JASC 5310

Service difficulty reports · 38,519

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.

SDR VNAA202512020018Post · corrodedFLIGHT COMPARTMENT RBL 9 ENTRY POST ARE CORRODED AT F.S. 280.Dec 4, 2025 · N515AE · Cndair CL6002C10SDR VNAA202512020010Retainer · damagedAFT CARGO DOOR LOWER SEAL RETAINER IS DAMAGED.Dec 4, 2025 · N515AE · Cndair CL6002C10SDR VNAA202512020006Strap · crackedCRACK ON THE LOWER AFT SIDE OF THE SIDE POST STRAP FOR THE RIGHT-HAND WINDSHIELD. RT WINDSHIELD POST STRAPDec 4, 2025 · N515AE · Cndair CL6002C10SDR VNAA202512020005Beam · gougedRIGHT INBD LATCH BEAM LUG NR 3 HAS A GOUGE. HINGE BEAMDec 4, 2025 · N515AE · Cndair CL6002C10SDR SWIA2025120375109Window Frame · crackedAFTER EDDY CURRENT INSPECTION OF THE WINDWSHIELD CENTER POST , NR 8 ATTACH STRUCTURE CRACKS WERE FOUND IN LOWER PART. R & R WINDWSHIELD CENTER POST NR 8 ATTACH STRUCTURE IAW 00 SRM 51-24-16, SRM 51-42-21, IPC 53-11-19, PAGE 6.Dec 3, 2025 · N956SW · Cndair CL6002B19SDR HNAA2026012200066Door Frame · damagedDMT 25 COMPLY WITH PERMANENT REPAIR PER ETD2025-145-922984-B, EO1-53-25-0204 AND SRM 145/1142, 53-00-04 RE OF FRAME 20 LOWER SERVICE DOOR WITH -IN 1100 FC AS OF TAT 44,880:30 TAC 40,964. REPAIRED FRAME 20 AT THE SERVICE DOOR CUTOUT LOWER NUTPLATE HOLE IAW EMBDec 3, 2025 · N933JN · Emb EMB145LRSDR SWAA2026011242281Retainer · missingMISSING RETAINER AT UPPER SILL DOOR CUT OUT IN THE FWD CARGO BAY. INSTALLED THE RETAINER IAW SOPM 20-50-12.Dec 3, 2025 · N241WN · Boeing 7377H4SDR ASAA2025120363503Door Frame · crackedMAIN CARGO DECK DOOR, FRAME FORWARD OF LATCH ACTUATOR CRACKED AT TORQUE TUBE BEARING MOUNT HOLE. GROUNDED - YES. REMOVED AND REPLACED FRAME IAW ASA EA #700-52EA-29710, FOR WORK ACCOMPLISHED SEE MG-5 N/R 1023675 Z/I 5000-0041.Dec 3, 2025 · N627AS · Boeing 737790SDR VNAA202512020004Beam · chafedR/H LOWER I/B LATCH BEAM BOTTOM SURFACE HAS SERVAL CHAFES. : CN624-0104-001 HINGE BEAMDec 3, 2025 · N515AE · Cndair CL6002C10SDR SWAA2025122942023Stub Frame · crackedCRACK FOUND ON THE R1 DOOR STUB FRAME, BS 291+ 8, WL 206+57, APPROX 0.1 INCH ABOVE SEAL DEPRESSOR. L: .3 INCH. REMOVED THE DAMAGED STUB FRAME, LOCATED, DRILLED, AND INSTALLED A NEW STUB FRAME IAW SRM 51-40-05-0G-0, 51-40-02-0G-0, AND DWG 141A8370, REV D.Dec 2, 2025 · N943WN · Boeing 7377H4SDR SWAA2025122342090Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN BS 663 - 675 IN THE MAIN WHEEL WELL. CRACK LENGTH: 0.186 INCH. REPAIRED HORIZONTAL PRESSURE DECK WEB AT LBL 60 - LBL 45.75, BS 663 - 675 IN THE MAIN WHEEL WELL IAW SRM 52-40-51-2R-A, REPDec 2, 2025 · N469WN · Boeing 7377H4SDR SWAA2025122941324Angle · crackedCRACK FOUND ON BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 9. CUT OUT AND REMOVED CRACKED PORTION OF VAPOR BARRIER ANGLE PER SRM 57-10-10-2R-5. COMPLIED WITH OPEN HOLE INSPECTION FOR REMOVED ATTACH ANGLE IAW NDT MANUAL, PART 6, 51-00-00, PROC 16. NO FAULDec 1, 2025 · N8511K · Boeing 7378H4SDR SWIA2025113076466Window Post · crackedCOCKPIT PILOT WINDOW SIDEPOST POSSIBLE CRACK AT TOP AFT, REMOVED LT WINDSHIELD POST IAW SRM 51-42-21-001-001-A01. INSTALLED NEW LT WINDSHIELD POST. IAW SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV. F. LEAK CHECKED GOOD. COMPLIED WITH SKYWEST TASK CARD 51-Nov 30, 2025 · N813SK · Cndair CL6002D24SDR SWAA2026010948328Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, LBL 30, BS 663. PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB, BS 663.75 - 675, LBL 25 - 60 IN THE MAIN WHEEL WELL IAW SRM 53-40-51-2R-2, REPAIR 2, STEP 4.Nov 30, 2025 · N241WN · Boeing 7377H4SDR SWAA2026010740916Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN. CRACK LENGTH 0.200 INCH.Nov 30, 2025 · N241WN · Boeing 7377H4SDR YENA2025120201167Door Actuator · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE A FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.077 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-90-00. PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE ANov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201166Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE 7 FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.107 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201165Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE D FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.101 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201164Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE B FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.081 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201163Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE C FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.102 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201162Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201161Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201160Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 E/A) (CRACK INDICATION FOUND OPEN HOLE B FR16 LH DOUBLE JOGGLE AREA) PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE AT HOLE B FR16 LH DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012.Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201157Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LT SIDE DOOR STOP 7 LOWER OUTBOARD HOLE AT 12 OCLOCK, CRACK LENGTH 0.078 INCH APROX; PERFORMED PERMANENT REPAIR OUTBOARD HOLE ON FR 16 LH SIDE DOOR STOP 7 LOWER IAW SRM 53-11-12-300-010 AND DWG D531354Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201156Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOU ND CONTINUITY FITTING WINDSHIELD RH SIDE.. CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTERNov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201155Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST, LOWER ATTACHMENT ARE A, INBOARD LOWER RADIUS LH SIDE, CRACK LONGITUDINAL DIRECTION, LENGTH= 0.120 INCHES APPROX; PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER POSTNov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201149Window Post · crackedDURING HEAVY MAINTENANCE: NOSE FWD FUSELAGE WINDSHIELD FRAME, CENTER POST LOWER NODE AREA CONTINUITY FITTING RT & LT SIDE CRACKED.Nov 30, 2025 · N585JB · Airbus A320232SDR YENA2025120201148Pressure Panel · crackedDURING HEAVY MAINTENANCE: CENTER FUSELAGE, FR 36 LT SIDE PRESSURE PANEL, HOLES #6, 7, 15 & 20 / CRACKED.Nov 30, 2025 · N585JB · Airbus A320232SDR VNAA202511290038Crossbeam · elongatedSEVERAL ELONGATE HOLES ON ANGLE LOWER SPLICE OF CROSS BEAM FS280. ANGLE LOWER SPLICE OF CROSS BEAM FS280.00 WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01Nov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290036Crossbeam · corrodedCORROSION ON RH CROSSBEAM AT FS280.00 WAS FOUND AT CPAX FLOOR STRUCTURE. RT CROSSBEAM AT FS280.00 WAS FOUND AT CPAX FLOOR STRUCTURE WAS EVALUATED THEREFORE IS OUT LIMITS PER CRJ-700 SRM 53-21-43-101-001-A03 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, SNov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290035Crossbeam · corrodedCORROSION ON LH CROSSBEAM AT FS280.00 WAS FOUND AT CPAX FLOOR STRUCTURE. CORROSION ON LH CROSSBEAM AT FS280.00 WAS FOUND AT CPAX FLOOR STRUCTURE WAS EVALUATED EXCESSIVE CORROSION PER CRJ-700 SRM 53-00-00-101- 001-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-00Nov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290021Crossbeam · corrodedCORROSION ON CROSSBEAM FS333 LBL24 AT PAX CABIN. CORROSION ON CROSSBEAM FS333 LBL24 AT PAX CABIN WAS REPAIRED PER REO 670-53-21-2728 REV - -.Nov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290016Post · corrodedCORROSION ON BULKHEAD FS280 LOWER POSTS; ON LBL11 ON POST AND ON PREVIOUS REPAIR ALSO ON RBL11 ON POST AT PASSENGER COMPARTMENT. CORROSION WAS REMOVED ON BULKHEAD FS280 LOWER POST RBL11 PER CRJ-700 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN OF LIMITS PER CNov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290010Door Frame · corrodedCORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01Nov 30, 2025 · N537EA · Cndair CL6002C10SDR IXXA20251130002Failsafe · corrodedFLC DOOR CUTOUT STA 566 CORROSION AT FAILSAFE STRAP AND INNER CHORDNov 30, 2025 · N479AZ · Boeing 767300SDR HNAA2026012100034Gusset · corrodedCORROSION ON LH NR 1 BEAM GUSSET. R & R L/H # 1 BEAM GUSSET IAW EMB-145 SRM 51-40-02Nov 29, 2025 · N690AE · Emb EMB145LRSDR HNAA2026012100032Door Sill · corrodedCORROSION ON SERVICE DOOR CUT-OUT FWD SILL. R & R THE SERVICE DOOR CUTOUT FWD SILL IAW EMB 145 SRM 51-40-02.Nov 29, 2025 · N690AE · Emb EMB145LRSDR HNAA2026012100027Structure · corrodedLAV WASTE BUCKET IS CORRODED AT AFT OF THE WASTE DRAIN VALVE. REMOVED AND REPLACED LAV WASTE BUCKET IAW EMB 145 SRM 51-40-02.Nov 29, 2025 · N690AE · Emb EMB145LRSDR SWIA20251222129Fitting · wornALL EMERGENCY EVAC SLIDE FLOOR FITTING HARDWARE WORN AND/OR CORRODED (C-CHECK RO 12/19/2025)REMOVED AND REPLACED ALL EMERGENCY EVACUATION SLIDE FITTING HARDWARE PER ERJ 175 AMM 53-23-25. REF CONTINUATION CARD FOR WORK PERFORMED.Nov 29, 2025 · N132SY · Emb ERJ170200LRSDR AALA202603172307Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: INTERIM REPAIR ON ASSOCIATED HOLES N5, B AND D LOCATED ON FRAME 16 RH DOUBLE JOGGLE AREA AT DOOR STOP FITTING N7 LVL ON UPPER FUSELAGE. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON FR 16 RH DOUBLE JOGGLE AREA PARTIAL FRAME REPLNov 28, 2025 · N830AW · Airbus A319132SDR SWAA2025123040480Tie Clip · crackedCRACKED TIE CLIP, FWD FACE BS 500I, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A.Nov 28, 2025 · N8624J · Boeing 7378H4SDR SWAA2025122946834Tie Clip · crackedCRACKED TIE CLIP, BS 500I, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A.Nov 28, 2025 · N8624J · Boeing 7378H4SDR AALA202512021382Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 4 AT Y0. REPLACED CONTINUITY FITTING PER EA 355317.Nov 28, 2025 · N668AW · Airbus A320232SDR CALA2025120211640Crease Beam · corroded(SDR) MAIN DECK RH SIDE CREASE BEAM BETWEEN STA 1290 AND STA 140 0 HAS CORROSION EXFOLIATED. ESFR ENTRY CREASE BEAM WAS EXFOLIATED REMOVE DAMAGE CREASE BEAM IAW SRM 51- 40-02, FABRICATED NEW CREASE BEAM, TRAVELER:T25/1841659, LOCATED AND DRILLED IAW SRM 51-40-Nov 28, 2025 · N77865 · Boeing 75733NSDR REXA2026052700768Door Sill · crackedCRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR WAS REPLACED PER EA NO. CRJ953-21058 REV . IR, CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01Nov 27, 2025 · N921XJ · Cndair CL6002D24SDR SWAA2025123040382Tie Clip · crackedCRACKED TIE CLIP FWD FACE BS 500I, STR 26R AT FWD CARGO BAY. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A.Nov 27, 2025 · N8624J · Boeing 7378H4SDR SWAA2025121940241Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, LBL 30, BS 663. CRACK LENGTH: 0.437 INCH. REPAIRED PAX CABIN PRESSURE DECK, BTW BS 663.75 & 675, LBL 20 & 60 IAW EA 25-153-03322-WIP1, & EA 25-153-03322.Nov 27, 2025 · N459WN · Boeing 7377H4SDR SWAA2025121748007Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41, BS 663 IN THE PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2 REPAIR 2.Nov 27, 2025 · N459WN · Boeing 7377H4SDR SWAA2025121740240Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41, BS 663 IN PASSENGER CABIN. PERFORMED A PERMANENT REPAIR ON THE HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2.Nov 27, 2025 · N459WN · Boeing 7377H4SDR SWIA202602274474Buttstrap · corrodedCORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (C-CHECK RO 02/25/2026)CHAFFING UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00 BLEND-OU AND FOUND WITHIN LIMITS IAW MHICRJ700 SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IANov 26, 2025 · N609SK · Cndair CL6002C10
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