Boeing 737-301

Service difficulty reports · 4,797

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Query with SQL
duckdb -csv -c "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 aircraft_model_key = '737301'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA96006B-Nut · looseSNA/PHX - FLT 0207 - FUEL LEAK SUSPECTED ON NR 2 ENGINE. OCCURRED DURING START AND APPEARS TO BE UNDER PRESSURE, NO SHAFT LEAK DETECTED. LOCATED AND RETORQUED LOOSE B-NUT TO M.E.C. FUEL INLET LINE AT FORWARD STRUT THROUGH-FITTING. RAN ENGINE. LEAK CHECK GOJan 6, 1996 · N326AW · Boeing 737301 · Engine Fuel DistributionSDR USAASB96002Press Selector · failedFLT NR 1440 - MCO - ON TAKEOFF FROM PBI, AIRCRAFT WOULD NOT PRESSURIZE. SELECTED STANDBY THEN MANUAL, NO HELP, OUTFLOW VALVE FULL CLOSED. MAINTENANCE REPLACED PRESSURIZATION SELECTOR PANEL. PRESSURIZED AIRCRAFT ON GROUND AT MCO. OPS CHECKS OK. (M)Jan 5, 1996 · N350US · Boeing 737301 · Cabin Pressure Control SystemSDR W8PA9491Solenoid · failedAFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE UP PAST THE OFF POSITION. AIRCRAFT RETURNED TO COS. FOUND M-241 LEVER LATCH SOLENOID DEFECTIVE. REMOVED AND REPLACED SOLENOID. (X)Dec 21, 1995 · N949WP · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAASB95030Passenger Door · not closedPHL - FLT 451 - UNABLE TO PRESSURIZE AIRCRAFT. FOLLOWED ALL USAIR PROCEDURES, NO HELP. F/A ADVISED IN PHL THAT THE DOOR WAS HARD TO SHUT. ALSO, HAD TO SHUT DOWN AND RESTART LEAVING DCA PRIOR TO STARTING ENGINE. THERE WAS A PRESSURE BUMP. FOUND CABIN DOOR Dec 17, 1995 · N350US · Boeing 737301 · Passenger/Crew DoorsSDR USAASB95019Controller · failedPHL - 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)Nov 30, 1995 · N342US · Boeing 737301 · Cabin Pressure ControllerSDR USAASB95013Hyd Pump · failedIND - FLIGHT NR 0133 - RIGHT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM HYDRAULIC QUANTITY DROPPED TO ONE QUARTER. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND SERVICED HNov 12, 1995 · N334US · Boeing 737301 · Hydraulic Pump (Electric/Engine), MainSDR USAASB95010Contl Alternator · leakingPIT - FLT 0223 - EN ROUTE IND TO BWI, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED TO RED LINE. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND DIVERTED TO PIT. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED RT ENGINE N2 ALTERNATOR AND ROTOR DUENov 7, 1995 · N589US · Boeing 737301 · Engine RPM Indicating SystemSDR AWXA9500726Sensor · badLAS/DEN - FLT NR 749 - WHEN GEAR HANDLE WAS RAISED ON TAKEOFF, THE RED LIGHT ILLUMINATED AND REMAINED ON. GEAR WAS RECYCLED WITH NO HELP. AIRCRAFT RETURNED TO LAS LANDING UNEVENTFULLY. MAINTENANCE FOUND S846 NOSE LOCK SENSOR BAD. REMOVED ADN REPLACED SENSONov 3, 1995 · N325AW · Boeing 737301 · Landing Gear Position and WarningSDR USAASB95007Oil Temp Bulb · failedMCO - FLT NR 0417 - EN ROUTE FLL TO PIT, NR 1 ENGINE OIL TEMP CLIMBED ABOVE RED RADIAL. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER PILOTS HANDBOOK. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED ALL CHIP DETECTORS, NO PROBLEMS FOct 31, 1995 · N300AU · Boeing 737301 · Engine Oil TemperatureSDR W8PA9502Actuator · bypassingCOS - RIGHT ENGINE THRUST REVERSER OVERHEAD LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND NR 2 THRUST REVERSER OUTBOARD CENTER ACTUATOR BYPASSING. REPLACED ACTUATOR. ALSO, ADJUSTED THRUST REVERSER TARGETS ON SWITCHES S-831 AND S-832Oct 30, 1995 · N301AU · Boeing 737301 · Engine Thrust ReverserSDR USAASB95005Oil Qty Xmitter · failedSTL - FLT NR 0091 - EN ROUTE FROM PIT TO SAN, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE WAS FLUCTUATING BETWEEN 35 AND 40 PSI. FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED TO STL WHERE LANDING WAS WITHOUT INCIDENT. MAINTOct 28, 1995 · N592US · Boeing 737301 · Engine Oil Indicating SystemSDR USAASB95002Oil Cooler · blockedEWR - FL 1468 - EN ROUTE DCA-BOS, WITH THE NR 1 GENERATOR ON MEL AND THE APU RUNNING, THE APU SHUT DOWN DUE TO HIGH OIL TEMPERATURE. FLIGHT DIVERTED TO EWR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND COULD NOT FIND A PROBLEM WITH THE APUOct 22, 1995 · N354US · Boeing 737301 · APU Oil SystemSDR USAASB95001Generator · failedCLT - FL 2040 - EN ROUTE TO LGA, CREW NOTED PERIODIC SPIKING FROM THE NR 1 GENERATOR, WHICH CAUSED TR NR 1 CIRCUIT BREAKER TO TRIP. CREW DISCONNECTED THE GENERATOR, AND COULD NOT GET THE APU TO START. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER PROBLEMOct 21, 1995 · N354US · Boeing 737301 · AC Generator-AlternatorSDR USAA951132Skin · damagedROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, FORWARD SERVICE DOOR, TOP AND LOWER HINGE, DAMAGED. TWO DOUBLERS INSTALLED, ONE TOP HINGE, AND ONE BOTTOM HINGE, TOP 7 INCHES BY 8 INCHES, BOTTOM 5 INCHES BY 5 INCHES. REPAIREDOct 17, 1995 · N579US · Boeing 737301 · Service DoorsSDR USAA951131Skin · damagedROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, AFT CARGO DOOR. TWO DOUBLERS INSTALLED ONE ABOVE HANDLE, 7 INCHES BY 12.50 INCHES BY 7.50 INCHES BY 21 INCHES. ONE BELOW HANDLE, 8.25 INCHES BY 7.25 INCHES. REPAIRED PER SRM 5Oct 17, 1995 · N579US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA951130Skin · damagedROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR FUSELAGE SKIN BS 927, STR 18L - STR 19L, DAMAGED. ONE DOUBLER INSTALLED 12 INCH BY 10.50 INCH. REPAIRED PER SRM 53-00-01. (X)Oct 17, 1995 · N579US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA9500688Outflow Valve · failedLAS/LAX - FLT 707 - DURING TAKEOFF/CLIMB, AIRCRAFT WAS UNABLE TO BE PRESSURIZED. CREW RETURNED AIRCRAFT TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FORWARD OUTFLOW VALVE INOPERATIVE. REMOVED AND REPLACED FORWARD OUTFLOW VALVE. AIRCRAFT REOct 9, 1995 · N324AW · Boeing 737301 · Pressure Regulator/Outflow ValveSDR USAA951048Trim Switch · failedDAY - FLT 0223 - EN ROUTE IND TO BWI, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT FULL RUDDER TRIM. CREW DISCONNECTED THE AUTOPILOT AND YAW DAMPER WITH NO EFFECT. FLIGHT DIVERTED TO DAY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RUDDER TRIM Sep 29, 1995 · N563AU · Boeing 737301 · Rudder Control SystemSDR USAA951010Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5. FABRICATED NEW INTERCOSTAL FROM BAC1506-437075-T6 AND INSTALLED. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 21, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951034Skin · mis mfgCLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L. INSTALLED PROTRUDING HEAD RIVET 211TT3. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951033Doubler · damagedCLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R. VISUALLY INSPECTED. PREVIOUS REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951032Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L. PREVIOUS REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951031Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND. EXISTING REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951030Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L. EXISTING REPAIR, DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951013Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR. REPAIRED PER BOEING DRAWING 65-52878. CORROSION LEVEL 2. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (M)Sep 19, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951011Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING 65C80735. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951009Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER. REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951012Angle · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING NR 6545875. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Sep 12, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950977Skin · dentedROA - DURING 'FULL C' CHECK VISUAL INSPECTION, FOUND 6 INCH BY 3 INCH DENT BETWEEN STATION 1040 AND STATION 1064 LOWER RIGHT AFT FUSELAGE. INSTALLED DOUBLER, REPAIR DOCUMENT SRM 53-00-01 PAGE 204. (M)Sep 11, 1995 · N578US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951007Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Sep 8, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951008Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES. REPLACED UPPER T-CAP OF BEAM. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Sep 6, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950964Engine · failedPHL - FLT NR 0803 - ON CLIMB-OUT FROM PHL, PASSING THROUGH 7500, NR 1 ENGINE FAILED. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO PHL. LANDING WAS WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REPLACED THE LEFT ENGINE ASSEMBLY. (M)Aug 31, 1995 · N354US · Boeing 737301 · Engine (Turbine/Turboprop)SDR USAA950946Angle · corrodedINT - 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)Aug 30, 1995 · N342US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950947Angle · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 25 INCH CORROSION AT BS 857 TO BS 787 ON FLOOR SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE SECTION INCLUDING DOUBLER AND FILLER. ALSO, COMPLETED JOGGLE MOD AT STATION 852 SRM 53-00-53 FIG 202. CORROSIAug 29, 1995 · N342US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951026Skin · damagedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH ROUND HOLE IN SKIN (PRIOR REPAIR CLEANUP) LOCATED FS 935, STRINGER 18 RT. INSTALLED DOUBLER. (M)Aug 22, 1995 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951024Floor Beam · crackedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.4 INCH CRACK LOCATED AT STATION 520 EXTENDING .6 INCH OUTBOARD AND .8 INCH INBOARD OF LBL 45.5. INSTALLED DOUBLER. (M)Aug 22, 1995 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA951029Skin · crackedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A .9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH OF RBL 45.5. INSTALLED DOUBLER. (M)Aug 18, 1995 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951028Skin · crackedCLT - DURING A Q-3 CHECK INSPECTION, VISUALLY FOUND A 1.9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING .9 INCH OUTBOARD AND 1 INCH INBOARD OF LBL 24.75. INSTALLED DOUBLER. (M)Aug 18, 1995 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951027Skin · crackedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.8 INCH CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75. INSTALLED DOUBLER. (M)Aug 18, 1995 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA950908Frame · damagedCLT - DURING AN UNSCHEDULED MAINTENANCE CHECK INSPECTION, FOUND A DEEP CUT BY TOOLING WHEEL LOCATED AT FRAME 360, S-4 RT TO S-4 LT. INSTALLED REPAIR DOUBLE SECTION. (X)Aug 18, 1995 · N558AU · Boeing 737301 · Fuselage Main, FrameSDR USAA950897Eel Battery Pack · dischargedLGA - THE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK FOR ROW 12 TO 16. OPERATIONS CHECKED GOOD. (M)Aug 18, 1995 · N334US · Boeing 737301 · Emergency LightingSDR USAA951025Skin · corrodedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY INSPECTED AND FOUND A 1 INCH SKIN BULGE AND CHUNK MISSING BETWEEN STRINGER 21-20 RIGHT STATION 492.4. INSTALLED DOUBLER. (M)Aug 16, 1995 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA9500553Eel Wire · brokenPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT 5ABC. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (X)Aug 16, 1995 · N325AW · Boeing 737301 · Emergency LightingSDR W8PA9501Tr Prox Switch · out of adjustFLT 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M)Aug 15, 1995 · N301AU · Boeing 737301 · Engine Thrust ReverserSDR USAA950944Floor Track · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AND .5 BY 1 INCH CORROSION AT NUT PLATE BS 737 TO BS 797. FABRICATED NEW FLOOR TRACK AND INSTALLED, REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Aug 15, 1995 · N342US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR 9501W8PAStow Prox Switch · out of adjustFLT NR 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M)Aug 15, 1995 · N301AU · Boeing 737301 · Engine Thrust ReverserSDR USAA950945Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 986 BL ZERO TO LBL 20 INCHES ON FLOOR BEAM. INSTALLED REPAIR DOUBLERS, REPAIRED PER TR 53-10-01A. (M)Aug 9, 1995 · N342US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950840Door · ajarPHL - FLT NR 1487 - RETURN TO FIELD DUE TO THE AFT CARGO DOOR LIGHT ILLUMINATING. MAINTENANCE FOUND THE REAR CARGO DOOR AJAR. VISUAL AND MECHANICAL INSPECTION CHECKS GOOD. NO DEFECTS OR LIGHT MALFUNCTION NOTED. (M)Aug 8, 1995 · N334US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA950846Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 12 INCH AND .5 INCH BY 14 INCH CORROSION, BS 985.6 AT LBL 43 INCHES - RBL 30 INCHES ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED T-CAP ON FLOOR BEAM, REPAIRED PER TR 53-1Aug 1, 1995 · N338US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950973Skin · crackedCLT - FOUND TWO CRACKS APPROXIMATELY 4 INCHES LONG LOWER FUSELAGE SKIN, 1 INCH LEFT AND 1 INCH RIGHT OF BL-0, STATION 727 D DIRECTLY BELOW VHF ANTENNA. VISUALLY INSPECTED. INSTALLED DOUBLER. (M)Jul 26, 1995 · N341US · Boeing 737301 · Fuselage Main, Plate/Skin
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