# Service difficulty reports: N355US, cancelled Aug 9, 2006

A list on [N355US, cancelled Aug 9, 2006](https://openairdocs.org/deregistered/N355US-2006-08-09.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 · 53 reports

- [SDR SB05176](https://openairdocs.org/sdr/SB05176.md): Charger · faulty · Dec 25, 2005 · N355US · Boeing 737301 · Emergency Lighting
  > TPA - THE SEAT MOUNTED EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY. EMERGENCY LIGHTS CHECK OK.
- [SDR SB05147](https://openairdocs.org/sdr/SB05147.md): Fuse · blown · Nov 16, 2005 · N355US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE AFT LEFT EXTERIOR EMERGENCY LIGHT AND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 AND 23 INOPERATIVE. MAINTENANCE RELAMPED THE EXTERIOR EMERGENCY LIGHT AND REPLACED A BLOWN FUSE ON POWER SUPPLY M1197. OPERATIONAL CHECK GOOD.
- [SDR USAA040340](https://openairdocs.org/sdr/USAA040340.md): Frame · cracked · Jul 8, 2004 · N355US · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.125 INCH, STATION 480, S8L-S9L. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)
- [SDR USAA040288](https://openairdocs.org/sdr/USAA040288.md): Beam · cracked · Jun 11, 2004 · N355US · Boeing 737301 · Vertical Stabilizer
  > PIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M)
- [SDR USAA040287](https://openairdocs.org/sdr/USAA040287.md): Floorbeam · corroded · Jun 10, 2004 · N355US · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - FOUND BEAM CORRODED THREE 1 INCH DIAMETER AREAS, BS 947 LBL 30 TO LBL 46. REMOVED CORROSION, TREATED AND PRIMED, PERFORMED TYP REPAIR 53-15-01B, SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA040348](https://openairdocs.org/sdr/USAA040348.md): Stringer · corroded · Mar 27, 2004 · N355US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER CORRODED TWO AREAS, 1 INCH BY 6 INCHES AND 1 INCH BY 4 INCHES, FS 1016-1022 FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED STIFFENERS AND INSTALLED DOUBLERS AND SPLICES PER SRM 53-80-08 AND BOEING DWG PL 65C28106. (M)
- [SDR USAASB04024](https://openairdocs.org/sdr/USAASB04024.md): Arm · fractured · Mar 2, 2004 · N355US · Boeing 737301 · Landing Gear Retraction/Extension System
  > CLT - FLT 240 - UPON GEAR RETRACTION, CREW HEARD A LOUD THUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BOTH LUGS OF THE LEFT MAIN GEAR ACTUATOR BEAM ARM
- [SDR USA2004F00019](https://openairdocs.org/sdr/USA2004F00019.md): Arm · cracked · Mar 2, 2004 · N355US · Boeing 737301 · Landing Gear Actuator
  > UPON GEAR RETRACTION, CREW HEARD A LOUD THRUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. LT MAIN LANDING GEAR ACTUATOR BEAM ARM FOUND CRACKED. REAR
- [SDR USAA040049](https://openairdocs.org/sdr/USAA040049.md): Skin · cracked · Feb 12, 2004 · N355US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 2 INCHES, 727D AND S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB03211](https://openairdocs.org/sdr/USAASB03211.md): Servo · failed · Dec 5, 2003 · N355US · Boeing 737301 · Autopilot Main Servo
  > DURING FLIGHT, EN ROUTE, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. THE AUTOPILOT WOULD NOT TRIM. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT SERVO MOTOR. OPS CHECK AND BITE TEST NORMAL. (M)
- [SDR USAA030029](https://openairdocs.org/sdr/USAA030029.md): Support Fitting · worn · Mar 21, 2003 · N355US · Boeing 737301 · Vertical Stabilizer
  > PIT - FOUND TERMINAL SUPPORT FITTING HAS TWO WORN BOLTS, VERTICAL STABILIZER AFT TERMINAL SUPPORT FITTING BOLT HOLES. REWORKED WORN HOLES PER EA 94263A, THIS IS AN INTERIM REPAIR. (M)
- [SDR USAA020390](https://openairdocs.org/sdr/USAA020390.md): Stiffener · cracked · Oct 4, 2002 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > IT - FOUND STIFFENER ANGLE CRACKED 1 INCH LONG, VERTICAL STIFFENER MLG W/W FORWARD BULKHEAD CENTER LINE STATION 663. FABRICATED AND INSTALLED 2 REPAIR STRAPS AND ATTACH ANGLE IAW EA 75025. (M)
- [SDR USAASB01224](https://openairdocs.org/sdr/USAASB01224.md): Outflow Valve · failed · Aug 7, 2001 · N355US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > PIT - FLT 1146 - EN ROUTE FROM PHL TO CMH, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW NOTICED CABIN ALTITUDE AT 11,000 FEET. CREW WAS UNABLE TO CONTROL CABIN ALTITUDE, DESCENDED TO 10,000 FEET PER QUICK REF HANDBOOK PROCEDURES. FLIGHT DIVERTED
- [SDR USAA010022](https://openairdocs.org/sdr/USAA010022.md): Skin · cracked · Jan 15, 2001 · N355US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED, STATION 200, LBL 5. INSTALLED EXTERIOR DOUBLER PER EA 68798. (M)
- [SDR USAA002204](https://openairdocs.org/sdr/USAA002204.md): Bulkhead · cracked · Dec 27, 2000 · N355US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED 1 INCH, STATION 178, WL 198, LBL 4. INSTALLED DOUBLER PER EA 68679. (M)
- [SDR USAA002197](https://openairdocs.org/sdr/USAA002197.md): Frame · cracked · Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 727B STRINGER 14R. INSTALLED ANGLE PER SRM 53-00-07. (M)
- [SDR USAA002198](https://openairdocs.org/sdr/USAA002198.md): Frame · cracked · Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND CHORD CRACKED 1.5 INCH, BS 178, WL 207, RBL 29. REMOVED SECTION AND INSTALLED NEW SECTION PER EA 68680 AND EO 5300V157. (M)
- [SDR USAA002199](https://openairdocs.org/sdr/USAA002199.md): Intercostal · cracked · Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND INTERCOSTAL CRACKED 1 INCH BY 1 INCH, BS 178, WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M)
- [SDR USAA002200](https://openairdocs.org/sdr/USAA002200.md): Intercostal · cracked · Dec 26, 2000 · N355US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND INTERCOSTAL CRACKED.750 INCH BY 1 INCH, BS 178, WL 195, RBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND EO5300V157. (M)
- [SDR USAA002194](https://openairdocs.org/sdr/USAA002194.md): Floorbeam · cracked · Dec 22, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CRACKED 1 INCH BY 1 INCH, STATION 344, LBL 9. CORROSION LEVEL 1. REMOVED T-CAP AND FABRICATED NEW T-CAP AND SPLICE PER SRM 53-10-51 AND 53-40-51. (M)
- [SDR USAA002184](https://openairdocs.org/sdr/USAA002184.md): Doubler · cracked · Dec 21, 2000 · N355US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND ANTENNA DOUBLER CRACKED.5 INCH, STATION 727D-727E, BL 0. INSTALLED NEW DOUBLER PER SRM 51-10-02. (M)
- [SDR USAA002175](https://openairdocs.org/sdr/USAA002175.md): Floorbeam · corroded · Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND T-CAP CORRODED 1 INCH, STATION 328 FLOORBEAM AT RBL 14, 21, 35. CORROSION LEVEL 1 C53-107-01. INSTALLED NEW T-CAP AND FABRICATED SPLICE ANGLES PER SRM 53-10-51. (M)
- [SDR USAA002176](https://openairdocs.org/sdr/USAA002176.md): Tie Clip · cracked · Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 344, STRINGER 10R. FABRICATED NEW CLIP PER SRM 53-10-15 AND SRM 51-10-2. (M)
- [SDR USAA002177](https://openairdocs.org/sdr/USAA002177.md): Shear Tie · cracked · Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND TIE ANGLE CRACKED.333 INCH, FRAME 360 BETWEEN STRINGER 14R AND STRINGER 15R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M)
- [SDR USAA002178](https://openairdocs.org/sdr/USAA002178.md): Intercostal · cracked · Dec 20, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED.25 INCH, INTERCOSTAL AT FS 294.5, STRINGER 7L. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA002163](https://openairdocs.org/sdr/USAA002163.md): Floorbeam · corroded · Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED.5 INCH, STATION 312 BL 0. CORROSION LEVEL 2 C53-107-02. REPLACED T-CAP PER SRM 53-00-51. (M)
- [SDR USAA002160](https://openairdocs.org/sdr/USAA002160.md): Attach Angle · cracked · Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ATTACH ANGLE CRACKED.5 INCH, FORWARD OF FS 303.9 ABOVE STRINGER 10L. INSTALLED NEW ATTACH ANGLE PER SRM 51-10-02. (M)
- [SDR USAA002161](https://openairdocs.org/sdr/USAA002161.md): Attach Angle · cracked · Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND FRAME ATTACH ANGLE CRACKED.25 INCH, FRAME ATTACH ANGLE AT FS 348.2 STRINGER 11L. FABRICATED NEW ATTACH ANGLE PER SRM 51-10-2. (M)
- [SDR USAA002162](https://openairdocs.org/sdr/USAA002162.md): Shear Tie · cracked · Dec 18, 2000 · N355US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME SHEAR TIE CRACKED.5 INCH, STATION 967, BETWEEN STRINGER 6L AND 7L. REMOVED AND INSTALLED DOUBLER PER EA 68751. (M)
- [SDR USAA002158](https://openairdocs.org/sdr/USAA002158.md): Floorbeam · corroded · Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND SPLICE ANGLE T-CAP CORRODED, STATION 344, RBL 9, LBL 37. REPLACED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA002156](https://openairdocs.org/sdr/USAA002156.md): Frame · cracked · Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, FRAME STATION 887 STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002157](https://openairdocs.org/sdr/USAA002157.md): Angle · cracked · Dec 15, 2000 · N355US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND CORNER ANGLE CRACKED.75 INCH, DOOR CUTOUT LOWER AFT CORNER ANGLE. INSTALLED NEW CORNER ANGLE. (M)
- [SDR USAA002148](https://openairdocs.org/sdr/USAA002148.md): Stringer Clip · cracked · Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CLIP CRACKED 1 INCH, STATION 807, STRINGER 4L. REPLACED CLIP PER SRM 51-10-02. (M)
- [SDR USAA002149](https://openairdocs.org/sdr/USAA002149.md): Frame · cracked · Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, FS 847, STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002150](https://openairdocs.org/sdr/USAA002150.md): Frame · cracked · Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FUSELAGE FRAME CRACKED.5 INCH, STATION 827 ABOVE STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002151](https://openairdocs.org/sdr/USAA002151.md): Frame · cracked · Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, FRAME 400 ABOVE STRINGER 9R. REPAIRED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA002152](https://openairdocs.org/sdr/USAA002152.md): Stringer Clip · cracked · Dec 14, 2000 · N355US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CLIP CRACKED.5 INCH, STATION 639, STRINGER 2L CLIP. REPLACED PART PER SRM 51-10-2 AND 51-40-2. (M)
- [SDR USAA002092](https://openairdocs.org/sdr/USAA002092.md): Tie Clip · cracked · Dec 11, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.50 INCH, STATION 616 STRINGER 2R. INSTALLED TIE CLIP PER SRM 51-10-02 AND SRM 51-40-03. (M)
- [SDR USAA002093](https://openairdocs.org/sdr/USAA002093.md): Tie Clip · cracked · Dec 11, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, STATION 727E, STRINGER 7R. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA002077](https://openairdocs.org/sdr/USAA002077.md): Web · cracked · Dec 7, 2000 · N355US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB PLATE CRACKED 2 INCHES, STATION 639 STRINGER 17R. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA002078](https://openairdocs.org/sdr/USAA002078.md): Crease Beam · cracked · Dec 7, 2000 · N355US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND CREASE BEAM CRACKED 1 INCH, BS 639 BETWEEN STATION 619-639 STRINGER 17L REPAIRED PER SRM 51-10-2. (M)
- [SDR USAASB00055](https://openairdocs.org/sdr/USAASB00055.md): Actuator · failed · Feb 28, 2000 · N355US · Boeing 737301 · Stabilizer Actuator
  > PHL - FLT 1063 - EN ROUTE FROM RIC TO BOS, THE STABILIZER ELECTRIC TRIM HAD FAILED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTEHR INCDIENT. NO EMEGENCY WAS DECLARED. MAINTENANCE PERFORMED FUNCTIONAL CHECK ON STABILIZER TRIM SYSTEM AND FOUND ALL FUNCTION
- [SDR USAASB00039](https://openairdocs.org/sdr/USAASB00039.md): Battery Pack · discharged · Feb 12, 2000 · N355US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTING INOPERATIVE AT ROW 12 ABC THROUGH ROW 16 ABC AND AT ROW 21 AND 22 ABC. ALSO, FOUND THE RIGHT AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA
- [SDR USAASB00014](https://openairdocs.org/sdr/USAASB00014.md): Controller · failed · Jan 21, 2000 · N355US · Boeing 737301 · Cabin Pressure Controller
  > PIT - FLT 723 - ON CLIMB-OUT FROM PIT, THE AUTO FAIL PRESSURIZATION LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES BUT WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY W
- [SDR USAASB99301](https://openairdocs.org/sdr/USAASB99301.md): Unknown · odor · Dec 23, 1999 · N355US · Boeing 737301 · Air Distribution System
  > MCO - FLT 2152 - 20 MINUTES AFTER T/O FROM RSW, UNIDENTIFIED FUMES WERE RECOGNIZED IN THE AFT GALLEY. CREW TURNED OFF GALLEY POWER SWITCH AND PULLED ALL CIRCUIT BREAKERS IN THE GALLEY. NO SMOKE WAS PRESENT BUT FUMES BECAME STRONGER. CREW DECLARED EMERGENCY
- [SDR USAASB99293](https://openairdocs.org/sdr/USAASB99293.md): Engine · vibration · Dec 14, 1999 · N355US · Boeing 737301 · Engine (Turbine/Turboprop)
  > CLT - FLT 8052 - ON CLIMB-OUT FROM CLT, THE NR1 ENGINE VIBRATION MONITOR INDICATED 2 UNITS ACCELERATING THROUGH 210 KNOTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYWAS DECLARED. MAINTENACNE ACCOMPLISHED TROUBLESHOOTI
- [SDR USAASB99261](https://openairdocs.org/sdr/USAASB99261.md): Coffeemaker · malfunctioned · Oct 29, 1999 · N355US · Boeing 737301 · Buffet/Galleys
  > IAD - FLT 488 - EN ROUTE FROM PIT-BWI, F/A REPORTED SMELL OF BURNING WIRES AND FUMES IN THE AFT CABIN. NO VISIBLE SMOKE WAS NOTED. AN EMERGENCY WAS DECLARED AND FLT DIVERTED TO NEAREST AIRPORT AT IAD. FLT LANDED W/O FURTHER INCIDENT. MX RAN BOTH ENGINES TO
- [SDR USAASB98095](https://openairdocs.org/sdr/USAASB98095.md): Indicator · failed · Apr 15, 1998 · N355US · Boeing 737301 · Trailing Flap Position Indicating System
  > RDU - FL 1494 - ON APPROACH TO RDU, CREW EXTENDED FLAPS FROM 25 TO 30 DEGREES AND RECEIVED A FLAP ASSYMETRY. CREW PLACED FLAPS BACK TO 25 DEGREES, ADVISED THE TOWER THEY HAD A PROBLEM AND DECLARED AN EMERGENCY. CREW ACCOMPLISHED A GO-AROUND AND PERFORMED EME
- [SDR USAASB97064](https://openairdocs.org/sdr/USAASB97064.md): Wire · loose · Mar 2, 1997 · N355US · Boeing 737301 · Light System Wiring
  > BWI - MAINTENANCE REPORTED THE LEFT AFT EXTERIOR EMERGENCY ESCAPE LIGHT WAS INOP. MAINTENANCE INSTALLED NEW WIRE FROM M1197 BATTERY PACK D3122 PIN 9 TO L732 ESCAPE SLIDE LIGHT. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97062](https://openairdocs.org/sdr/USAASB97062.md): Wire · broken · Feb 28, 1997 · N355US · Boeing 737301 · Light System Wiring
  > BDL - AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED WIRE BETWEEN POWER SUPPLY AND LIGHT ASSEMBLY CONNECTORS D3122 AND D3170. (M)

Next page: https://openairdocs.org/deregistered/N355US-2006-08-09/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 = 'N355US' AND deregistration_id = 'N355US-2006-08-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N355US-2006-08-09/reports

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