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 P5CA2021111100419None · noneEVIDENCE OF BIRD STRIKE ON #1 ENGINE INLET(<P>CLEANED AND PERFORMED BIRD STRIKE INSP TO #1 ENG INLET & SURROUNDING IAW B767 AMM 05-51-18. NO DEFECTS NOTED AT THIS TIME.</P> / <P>DATED 10NOV21 - LOG PAGE 1396057 - ITEM 16: COMPLIED WITH BORESCOPE INSPECTION OF SDR CALA2021111102087Skin · crackedAD 2019-11-02 SUPPORT TASK EA 5310-06900 OP 13 3EA HOLE CRACK FOUND AT FX SKIN BS 1035 UNDERWING LONGERON, DETAIL REFER REPORT. TRANSFER REF L/P 9130955 AND ORIGINATED BY V917699 4000 TOTAL CYCLES. CARRIED FOR DTA. ACCOMPLISH THE INSPECTIONS PER THE LATEST REVSDR CALA2021111002082Seat Track · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACESDR SWIA202163834None · dented*EXTERNAL SKIN UNDER THE PROTECTOR PLATE HAS A DENT LOCATED @FS1015.00 BETWEEN STRG 17LH & 18LH (C CHECK RO 1/16/2022) / PERFORMED AND COMPLIED WITH ALL STEPS OF MHIRJ REO 670-53-61-2004 REV -- DATED 2021-12-15, REPAIR FOR EXTERNAL SKIN DENT UNDER PROTECTSDR SWIA202163212None · crackedANGLE ON BULKHEAD FS280.00 AND LBL26.00 IS CRACKED (C CHECK RO 12-19-21) REMOVED AND INSTALLED NEW ANGLE ON BULKHEAD FS280.00 AND LBL26.00 REF CRJ-700 SRM 51-42-06-001-001-A01SDR R61A2021111800905Web · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK ** COCKPIT FLOOR STRUCTURE CORROSION FOUND ON FLOOR STRUCTURE AT FR 12 LH SIDE BEHIND PILOT SEAT. MX REPAIRED FLOOR WEB PN 170-03237-005 IAW ETD2021-170-037719.SDR R61A2021111800904Shear Angle · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK ** CENTER FUSELAGE 3 SHEAR CLIP FOUND CORRODED AT FR 87 BTWN STR 28R-27R. MX REPLACED SHEAR CLIP PN 170-66041-002 IAW SRM 51-41-02,51-43-03SDR R61A2021111200901Skin · puncturedFOUND PUNCTURE TO AIRCRAFT SKIN LH SIDE AFT OF L1 DOOR BETWEEN FR 20 TO FR 23 STR 14L TO 15L. REPAIRED IAW SRM 51-23-04 AND 53-10-01SDR CALA2021111002071None · noneAS 2012-09-04 SUPPORT TASK EA 5340-01385 REV ORIG OP 001 LH STA 955 REAR BULKHEAD FAILSAFT STRAP 1EA FASTENER HOLE FOUND 2EA CRACKS RUNNING FWD AND AFT TRANSFER REF. NON-ROUTINE LP 9131340 AND ORIGINATED BY EMP NO. V906014 LH STA 955 REAR SPAR BULKHEAD FAILSAFSDR CALA2021111002070None · noneAD 2012-09-04 SUPPORT TASK EA 5340-01385 REV ORIG OP 002 STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP 1EA FASTENER HOLE FOUND 2EA CRACKS RUNNING FWD AND AFT TRANSFER REF. NON-ROUTINE LP 9131338 AND ORIGINATED BY EMP NO. V906014 RH STA 955 REAR SPAR BULKHEAD FAILSSDR CALA2021111002068Fitting · crackedSUPPORT TASK FUSELAGE BS1035 LH BUILT- UP UNDERWING LONGERON THE MOST I/B LAYER FOUND 1EA CRACK, PLEASE PRINT AND ACCOMPLISH OP 13 OF THIS EA. TRANSFER REF L/P 9130189 AND ORIGINATED BY V906013 FUSELAGE BS1035 LH UNDERWING LONGERON FITTING REPLACED AND INSTA LSDR MASA20211109552None · damagedAFT LAVATORY SERVICE DOOR.(196ER) INSTALLED ON THE WING-TO-BODY FAIRING PANEL 196DR WAS FOUND TO HAVE DAMAGE ON ONE OF THE TWO HINGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 52-45-01, FIGURE 1, ITEM 30, EA 81-2021-084.SDR JR2R20211109422Beam · corrodedFLOOR BEAM AT FR85 AND LBL9 IS CORRODEDSDR IXXA20220111002Stringer Splice · corrodedSTR 33L CORRODED AT STA 742SDR SWIA202163414None · corroded* TCAS DOUBLER BETWEEN FS295-FS310 & STGR26L-STGR26R CORRODED (C CHECK RO 12-31-21) REPLACED TCAS DOUBLER BETWEEN FS295 AND FS310 FROM STGR 26L TO 26R. REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-30023 REV. G. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR IXXA2021120702Channel · corrodedCORROSION FOUND ON Z CHANNEL AT STATION 522-544/24LBL-40LBLSDR HNAA2021112900569None · noneE887289 - R/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-77 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON R/H EXTERNAL FUSELAGE SKIN AT FR-77 APPROXIMATELY 1" BELOW STR 8R AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0324SDR HNAA2021112900568None · noneE887287 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-79 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-79 APPROXIMATELY 1" BELOW STR 6L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-0325SDR HNAA2021112900567None · noneE887286 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-78 MARKED .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-78 APPROXIMATELY 1" BELOW STR 8L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-2SDR HNAA2021112900566None · noneE887285 - L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET FR-77 .... PREPPED, FABRICATED AND INSTALLED BUSHING (.500") ON L/H EXTERNAL FUSELAGE SKIN AT FR-77 APPROXIMATELY 1" ABOVE STR 9L AT RIVET IAW EMB-145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-21-032SDR FDEA202111082797Skin · crackedPUNCTURE AND DENT DAMAGE ON SKIN PN:148T3211 BETWEEN STA 1582 AND STA 1629 AND S-33L AND S- 35L. REPAIRED SKIN PN:148T3211 PER E.A.#:H-5330-T0365358 DATED: NOV 13, 2021 "TITLE: FUSELAGE - SECTION 48 FUSELAGE SKIN - PERMANENT REPAIR OF IMPACT DAMAGE BETWEEN SDR CALA2021111002064None · noneAD 2019-11-02 SUPPORT TASK EA 5310-06900 2EA HOLES FOUND CRACK AT LH BS1035 CTR SECTION FRONT SPAR LWR CHORD. TRANSFER REF L/P 9130956 AND ORIGINATED BY V917699 WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIRED AS PER SRM 5 7-10-10-2R-1 REPAIR 1 JUST AT LBL SDR SWIA202163400None · corroded*FRETTING ON A-BAY DOOR CUT OUT INNER SKIN SURROUND/DOOR SEAL MATING SURFACE (C CHECK RO 12-31-21) REMOVED DAMAGE TO A-BAY DOOR CUT OUT INNER SKIN AND REPAIRED PER REF: REO 690-53-21-032, REV: --, 2008-03-07. COMPLIED WITH 51-900-1002-SKY.SDR SWIA202163394None · corroded*CORROSION ON SRVC DOOR LOWER SILL MOUNTING ANGLE (C CHECK RO 12-31-21) / REPLACED SRVC DOOR LOWER SILL MOUNTING ANGLE(SEAL STRIKER) REF DWG SH670-31950 REV. Y AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.SDR SWIA202163389None · corroded*CORROSION ON FWD CABIN STORAGE INBD AFT MOUNT AT FS310.00 LBL18 (C CHECK RO 12-31-21) / REMOVED AND REPLACED FITTING AT FS310.00 LBL18. REF: CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-32120 REV Y. COMPLIED WITH 51-900SDR CALA2021110802061Seat Track · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACESDR CALA2021110802055None · noneSUPPORT TASK (TAR) DURING ACCOMPLISH EA 5340-01385 REV ORIG OP 004 RH SIDE STA 955 REAR SPAR BULKHEAD FAIL STRAP STRAP REPAIR, AT STEP -14.0 PREPARE NEW T-FITTING FOR INSTALLATION, WE FOUND THE I/B ROW AFT 5EA FASTENER HOLES HORT EDGE MARIGIN TRANSFER REF. NONSDR CALA2021110802054Fitting · noneB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. FURTHER DETAILS AWAITED.SDR CALA2021110802053Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. FURTHER DETAIL AWAITEDSDR CALA2021110802052Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. FURHTER DETAILS AWAITEDSDR CALA2021110802051Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. FURTHER DETAILS AWAITEDSDR CALA2021110802050Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. FURTHER DETAILS AWAITEDSDR CALA2021110802049Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. FURTHER DETAILS AWAITED.SDR CALA2021110802048Stringer · crackedSUPPORT TASK - EA 5310-06900 OP 4, AD2019-11-02, 1EA THROUGH THICKNESS CRACK WAS FOUND ON THE MOST I/B LAYER OF THE LONGERON AS MARKED. PLS PRINT & ACCOMPLISH OP 14 OF THIS EA TO ACCOMPLISH RH LONGERON REPLACEMENT PRIOR TO FURTHER FLIGHT. TRANSFER REF. NON-ROUSDR CALA2021110802056None · crackedAS 2012-09-04 SUPPORT TASK EA 5340-01385 REV ORIG OP 001 LH STA 955 REAR BULKHEAD FAILSAFT STRAP 1EA FASTENER HOLE FOUND 2EA CRACKS RUNNING FWD AND AFT TRANSFER REF. NON-ROUTINE LP 9131340 AND ORIGINATED BY EMP NO. V906014 LH STA 955 REAR SPAR BULKHEAD FAILSAFSDR JR2R20211107452Beam · corrodedGALLEY SUPPORT FITTING AT FR90 FOUND TO BE CORRODED OUT OF LIMITSSDR 29GA2021111200001None · damagedSUPPLEMENTAL: REPORT: LH AFT MAIN LANDING GEAR BODY PANELS AND PROTION OF FUSELAGE DAMAGE DUE TO TUG
CONTACT WITH AIRCRAFT. CORRECTIEV ACTION: REPAIRED LEFT AFT MAIN LANDING GEAR BODY PANLES AND FUSELAGE DAMAGE IAW EO ATR42-5300-2021-001 AND ATR INSTRUCTION SDR HNAA2021112900592None · noneE889024 - REINFORCEMENT ON FR 69 DAMAGED FROM CHAFING BETWEEN STRGS 18L-19L .... REMOVED AND INSTALLED SERVICEABLE LOWER LH FR 69 FRAME REINFORCEMENT ANGLE IAW PIEDMONT EO1-53-21-0319 AND EMB 145 SRM 51-40-02.SDR JR2R20211106421Beam · corrodedFLOOR BEAM CORRODED AT FR87 AND LBL9SDR JR2R20211105430Beam · corrodedFLOOR BEAM CORRODED AT FR87 AND RBL9SDR 2021FA0000348Intercostal · crackedFWD. CARGO FWD. BULKHEAD CEILING HAS CRACKED INTERCOSTAL AT STA. 270.00, REF. NRC B000152SDR R61A2021111900921Splice · corrodedWHILE AC WAS IN FOR HVY CK FOUND AFT WING TO BODY FAIRING FWD SPLICE ASSY CORRODED. MX REPLACED SPLICE PN 170-02460-401 IAW SRM 20-10-01 SEE AAR NRC# 4500985-1000-0100 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR MASA20211105528None · noneWEAR DAMAGE WAS ACCIDENTALLY CAUSED TO CROSS BEAMS (P/N MM670-35314-009 AND MM670-35319-001} AT THE JOINT WITH CLIP (P/N MM670-35335- 001} LOCATED AT FS1015.00 DURING MTC ACTIVITIES WHEN FLOOR BEAM WAS REMOVED. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53SDR 2A6D2021110509702Tail Boom · chafedCHAFING WAS DISCOVERED ON THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.AL) MEASURING APPROXIMATELY 0.10” X 0.10” AND 0.011” DEEP.SDR SWIA202164029None · damaged2 DAMAGED HOLES ON R/H CHECK PANEL (C CHECK RO 1/20/22) OPENED UP (2) HOLES AND INSTALLED FREEZE PLUG BUSHINGS IAW CRJ200 BOMBARDIER REO 601R-53-11-162. REV. D. DATE: 2019-02-05. / BUSHINGS FABRICATED BY OUTSIDE VENDOR SEE ATTACHED INVOUIC # 12684CURRENT SDR A6WA202111197977None · dentedAFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .600"L X .500"W X .025"D AT FS 621, 3.7" O/B OF RBL 36.20, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .011"D. CUTOUT DAMAGED AREASDR R61A2021112200925Crossbeam · corrodedLEVEL 2 CORROSION WAS FOUND AT FWD WET AREA CROSSBEAM FR16 LH. CROSSBEAM WAS REPAIRED IAW ETD 2021-170-037104.SDR R61A2021111900922Angle · corrodedWHILE AC WAS IN FOR HVY CK FOUND FWD WET AREA FLOOR BOARD SUPPORT ANGLE AT FR 19 LH BEHIND L1 DOOR FOUND CORRODED. MX REPLACED SUPPORT ANGLE PN 170-12320-403 IAW SRM 51-43-01 SEE AAR NRC# 4500985-1000-0079 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR A6WA202111197978None · dentedAFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .500"L X .300"W X .015"D AT FS 621, LBL 9.5 TO LBL 18.00, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .013"D. CUTOUT DAMAGED AREA SDR A6WA202111197976None · dentedAFT PRESSURE BULKHEAD HAS DENT .400"L X .300"W X .010"D AT FS 621 IN BETWEEN LBL 27.50 AND LBL 36.20 AND 1.70" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** DRESSED BACK DENT ON AFT PRESSURE BULKHEAD TO ORIGINAL CONTOUR. HFEC WAS PERFORMED AT REWORK AR
Back to JASC 5300