JASC 5311

Service difficulty reports · 61,540

Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311'
  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 HNAA2024072900632Frame · cracked53-2326 LH COCKPIT OVERHEAD FRAME CRACKED. REAIRED IAW EO1-53-24-0392Jun 21, 2024 · N662EH · Emb EMB145LRSDR SWAA2024072304295Frame · crackedFWD GALLEY DOORWAY; BS 294.5 STR 17R FWD SUB-FRAME CRACKED AT THE IB FASTENER HOLE; MARKED.<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; .400' CRACK NOTED. MARKED DIRECTION.<BR><BR>EQUIP ID ATS2353 DUE 01/25;[02] REMOVED AND REPLACEDJun 21, 2024 · N252WN · Boeing 7377H4SDR AALA202406279890Frame · out of toleranceAIRCRAFT IN BASE MAINTENANCE: OVERSIZE FASTENER HOLES IN AFT CARGO COMPARTMENT DOOR OPENING FORWARD FRAME AT STA 787 PLUS 5 INCHES, BETWEEN S21R AND S23R. REPAIRED FRAME PER EA 354789.Jun 21, 2024 · N947AN · Boeing 737823SDR DALA2024062506502Frame · crackedRIGHT FUSELAGE FRAME BS 1640 CRACKED. ER/A 569586-14AD SECTION III IS ISSUED FOR GAP BETWEEN SKIN & LOWER HINGE INTERCOSTAL BS 1620 TO BS 1635. CURRENT REVISION IS B. REF ERA 569586-14.Jun 21, 2024 · N664DN · Boeing 757232SDR DALA2024062406409Frame · corrodedCORROSION ON FRAME WEB 1160 BTW S-16L AND S- 17L IN PAX CABIN. PERMANENT REPAIR ON FRAME WEB 1160 BTW S-16L AND S-17L IN PAX CABIN WAS PERFORMED PER PRI NO.618609-14. REV.1. AND ER/A NO.618609-14, REV.ORIGINAL , SECTION I.Jun 21, 2024 · N684DA · Boeing 757232SDR DALA2024062406339Frame · crackedA.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF NRC 00508: OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B AND B717-200 SRM 51-41-Jun 21, 2024 · N930AT · Boeing 717200SDR SWI2024F01134Frame · corrodedFRAME 265.0 / LH STGR 26 TO RH STGR 26 IS CORRODED FLAGGED S/N:0659 (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED AND REPLACED STIFFENING ANGLE ON FRAME FS265 P/N CC670-34104-1 REF DWG CC670-34020 REV. B. AND DWG CC670-33025 REV. D REF. CRJ 700 SRM 51-42-06-0Jun 20, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00978Frame · corrodedFRAME 265.0 / LH STGR 26 TO RH STGR 26 IS CORRODED FLAGGED S/N:0659 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED AND REPLACED STIFFENING ANGLE ON FRAME FS265 P/N CC670-34104-1 REF DWG CC670-34020 REV. B. AND DWG CC670-33025 REV. D REF. CRJ 700 SRM 51-42-06-001Jun 20, 2024 · N752EV · Cndair CL6002C10SDR VNAA20240726015Frame · corrodedCORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUTED WITHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01Jun 20, 2024 · N585NN · Bombdr CL6002D15SDR DALA2024062406389Frame · cracked(LOG 0405705) FOUND CRACK AT R/H FRAME STA 867 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406388Frame · cracked(LOG 0405702) FOUND CRACK AT R/H FRAME STA 787 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406387Frame · cracked(LOG 0405698) FOUND CRACK AT R/H FRAME STA 727B AT A/C RAIL. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406386Frame · cracked(LOG 0405697) FOUND CRACK AT R/H FRAME STA 500F AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406385Frame · cracked(LOG 0405693) FOUND CRACK AT R/H FRAME STA 500D AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406384Frame · cracked(LOG 0405688) FOUND CRACK AT R/H FRAME STA 500C AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02B.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406383Frame · cracked(LOG 0405678) FOUND CRACK AT L/H FRAME STA 867 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406382Frame · cracked(LOG 0405668) FOUND CRACK AT L/H FRAME STA 827 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406381Frame · cracked(LOG 0405666) FOUND CRACK AT L/H FRAME STA 727D AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406380Frame · cracked(LOG 0405665) FOUND CRACK AT L/H FRAME STA 727B AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406379Frame · cracked(LOG 0405658) FOUND CRACK AT L/H FRAME STA 500D AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406378Frame · cracked(LOG 0405656) FOUND CRACK AT L/H FRAME STA 500A AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406377Frame · cracked(LOG 0405652) FOUND CRACK AT L/H FRAME STA 480 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406376Frame · cracked(LOG 0405648) FOUND CRACK AT L/H FRAME STA 440 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR DALA2024062406375Frame · cracked(LOG 0405642) FOUND CRACK AT L/H FRAME STA 380 AT A/C RAIL BRACKET. REPAIRED PER WORK CARD 2526-01236-02A.Jun 20, 2024 · N394DA · Boeing 737832SDR UIEA2024061800546Frame · crackedCRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE.(<P>CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE. WAS REPAIRED IAW TRE6753695 ISSUED DATE JUN 08/2024, FVCI CONTROL# 24088-Jun 20, 2024 · N1229A · Boeing 767306SDR DALA2024062106328Frame · crackedSHIP 3161 WHILE ACCOMPLISHMENT OF JIC 5311-01246-02B REGARDING THE FR20RH DOUBLE JOGGLE INSPECTION, A CRACK INDICATION WAS FOUND AFFECTING HOLE #5. CORRECTIVE ACTION: REPAIRED PER ERA 618180-14AD. (0404585)Jun 20, 2024 · N361NB · Airbus A319114SDR DALA2024062106327Frame · crackedSHIP 3161 WHILE ACCOMPLISHMENT OF JIC 5311-01246-01B REGARDING THE FR16RH DOUBLE JOGGLE INSPECTION A CRACK INDICATION WAS FOUND AFFECTING HOLE #6. CORRECTIVE ACTION: REPAIRED PER ERA 618587-14AD (0404492)Jun 20, 2024 · N361NB · Airbus A319114SDR DALA2024062106314Frame · dentedSHIP 684 DENTS ON FRAME STA. 1580 ABOVE S-26R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00437. FRAME STA. 1580 ABOVE S-26R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53-00-07-2R PROCEDURE 5. (0404406)Jun 20, 2024 · N684DA · Boeing 757232SDR AALA202406218520Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: FASTENER HOLE IN CARGO DOOR FRAME MISDRILLED WITH CORROSION AT BS 797. INSTALL FREEZE PLUG FOR MISDRILLED HOLE. PER FINAL EA 354813.Jun 20, 2024 · N942AN · Boeing 737823SDR DALA2024062006270Frame · crackedCRACK ON MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN. SUMMARY OF NRC 00441: MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4, PAR 5A. (LP #0402943)Jun 20, 2024 · N965AT · Boeing 717200SDR VNAA20240726011Frame · corrodedCORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH. CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED WITHIN LIMITS PER CRJ900 SRM Jun 19, 2024 · N585NN · Bombdr CL6002D15SDR CALA2024070201953Frame · crackedCRACK INDICATION NOTED AT RH FR20 DOOR STOP FITTING #1, HOLE #3 WHILE ACCOMP''G INSP IAW EA5311-02164 (B), AT BFM HMV ON N/R 93794. 1.6 AS FOLLOWS: RH FR20 DOOR STOP FITTING #1, HOLE #3 WAS REP''D ER PART 2 OF LATEST REVISION OF ECRA5311-03231 ON/BEFORE ACFT RJun 19, 2024 · N897UA · Airbus A319132SDR CALA2024062101878Frame · corrodedDURING C-CK IN ILN (WILMINGTON, OH) AMES MAINTENANCE FOUND THE L WR CHORD CORRODED LOCATED AT STA 1809.5 BULKHEAD FRAME INSTALLATION(P/N-148T1150-1). CORROSION WAS COMMON TO THE VERTICAL & HORIZONTAL FLANGE AS SHOWN IN FIGURES. DAMAGE WAS RE MOVED BY BLENDING Jun 19, 2024 · N651UA · Boeing 767322SDR VNA2024F00008Frame · cracked6EA. MISDRILLED HOLES TO FUSELAGE STRUCTURE, FRAME SECTOR (DWG CC670-34203, 7475-T7351, 0.063" NOM THK, REF), POST FS193.00 (DWG CC670-32133, 7475-T7351 AL ALY, 0.060" NOM THK, REF) AND BOX EXTERNAL POWER PROVISIONS AFT FLANGE (DWG CC670-33401, 2024-T42 AL ALYJun 19, 2024 · N533AE · Cndair CL6002C10SDR JJBA20240808008Frame · corrodedUPON REMOVAL OF BAGGAGE DOOR PROTECTOR STRIP, FOUND CORROSION ON FRAME 66 DIRECTLY UNDER REMOVED PROTECTOR STRIP AREA. REMOVED AND REPLACED BAGGAGE DOOR SILL. APPLIED TOP COAT TO BAGGAGE DOOR SILL.Jun 18, 2024 · N17196 · Emb EMB145XRSDR DALA2024062106310Frame · dentedSHIP 6806 DENTS ON FRAME STA. 540, BTW S-24L TO S-26L AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00802: FRAME STA. 540, BTW S-24L TO S-26L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 618543-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (040Jun 18, 2024 · N709TW · Boeing 7572Q8SDR DALA2024061906239Frame · dentedSHIP 6806 AMOC, ERA 618543-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 540, BETWEEN S-24L & S-25L WAS FOUND DENTED. CORRECTIVE ACTION:REF ERA 618543-14. (0399211)Jun 18, 2024 · N709TW · Boeing 7572Q8SDR SWAA2024071802720Stub Frame · crackedCRACK ON STUB FRAME LOC. AT LEVEL STR-7R TO STR-9R FWD SERVICE DOOR SIDE AT FWD GALLEY AREA 2024-393320<[01] REPLACED STUB FRAME LOC. AT LEVEL STR-7R TO STR-9R FWD SERVICE DOOR SIDE AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02 AND DWG-141A8370 REV: D SEE INDIVJun 17, 2024 · N251WN · Boeing 7377H4SDR DALA2024061806166Frame · corrodedSHIP 3138 CORROSION WEB FRAME 20 AT LEVEL STR 23R AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOC. FRAME 20 AT LEVEL STR 23R AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0398581)Jun 17, 2024 · N338NB · Airbus A319114SDR DU4R2024061700024Frame · crackedDURING SCHEDULED INSPECTION/MAINTENANCE AT HAECO, LAKE CITY, FOUND R/H FR 16 DOUBLE JOGGLE UPPER HOLE #5 IS LARGER THAN REPORTED AFTER BUSHING REMOVAL. S/O 194150 NR01362425 HAECO 26682Jun 17, 2024 · N215NV · Airbus A320214SDR SWI2024F01091Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED ON AFT SIDE, LOCATED AT FS879.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)EVALUATED CORROSION ON FRAME AT FS879.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWIA202411040615Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED CLOSED)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00952Frame · corrodedREAR FUSELAGE INTERNAL STRUCTURE CORROSION ON FS1015.00 FORWARD SIDE BETWEEN STGR22L TO STGR23L AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED CORROSION ON FRAME AT FS1015.00 STGR22L-STGR23L FWD SIDE AND FOUND OUT OF LIMITS PER CRJ700SRM 53-61-06-101-0Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00949Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED ON AFT SIDE, LOCATED AT FS879.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION ON FRAME AT FS879.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A0Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00948Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND COJun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00942Frame · corrodedREAR FUSELAGE INTERNAL STRUCTURE CORROSION ON FS1015.00 FORWARD SIDE BETWEEN STGR22L TO STGR23L AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED CORROSION ON FRAME AT FS1015.00 STGR22L-STGR23L FWD SIDE AND FOUND OUT OF LIMITS PER CRJ700SRM 53-61-06-101-0Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00938Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND COJun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00927Frame · corrodedREAR FUSELAGE INTERNAL STRUCTURE CORROSION ON FS1015.00 FORWARD SIDE BETWEEN STGR22L TO STGR23L AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED CORROSION ON FRAME AT FS1015.00 STGR22L-STGR23L FWD SIDE AND FOUND OUT OF LIMITS PER CRJ700SRM 53-61-06-101-0Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00924Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED ON AFT SIDE, LOCATED AT FS879.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION ON FRAME AT FS879.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A0Jun 15, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00937Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND COJun 15, 2024 · N752EV · Cndair CL6002C10
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