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 DALA2024040804176Window Frame · damaged(LOG 5748470) RT WINDOW 18 AT STA. 500K-500L LIGHT STRIKE. REPAIRED LIGHTNING STRIKES PER NON ROUTINE CARD 002 AND ERA 617133-14.SDR 2024FA0000294Web · chafedDURING THE 96 MONTH INSPECTION FOUND THE RH WEB FORWARD OF E-EXIT TO HAVE 3 EACH CHAFE LOCATIONS. REPAIR 3 CHAFFED AREAS ROUND E-EXIT PER AQRD ERO-979437. REPAIRED 3 CHAFFS AROUND E-EXIT IAW AQRD ERO-979437 N678QS EMERGENCY EXIT DOUBLER CHAFED. REV. IR DATEDSDR N6WA2024050211Stringer · corrodedSTRINGER 21RH BETWEEN FS333.00 - FS379.00 HAS CORROSION. R&R STRINGER 21RH BETWEEN FS333.00 - FS379.00 IAW CRJ SRM 51-42-06 EO C700-53MR-005-OSDR SWAA2024041870767Structure · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK<BR>IAW SRM 51-40-02 & DWG 143A0060;[02] REMOVED AND REPLACED PANEL BREAK<BR>IAW SRM 51-40-02 & DWG 143A0060<BR>BS540 LBL1 WL208SDR IXXA2024041703Door Frame · corrodedALC DOOR FRAME HAS 4 EACH NUTPLATE HOLES WITH CORROSIONSDR AALA202404121936Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED LEFT HAND CONTINUITY FITTING PER EA 351275.SDR CALA2024040500983Window Frame · cracked(SUPPORT TASK) COCKPIT LH NO. 1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER CRACK REPAIRED PER EA 5310-04554 CARD IS FOR REPORTING ONLY NO M AIT ON THIS NR REPAIR WAS ACCOMPLISHED ON OP 4005. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 4066 NR 20611 BY MSDR CALA2024040500982Window Frame · cracked(SUPPORT TASK) COCKPIT RH NO. 1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER. CRACK REPAIRED PER EA 5310-04554 CARD IS FOR REPORTING ONLY NO M AIT ON THIS NR REPAIR WAS ACCOMPLISHED ON OP 4003. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 4066 NR 20612 BY SDR DALA2024040404051Web · corrodedCORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH. SUMMARY OF NRC 00651: CORROSION LEVEL 2. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH WAS REPAIRED PER PRI 616779-14 REV 1 AND ER/A 616779-14 REV ORIGINAL SECTION I: PERMANENT SDR REXA2024073000580Floorbeam · crackedR/H COCKPIT FLOOR BEAM IS CRACKED ALONG VERTICAL RADIUS AT FS280.00, RBL 12. REPAIRED CENTER COCKPIT FLOOR BEAM AT RBL 12.00, F.S.280 IAW MHIRJ AVIATION REO 690-53-11-1710 REV -- DATED 2024-03-25.SDR UIEA2024040500250Door Frame · corrodedCRACK-VERTICAL FRAME, L2 MAIN ENTRY DOOR FWD UPPER SIDE.(<P>1. PERFORM EI T2024A52M-488, SEQUENCE A REV=0 2. ACCOMPLISHED EI T2024A52M-488 REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024040500249Door Frame · corrodedFIND DOOR R1 AFT LOWER SIDE FRAME WEB CORROSION(<P>1. PERFORM EI T2024A52M-491, SEQUENCE A. REV=0 2. ACCOMPLISHED EI T2024A52M-491. REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR CALA2024040500984Window Frame · crackedFOUND CRACK ON THE LH WINDOW POST AFTER NDT WAS PERFORMED PER EA 5310-04554 REV C (REF. AAR NR 100004994)SDR ASAA2024040249389Floorboard · delaminatedFLOOR BOARD AFT WET AREA DELAME P/N 147A5810-23. GROUNDED - YES. REPAIRED FLOOR BOARD AFT WET AREA P/N 147A5810-23 DELAMINATION USING A PERMANENT REPAIR IAW B737-800 SRM 53-00-50-2R-0 AND 53-00-50-2R-7.SDR 4DPA2024040200001Access Door · missingCREW REPORTED- AFTER GEAR RETRACTION WE HEARD LOUD WIND BLOWING NOISE AROUND THE FRONT OF THE AIRCRAFT. AS WE TRIED TO FIGURE OUT THE PROBLEM UPON REACTION 7-8 THOUSAND FEET THE FWD ACCESS DOOR OPEN EICAS MSG APPEARED. RETURNED TO BURBANK AND HAD IT INSPECTESDR CALA2024040300968Stiffener · crackedUPON INSTALL OF R/H LATERAL SKIN PANEL FOUND SKIN STIFFENER AT L OWER LAP JOINT FR1-2 TO HAVE CRACK AT AFT END. REMOVED AND INSTALLED NEW R/H LATERAL SKIN PANEL SKIN STIFFENER AT LOWER LAP JOINT FR1-2 AS PER A319 SRM 51-42-11.SDR CALA2024040300954Window Frame · crackedFLIGHT DECK FR4 WINDSHEILD LOWER CENTER POST L/H NODE UPPER CROSS BOLT PRODUCED CRACK INDICATIONS AROUND BOLT HEAD AT THE 1:00 POSITION (FACING BOLT HEAD) AND CONTINUITY FITTING PER PART 2 OF THE LATEST REVISION OF ECRA AIRCRAFT FLIGHT CYCLES. 5311-03160 ON ORSDR SWIA2024040300002Window Frame · crackedCRACKED FRAME AROUND WINDOW BY SEAT 13BC: DEFERRED SEAT 13B WINDOW TRIM USING NEF-CAB-6D. SHARP EDGES COVERED WITH TAPE. NO FURTHER DISCREPANCIES FOUND. PLACARD PLACEDCAT: CDUE DATE: 11 APRIL 2024CRACKED FRAME AROUND WINDOW BY SEAT 13B (FILED CLOSED)REMOVED ANSDR 2A6D20240402001Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE L/H SIDE TRANSMISSION DECK.SDR MASA20240705018Door Frame · damagedBIRDSTRIKE STRIKE: MAJOR REPAIR: FS193.00 FRAME REPAIR / R&R FS 193.00/REPAIRED PER: C/W ALL STEPS CRJ9-51-4380.SDR ASAA2024040149505Access Panel · corrodedNOSE WHEEL WELL ACCESS PANEL 114AC HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-10-14. ORG THICK 0.060. REMOVED 0.004 REMAINING THICK 0.056. WITH IN LIMITS IAW B737-800 SRM 53-10-14. ALODINED IAW B737-800 AMM 51-21-41. PRIMED ISDR REXA2024042400362Door Frame · crackedRH AFT EMERGENCY EXIT FWD LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16335 REV IR DATED 4-9-2024.SDR REXA2024042400361Door Frame · crackedRH FWD EMERGENCY EXIT AFT LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16334 REV IR DATED 4-9-2024.SDR FDEA202404010425Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR61 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS SDR DALA2024040103963Door Frame · damagedSHIP 3313 AFT CARGO DOOOR FRAME DAMAGE ON LOWER AFT CORNER AT FLOOR LEVEL. CORRECTIVE ACTION: REWORKED AREA (L2",W0.25",D0.04") PER SRM TASK 53-41-11-205-003 FIR 001 ZONE 3. REPETITIVE CHECK REQD EVERY 2500FC. PER RSM 53- 41-11-283-001 OC OK FOR SVC. (5320095)SDR DXTA2024040111370Rub Strip · out of adjustMAIN DOOR: MAIN CABIN ENTRY DOOR REQUIRES SLIGHT PUSH TO OPEN ONCE HANDLE IS MOVED TO OPEN POSITION. CLEANED AND LUBRICATED DOOR HANDLE AND HINGE POINTS ON MED, NOTICED NO CHANGE. CLOSED AND OPENED DOOR SEVERAL TIMES TO IDENTITY WHERE IT WAS RUBBING FROM. FOUSDR SWI2024F00420Landing · cracked* L/H FORWARD EQUIPMENT COMPARTMENT BOTTOM DOOR LANDING IS CRACKED AT THE FORWARD LATCH CUTOUT. (C-CHECK RO 5/28/2024) REMOVED AND REPLACED WITH NEW L/H FWD AVIONICS COMPARTMENT DOOR LANDING P/N: CC670-33151-3 REF REO 690-53-11-1731, REV --, DATED 2024-04-SDR SWI2024F00419Landing · cracked* R/H FORWARD EQUIPMENT COMPARTMENT BOTTOM DOOR LANDING IS CRACKED AT THE AFT LATCH CUTOUT. (C-CHECK RO 5/28/2024) REMOVED AND REPLACED RH FWD EQUIPMENT COMPARTMENT DOOR LANDING REF CRJ900 SRM 51-42-06-001-001-A01, DWG CC670-33040, REV -G, AND REO 690-53-1SDR SWIA2024052900330Striker · gougedLOWER PAX DOOR SEAL STRIKER (ACFT SIDE) IS SCALLOPED WITH GOUGES. FLAGGED (C-CHECK RO 5/25/2024) INSTALLED NEW PAX DOOR LOWER SEAL STRIKER (P/N: SH670-31886-1) REF CRJ 700 SRM 51-42-21-001-001-A01 & BOMBARDIER DWG SH670-31810 REV AE. COMPLIED WITH SKYWERSSDR AALA202405075990Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON NOSE WHEEL WELL FORWARD UPPER ACCESS PANEL 114AC AT STA 243.7, RBL 10. REPLACED PANEL PER AARD 51-00-05-1.SDR AALA202405073717Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON NOSE WHEEL WELL FORWARD ACCESS PANEL 114AW AT STA 277, LBL 14. REPLACED PANEL PER AARD 51-00-05-1.SDR AALA202405078331Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON NOSE WHEEL WELL FORWARD ACCESS PANEL 114BW AT STA 243.7, S23L. REPLACED PANEL PER AARD 51-00-05-1.SDR AALA202405070173Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON NOSE WHEEL WELL FORWARD ACCESS PANEL 113BW AT STA 277, S23R. REPLACED PANEL PER AARD 51-00-05-1.SDR AALA202405079684Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON NOSE WHEEL WELL FORWARD UPPER ACCESS PANEL 113AC AT STA 243.7, LBL 10. REPLACED PANEL PER AARD 51-00-05-1.SDR FDEA202403300416Beam · crackedWINGS - CENTER WING JOINT - FR40 STGR27L - STGR28L LH HOLE C FOUND CRACK REPAIRED CENTER WING JOINT FR40 STGR27L - STGR28L CRACKED LH HOLE C PER A300-600 SRM57-10-24-201. THIS IS CATEGORY B REPAIR AND THE FIRST INSPECTION WAS 3700FC / 8100FH WHICHEVER OCCUSDR FDEA202403300415Structure · crackedCENTER WING BOX - FR47 LHS REAR SPAR DATUM HOLE C FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378646 REPAIRED THE FR47 LHS REAR SPAR DATUM CRACKED HOLE C. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE C AT FR47 LHS DURING SB57-6086 EMBODIMENT. THIS IS ASDR ASAA2024032950069Door Frame · corrodedAFT CARGO BAY FLOOR ON DOOR FRAME AT C53R CORRODED. GROUNDED - YES. REMOVED 2EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC INSPECTSDR ASAA2024032950062Door Frame · corrodedAFT CARGO BAY FLOOR, AT DOOR FRAME FORWARD CORNER AT NET MOUNT PUCK, BETWEEN C52R AND C53R GROUNDED - YES. REMOVED 2EA FASTENERS IN CORRODED AREA IAW A320 SRM 51-42-11/001 REV 148-01FEB.2024. REMOVED CORROSION IN AREA WITH A REMAINING THICKNESS OF .087 AND FOUSDR ASAA2024032950003Door Frame · corrodedAFT CARGO BAY FLOOR ON DOOR FRAME CORRODED AT STATION C55R GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC ISDR N6WA2024050101Former · corrodedCORROSION ON PAX DOOR FWD FORMER UNDER ACCESS 832FL. R&R FS311.75 FORMER IAW EO C55/700-52MR-004-O.SDR 2A6D20240329001Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROXIMATELY 0.3” LONG, 0.1 WIDE WITH A MAXIMUM DEPTH OF 0.010".SDR DALA2024040203993Crease Beam · damaged(LOG 0268330) CREASE BEAM WEB STA 332-344 RBL 52 WL 208 HAS 2EA DOUBLE DRILLED FLOOR PANEL FASTENER HOLES. C/W ERA 616537-14 REV ORIGINAL.SDR UIEA2024032200192Door Frame · dentedDENT AT FWD EDGE AFT CARGO DOOR FRAME DENT. SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 REV 42. MEASURED LENGTH 1.25" DEPTH 0.100" WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL I LIMIT REV 42. NO FURTHER DEFECTS NOTED.SDR IPXA2024040127476Fitting · brokenFOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1109 BL0. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALSDR JJBA20240412025Crossbeam · crackedIN NLG LH SUPPORT AFT OF FWD CROSSBEAM FOUND CRACKED. IN NLG LH SUPPORT AFT OF FWD CROSSBEAM REPLACED WITH NEW ONE.SDR DALA2024040203977Fitting · crackedSHIP 3272 DISC: CRACK INDICATION FOUND ON CONTINUITY FITTING LH SIDE. CRACK L= 0.200 I NCH. CRACK DIRECTION VERTICAL. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FU RTHER FLIGHT. C/A: REF. ER/A 615SDR LR7A2024032803406Web · chafedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC3212, FOUND RH AFT WHEEL WELL BULKHEAD WEB CHAFED AT FS617. RBL75, WL215. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-10. NR# 1001097551. / PSE# 53-40-17, AD 2012-06-09SDR LR7A2024032803405Rib · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD FUSELAGE RIB ASSY. CRACKED AT FS116.7, RBL43, WL231.7. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR# 1001093237.SDR LR7A2024032803404Web · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH WHEEL WELL WEB CORRODED AT FS582-588, WL146, LBL61.62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001090781.SDR LR7A2024032803402Web · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH MLG WELL WEB CORRODED AT FS596-614, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001090736.
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