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 CALA2025041503856Window Frame · crackedFOR SDR TRACKING PURPOSES. REF EA 5310-08195 OP 003 LH SIDE NO. 3 WINDOW FRAME POST PERMANENT REPAIR. (REF AAR N/R 9960183) REFERENCE EA 5310-08195 REV B OP 003 SEQ#1205. PERMANENT REPAIR ACCOMPLISHED AS PER ROUTINE CARD SEQ NO. 1205 (EA 5310-08195 REV B SDR SWIA20250613411Pressure Deck · corrodedRH PRESSURE FLOOR HAS NUMEROUS AREAS OF CORROSION, BETWEEN FS409.00 +128 AND FS559.00. (FILED CLOSED)BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 - RBL 42.00 AND BETWEEN FS409.00 +128 AND FS559.00 WITH REFERENCE TO SRM 51-21-06. PESDR SWI2025F00719Pressure Deck · corrodedLH PRESSURE FLOOR BETWEEN FS409+128 AND FS559.00 HAS NUMEROUS AREAS OF CORROSION. (FILED CLOSED)BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY APPROX LBL 36.00 - LBL 42.00 AND BETWEEN FS409.00 +128 AND FS559.00 WITH REFERENCE TO SRM 51-21-06. PERFORMSDR AALA202504216211Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH DOORSTOP FITTING 7, LOWER INBOARD HOLE (H3) AT 11 O CLOCKCRACK LENGHT IS D=0.153 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING 7 LOC. AT LEVEL DOOR STOP #7 BTW FR15 TO FOR FR16 R/H I.A.W A319 SRSDR AALA202504217957Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR 20 RH DOORSTOP FITTING 7, UPPER INBOARD HOLE (H1) AT 1 O'CLOCK. CRACK LENGHT IS D=0.113 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING 7 LOC. AT LEVEL DOOR STOP #7 FR 20 R/H I.A.W A319 SRM 51-42-11-80SDR AALA202504218390Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LH DOORSTOP FITTING 7, LOWER INBOARD HOLE (H3) AT 5 O'CLOCK. CRACK LENGHT IS D=0.162 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING 7 LOC. AT LEVEL DOOR STOP #7 BTW FR15 TO FR16 L/H I.A.W A319 SRM SDR DALA2025041502942Pressure Deck · cracked(LOG 0908392) CRACK OF 2.000IN (LENGTH) PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0/LBL45.0. PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0 TO LBL45.0 WAS REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 3.SDR DALA2025041502940Window Frame · cracked(LOG 0907749) FUSELAGE RH NO. 1 FLIGHT COMPARTMENT WINDOW FRAME UPPER FWD CORNER HAS CRACKS. REPAIRED PER ERA 625593-14.SDR CALA2025041503854Fitting · crackedLH AND RH CONTINUITY FITTINGS HAVE CRACK INDICATION. REMOVED AND REPLACED CONT FITTINGS IAW A320 R53112919/ SRM 51-42 -11.SDR SWI2025F00445Pressure Deck · corrodedLH PRESSURE FLOOR BETWEEN FS409+128 AND FS559.00 HAS NUMEROUS AREAS OF CORROSION. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA2025041400011Pressure Deck · corrodedRH PRESSURE FLOOR HAS NUMEROUS AREAS OF CORROSION, BETWEEN FS409.00 +128 AND FS559.00. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR NACA2025041000001Failsafe · crackedA CRACK WAS FOUND AT FAIL-SAFE CHORD S-15R OF RIGHT SIDE(AT UPPER FASTENER LOCATION , LENGTH 5MM). PERFORMED REPAIR AT FAIL-STAFE CHORD STA 380, S-15R. 1. TRIM OFF DAMAGED AREA 2. MADE REPAIR PARTS AND INSTALLED I.A.W. EO 737-53-0379, REF FAA 8110-3 DTD 04/28SDR JR2R20250410922Door Frame · chafedMID AVIONICS BAY DOOR, 147AL, HAS MULTIPLE AREAS OF CHAFING ALL AROUND DOOR FRAMESDR SWI2025F01251Drain · corrodedLOWER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 23R HAS CORROSION ( 29949074 ) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW LOWER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 23R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SHSDR SWI2025F01250Angle · damagedFWD LAV DRAIN BOX ANGLE IMPACT BETWEEN FS379 - FS394 AT STR23R HAS CORROSION ( 29949078 ) (C-CHECK RO 09/07/2025)INSTALLED NEW FWD LAV DRAIN BOX ANGLE IMPACT BETWEEN FS379 - FS394 AT STR23R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPLSDR SWI2025F01249Drain · corrodedUPPER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 21R HAS CORROSION ( 29949033 ) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW UPPER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 21R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH6SDR ASAA2025040957364Door Frame · crackedR1 DOOR CUTOUT FWD UPPER STUB FRAME IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED STUB FRAME IAW B737-700 SRM 51-40-02-0G-0.SDR CALA2025041503849Door Frame · crackedL/H AFT O/W ESCAPE HATCH,AFT VERT.FRAME APPEARS TO BE CRACKED . REMOVED AND REPLACED L/H AFT O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A320 SRM 51-72-11-911-001 REMOVED AND REPLACED LH AFT O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A320 SRM 51-72-11-911-001.SDR CALA2025041503848Door Frame · crackedL/H AFT O/W ESCAPE HATCH,FWD. VERT.FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED L/H AFT O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A320 SRM 51-72-11-911-001. REMOVED AND REPLACED LH AFT O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A320 SRM 51-72-11-911-001.SDR SWI2025F00971Door Frame · corrodedAVIONICS BAY DOOR SURROUND DOOR CUTOUT BETWEEN FS364.00 €“ FS394.00 AND STRGR25R €“ STGL25L HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 07/16/2025)REPAIRED AVIONICS BAY DOOR SURROUND CUTOUT BETWEEN FS360-FS394 AND STGR25R-STGR25L REF REO 690-53-21-SDR SWAA2025042922877Floorbeam · crackedCRACKED BREAK PANEL BS 540 BL 0-LBL 25 WL 208.<[01] REMOVED AND REPLACED BREAK PANEL BS 540 BL 0-LBL 25 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060SDR QXEA2025042300153Doubler · corrodedDOUBLER AT AFT WET AREA AT FR.87-88R AT AFT SIDE R2 DOOR CORRODED. DOUBLER AT AFT WET AREA FR87-88 AT AFT SIDE OF R-2 DOOR FOUND TO BE OUT OF LIMITS REPLACED DOUBLER IAW SRM 51-40-08.SDR DALA2025040802710Crossbeam · corrodedSHIP 3358 CABIN CROSS BEAM UPPER CHORD UPPER SURFACE FOUND CORROSION AT FR75 LH Y450 TO RH-Y450. CORRECTIVE ACTION: COMPLIED WITH ERA 622900-14 REV ORIGINAL. (0901845)SDR 2025FA0000251Panel · crackedOUTBOARD RIGHT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD UNDERNEATH A DOUBLER BRACKET THROUGH THE PANEL AND A PREVIOUS REPAIR DOUBLER, THROUGH A FUEL LINE PENETRATION HOLE IN THE PANEL. THE PREVIOUS SDR 2025FA0000250Panel · crackedOUTBOARD LEFT LANDING GEAR WELL STRUCTURAL PANEL CRACKED FROM LOWER FORWARD EDGE OF PANEL. THE CRACK EXTENDED UPWARD THROUGH THE PANEL AND A DOUBLER BRACKET TO THE FUEL LINE PENETRATION HOLE IN THE PANEL. NO PREVIOUS REPAIR ON THIS PANEL.SDR SWIA2025090200013Lintel · crackedPASSENGER DOOR LINTEL (STGR3L) BETWEEN FS280.00 AND FS295.00 CRACKED . COMPLIED WITH SB 670BA-53-040 REV-C PART A & B AND ALL STEPS OF REO 670-53-21-493 REV-D, REPAIR OF PASSENGER DOOR LINTEL AT STGR 3LSERVICE BULLETIN 670BA-53-040, REVISION C, BS 280 TO BS.SDR NACA2025040700007Pressure Web · crackedMAIN WHEEL WELL PRESSURE WEB CRACK STA663.75+3" LBL24.5+8" APPROXIMATE SIZE L0.375. PERFORMED REPAIR AT STA 663.75+3, LBL 245.5+8 IAW SRM 53-60-51 REPAIR 4.SDR VNAA202504140037Post · corrodedVERTICAL POST LBL12 IS CORRODED AT F.S.280 FRAME AND STRINGER 25L REMOVED VERTICLE POST AT LBL12 AND INSTALLED NEW SERVICEABLE VERTICLE POST P/N CC670-34180-7 AT LBL12 F.S 280 WITH NEW IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01SDR DALA2025040902776Deck Plate · corrodedSHIP 6710 CORROSION OUT OF LIMITS IN REF. NRC 0444: CORROSION ON DECK PLATE FROM STA 1680 LBL 17 AND RBL 16 TO RBL 26, STA 1720 LBL 41 PASSENGER CABIN, IT IS OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 FIG 101. DETAIL III. CORRECTSDR IXXA2025040702Bracket · corrodedFLC CARGO DOOR LOWER SEAL DEPRESSOR BRACKET CORROED AT STA 578SDR EE4Y2025040722145Fitting · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT EO A32X-E5311-0013 WINDSHIELD CENTRAL NODE CONTINUTIY FITTING OINLY REPLACMENT REPAIR. PERFORMED EO E5311-0013-R00 AD 2020-17-03 WNDISHIELD CENTRAL LOWER NODE CONTINUITY FITTING ONLY REPLACMENT REPAIR.THIS REPAIR WAS DOCUSDR EE4Y2025040722143Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 3 UPPER OUTBOARD HOLE WITH CRACK INDICATION WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN CREW ENTRY DOOR ASDR SWIA2025090900406Window Frame · crackedLH UPPER SIDE FRAME SECTOR AT FS235 BELOW SIDE WINDOW SILL IS CRACKED (C-CHECK RO 09/07/2025) INSTALLED NEW LH UPPER SIDE FRAME SECTOR AT FS235 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG#CC670-34040 REV-C. COMPLIED WITH REOSDR SWI2025F00799Door Sill · corrodedSERVICE DOOR SILL BOTTOM ANGLE HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED MOUNTING ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND DRAWING# SH670-31950, REV Y. AND REMOVED AND REPLACED 4 EA WEB FLOOR PROTECTORS ON SERVICE SDR EE4Y2025040622139Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 2022-08-08-30200/2 UPPER FUSELAGE FORWARD ENTRY PASSENGER /CREW DOOR FR16 RHDOUGLE JOGGLE AREA STOP FITTING # 7 HOLE # 4 WITH CRACK INDICATION IN FRAME LAYER WAS FOUND. REPAIRED FUSELAGE FRAME AT DOUBLE JOGGLE AREA SDR EE4Y2025040622138Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FREEZE PLUG AND OVER SIZE BOLTS INSTALLATION AT FR66LH DOOR STOPSDR EE4Y2025040622137Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR68 RH DOR STOP FITTING # 1 HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME AT FR68RH STOP FITTING #1 IAW A320 SRM TASK 53-41-12-30SDR EE4Y2025040622136Door Frame · crackedDURING ALLEGAINT TASK ACCOMPLISHMENT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR, FR68 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME SECTION AT FR68 LH STOP FITTING # 1 IAW ASDR 2025FA0000239Panel · unknownREPAIR EVALUATION - PANEL BONDED ASSY, KEEL BEAM FAIRING (149AL), P/N 145T8616-21.SDR SWI2025F00804Door Sill · corrodedPAX DOOR LOWER SILL LOWER ANGLE HAS CORROSION IN MULITPLE LOCATIONS. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED NEW PAX DOOR LOWER SILL LOWER ANGLE REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG# SH670-31810 REV AE. LEAK CHECK GOOD. ( SEE CONTINUE CARD FOR WOSDR SWIA2025070100405Door Frame · gouged4EA GOUGES ON UPPER PAX DOOR SURROUND AT APPROX STGR 4L BEHIND NUTPLATE BRACKETS. COMPLETED REO 690-53-21-1925 REV.--, DATED 2025-04-21 FOR GOUGE DAMAGE TO UPPER LINTEL DOUBLER ABOVE PAX DOOR BETWEEN FS333.00-FS337.50 AT STR 3L. (#3 DOUBLER BLEND). ENSURED GSDR SWAA2025051956183Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.250 IN. APPROX. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAISDR DALA2025040802730Deck Plate · corrodedSHIP 6710 CORROSION PREVIUOS REPAIR ON DECK PLATE FROM STA 1705 TO 1720 RBL 15 TO LBL 15 AT PASSENGER CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00496 CORROSION LEVEL 2, PREVIUOS REPAIR ON DECK PLATE FROM STA 1705 TO 1720 RBL 15 TO LBL 15 AT PASSENGER CABIN WAS SDR UIEA2025040400441Cover · dentedDURING RAM AIR TURBINE DEPLOYMENT TEST BY TASK CARD 8017-0101, FOUND A DENT ON RAM AIR TURBINE COVER SURFACE; IT WAS EVALUATED AND FOUND OUT OF LIMITS. L= 2.400 IN, W= 1.100 IN, D= 0.075 IN.(<P>N/R 00278 THE COVER WAS REMOVED FROM THE RAM AIR TURBINE IAW CMM 2SDR 9WGA2025060954501Pressure Panel · corrodedDURING HEAVY CHECK HORIZONTAL PRESSURE PANEL, STA 464 (CANTED) - 595 SPOTS OF CORROSION (LIGHT CORROSION) AT ZONES 113 AND 114. REMOVED LIGHT CORROSION AT HORIZONTAL PRESSURE PANEL STA. 464 (CANTED) 515 ZONES 113 AND 114, MATERIAL REMOVED 0.001, IAW MD-11 SRMSDR AALA202504161200Fitting · noneAIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING RH SIDE FOR EA REQUEST EA 361898. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE FOR EA REQUEST EA 361898.SDR IXXA20250404001Frame · corrodedCORROSION ON THE SMALL FRAME, LOCATED AT THE AFT EDGE OF THE FUSELAGE CUTOUT FOR THE 313AL ACCESS DOOR, AT STA.1882, LBL14 TO RBL14.SDR SWI2025F00809Receiver · crackedS/N 0444EXTERNAL INSPECTION OF THE RH AFT FUSELAGE TRU BAY LATCH RECEIVER HAS A POSSIBLE CRACK. FLAGGED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED RH TRU LATCH RECEIVER (LANDING PN CC670-33151-6) PER DWG CC670-33040 REV-G, CRJ 900 SRM 51-42-06-001-001-A01 RESDR SIMA20250403001Seal Rest · corrodedSSI 53-21-009 FWD CARGO DOOR CUTOUT LOWER FWD, MIDDLE AND AFT SEAL REST SCREW HOLES CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR FWD CARGO DOOR CUTOUT LOWER FWD, MIDDLE, AND AFT SEAL RESTS IAW EMB 175 SRM 51-40-08 AND AMM 20-10-01.SDR AALA202504102325Door Frame · deformedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FRAME 640 AT AFT OVER WING EMERGENCY EXIT AFT LOWER DOOR GUIDE LOWER INBOARD FRAME HOLE HAS AN INDICATION OF DEFECT NOTED ATTHE 12 O'CLOCK POSITION. REAMED THE HOLE TO SIZE 0.309, THE REWORK IS WITHIN LIMITS. PER B737 S
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