JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 YENA2020122100620Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 844, INNER FRAME SEGMENT 1, IN PASSENGER CABIN, REF AEROMAN NR 2020-359260 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-04 DOORS EMERGENCY EXIT OVERWING EMERGENCY EXIT HATCH (AFT RT EEH)SDR YENA2020122100619Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 834 INNER FRAME SEGMENT 1 IN PASSENGER CABIN, REF AEROMAN NR 2020-359260 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-03 DOORS, EMERGENCY EXIT, OVERWING EXIT HATCH (AFT RT EEH) FRAME. RSDR CALA2020121801396Pressure Panel · damagedEA 5330-05216 REV B OP 003 R/H SIDE PRESSURE PANEL BETWEEN FR 35-36. ACCOMPLISHED EA 5330-05216 REV B OP003 RT SIDE PRESSURE PANEL BETWEEN FR 35-36. ADD EMP:V894270 INSP C/W THIS ITEM WAS ENTERED IN ERROR WAS FOR A/C N4248 ADD EMP:V891438. THIS ITEM WAS CRSDR R61A2020121600889Structure · damagedDAMAGE TO AFT LOWER FUSALAGE BETWEEN FR 87 AND 88 AND BETWEEN STR 29L AND 26L, REF VP-040437-2020/NR2 C1-4.SDR SWIA202056725Doubler · chafed*DOUBLER UNDER PNLS.195DR/DL CHAFED IN SEVERAL AREAS. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED DAMAGED DOUBLER IAW REO 670-53-00-290 REV F DATED 2019/04/26. PRESSURE LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR SWIA202056198Fitting · chafed*R/H INBD LUG FITTING AT WS178.00 HAS EVIDENCE OF CHAFFING (MARKED) (C-CHECK) RO 2/9/2021 BLENDED R/H INBD LUG FITTING AT WS178.00 CHAFFE DAMAGE TO A SMOOTH CONTOUR AND RESTORED FINISH. FOUND TO BE WITHIN LIMITS. REF REO 601R-57-21-3390 REV -- DATED 2020-1SDR SWIA202056197Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR12L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED GUSSET PLATE AT APPROXIMATELY FS349.00 ON STRINGER 12L. REF BOMBARDIER DWG 601R31098 REV -C AND CRJ200 SRM 51-42-06. COMPLIED WITH TASKSDR SWIA202056196Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR9L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED PAX DOOR GUSSET PLATE AT APPROXIMATELY FS349.00 AND STRINGER 9L REF DWG# 601R31098 REV. NC , AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYSDR SWIA202056195Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR7L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED GUSSET PLATE AT FS349 STRINGER 7L IAW BOMBARDIER DWG 601R31096 REV D AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYCARD 51-900-1003-SKY.SDR SWIA202055982Door Frame · corrodedPAX DOOR FWD FORMER FRAME, UNDER PANEL 832FL, IS CORRODED. (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR FWD FORMER FRAME. REF: CRJ 700 SRM 51-42-06-001-001 (A01), 51-42-21-001-001 (A01), AND DWG 601 R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR 2A6D2020121504402Deck Plate · chafedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE. THE DAMAGE AREA WAS DISCOVERED TO BE JUST AFT OF THE SCUPPER DRAIN HOLE AND IS APPROXIMATELY 0.50 LONG,
0.375 WIDE, AND 0.015 DEEP AT THE DEEPEST POINT. THE REMAINDER OF THE CHAFE EXTENDSDR SWIA202056213Door Frame · crackedAVIONICS COMPARTMENT DOOR SURROUND. THE RH / FWD AND AFT DOOR GUIDES ARE CRACKED. FLAGGED (C-CHECK) RO 2/9/2021 INSTALLED NEW SERVICEABLE AVIONICS COMPARTMENT DOOR SURROUND RH FWD AND AFT DOOR GUIDES (FRAME GUIDE FITTINGS), REF. CRJ200 SRM 51-41-02 AND CRSDR SWAA2021011441985Pressure Deck · elongatedRT CABIN FLIGHT DECK DOOR SURROUND AT STA 277 STR 1R-STR 2R UPPER SUPPORT HAS (2 EACH) FASTENER HOLES ELONGATED (18-048). REMOVED AND REPLACED UPPER SUPPORT AND WEB AT RT CABIN FLIGHT DECK DOOR STA 277 STR 1R-STR 2R, AS PER B737-7 SRM 51-40-02-0G-0; 51-40-05-SDR SWIA202054826Bracket · corrodedREFUEL TENSION BRACKET AT STR 19R AND FS 661+90 IS CORRODED. C-CHECK RO 12/26/2020. REPLACED TENSION FITTING AT STRINGER 19R FS 661+90, REF CRJ900 SRM AND DWG. LEAK CHECK GOOD.SDR SWIA202056070Door Frame · chafed*PAX DOOR SURROUND, FS310 FRAME, THE FORWARD UPPER DOOR CENTERING ROLLER FITTING IS CHAFED.(FLAGGED) (C-CHECK) RO 2/6/2021 REPLACED PASSENGER DOOR SURROUND STRUCTURE FS310.00 FRAME FOWARD UPPER DOOR CENTERING ROLLER FITTING WITH NEW. REF CRJ-700 SRM 51-41-SDR SWAA2021011338748Stub Frame · crackedCRACK SERVICE DOOR CUT OUT STUD FRAME LOCATED BS 296 BETWEEN STR 8R TO STR 9R UPPER AREA AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BS 296 BETWEEN STR 8R TO STR 9R UPPER AREA AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 PAR 9 AND DRAWING 141A8370 REV 'FSDR AALA202012149027Window Frame · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION OF L1 AND R1 WINDOW STRUCTURE, MEASURING W=4.0 IN, D=0.026 IN. ACCOMPLISHED TIME-LIMITED BLEND REPAIR, IAW EA310192 WITH A 50,000 FLIGHT CYCLE FINAL RESTORATION THRESHOLD.SDR DALA2020121404079Door Frame · corrodedCORROSION ON LOWER SILL PASSENGER CREW DOOR 832 AT LEVEL OF FR 68 AFT GALLEY AREA. CORRECTIVE ACTION: REMOVED AND REPLACED LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23L FLOOR STRUCTURE AFT GALLEY AREA, AS PER A320 SRM 51-72-11, SRM 51-42-11. OK SDR SWAA2021041535732Web · crackedPER CUSTOMER REQUEST L/H 663 VAPOR BARRIER CRACKED / REMOVED AND REINSTALLED VAPOR BARRIER WEB L/H FS 663 IN REF B737-700 SRM 51-40-02-0G-0 AND DRAWING 141A1001; CRACK REPAIRED ACCOMPLISHED ON N/R W193310SDR SWAA2021011139969Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT BS 255, RBL 4-LBL 14, WL 207.54. THE DAMAGE IS REPAIRED, PER EA 1-A53-33179 REV 1 AND EA 20-153-02588 REV IR. 56040C 04JAN21.SDR DALA2020121104057Crossbeam · crackedCRACK CROSSBEAM FR 74 AT LEVEL YB AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON CROSSBEAM FR 74 AT LEVEL YB AFT GALLEY AREA, AS PER ER/A NR 588900-14.SDR SWIA202056360Stop Fitting · corrodedPAX DOOR FUSELAGE FWD LWR PIN STOP FITTING IS CHAFED. (C-CHECK) RO 2/17/2021. REPLACED THE PAX DOOR FUSELAGE FWD LWR PIN STOP FITTING IAW CRJ 200 AMM 53-21-23-400-801 REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA202056359Stop Fitting · chafedPAX DOOR FUSELAGE FWD CENTER PIN STOP FITTING IS CHAFED. (C-CHECK) RO 2/17/2021. REPLACED THE PAX DOOR FUSELAGE FWD CENTER PIN STOP FITTING IAW CRJ 200 AMM 53-21-23-400-801 REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.SDR CALA2020121001364Stop Fitting · crackedR1 DOOR STOP NR 7 FRAME 16 AT DOUBLE JOGGLE AREA HOLE NR 6 IS CRACKED IN THE CORNER DOUBLER AND FRAME AT 2:00. CONTACT ENGINEERING F OR REPAIR-A3NB-53-4-0024 NR 9294237 GENERATED BY V061633 AT HA ECO LCQ, DUE TO CRACK AT RI DOOR STOP NR 7 FRAME 16 AT DOUBLE JSDR SWIA202056170Cap · cracked*LH WING BATT RIB CAP AT WS 48.30 BETWEEN APPROX. FS 529.00 - 544.00 IS CRACKED (C-CHECK) RO 2/9/2021 LH WING BATT RIB CAP AT WS48.30 REMOVED AND REPLACED. REF CRJ200 SRM 51-42-21 AND DWG 601R10204 REV J / COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA202055572Gusset · corrodedCORROSION ON GUSSET (P/N SH670-31998-1) FS 349.00, STGR 20R. C-CHECK RO 1/17/2021. REMOVED CORRODED GUSSET AND REPLACED WITH NEW FABRICATED GUSSET (P/N SH670-31998-1) AT FS 349.00 AND STGR 20R, REF BOMBARDIER DWG SH670-31950 REV Y AND CRJ700 SRM 51-42-06-001SDR SWIA202057261Landing · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA41533-601R-53-11-2381 943SW-PR1 - LEFT TRU DOOR AFT LATCH CUT-OUT CRACKED. COMPLED WITH TEMPORARY REPAIR PER REO 601R-53-11-2381 DATED 2013-04-18 STEP 1 AND 2. PERMANENT REPAIR DUE WITHIN 6000 FLT HRS WITH ESCALATION SDR SWAA2020123135448Door Frame · crackedFWD ENTRY DOOR AFT SIDE DOOR FRAME IS CRACKED AT INBOARD UPPER CORNER. REPAIRED FWD ENTRY DOOR AFT SIDE DOOR FRAME DAMAGE AT INBOARD UPPER CORNER, PER ER 20-03691 REV IR AND EA 20-152-02514 REV IR.SDR SWAA2020123135452Pressure Deck · crackedLEFT HAND MAIN WHEEL WELL HORIZONTAL BEADED PRESSURE DECK WEB CRACKED AT LBL 31 STA 665 WL 201. CRACK IS ON FWD INBOARD SIDE OF INBOARD MOST BEAD. REMOVED DAMAGE PART OF THE HORIZONTAL PRESSURE DECK BS 663-674 LBL 30-LBL 60 WL 201 AND REPAIRED, IAW SRM 53-40SDR 2020F00485Doubler · crackedREPAIR TO NOSE LANDING GEAR WHEEL WELL CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. WITH FAA FORM 8100-9 DATED 06/01/2020.SDR N6WA2020120702Beam · corrodedCORROSION ON TOP CAP OF LBL 27.00 AFT OF FS 1031. REMOVED BEAM AND FABRICATED REPAIR PARTS, IAW EA 10-2020-009. INSTALLED BEAM SPLICE REPAIR AND PAINTED LBL 27.00 FROM FS 1000 TO 1031, IAW EA 10-2020-009 AND EO CRJ500/700-53MJ-011-O.SDR CALA2020120701348Beam · corrodedM/D LAV M DOOR THRESHOLD LOWER BEAM FOUND CORROSION, REFER TO NON- ROUTINE NR 9419961. M/D LAV M DOOR THRESHOLD LOWER BEAM REPAIRED, AS PER ECRA2541-01518 REV ORIG REFER NON-ROUTINE NR 9419961 SWS FOR DETAILS.SDR CALA2020120701347Beam · crackedM/D LAV L DOOR THRESHOLD LOWER BEAM FOUND CRACKED AND CORROSION, REFER TO NON-ROUTINE NR 9419968. M/D LAV L DOOR THRESHOLD LOWER BEAM REPAIRED, AS PER ECRA2541-01519 REV ORIG REF TO NON-ROUTINE NR 9419968 SWS FOR DETAIL.SDR SWIA202055686Pressure Deck · corroded* LH UPPER SURFACE OF PRESSURE FLOOR SILL HAS MULTIBLE AREA'S OF CORROSION. CIRCLED WITH GREASE PENCIL (C-CHECK) RO 1/29/2021 REMOVED CORROSION ON LH UPPER SURFACE OF PRESSURE FLOOR SILL, WITHIN LIMITS REF REO 601R-53-41-666 REV -C DATE 2012-11-6. COMPLIEDSDR SWIA202055685Pressure Deck · corroded* RH UPPER SURFACE OF PRESSURE FLOOR SILL HAS MULTIBLE AREA'S OF CORROSION. CIRCLED WITH GREASE PENCIL (C-CHECK) RO 1/29/2021 REMOVED CORROSION FROM RH UPPER SURFACE OF PRESSURE FLOOR SILL PANEL TO ACCEPTABLE LIMITS REF. REO 601R-53-41-666 REV. C DATED 20SDR SWIA202055684Post · damagedF.S 409+128 BL 0 RH VERTICAL POST AFT RADIUS DEFECT NOTED. (C-CHECK) RO 1/29/2021 REMOVED AND INSTALLED NEW RE-INFORCING ANGLE REF. CRJ 200 SRM 51-42-22 & CRJ 200 SRM 51-42-06 & REO 601R-53-41-889 REV. C DATED 2018-01-03. COMPLIED WITH TASK CARD 51-900-100SDR SWIA202055449Post · damagedFS 409+128 BL 0 RT VERTICAL POST FWD RADIUS DEFECT NOTED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW POST ASSEMBLY (LT & RT), AND NEW (LT & RT) SUPPORT ANGLES AT FS 409 +128 BL 0, REF CRJ 200 SRM 51-42-06 AND REO 601R-53-41-889 REV B DATED 2017-03-06, CSDR SWAA2021011338316Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK AT LEVEL STA 663 AND LBL 32 PASSENGER CABIN CENTER SECTION. CRACK LENGTH: 0.196 INCH APPROXIMATE. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75 TO STA 675 AND LBL 30.00 TO LBLSDR REXA2020122300846Door Frame · corrodedFS 280.00 BULKHEAD, LT DOOR FRAME SKIN IS CORRODED AT FLOOR LEVEL. REPAIRED FS 280.00 BULKHEAD LT DOOR FRAME SKIN, IAW REO 670-53-11-745 REV-A DATED 2016/10/28.SDR FDEA202012063049Strap · damagedAFT CARGO COMPARTMENT FUSELAGE CIRCUMFERENTIAL STRAP AT STA 1620 FROM STRINGER S-28L TO S-29R PUNCTURED, DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED CIRCUMFERENTIAL SPLICE STA 1620 S-27L TO S27R, IAW SRM 51-40-02 AND DWG 146N3810. MAJOR REPAIR.SDR SWIA202055756Fitting · crackedRH WINDSHIELD SIDE POST LOWER O/B ANGLE IS CRACKED. (C-CHECK) RO 2/1/2021 REMOVED OLD UNSERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE. DRILLED, LOCATED, AND INSTALLED NEW SERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE, P/N 601R33235-4S IAW CRJ 2SDR SWIA202055480Support Beam · chafedCARGO DOOR SURROUND TRACK SUPPORT BEAM FORWARD OF FS 621 CHAFED FROM CABLE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW CARGO DOOR SURROUND-TRACK SUPPORT BEAM FORWARD OF FS 621.00, CRJ 200 SRM 51-40-11, SRM 51-42-21. SEE ATTACHED CONTINUATION CARD FOR DESDR SWIA202055456Support Beam · crackedCARGO DOOR SURROUND TRACK SUPPORT BEAM BRACKET AT FS 574 CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW BRACKET PART NUMBER 601R35050-121, IAW CRJ200 SRM 51-42-21.SDR SWAA2020122234343Pressure Deck · damagedFLIGHT DECK FLOOR DAMAGED. ACCOMPLISHED FLIGHT DECK FLOOR REPAIR WEB, PER EA NR1-A53-33179.SDR UIEA2020112402454Doubler · corrodedUPON REMOVAL OF Z-STIFFNER AT BULK CARGO THRESHOLD, FOUND DOUBLER AT AFT SIDE OF FRAME 1417 CORRODED. REMOVED AND REPLACED THE CORRODED DOUBLER AT THE AFT SIDE OF THE FRAME AT STA 1417 STR 32L-34L, IAW FAS EA 20031 REV R.SDR UIEA2020112902470Door Frame · corrodedFWD PIT CORROSION ON MAIN FRAME AFT DOOR JAMB AT THRESHOLD. EVALUATED 615.5 FRAME LOWER CHORD STR 33R-34R AND FOUND 100% OUT OF LIMITS AND REPAIRED, IAW FAS EA 20036 REV IR.SDR DALA2020120703983Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 LT SIDE AT OPEN FASTENER HOLE 2. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE 2 FRAME 68 DOOR STOP 1 LT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.SDR DALA2020120703982Stop Fitting · crackedCRACK INDICATION ON FRAME 66 DOOR STOP FITTING NR 7 LT SIDE AT OPEN FASTENER HOLE 2. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: REPAIRED HOLE NR 2 ON DOOR STOP FITTING NR 7 ON FRAME 66 LT SIDE, AS PER SRM A320 53-41-12-300-008 AND 53-41-12-300-010.SDR DALA2020120703981Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 RT SIDE AT OPEN FASTENER HOLE 4. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE NR 4 FRAME 68 DOOR STOP 1 RT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.SDR DALA2020120703980Stop Fitting · crackedCRACK INDICATION ON FRAME 68 DOOR STOP 1 LT SIDE AT OPEN FASTENER HOLE 4. AA 5311-01216, AD RELATED. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE 4 FRAME 68 DOOR STOP NR 1 LT, AS PER A320 SRM 53-41-12-300-008 AND 53-41-12-300-010.
Back to JASC 5310