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.

SDR YENA2025011600059Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER OUTB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 LH. CRACK DIRECTION 10 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00038) REF AE WO 2024-413/1.N/R# 2024 - 749228. PERFORMEJan 15, 2025 · N505JB · Airbus A320232SDR YENA2025011600058Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON UPPER INB FASTENER HOLE OF DOOR STOP FITTING Ñ7 AREA FR 66 RH. CRACK DIRECTION 5 AND 11 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00039) REF AE WO 2024-413/1. N/R# 2024 - 749229. PEJan 15, 2025 · N505JB · Airbus A320232SDR YENA2025011600057Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00040) REF AE WO 2024-413/1. N/R# 2024 - 749231. PEJan 15, 2025 · N505JB · Airbus A320232SDR YENA2025011600056Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER OUTB FASTENER HOLE OF DOOR STOP FITTIN G Ñ1 AREA FR 68 LH. CRACK DIRECTION 10 OCLOCK. CRACK D= 0.170 INCH.(THIS TASK CARD IS GENERATED FOR PURPOSES TRACKING AREA 4); (RESOLVED ON W/O: 1347560 TASKCARD: Jan 15, 2025 · N505JB · Airbus A320232SDR YENA2025011600055Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 OCLOCK. CRACK D= 0.170 INC H.(THIS TASK CARD IS GENERATED FOR PORPUSES TRACKING AREA 2); (RESOLVED ON W/O: 1347560 TASKCJan 15, 2025 · N505JB · Airbus A320232SDR YENA2025011600054Stop Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 OCLOCK. CRACK D= 0.170 INC H. (THIS TASK CARD IS GENERATED FOR PORPUSES TRACKING AREA 4); (RESOLVED ON W/O: 1347560 TASKJan 15, 2025 · N505JB · Airbus A320232SDR DALA2025011600392Crossbeam · bentSHIP 3147 BENT INTERNAL STRUCTURE CROSS BEAM LOCATED FR27 AND FROM STR41R TO STR38L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED NEW CROSS BEAM AND NEW FASTENERS AS PER A319 SRM51-42-11 AND A319 SRM 51-72-11. (0763031)Jan 15, 2025 · N347NB · Airbus A319114SDR VNAA20250115019Window Frame · gougedCO-PILOT WINDSHIELD LOWER LANDING IS GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED DAMAGED AREA IAW MHIRJ REO 670-53-11-2032 REV. -- DATED 2024-10-10Jan 15, 2025 · N709PS · Cndair CL6002C10SDR VNAA20250115018Window Frame · gougedPILOT WINDSHIELD LOWER LANDING IS GOUGED IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED DAMAGED AREA IAW MHIRJ REO 670-53-11-2032 REV. -- DATED 2024-10-10.Jan 15, 2025 · N709PS · Cndair CL6002C10SDR VNAA20250115017Plate · gougedAFT FUSELAGE PROTECTION PLATE AT FS 977.00 NOT IN PLACE. FUSELAGE GOUGED. 2 FASTNERS REQUIRE REMOVAL. CORRECTIVE ACTION: REPAIRED IAW BOMBARDIER REO 670-53-00-290 REV -F, DATED 2019/04/26, SOLUTION 2 (CRJ-700)Jan 15, 2025 · N709PS · Cndair CL6002C10SDR IPXA2025050588745Failsafe · damagedCUT OUT DAMAGED SECTION OF LOWER TEE CHORD ON FRAME AT STA 1439 PART REPLACED ON REM-13.Jan 14, 2025 · N324UP · Boeing 76734AFSDR IPXA2025050588761Failsafe · damagedCUT OU DAMAGED SECTION OF TEE CHORD FROM FRAME AT STA 1461 PART REPLACED ON BOEING REPAIR DOC REM-14 (ATTACHED). ENTIRE BOEING WORK PACKAGE ATTACHED TO LINE ITEM 103. (PLEASE SEE BARCODE T3F18E005W6PJ - NLL 0782896)Jan 14, 2025 · N324UP · Boeing 76734AFSDR AALA202502035745Stop Fitting · gougedAIRCRAFT IN BASE MAINTENANCE: AFT ENTRY DOOR FORWARD FRAME-MOUNTED UPPER STOP FITTING HAS A GOUGE ON FORWARD SIDE. BLENDED AND REMOVED GOUGE IN UPPER FORWARD STOP FITTING. PER B737-NG-SRM 51-10-02. AFTER BLENDING BUSHING FOUND TO BE WITHIN LIMITS. PER B737-NGJan 14, 2025 · N987NN · Boeing 737823SDR CALA2025011500127Door Frame · crackedDURING NDT INSPECTION PER EA 5310-07694 REV C FOUND CRACK FRAME AT R1 DOOR FWD CUTOUT.Jan 14, 2025 · N18223 · Boeing 737824SDR CALA2025011500125Door Frame · crackedL-1 DOOR CUTOUT CRACK UPPER CHORD AT STA 312, BETWEEN S-5L AND S-6L. ACCOMPLISHED REPAIR AT STA 312 STR 5L-6L IAW B737-800 SRM 53-10-07-2R-1.Jan 14, 2025 · N26232 · Boeing 737824SDR EE4Y2025011421552Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-003-P1-OP-UP-UF-NDT/003, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR68 LH STOP FITTING #1, LOWER OUTBOARD HOLE WITHCRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-010 Jan 14, 2025 · N274NV · Airbus A320214SDR EE4Y2025011421551Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-002-P1-OP-UP-UF-NDT/003, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH STOP FITTING #1, LOWER INBOARD HOLE WITH CRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-010 Jan 14, 2025 · N274NV · Airbus A320214SDR EE4Y2025011421550Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-002-P1-OP-UP-UF-NDT/002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH STOP FITTING #2, UPPER OUTBOARD HOLE WITH CRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-010Jan 14, 2025 · N274NV · Airbus A320214SDR EE4Y2025011421549Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-003-P1-OP-UP-UF-NDT/002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR68 LH STOP FITTING #1, UPPER OUTBOARD HOLE WITH CRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-011Jan 14, 2025 · N274NV · Airbus A320214SDR EE4Y2025011421548Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-003-P1-OP-UP-UF-NDT/001, UPPERFUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR68 LH STOP FITTING #7, UPPER INBOARD HOLE WITHCRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-010 PAJan 14, 2025 · N274NV · Airbus A320214SDR EE4Y2025011421547Stop Fitting · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK CARD A32X-53-260-002-P1-OP-UP-UF-NDT/001, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH STOP FITTING #7, UPPER INBOARD HOLE WITH CRACK INDICATION. PERMANENT REPAIR WAS PERFORMED IAW A320 SRM TASK 53-41-12-300-010 Jan 14, 2025 · N274NV · Airbus A320214SDR SWAA2025021985451Receiver · crackedDOT#38 A-043 FWD CARGO COMPARTMENT AFT BKHD UPPER STAINTION RAIL CAMLOCK RECIVER CRACKED STA 500D LBL 39 WL 193<[01] REMOVED AND REPLACED CAMLOCK AT AFT BULKHEAD UPPER RAIL IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/WJan 13, 2025 · N7723E · Boeing 73776NSDR 9WGA20250205037Pressure Deck · erodedEVIDENCE OF CORROSION STA 1240 ON THE RH CANTED PRESSURE DECK AREA ON THE OUTBOARD WALL.Jan 13, 2025 · N344KD · Boeing 747446SDR CALA2025011400114Window Frame · crackedL/H WINDSHIELD FRAME I/B HOLE HAS A CRACK INDICATION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9296891/20891 GEN BY V061632Jan 13, 2025 · N829UA · Airbus A319131SDR DALA2025011400317Window Frame · crackedSHIP NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH & RH CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 622157-14AD. (0759856)Jan 13, 2025 · N347NB · Airbus A319114SDR DALA2025011400316Window Frame · crackedSHIP 3147 CRACK INDICATIONS WERE FOUND AT LHS (CENTER POST, LOWER RADIUS), RHS (CENTER POST, LOWER RADIUS AND LOWER NODE CONTINUITY FITTING), FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: REPAIRED PER ERA 622157-14AD. (0759601)Jan 13, 2025 · N347NB · Airbus A319114SDR DALA2025011400315Window Frame · crackedSHIP 3147 CRACK INDICATIONS WERE FOUND AT LHS, RHS, FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: REPAIRED PER ERA 622156-14AD. (0759348)Jan 13, 2025 · N347NB · Airbus A319114SDR WRXR202500113001Mount · crackedHAIRLINE CRACK MEASURING .55'' WAS FOUND IN THE RADIUS OF THE STRUCTURE FOR THE SPR. FABRICATED REPAIR ANGLE -1 MAKE FROM ALUM ALLOY 2024 T3 .050 LOT# 44682B7/1.16. LOCATED AND DRILLED NEW FABRICATED ANGLE -1 IAW REO 670-28-25-013 REV. --. INSTALLED NEW ANGLE:Jan 13, 2025 · N540EG · Cndair CL6002C10SDR SWIA20250218112Support · corrodedAFT WET AREA RH BEAM BETWEEN FRAMES 86-87 HAS CORROSION AROUND FASTENER HOLE. (C-CHECK RO 2/15/2025) REMOVED AND REPLACED RH FR 86-87 BEAM WITH NEW REF. ERJ175 SRM 51-40-08. REPLACED WITH OEM PART NO CHANGE IN WEIGHT AND BALANCE. SEE CONTINUATION CARD FJan 12, 2025 · N614CZ · Emb ERJ170200LRSDR REXA2025021100187Lug · crackedL/H FWD EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV- DATED 2024-11-06Jan 12, 2025 · N936XJ · Cndair CL6002D24SDR REXA2025021100186Lug · crackedR/H AFT EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV0 DATED 2024-11-06Jan 12, 2025 · N936XJ · Cndair CL6002D24SDR REXA2025021100184Lug · crackedR/H FWD EMERGENCY EXIT DOOR AFT UPPER LUG IS CRACKED. REPAIRED IAW MHIRJ REO 670-52-21-103 REV-- DATED 2024-11-06Jan 12, 2025 · N936XJ · Cndair CL6002D24SDR AALA202501130534Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK CROSS BEAM CONNECTION LOCATED AT FR 68 BETWEEN STR 22L TO STR 23L AT AFT GALLEY AREA, REPLACED CROSSBEAM SECTION CONNECTION PER SRM 51-72-11-911-001.Jan 12, 2025 · N163US · Airbus A321211SDR AALA202501139112Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON CROSSBEAM SECTION CONNECTION LOCATED AT FR 66 BETWEEN STR 22L AND 23L IN AFT GALLEY AREA. REPLACED CROSSBEAM SECTION CONNECTION PER SRM 51-42-11-801.Jan 12, 2025 · N163US · Airbus A321211SDR AALA202501136868Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED ON FRAME 68 IN THE PASSENGER CABIN. PERFORMED REPAIR ON LOWER SILL PER SRM 53-41-14-300-001.Jan 12, 2025 · N163US · Airbus A321211SDR IPXA2025021143679Support · crackedR/H A/C BAY DOOR CTR WEB SUPPORT IS CRACKED (114-49) ATA 53-10. INSTALLED INTERCOSTAL ON R/H A/C BAY DOOR IAW MD11 SRM 51-35-01.Jan 11, 2025 · N255UP · Doug MD11FSDR IPXA2025020444461Bracket · crackedFS 900 LBL12 BRACKET THAT ATTACHES TO INTERCOSTAL TO 900 T-CHORD IS CRACKED INSTALLED NEW BRACKET ON STR FS 900 LBL12 IAW SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APFSDR ASAA2025011155645Strap · corrodedAFT CARGO DOOR CUTOUT HAS CORROSION AROUND SCREW HOLES,AND OTHER SPOTS ON FLOOR STRUCTURE BEHIND THE SILL WEB PANEL. CIRCLED IN RED. GROUNDED - YES. AFTER FURTHER EVALUATION, CORROSION FOUND ON PREVIOUS REPAIR. NO ALLOWABLE DAMAGE LIMITS FOUND. REMOVED ADDITIOJan 11, 2025 · N514AS · Boeing 737890SDR SCNA20250114011Stop Fitting · unsecureOVERWING EMERGENCY EXIT DOORS (ALL). ALL DOOR STOPS ON FRAMES ARE NOT SECURED.VERIFICATION OF PROPER INSTALLATION REQUIRED. RESOLUTION: (IN PROGRESS)Jan 11, 2025 · N5209A · Boeing 73783NSDR CALA2025011300098Window Post · cracked(SUPPORT TASK) CRACK DETECTED AT R/H #3 WINDOW POST 4TH LOWER CORNER FASTENER HOLE AFTER BEING REAMED TO PRE-COLD WORK DIAMETER PER EA 5310-08195 REV ''A''. REF 3499219 AND 3499177 REPAIRED R/H #3 WINDOW POST 4TH LOWER CORNER FASTENER HOLE PER UAL ECRA 5310Jan 11, 2025 · N14230 · Boeing 737824SDR SWIA202503170110Landing · crackedRH SIDE TRU BAY DOOR LOWER LANDING HAS A CRACK ON AFT LATCH CUT OUT (C-CHECK RO 3/14/2025) REMOVED AND REPLACED TRU LOWER LANDING WITH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, 51-42-22-001-001-A01 , REO- 670-53-11-2086 REV -- DATE 2025-01-16. (Jan 10, 2025 · N751EV · Cndair CL6002C10SDR AALA202503139400Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON OPEN FASTENER HOLE JUNCTION WINDSHIELD RH LATERAL POST. CRACK DEPTH: D1-D2=0.302 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ( REPLACED RH LATERAL WINDOW FRAME) LOCATED BTW FR 4 TO FR 8 AT LEVEL -Y765 IAW EA #Jan 10, 2025 · N753US · Airbus A319112SDR SWIA20250311110Track · damagedFOUND TOP OF AFT CARGO DOOR TRACK AT FS621.00 TO BE DAMAGED (FILED CLOSED) REMOVED AND REPLACED AFT CARGO DOOR TRACK AT FS621.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH THE ENTIRE STACJan 10, 2025 · N856AS · Cndair CL6002B19SDR DALA2025011000220Door Frame · crackedSHIP 3319 AFT CARGO DOOR LOWER FRAME FORK CRACK AT FR61. CORRECTIVE ACTION: REPLACED WITH NEW FRAME FORK PER ER/A 623371-14AD REV ORIGINAL PRI REV 0. (0754169)Jan 10, 2025 · N819NW · Airbus A330323SDR DALA2025011000219Door Frame · crackedSHIP 3319 AFT CARGO DOOR LOWER FRAME FORK CRACK AT FR61A. CORRECTIVE ACTION: COMPLIED WITH THE ER/A 623371-14AD REV ORIGINAL SECTION I. (0754162)Jan 10, 2025 · N819NW · Airbus A330323SDR FDEA202501100052Skin · cracked02 EACH FASTENER HOLES (#14 AND #15) FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.400 AND STATION XORS=713.600. REPAIR CARRIED OUT AT RIGHT HAND WINJan 10, 2025 · N607FE · Doug MD11FSDR SWIA2025031900109Door Frame · crackedRH OVERWING FWD EMER DOOR HAS POSSIBLE CRACK ON TOP FRAME. MARKED (C-CHECK RO 3/18/2025) REPAIRED RH OVERWING EMERGENCY EXIT DOOR PER MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 ALL STEPS COMPLIED WITH, SEE CONTINUATION FOR WORK PERFORMED. COMPLIED Jan 9, 2025 · N554CA · Cndair CL6002D24SDR SWIA20250311109Structure · crackedTHERE IS A CRACK ON WINGBOX (MARKED IN) INTERIOR @ FS 461 (FILED CLOSED) COMPLIED WITH REO 601R-53-41-3284 FOR REPAIR OF AREA DOUBLERS FABRICATED FROM 2024 T-3 .050 AND 2024 T-3 .040. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHEDJan 9, 2025 · N448SW · Cndair CL6002B19SDR SWIA20250303109Structure · crackedTHERE IS A CRACK ON WINGBOX (MARKED IN) INTERIOR @ FS 461 (FILED OPEN) COMPLIED WITH REO 601R-53-41-3284 FOR REPAIR OF AREA DOUBLERS FABRICATED FROM 2024 T-3 .050 AND 2024 T-3 .040. TASK CARD 51-900-1003-SKY COMPLETED, M-337 ATTACHEDJan 9, 2025 · N448SW · Cndair CL6002B19SDR SWAA2025022084613Crease Beam · corrodedCABIN FWD WET AREA R1 CREASE BEAM CRRODED AT STA 312+15' LBL 60 WL 208<[01] REMOVED DAMAGE FROM CABIN FWD WET AREA R1 CREASE BEAM CORRODED AT STA 312+15' LBL 60 WL 208; FOUND IT OUT OF LIMITS ; ORIG T . ADJACENT TO BLEND .085'; LOSS .017'; REMOVED DAMAGED PARTJan 9, 2025 · N7723E · Boeing 73776N
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