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 2025FA0000073Frame · brokenBRAKE MASTER CYLINDER LOWER CONNECTING/SUPPORT ROD ON PEDAL FRAME P/N 22-2729-60-00 HAD A FAILURE CAUSING THE BRAKE MASTER TO HAVE ENOUGH SLOP TO JAM ON THE FLOOR CREATING SUBSEQUENT JAMMING OF THE RUDDER PEDAL ON THAT SIDE OF THE AIRCRAFT. PIECE OF MAIN FRAMSDR 2A6R2025013072203Deck Plate · chafedCHAFE DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK LH BEAM CAP (PN: B533K3202-201) BY A MEDICAL INTERIOR PANEL SCREW. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3189, ISSUE A DATED 16 OCT 2024, SDR 2A6R2025013072202Deck Plate · dentedDENT DAMAGE WAS DISCOVERED ON THE RH ENGINE DECK PANEL (PN: B533K3339-213) THROUGH TO THE RH ENGINE MOUNT INBOARD SUPPORT BEAM (PN: B533K3316-207). AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3426SDR CALA2025013000248Door Frame · corrodedR-1 DOOR FWD CUTOUT LOWER PAN FRAME CORROSION AND CRACKED.SDR FDEA202501290149Door Frame · deformedON PREFLIGHT WALK AROUND FOUND EMERGENCY ESCAPE ROPE RETAINER ON L-1 DOOR AFT SIDE OF DOOR JAMB DISFORMED. NOTE : DEFORMED AREA IS AT TOP AND CENTER OF AFT SIDE OF L1 DOOR JAMB.SDR DALA2025013000725Drain · crackedCRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00027: CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622331-14 REV 1 AND ER/A 622331-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-SDR CALA2025012900235Fitting · crackedLH WINDSHIELD SIDE POST UPPER ATTACHMENT, 3RD HOLE AT LOWER FACE MARKED, HAS CRACK INDICATION IN FRAME LAYER. 50% S.H. PERFORMED PERMANENT REPAIR BY GUSSET REPLACEMENT AS DIRECTED BY ECRA 5311-01953.SDR JR2R20250129766Seal Rest · corrodedFORWARD CARGO CUT OUT; FORWARD LOWER SEAL REST CORRODEDSDR JR2R20250129765Seal Rest · corrodedFORWARD CARGO CUT OUT; CENTER LOWER SEAL REST CORRODEDSDR JR2R20250129764Seal Rest · corrodedFORWARD CARGO CUT OUT; AFT LOWER SEAL REST CORRODEDSDR FDEA202501290148Pressure Deck · corrodedFWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE CORRODED AT FR40 Y953 - Y1456. COMPLIED WITH EA: 6-5310-T0382182 P1. TITLE: FUSELAGE - MAINFRAME- EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BETWEEN FR39-FR40. REPAIRED THE CORRODED PANEL AT HOSDR VNAA20250329003Support Plate · corrodedCORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELL. CORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELLWAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND SDR VNAA20250329002Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. LANDING DOOR SECTION AND STRAP AFT SIDE WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 ASDR SWAA2025030590518Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 1.250 INCH AT PASSENGER CABIN. 2025-94080<[01] REPLACED STUB FRAME AND FASTENER LOCATE BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FSDR AALA202502170750Post · damagedAIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTANDENTS REPORTS AFT LEFT LAVATORY-D DOOR IS HARD TO OPEN AND CLOSE. REMOVED AND REPLACED LAVATORY-D AFT DOOR POST. PER B737-NG SRM 51-40-02.SDR CALA2025021400360Stub Frame · crackedCRACK FOUND AT INTERNAL STUB FRAME SKIN FWD GALLEY DOOR (R1 UPPER FWD CUT OUT) APPROX. STA 294.5 BETWEEN STR 9R AND 8R CRACK LENGTH APPROX. 0.750"SDR 2VKA2025020553456Washer · crackedWHILE CHANGING THE TRANSMISSION THE TECHNICIAN DISCOVERED ONE WASHER PN:140-007-25S22E6 CRACKED.SDR VNAA20250329015Support Plate · corrodedCORROSION ON METAL SUPPORT OF CONNECTORS PX34-PX33/ PX17-PX33 RH/LH SIDE AT WHEEL WELL AREA. CORROSION ON METAL SUPPORT RH OF CONNECTORS PX34-PX33/ PX17-PX33 AT WHEEL WELL AREA WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRSDR CALA2025012900230Deck Plate · damaged{ B737-53-3-0733} FLIGHT DECK FLOOR SKIN CREASE AT LBL 14" STA 259.5. REF AAR N/R 9937202 FOUND CREASE OUT OF LIMITS AT FLIGHT DECK FLOOR SKIN STA 259.5, LBL 14" CUTOUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 53-10-51-2R-2.SDR JR2R20250127183Beam · corrodedCARGO DOOR CUTOUT LOWER BEAM UNDER LOWER SEAL RESTS CORRODED IN MULTPLE PLACES.SDR 2025FA0000055Tear Strap · corrodedFOUND CORROSION INSIDE BULK CARGO COMPARTMENT BETWEEN STA 1480 AND STA 1502, BETWEEN STR 29L AND STR 30L AND ON TEAR STRAP AT STA 1502.SDR DALA2025012900701Spar · damaged(LOG 0780822) L/H SECOND HOLE FROM THE TOP IN THE SPAR O/B HAS TOOLING DAMAGE. C/W ON ERA 623796-14AD.SDR DALA2025012700634Window Frame · crackedSHIP 3266 DISC: CRACK INDICATION ON FRAME 4 LH SIDE IN UPPER ATTACHMENT HORIZONTAL ST IFFENER. CRACK DIMENSIONS ARE: X1: 0.438 INCH APPROX, X3: 0.356 INCH A PPROX. AD RELATED. IN COCKPIT (1 EA). AA CARD 5316-01052-05A. C/A: COMPLIED WITH ER/A 544200-14AD REV. SDR JR2R20250126183Track · gougedRH DIRECT VISION WINDOW, LOWER AFT TRACK GOUGEDSDR SIMA20250125004Crossbeam · corrodedSS1 53-10-026: CENTER FLOOR CROSSBEAM AT FR11 HAS CORROSION. (LEVEL 2 CORROSION) (MAJOR REPAIR) REPAIRED CENTER FLOOR CROSSBEAM AT FR 11 IAW ERS-EJ-53MR-5138SDR FDEA202501240123Failsafe · crackedHFEC INSPECTION OF REWORKED AREA ON LH #1 DOOR FAIL SAFE RING FWD LWR CORNER FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5312-82930 C P3. TITLE: FUSELAGE NOSE SECTION - EXFOLIATION CORROSION AT FAIL SAFE RING ON DOOR #1 LHS. REPAIRED THE LH #1 DOOR FAIL SAFE RISDR J6BA20250128024Door Frame · corrodedCORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2025012800673Window Frame · cracked(LOG 0777794) INITIAL INSPECTION:CRACK ON WINDOW FRAME UPPER AFT CORNER AREA #1 RH WINDOW. WINDOW FRAME UPPER AFT CORNER AREA #1 RH WINDOW WAS REPAIRED PER ER/A 619132-14.SDR DALA2025012800672Window Frame · cracked(LOG 0777640) CRACK ON WINDOW FRAME UPPER AFT CORNER AREA #1 LH WINDOW. WINDOW FRAME UPPER AFT CORNER AREA #1 LH WINDOW WAS REPAIRED PER ER/A 619132-14 REV A.SDR CALA2025012700212Window Frame · cracked(EA5310-08195 OP1) LH SLIDE UMBER 3 WINDOW FRAME OPOST CRACKED AT FIRST LOWER CORNER FASTENER HOLE REF AAR N/R 9914099 REPLACED THE FLIGHTDECK L/H NO.3 WINDOW FRAME PER ESR-WI 16-11279 IR AND ECRA 5310-08500.SDR REXA2025021900203Door Frame · crackedL/H FWD. OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED REPAIRED LH FWD EMERGENCY EXIT DOOR IAW REO 690-52-21-182 REV -- DATED 2025-02-02 AND REO 670-52-21-103 REV -- DATED 2024-11-06SDR REXA2025021300194Door Frame · cracked"L/H AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-181 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. RESTORED TO FINISH IAW CRJ-900 SDR REXA2025021300193Fitting · cracked"RIGHT AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-180 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. INSTALLED THE R/H AFT OVER WSDR DALA2025012700635Window Frame · crackedSHIP 3266 DISC: *DTE* DURING H2 AND WHILE INSPECTING PER EM 5316-01052-05A 2 EA CRACK INDICATIONS FOUND EMATATING FROM TEH SPOT FACE OF HOLE 1 AT THE UPPER FWD CORNER OF LHS FR4 LATERAL WINDOW FRAME. C/A: ***DTE REQUIRED*** PER SECTION DTE OF 544200-14, REV C,SDR DALA2025012400585Window Frame · crackedSHIP 3136 CRACK INDICATION WAS FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, UPPER RADIUS). CORRECTIVE ACTION: COMPLIED WITH ER/A 622114-14AD. (0775567)SDR DALA2025012400584Window Frame · crackedSHIP 3136 CRACK INDICATION FOUND ON WINDSHIELD FRAME LOWER CENTER POST LH SIDE STARTING FROM UPPER FASTENER. CORRECTIVE ACTION: COMPLIED WITH ER/A 622025-14AD. (0775563)SDR CALA2025022000394Door Frame · corrodedPOSSIBLE CORROSION ON DOOR 31BL CUT OUT ZONE 311.(REF AAR NR 100 0025906) REMOVED AND REPLACED (BRAKET, AND SHER-TIE) & REINSTALLED ACCESS DOOR 311BL IAW B737-800 SRM 51-40-02-0G, SRM 51-40-05-0G-0, AMM 50-11-910-801, AIPC 52-49-11-01 & PL148A3410-10,PL148A331SDR QXEA2025021800033Doubler · corrodedDOUBLER IB OF TEXAS DOUBLER AT RBL 11 ON FRAME 90 IS CORRODED. REMOVED AND REPLACED DOUBLER IB OF TEXAS DOUBLER AT RBL 11 ON FRAME 90 IAW SRM 51-40-08.SDR ASAA2025012255968Crease Beam · corrodedRH CREASE BEAM ANGLE HAS AREAS OF CORROSION FROM FS867 TO FS 905. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-60-13-1A-1. REPAIRED DAMAGE IAW EA 900ER-53EA-28202 W:1" O: .050 R: .035 L: 5" D: .015.SDR DALA2025012300549Stiffener · crackedSHIP 3136 CRACK INDICATION FOUND ON THE HORIZONTAL UPPER STIFFENER OF THE LATERAL WINDOW FRAME AT FR 4, RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 576072-14AD. (0774234)SDR AALA202504217430Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR LOCATED AT FR16 LH AT LEVEL OF THE DOOR STOP 7 HOLE 7 IN PASSENGER CABIN 1 EA CRACK DIRECT ION 9 O CLOCK MEASURE CRACK IS L=6.352 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (REPLACED PASDR SWI2025F00426Window Post · crackedCO-PILOT WINDSHIELD POST UPPER ATTACH SUPPORT FITTING CRACKED, UPPER CANOPY AREA (MARKED) (C-CHECK RO 04/04/2025)INSTALLED NEW ATTACH SUPPORT FITTING AT CO-PILOT WINDSHIELD POST UPPER REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. AND DWG# CC6SDR IPXA2025022001204Splice Angle · corrodedCORROSION - ANGLE , MAIN DECK STA 500 LBL 40 (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-92797-REQ1 REV.1 JOB COMPLETED.SDR FDEA202501210109Crossbeam · crackedMDCC CROSSBEAM C31,-Y700 CRACKED. REPAIRED THE CROSSBEAM AT C31, -Y700 PER A300-600F SRM53-10-15-201 FIG212 & EA:6-5310- T0381895 P1. TITLE: FUSELAGE - MAINFRAME - CRACK ON FR31 CROSSBEAM, BETWEEN -Y450 AND -Y953. THIS IS A CAT A REPAIR. MAJOR REPAIR IAW FESDR SWIA20250211121Doubler · corrodedRH COCKPIT FLOOR DOUBLER HAS CORROSION ON UPPER SURFACE AROUND THE AFT END OF INBOARD CO-PILOT SEAT TRACK, BETWEEN FRAMES 11 AND 12. (C-CHECK RO 2/10/2025) CUT OUT DAMAGED PORTION OF THE RH COCKPIT FLOOR DOUBLER AND INSTALLED NEW FILLER PIECE AND FABRICSDR GTIA2025011638684Stop Fitting · crackedFR 68 LH DOORSTOP FITTING #7 HOLE #1 HAS CRACK INDICATIONS RAF-01 3371750-02 -REPAIR ACP ON HAECO S.O 122206 OPS 44630 IAW A320 SRM 53-41-12-300-010 CAT A REPAIR NO RE INSPECT REQUIREDSDR GTIA2025011638679Stop Fitting · cracked" FR 66 DOORSTOP FITTING #7, HOLE #1, (TOP, INBD) HAS A CRACK INDICATION 10:OCLOCK POS (AFT LOOKING FWD) 100% . LENGTH .4735 WIDTH 4.735-REPAIR ACCOMPLISHED REF HAECO S.O. 122206 OPS 44631 IAW A320 SRM 53-41-12-300-011 CAT B REPAIR RE INSPECT AT 15400 FC SUBSSDR SWIA20250317120Plate · gougedUPON REMOVAL OF CARGO NET MOUNTING PLATE INTERCOSTAL FOUND DEEP GOUGES IN RADIUS. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INTERCOSTAL WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-06-001--001-A01,51-42-21-001-001-A01, 51-45-00-001--001-A01, DWG-SH670-335SDR SWI202502210170Doubler · corrodedCORROSION ON CO-PILOT COCKPIT FLOOR DOUBLER BETWEEN FR 7 AND 12 IN MULTIPLE LOCATIONS AS MARKED. (C-CHECK RO 2/21/2025) REMOVED DAMAGED SECTION OF CO-PILOT COCKPIT FLOOR DOUBLER BETWEEN FR 7 AND 12. LOCATED, DRILLED, AND INSTALLED NEW CO-PILOT COCKPIT SDR SWIA20250221120Doubler · corrodedCORROSION ON PILOT COCKPIT FLOOR DOUBLER BETWEEN FR 7 AND 12 IN MULTIPLE LOCATIONS AS MARKED. (C-CHECK RO 2/21/2025) REMOVED THE DAMAGED PORTION OF THE L/H COCKPIT FLOOR DOUBLER BETWEEN FRAMES 7-12 AND REPLACED WITH A NEW SECTION BETWEEN FRAMES 9-12 REF
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