JASC 5311
Service difficulty reports · 61,524
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 SWAA2026100956663Frame · crackedCRACKED FRAME, BS 312, STR 5L - 6L. PERFORMED A REPAIR CAT B ON THE FRAME IAW EA 26-153-02554-WIP1, & EA 26-153-02554.SDR IPXA2026091716966Frame · dentedAFT CARGO COMPARTMENT FUSELAGE FRAME HAS 2 DENTS APPROX AT BS 1460, STGR 26R, VERIFIED REMOVAL OF FITTING ON STEP 27 PER DOCUMENT AND PER GMM RII 04-02SDR DALA2026091005063Frame · damagedS.B A320-53-1491-WORK CARD 5311-01244-02B R/H FRAME 68 FLANGE HAS PREVIOUS REPAIR REQUIRING FURTHER ENGINEERING TO COMPLETE WORK CARD. CURRENT ERA 603003-14AD. REV 0. C/A: COMPLIED WITH ERA 6365560-14 REV 0 FOR THE R/H FR 68 FLANGE NO DEFECTS NOTED. JOB COMPLESDR DALA2026091005062Frame · damagedS.B A320-53-1491-WORK CARD 5311-01244-02A L/H FRAME 68 FLANGE HAS PREVIOUS REPAIR REQUIRING FURTHER ENGINEERING TO COMPLETE WORK CARD. CURRENT ERA 602719-14AD. REV 0. COMPLIED WITH ERA 602719-14AD, REV 0, SECTION II IAW ESR 18175. ALL STEPS OF PRI 636551-14 RSDR FDEA202609061267Frame · crackedINSPECTION OF FRAME 40 LT, LOWER WING JUNCTION, FOUND A CRACK SIGNAL AT FASTENER HOLE NR 1. COMPLIED WITH EA: 6-5710-T0388595 P1. REPAIRED FRAME 40 LT LOWER JUNCTION, CRACKED FASTENER HOLE NR 1. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION IAW EA 6-5710-SDR YENA2026091000778Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE MIDD LE LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0 .105 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00065 ) RESDR YENA2026091000777Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE AFT LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.12 0 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00066 ) REF ASDR YENA2026091000776Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE LOWE R OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION IS 3 OCLOCK, CRA CK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: SDR YENA2026091000774Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE FWD MIDDLE COMMON TO SKIN,CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS0.085INCH,IN FWD CARGO COMPARTMENT (1EA) ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00070 ) REF AEROMSDR YENA2026091000772Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR39RH STR14 PLUS 4 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00072 ) REF AEROMAN WO 2026-280/1,SDR YENA2026091000771Frame · crackedDURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR41LH STR14 PLUS 3 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH )PAX CABIN ; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00073 ) REF AEROMAN WO 2026-280/1, SDR YENA2026091000768Frame · crackedDURING HEAVY MAINTEANCE,DURING HEAVY MAINTEANCE,CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND ON OPENHOLE LOC FR39LH STR14 PLUS 4 INCH. CRACK DIRECTION 9 OCLOCK AND DEPTH =0.100 INCH )PAXCABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00076 ) REF AEROSDR YENA2026091000752Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 20 LH SIDE IN OPEN FASTENER HOLE H26 AT CROSSBEAM SPLICING AREA, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.0 85 INCH, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1474396 TASKCARD: NR-00025 ) REF: ARM WSDR IPXA2026091580804Frame · corrodedFRAME STA 1992 FWD AND AFT SIDES HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH WITH HEAVY DEBRIS ON BACK SIDE PLUGGING DRAIN HOLE.SDR IPXA2026091478857Frame · corrodedAFT FUSLAGE FRAME STA 1963 FWD AND AFT SIDES AND ALL ATTACHING STRUCTURE CIRCUMFERENTIALLY HAVE AREAS OF CORROSION AND LARGE AREAS OF MISSING PROTECTIVE FINISH AND TOPCOAT. VERIFIED STEP 20, C/W RII GMM 04-02.SDR SWAA2026101947890Frame · puncturedFRAME WEB, BS 380, WL 153, STRINGER 27R WAS PUNCTURED. REPAIRED IAW EA 26-153-02454.SDR 2A6R2026090375403Frame · corrodedFOUND CORROSION DAMAGE ON FRAME 1, REQUIRING REPLACEMENT OF THE FRAME.SDR HNAA2026100700952Frame · crackedCOCKPIT, LEFT UPPER FRAME CRACKED. REPAIRED IAW ETD 2026-145-015252 AND EO 1-53-26-0462.SDR CALA2026092819874Frame · crackedAFTER NDT INSPECTION ON FRAME 727E UPPER HOLE, FOUND A CRACK . EVALUATED DENT ON VERTICAL LEADING EDGE, FOUND TO BE WITHIN LIMITS IAW SRM 55-30-01-1A-1, PAR. 4.A, TABLE 101. PERFORMED DENT REWORK. PERFORMED NDT, NO CRACK SIGNAL NOTED, AND APPLIED ALODINE IASDR HNAA2026100600949Frame · crackedFRAME 25 CRACKED AT LWR HOLE FOR SILL ATTACHMENT BTW STR15-16L. REPAIRED IAW STD 2026-145-015471SDR AALA202608319919Frame · wornAIRCRAFT IN BASE MAINTENANCE: HORIZONTAL SLIDER FRAME WORN AT STA 1006, LBL 56. MAINTENANCE REPLACED HORIZONTAL SLIDER FRAME WORN AT STA 1006, LBL 56 AW AARD 51-00-05-1 AND DRAWING 181A8014-31.SDR DALA2026083104900Frame · corrodedCORROSION ON FRAME BS 1681, BTW S27R TO S30R AT AFT CARGO BAY. CORROSION LEVEL 2, FRAME BS 1681 BTW STR 24R-24L MANUFACTURED AND REPLACED IAW SRM 51-40. (1780312)(AIRCRAFT GROUNDED)SDR DALA2026082704872Frame · crackedFRAME 40 LOWER SHELL PANEL JUNCTION, RT SIDE. FOUND A CRACK IN THE H378 FASTENER HOLE, THE LENGTH OF CRACK IS ABOUT 15MM. REPAIRED IAW ERA 636140-14AD, REV ORIGINAL. (1779678) AIRCRAFT WAS GROUNDED.SDR FDEA202608261232Frame · crackedRIGHT, BS 1640 FUSELAGE FRAME WEB AT STRINGER 14R UPPER INBD CRACK INDICATION AT 2:00 O'CLOCK, AROUND THE BOTTOM INBD HOLE WITH TWO CRACK INDICATIONS AT 2:00 O'CLOCK AND 7:00 O'CLOCK FACING AFT. FRAME REPAIRED IAW EA F-5310-T0388261, PART 1, & 2. THIS EA DEVSDR 2A6R2026082575402Frame · crackedTWO CRACKS APPROXIMATELY 6MM IN LENGTH EACH WERE DISCOVERED ON THE LH UPPER FRAME 5 MEDICAL INTERIOR MOUNT LOCATION. BOTH CRACKS PROPAGATED FROM THE SAME RIVET HOLE AT APPROXIMATELY FS: 4780, WL: 2400, AND BL: -710. THE CRACKS WERE LESS THAN 1.5” IN LENGTH ANSDR DALA2026082704867Frame · corrodedCORROSION ON RT SIDE FRAME AT MULTIPLE LOWER PANEL FASTENER AREAS. WORKED WITH NR 303 FOR REMOVAL AND REPLACEMENT OF LONGERON. (LP# 1774104; AIRCRAFT WAS GROUNDED)SDR SWIA2026082377263Frame Angle · crackedCRACK FOUND ON THE RT FRAME ANGLE, BS 605, STR 20R. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM 51-42-06, REV 39, SRM 51-42-21, REV 39, AND DWG 601R36026 REV AF.SDR SWIA2026082377249Frame Angle · crackedCRACK ANGLE AT FRAME BS 605, STR 20L. REMOVED AND REPLACED THE FRAME ANGLE AT BS 605, STR 20L IAW SRM 51-42-06, REV 39, SRM 51-42-21, REV 39, AND DWG 601R36026, REV AF. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1003-SKY LEAK CHECKED GOOD.SDR DALA2026082404791Frame · damagedELONGATED FRAME HOLE TO ATTACH AFT ROD OF LT AIR CONDITIONING PACK BS Y=1133 & LONG 9L AT AFT ACCESORY COMPARTMENT, REPAIRED FRAME HOLE IAW SRM 53-00-07-2R. (1772689) (AIRCRAFT GROUNDED).SDR SWAA2026091816104Frame · crackedCRACK ON OPEN HOLE LOC INNER CHORD LOC BTW BS639 LBL60 AT PASSENGER CABIN 2026-490475 REPLACED INNER CHORD LOCATED BTW BS616 TO BS663 PLUS 9 AT LEVEL STR 17L PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG: 144A5901 SHEET: 36 REV: -.SDR IPXA2026090472486Frame · crackedDEFERRAL. WHILE ACCOMPLISHED A DETAIL INSPECTION OF THE FUSELAGE SUPPORT, FRAME FOUND A 3 INCH LENGTH CRACK AT BS 1060. ACCOMPLISH THE PERMANENT REPAIR PER EO-98554-REQ1 AND STE-MAE EA 757-5340-27-A4611, REV.SDR SWAA2026092433515Frame · crackedCRACKED FRAME, BS 312, BTWN STR 5L - 6L. REPAIRED THE FRAME IAW M-22-153-01244.SDR SWIA2026082077610Frame · corrodedFRAME, BS 379, S19L POSSIBLE CORROSION. THE FRAME WAS REWORKED & REPAIRED IAW SRM 53-00-15, PAGE 204, FIGURE 202.SDR SWAA2026092148509Frame · crackedCRACKED FRAME, BS 259.5 BTWN STRINGERS 8 - 9R. REPAIRED THE FRAME BS 259.5, STR 6 - 11R IAW EA 26-153-02323-WIP1, AND EA 26-153-02323.SDR SWAA2026091433998Frame · crackedCRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED TRIM OUT OF FRAME UPPER ANGLE IAW EA M-22-153-01244, REV B.SDR CALA2026082518902Frame · damagedAFT CARGO RH FREE FLANGE AT STA 1500 B/W STR 26 AND 27 HAS OPEN HOLE NEXT TO PLUG FASTENER. ACCOMPLISHED REPAIR PER VT MAE EA 757-5360-13-A4581 WITH NO DEVIATIONS. REF ECRA 5360-02196 PART 1- INTERIM REPAIR. ADD EMP:V944084 ACCOMPLISH A PERMANENT REPAIR AT FUSSDR CALA2026082518896Frame · damagedAFT FARGO COMPARTMENT RH SIDE FR 1520 B/W STGR 23 - 26 FREE FLANGE HAS 2EA HOLES PLUGGED. FOR THE REPAIR AT FUSELAGE SECTION 46, AFT CARGO COMPARTMENT RH STA 1520 FRAME STGR 23R-24R AND STGR 25R-26R, PLANNING TO CONTACT ENGINEERING AFTER 18-JAN-2028 BUT BEFORSDR CALA2026082518894Frame · damagedAFT CARGO RH FREE FLANGE AT STA 1500 B/W STR 26 AND 27 HAS OPEN HOLE NEXT TO PLUG FASTENER. FOR THE REPAIR AT FUSELAGE SECTION 46, AFT CARGO COMPARTMENT RH STA 1500 STGR 26R-27R, PLANNING TO CONTACT ENGINEERING AFTER 18-JAN-2028 BUT BEFORE 04-FEB-2028 FOR THE SDR CALA2026082518892Frame · damagedAFT FARGO COMPARTMENT RH SIDE FR 1520 B/W STGR 23 - 26 FREE FLANGE HAS 2EA HOLES PLUGGED. ACCOMPLISHED REPAIR PER VT MAE EA 757-5360-13-A4585 WITH NO DEVIATIONS.REF EC/RA 5360-02197 PART 1 INTERIM REPAIR FIGURES 1-13.. ACCOMPLISH A PERMANENT REPAIR AT FUSELAGESDR DALA2026082104769Frame · crackedCRACK ON CAP STA Y=1178 CANT AND LONG 17L AT AFT FUSELAGE COMPARTMENT, COMPLIED WITH ER/A 636312-14. (1767796) (AIRCRAFT GROUNDED).SDR CALA2026082118794Frame · damagedAFT CARGO, RT FREE FLANGE AT BS 1500 BTWN STRINGERS 26 - 27 HAS AN OPEN HOLE NEXT TO PLUG FASTENER. REPAIRED PERFORMED ON AFT CARGO, RT FREE FILANGE AT BS A500 BTWN S26 - 27 IAW EC/RA #5360-02196, & EA757-5360-13-A4581 REV-.SDR CALA2026082118792Frame · gougedMAIN CABIN LT FRAME AT BS 1100 BTW STRINGERS 16L-17L GOUGED. ACCOMPLISHED REPAIR IAW ECRA 5340-02283, AND EA 757-53 40-13-A4586 REV-.SDR SWIA2026081977609Frame · corrodedEVALUATION OF POSSIBLE CORROSION ON FRAME, BS 589, STRINGERS 21L - 21R. REMOVED AND REPLACED THE FRAME SECTOR, BS 589 BWTN S21L - 21R IAW SRM 51-42-06.SDR CALA2026082118786Frame · dentedAFT CARGO, FRAME DENTED AT LT BS 1320, BTWN STR 25- 26. REPAIRED THE FRAME BS 1320, STR 25 - 26 IAW UAL ECRA 5360-02198 AND VT MAE EA 757-5360-13-A4576 REV-.SDR CALA2026082018756Frame · dentedFWD CARGO RT BS 680 FRAME DENTED AT S24R. REPAIRED IAW ECRA 5330-07809 AND EA 757-5330-13-A4551 REV-.SDR CALA2026082018744Frame · crackedTHE LT SIDE FRAME WEB BOTTOM HOLE AT BS 1640, IS OUT OF ROUND AND A CRACK INDICATION, BY THE 6 O'CLOCK POSITION. CRACK INDICATION IN THE FRAME WEB LAYER ONLY. DEPTH: 1/16", ACCOMPLISHED WORK IAW EC/RA: 5360-02196 AND EA 757-53 60-13-A4550, REV-.SDR CALA2026082018742Frame · damagedAFT CARGO, RT SIDE FRAME BS 1520 BTWN STR 23 - 26R, FREE FLANGE HAS 2EA HOLES PLUGGED. ACCOMPLISHED REPAIR IAW ECRA 5360-0 2197 AND EA 757-5310-13-A4585 REV-.SDR SWAA2026092345565Frame · dentedDENTED FRAME, BS 500B, STR 25L - 26L IN THE FWD CARGO BAY. MADE & DRILLED A REPAIR FOR FRAME BS 500B, STR 25L - 26L IAW SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1.SDR LR7A2026081503899Stiffener · crackedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BS 491 BELLY STIFFENER CRACKED AT BS 491, RBL 62, WL 140. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, 51-60 & 51-70.SDR IPXA2026091780741Frame · damagedRIGHT WING FR 47 UPPER RADIUS BRACKET HAS ELONGATED HOLES. INSTALLATION OF SPLICE AND SPAR CONTROLLED IN THE EO-18290-JIC004.
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