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 CALA2021121702381Skin · bulgedAFT FUSELAGE LOWER EXTERNAL SKIN STA 1519, S28L - S29L SKIN BULG E FWD OF BLANKING PLATE. MARKED REPAIRED IAW B757 SRM 53-00-01 REPAIR 29. SEE PARTIAL WORK ACCOM PLISHED. ADD EMP:V931850SDR R61A2021121601019Door Sill · corrodedCORROSION IN CENTER OF AFT PAX DOOR SILL AS MARKED. REMOVED AND REPLACED AFT PAX DOOR SILL FWD AND AFT SEAL REST REF SRM 51-40-08.SDR 2A6D20211216001Door Frame · chafedC130 S/N 7174 WAS FOUND TO HAVE LUGGAGE COMPARTMENT DOOR FRAME DAMAGE AT APPROXIMATELY STA 1863, WL 1990, AND BL 280L/R WITH A MAXIMUM DEPTH OF 0.021SDR 2021F00340None · noneCRACK FOUND DURING ESCAPE HATCH INSPECTION ON RH EMERGENCY EXIT DOOR CROSS TIE, BOTTOM AFT CORNER OF FUSELAGE SIDE AT FS 201.775 ZONE 250, WL 119SDR 2022FA0000610None · noneSEVERAL CRACK-LIKE INDICATIONS WERE FOUND ON THE GEAR TEETH IN THE MAIN ROTOR TRUNNION. THESE INDICATIONS MEASURED ~3/8" LONG IN THE AREA OF INTEREST. CRACKS WERE FOUND WITH FLUORESCENT MAGNETIC PARTICLE TESTING. INSPECTION WAS PERFORMED PER ASTM E1444 AS REQUSDR SWIA202164652None · cracked*FS 280 RH ANGLE HAS A SUSPECTED CRACK (MARKED) (C CHECK RO 02/22/2022) REMOVED AND RE-INSTALLED FS.280 RH SHEARBOX OB FWD ANGLE REF. CRJ 700 SRM 51-42-21-001-001-A01, NO CRACKS FOUND PER NDT REPORT.SDR SWIA202164541None · corrodedAVIONICS FLOORBOARD ANGLE ON AFT FACE OF FS280 FRAME APPEARS CORRODED. (C CHECK RO 2/17/2022) REMOVED AND REPLACED WITH NEW THE AVIONICS BAY CRAWLWAY FLOORBOARD SUPPORT ANGLE ON THE AFT FACE OF FS280.00 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42SDR SWIA202164505None · corrodedPAX DOOR LOWER KICK PLATE ANGLE CORRODED (C CHECK RO 2/17/2022) REMOVED CORROSION FROM PAX DOOR LOWER KICK PLATE ANGLE, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED NEW PAX DOOR LOWER KICK PLATE ANGLE. REF. BOMBARDIER DWG SH670-31810 REV AE AND CRJ700 SRM 51-SDR SWIA202164413None · corroded*MULTIPLE AREAS OF CORROSION ON FUSELAGE INTERIOR SKIN AVIONICS BAY DOOR CUTOUT AROUND DOOR SEAL MATING SURFACE. AREAS MARKED. (C-CHECK RO 2/16/2022) BLENDED CORROSION DAMAGE FROM INTERIOR FUSELAGE SKIN @ AVIONICS BAY DOOR CUTOUT AROUND DOOR SEAL MATINGSDR SWIA202164412None · corrodedEXTERNAL FUSELAGE SKIN HAS EVIDENCE OF CORROSION AT STGR 27 BETWEEN FS 881.00 AND FS 906.00 (C-CHECK RO 2/16/2022) REPAIRED EXTERNAL FUSELAGE SKIN BETWEEN FS881.00 TO FS906.00 AT STRINGER27 IAW REO 690-53-51-316 REV -- DATE 2021-20-12 COMPLIED WITH ALSDR SWIA202164188None · crackedFOUND CRACK ON Z STIFFENER ANGLE @ PAX DOOR AFT WEB. REPLACE. (C CHECK RO 02-03-22) REPLACED PAX DOOR AFT WEB Z STIFFENER. REF CRJ700 SRM 51-42-06-001-001-A01.SDR A6WA202102018091Channel · gougedCARGO DOOR UPPER FWD SUPPORT CHANNEL P/N: 601R35050-129 HAS A GOUGE ON FLANGE. DIMENSIONS ARE: (P1) 1.900L X .063W X .190D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***SDR A6WA202102018090Bulkhead · noneAFT PRESSURE BULKHEAD REAR WEB HAS 2 EACH RIVETS INSTALLED AT THE EDGE OF CHEM MILL I/B OF Z STIFFENER AT LBL 17 WL 140.5 AND 141.5. ******************AIRCRAFT REMOVED FROM SERVICE********************** REMOVED 2 EACH RIVETS AT THE EDGE OF CHEM MILL ON AFT PSDR MASA20220125089None · corroded"CORROSION ON FLOOR SEAT RAIL FS693-667+32 LBL9 AND RBL9 (CPAX).
FLOOR SEAT RAIL WERE REPLACED PER CRJ/900 AMM 53-00-49."SDR MASA20211215075Skin · none"SEVERAL NICKS ON EXTERNAL FUSELAGE SKIN BTW FS=1015-FS=1051 AND STGR27-21RH.
SEVERAL NICKS ON EXTERNAL FUSELAGE SKIN BTW FS=1015-FS1051 AND STGR27-21RH WAS REPAIRED PER EA 81-2022-006 REV. B"SDR R61A2022010500027Latch · corrodedLIGHT CORROSION FOUND ON RH INBD CABIN SEAT TRACK BETWEEN FR82 & FR83 REPAIRED IAW SRM 53-00-10 REPAIR 02SDR CALA2021121702379Stringer · corrodedFWD CARGO LWR SILL WEB PLATE FR26 TO FR28 UPPER SURFACE HAS SEV ERAL AREAS OF CORROSION (A3NB-53-3-6105) GENERATED BY N078592 AT HAECO LCQ PER NON ROUTINE 9294405 (22405) REMOVED CORRODED FWD CARGO SILL WEB PLATE AND INSTALLED NEW WEB PLATE IAW A320 SRM 51-42-SDR IXXA20211215006Support Strap · crackedGILINER SUPPORT FOR VERTICAL SIDEWALL TO
CEILING, RH , STA 1263~1241, BENT AND
CRACKED.SDR IXXA2021121503Stringer · corrodedSTRINGER 39R CORRODED STA. 1272-1276SDR IXXA2021121502Stub Frame · crackedFRAME INNER CHORD CRACKED AND LOWER END.SDR IXXA2021121501Stringer · corrodedCORROSION ON STRINGER 35LSDR JJBA20211214028None · noneVENTRAL TANK FRONTAL FACE LIP TO ATTACH THE PANELS IS BARE METAL. CUTOUT DONE ON VENTRAL TANK FWD FACE LIP AND PART FABRICATED. VENTRAL TANK FRONTAL FACE LIP REPAIREDSDR JJBA20211214027None · noneCORROSION FOUND ON LOWER SKIN UNDER RAD ALT ANTENNA #2 AFT SUPPORT BTW FR 68-69 IN REAR FUSE I AREA. RAD ALT #2 ANTENNA, SUPPORT, SUPPORT ASSEMBLY AND FAIRING REMOVED FOR ACCESS. ANTENNA SUPPORT AND SUPPORT ASSY BLENDED OUT OF LIMITS. AFTER INVESTIGATION SKINSDR JJBA20211214026None · noneDENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CF II AREA. DENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CFII AREA. CUT-OUT PERFORMED ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R SKIN REPAIRED. REPROTECTION COVERED.SDR JJBA20211214025None · noneCORROSION FOUND ON LOWER SKIN BTW FR 20-21 AND BTW STR 21L-21R IN CF1 DOOR STRUCTURE AREA. SKIN AT FR20-21 BTW 21L-21R CORROSION BLENDED FOR ENGINEERING REVIEW. IN CF1 FLOOR STRUCTURE AREA. BTW FR20-21 AND BTW STR 21L-21R, LOWER SKIN REPAIRED WITH DOUBLER AND SDR JJBA20211214024None · noneDENTS FOUND ON LH SKIN BTW FR 19-21 AND BTW STR 11L-12L IN CF I AREA. LH SKIN BTW FR19-21 AND BTW STR 11L-12L IN CF! AREA, PATCH REMOVED FOR INVESTIGATION. 3 DENTS CUT OUT. LH SKIN BTW FR 19-21 AND BTW STR 11L-12L SKIN REPAIREDSDR FDEA202112143094Web · damagedCOMPLY WITH WORK IN PROCCESS EA #F-5310-T0365897 WORK ACCOMPLISHED PER FEDEX EA #F-5310-T0365897SDR JJBA20211214019None · noneDAMAGE FOUND ON RH OUTBD OMEGA BEAM AT FR 48 IN FLOOR STRUCTURE CF III AREA. ON RH OUTBD OMEGA BEAM AT FR48 IN FLOOR STRUCTURE CF3 AREA, DAMAGE CUTOUT ON RH OMEGA BEAM AT FR 48 IN FLOOR STRUCTURE REPAIR PERFORMEDSDR CALA2021121402366Web · crackedREF AMES NR 0100-0123, WEB CRACKED @ STA 400 RBL 46 NEEDS REMOVE D FOR REPLACEMENT. REMVOED & REPLACED WEB STA 400 RBL 4G IAW BOEING DWG 141N5150 RE V ABD B757 SRM 51-40-02. ADD EMP:V931845SDR CALA2021121402365None · crackedEA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 ANSDR CALA2021121402359None · crackedEA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 ANSDR U2RA202121400070Panel · puncturedREFERENCE NATIONAL AIRLINES AIRCRAFT MAINTENANCE LOG PAGE 52103, FORWARD LOWER CARGO COMPARTMENT FLOOR PANEL PUNCTURED AT STATION 680, BETWEEN STRINGERS 45R AND 46R. ACCOMPLISHED TIME LIMITED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERISDR SWIA202163915None · damagedFOUND PREVIOUS DOUBLER REPAIR FOR SB 670-BA-53-057 JOB 710234105 OP 5786 (C CHECK RO 1/18/2022) INSTALLED A NEW REPAIR TRIPLER AND 2 EA FWD WATER DRAIN DOUBLERS AT APPROX. FS265.00-FS295.00 BETWEEN STR24L-STR25R. COMPLIED WITH ALL STEPS OF THE REPAIR, INCSDR SWIA202163873None · dentedTRANSFER FROM EAML 797832 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 797188 / AIRCRAFT WAS DENTED ON L/H SIDE OF FUSELAGE BELOW AND BETWEEN 3A AND 4A WINDOWS DUE TO IMPACT WITH JET BRIDGE DUE TO HIGH WINDS AND AIRCRAFT SLIDING ON ICE. AIRCRAFT WASDR 2A6R2021131262601Skin Panel · crackedCRACK DAMAGE WAS NOTED TO THE LEFT SIDE AFT BOX BEAM INNER SKIN PANEL (PN: B533K5606-212) MEASURED TO BE APPROXIMATELY 0.625” LONG. THE DAMAGE WAS REPAIRED VIA A REPAIR DOUBLER IN ACCORDANCE WITH AIRBUS RDAS-BK117-53-2021-4226, REVISION B DATED 02 DEC 2021.SDR QXEA2021121600553None · noneCORROSION CABIN RH FLOOR LEVEL GUSSET FR89 Y+13". BLENDED CORROSION ON RH FLOOR GUSSET AT FRAME 89 Y +13' IAW SRM 51-10-03, FOUND TO HAVE 100% MATERIAL LOSS AND IS OUT OF ALLOWABLE LIMITS IAW SRM 51-75-16. PART REQUIRES REPLACEMENT. REMOVED AND REPLACED RH GUSSDR QXEA2021121600552None · noneCORROSION CABIN RH FLOOR LEVEL GUSSET FR90 Y+13". REMOVED AND INSTALLED NEW GUSSET AT FRAME 90 Y +13" IAW SRM 51-40-08.SDR QXEA2021121600550None · noneCORROSION CABIN RH FLOOR LEVEL GUSSET FR 90 Y+23". REMOVED AND INSTALLED NEW GUSSET AT FRAME 90 Y +23" IAW SRM 51-40-08.SDR JJBA20211213016None · noneBAG BAY CUTOUT TRAILING EDGE GOUGED. BLENDED OUT DAMAGED AREA AND EVALUTATED. FOUND TO BE OUT OF LIMITS. PERFORMED ET AND UT INSPECTION BY BARON NDT, LLCSDR 2021F00356None · crackedPERMANENT REPAIR OF NOSE WHEEL WELL UPPER WEB CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890, STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS FS 75. WITH FAA FORM 8100-9.SDR JJBA20211213010None · noneREAR FUSELAGE - SKIN HAS CORROSION UNDER RAR 2 ANTENNA MOUNT PLATE. REPAIRED WITH CUTOUT OF DAMAGE AT REAR FUSELAGE SKIN UNDER RAR #2 ANTENNA AT FR68-69 AND STR 21L-21R AND INSTALLED REPAIR DOUBLER. CORROSION LEVEL IISDR SWIA202164265None · shearedFS621-625 ATTACH ANGLE HAS SHEARED FASTENERS AT RBL 36 BETWEEN STGR 9R AND 10R (C CHECK RO 2-11-2022) REMOVED AND REPLACED FS621-FS 625 ANGLE AT RBL 36 BETWEEN STGR 9R AND 10R IAW MHIRJ REO 601R-53-61-7766 REV -- DATED 2021-12-16 REF ATTACHED CONTINUATION SDR SWIA202164264None · crackedRH OBLIQUE ANGLE CRACKED FROM FS 621-625 (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDSDR QXEA2021121600551None · noneCORROSION CABIN RH FLOOR LEVEL SHEAR PANEL FR 87-88. CABIN RH FLOOR SHEAR PANEL FR 87-88 REQUIRES REPLACEMENT REF SRM 51-10-02 PAR 6 D,3. REMOVED AND REPLACED NEW SHAER PANEL IAW SRM 51-42-01.SDR CALA2021121202350Intercostal · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33SDR SWIA202164062None · damagedFOUND R/H AND L/H UPLOCK BRACKETS TO HAVE OVERSIZE FASTENER HOLES ON I/B ATTACHMENT ANGLE (FILED CLOSED) COMPLIED WITH ATTACHED MHIRJ REO 670-53-41-578 REV -- DATED 2021-12-13, SKYCARD 51-900-1002-SKY(CL600-2C10), AND FORM M-337. NO WEIGHT CHANGE NOTEDSDR YENA2021121600840Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED FR 33 BTW STR 40R AND 41 R IN FORWARD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE IAW 51-72-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475444SDR CALA2021121202345Bulkhead · cracked(AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND CSDR 2021FA0000377None · noneADSB INOP ON MULTIPLE AIRCRAFT USING THIS SYSTEM. THERE’S NO ANNUNCIATION THAT IT’S NOT WORKING, SO USUALLY DISCOVERED BY ACCIDENT MONTHS AFTER UNSAFE OPERATION. MANUFACTURER REFUSES TO DO ANYTHING ABOUT ITSDR SWIA202164827None · corrodedL/H AND R/H FUSELAGE SKIN IS CORRODED AROUND SCREW HOLES FOR PANELS 191BB AND 192BB (FWD WING TO FUSELAGE FAIRINGS). (C CHECK RO 3/11/2022) REPAIRED CORROSION AT L/H AND R/H FUSELAGE SKIN AROUND SCREW HOLES FOR PANELS 191BB AND 192BB IAW MHIRJ REO 601R-53
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