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.
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
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 FDEA202201260230Floor Support · corrodedMAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR11 ~ FR13A , Y730MM ACCOMPLISHED THE SUPPORT REPLACED I.A.W A300-600F SRM 51-72-10-001 P2SDR VNAA202201271112Skin · damagedDURING ROUTINE MAINTENANCE AT GREER, SC (GSP), MAINTENANCE FOUND ONE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN FS1098 Ï¿½ FS1108 AND STGR 16L-17L. THE DAMAGE MEASURES 5/32Ï¿½ IN DIAMETER AND APPROX. 0.0075Ï¿½ DEEP. / EA 21-C9-53-942 REV A. DATED JAN 20, 2022 DSDR EE4Y2022012615038None · noneDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FWD FUSELAGE BETWEEN FR13 AND FR14, Y=285.00MM FLOOR SUPPORT WITH CORROSION, THE DAMAGE WAS TRIMMED, NO SRM REPAIR WAS FOUND TO THE DAMAGE AREA, WAS REPAIRED INSTALLING REPAIR DOUBLER AS PER E.O. # COO-EO-2022-1SDR V0XD20220321001Intercostal · corrodedINTERCOSTAL AT F.S. 364 AT STRG 27 R/H INTERCOSTAL IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL (PN: SH670-320-75-4S) IAW CRJ 200 SRM 51-42-06-001-001A01.SDR FDEA202201250127Frame · noneCABIN - LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING AS MARK. CABIN LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR CARRIED OUT AS PER SRM 53-20-07-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR ASAA2022012437276Web · corrodedAFT PIT DOOR SUROUND LOWER SILL WEB CORRODED MILTIPLE AREAS BETWEEN STA 787 TO STA 847. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-60-15-1A-1. REMOVED AND REPLACED SILL WEB IAW 737-900ER SRM 51-40-02-0G-0.W= 2" O= .050 R=SDR CALA2022012400208Skin · corroded(B757-53-3-0479) AFT GALLEY WET AREA - STA 1680 FLOOR BEAM PRESS URE DECK - FROM LBL 51.50 TO RBL 51.50 - SPLICE PLATE AT BL 0 - STA 1720 AT BL 0 - UPPER SKIN HAS SURFACE CORROSION, TRANSCRIBE D FROM HAECO GSO NR LP 9281120. 12 EA DISCREPANT AREAS WERE FOUND.SDR FDEA202201220242Floor Support · corrodedMAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR12A ~ FR13A , Y1450MM REPAIRED THE DAMAGE AREA WITH TEE SPLICE REPAIR I.A.W. A300-600F SRM 53-12-15-201-2 PARA.5.G P.239-244 FIG.207SDR IPXA2022021078833None · brokenINSPECTION TYPE:A300AT FRAME 38.1 APPROX Y1426 CLS ADAPTER BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.SDR AALA202202145108Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF LH TRANSITION PANEL BETWEEN STA 460 AND STA 500I AT LBL 23, MEASURING L=1.0 IN, W=2.0 IN, D=0.015 IN. REPLACED TRANSITION PANEL WITH NEW IAW SRM 53-00-53-2R-5.SDR R61A2022021000116Beam · corroded5 EACH AREAS OF CORROSION ON FWD SERVICE DOOR SILL AS MARKED. REMOVED AND REPLACED FWD SERVICE DOOR LOWER SILL , REF SRM 51-40-08.SDR AALA202202072654None · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CREASE ANGLE NEAR FASTENER HOLE AT STA 303.9 AND LBL 58, MEASURING L=0.5 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 53-10-15-2R-8.SDR SWIA202265401Pressure Deck · corrodedRH PRESSURE FLOOR SILL PANEL CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 AND FS 529. (C-CHECK RO 4/20/2022) REPAIRED R/H PRESSURE FLOOR SILL BETWEEN F.S. 409.00+128 AND F.S. 529.00 I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06. COMPSDR IPXA2022020178562Longeron · noneINSPECTION TYPE:C3CENTER CARGO HAS A CRACK LONGERON 39R BETWEEN R/H STA 5-113 TO 1541.REPAIRED CRACKED LONGERON 39R BETWEEN STA Y=1531 AND Y=1561 IAW MD11 SRM 53-00-05 REPAIR 1 FIGURE 201/202 (MAJOR)SDR FDEA202201190094None · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1541 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1541 LONGERON -12 LEFT HAND TO LONSDR FDEA202201190093None · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1561 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1561 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHT HSDR FDEA202201190092Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1541 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1541 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHT HSDR FDEA202201190091Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 5-113 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 5-113 LONGERON -12 RIGHT HAND TO LONGERON -13 RIGHTSDR FDEA202201190090Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1621 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1621 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND SDR FDEA202201190089Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1601 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1601 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND SDR FDEA202201190088Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1581 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1581 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND SDR FDEA202201190087Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1561 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 1561 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND SDR FDEA202201190086Frame · unknownAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT FRAME STATION 5-73 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT FRAME STATION 5-73 LONGERON -12 LEFT HAND TO LONGERON -13 LEFT HAND EVSDR LR7A2022011903076Beam · corrodedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB3200, FOUND LH MLG FS597 BEAM FITTING CORRODED AT LBL61.6-67, WL146. / REPAIRED IAW LAC MEA 382-53-22-001. NR#1000669804.SDR K11A2022030300121Frame · corrodedFRAME AT STATION 1166 OUTBOARD OF STRINGER 29 RIGHT HAS EVIDENCE OF CORROSION AT INTERFACE BETWEEN LOWER CHORD AND WEBSDR K11A2022021700116Stringer · corrodedAFT PIT FRAME AT STATION 1030 STRING 27 R HAS EVIDENCE OF CORROSION ON UPPER SURFACESDR K11A2022021700115Frame · corrodedAFT PIT FRAME AT STATION 1010 BETWEEN STRINGER 26R AND 27R HAS EVIDENCE OF CORROSION ON UPPER SURFACESDR IPXA2022012878390None · noneINSPECTION TYPE:C12CRACK ON WERTICAL STIFFENER (P/N:141T2938-16) OF WHEEL WELL BULKHEAD AT STA 287 ,LBL 25 ,WL159.REPAIR I.A.W 767-300F SRM 51-70-12 GENERAL ,FIGURE 1 , REV82.01.SDR KCSA202201181007Web · crackedCREASE BEAM WEB AT STA 940 R/H CRACKED AT O/B SIDESDR KCSA202201181006Tension Tie · crackedTENSION TIE AT STA 740 L/H AFT SIDE OF TENSION TIE UPPER O/B HOLE CRACKED TO EDGE. FOUND VISUALLY AND VERIFIED WITH HFEC OPEN HOLE AND HFEC SURFACE SCANSDR KCSA202201181005Web · crackedCRACK ON CREASE BEAM 980 LEFT ON OUTER WEBSDR KCSA202201181003Web · crackedCRACK 960 LEFT ON CREASE BEAM OUTER WEBSDR KCSA202201181002Web · crackedCRACK 960 LEFT ON CREASE BEAM INNER WEBSDR KCSA202201181001Web · crackedCRACK 950 RIGHT, IN CREASE BEAM WEBSDR V0XD20220216001Frame · damagedSPLICE REPAIR AT FS 319 AT STR 27 IN FWD AVIONICS BAY. CORRECTIVE ACTION: PERFORMED REPAIR TO FS 319 (P/N: SH670-31355-1) AT STR 27 IAW BOMBARDIER REO 670-53-21-799 REV A DATE 2016-11-27.SDR FDEA202201170275Shear Web · crackedN00253 MAIN DECK FLOOR STRUCTURE'S SHEAR WEB CRACKED AT FR79 160MM,-Y1630MM POS. REPLACED THE WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 P.2.SDR R61A2022020500104Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION FOUND ON FWD FUSELAGE SHEAR TIE CLIP AT FR17 BETWEEN STGR 27L AND STGR 28L. SHEAR CLIP AT FRAME 17 BETWEEN STRINGER 27L AND STRINGER28L IN FORWARD FUSELAGE WAS REMOVED AND REPLACED IAW SRM 51-41-02.SDR FDEA202201160074Doubler · unknownWHILE ACCOMPLISHING RIGHT HAND E.A.#G-5710-T0366056A P2 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#G-5710-T0366458 P2 TITLE : WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT SDR FDEA202201160073Doubler · unknownWHILE ACCOMPLISHING LEFT HAND E.A.#G-5710-T0366056A P1 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#G-5710-T0366458 P1 TITLE : WING - BASIC WING STRUCTURE - CENTER WING RING CHORD, FRONT SPSDR FDEA202201160072Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND EXTERIOR FUSELAGE SKIN COMMON TO UNDERWING LONGERON FITTING, FOUND 01 EACH CRACK AROUND FASTENER HOLE AT STATION 1033 STRINGER 37R, APPROXIMATELY 1.0 INCH IN LENGTH, AS MARKED.SDR FDEA202201160123Seat Track · damagedN00464 MAIN DECK SEAT TRACK LOBE AT LOCKS L1206 & L1199 DAMAGED. REPLACED THE DAMAGED SEAT TRACK WITH NEW ONE. I.A.W. A300-600 SRM 51-72-10-001 PAGE. 1~3. SEE ATTACHED JPF FOR DETAIL.SDR FDEA202201150071Hinge · wornMAIN DECK CARGO CUTOUT UPPER EDGE,AFT HINGE FITTING (PART NUMBER ACA 7223-1) LOBES #3 TO #11 FOUND OUT OF TOLERANCE LIMITS. MAIN DECK CARGO CUTOUT UPPER EDGE,AFT HINGE FITTING (PART NUMBER ACA 7223-1) LOBES #3 TO #11 REWORKED AND FOUND #9 TO #11 EXCEED LSDR FDEA202201150070Hinge · wornMAIN DECK CARGO DOOR CUTOUT UPPER EDGE,FORWARD HINGE FITTING (PART NUMBER ACA 7223-513) LOBES #1, AND #9 TO #17, FOUND OUT OF TOLERANCE LIMITS. MAIN DECK CARGO DOOR CUTOUT UPPER EDGE,FORWARD HINGE FITTING (PART NUMBER: ACA 7223-513) LOBES #1, AND #9 TO SDR SWAA2022021461831Doubler · crackedPOWER RECEPTICAL CUTOUT LOWER LATCH DOUBLER IS CRACKED ; / [01] CUTOUT DAMAGE AT POWER DOOR LOWER LATCH DOUBLER IAW SRM 53-10-15-2R-4 REPAIR4; [02] VERIFIED STEP 1 COMPLETE<BR><BR>HFEC IAW B737 NDT P6 51-00-00 P23 TOOL 36303 DUE 13APR22 NO CRACKS NOTED; [03] VSDR ASAA2022011437340Cargo Track · corrodedAFT PIT CARGO TRACK AT RBL-16 HAS CORROSION AT STA 767+6. GROUNDED - YES. REPAIR TO AFT PIT CARGO TRACK AT RBL-16 AND AT 767+6 IAW ASA EA 900ER-53EA-24154 CAT A REPAIR NO FURTHER INSPECTION REQ.W= .90 O= .070 R= .037 L= 3.75" D= .033.SDR ASAA2022011437331Cargo Track · corrodedAFT PIT CARGO TRACK AT RBL-16 HAS CORROSION AT STA 767+6. GROUNDED - YES. REPAIR TO AFT PIT CARGO TRACK AT RBL-16 AND AT 767+6 IAW ASA EA 900ER-53EA-24154 CAT A REPAIR NO FURTHER INSPECTION REQ.W= .90 O= .070 R= .037 L= 3.75" D= .033.SDR ASAA2022011437245Plate · corrodedAFT PIT TRANSITION AT RBL-21 HAS MULTIPLE AREAS OF CORROSION BETWEEN STA 727I+6 TO STA 767. GROUNDED - YES. REPAIRED DAMAGED SECTION OF TRANSITION FROM STA 727I+6 TO 767 R/H IAW B737-900 SRM 53-00-53-2R-5.W= 3.00" O= .040" R= .000" L= 3.0" D= .040".SDR DALA2022011400280None · noneCORROSION STA 927 TO 946 AT LONGERON 30 AND SPLICE. SUMMARY SEE NRC 088-0008:5331-2001/011 00381: REMOVED CORROSION AND CHECKED LIMITS STA 927 TO 946 LONGERON 30 PER B717 SRM 53-00-00. REPLACED SPLICED PER B717 SRM 53-20-05-2R. (LP #2085655)SDR K11A2022030300119Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER 27 RIGHT SPLICE AT STATION 1050SDR CALA2022011400147Stop Fitting · cracked(REPAIR BEFORE NEXT FLT) CRACK FOUND IN LH FR16 #1 DOOR STOP FIT TING HOLE #3 CRACK IS IN THE FRAME AND INTERCOSTAL. () REPIR L/H FILE #1 DOOR STOP FITTING HOLE #3 IAW EC/RA 5311-02702 ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. NR#00187 18.
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