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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 FSDR 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.SDR 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 RSDR 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-SDR 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 737SDR 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 BSDR 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 DRAWINSDR 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 CHORSDR 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 FABRICASDR 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. INSTALLSDR 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 ERSDR 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 STRASDR 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 SDR 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 ASDR 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 BOEINSDR 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 PARTSDR 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 PARTSDR 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 ASDR 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 03-5310-0528SDR 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 BOSDR 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 ASDR 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 FILLERSDR 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 NEWSDR 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 FISDR 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. FABRICATSDR 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.SDR 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 PERFORSDR 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 SDR 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 REPAISDR 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.SDR 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-RC1SDR 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 SDR 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 STABILSDR 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 BOEISDR 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 BOEISDR 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 SWSDR 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. SDR 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 SDR 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. ASDR 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 51-40-02-0SDR 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 OCSDR 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 INSTSDR 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 INTERCOSDR 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 737-300SDR 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 IAWSDR 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 205SDR 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.SDR 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 SDR 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 SRMSDR 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. OPERATIONAL
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