURIZATION WAS OK AT FL250 FOR 15 MINUTES, BUT THEN THE CABIN PRESSURE BEG
- [SDR USAA020104](https://openairdocs.org/sdr/USAA020104.md): Angle · cracked · Dec 30, 2001 · N393US · Boeing 7373B7 · Nacelle/Pylon Structure
  > PIT - FOUND ANGLE CRACKED 1 INCH, VERTICAL ANGLE AT STATION 363. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED CHANNEL PER NR 313A1355. (M)
- [SDR USAA011364](https://openairdocs.org/sdr/USAA011364.md): Skin · cracked · Nov 15, 2001 · N393US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND ON WALK AROUND, FOUND SKIN CRACKED 3 INCHES, NR 6 SLAT BOTTOM INBOARD END. CUT OUT DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, FIG 206. (M)
- [SDR USAASB01282](https://openairdocs.org/sdr/USAASB01282.md): Charger · failed · Oct 3, 2001 · N393US · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACKS (P/N 2013-1A) AND THE RIGHT FORWARD CHARGER ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAA010162](https://openairdocs.org/sdr/USAA010162.md): Crossbeam · corroded · Jan 10, 2001 · N393US · Boeing 7373B7 · Engine Mount Section
  > PIT - FOUND ENGINE MOUNT CROSSBEAM CORRODED, BEARING BORE OF CROSS BEAM. CORROSION LEVEL 1. ENLARGED BORE.010 CHANFERED BORE, MPI ROTO PEEN. INSTALLED OVERSIZED BEARING PER TYP REP 54-50-09. (M)
- [SDR USAASB00280](https://openairdocs.org/sdr/USAASB00280.md): Uplock Switch · failed · Oct 1, 2000 · N393US · Boeing 7373B7 · Landing Gear Position and Warning
  > GSO - FLT 1658 - ON CLIMB-OUT, AFTER GEAR RETRACTION, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO FIELD AT GSO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTEN
- [SDR USAASB00220](https://openairdocs.org/sdr/USAASB00220.md): Control Cable · out of adj · Aug 18, 2000 · N393US · Boeing 7373B7 · Drag Control System
  > MCO - FLT 808 - AFTER TAKEOFF FROM MCO, CREW WAS UNABLE TO RAISE LANDING GEAR. THE GEAR SELECTOR LOCKED AT MID-POINT. UPON FLAP TO ZERO, THE WARNING HORN BEGAN SOUNDING. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARE
- [SDR USAASB00219](https://openairdocs.org/sdr/USAASB00219.md): Solenoid · faulty · Aug 17, 2000 · N393US · Boeing 7373B7 · Landing Gear Retraction/Extension System
  > MCO - FLT 676 - AFTER TAKEOFF FROM MCO, CREW RAISED GEAR HANDLE TO STOW THE GEAR BUT THE HANDLE STOPPED BEFORE REACHING THE GEAR UP POSITION. DURING TROUBLESHOOTING, CREW RECEIVED A WARNING HORN. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR USAASB00127](https://openairdocs.org/sdr/USAASB00127.md): Adc · failed · Apr 27, 2000 · N393US · Boeing 7373B7 · Air Data Computer
  > CLT - FLT 463 - CLIMB-OUT FROM CLT, AT FL 230, OFF FLAGS APPEARED ON CAPTAIN''S AIRSPEED INDICATOR AND ALTIMETER. CREW WAS UNABLE TO ENGAGE A-SYSTEM AUTOPILOT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.
- [SDR USAASB00044](https://openairdocs.org/sdr/USAASB00044.md): Shutoff Valve · leaking · Feb 18, 2000 · N393US · Boeing 7373B7 · Hydraulic System, Main
  > PIT - FLT 8054 - INBOUND TO PIT, FROM IAH, SYSTEM A HYDRAULICS FAILED. CREW DECLARED AN EMERGENCY AND HAD TO MANUALLY EXTEND LANDING GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. LANDING GEAR WAS PINNED BEFORE BEING TOWED TO THE GATE. MAINTENANCE FOUND THE
- [SDR USAASB99222](https://openairdocs.org/sdr/USAASB99222.md): Seal · torn · Sep 7, 1999 · N393US · Boeing 7373B7 · Cargo/Baggage Doors
  > TPA - FLT 1469 - EN ROUTE FROM CLT TO TPA, ABOVE GAINESVILLE FLORIDA AT FL310, FLIGHT LOST PRESSURIZATION. THE CREW FELT A THUMP IN THE CABIN ALONG WITH A RISE IN CABIN ALTITUDE OF 4,000 FEET PER MINUTE. CREW DECLARED AN EMERGENCY AND QUICKLY DESCENDED TO 10
- [SDR USAASB98264](https://openairdocs.org/sdr/USAASB98264.md): Warning Light · illuminated · Oct 5, 1998 · N393US · Boeing 7373B7 · Landing Gear Position and Warning
  > PIT - FLIGHT WAS EN ROUTE FROM BOS, WHEN THE CREW RECEIVED A RIGHT MLG UNSAFE INDICATION. AIRCRAFT MADE AN UNEVENTFUL LANDING AT PIT. (M)
- [SDR USAA980465](https://openairdocs.org/sdr/USAA980465.md): Floorbeam · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AROUND FASTENERS.5 INCH BY.5 INCH BY 37 INCH STAITON 312 BETWEEN LBL 14 AND RBL 23 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED NEW T-SECTION WITH DOUBLER PER SRM 53-10-
- [SDR USAA980443](https://openairdocs.org/sdr/USAA980443.md): Floorbeam · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORRODED AREA BS 967 RBL 49 BEAM INST PAX FLOOR. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-10-05. (M)
- [SDR USAA980442](https://openairdocs.org/sdr/USAA980442.md): Web · cracked · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK SHEAR BEAM WEB 518A RIGHT BS 721. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)
- [SDR USAA980441](https://openairdocs.org/sdr/USAA980441.md): Frame · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2 INCH CORRODED AREA BS 827 BETWEEN STRINGER 28L AND STRINGER 28R RBL 2 BOTTOM FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980440](https://openairdocs.org/sdr/USAA980440.md): Web · cracked · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CRACKED AREA.25 INCH FORWARD SERVICE DOOR OPENING LWR FWD CORNER BS 294 STRINGER 17R FLOOR LEVEL. INSTALLED DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA980425](https://openairdocs.org/sdr/USAA980425.md): Floorbeam · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS.5 INCH BY.5 INCH BY 26 INCH BS 328 LB 12 TQ RBL 14, WL 208.1 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER SRM 51-70-12. (M)
- [SDR USAA980424](https://openairdocs.org/sdr/USAA980424.md): Floorbeam · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 2 INCH CORRODED AREA STATION 1006 BEAM T-CAP RBL 10. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-58-53500-012. (M)
- [SDR USAA980423](https://openairdocs.org/sdr/USAA980423.md): Floorbeam · corroded · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH AREA OF CORROSION BS 986.5 LBL 4, 11, 21 AND LOWER SURFACE LBL 36 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP UPPER CHORD PER SRM 53-00-51 AND EA 62431. (M)
- [SDR USAA980422](https://openairdocs.org/sdr/USAA980422.md): Splice · cracked · Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND STRINGER SPLICE CRACKED AROUND 4 RIVET HOLES.125 INCH EACH STRINGER AT STATION 907 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-40-02. (M)

Next page: https://openairdocs.org/deregistered/N393US-2013-07-05/reports.md?page=2

## 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 = 'N393US' AND deregistration_id = 'N393US-2013-07-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N393US-2013-07-05/reports

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