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 A6WA202112108023Skin · dentedAIRCRAFT SKIN L/H EXTERIOR HAS 1 EACH DENT AT FS 409.00+15" AND S18L+3.80". DENT DIMENSIONS ARE: (P1) .500L X .450W X .002D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**SDR A6WA202112108022Skin · dentedAIRCRAFT SKIN UPPER CROWN EXTERIOR HAS 1 EACH DENT AT FS 672.20+5.2" AND S3R+4". DENT DIMENSIONS ARE: (P1) 1.900L X .900W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERSDR A6WA202112088017Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 625.30+11 AND S24L+2. DENT DIMENSIONS ARE: (P1) .700L X .600W X .015D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******SDR A6WA202112088014Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+11 AND S24L+3. DENT DIMENSIONS ARE: (P1) .600L X .600W X .013D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******SDR A6WA202112088013None · gougedMAINTENANCE FOUND 2 EACH SCRATCHES COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS 621 AND RBL 29.75 AT WL 137.18-137.95 . DAMAGE MEASURES: (P1) = .350"L X .010"X .005" AND (P2) = .500"L X .010"W X .005"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRSDR A6WA202112088015Skin · dentedAIRCRAFT SKIN EXTERIOR HAS 1 EACH DENT AT FS 559.00+7 AND S8L. DENT DIMENSIONS ARE: (P1) .800L X .650W X .004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***************SDR IXXA2021120704Channel · corrodedSUPPORT CHANNEL AT RBL65, TOP OF P39 BOX, RUNNING FWDTO AFT IS CORRODED IN FASTENER HOLE FOR STANCHION CONNECTIONSDR A6WA202112078008Skin · gougedMAINTENANCE FOUND 1 EACH SCRATCH AT FS 409+48 AND S25L+4 ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) .600"L X .500"W X .005"D. SCRATCH WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE****SDR A6WA202112078009Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 559+80 AND S7R+3. DENT DIMENSIONS ARE: (P1) .600L X .350W X .005D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***********SDR A6WA202112078011None · dentedMAINTENANCE FOUND DENT COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS621 AND RBL 41. DAMAGE MEASURES .600"L X .500"W X .012"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE*******************SDR A6WA202112068006None · gougedMAINTENANCE FOUND SETMARK DAMAGE AROUND RIVET ON AFT PRESSURE BULKHEAD AT FS621 AND RBL 38. DAMAGE MEASURES 1.00"L X .750"W X .040"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE***************SDR A6WA202112068007Skin · gougedMAINTENANCE FOUND 1 EACH GOUGE AT FS 640+2 AND S19L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) 1.6"L X 1.2"W X .014"D. GOUGE WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE************SDR A6WA202112068003Skin · gougedMAINTENANCE FOUND 3 EACH PREVIOUS BLENDS AT FS 409+48 TO FS 409+48+6 AND S27L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) FS 409+48 AT S27L .600"L X .500"W X .003"D (P2) FS 409+48+1.6 AT S27L .500"L X .400"W X .002"D (P3) FS 409+48+6 AT S27L .500"L X .450"W X .SDR A6WA202112068001Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 700.00+13 AND S21L+4. DENT DIMENSIONS ARE: (P1) .600L X .600W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******SDR A6WA202112068002Skin · gougedMAINTENANCE FOUND A PREVIOUS BLEND (P1) AT FS 409.00+80 AT S26R+1 MEASURING .500"L X 007"D AND A SCRATCH (P2) AT FS 409.00+72 AT S26R MEASURING .450"L X .005"D. BOTH AREAS FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31. ***************AIRCRAFT SDR 7C7A2021102300031None · noneR/H FUSELAGE DENT AT STA X178.20, ABOVE STRINGER 32R. REPAIRED IAW RD8-53-17264SDR IPXA2021102475281Strap · crackedINSPECTION TYPE:CDURING CUSTOMER WALK THROUGH FOUND STIFFENER BETWEEN FR85 AND FR86 CRACKEDREMOVED AND REPLACED STIFFENER IAW SRM 51-40-21SDR SWIA202163489None · corroded* ANTENNA DOUBLER BETWEEN FS295 AND FS310, STR27, IS CORRODED. (C-CHECK RO 1/7/2022) REPLACED ANTENNA DOUBLER BETWEEN FS 298 AND FS310, STRGR 27 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-30023 REV G. SEE CSDR SWIA202163301None · crackedDURING VISUAL INSPECTION OF LITEL REPAIR FOUND SUPPORT ANGLE CRACKED AT UPPER SIDE OF FITTING BETWEEN FS 621 AND FS 625 (C CHECK RO 12/28/2021) REPLACED FS621 LINTEL UPPER SUPPORT ANGLE IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-21.COMPLETED SKY CARD 51-SDR IXXA2021122306Angle · corrodedFORWARD LOWER CARGO BILGE PANEL STATION 522-544 RIGHT HAND HAS CORROSION AT 3 LOCATIONSSDR SWIA202163221None · crackedSTIFFENER P/N 601R317745-7 IS CRACK (C CHECK RO 12-19-21) INSTALLED NEW STIFFENER P/N 601R317745-7 REF CRJ 700 SRM 51-40-11-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01SDR SWIA202162920None · corrodedPASSENGER DOOR SURROUND LOWER FWD CAP ANGLE IS CORRODED (C-CHECK RO 11-27-21) PASSENGER DOOR SURROUND LOWER FWD CAP ANGLE IS CORRODED ON MULTIPLE ELEMENTS AND OVER FASTENER HOLES AND IS OUT OF LIMITS REF CRJ700 SRM 53-21-23-101-001-A01. REMOVED BAD FWD CASDR IXXA20211109070Frame · corrodedT FRAME AT AFT END OF KEEL PANEL 139BL IS CORRODED. T FRAME BLENDED AND REPLACED AS REQUIRED IAW B767 SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101 DETAIL VII B767 SRM 51-40-05 FIG 6 AND B767 SRM 51-40-02 PARA 4SDR CALA2021102601973Skin · noneAHM: AHM REPORTED{29-1137-S905}*LEFT HYDRAULIC FLUID LEVEL AT OR BELOW SERVICE LIMIT.* REQUEST MAINTENANCE TO PERFORM A HYD RESERVOIR FLUID LEVEL CHECK IAW AMM 12-12-01-610-801, SERVICE AS REQUIRED. IF ANY EVIDENCE OF LEAKAGE IS OBSERVED PLAN TO ACCOMPLISH MAISDR SWIA202163581None · corroded*AFT CARGO DOOR SILL ANGLE HAS CORROSION BETWEEN FS1015 AND FS1047. (C CHECK RO 1/04/2021) REMOVED CORROSION FROM AFT CARGO DOOR SILL ANGLE BETWEEN FS1015 AND FS1047, REF BOMBARDIER REO 670-53-61-913 REV A DATED 2012-11-02 COMPLIED WITH STEPS 1-6 FOR COMPLSDR R61A2021111000889Shear Web · corrodedCORROSION FOUND ON L/H SHEAR WEB AT MONUMENT ATTACHMENT HOLE AT FR 19 AFT OF L1 DOOR. ON L/H SHEAR WEB AT MONUMENT ATTACHMENT AT FR 19 AFT OF L1 DOOR HAS BEEN REPLACED IAW SRM 51-41-02 AND 51-43-02SDR R61A2021111000888Shear Plate · corrodedRH SHEAR PLATE FOUND CORRODED FROM FR 12-FR14, RH, FWD OF R1 DOOR. RH SHEAR PLATE REPLACED WITH NEW FROM FR12-FR14. FWD OF R1 DOOR IAW SRM 51-41-02 AND 51-43-02.SDR R61A2021111000895Shear Web · corrodedLEVEL 2 CORROSION FOUND ON CFIII RT SHEAR WEB FR 87-88. SHEAR WEB WAS REPLACED IAW SRM 51-42-01.SDR R61A2021111000887Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT FROM FR 12 - FR 16 L/H, FWD OF L1 DOOR. FLOOR SUPPORT FROM FR 12 - FR 16 L/H, FWD OF L1 DOOR, REPLACED IAW SRM 51-41-02 & SRM 51-43-04SDR R61A2021111000894Floor Support · corrodedLEVEL 2 CORROSION FOUND ON CFIII RT FLOOR SUPPORT FR 88-90. SUPPORT WAS REPLACED IAW SRM 51-43-03.SDR R61A2021111000886Shear Web · corrodedLH SHEAR WEB FOUND WITH CORROSION. AT FR16, FWD OF L1 DOOR. ON L/H SHEAR WEB AT FR 16, FWD OF L1 DOOR HAS BEEN REPLACED IAW SRM51-42-02.SDR R61A2021111000893Floor Support · corrodedLEVEL 2 CORROSION FOUND ON CF III LT FLOOR SUPPORT FR 88-90. SUPPORT WAS REPLACED IAW SRM 51-41-01.SDR IPXA2021103175473None · noneINSPECTION TYPE:C13DAMAGE ON MAIN DECK FLOOR PANEL ASSY (P/N:368-53-16-94477-127) BETWEEN LBL 11.0 AND RBL 11.0.FABRICATE A NEW FLOOR PANEL I.A.W UPS EO B767-5320-82003-ASDR CALA2021102201951Beam · noneA3NB-53-3-6038 CABIN FWD FLOOR STRUCTURE SUPPORT BAM HAVE CORROS ION FR20 Y254 DOT 42-047 () REPLACED SUPPORT BAM P/N D5311146100200 BATCH:0003854609 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001. Y254 BETWEEN FR 12 TO F R 24. ACCOMPLISHED BY EMP#V935834 AT SDR CALA2021102201949Seat Track · noneA3NB-53-3-6038 CABIN FLOOR SEAT TRACK Y-1292 FR20 HAVE WEAR MARK S AND GOUGES. DOT 42-053 EVALUATED FLOOR BEAM IAW SRM A320 53-00-15-283-002 FOUND OUT OF LIMITS, REPLACED BY NEW FLOOR BEAM PN:D5311278220201 BATCH:00038 6549, REPLACED IAW A320 SRM 51-42-11-001.SDR MASA20211021511None · noneCORROSION ON ANTENNA DOUBLER FS295-FS310 IN MAIN AVIONICS BAY |R&R TCAS ANTENNA DOUBLERSDR MASA20211021510Frame · noneCORROSION ON FRAME FS319 STGR 25L-25R IN MAIN AVIONICS BAY |R&R FRAME SECTORSDR MASA20211021509Stringer · noneCORROSION ON STGR 27 FS280-FS295 IN MAIN AVIONICS BAY |R&R STGR 27SDR MASA20211021508Stringer Splice · noneCORROSION ON STGR 26R SPLICE AT FS333 IN MAIN AVIONICS BAY |R&R STGR 26R SPLICESDR MASA20211021507Stringer Splice · noneCORROSION ON STGR 25R SPLICE AT FS333 IN MAIN AVIONICS BAY |R&R STGR 25R SPLICESDR MASA20220329122Web · corrodedCORROSION WAS FOUND ON AFT SIDE OF CABIN BULKHEAD WEB ON LOWER CORNER BTW 9RBL AND 12RBL APROX ON FS STA 280 | CORRECTIVE ACTION:WEB ON LOWER CORNER BTW 9RBL AND 12RBL APROX ON FS STA 280 WASREPLACED PER CRJ-900 SRM 53-11-10-201-003-A01.SDR SWIA202163487None · cracked*LEFT SIDE OF THE TRU BAY FLOOR CRACKED EMANATING FROM THE INBOARD EDGE AT THE UPPER FRAME FS193.00. (MARKED) (C-CHECK RO 1/7/2022) PERFORMED REPAIR TO LEFT SIDE OF THE TRU BAY FLOOR INBOARD EDGE AT THE UPPER FRAME OF FS193.00 IAW ALL STEPS OF REO 670-5SDR SWIA202163183None · corrodedPAX DOOR INNER STRUCTURE - INTERCOSTAL DOUBLER BRACKET CORRODED - DATUM 7 - BTWN FS'S 311/320 - REF DWG 601R31702 REV N (C CHECK RO 12-19-21) REMOVED AND REPLACED INTERCOSTAL DOUBLER BRACKET - DATUM 7 - BTWN FS'S 311/320, REF CRJ 700 SRM 51-42-06-001-001-SDR SWIA202163179None · corrodedPAX DOOR INNER STRUCTURE - INTERCOSTAL DOUBLER BRACKET CORRODED - DATUM 6 - BTWN FS'S 344/347 - REF DWG 601R31702 REV N (C CHECK RO 12-19-21) BLENDED CORROSION ON PAX DOOR INNER STRUCTURE - INTERCOSTAL DOUBLER BRACKET - DATUM 6 - BTWN FS'S 344/347. BLEND WSDR SWIA202163174None · corrodedPAX DOOR INNER STRUCTURE - INTERCOSTAL DOUBLER BRKT CORRODED - DATUM 6 - BTWN FS'S 311/320 - REF DWG 601R31702 REV N (C CHECK RO 12-19-21) REMOVED AND REPLACED INTERCOSTAL DOUBLER BRKT - DATUM 6 - BTWN FS'S 311/320, REF CRJ 700 SRM 51-42-06-001-001-A01, DWSDR SWIA202163171None · corrodedPAX DOOR INNER STRUCTURE - INTERCOSTAL DOUBLER BRACKET CORRODED - DATUM 5 - BTWN FS'S 311/315 - REF DWG 601R31702 REV N (C CHECK RO 12-19-21) REMOVED AND REPLACED INTERCOSTAL DOUBLER BRACKET - DATUM 5 - BTWN FS'S 311/315, REF CRJ 700 SRM 51-42-06-001-001-SDR FDEA202110202599None · noneMAIN DECK FLOOR SEAT TRACK FOUND GOUGE AT FR60 9" Y953 ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W A300-600F SRM 53-10-16-201, PARA4, P203-208, FIG201SDR MASA20211022514None · damagedFUSELAGE SKIN PANEL BETWEEN FS1000.00 -FS1051.30 AND STGR15L-STGR18L WAS FOUND WITH MULTIPLE DISCREPANCIES PER THE SRM. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01-001-003-A02, FIGURE 53-61-01-991-806, ITEM 1, ITEM A, EA 69-2021-177SDR CALA2021102201946None · noneAFT CARGO FR50 STRGT41RT STRINGER CORRODED. GENERATED BY N078592 ON HAECO LCQ NR 9294560/28560 0-13-205-002 TABLE 5 INSPECTION THRESHOLD FROM TIME OF EMBODIMEN T FC 60,000 OR FH 120,000 WHICHEVER VALUE IS ACHIEVED FIRST. SUB SEQUENT INSPECTIONS TBD. INSPECTIONSDR CALA2021102201943None · wornREF LP 72444378. WASTE TANK DRAIN BALL VALVE LEAKING. PERF ECRA 2011-01000 SPILL CLEAN UP PROCEDURES FOR CARGO COMPARTMENT. IMMEDIATE CLEAN UP C/W PER PARAGRAPH 2. A. 17.0 DIP REQUIRED WITHIN 7 DAYS TO ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTI
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