JASC 5311

Service difficulty reports · 61,537

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 UIEA2025032800410Frame · crackedLH BS 2231 FRAME STR 16 ONE EACH FASTENER HOLE FOUND 2EA CRACK.(<P>STR 16 AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR UIEA2025032800411Frame · crackedLH BS 2231 FRAME STR 17 ONE EACH FASTENER HOLE FOUND CRACK(<P>STR 16L AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. (WORK DETAIL REFER WO.4545643 (5.738)). NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR J6BA2025070100417Frame · corrodedBS 409 AT S26L THERE IS SIGNS OF CORROSION. REPAIRED FRAME SECTION FS409.00 BETWEEN STRG 24L TO STGR 27 IAW CRJ-200 MHIRJ REO 601R53-21-3741 REV-- 2025-06-16Apr 17, 2025 · N886AS · Cndair CL6002B19SDR IPXA2025052562688Skin · crackedCRACK FOUND IN HOLE T ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93642-REQ1 AND EA 300-5710-27-A3893 REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH Apr 17, 2025 · N125UP · Airbus A300F4622RSDR SCNA20250505154Frame · crackedSTA 312 FRAME HAS A CRACK ON THE EDGE BETWEEN STR 5-6 LH - STA 312 FRAME REPAIRED IAW SRM 53-10-07-2R-1 BETWEEN STA 5-6 LHApr 17, 2025 · N827SY · Boeing 7378F2SDR VNAA202504170109Frame · corrodedFS319 BETWEEN STGR25L & 25R FOUND TO BE CORRODED IN MULTIPLE LOCATIONS ON ATTACH FLANGE. CORRECTIVE ACTION: INSTALLED COMPLETE FRAME LOWER SEGMENT PN: SH670-31355-1S FS319 BETWEEN STGR21L & 23R IAW CRJ700 SRM 51-42-06-001-001-A01 SH670-31355-1SApr 17, 2025 · N508AE · Cndair CL6002C10SDR VNAA202504170077Frame · corrodedFS295 FRAME LOWER ELEMENT AND WEB CORRODED FROM STGR 20L TO 22L. CORRECTIVE ACTION: FS295 FROM STGR 20L TO 22L FOUND TO BE OUT OF LIMITS PER NOTE 1: DAMAGE IS ALLOWED ONLY IN ONE ELEMENT AT A GIVEN CROSS-SECTION. REMOVED DAMAGE AT ONE ELEMENT MUST NOT OVERLAP Apr 17, 2025 · N508AE · Cndair CL6002C10SDR AALA202508129470Frame · crackedAIRCRAFT IN BASE MAINTENANCE: R1 DOOR CUTOUT UPPER CORNER FRAME CRACKED AT FR 16. REPAIRED CORNER FRAME PER EA 364901Apr 16, 2025 · N183UW · Airbus A321211SDR SWIA202507210416Frame · corrodedFRAME FS 1051.30 CORRODED BETWEEN STGR 27 AND STGR 25LH #29987334 (C-CHECK RO 07/18/2025)REPAIRED FRAME AT FS1051.30 BETWEEN STGR 27 AND STGR 25LH IAW REO 670-53-61-2500 REV -- 2025-05-26. COMPLIED WITH ALL STEPS OF REO 670-53-61-2500 REV -- 2025-05-26. COApr 16, 2025 · N723EV · Cndair CL6002C10SDR AALA202506098403Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE AT FR 68 AND S8L. REPAIRED FRAME PER EA 364308.Apr 16, 2025 · N172US · Airbus A321211SDR IPXA2025052546594Skin · crackedCRACK FOUND IN HOLE S ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025052546546Skin · crackedCRACK FOUND IN HOLE E ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025052546559Skin · crackedCRACK FOUND IN HOLE G ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622RSDR DALA2025042103078Frame · dentedSHIP 6710 DENT ON FRAME AT STA 1480 AND S-26L AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00292 REPAIR CATEGORY "B" ON FRAME AT STA 1480 AND S-26L AFT CARGO COMPARTMENT WAS PERFORMED PER B757-200 SRM 53-00-07-2R PROCEDURE 5 REPAIR 5. (0916132)Apr 16, 2025 · N6710E · Boeing 757232SDR FDEA202504160598Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 D P2. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUApr 16, 2025 · N676FE · Airbus A300F4605RSDR CALA2025042304165Frame · crackedDOUBLE JOGGLE AT RT FR 20 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER, 3 DIRECTION, 100% S.H. REPAIRED HOLE #6 AT RH FR20 DOUBLE JOGGLE WITH BUSHING AND RPR WASHER IAW SRM 53-11-12-300-012. FINAL REAM .2800 THIS IS A CAT B. COMPLETED DOUBLE JOGGLE AT RH FR Apr 15, 2025 · N462UA · Airbus A320232SDR N6WA2025041505Frame · corrodedCORROSION ON FRAME AT FS319 BETWEEN STRINGER 25L AND STRINGER 25R IS OUT OF LIMITS. REPAIRED FRAME AT FS319 BETWEEN STRINGER 25L AND STRINGER 25R IAW GOJET EO C550-53MR-049.Apr 15, 2025 · N540GJ · Cndair CL6002C11SDR N6WA2025041504Frame · corrodedCORROSION ON FS349 BETWEEN STRINGER 25R AND STRINGER 25L. REPAIRED FS349 BETWEEN STRINGER 25R AND STRINGER 25L IAW GOJET EO C550-53MR-049.Apr 15, 2025 · N540GJ · Cndair CL6002C11SDR IPXA2025052507731Frame · crackedCRACK FOUND IN HOLE G ON FR47 LH HORIZONTAL JUNCTION. COMPLIED WITH STEP 15 OF PRELIM 1 EA-300-5710-27-A3893.Apr 14, 2025 · N125UP · Airbus A300F4622RSDR CALA2025041603887Frame · crackedWHILE PERFOMING REINSPECT OF RH FR35 STR 30 FOUND PREVIOSLY REPAIRED HOLE #2 TO BE CRACKED. ACCOMPLISHED IMPROVED INTERIM REPAIR PER ECRA 5331-02334 REV B. PART 1A STEP 1. REF LPS 9144384 ASSOCIATED DIP LIMITS.Apr 14, 2025 · N459UA · Airbus A320232SDR AALA202504152612Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND PICKLE FORK FITTING LOCATED AT BS 663.75, RBL 64. REPLACED FRAME PER EA 363398.Apr 14, 2025 · N906AN · Boeing 737823SDR CALA2025041503881Frame · crackedR/H FR16 DOUBLE JOGGLE HOLE "A" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE A R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WIApr 13, 2025 · N818UA · Airbus A319131SDR CALA2025041503880Frame · crackedR/H FR16 DOUBLE JOGGLE HOLE "C" HAS A CRACK INDICATION AT 9 O'CL OCK IN THE FRAME LAYER. REPAIRED HOLE C R/H FRAME 16 DOUBLE JOGGLE WITH BUSHING AND WASH ER IAW SRM 53-11-12-300-012. FINAL HOLE SIZE REAMED WITH BUSING INSTALLED IS .2175. HFEC ACCOMPLISHED WApr 13, 2025 · N818UA · Airbus A319131SDR SWIA20250613412Frame · corrodedFS589.00 BETWEEN STRINGERS 19L AND 18R HAS MISSING PAINT AND SURFACE CORROSION ON FLANGE/WEB. (C-CHECK RO 06/12/2025)COMPLIED WITH REO 601R-53-61-8328 DATED: 2025-05-06 REV:A REPAIR FOR CORROSION DAMAGE TO FRAME FS589.00 BTW STR18R-19R. COMPLIED WITH TASK CARApr 12, 2025 · N954SW · Cndair CL6002B19SDR IPXA2025052383131Frame · crackedMDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. INSTALLED NEW SHEAR WEB I.A.W A300-600 SRM 51-40-21.Apr 12, 2025 · N125UP · Airbus A300F4622RSDR SWAA2025052057360Stub Frame · crackedAFTER REMOVE SEAL DEPRESSOR CRACK INDICATION FOUND ON STUB FRAME LOCATED ON BS 296.5 BTW STR 8 TO S-9R AT FWD GALLEY DOOR AREA. CRACK LENGTH : 0.395 INCHES APPROX AT PASSENGER CABIN. 2025-250429<[01] REPLACED STUB FRAME AND FASTENERS LOCATED ON BS 294.5 AT FWDApr 12, 2025 · N7747C · Boeing 7377BDSDR CALA2025041703947Frame · delaminatedDENT ON FRAME AT STA 760 STR 24 RH, REPAIRED DENT ON FRAME AT STA 760 STR 24RH PER 757-200 SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL II. INSPECTION THRESHOLD 37500 OR 50000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT INSPECTIONS AT 12000 FLIGHT CYCApr 12, 2025 · N57111 · Boeing 757224SDR CALA2025041503847Frame · dentedSUPPORT TASK: FRAME STA 1420 STR 25LH HAS A DENT. REPAIRED IAW B757-200 SRM 53-00-07-2R-5 FIG 201 DETAIL III DIP # 4483385 CREATED IAW B757-200SRM 53-00-07-2R-5 FIG 201 TABLE III RII VERIFIED REPAIR PERFORMEDApr 12, 2025 · N57111 · Boeing 757224SDR SIMA20250411002Frame · corrodedFR 88 CORRODED BETWEEN STGR 28R-27R (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION FROM FR88 BETWEEN STGR 27R-28R IAW EMB 175 SRM 51-10-03. DAMAGE FOUND TO BE ACCEPTED AS IS IAW ENVOY ERS-EJ-5300-5174Apr 11, 2025 · N231AN · Emb ERJ170200LRSDR DALA2025041502941Window Frame · cracked(LOG 0907998) LH NO. 3 FLIGHT COMPARTMENT WINDOW FRAME / LOWER FWD CORNER / CRACK. REPAIRED PER ERA 625473-14.Apr 11, 2025 · N3755D · Boeing 737832SDR CALA2025041503855Frame Splice · gougedAFT CARGO COMP. FRAME SPLICE STA RH BTW STRG 23R-25R WITH GOUGES(3EA). ENTRY FOR SDR REPORTING FRAME SPLICE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FRA ME SPLICE FABRICATED ON VT/MAE TRAV T25/1808559 IAW B757-200 SRM 53-00-07-1A-1 FIG 1 51-40-02Apr 11, 2025 · N57111 · Boeing 757224SDR DALA2025041402901Frame · dentedSHIP 6712 AGING AIRCRAFT INSPECT, STA 580 BTW S25L-S24L FRAME DENTED. CORRECTIVE ACTION: REPAIRED DENT ON FRAME AT STA 580 S25L-S25L IAW B757 SRM 53-00- 07-2R-5 FIG 201. (0907701)Apr 11, 2025 · N6712B · Boeing 757232SDR DALA2025041402900Frame · dentedSHIP 6712 FRAME DENTED AT ST 1340 S26 L. CORRECTIVE ACTION: REPAIRED ALC FRAME AT STA 1340 S26L IAW B757 SRM 53-00-07-2R-5. (0907699)Apr 11, 2025 · N6712B · Boeing 757232SDR DALA2025041402898Frame · dentedSHIP 6712 FRAME DENTED AT STA 1400 S26 L. CORRECTIVE ACTION: REPAIRED FRAME IAW B757 SRM 53-00-072R-5 REPAIR 5. (0906943)Apr 11, 2025 · N6712B · Boeing 757232SDR DALA2025041402896Frame · dentedSHIP 6712 AGING AIRCRAFT INSPECT, STA 580 BTW S25L-S24L FRAME DENTED. CORRECTIVE ACTION: REPAIRED DENT ON FRAME AT STA 580 S25L-S25L IAW B757 SRM 53-00- 07-2R-5 FIG 201. (0906963)Apr 11, 2025 · N6712B · Boeing 757232SDR DALA2025041402866Frame · damaged(LOG 0906295) ACCOMPLISH AMDS 5311-01251-02B R/H STA 1TJ FRAME INNER CHORD, 737 REPAIR. COMPLIED WITH AMDS CARD 5311-01251-02B. INSTALL A NEW SHIM R/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-53A1402 REV 1.Apr 10, 2025 · N3773D · Boeing 737832SDR DALA2025041402865Frame · damaged(LOG 0906280) ACCOMPLISH AMDS 5311-01251-02A L/H STA 727 FRAME INNER CHORD, 737 REPAIR. COMPLIED WITH AMDS CARD 5311-01251-02A. INSTALL A NEW SHIM L/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-53A1402.Apr 10, 2025 · N3773D · Boeing 737832SDR CALA2025041103706Frame · wornFWD CARGO FWD BULKHEAD SUPPORT STRUT WORN/HAS PLAY AT UPPER ATTACH POINT. REMOVED AND REPLACED NEW VERTICAL MEMBER ASSY ON FWD CARGO FWD B ULK HEAD SUPPORT STRUT IAW A320 AMM 25-54-81-400-801-A.Apr 10, 2025 · N464UA · Airbus A320232SDR SWIA2025090900409Frame · corrodedLOWER FRAME SECTION AT FS379 BETWEEN STR 23R - STR 21R IS CORRODED (29947635) (C-CHECK RO 09/07/2025)INSTALLED NEW LOWER FRAME SECTION AT FS379 BETWEEN STR 25R - STR 20R REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-32280 REApr 9, 2025 · N896SK · Cndair CL6002D24SDR SWI2025F00773Frame · corrodedCORROSION FOUND ON REINFORCING ANGLE OF FRAME FS549.00 BETWEEN STGR 17L AND 18L. (29947227). (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLEAT PN: SH670-33796-1 AT FS549 BETWEEN STGR 17 AND STGR 18 PER CRJ 900 SRMS 51-42-06-001-001-A01 AND 51-42-22-001-001-A0Apr 9, 2025 · N800SK · Cndair CL6002D24SDR SWAA2025051957299Stub Frame · crackedCRACK STUB FRAME LOCATED ON BS 294.5 AND RBL53 LOWER POSITION AT FWD GALLEY AREA 2025-250257<[01] ON STEP 7 AND 8. PERFORMED PERMANENT REPAIR ON STUB FRAME LOCATED ON BS294.5 AND RBL53 LOWER POSITION AT FWD GALLEY AREA I.A.W. B737-700 SRM 53-10-15-2R-7.Apr 9, 2025 · N7747C · Boeing 7377BDSDR CALA2025041703946Frame · dentedFRAME STA 1500 STR 26LH HAS A DENT. REPAIRED STA 1500 STR 26LH FRAME IAW B757-200 SRM 53-00-07-2R-S-DETAIL II. ACCOMPLIHSED ON VT NR 124726. INSPECTION THRESHOLD AT 37500 FLIGHT CYCLES AFTER REPAIR OR 50000 AIRCRAFT FLIGHT CYCLES WHICHEVER COMES FIRST. INSPApr 9, 2025 · N57111 · Boeing 757224SDR N6WA2025040903Frame · corrodedCORROSION AT FS501 BETWEEN STRINGER 24L - STRINGER 25L. PERFORMED FRAME FLANGE REPAIR AT FS501 BETWEEN STRINGER 24L - STRINGER 25L IAW CRJ SRM 53-00-06.Apr 9, 2025 · N542GJ · Cndair CL6002C11SDR N6WA2025040901Frame · corrodedCORROSION ON FRAME AT FS310 BETWEEN STRINGER 25R AND STRINGER 25L. PERFORMED REPAIR ON FRAME AT FS310 BETWEEN STRINGER 25R AND STRINGER 25L IAW GOJET EO C550-53MR-049 REV O.Apr 9, 2025 · N542GJ · Cndair CL6002C11SDR SWI2025F00781Frame · corrodedCORROSION FOUND ON FRAME FS533.00 BETWEEN STGR 17L AND 18L WEB PORTION AND ATTACHING FLANGE. (29941771) (C-CHECK RO 06/29/2025)PERFORMED SPLICE REPAIR ON FRAME FS533.00 BETWEEN STGR 17L AND 18L. REF CRJ-900 SRM 53-00-06-201-001-A03, CRJ-900 SRM 51-42-06-001-Apr 8, 2025 · N800SK · Cndair CL6002D24SDR SWAA2025051922939Frame · corrodedCORROSION FRAME ON BS 303.9 AND LBL52 WL210 FWD GALLEY AND LAV. PERFORMED REPAIR ON FRAME LOCATED BS 303.9 LBL 55 WL 208.3 AT FWD GALLEY AREA IAW EA 25-153-01057-WIP1.Apr 8, 2025 · N7747C · Boeing 7377BDSDR SWIA2025043008Frame · damagedDURING REWORK OF TWO TEMPORARY INSTALLED FASTENERS DUE TO LIGHTNING STRIKE DAMAGE LOCATED JUST AFT OF FUSELAGE FRAME FS11 AND ON STRG 24L WE HAVE FOUND AN OUT OF LIMIT CONDITION TO FUSELAGE SKIN, INTERNAL SKIN SPLICE STRAP AND STRG 24L SPLICE SECTION. THIS HASApr 8, 2025 · N174SY · Emb ERJ170200LRSDR N6WA2025040813Frame · corrodedCORROSION ON FRAME AT FS295 BETWEEN STRINGER 26R - STRINGER 26L. REPAIRED FRAME AT FS295 BETWEEN STRINGER 26R AND 26L IAW GOJET EO C550-53MR-049.Apr 8, 2025 · N542GJ · Cndair CL6002C11SDR SWIA2025070100407Frame · corrodedCORROSION ON FRAME IN MULTIPLE LOCATIONS AT FS613 BETWEEN STGR 26L AND STGR 26R. (C-CHECK RO 06/29/2025)PERFORMED FRAME FLANGE SPLICE REPAIR ON FS613 BETWEEN STRG27 AND STRG26R REF CRJ900 SRM 53-00-06-201-001-A03 AND CRJ-900 SRM 51-42-06-001-001-A01. COMPLIEApr 7, 2025 · N800SK · Cndair CL6002D24SDR 8G962025052300407Frame · crackedFRAME CRACKED ALONG BOTTOM FLANGE THROUGH BOLT HOLE FOR GUST LOCK CASTING TO LIGHTNING HOLE AT FS 434 BL 0 ROOF LEVEL. CRACK MEASURES 1.5" IN LENGTH.Apr 7, 2025 · N415BT · Cndair CL2156B11215
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