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.
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
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 SWAA2024102337549Frame · crackedCRACK FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN 2024-572738<[01] PERFORMED TRIM OUT ON FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN I.A.W EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFSDR CALA2024101102627Frame · cracked(SUPPORT TASK) DURING ROTO TEST OF RH FRAME 16 HOLE 6 FOUND CRAC KED IN FRAME LAYER AT THE 3:00 POSITION. REPAIR BEFORE NEXT FLIG HT.() TRANSFERRED REPAIR INFORMATION AND DIP REQUIREMENTS TO LP''S 9509350, 9509474 & 9509861. THIS ITEM CAN BE CLEARED.SDR IPXA2024091982984Frame · dentedFAULT ZONE 100, STR: 02 EA DENTS ON FR STA 1480 AND BTW STRG 22R TO 23R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, TABLE III. VERIFIED ACCOMPLISHMENT OF REPAIR ON FR 1480, BETWEEN STR 22R-23R.SDR IPXA2024091983273Frame · dentedFAULT ZONE 100, STR: 01 EA DENTS ON FR STA 1300 AND BTW STRG 23R TO 24R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-6, DETAIL IV PER SRM 53-60-07-2R. VERIFIED ACCOMPLISHMENT OF REPAIR ON FR 1300, BETWEEN STR 23R-24SDR DALA2024091909219Frame · corroded(LOG 0563550) CORROSION ON L/H STA 767 FRAME UNDER ZEE CHANNEL ATTACH POINT. PERFORMED REPAIR B737-SRM-53-60-07-2R-2 ON FRAME BSTA 767 L/H UNDER ZEE CHANNEL, BETWEEN STRINGER 25L AND 26L.SDR DALA2024091809171Frame · corroded(LOG 0560131) CORROSION ON L/H STA 767 FRAME UNDER ZEE CHANNEL ATTACH POINT. PERFORMED REPAIR B737-SRM 53-60-07-2R-2 ON FRAME 767 L/H UNDER ZEE CHANNEL, BETWEEN STRINGER 25L AND 26L.SDR DALA2024091809170Frame · cracked(LOG 0560094) FRAME CRACKED AT BS 440, STR 8L AT INBD HOLE.REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809169Frame · cracked(LOG 0560059) FRAME CRACKED AT BS 867, STR 8L AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809168Frame · cracked(LOG 0560057) FRAME CRACKED AT BS 827, STR 8L AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809167Frame · cracked(LOG 0560050) FRAME CRACKED AT BS 727D, STR 8L AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809166Frame · cracked(LOG 0560041) FRAME CRACKED AT BS 500C, STR 8L AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT.REPAIRED PER WORK CARD 2526-01236-02A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809165Frame · cracked(LOG 0560006) FRAME CRACKED AT BS 440, STR 8L AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809164Frame · cracked(LOG 0559993) FRAME CRACKED AT BS 867 STR 8R AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091809163Frame · cracked(LOG 0559989) FRAME CRACKED AT BS 500C STR 8R AT INBD HOLE. REPAIR PRIOR TO FURTHER FLIGHT. REPAIRED PER WORK CARD 2526-01236-02B INSTRUCTIONS, REF SUPPORTING AA 2526-01236.SDR DALA2024091709104Frame · dented(LOG 0554769) DENT ON FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT. FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT WAS REPAIRED PER. B737-800 SRM 53-30-07-2R.SDR DALA2024091709103Frame · dented(LOG 0554761) DENT ON FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT. FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT WAS REPAIRED PER. B737-800 SRM 53-30-07-2R.SDR DALA2024091709102Frame · dentedLOG 0554755) DENT ON FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT. FRAME STA 500E S-25L AT FWD CARGO COMPARTMENT WAS REPAIRED PER. B737-800 SRM 53-30-07-2R.SDR DALA2024091709100Frame · dented(LOG 0553674) DENT ON FRAME STA 500B BTW S-24L AND S-25L AT FWD CARGO COMPARTMENT. FRAME STA 500B BTW S-24L AND S-25L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-30-07-2R REPAIR 1.SDR DALA2024091709099Frame · cracked(LOG 0553622) CRACK OF 1)L=0.438IN LENGTH WAS FOUND ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827 BTW S-8R & S-9R. FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024091709098Frame · cracked(LOG 0553620) CRACK OF 1)L=0.625 IN LENGTH WAS FOUND ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8R & S-9R. FUSELAGE FRAME STA 500A BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024091709097Frame · cracked(LOG 0553614) CRACKS OF 1)L=0.688IN & 2)L=0.500IN LENGTH WERE FOUND ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 480 BTW S-8R & S-9R. FUSELAGE FRAME STA 480 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024091609049Frame · crackedCRACKED FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX. SUMMARY OF NRC 00386: FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0554632)SDR SWAA2024102837069Frame · crackedCRACK FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN 2024-572213<[01] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-153-01244.;[02] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-15SDR SWAA2024102537066Stub Frame · crackedCRACK STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-572210<[01] TOOL USED ON STEP 5 AND 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] REPAIRED STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-SDR SWAA2024101636998Frame · crackedCRACKED FRAME BS 312 COMMON TO STR 6L LBL 33 WL 282.<[01] REPAIRED FRAME BS 312 COMMON TO STR 6L; LBL33; WL 282 PER EA M-22-153-01244 CUSTOMER SYSTEM ID: TTG8Q00VWUP8.;[02] VERIFIED CORRECTIVE ACTION #1SDR CALA2024092302461Stub Frame · damagedSTUB FRAME P/N 141A8370U13 AT R-1 DOOR CUT OUT UPPER FWD CORNER WAS REMOVE AND REPLACED SEE BAM NON=ROUTINE 21738 27 FOR WORK ACCOMPLISHED. THIS NON-ROUTINE WAS CREATED FOR STRUCTURAL SIGNIFICANT FINDINGS REPORT. CREATED SFR # 9236488 FOR BAM NON-ROUTINE 00217SDR DALA2024091609024Frame · dented(LOG 0553448) DENT ON FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMENT. FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMEN WAS REPAIREED PER PER B 737-800 SRM 53-30-07-2R.SDR DALA2024091609023Frame · dented(LOG 0553439) DENT ON FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMENT. FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMEN WAS REPAIRED PER PER B 737-800 SRM 53-30-07-2R.SDR DALA2024091609022Frame · dented(LOG 0553435) DENT ON FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMENT. FRAME STA 500A BTW S-25R TO S-24R AT FWD CARGO COMPARTMEN WAS REPAIREED PER PER B 737-800 SRM 53-30-07-2R.SDR DALA2024091609019Frame · dented(LOG 0553295) DENTS (2EA) ON FRAME STA 500C BTW S-25L AND S-26L AT FWD CARGO COMPARTMENT. FRAME STA 500C BTW S-25L AND S-26L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-30-07-2R-1.SDR DALA2024091609006Frame · cracked(LOG 0552643) CRACK ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8L & S-9L. FUSELAGE FRAME STA 500A BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02ASDR DALA2024091609004Frame · dentedDENT ON FRAME STA 500B BTW S-24L AND S-25L AT FWD CARGO COMPARTMENT. FRAME STA 500B BTW S-24L AND S-25L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-30-07-2R REPAIR 1.SDR VNAA202409110021Stub Frame · crackedL/H STUB FRAME @ FS 1031 STR. 17 - 19 FOUND TO BE CRACKED AT ATTACH FLANGE, REQUIRES REPAIR/REPLACEMENT. LOCATED, DRILLED AND INSTALLED NEW FS 1031 STUB FRAME PN# MM670-36133-007 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-SDR SWAA2024102836589Stub 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 1.687 INCH AT PASSENGER CABIN 2024-572141<[01] REPLACED STUB FRAME (1EA) ANGLE (1EA) AND FASTENERS LOCATED BTW BS 294.5 TO BS 296 ASDR UATA2024092400001Frame · buckledFRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILABSDR UATA202409245303Frame · buckledFRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILABLSDR UATA202409245302Frame · crackedONE PROFILE AT FRAME 10 IS CRACKED AT THE TOP END AND THE FRAME IS BUCKLED (UNDER FLOOR). REPLACED PROFILE, STRAIGHTENED FRAME, AND INSTALLED FRAME DOUBLER. FAA FORM 337 WAS COMPLETED.SDR EE4Y2024091020871Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT ENGINEERING ORDER E5311-0018, UPPER FUSELAGE R1 DOOR CUTOUT FR16 DOUBLE JOGGLE AREA WITH CRACK INDICATION AT DOOR STOP FITTING 7 LOCATION ON LOWER 3/16" DIAMETER HOLE WAS FOUND. REPAIRED R1 DOOR CUT OUT FR16 DOUBLE JOGGLESDR SWIA202412240909Frame · corrodedFRAME AT FS280 BETWEEN STR25L AND STR25R HAS CORROSION ON TOP IN MULTIPLE LOCATIONS. (C-CHECK RO 12/21/2024) (FILED CLOSED)BLENDED DAMAGE AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ EO CL-600-2C10-53-L08266 REV IR DATE 9/17/2024. SEE CONTINUATION CARD FOR DETASDR AALA202411194105Frame · crackedAIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR CUTOUT UPPER AFT CORNER FRAME CRACKED AT FR 68 AND S8R. REPLACED FRAME PER SRM 51-42-11.SDR YENA2024091001242Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 35 PRESSURE BULKHEAD FWD FACE LH SIDE, FROM LOWER OUTBOARD FASTENER AT LEVEL OF STGR30, CRACK LENGTH IS 0.095 INC H APROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN N/R 2024-501382, ACCOMPLISHED REPAIR HOLSDR R61A2024090900384Frame · corrodedDURING HEAVY CHECK, CFIII AFT CARGO FR80 STR27--28R CORROSION FOUND ON MACHINED FRAME. CORROSION ON MACHINED FRAME AT CFIII AFT CARGO FR80 STR27-28R REMOVED AND REPLACED IAW SRM 51-41-01, SRM 51-43-03, SRM 51-41-02, SRM 51-43-04.SDR DALA2024090908812Frame · corrodedSHIP 3133 CORROSION WEB FRAME LOCATED FROM FR69 TO FR70 AND STR 23LH AT AFT GALL EY AREA. CORRECTIVE ACTION: REPLACED SUPPORT WEB AND FASTENERS LOC. ON STRINGER 23L BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0545835)SDR SWIA20241108907Frame · crackedFRAME FS333.00 BETWEEN STGR 1R-2R CRACKED CAMP 28807442 (C-CHECK RO 11/6/2024) COMPLIED WITH ALL STEPS 1-20. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS AT FS333- STGR1R - STGR2R REF REO 670-53-21-2457 REV -A DATE 2024-09-25. COMPLIED WISDR AALA202411084056Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME DOUBLE JOGGLE AREA FASTENER HOLE AT FR 16 RIGHT AND S5R. REPAIRED FRAME PER EA 357885.SDR SWIA202501060018Frame · corrodedCORROSION NOTED ON FRAME FLANGE AT FS517.00 BTWN STRG 24L-25L (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACE FRAME SECTOR AT FS517.00 BETWEEN STR 25L-19L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH670-33200 REV. G. LSDR SWI2024F01392Frame · corrodedCORROSION ON FRAME FS 1015.00 BETWEEN STGR 24L - 22L(C-CHECK RO 12/21/2024) (FILED CLOSED)COMPLIED WITH EO NO: CL-600-2C10-53-L08265 REV IR REPAIR OF CORROSION ON FRAME FS 1015.00 BETWEEN STGR 24L - 22L LEAK AND OPS CHECK GOODSDR SWI2024F01382Frame · corrodedCORROSION NOTED ON FRAME FLANGE AT FS517.00 BTWN STRG 24L-25L (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACE FRAME SECTOR AT FS517.00 BETWEEN STR 25L-19L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH670-33200 REV. G. LEASDR REXA2024121101574Frame Splice · corrodedSTR 25R CIRCUMFERENTIAL JOINT AT FS333 REQUIRES REPLACEMENT DUE TO CORROSION LOCATED AND DRILLED STR 25R CIRCUMFERENTIAL JOINT AT FS333 IAW CRJ 700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE PART, P/N SH670-32429-4S. REFERENCE HN00184967, TASK 6A, FOR THE INSSDR SWIA202411120906Frame · corrodedCIRCUMFERENTIAL JOINT @ FS 333 HAS CORROSION UNDER STGR 20 L (C-CHECK RO 11/9/2024) AFTER EVAL DAMAGED AREA MEASURES L.4", W.1.5", D.100% FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-00-00 REMOVED AND REPLACED JOINT AT FS 333 IAW CRJ700 SRM 51-42-06 AND
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