Boeing 737-3S3

Service difficulty reports · 1,209

Newest first. General aviation reporting is voluntary.

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 = '7373S3'
  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 AWXA200501204Stop Fitting · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED L1 DOOR UPPER AFT STOP FITTING ON DOOR CRACKED, 1.0 INCHES IN LENGTH, AT BS 344 AND STR 8L. MAINTENANCE REMOVED CRACKED UPPER AFT STOP FITTING IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW UPPER AFT STOP FSep 27, 2005 · N314AW · Boeing 7373S3 · Passenger/Crew DoorsSDR AWXA200501247Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STR 16L CLIP CRACKED, .3 INCHES, BETWEEN BS 348. MAINTENANCE REMOVED STR 16L CLIP AND REPLACED WITH NEW FABRICATED PART AT BS 348 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5310-05285-ES5.Sep 24, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501246Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STRINGER 16L CLIP CRACKED, .35 INCHES, BETWEEN BS 348.2 AND BS 351.2. MAINTENANCE REMOVED STR 16L CLIP AND REPLACED WITH NEW FABRICATED PART BETWEEN BS 348.2 AND BS 351.2 IAW AMERICA WEST AIRLINES ENGINEERING RSep 24, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501240Stringer Clip · crackedDURING C18 CHECK DISCOVERED CLIP CRACKED, .05 INCHES, AT STR 16L AND BS 348. REMOVED CLIP AT STR 16L AND BS 348.1 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5285-ES5. FABRICATED NEW CLIP AND INSTALLED AT BS 348 AND STR 16L IAW AWA ER NR 03-5310-Sep 24, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501232Stringer Clip · corrodedDURING C18 CHECK DISCOVERED EXFOLIATION CORROSION LOCATED AT AFT CARGO COMPARTMENT ON A STRINGER TIE AT BS 727D AND STR 26L. MAINTENANCE REMOVED STRINGER TIE IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW STRINGER TIE AT BS 727D AND STR 27L IAW BOEING 737Sep 24, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501197Skin · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED THE NR 5 SLAT LOWER SKIN CRACKED, .750 INCHES IN LENGTH, APPROXIMATELY 39 INCHES FROM INBOARD SIDE, UNDER THE CENTER AUXILIARY TRACK AT SS 163.53. MAINTENANCE REMOVED DAMAGED PART OF SKIN ON THE NR 5 SLAT IAW BSep 24, 2005 · N314AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200501271Frame · crackedMCN - DURING C18 CHECK DISCOVERED FRAME ANGLE CRACKED, .375 INCHES IN LENGTH, AT BS 500D AND STR 13L. MAINTENANCE REMOVED FRAME ANGLE FROM STR 11L TO STR 13L AND BS 500D IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT FRAME ANGLE IAW BOEING DRAWINSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, FrameSDR AWXA200501270Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED CORROSION ON THE TOP OF UPPER CHORD FROM BL 32R TO BL 38R, WL 208 AND BS 294. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. MAINTENANCE FABRICATED REPAIR CHORSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Floor BeamSDR AWXA200501239Angle · crackedDURING C18 CHECK DISCOVERED ANGLE CRACKED, .05 INCHES IN LENGTH, AT BS 348 AND STR 15L. MAINTENANCE REMOVED CRACKED ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05285-ES4. FORMED NEW ANGLE IAW AWA ER NO. 03-5310-05285-ES4. INSTALLED FABRICASep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200501238Attach Angle · crackedDURING C18 CHECK DISCOVERED ATTACH ANGLE CRACKED, .375 INCHES IN LENGTH, FROM BS 927 TO BS 947, WL 207 AND BL 0. MAINTENANCE REMOVED CRACKED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G. FORMED NEW ATTACH ANGLE IAW BOEING 737-300 SRM 51-30-01-0G. INSTALLSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501237Frame · crackedDURING C18 CHECK DISCOVERED FRAME ANGLE CRACKED, .5 INCHES IN LENGTH, AT BS 400 AND STR 14L. MAINTENANCE TRIMMED OUT CRACK ON FRAME IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5332-05284-HF1. FABRICATED REPAIR ANGLE, SPLICE ANGLE AND FILLER IAW AWA ERSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, FrameSDR AWXA200501228Floorbeam · crackedDURING C18 CHECK DISCOVERED 2 CRACKS, .75 INCHES IN LENGTH, ON FLOORBEAM UPPER CHORD AT BS 727B AND BL 45L. MAINTENANCE TRIMMED OUT CRACK AT BS 727B AND BL 24L IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-4702-05280-DF1. FABRICATED FILLER, REPAIR STRASep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Floor BeamSDR AWXA200501202Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED GALVANIC CORROSION ON THE TOP OF BEAM AT BS 328, WL 208 AND FROM BL 27R TO BL 33R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. CUT OUT DAMAGED AREA OF BEAM Sep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Floor BeamSDR AWXA200501201Stringer · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STRINGER 16L CRACKED AT BS 500C. MAINTENANCE REMOVED CRACKED END OF STRINGER IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REQUEST (ER) 03-5312-01094-001 FIG 6. FABRICATED FILLER, CHANNEL AND RADIUS FILLER IAW ASep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Longeron/StringerSDR AWXA200501199Channel · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED CHANNEL CRACKED IN 2 PLACES AT WL 207, BL 47L BS 313 AND BS 327. MAINTENANCE REMOVED DAMAGE CHANNEL AT BS 313 AND BS 327 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. PREPPED NEW CHANNEL FOR INSTALLATION IAW BOEINSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200501192Stringer Clip · crackedMCN - DURING C18 CHECK DISCOVERED STRINGER TIE CLIP CRACKED .4 INCHES IN LENGTH LOCATED AT BS 500A AND STR 16R. MAINTENANCE REMOVED STRINGER TIE CLIP AND FABRICATED NEW CLIP IAW BOEING 737-300 SRM 51-40-05-0G FIG 3 AND FIG 7. INSTALLED FABRICATED REPAIR PARTSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501191Stringer Clip · crackedMCN - DURING C18 CHECK DISCOVERED STRINGER TIE CLIP CRACKED .375 INCHES IN LENGTH LOCATED AT BS 360 AND STR 4L. MAINTENANCE REMOVED STRINGER TIE CLIP AND FABRICATED NEW CLIP IAW BOEING 737-300 SRM 51-40-05-0G FIG 3 AND FIG 7. INSTALLED FABRICATED REPAIR PARTSep 23, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200501236Intercostal · crackedDURING C18 CHECK DISCOVERED INTERCOSTAL CRACKED, .375 INCHES IN LENGTH, AT STR 12L AND BS 294.5. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294.5 IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5310-5285-ES4. FABRICATED NEW INTERCOSTAL AND INSTALLED ASep 22, 2005 · N314AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200501234Channel · crackedDURING C18 CHECK DISCOVERED CHANNEL CRACKED, .5 INCHES IN LENGTH, AT STR 15L AND BS 360. MAINTENANCE REMOVED CRACKED CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05285-ES4. FABRICATED NEW CHANNEL IAW DWG 65-61777 AND AWA ER NR 03-5310-0528Sep 22, 2005 · N314AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200501203Skin · debondedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 1 SPOILER, APPROXIMATELY 6 INCHES FROM INBOARD EDGE, FROM WBL 398.50L TO WBL 408.50L. MAINTENANCE REMOVED DISBOND AREA AND CORE FROM NR 1 SPOILER LOWER SURFACE IAW BOSep 22, 2005 · N314AW · Boeing 7373S3 · SpoilersSDR AWXA200501272Support Angle · crackedMCN - DURING C18 CHECK DISCOVERED TWO CRACKS, .890 INCHES EACH, LOCATED AT THE AFT PIT DOOR INNER CHORD AND SUPPORT ANGLE AT BS 800 AND STR 20R. MAINTENANCE REMOVED SUPPORT ANGLE AND CHORD IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. FABRICATED REPAIR DOUBLER ASep 21, 2005 · N314AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200501231Stringer · crackedDURING C18 CHECK DISCOVERED CRACK, 1.7 INCHES IN LENGTH, AT STRINGER 18A ON WEB JUST FORWARD OF BS 727. MAINTENANCE TRIMMED OUT CRACK AT BS 727 AND STR 18A IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5361-05285-ES1. FABRICATED FILLER AND RADIUS FILLERSep 21, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, Longeron/StringerSDR AWXA200501200Frame · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED FORWARD CARGO COMPARTMENT DOOR FRAME CRACKED, 1.5 INCHES IN LENGTH, AT THE UPLOCK AT BS 445 AND STR 24R. MAINTENANCE REMOVED THE CRACKED FRAME IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 11. INSTALLED NEWSep 21, 2005 · N314AW · Boeing 7373S3 · Fuselage Main, FrameSDR AWXA200501195Skin · debondedDURING C18 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE RT INBOARD AFT FLAP, FROM WS 230.68 TO WS 236.68. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATED DOUBLER AND FISep 21, 2005 · N314AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200501194Skin · debondedMCN - DURING C18 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE LT OUTBOARD AFT FLAP, 25" FROM INBOARD END FROM WS 254.68 TO WS 256.68. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATSep 21, 2005 · N314AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200501193Wedge · debondedMCN - DURING C18 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD END OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, LOWER SURFACE FROM WS 176.5 TO WS 183.0. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202.Sep 21, 2005 · N314AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200501031Warning Light · illuminatedFLT 122 - REJECTED TAKEOFF, AT 70 KNOTS, IN PHX FOR NR 1 ENGINE OVER TEMP. CREW REPORTED THE NR 1 ENGINE EGT REACHED 930 DEG AND RED LIGHT ILLUMINATED FOR LESS THAN A COUPLE SECONDS. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORSep 7, 2005 · N314AW · Boeing 7373S3 · Engine EGT/TIT Indicating SystemSDR AWXA200500912Indicator · inoperativeLAS - ABORTED TAKEOFF - FLT 831 - DURING TAKEOFF, CAPTAINS AIRSPEED INDICATOR FLAGGED. REJECTED TAKEOFF AT 90 KNOTS. CREW RESET ADC NR 1 CIRCUIT BREAKER PER MAINTENANCE CONTROL. FLIGHT CONTINUED ON WITHOUT FURTHER INCIDENT. A FOLLOW UP HAS BEEN WRITTEN TO Aug 6, 2005 · N312AW · Boeing 7373S3 · Airspeed/Mach IndicatorSDR AWXA200500931Frame · crackedDURING C18 CHECK, FOUND FUSELAGE FRAME CRACKED, .50 INCHES IN LENGTH, AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA. MAINTENANCE REMOVED CRACK FROM INNER CHORD FRAME AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIJul 31, 2005 · N313AW · Boeing 7373S3 · Fuselage Main, FrameSDR AWXA200500927Power Unit · inoperativeDURING C18 CHECK DISCOVERED AFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT SEAT FLASHLIGHT POWER UNIT AS REQUIRED. OPERATIONAL CHECKS WERE GOOD.Jul 28, 2005 · N313AW · Boeing 7373S3 · Emergency LightingSDR AWXA200500996Floorbeam · crackedMCN - DURING C18 CHECK, DISCOVERED INNER CHORD CRACKED, 1 INCH, IN CABIN AREA, BS 616, WL 208, BL 60R. MAINTENANCE CUT OUT DAMAGED SECTION OF INNER CHORD AT BS 616, WL 208, BL 60R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NUMBER 03-5361-0522-RC1Jul 24, 2005 · N313AW · Boeing 7373S3 · Fuselage Main, Floor BeamSDR AWXA200500923Web · crackedDURING C18 CHECK DISCOVERED WEB CRACKED, 2.3 INCHES IN LENGTH, IN THE CABIN AREA AT BS 616, BL 60R, WL 208. MAINTENANCE REMOVED CRACKED WEB AT BS 616, BL 60R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW WEB AND PREPARED FOR INSTALLATION IAW Jul 24, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500958Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING. CORROSION WAS REMOVED IAW BOEING 737-300 SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW BOEING 7 37-300 SRM 57-20-90-1 FIG 102. MAINTENANCE REMOVED THE RT MLG STABILJul 18, 2005 · N313AW · Boeing 7373S3 · Wing, Attach FittingsSDR AWXA200500929Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE LT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE LT MLG STABILIZER BEAM IAW BOEIJul 18, 2005 · N313AW · Boeing 7373S3 · Wing, Attach FittingsSDR AWXA200500928Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE RT MLG STABILIZER BEAM IAW BOEIJul 18, 2005 · N313AW · Boeing 7373S3 · Wing, Attach FittingsSDR AWXA200500825Switch · failedDURING FLT AUTO FAIL LIGHT ON PRESSURE CONTROLLER ILLUMINATED WITH CABIN HORN COMING ON. SWITCHED TO STANDBY AND DESCENDED. MASKS DID DEPLOY. EMERGENCY NOT DECLARED AND AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND AIR/GROUND SWJul 18, 2005 · N312AW · Boeing 7373S3 · Cabin Pressure ControllerSDR AWXA200500926Stringer · crackedDURING C18 CHECK DISCOVERED STRINGER 8L CRACKED, 1.125 INCHES IN LENGTH, AT BS 380. MAINTENANCE CUT OUT CRACK ON STRINGER 8L, BS 380, IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. FABRICATED TWO ZEE ANGLES AND FILLER IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. Jul 17, 2005 · N313AW · Boeing 7373S3 · Fuselage Main, Longeron/StringerSDR AWXA200500920Bolt · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. NO CORROSION REMOVAL LIMITS AVAILABLE FOR RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. MAINTENANCE REMOVED AND REPLACED BOLTS ON THE LT Jul 17, 2005 · N313AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200500813Bulb · burned outON DESCENT, WHEN GEAR EXTENDED, LT MLG LIGHTS WOULD NOT ILLUMINATE. AIRCRAFT FLEW BY TOWER AND MANUALLY CHECKED GEAR TO ENSURE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BULBS AND CYCLED GEAR SEVERAL TIMES. AJul 17, 2005 · N315AW · Boeing 7373S3 · Landing Gear Position and WarningSDR AWXA200500908Stringer Clip · crackedDURING C18 CHECK DISCOVERED STRINGER TIE CRACKED, .200 INCHES IN LENGTH, AT BS 312, STR 28R. MAINTENANCE REMOVED STRINGER TIE AT BS 312, STR 28R, IAW BOEING 737-300 SRM 51-40-02. INSTALLED NEW STRINGER TIE AT BS 312, STR 28R IAW BOEING 737-300 SRM 51-40-02-0Jul 16, 2005 · N313AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200500832Warning System · false activationDURING TAKEOFF RECIEVED TAKEOFF CONFIGURATION WARNING. ABORTED TAKEOFF. CREW TAXIED BACK AND DEPARTED NORMALLY. AWAITING SAFTEY EVENT REPORT, FROM PILOT, TO DETERMINE CAUSE OF T/O CONFIG WARNING AND SPEED THAT AIRCRAFT ABORTED T/O AT. THIS IS THE SECOND OCJul 16, 2005 · N316AW · Boeing 7373S3 · Central WarningSDR AWXA200500995Stiffener · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON THE BOTTOM OF FLOOR SUPPORT STIFFENER AT RBL 11, WL 208, BS 297 TO BS 308. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED STIFFENER AND PREPARED NEW STIFFENER FOR INSTJul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Main, Floor BeamSDR AWXA200500942Web · crackedDURING C18 CHECK DISCOVERED L1 DOOR CUTOUT WEB CRACKED, .5 INCHES IN LENGTH, AT THE FORWARD INBOARD SIDE AT BS 294.5, STRINGER 12L. MAINTENANCE REMOVED THE L1 DOOR CUTOUT AT BS 294.5, STRINGER 12L WEB IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW INTERCOJul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500941Angle · corrodedDURING C18 CHECK DISCOVERED CORROSION ON FLOOR WEB ANGLE AT BS 270, FROM BL8L TO BL8R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. MAINTENANCE REMOVED DAMAGED SECTION ON ANGLE AT BS 270, BL8L TO BL8R IAW BOEING 737-300Jul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500940Angle · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE R1 INNER CHORD, UPPER ANGLE AT BS 305 TO BS 324, BL 58R, WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-13-1 FIG 101. MAINTENANCE REMOVED ANGLE AT BS 305 TO BS 324, BL 58R, WL 209 IAWJul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500933Beam · corrodedDURING C18 CHECK DISCOVERED CORROSION ON BS 312 BEAM FROM BL 0 TO BL 21R, WL 208. PREVIOUS BLEND OUT PRESENT, MATERIAL LOSS GREATER THAN ALLOWED, IAW BOEING 737-300 SRM 53-10-51-1. MX CUT OUT DAMAGED SECTION OF BEAM IAW BOEING 737-300 SRM, 53-10-51-2 FIG 205Jul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500833Support Angle · crackedMCN - MAJOR REPAIR - DISCOVERED, DURING C16 CHECK, L1 DOOR CUTOUT SIDEWALL LINER SUPPORT ANGLE CRACKED AT BS 344, ST 14L. MAINTENANCE REMOVED THE DAMAGED AREA ON THE SUPPORT ANGLE FOR THE L1 DOOR CUTOUT SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1.Jul 15, 2005 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200500812Generator · malfunctionedNR 1 ENGINE GENERATOR HAD LOW OIL PRESSURE AND HIGH OIL TEMP. DISCONNECTED GENERATOR AND RETURNED TO GEG. APU WAS ON MEL. MX R & R APU BLEED VALVE, CLEARED APU MEL. ISSUED MEL FOR NR 1 ENGINE GENERATOR. VENDOR TEAR DOWN REPORT SHOWS THAT CSD HAD VERY HIGH Jul 15, 2005 · N315AW · Boeing 7373S3 · Alternator-Generator DriveSDR AWXA200500997Skin · debondedMCN - DURING C18 CHECK, DISCOVERED DISBOND AREA ON TOP SURFACE OF THE NR 3 SLAT AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLER AND CORE IAW BOEING 737-300 SRMJul 14, 2005 · N313AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200500984Skin · crackedMCN - DURING C18 CHECK, DISCOVERED FOUR CRACKS IN THE NR 1 SLAT, .250 INCHES IN LENGTH, LOCATED AT THE LOWER SKIN AT OUTBOARD END SS 385. MAINTENANCE REMOVED AND REPLACED THE NR 1 SLAT IAW BOEING 737-300 AMM 27-81-21-004-001 AND 27-81-21-404-002. OPERATIONALJul 14, 2005 · N313AW · Boeing 7373S3 · Leading Edge Devices
Back to Boeing 737-3S3