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 SWIA2024F00625Door Frame · corrodedPAX DOOR FRAME, FS313.56, DD4 AND DD5 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR FRAME, FS313.56, DD4 AND DD5. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH 51-900-1002-SKY AND SDR SWIA2024F00624Cleat · corroded1 EA CLEAT @ PAX DOOR FRAME, FS313.56 AND DD4 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND REPLACED 1 EA CLEAT @ PAX DOOR FRAME, FS313.56 AND DD4. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1SDR SWIA20240519Post · crackedCOCKPIT WINDSHIELD L/H SIDE WINDOW POST HAS CRACK AT UPPER MOST BARREL NUT LOCATION. (C-CHECK RO 7/17/2024) REMOVED DAMAGE COCKPIT WINDSHIELD L/H SIDE WINDOW POST REF CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW COCKPIT WINDSHIELD L/H SIDE WINDOW PSDR SWAA2024062687637Pressure Deck · crackedCRACK INDICATION ON WEB PRESSURE DECK AT STA 663 LBL 31 AT MAIN WHEEL WELL COMPARTME (1 EA) (CRACK LENGHT 0.187 IN. ) 2024-340911<[01] TOOL USED ON STEP#6; TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 28-NOV-24;[02] TOOL USDR SWIA202406210519Frame · corrodedAVIONICS BAY FRAME LANDING AT F.S. 364.00 BETWEEN STRINGER 25R AND 26R HAS AN AREA OF SUSPECTED CORROSION. (S/N00986) (C-CHECK RO 6/19/2024) COMPLIED WITH FRAME SPLICE REPAIR AT FS364 STGR 24R TO 24L PER CRJ 700 SRM 53-21-23-201-008-A01. LEAK CHECK GOODSDR AALA202405207043Door Frame · looseAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. TIGHTENED LOOSE LAVATORY DOOR FRAME SCREWS. FUNCTIONAL CHECK GOOD. PER AMM 20-00-00.SDR SWI2024F00584Crossbeam · corrodedAFT BAGGAGE-BAY FLOOR CROSSBEAM FS1051.3 OUTBOARD OF RBL27, CORROSION AND SCRATCHES, HN00161479 (C-CHECK RO 7/17/2024) COMPLIED WITH ALL STEPS OF REO 670-53-61-2288 REV €“ DATED: 2024-06-14 TO REPAIR CROSS BEAM AT FS1051.30 BETWEEN RBL27.00 & RBL44.SDR CALA2024052001527Landing · corrodedDURING INSPECTION AT 313AL TAIL COMPARTMENT SEC 48 STA 1809.5 RH TO STA 1832 RH WAS FOUND RS-39 TO RS-37 STRINGERS WITH CORROSION. SEE IMAGES FOR FUTHER DETAILS. REPLACED THE STRINGER 30RH, 32RH AND 36RH AS PER BOEING 767 SRM 51-40-02 AND DWG 148T3280. ITEM OKSDR CALA2024052001526Landing · corrodedAT 313AL SEC 48 TAIL COMPARTMENT ACESS BETWEEN STA 1809.5 LH AND S-30 TO S-36WAS FOUND CORROSION. SEE IMAGES FOR FUTHER DETAILS. TION ON THE EXISTENT HOLES ON AIRCRAFT SKIN, AT AREA OF STRINGER S 30LH, 32LH AND 36LH, ACCORDING TO B767 NDT MANUAL PART 6, 51-0 0SDR FDEA202405180685Crease Beam · corrodedMAIN DECK CREASE BEAM CORRODED BETWEEN STA 860-880 LH. REMOVED AND REPLACED CREASE BEAM BETWEEN STA 860-880 LH P/N BAC1515-553 (143N5540-9) BATCH 0002677936 IAW B757 SRM 51-40-02 AND SRM 53-30-13-01. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52-2R. MAJOSDR COEA2024072503917Window Frame · corrodedWO 254917 NR 200066 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: L/H FRAME 19-20 WINDOW FRAME HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FRAME PER ATR42 SRM 51-25-04 AND 51-21-27.SDR DALA2024052105375Roller Tray · crackedSHIP 1801 FOUND OUT AFT CARGO LH NO.1 ROLLER TRAY CRACKED AT BS1480. CORRECTIVE ACTION: THE CRACKED ROLLER TRAY APPLIED DOUBLER REPAIR AS PER B767-400 SRM 53-00-53-2R-1 (0346502)SDR CALA2024052001523Pressure Deck · unknownACCOMPLISH PERMANENT REPAIR AT LH W/W VERTICAL PRESSURE DECK WEB BETWEEN LBL 40.0 AND LBL 45.64.SDR VNAA2024052011101Structure · damagedGASH/HOLE IN RT SIDE OF CABIN EXTERIOR AT THE "G" IN EAGLE / C/W MAJOR AIRFRAME REPAIR ( FS453.00 - FS469.00 ) & ( STGR16 - STGR17 ) IAW CRJ900 SRM 53-00-01-201-001-A03.SDR JR2R20240517117Door Frame · corrodedFWD CARGO LOWER DOOR SURROUND BEAM CORRODED. REPAIREDSDR JR2R20240517114Landing · corrodedFWD CARGO DOOR CUT-OUT LOWER SEAL LANDS CORRODED IN MULTIPLE LOCATIONS . REPLACEDSDR JR2R20240517113Landing · corrodedFWD CARGO DOOR CUT-OUT LOWER SEAL LANDS CORRODED IN MULTIPLE LOCATIONS . REPLACEDSDR JR2R20240517112Landing · corrodedFWD CARGO DOOR CUT-OUT LOWER SEAL LANDS CORRODED IN MULTIPLE LOCATIONS . REPLACEDSDR JR2R20240517227Beam · corrodedRH AFT LONG BEAM REPAIR AT FR87-FR88 RBL11 CORRODED. REPLACEDSDR KCSA202405171061Pressure Deck · crackedMAIN DECK R/H CANTED PRESSURE DECK COMPOSITE CLOSE OUT PANEL CRACKED STA 1240 RBL 82SDR DALA2024051705297Door Frame · corrodedCORROSION ON DOOR JAMB BTW L24 AND L24 LOWER AREA AFT CARGO. SUMMARY OF NRC 00205: CORROSION LEVEL 2. DOOR JAMB AND REPAIR DOUBLERS (ANGLES) BTW L24 AND L24 LOWER AREA AFT CARGO WERE REPLACED PER B717 SRM 53-20-15-2R REP 7.SDR SWIA202406210516Frame Splice · damagedACCESS REQUIRED (FRAME SPLICE REPAIR) FOR SECTION OF STRINGER 26L REMOVAL TO ACCOMPLISH STRINGER REPAIR BETWEEN FS953.00 - FS969.00, ON WORK CARD HN00156947 / CAMP 28170629. (C-CHECK RO 6/19/2024) COMPLIED WITH ACCESS FOR (FRAME SPLICE REPAIR) FOR SECTSDR SWIA20240516Window Post · crackedWINDSHIELD CENTER POST LOWER FITTING CRACKED ON AFT RIGHT FACE FROM LOWER EDGE TO SECOND/UPPER FASTENER. (C-CHECK RO 6/6/2024) REMOVED AND REPLACED WINDSHIELD CENTER POST LOWER RIGHT FITTING WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1SDR QXEA2024052800142Beam · corrodedRH LONGITUDINAL BEAM AT FR 88 HAS CORROSION. REMOVED AND REPLACED RH LONGITUDINAL BEAM BETWEEN FRAME 85-89 REF SRM 51-40-08. RESTORED SURFACE PROTECTION AND APPLIED A LAYER OF CIC TO THE RH LONGITUDINAL BEAM BETWEEN FRAME 85-89 REF SRM 51-23-06 AND CPM 51-25-0SDR CALA2024052001522Door Frame · crackedSTRUCTURE ON TOP OF L-1 DOOR CUTOUT CRACKED AT STA312 WL282 LBL33. REF AAR N/R 9884852. ACCOMPLISHED REPAIR AT L-1 DOOR CUTOUT STA 312 WL 282 LBL 33 REF USED BOEING SRM 53-10-07-2R-1 REPAIR 1. NOTE, THIS REPAIR RE QUIRE INSPECTION WITH AN INTERVAL OF 12,000 FLSDR DALA2024051905328Window Post · damagedAIRCRAFT 3723, DURING INSPECTION DAMAGE WAS FOUND TO THE UPPER RIGHT CORNER OF THE LH NO. 1 FLIGHT DECK WINDOW. THE DAMAGE CONSISTS OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-3) OF THE LH NO. 1SDR CALA2024051701498Window Frame · damagedFUSELAGE LH #3 WINDOW FRAME E-F, G-H POST AND E-G UPPER SILL WERE REPAIRED AT GYR. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF EC/RA 5610 -01548 ON OR BEFORE THE AIRCRAFT REACSDR DALA2024051605251Door Frame · corrodedCORROSION ON DOOR JAMB BTW STA Y=370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00172: CORROSION LEVEL 2. DOOR JAMB BTW STA Y =370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R-REP 6, PAR 6. (LSDR VNAA20240619012Strap · corrodedCORROSION ON STRAP, INNER FS 349.00 AND STGR 17LH AT PASSENGER DOOR SURROUND STRUCTURE. FITTING WAS FOUND OUT OFF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR SWAA2024061085889Beam · crackedLOWER HORIZONTAL BEAM WEB AT STA 1088+1' RBL 20 CRACKED<[01] SUMMARY EA 24-153-01328 HAS BEEN ISSUED.SDR IPXA2024052191808Adapter · brokenFOUND BROKEN "CLS" ADAPTOR , RH FR19 BETWEEN MCD FLOOR PANELS 222DG AND 232EF REMOVED AND REPLACED CLS ADAPTER IN R/H FR 19 IAW A300 SRM 51-40-21 PARAGRAPH 7. P/N: B5377413820200 S/N: TAG 02036446. INSTALLED MCD FLOOR PANELS 222DE AND 232EF. IAW AMM 53-10-23-SDR YENA2024051700761Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16RH DOOR STOP FITTING 7 LOWER INBOARD HOLE, CRACK DIRECTION 6 OCLOCK AND CRACK DEPTH 0.179 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00015) REF AE W/O# 2024-49/1. N/R# 2024-218389. REMOVED AND REPLASDR YENA2024051700758Crossbeam · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON OPEN HOLE H1 LOC ON CROSSBEAM FR16LH. CRACK DIRECT ION 12 OCLOCK AND DEPTH =0.100 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00018) REF AE W/O# 2024-49/1. N/R# 2024-218446. PERMANENT REPAIR ON CROSSBEAM FR16 LH ISDR YENA2024051700757Frame · crackedDURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON AFT FRAME SEGMENT (1) OF THE EEH 833 CRACK LENGTH 0.350 INCH;(RESOLVED ON W/O: 1301529 TASKCARD: NR-00019) REF AE W/O# 2024-49/1. N/R# 2024-218388. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCSDR YENA2024051700756Door Frame · crackedDURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON FWD AND AFT FRAME SEGMENT (1 OF THE EEH 844 CRACK LENGTH 0.270 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00020) REF AE W/O# 2024-49/1. N/R# 2024-218387. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON SDR YENA2024051700755Frame · crackedDURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON FWD AND AFT FRAME SEGMENT (1) OF THE EEH 843 CRACK LENGTH 0.315 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00021) REF AE W/O# 2024-49/1. N/R# 2024-218386. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE OSDR CALA2024051701493Door Frame · gougedRH EMERGENCY EXIT UPPER FRAME IS GOUGED BY LINER HARDWARE. RMVD AND RPLD RH EMERGENCY EXIT UPPER FRAME IAW A319 SRM 51-42- 11-001 AND A319 SRM 51-72-11-911-001.SDR DALA2024051605283Door Frame · gougedSHIP 3402 GOUGE DAMAGE AT AFT LOWER EDGE OF FORWARD CARGO DOOR CUT-OUT. CORRECTIVE ACTION: COMPLIED WITH ERA 618123-14. (5875791)SDR YENA2024051500733Beam · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON CENTRAL BEAM RH BTW FR17 AND FR18 Y=280 AT CABIN FLOOR STRUCTURE (W1); REF TOMEX WO N265JB/2552/E190/BRIDGE CHECK: : CORROSION ON CENTRAL BEAM RH BTW FR17 AND FR18 Y=280 AT CABIN FLOOR SSDR ASAA2024051451614Beam · corrodedR2 THRESHOLD CORROSION AT FR 68 - Y1750 GROUNDED - YES. REMOVED AND REPLACED R2 THRESHOLD SILL BEAM IAW A320 SRM 51-42-11/001 REV 148- 01 FEB 2024 AND AIRBUS DWG D53480019. P/N-D5348004320701 PO# 10409518SDR SWAA2024062685371Vapor Barrier · crackedCUSTOMER REQUEST-CRACK ON VAPOR VARRIER LOCATED RBL 39 AT BS 663.75 AT CENTER WING COMPARTMENT 2024-335583<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 11-APR-25SDR REXA2024062000460Door Frame · crackedL/H AFT OVERWING EMERGENCY EXIT DOOR S/N SB1423 TOP FORMER IS CRACKED. REPAIRED LH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-16665 REV A DATED 5/31/24. REQUIRES NDT STEP 3 IAW CRJ900, EA NO: CRJ952-16665, REV IR. CONDUCTED AN EDDY CURRENT INSPECTION ON SDR REXA2024062000459Door Frame · cracked"R/H AFT OVERWING EMERGENCY EXIT DOOR S/N SB1424 TOP FORMER IS CRACKED. REPAIRED RH AFT EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-16668 REV IR DATED 5/31/24. REQUIRES NDT STEP 3 IAW CRJ900, EA NO: CRJ952-16665, REV IR. CONDUCTED AN EDDY CURRENT INSPECTION ONSDR REXA2024062000458Door Frame · cracked"R/H FWD OVERWING EMERGENCY EXIT DOOR S/N SB1426 TOP FORMER IS CRACKED. REPAIRED RH FWD EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-16667 REV IR DATED 5/31/24. REQUIRES NDT STEP 3 IAW CRJ900, EA NO: CRJ952-16665, REV IR. CONDUCTED AN EDDY CURRENT INSPECTION ONSDR VNAA20240619031Strap · corrodedCORROSION ON STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WAS REPAIRED PER REO 690-53-21-1774 REV - -SDR VNA20240530001Support · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM-53-11-43-201-001-A01SDR IPXA2024052850743Door Frame · crackedL5 DOOR, FORWARD CUTOUT, DOOR RELEASE HANDLE AREA SKIN FOUND CRACKED. PERFORM STEP 4.A TO STEP 4.C I.A.W SRM 53-60-15-2R-7 REV.100 AND WS NO.40398 STEP 1 TO STEP 3. PERFORM STEP 4.E TO STEP 4.L I.A.W SRM 53-60-15-2R-7 REV.100 AND WS NO.40398 STEP 5 TO STEP 14SDR CALA2024051701492Window Frame · corrodedCORROSION WAS FOUND ON THE LH #1 WINDOW POST COMMON TO THE C-D POST WHILE ACCOMPLISHING EA 5310-04554 IN GYR. CORROSION WAS BLENDED PER ECRA AND AN INTERIM REPAIR ACCOMPLISHED PER THE SAME ECRA PART 1. PER PART 2 NEED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFSDR DALA2024051605259Panel · corrodedSHIP 3219 DISC: DURING CCK AND WHILE INSPECTING PER 522877-14,REV E (LP 1869716) CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE RHS NLG LATERAL PANEL (P/N D53113475202). PANEL REPLACEMENT REQUIRED. AT REV A DTE IS COMPLETE FOR THE SECTION I REPAIR. C/A: PER SSDR CALA2024051701497Forging · crackedAFTER NDT INSPECTION PER EA5310-04554 REV C, OP-003, AT LH #1 WINDOW FRAME FOUND TO BE CRACKED. REMOVED DAMAGE (CRACK) ON #1 LH WINDOW FRAME IAW EA 5310-04554 OP 003, REV C, CONFIG B.
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