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 R61A2022042500308Cover Plate · damagedDRILL DAMAGE TO L2 DOOR PROTECTIVE PLATE AND FUSELAGE @ FRAME 88 STR 18L. PERFORMED PERMANENT REPAIR TO DRILL DAMAGE ON FUSELAGE SKIN IAW ETD2022-170--0142691.SDR IXXA2022060802Floor Support · corrodedALC PRESSURE DECK WEB SUPPORT STRUCTURE CORRODEDSDR IXXA2022060201Support Bracket · corrodedALC PRESSURE WEB PANEL SUPPORT STRUCTURE AT STA 1324 CORRODEDSDR FDEA202204151101Fitting · gougedLH FWD PAX/CREW DOOR CUTOUT FOUND GOUGE NEAR FWD-UPR CORNER. DAMAGED FITTING REPLACED NEW PART, INSTALLED WITH RIVETS. I.A.W A300-600 SRM 51-40-21- 001 PARA.6 PAGE.7B-23 AND 51-72-10-001 PAGE.2.SDR R61A2022050300314Stiffener · corrodedWASTE DOOR STIFFENER FOUND CORRODED. R&R NEW STIFFENER IAW SRM 51-41-02.SDR IXXA2022041501Seal Depressor · crackedMAIN DECK CARGO DOOR SEAL DEPRESSOR CRACKED.SDR SWIA202265433None · dentedDENT LOCATED APPROX 18 INCHES AFT OF FWD RH SERVICE DOOR OUTER HANDLE REQUIRES EVALUATION AND REPAIR. (C-CHECK RO 4/21/2022) REPAIRED DENT LOCATED APPROX. 18 INCHES AFT OF FWD RH SERVICE DOOR OUTER HANDLE BY WAY OF CUTTING OUT DAMAGE AND INSTALLING A FASDR CALA2022041801000Beam · corrodedSUPPORT TASK MAIN CABIN FLOOR BEAM 1681 CORRODED UNDER AFT DECK PRESSURE PLATE BETWEEN BL 0 AND LBL 54, TRANSCRIBED FROM HAECO G SO NR 9283143 TRANSCRIBED FROM HAECO LP 9283143. REPAIRED IAW ECRA 5365-01097.SDR GTIA2022041436385None · noneENROUTE HAD STRONG ODOR AFT CABIN "DIRTY SOCK MUSTY OIL SMELL" COUPLED WITH SUPPLEMENTAL PROCEDURE ODOR/FUMES CABIN PG 3.226.1 TURNED OFF PACK 2 ODOR WAS ELIMINATED CONTNUED FLIGHT-ACCOMPLISHED TSM PROCEDURE IAW 05-50-00-810-831-A TO COULD NOT DUPLICATE SMELL SDR CALA2022041400989Angle · crackedREF AMES N/R 0100-0049 A SUPPORT ANGLE IS CRACKED AT B STA 1180, S-29R AT EXTERNAL LWR FUSELAGE. REMOVE AND REPALCED ANGLE PN 146N7528066 IAW B757 SRM 51-40-22 P ARA 7 51-31-01 SEE REVERSE FOR PARTIAL WORKSDR CALA2022041400988Floor Support · corrodedSTA 365BLO FLOOR SUPPORT STRUCTURE HAS CORROSION. REPORTED BY V9 21209 FOUND AREA ON FLOOR SUPPORT TO BE OUT OF LIMITS. REMOVED AND REP LACED FLOOR SUPPORT FROM STA 365B BLO IAW B757 SRM 51-40-02 PARA GRAPH 7. REF NON-ROUTINE 145078-0100-0161 FOR INFOSDR CALA2022041400987Door Frame · gouged(MED 4 LEFT AFT OF DOOR CUTOUT APPOX 8 INCH AFT AT LAP SKIN JOINT FOUND A GOUGE .DAMAGED IS APPROC 2" X 1/4" AN D 1/16 " DEEP AT THE DEEPEST POINT AT THE EDGE).PER ECRA 5330- 06934 REPAIR HAS BEEN ACCOMPLISHED AND REQUIRES "PLANNING TO CONTACT ENGINEERING ASDR SWIA202265865None · crackedRH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW SUPPORT ANGLE AT R/H WINDSHIELD POST AT FS236.75 AND WL103.90 REF CRJ200 SRM 51-42-06 AND DWG 601R34032 REV P. COMPLIED WISDR SWIA202265864None · crackedLH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REPLACED LH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL 103.90 PER CRJ200 SRM 51-42-06 & DRAWING 601R34032 REV P. CHECKS GOOD. SEE CONTINUASDR DALA2022041802645None · noneSHIP 6821 EXCESSIVE CORROSION: FLOOR STRINGER (Z) BTW STA 1310 AND STA 1342 AND LBL 7.55 AT AFTER CARGO COMPARTMENT ,IT'S OUT OF LIMITS IN REFERENCE TO NRC 191. CORRECTIVE ACTION: SUMMARY OF NRC 00492 : FLOOR STRINGER (Z) BTW STA 1310 AND STA 1342 AND LBL 7.55SDR FDEA202204130967None · damagedAIRCRAFT STRUCK LH WINGTIP WITH RH WINGTIP OF A/C 597 COMPLY WITH EA 6-0550-T0367981 COMPLIED WITH EA 6-0550-T0367981SDR CALA2022041400980Fitting · crackedDURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTE D ON AFT LOWER HOLE. INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5321-02067 REF VT MAE NR0024388. EXTERNAL ANGLE FITTING BEFORE AC4010 REACHES 61391TFC / 132942TF ECRA 5321-02067 H WHICHEVER OCCURS SDR CALA2022041400979Structure · corrodedSUPPORT TASK MAIN CABIN R1 DOOR LOWER SILL HAS CORRODED CHROD ST A 365 RBL 65, TRANSCRIBED FROM HAECO GSO NR 9287527SDR MASA20220413200Exhaust Cone · dentedMAINTENANCE DISCOVERED TWO DENTS AFFECTING THE SKIN AFT CONE (P/N: WA670-30701-1). PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 53-85-00-001-002-A01, ITEM 1.SDR 2A6R2022041363304Frame · mechanic errorDURING INSPECTION, IT WAS DISCOVERED THAT THE MARTIN BAKER SIDE SEAT INSTALLATION WAS PREVIOUSLY PERFORMED IN A MANNER THAT DEVIATED FROM THE APPROVED AIR METHODS STC # SR00605DE INSTALLATION DATA, DRAWING # 739-1911. THE STC WAS INSTALLED ON THIS AIRCRAFT PESDR 2A6R2022041363303Keelbeam · corrodedTHE AFT LEFT SIDE OF THE KEEL BEAM CAP (PN: L533M1009203) AT FUSELAGE STATION 5,700MM AND LBL 500MM WAS FOUND TO HAVE CORROSION DAMAGE AT THE NUT PLATE SECURING THE CABIN FLOOR NEAR THE GROUNDING POINT. THE CORROSION DAMAGE PENETRATED THE FULL THICKNESS OF TSDR 2A6R2022041363302Frame · mechanic errorDURING A SCHEDULED INSPECTION REQUIRED BY AIR METHODS ASB21-01, DAMAGE WAS DISCOVERED AT FRAME 5 AT APPROXIMATELY FS 4,709MM. THE DAMAGE IS ADJACENT TO THE MEDICAL WALL LOWER RH & LH AND UPPER LH, CENTER, AND RH ATTACH FITTING LOCATIONS. THE MEDICAL WALL IS SDR 2A6R2022041363301Skin Panel · corrodedDAMAGE WAS NOTED TO THE COCKPIT FLOOR (PN: L533M1013108) IN THE FORM OF AN AREA OF CORROSION ON THE UPPER SKIN PANEL AT THE RH FWD GROUNDING POINT MEASURING APPROXIMATELY 1.0” X 1.5”
THE CORROSION WAS REMOVED BY MECHANICAL MEANS, STRUCTURALLY RESTORED BY FSDR IXXA2022060810Stiffener · crackedSTA 676 AT 34L STIFFNER CRACKEDSDR SWIA202265891None · corroded* AVIONICS BAY FLOOR BOARD MOUNT ANGLE AT FS.280.00 FROM LBL9 TO RBL9 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 6/6/2022) REMOVED AND REPLACED NEW AVIONICS BAY FLOOR BOARD MOUNT ANGLE AT FS.280.00 FROM LBL9 TO RBL9. REF CRJ700 SRM 51-42-21-0SDR SWIA202265888None · corroded* AVIONICS BAY CIRCUMFERETIAL FRAME AT FS.295.00 FROM STR.26L TO STR.26R CORRODED (MARKED). (C-CHECK RO 6/6/2022) REMOVED AND REPLACED DAMAGED FRAME SECTOR ON FS 295 FROM STR 25L TO STR 25R REF CRJ 700 SRM 53-00-06-201-006-A01. LEAK CHECK GOOD.SDR SWAA2022050293154Track · missingTAIL CONE (SECTION 48) LEFT BODY TO HORIZONTAL STABILIZER REAR SPAR; UPPER FWD LEFT SIDE TRACK ASSY. WORN/PIECE MISSING. / [01] REMOVED PANEL # 333AT LEFT SIDE UPPER HORIZONTAL STABILIZER FOR ACCESS IAW B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP #1; PANEL SDR CALA2022041400976Bulkhead · cracked(SDR) RH FR16: DURING ROTO INSP OF RH FR16 DOUBLE JOGGLE, CRACK INDICATION WAS NOTED IN HOLES #B, #C, AND #D. V934344. ACCOMPLISH INITIAL INSPECTION OF FR16 LHS HOLES #C AND BEFORE THE AIRCRAFT REACHES 37,691 TOTAL AIRCRAFT FLIGHT 4,700 FLIGHT CYCLES THEREAFTESDR YENA2022041300371None · noneFLT#655, SYR-MCO. 'FUMES STRONG CHEMICAL BURNING SMELL DESCENDING THROUGH 5,000; AS PRECAUTIONARY PERFORMED ENGINE RUNS (ENG 1-2)- WITH ASSOCIATED PACKS, COULD NOT DUPLICATE. COMPLIED WITH INFO. NOTICE 2017-T015, SECTION A. ISOLATED FAULT TO TYPE 10A. PER TSM SDR A6WA202204118483Angle · crackedFLOOR SUPPORT ANGLE ALONG FS621 BULKHEAD OUTBOARD OF FLOOR BEAM LBL27 IS CRACKED (MARKED) *****AIRCRAFT REMOVED FROM SERVICE***** R&R -1 ANGLE, (EXISTING REPAIR), REF BOMBARDIER REO 601R-53-61-117 REV-D DATED 2017-02-26 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51SDR SWIA202265537None · corrodedL/H FLOOR DOUBLER HAS CORROSION ON AFT INBOARD SURFACE LOCATED AT FRAME 15. (C-CHECK RO 4/27/2022) REMOVED AND REPLACED CORRODED L/H FLOOR DOUBLE AT FRAME 15 REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK ACCOMPLISHEDSDR R61A2022042500304Stringer Splice · corrodedSTRINGER 21L CORRODED BETWEEN FRAMES 88-89. PERFORMED STRINGER 21L REPAIR BETWEEN FR83 AND FR90 REF ETD2022-170-013734SDR QXEA2022041300152Splice · corrodedCENTER FUSELAGE III RH SPLICE FR 89 AND Y=+12 HAS CORROSION. REMOVED AND REPLACED CENTER FUSELAGE III SPLICE IAW SRM 51-40-08.SDR QXEA2022041300151None · noneCENTER FUSELAGE III RH INTERCOSTAL AT FR 90-91 AND Y=+11 HAS CORROSION. BLENDED CORROSION AT CENTER FUSELAGE III RH INTERCOSTAL AT FR 90-91 Y=+11 IAW SRM 51-10-03.SDR 2022FA0000205Bulkhead Web · chafedDAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.60) WAS NOTED IN THE FORM OF NUMEROUS CHAFES. THE CHAFES WERE MEASURED TO BE ON AVERAGE 0.50" IN LENGTH WITH THE DEEPEST CHAFE BEING 0.008" DEEP.SDR R61A2022040800259Shear Angle · corrodedSHEAR CLIP CORRODED FRAME 86 STRINGER 27R-28R.REMOVED AND REPLACED SHEAR CLIP AT FRAME 86 STRINGER 27R-28R REF: SRM 51-40-08.SDR HALA2022041300091Floorbeam · gougedC-CHECK MAJOR REPAIR - DURING C CHECK ON 495, GOUGES WERE FOUND ON THE LH OVER WING FLOOR BEAM TO FUSELAGE MAIN FRAME FITTING AT STA. 674 AND STA. 756. THE GOUGES WERE SMOOTHED TO A 63 RMS FINISH OR BETTER WITH A MINIMUM BLEND RADIUS OF 1.0 IN. AND HFEC INSPECSDR R61A2022042500303Shear Angle · corrodedCORRODED SHEAR CLIP FR90 STR29L. REMOVED AND REPLACED SHEAR CLIP AT FR90 STR29L. REF: SRM 51-40-08SDR R61A2022042500302Shear Angle · corrodedCORRODED SHEAR CLIP FR88 STR28R. REMOVED AND REPLACED SHEAR CLIP ON FR88 STGRS 27R - 28R REF EMB 170/175 SRM 51-40-08SDR R61A2022042500297Shear Angle · corroded"CORRODED SHEAR CLIP FR86 STR28L. REMOVED AND REPLACED SHEAR CLIP AT
FR86 STR28L. REF SRM 51-40-08."SDR R61A2022042100287Shear Tie · corrodedCORRODED SHEAR CLIP FR85 STR28L. : REMOVED AND REPLACED SHEAR CLIP AT FR85 STR28L. REF SRM 51-40-08.SDR R61A2022042100285Shear Tie · corrodedCORRODED SHEAR CLIP FR86 STR 23L ALT SURFACE. : REMOVED AND REPLACED SHEAR CLIP AT
FR86 STR 23L. REF SRM 51-40-08.SDR 2022FA0000524Exhaust Valve · brokenDURING CRUISE FLIGHT PILOT REPORTED ENGINE BEGAN TO RUN ROUGH AND MANIFOLD PRESSURE INCREASED. HELICOPTER RETURNED TO HELIPAD AND MADE A NORMAL LANDING. EXHAUST VALVE STEM BROKE AT BELL CURVE AND WAS RELEASED INTO CYLINDER.SDR SWIA202265801None · damagedAFT FACE BULKHEAD AT FS280.00 ANGLE DEFORMED / CRACKED AT WL97.70. (C CHECK RO 5/23/22) REMOVED AND REPLACED ANGLE ON AFT FACE BULKHEAD AT FS280.00 AT WL97.70 IAW CRJ 900 SRM 51-42-06-001-001-A01 / DRAWING #CC670-34010 REV K. (SEE CONTINUATION SHEET FOR SDR SWIA202265800None · damagedAFT FACE BULKHEAD AT FS280.00 ANGLE DEFORMED / CRACKED AT WL85.60. (C CHECK RO 5/23/22) REMOVED AND REPLACED NEW ANGLE ON AFT FACE BULKHEAD AT FS280.00 AT WL85.60 IAW CRJ 900 SRM 51-42-06-001-001-A01 / DRAWING # CC670-34010 REV K. (SEE CONTINUATION SHEETSDR R61A2022042500301Shear Angle · corroded"AFT CARGO SHEAR CLIP CORRODED ON FRAME 84 AND STRINGER 28L-29L. REMOVED AND REPLACED SHEAR CLIP AT FR. 84 BTWN STGRS 28L - 29L REF EMB 170/175
SRM 51-40-08"SDR R61A2022041900272Shear Tie · corrodedAFT CARGO- CORROSION ON FLOOR BOARD SUPPORT BRACKET ON FRAME 76 FROM CENTER LINE TO STRINGER 29R. REMOVED AND REPLACED RH SUPPORT FR
76 STGR 29R-CTR REF EMB SRM 51-40-08.SDR R61A2022041800269Shear Tie · corrodedAFT CARGO- CORROSION ON FLOOR BOARD SUPPORT BRACKET ON FRAME 75 FROM CANTER LINE TO STRINGER 29R. REMOVED AND REPLACED FLOOR BOARD SUPPORT BRACKET ON FRAME 75 FROM CENTER LINE TO STRINGER 29R. REF SRM 51-40-08.SDR R61A2022041400266Shear Angle · corroded"AFT CARGO SHEAR CLIP CORRODED ON FRAME 85 AND STRINGER 23L-24L.REMOVED AND REPLACED AFT CARGO SHEAR CLIP AT FRAME 85 AND STRINGER 23L-24L.REF: SRM
51-40-08. "SDR SWIA202265854None · crackedAFT EQUIPTMENT BAY R/H SIDE FS 625 CLIP AT STR 14R IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR14R CLIP REF DWG 601-35012 REV-B AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.
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