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 KCSA202007151113Frame · crackedSTA 800 STR 17 L 2 AFT FRAME FASTENER HOLES HAVE CRACK INDICATION.SDR SWIA2020090252165Frame · corrodedF.S. 319 FRAME IS CORRODED BETWEEN STRINGER 27 TO 26L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTION AND SPLICES IAW CRJ 200 SRM AND SKYWEST CARD. COMPLETED FORM M-337 AND M-131. WEIGHT REMOVED .35 WEIGHT INSTALLED .6 TOTAL WEIGHT INSTALLEDSDR SWIA2020090252164Frame · corrodedF.S.333 FRAME IS CORRODED BETWEEN STRINGER 27 TO STRINGER 26L AND 23L TO 22L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS 333 STRINGER 18L-23R IAW CRJ 200 SRM, AND DWG. COMPLIED WITH SKY CARD FORM M-337 COMPLETED. WEIGHT AND BALANCSDR FDEA2020082641970Frame · damagedWEAR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE, IAW EA 6-5310-T0355376 P1 EA TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGO COMPARTMENT - CHAFE/WORN DAMAGE COMMON TSDR SWIA202008252042Frame · corroded280 FRAME HAS MULTIPLE AREAS OF CORROSION ON THE LOWER AFT SIDE BETWEEN STRG25L & STRG25R, COMPLIED WITH CORROSION REPAIR OF 280 FRAME AFT SIDE BETWEEN STRINGER 25L AND STRINGER 25R AS PER SRM AND REO.SDR SWIA202008252027Frame · corroded* A BAY - FS 319 - FRAME CORRODED ON AFT SIDE OF STGR 26R. REMOVED CORROSION ON FRAME AT FS319 BETWEEN 25L & 25R. FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO.SDR SWIA202008252019Frame · corrodedA BAY - FS 295 - FRAME CORRODED BOTH SIDES OF STGR 27. REPAIRED FRAME 295.00 FROM STRG 25L TO STRG 25R REF SRM.COMPLIED WITH TASK CARD. NO LEAKS NOTED.SDR SWIA202008252015Frame · corroded* FWD FUSELAGE - BELOW FLOOR - FS 250 FRAME CORRODED @ STGR 26R. REPAIRED DAMAGE REF REO.SDR SIMA202007154005Frame · corrodedFUSELAGE BAGGAGE DOOR LATERAL L-SHAPE AT FR 68 BETWEEN STGR 16L-17L CORRODED. REPAIRED FRAME 68 BETWEEN STGR 16L-17L IAW SRM 53-31-04. PART REPLACED: SHEAR CLIP PN 145-25369-603.SDR 2020F00336Frame · crackedCRACK DAMAGE REPAIR OF NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS, FS 75. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020 WITH FAA FORM 8100-9 DATED 06/01/2020.SDR SWIA2020072951538Frame · corrodedFS364.00 FRAME IS CORRODED ON LOWER FLANGE AT STRINGER 27. CUT AWAY DAMAGE FROM FS364 FRAME SECTION FROM STR24L - STR24R, FABRICATED REPAIR PARTS AND INSTALLED NEW FRAME IAW SRM, DRAWING.SDR AALA202007189004Frame · damagedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FRAME HAS OVERSIZED FASTENER HOLE AT BS 727G AND S25R. REPAIRED FRAME PER EA 306896.SDR AALA202007189003Frame · damagedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FRAME HAS OVERSIZED FASTENER HOLE AT BS 727H AND S25R. REPAIRED FRAME PER EA 306896.SDR AALA202007189002Frame · damagedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FRAME HAS OVERSIZED FASTENER HOLE AT BS 747 AND S25R. REPAIRED FRAME PER EA 306896.SDR SWAA2020080700932Frame Splice · corrodedCORROSION ON FRAME AT ACB BS 787, RBL 26, WL 158. REMOVED AND REPLACED SPLICE ON ACB FRAME ITEM 146 A130003 IAW SRM 51-40-02-0G-0 AND DWG 146A1262.SDR SWIA2020081151724Frame · corrodedFRAME AT F.S. 349.00 CORRODED BETWEEN STGR 27 AND STGR 26L. (C-CHECK) RO 8/8/2020 REMOVED AND REPLACED F.S.349 FRAME IAW CRJ 200 SRM AND DWG ( FASTENER CALL OUT). COMPLETED AND ATTACHED TASK CARD AND M- 337. NO WEIGHT CHANGE.SDR SWIA2020081151722Frame · corrodedF.S. 574 FRAME IS CORRODED BETWEEN STRG 27 TO STRG 26L, AND 27 TO 26R AND 22L TO 21L. REMOVED AND REPLACED F.S. 574 LOWER FRAME SECTOR BETWEEN STRG 21R TO 21L. IAW CRJ 200 SRM AND DWGS.SDR SWAA2020072797632Frame · corrodedBS 847 FRAME UPPER SURFACE CORRODED. LBL20; WL156. REPAIRED THE FRAME IAW ER20-02837, REV IR, AND EA 20-153-01157, REV IR.SDR UIEA2020070771426Frame · crackedBS 2598 BULKHEAD RT INNER CHORD AREA, ONE CRACK FOUND ON THE FWD SPLICE FITTING, SECOND LAYER COUNT FROM INBD. APPROX 0.040" IN DEPTH RUNNING AFT AT 4 O`CLOCK POSITION, THE BULKHEAD UPPER CORNER RT SPLICE FITTING WAS REPAIRED IAW RI-53-00-14106 REV A.SDR FDEA2020070211410Frame · crackedCRACK INDICATION FOUND IN HOLE MARKED BS760 AT S-20R-21R, FWD SIDE OF FRAME AT 8 O CLOCK POS [FWD PIT]. REPAIRED AREA PER EA F-5310-T0354804 FUSELAGE-MAINFRAME-FUSELAGE FRAME, STA760 S-21R TO 22R, INSULATION STUD HOLE, CRACK.SDR P5CA2020070100244Frame · crackedFX STA 880 BODY FRAME UPPER FOUND CRACKED. BODY FRAME REPAIRED IAW SRM 53-00-71 REPAIR 4 FIG 201.SDR MASA20200630052Frame · corroded(C-CHECK) REPAIRED FRAME AT FS319 BETWEEN STGR 23R AND 25L. A SECTION OF FRAME WAS SPLICED IN TO COMPLETE THIS REPAIR,.SDR MASA20200630051Frame · corroded(C-CHECK) REMOVED AND REPLACED FRAME SECTOR AT FS295 STGR 25R-25L.SDR SWAA2021080596116Frame · corrodedFUSELAGE BS 887 BETWEEN S-25R TO S-27L HAS MULTIPLE SMALL AREAS OF CORROISION ON AFT SIDE OF BS 887 FRAME (AFT CARGO) / REMOVED CORROISION PER SRM 51-10-01; INSTALLED FASTENERS PER REF SRM 53-00-01; TREATED PER SRM 51-20-01 REF SA-M 326: A1131711SDR 2A6R2020062556702Frame · corrodedHEAVY CORROSION FOUND ALONG RIGHT HAND FUSELAGE CABIN FLOOR EDGING FRAME.SDR 2A6R2020062556701Frame · corrodedHEAVY CORROSION FOUND ALONG LEFT HAND FUSELAGE CABIN FLOOR EDGING FRAME.SDR 2020F00320Frame · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, BS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV-, AND 8100-9. STANDARD REPAIR CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS.SDR SWIA2020072951517Frame · corrodedTHE FRAME AT FS1015.00 FROM STRINGER 26L TO 26R HAS CORROSION. THE FRAME WAS FOUND OUT OF LIMITS, NO DAMAGE ALLOWED TO ATTACHING FLANGE IAW SRM (ORIGINAL: .050) - (REMAINING: .047) - (LOSS: .003). REMOVED AND REPLACED THE FRAME IAW SRM AND DRAWING.SDR SWIA2020072951516Frame · corrodedTHE FRAME AT BS 1000 AT STRINGER 21L HAD CORROSION. BLENDED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM. (ORIGINAL: .050) - (REMAINING: .037) - (LOSS: .013). CUT AWAY DAMAGE, FABRICATED AND INSTALLED NEW REPAIR ANGLE FLANGE IAW REO, AND SRM.SDR VNAA202006239997Frame · corrodedFRAME 310 CORRODED STRINGER 27L - 26R. REMOVED AND REPLACED FRAME 310 IAW SRM 53-00-06-201-006-A01.SDR SWIA2020072951508Frame · corroded* LH FS333.00 / BETWEEN STGR 18-19 BOTH SIDES FRAME ARE CORRODED. FLAGGED (C-CHECK) RO 7/25/2020 --FRAME FS333 BETWEEN STR18L - STR19L "OUT OF LIMITS" DUE TO OVER LAPPING DAMAGE IN MULTIPLE ELEMENTS REF SRM. REMOVED AND REPLACED FRAME SECTOR FS333 BESDR 2020F00317Frame · crackedNLG WHEEL WELL WEB AND UPPER MID FRAME CRACKED. STANDARD REPAIR SR-680A-ATA53-25890 , CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW),SDR 2A6D2020062201502Frame · crackedDAMAGE TO THE X2258 RH CROSSBEAM (PN: 350A21-4065.22) IN THE FORM OF A CRACK. THE CRACK WAS MEASURED TO BE APPROXIMATELY 1.20” IN LENGTH.SDR HNAA2020072000215Frame · chafedDURING HEAVY CHECK, FRAME 81 WAS CHAFED THROUGH AT THE 6 O'CLOCK POSITION. R & R THE LOWER SECTION OF THE FRAME IAW SRM 51-40-02.SDR SWIA2020080751683Frame · corrodedBB 295 FRAME, BETWEEN STRINGERS 26L & 26R HAD SIGNS OF CORROSION. SPLICED IN A NEW FRAME SECTION IAW SRM.SDR SWIA2020072951497Frame · corrodedFRAME @ FS319 STGR17L-STGR21L IS CORRODED (C-CHECK) RO 7/25/2020 --FRAME FS319 STR17L - STR21L "OUT OF LIMITS" DUE TO CORROSION ON TWO LOCATIONS ON THE FRAME REF CRJ700 SRM --REMOVED AND REPLACED FRAME FS319 BETWEEN STR17L - STR21L REF CRJ700 SRM, DRAWINGSDR HNAA2020062900186Frame · crackedFR 73 IS CRACKED BETWEEN STR 17R-16R. MAINTENANCE: REMOVED AND INSTALLED NEW LOWER SECTION OF FRAME 73 IAW EMB 145 SRM 51-40-02.SDR FXGA202006182009Frame · crackedCRACKED FRAME AT F/STA 937 LBL6 & RBL6. TO REPAIR 2 SMALL CRACKS IN FAIRING SUPPORT FRAMES AT F/STA 937 LBL6 & RBL6. (JUST FORWARD OF MAIN WHEEL WELL DOORS). PERFORM REPAIRS ON CRACKED FRAMES PER DC-9/MD-80 SRM 53-01 FIGURE 2 (SHEET 4).SDR DU4R2020061800049Frame · crackedAD 2019-08-02(H): TABLE 2 / PART 2 AND BOEING SB 737-53A1360,IR,PART 2 INSPECTION FIGURE 7,8,13 AND 14, FORWARD SIDE OF FRAME WEB HAS A CRACK RUNNING OUTBOARD FROM FASTENER HOLE 1/4" LONG BS 500E JUST BELOW STR10LSDR SWAA2021072793183Frame · corroded***CORROSION*** ACB BS 947 FRAME LBL 10 WL 156 HAS CORROSION / REMOVED CORROSION IN AN AREA OF 2.3X7.4. REMOVED .011'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 FIG 102 DETAIL C. REMOVED FASTENERS PER SRM 51-40-02-0G-0. ACB BS 947 FRAME STR 23L TO 23R WISDR SWIA2020072251389Frame · crackedFRAME SECTOR APPROX BS 333, STRINGER 1L, CRACKED AT TOOLING HOLE. REMOVED AND INSTALLED A NEW FRAME IAW DRAWING, AND SRM. COMPLIED WITH TASK CARD. ALL CHECKS GOOD.SDR FDEA202006171260Frame · crackedDURING HFEC INSPECTION, FRAME AT BS 1721, BETWEEN STRINGER 12L AND 13. FOUND CRACKED ON ORIGINAL FRAME APPROXIMATE 1/2 INCH.SDR SWIA2020072251384Frame · corroded*CORROSION ON FRAME AT FS 605.00 ON FWD FACE BETWEEN STRG 24R STGR 26R (C-CHECK) RO 7/18/2020 REPLACED FS605.00 FRAME BETWEEN STGR 20R AND STGR 20L. REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.SDR SWIA2020072151352Frame · corroded* THE FRAME AT FS319.00 BETWEEN STRINGER 26R AND 25L HAD CORROSION. REMOVED CORROSION IAW SRM. CORROSION DAMAGE EXTENDS TO MULITIPLE COSSECTIONS AND TOTALS MORE THAN 30 PERCENT OF ITS LENGTH. DAMAGE IS OUT OF LIMITS IAW SRM. REMOVED LOWER FRAME SECTOR SDR SWIA2020071451318Frame · chafedFRAME AT FS654.5 IS CHAFED THROUGH JUST FORWARD OF THE APU EXHAUST PORT. (C-CHECK) RO 7/10/2020 REPAIRED FRAME AT FS654.5 JUST FORWARD OF THE APU EXHAUST PORT REF REO. SEE CONTINUATION CARD FOR DETAILSSDR DU4R2020061500046Frame · crackedBS360 BETWEEN STR25L AND STR27 6 EACH FASTENER HOLES PRODUCED REJECTABLE INDICATIONS DURING ABHEC INSPECTION. ALL APPLICABLE DISCREPANT HOLES MARKEDSDR FDEA2020061091169Frame · crackedCRACK INDICATION FOUND: LT BS1640 AT S-14L AT LOWER I/B FASTENER HOLE AT INTERCOSTAL TEE CLIP. BETWEEN TEE CLIP & CHORD LAYER LOOKING AFT AT 8 O'CLOCK POSITION. (1ST & 2ND LAYER) ACCOMPLISHED EA F-5310-T0354398-P1 FUSELAGE - MAINFRAME - FRAME WEB, STA 1640 S14SDR QMLA2020061820027Frame · cracked2EA. CRACKS FOUND ON FRAME 5 AT: X 4740, Y -840, Z 2230, AND Z 2470. ONE CRACK WAS 1.5" AND THE OTHER CRACK WAS .875" IN LENGTH.SDR IPXA2020062977046Frame · crackedINSPECTION TYPE:2CFWD TAILCONE AFT R/H FRAME HAS 2 CRACKS IN RADIUS AT UPPER AND LOWER LATCH FITTINGS.REMOVED AND REPLACED CRACKED FWD TAILCONE AFT R/H FRAME IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR SWIA2020062351159Frame · not reportedREMOVE AND REINSTALL FRAME AT FS333.00, BETWEEN STGR 18R AND 20R. (C-CHECK) RO 6/21/2020 REMOVED AND INSTALLED NEW FRAME AT FS333.00 IAW SRM. LEAK CHECK GOOD.
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