JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), newest first.
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 jasc_code = '5300' 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 jasc_code = '5300' 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 UALA2010042001315Structure · unknownDOOR 4 LT & RT DOOR STOP TEE CLIP. ACP COA 506902 ON TASK CARD 5C0690201 BY INSP Q816. NO CRACKS FOUND.SDR 2011F00132Structure · dentedDURING INSPECTION A VERTICAL DENT 7.O"X2.5" WAS OBSERVED ON LT SIDE IN THE AREA DEFINED FOR RVSM BS259.5, WL 194.SDR ASOA201000476Intercostal · corrodedFWD OF FS 364.00 BETWEEN S26L & S26R THERE IS CORROSION. REMOVED 15 RIVETS THROUGH OUTER SKIN, REMOVED 3 RIVETS FROM ANGLE-ATTACHMENT, REMOVED 7 LOCK FASTENERS FROM GUSSET, REMOVED 4 LOCK FASTENERS FROM PROXIMITY SWITCH BRACKET, REMOVED RT LATCH PIN INTERCOSTSDR ASOA201000349Intercostal · corrodedRIGHT FUSELAGE, ST6R 20R, AT FS319.70 CONNECTION CORRODED (FLAGGED). REMOVED ANGLE IAW SRM 51-42-11. REMOVED GROUND ASSY IAW AMM 51-80-00. REMOVED CORROSION IAW AMM 51-21-06 REMOVED .003 FROM INTERCOSTAL THICKNESS. PAINTED AND TREATED IAW SRM 51-25-00. FSDR UALA2010030100738Unknown · unknownFLAPPING NOISE FROM DOOR 2R AREA, RTFL. CHECKED ALL AREAS ON RT SIDE OF ACFT INCLUDING EE BAY ON BOTH SIDES. CHECKED ALL DOOR SEALS, CARGO COMPT. FWD AND AFT, FWD NOSE GEAR DOORS, AND ALL ACCESS PANEL DOORS. NO PROBLEMS FOUND. CONTACTED OPBLM ABOUT ACTION TSDR ASOA201000109Angle · cracked70 PERCENT FSH HFEC INDICATION NOTED 0.2" LONG EXTENDING FROM THE BOTTOM FASTENER OF THE ESB FWD CLIP AT APPROX FS 625, RBL 27.5, WL 111.0. FAILS NDT INSP AT THIS TIME. RECEIVED NEW SERVICEABLE PART FROM STOCK. DRILLED AND INSTALLED NEW SERVICEABLE ANGLE FORSDR UALA2010011500178Unknown · leaking38E, OVRHEAD BIN, STILL DRIPPING WATER, SEEMS TO BE ONLY IN FLIGHT. REPLACED SEVERAL CROWN ARE A INSULATION BLANKETS THAT WERE FOUND WET WITH CONDENSATION. REPLACED CEILING PANELS.SDR 2010FA0000106Doubler · corrodedRT LOWER DOUBLER FWD PARTITION AT FR 61 CORRODED OUT OF LIMITS. DOUBLER R & R IAW SRM.SDR 2010FA0000124Doubler · corrodedDOUBLER AT FRAME 20, RY 479 HAS CORROSION. R & R DOUBLER IAW SRM.SDR A6WA200940810Unknown · vibrationAFTER GEAR RETRACTION ON T/O, HEARD LOUD BANGING NOISE COMING FROM NOSE WHEEL AREA. SOUND LASTED 3 TO 5 MIN THEN EXTINGUISHED. DURING WHICH NOSE DOOR OPEN WARNING MSG WAS ON. INSP NOSE GEAR AREA, DOORS, NOSE GEAR, NO DAMAGE NOTED. INSP FUSELAGE, ENGS AND ESDR 2010FA0000131Doubler · corrodedDOUBLER RT .478 FRAME 22 HAS CORROSION. R & R DOUBLER IAW 145 SRM.SDR 2010FA0000130Doubler · corrodedDOUBLER AT RT .479 FRAME 20R HAS CORROSION. R & R DOUBLER IAW SRM.SDR DLM88091959Unknown · damagedFUSELAGE DAMAGE LT SIDE STA 632.5/660.5/679. REPAIRED IAW ERA 478513-14.SDR VNAA2009101200004Skin · damagedCREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT AT TRI. MAINTENANCE INSPECTED AND REPAIRED DENT TO AIRCRAFT. INSPECTIONS AND REPAIRS WERE DONE PER AIRCRAFT MAINTENANCE MANUALS AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR ASOA200901105Angle · crackedRIGHT MID FS 625 OBLIQUE ANGLE IS CRACKED.SDR FDEA200908313155Frame · dentedCABIN - LT STA 1701 LONGERON 11 TO LONGERON 12 FOUND DENT. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 41. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG. 201, REPAIR 2, REVSDR FDEA200908303123Unknown · corrodedCORROSION FOUND STA 859L STR 45. REPAIRED REF: EA 8-5330-133747.SDR FDEA200908293120Unknown · corrodedCORROSION FOUND STA 1884R STR 47. REPAIRED REF: SRM 53-20-00 FIG 6.SDR DXTA2009090803779Cover · installedSHORTLY AFTER TAKEOFF, GOT AMBER EFIS MISCOMPARE MSG FOLLOWED BY AMBER IAS & ALT FLAGS ON BOTH PFD`S. AFTER CONSULTING ACP & MX, DIVERTED. PRIOR TO LANDING HEARD "POP" SOUND & ALL INSTRUMENTS RETURNED TO NORMAL. ON POST FLT, DISCOVERED PINS FOR RT LARGE SQUSDR CA090811002Structure · damagedAUG 09-2009 HS-125 700A INCIDENT REPORT HAIL DAMAGE. ACFT WAS RETURNING TO MAIN BASE FROM A 704 TRIP AND ATC ADVISED CREW OF THUNDER STORM ACTIVITY IN AREA. ACFT WAS HELD IN A HOLDING PATTERN AND THEN CLEARED. BETWEEN 13000FT AND 10000FT ACFT ENTERED AN ARESDR UALA9080502354AFrame · corrodedAFT LOWER FUSELAGE INTERNAL BILGE AREA, SHEAR TIE FWD FACE HAS CORROSION, BS 1681, STR 27L-28L. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE PER BAC DWG 140N2002-1011 AND INSTALLED.SDR FDEA200906182144Angle · corrodedCORRODED "L" ANGLE AT STA 1715, LBL 33.10 TO LBL 39.50, REMOVED AND REPLACED WITH A NEW "L" ANGLE IAW SRM 51-40-02 REV. 97. REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA.SDR QXEA2009060300427Structure · chafedOTBD SIDE OF FRONT APERTURE FOR TURTLE BACK PANEL 262HT IS CHAFED APPROX 2 INCH FROM OTBD EDGE. BLENDED AREA IAW 8/4-53-451 STEP NR 1 PAGE 5. HFEC IAW NDTM PT 6 51-00-01 AND RD 8/4-53-451, NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1 51-00-04 LOW .09SDR QXEA2009060100401Seat Track · corrodedRT OTBD SEAT TRACK AT APPROX FS X373.15 HAS PITTING CORROSION. BLENDED CORROSION IAW RD 8/4-53-884. MAX MATERIAL REMOVED .021", FOUND WITHIN LIMITS. HFEC IAW NDTM PART 6, 51-00-01. NO CRACKS NOTED. ALODINED REPAIR AREA PER RD 8/4-53-884 PG 6 NOTES 4 AND 6SDR QXEA2009050600308Beam · crackedFS 280 BEAM CRACKED ON LOWER FLANGE APPROX 12 INCHES RT FROM CENTERLINE OF ACFT. HFEC INSPECTED SUSPECT CRACK IAW NDTM 51-20-006 CONFIRMED APPROX 1 INCH CRACK. REMOVED RT DRIP TRAY ATTACHING INTERCOSTALS, CAMLOC CHANNEL AND RT SECTION OF 280 BEAM. LOCATED SDR AALA20090430TUL11Frame · crackedCRACK IN FRAME AT FASTENER HOLE AT AIR CONDITIONING RAIL ATTACH POINT AT LEFT STATION 400. LENGTH OF CRACK NOT SPECIFIED BY NDT. REPAIRED PER J1159ABSDR DL75E090888Frame · dentedFWD CARGO FRAME STA 580 AT STR 23 LT DENTED AND BULGED. REPAIRED IAW SRM 53-00-07 AT SAA SAT DURING HMV ON NR CARD 107906.SDR ASOA200900443Structure · crackedFS 202 APPEARS TO BE CRACKED.SDR DU4R2009343Keelbeam · corrodedDURING SCHEDULED INSPECTION, FOUND FWD FUSELAGE EXTERNAL SKIN BULGING (KEELBEAM CORRODED) AT BS 530 RT.SDR DU4R2009328Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON FLOORBEAM AT BS 1016 BL 0 TO RBL 36.SDR TRBACPCP20090006Flange · unknownLAVATORY SERVICE DOOR CUT OUT AT FUSELAGE LINE 0451. REMOVED AND REPLACED DOUBLER FLANGE IAW SRM NR 51-25-01.SDR TRBA2009041Unknown · vibrationF/A REPORTED VIBRATION IN BOTH FRONT AND REAR OF CABIN. FELT SLIGHT VIBRATION IN YOKE. SEEMED TO LESSEN AS AN INCREASED ON APP WITH GEAR AND FLAPS DEPLOYED-SEEMED SMOOTHER. PERFORMED GROUND RUNS OF ENGINES, NO PROPS VIBRATIONS EXPERIENCED. PERFORMED INSPECTSDR ASOA200900167Post · damagedLT AND RT FS 409.0+128 VERTICAL POST AT BL 18.0, WL 69.0 HAS INDICATIONS NOTED LBL 18 O/B SIDE APPROX .2" IN LENGTH AND RH SIDE RBL 18 I/B AND O/B SIDES APPROX .2" IN LENGTH LH AND RH BL 18. FAILED NDT INSPECTION.SDR QXEA2000902020006Floorbeam · crackedPDX - C2 - CRACK ON BEAM FS 280 AT APPROX RBL 9.00. REMOVED RT SECTION OF 280 BEAM. CUT REPLACEMENT RT SECTION OF 280 BEAM IAW REO 670-53-11-047. PERFORMED HFEC INSP OF BEAM CUTOUT IAW NDTM 51-20-006, NO CRACKS NOTED. LOCATED, DRILLED AND COUNTERSUNK REPLASDR AALA200910611Fitting · wrong partFITTING WRONG TYPE. REMOVED AND REPLACED UPPER AFT FITTING PER S/B DC9-52-189.SDR AALA200910610Fitting · wrong partFITTING WRONG TYPE. REMOVED AND REPLACED UPPER FORWARD FITTING PER S/B DC9-52-189.SDR AALA200910609Fitting · wrong partFITTING WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189.SDR AALA200910608Fitting · wrong partFITTING WRONG TYPE. REMOVED AND REPLACED FITTING, PER S/B DC9-52-189.SDR AALA200910613Fitting · wrong partUPPER FORWARD CLIP (FITTING) WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189.SDR AALA200810177Battery Pack · weakCABIN EMERGENCY BATTERY PACK BS-104 AT STATION 902R ARMING VOLTAGE WEAK. REPLACED BATTERY PACK WITH SERVICEABLE PACK.SDR QMLA1112200808053Structure · cracked1" CRACK FOUND IN LEFT UPPER NOSE COMPARTMENT.SDR SWIA200821047Unknown · damagedJOINT PIECE DAMAGED AT FS 394 AND STR 23S, DAMAGE REPAIR. REPLACED PER SRM.SDR ASOA1227Support Beam · unknownREMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW CRJ 200 SRM 51-42-21. PRESSURE CHECK DUE. PRESSURE CHECK GOOD OF CARGO DOOR IAW AMM 21-32-00-863-801. SUPPLEMENTAL SDR CLOSED 10/21/08.SDR 2008UALA05717Frame · dentedFRAME DENTED AFT PIT BS 1400 STR 26L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.SDR 2008UALA05616Structure · corrodedAFT PIT CORROSION ON FRAME CAP LOWER SURFACE AT BS 1197+110 AND STR 33L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED "T" CAP.SDR NSV2008F00023Structure · vibrationAIRPLANE SHAKES DURING CLIMBOUT AT SLOW SPEED AND DURING APPROACH. CAPTAINS CONTROL COLUMN SHAKES. MOVES APPROXIMATELY 3 INCHES. VIBRATION DIMINISHES SOME IN CRUISE FLIGHT. VIBRATION STOPPED COMPLETELY WHEN FLAPS SELECTED TO 15 DEG ON APPROACH.SDR CNMA20090045Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1871-2007 AND X=107.25. REMOVED CORROSION IAW SRM 51-21-01 V II REV 94 DIMENSIONS OUT OF LIMITS (120 X 50 X 2,3 MM). REPLACED PN NRA6222-9 IAW DWG NFA6222. INSTALLED PN AFA7789-535 IAW SRM 51-35-01 AND 51-33-01 V II INSTESDR CNMA20090044Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1902 - 2007 AND X=75.25. CORROSION REMOVED IAW SRM 51-21-01 V G REV 94 DIMENTIONS ARE OUT OF LIMITS (240 X 8T X 2,4 MM) FABRICATED AND INSTALLED TRACK PN AGA7086-506 IAW DWG AGA7086 AND DWG ASA 7127 AND MM 205002 REV 81.SDR CNMA20090043Track · corrodedFOUND CORROSION ON DOWN TRACK AT STA 1887-2007 AND X=27.50. REMOVED BEAM IAW SRM 51-31-01, VOL II, REV 94 AND MM 20-50-02 REV 81. FABRICATED PN ASA7087-1 IAW DWG ASA7087 AND INSTALLED IAW DWG AGA7127 AND MM 20-50-02 REV 81.SDR SWIA200820338Structure · crackedC-CHECK, RADIUS CRACKED ON STRUCTURE NEXT TO ADG PUMP. REPAIRED PER SRM.
Back to JASC 5300