# Service difficulty reports: N342US, cancelled Oct 16, 2003

A list on [N342US, cancelled Oct 16, 2003](https://openairdocs.org/deregistered/N342US-2003-10-16.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 USAA030015](https://openairdocs.org/sdr/USAA030015.md): Skin · cracked · Feb 5, 2003 · N342US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2.5 INCH, LEFT AFT FUSELAGE BS 727E STRINGER 23. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)
- [SDR USAASB02211](https://openairdocs.org/sdr/USAASB02211.md): Control Panel · faulty · Nov 26, 2002 · N342US · Boeing 737301 · Navigation System
  > ALB - FLT 342 - ON APPROACH TO ALB, FROM PHL, CREW REPORTED A BURNING SMELL IN THE COCKPIT. THE NR 1 NAV INDICATIONS ALL FLAGGED AND THE NR 1 NAV CIRCUIT BREAKER POPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 NAV C
- [SDR USAASB01356](https://openairdocs.org/sdr/USAASB01356.md): Light · inoperative · Dec 28, 2001 · N342US · Boeing 737301 · Emergency Lighting
  > PHL - PILOT REPORTED THE EMERGENCY PATH LIGHT AT SEAT ROW 2C WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 2C. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01253](https://openairdocs.org/sdr/USAASB01253.md): Battery Pack · discharged · Sep 15, 2001 · N342US · Boeing 737301 · Emergency Lighting
  > DCA - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHTS AND THE L1 DOOR EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01204](https://openairdocs.org/sdr/USAASB01204.md): Engine · malfunctioned · Jul 16, 2001 · N342US · Boeing 737301 · Engine (Turbine/Turboprop)
  > MSY - FLT 239 - EN ROUTE FROM CLT-IAH - AT FL350, THE CREW FELT A JOLT AND THEN A NR 2 ENGINE VIBRATION ALONG WITH A RISE IN EGT. FLIGHT ATTENDANT REPORTED SEEING A FLASH FROM THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTE
- [SDR USAASB00318](https://openairdocs.org/sdr/USAASB00318.md): Computer · failed · Nov 19, 2000 · N342US · Boeing 737301 · Flight Management Computing Hardware System
  > TPA - FLT 1091 - EN ROUTE FROM PHL TO GCM, BOTH FLIGHT MANAGEMENT COMPUTER SYSTEM CONTROL DISPLAY UNITS FAILED. FLIGHT DIVERTED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER. SYSTEM OPERATIONAL C
- [SDR USAASB00289](https://openairdocs.org/sdr/USAASB00289.md): Duct · leaking · Oct 6, 2000 · N342US · Boeing 737301 · Pneumatic Distribution System
  > TPA - FLT 1515 - EN ROUTE FROM CLT TO CUN, THE LT WING-TO-BODY OVERHEAT LIGHT ILLUMINATED AND REMAINED ON FOR TWENTY MINUTES AFTER QUICK REFERENCE HANDBOOK PROCEDURES ACCOMPLISHED. FLIGHT DIVERTED TO TPA, LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARE
- [SDR USAASB00159](https://openairdocs.org/sdr/USAASB00159.md): Gcu · failed · Jun 7, 2000 · N342US · Boeing 737301 · AC Generation System
  > BOS - FLT 6535 - ON CLIMB-OUT FROM BOS, AT APPROXIMATELY 3,500 FEET, THE NR 1 GENERATOR WENT OFF LINE AND ALL ELECTRICAL AVIONIC SYSTEMS ON THE CAPTAINS SIDE WENT BLANK. THE FIRST OFFICERS SIDE WAS FLICKERING AND EVENTUALLY RETURNED AFTER THE APU WAS STARTED.
- [SDR USAA991019](https://openairdocs.org/sdr/USAA991019.md): Angle · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION RT SERVICE DOOR Z-ANGLE BETWEEN STATION 947.5 AND 986.5. CORROSION LEVEL 1. INSTALLED NEW Z-ANGLE PER SRM 53-60-51, LIMITS AND SRM 51-10-02. (M)
- [SDR USAA991018](https://openairdocs.org/sdr/USAA991018.md): Angle · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREAS OF CORROSION AT ANCHOR NUT HOLES BS 312 TO BS 370 FORWARD ENTRY SILL Z-ANGLE. CORROSION LEVEL 2. REPAIRED AND REPLACED PER SRM 51-10-02. (M)
- [SDR USAA991017](https://openairdocs.org/sdr/USAA991017.md): Splice · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT RIVETS BS 907, STRINGER SPLICE 4R. INSTALLED NEW SPLICE PER SRM 51-10-02. (M)
- [SDR USAA991016](https://openairdocs.org/sdr/USAA991016.md): Frame · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORROSION SPOT AT FRAME BS 500 RBL 25 FORWARD CARGO. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER EA 65486 REV A AND SRM 53-00-07 FIG 202. (M)
- [SDR USAA991001](https://openairdocs.org/sdr/USAA991001.md): Stringer · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4.5 INCH CRACK BS 1138 TO STATION 1143 STRINGER 5R. INSTALLED REPAIR ANGLE PER EA 65627A. (M)
- [SDR USAA990999](https://openairdocs.org/sdr/USAA990999.md): Floorbeam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 24 INCH AREA OF CORROSION AT STATION 1016 FLOORBEAM AND INTERCOSTAL. CORROSION LEVEL 2. REPLACED INTERCOSTAL. INSTALLED REPAIR DOUBLERS AND STRAPS PER EA 65584. (M)
- [SDR USAA990993](https://openairdocs.org/sdr/USAA990993.md): Floorbeam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 3 INCHES AT STATION 986.5, 44 RBL FLOORBEAM. CORROSION LEVEL 2. INSTALLED BEAM CAP REPAIR PER TR 53-10-05. (M)
- [SDR USAA990983](https://openairdocs.org/sdr/USAA990983.md): Clip · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.75 INCH CRACK AND.500 INCH CRACK AFT CARGO AT BS 727D BL 3L AND 3R CLIP. INSTALLED REPAIR ANGLES PER SRM 51-10-02 AND BOEING DRAWING 65-65710. (M)
- [SDR USAA990982](https://openairdocs.org/sdr/USAA990982.md): Skin · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2.75 INCH CRACKS IN UPPER PRESS DECK OF LEFT MLG W/W BS 664, LBL 30, WL 203 SKIN. INSTALLED DOUBLER PER EA 65333. (M)
- [SDR USAA990981](https://openairdocs.org/sdr/USAA990981.md): Bracket · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.2 5INCH CRACK INBOARD COAT CLOSET BRACKET AT BS 1016. REPLACED BRACKET PER REPAIR DOCUMENT 51-10-02. (M)
- [SDR USAA990980](https://openairdocs.org/sdr/USAA990980.md): Frame · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, F OUND 2 CRACKS.750 LEFT AND.500 RIGHT AFT CARGO BS 727D, LBL 3 AND RBL 3 FRAME. INSTALLED DOUBLER PER EA 65325. (M)
- [SDR USAA990979](https://openairdocs.org/sdr/USAA990979.md): Beam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION RUNNING ALONG TOP AND SECONDARY CAPS OF BEAM APPROX 1 INCH BEAM 986.5, LBL 04, CORROSION LEVEL 1. INSTALLED UPPER BEAM CAP REPAIR PER SRM 53-10-05. (M)
- [SDR USAA990966](https://openairdocs.org/sdr/USAA990966.md): Angle · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178, BL 5 LEFT 10.5 INCH FROM BOTTOM BULKHEAD WEB ATTACH ANGLE. INSTALLED REPAIR FILLER, ANGLES, RADIUS STRAPS PER SRM 53-10-08 FIG 205. (M)
- [SDR USAA990962](https://openairdocs.org/sdr/USAA990962.md): Skin · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.250 INCH CRACK AT BS 379, LBL 2.5 AFT SIDE OF EQUIP COOLING EXHAUST OUTLET FUSELAGE SKIN. INSTALLED SKIN DOUBLER PER TR 53-30-07 AND BOEING DWG 65C33930. (M)
- [SDR USAA990961](https://openairdocs.org/sdr/USAA990961.md): Skin · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 327 FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER EXTERIOR SKIN. INSTALLED TRIPLER PER SRM 53-10-01. (M)
- [SDR USAA990960](https://openairdocs.org/sdr/USAA990960.md): Web · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE.25 INCH CRACKS AT FAST HOLES ALONG WEB SKIN AT BS 709-712, WL 203, BBL 0. INSTALLED WEB REPAIR PER EA 65480 AND SB 737-57-1210. (M)
- [SDR USAA990959](https://openairdocs.org/sdr/USAA990959.md): Intercostal · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, RBL 24, WL 195 INTERCOSTAL. INSTALLED NEW INTERCOSTAL PER TR 53-10-15/SRM 51-40-03 FIG 1/SRM 53-10-08. (M)
- [SDR USAA990938](https://openairdocs.org/sdr/USAA990938.md): Clip · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 1040, STRINGER 2R TO 3R SHEAR TIE CLIP. INSTALLED FABRICATED SHEAR TIE CLIP PER DWG 65-46369. (M)
- [SDR USAA990937](https://openairdocs.org/sdr/USAA990937.md): Bulkhead Web · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION LEFT FACE OF BS 1016 PRESSURE BULKHEAD CTR BL 0 STIFFENER. CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 53-80-08 AND EA 65447. (M)
- [SDR USAA990936](https://openairdocs.org/sdr/USAA990936.md): Frame · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203. INSTALLED DOUBLER AND FILLER PER EA 65336A AND TR 53-10-23. (M)
- [SDR USAA990935](https://openairdocs.org/sdr/USAA990935.md): Frame · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203 LEFT SIDE. INSTALLED DOUBLER AND FILLER PR EA 65336A AND TR 53-10-23. (M)
- [SDR USAA990934](https://openairdocs.org/sdr/USAA990934.md): T-Cap · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLE BS 344, LBL 49 FORWARD FLANGE AND LBL 31 SPLICE T-CAP. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51 FIG 1 AND TR 53-10-13 AND EA 65489. (M)
- [SDR USAA990933](https://openairdocs.org/sdr/USAA990933.md): Clip · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK IN RADIUS BS 1040 BETWEEN STRINGER 6R AND STRINGER 7R SHEAR TIE CLIP. FABRICATED NEW SHEAR TIE PER SRM 51-10-02 AND DRAWING 65-46569. (M)
- [SDR USAA990924](https://openairdocs.org/sdr/USAA990924.md): Floorbeam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 344, LBL 49 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-30-51. (M)
- [SDR USAA990923](https://openairdocs.org/sdr/USAA990923.md): Splice · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK, 2 RIVETS WORKING AND CRACKED AT BS 907, STRINGER SPLICE 4L. INSTALLED NEW SPLICE PER SRM 51-10-02. (M)
- [SDR USAA990919](https://openairdocs.org/sdr/USAA990919.md): Bulkhead · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY.300 INCH CRACK AT STATION 178, BULKHEAD LBL 7, 32 INCHES FROM BOTTOM OF BULKHEAD. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08 FIG 209. (M)
- [SDR USAA990917](https://openairdocs.org/sdr/USAA990917.md): Beam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING RON CHECK VISUAL INSPECTION, FOUND 7 EACH 1 INCH BY.50 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES AT BS 360 - BS 380, LT CREASE BEAM INBOARD ANGLE CORROSION LEVEL 1. REMOVED CORROSION WITHIN LIMITS PER SRM 53-10-51. (X)
- [SDR USAA990916](https://openairdocs.org/sdr/USAA990916.md): Floorbeam · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT BS 520, RBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)
- [SDR USAA990915](https://openairdocs.org/sdr/USAA990915.md): Floorbeam · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)
- [SDR USAA990914](https://openairdocs.org/sdr/USAA990914.md): Floorbeam · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 24 CABIN FLOORBEAM UPPER CHORD. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X)
- [SDR USAA990913](https://openairdocs.org/sdr/USAA990913.md): Clip · cracked · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.1250 INCH CRACK AT STA 520 AND STR 16L FRAME TIE CLIP. REMOVED AND REPLACED TIE CLIP PER BOEING DWG 65-46534 SHEET 3 AND SRM 51-10-02. (X)
- [SDR USAA990885](https://openairdocs.org/sdr/USAA990885.md): Floorbeam · corroded · Sep 27, 1999 · N342US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 328, LBL 20, TO RBL 50 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51. (M)
- [SDR USAA990920](https://openairdocs.org/sdr/USAA990920.md): Skin · cracked · Sep 20, 1999 · N342US · Boeing 737301 · Leading Edge Devices
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 EACH,.50 INCH CRACKS, NR 1 SLAT INBOARD EDGE OF LOWER SKIN AFT FASTENER ROW. INSTALLED DOUBLER PER BOEING DWG 65C30133 AND TR 57-50-01 REV H. (X)
- [SDR USAASB98064](https://openairdocs.org/sdr/USAASB98064.md): Line · loose · Mar 15, 1998 · N342US · Boeing 737301 · Air Data Computer
  > IAH - FLT1840 - SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FEET, THE FIRST OFFICERS AIRSPEED INDICATOR AND ALTIMETER BECAME UNRELIABLE. CAPTAINS SIDE WAS OPERATIONAL ALONG WITH THE STANDBY INSTRUMENTS. FLIGHT RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURT
- [SDR USAASB98032](https://openairdocs.org/sdr/USAASB98032.md): Transmitter · failed · Feb 6, 1998 · N342US · Boeing 737301 · Trailing Flap Position Indicating System
  > PIT - FLT 544 - AFTER TAKEOFF AND DURING FLAP RETRACTION, CAPTAIN REPORTED THAT THE TRAILING EDGE FLAPS WOULD NOT RETRACT TO THE UP POSITION BUT WOULD RETRACT TO BETWEEN FLAP POSITION 1 AND 2. CAPTAIN ACCOMPLISHED ALTERNATE FLAP EXTENSION PROCEDURE TO EXTEND
- [SDR USAASB97128](https://openairdocs.org/sdr/USAASB97128.md): Sensor · malfunctioned · May 12, 1997 · N342US · Boeing 737301 · Cabin Pressure Sensor
  > CLT - FLT 1594, DURING CRUISE FL350, THE CABIN ALT WARNING HORN WENT OFF AT 10,000 FT CABIN ALT. ALL SYS'S APPEARED TO BE OPERATING NORMAL WITH NO INDICATION OF SYS MALFUNCTION. AT THE TIME OF WARNING HORN, CABIN WAS CLIMBING AT 400 FPM. COULD NOT CONTROL T
- [SDR 97ZZZM734](https://openairdocs.org/sdr/97ZZZM734.md): Thermostat · malfunctioned · May 12, 1997 · N342US · Boeing 737301 · Cabin Temperature Controller
  > CLT - FLT 1594, DURING CRUISE FL350, THE CABIN ALT WARNING HORN WENT OFF AT 10,000 FT CABIN ALT. ALL SYS'S APPEARED TO BE OPERATING NORMAL WITH NO INDICATION OF SYS MALFUNCTION. AT THE TIME OF WARNING HORN, CABIN WAS CLIMBING AT 400 FPM. COULD NOT CONTROL T
- [SDR USAASB97106](https://openairdocs.org/sdr/USAASB97106.md): Flow Contl Valv · stuck · Apr 17, 1997 · N342US · Boeing 737301 · Cabin Cooling System
  > TPA - FL 1515 - EN ROUTE CUN, CABIN ALTITUDE WARNING HORN SOUNDED WITH CABIN INDICATOR SHOWING 10,000 FEET. CREW PERFORMED DESCENT TO 10,000 FEET. FLIGHT DIVERTED TO TPA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED PRESSURIZATION PANEL AND PRES
- [SDR USAASB97074](https://openairdocs.org/sdr/USAASB97074.md): Mec · malfunctioned · Mar 8, 1997 · N342US · Boeing 737301 · Fuel Control/Turbine Engines
  > PHL - FL 8550 - CAPTAIN REPORTED HE DIVERTED TO PHL DUE TO FLUCTUATING LEFT ENGINE PARAMETERS AND THROTTLE STAGGER. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE MAIN ENGINE CONTROL
- [SDR 97ZZZM476](https://openairdocs.org/sdr/97ZZZM476.md): Pmc · malfunctioned · Mar 8, 1997 · N342US · Boeing 737301 · Fuel Controlling System
  > PHL - FL 8550 - CAPTAIN REPORTED HE DIVERTED TO PHL DUE TO FLUCTUATING LEFT ENGINE PARAMETERS AND THROTTLE STAGGER. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE MAIN ENGINE CONTROL
- [SDR USAASB95019](https://openairdocs.org/sdr/USAASB95019.md): Controller · failed · Nov 30, 1995 · N342US · Boeing 737301 · Cabin Pressure Controller
  > PHL - FLT NR 2169 - EN ROUTE LGA TO FLL, PRESSURIZATION FAILED. FLIGHT DESCENDED TO 10,000 FEET AND DIVERTED TO PHL. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. BITE AND OPS CHECKED NORMAL. (M)
- [SDR USAA950946](https://openairdocs.org/sdr/USAA950946.md): Angle · corroded · Aug 30, 1995 · N342US · Boeing 737301 · Fuselage Miscellaneous Structure
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREA BS 294.5 ON Z ANGLE. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)

Next page: https://openairdocs.org/deregistered/N342US-2003-10-16/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 = 'N342US' AND deregistration_id = 'N342US-2003-10-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N342US-2003-10-16/reports

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