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.

SDR SWIA2026072377240Frame Splice · corrodedBS 559.112 FRAME LOWER SPLICE ANGLE WAS CORRODED BTWN STR 26R - 26L. REMOVED AND INSTALLED A NEW FRAME LOWER SPLICE ANGLE IAW DWG 601R32217, REV-L, DWG 601R31003, REV-K, SRM 51-42-21, AND SRM 51-42-06, & COMPLIED SKYWEST TASK CARD 51-900-1003-SKY.Jul 23, 2026 · N969SW · Cndair CL6002B19SDR IPXA2026090225374Frame · corrodedMAJOR REPAIR, AFT CARGO FLOOR FRAME AT STR 28L EXFOLIATED BS 1460. ACCOMPLISHED REPAIR PER EO-98508-REQ1 AND STE-SAA EA 757-5360-01-B0798, REV. I/RJul 23, 2026 · N461UP · Boeing 75724APFSDR IPXA2026091124435Frame · dentedMAJOR REPAIR, AFT CARGO COMPARTMENT INTERNAL FUSELAGE STRUCTURE FRAME HAS A DENT APPROX AT BS 1380 BTW STGR 24L AND STGR 23L, ACCOMPLISH ED THE REPAIR IN ACCORDANCE WITH EO-98452-REQ1 AND STE-SAA EA 757-5360-01-B0800 REV. I/R.Jul 23, 2026 · N438UP · Boeing 75724APFSDR IPXA2026090806015Frame · dentedMAJOR REPAIR, AFT CARGO BAY INTERNAL FUSELAGE STRUCTURE, FRAME HAS 2 EA DENT APPROX AT BS 1500, BTW STGR 25R AND STGR 26R, ACCOMPLISHED REPAIR PER EO-98513-REQ1 AND STE-SAA EA 757-5360-01-B0804, REV. I/RJul 22, 2026 · N455UP · Boeing 75724APFSDR IPXA2026082605349Frame · crackedNDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS. INSTALLED STIFENER REPAIR, DOUBLER AND FRAME STIFENER WAS INSTALLED IAW SRM 51-40-21 AND SRM 57-10-21/201 PER GMM 04-02.Jul 22, 2026 · N144UP · Airbus A300F4622RSDR IPXA2026091787315Frame · crackedCRACKS FOUND ON LT FR47 HORIZONTAL JUNCTION IN HOLE C BEFORE SEALANT CHANNEL AND AFTER SEALANT CHANNEL, CLOCKED AT 6 O'CLOCK. ACCOMPLISH THE REPAIR PER EO-98292-REQ1 AND EA 300-5710-27-A4579 REV -.Jul 21, 2026 · N136UP · Airbus A300F4622RSDR SCNA20260814361Frame · crackedINITIAL INSPECTION: CRACK ON FRAME STA 360 BTW STGR 7R/8R AT PASSENGER CABIN - -(WORK IN PROGRESS)Jul 20, 2026 · N820SY · Boeing 7378FHSDR SWAA2026081794413Frame · crackedCRACKED FRAME, BS 727B, STRINGERS 8L - 9L IN THE PASSENGER CABIN. REPAIRED THE FRAME IAW EA 1-A53-12114, REV 10.Jul 19, 2026 · N499WN · Boeing 7377H4SDR HNAA2026082700800Frame · corrodedSERVICE DOOR AFT, FR 22 CORRODED. REPAIRED IAW SRM 53-00-04, ITEM 6.Jul 17, 2026 · N925AE · Emb EMB145LRSDR IPXA2026082692177Frame Angle · crackedE&E COMPARTMENT AT FR 10 LH Y953 HAS A CRACKED BRACKET AT COCKPIT FLOOR LEVEL . INSTALLED NEW BRACKET " ON E&E COMP. AT FR.10 LH Y953 IAW SRM 51-40-21.Jul 16, 2026 · N136UP · Airbus A300F4622RSDR HNAA2026082400752Frame · crackedCARGO FR 73 HAS POSSIBLE CRACK BETWEEN STGR 16R /17R. R & R FR 73 BTW STGR 14R-17L IAW EMB 145 SRM 51-40-02.Jul 16, 2026 · N935AE · Emb EMB145LRSDR SIMA20260803006Frame · corrodedAFT CARGO FRAME HAS CORROSION AT FR 88 BETWEEN STR 28R - STR 27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON AFT CARGO FRAME 88 BETWEEN STR 28R - 27R IAW E-175 SRM 51-10-03. BLENDED AREA MEASURES L= 6" W=4" H=.027". ORIGINAL THICKNESS .063" IAW E-Jul 16, 2026 · N213NN · Emb ERJ170200LRSDR DALA2026072004241Frame · damagedSHIP 3252 DISC: NIV STEPS 6 AND 16 IF DAMAGE FOUND CONTACT ENGINEERING UPPER FUSELAGE PAX CABIN AT FR 20 RH DOUBLE JOGGLE AREA AT HOLES NR 5 AND 6 FOUND WITH BURR DAMAGE INDICATION AT FRAME LAYER. NOTE: PER MONITOR LOG PAGE 0252469 RELATED TO ER/A #550431-14ADJul 16, 2026 · N352NW · Airbus A320212SDR AALA202608248782Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME SIDE WEB AFT FACE HORIZONTAL FLANGE RADIUS AT FR 68 AND S8R - REPAIRED FRAME PER SRM 53-41-12-300-012Jul 15, 2026 · N195UW · Airbus A321211SDR HNAA2026072000599Frame Angle · crackedCOCKPIT, RT FR 10 ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02.Jul 15, 2026 · N939AE · Emb EMB145LRSDR SWAA2026080553996Frame · crackedCRACKED FRAME, BS 312, S5L & 6L IN THE FWD GALLEY AREA. REPAIRED FRAME IAW M-22-153-01244, SEE TTG8Q01D738K. COMPLETED TASK.Jul 14, 2026 · N953WN · Boeing 7377H4SDR IPXA2026082045373Frame · damagedRH FR58, FWD FASTENER ROW, 6TH HOLE OUTBOARD FROM STRINGER 4 HAS DAMAGE INDICATION OVER 100% FSH.Jul 13, 2026 · N144UP · Airbus A300F4622RSDR YENA2026071700592Frame · crackedDURING HEAVY MAINTENANCE,CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTICAL STRINGER AREA 3 (Y254), CRACK DIRECTION ON ZONE 1: 12 OCLOCK, D1-D2= 0.124 INCH; CRACK DIRECTION ON ZONE 2: 1 OCLOCK, D1-D2= 0.165 INCH, AD RELATED TASK CARD NUMJul 13, 2026 · N520JB · Airbus A320232SDR YENA2026071700591Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN OPEN HOLES (2EA) (ZONE1 AND ZONE 2) ON VERTICAL STRINGER AREA 2 (Y765, FRAME 36), CRACK DIRECTION ON ZONE 1: 1 OCL OCK, D1-D2= 0.137 INCH ; CRACK DIRECTION ON ZONE 2: 12 OCLOCK, D1-D2= 0.148 INCH, AD RELATED Jul 13, 2026 · N520JB · Airbus A320232SDR YENA2026071700590Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON HOLE Ñ2 LOC AT FR35, STR30 RH SIDE, LOWER FU SELAGE. DIRECTION OF CRACK IS AT 7 OCLOCK LOOKING TO IB. CRACK DEPTH I S: 0.320 IN APPROX; (RESOLVED ON W/O: 1435455 TASKCARD: NR-00050 ) REF AEROMAN N/R 289643, Jul 13, 2026 · N520JB · Airbus A320232SDR YENA2026071700586Frame · crackedDURING HEAVY MAINTENANCE, EA A26-473-01 FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT, @ LEVEL OF STGR 30RH / FASTENER HOLE #2 / CRACK DAMAGE – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Jul 13, 2026 · N520JB · Airbus A320232SDR DALA2026071304089Frame · corrodedLEVEL 2 CORROSION, CORROSION WEB FRAME 20 LOCATED LEVEL STR 23R AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC. ON FRAME 20 AT LEVEL STR 23R IN FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11,DWG: D53114392 RELEASE DATE: 01-FEB-19 ISSUE:B00 ANJul 13, 2026 · N378NW · Airbus A320211SDR CALA2026083119102Frame · corrodedBS 977 BELOW FLOOR RT S/W O/B FRAME LWR EDGE (NEAR PRESSURE DECK AREA) FOUND CORRODED. INTERIM REPAIR WAS ACCOMPLISHED ON HAECO NR 3308700, IAW ECRA 5311-03241 PART 1.Jul 11, 2026 · N647UA · Boeing 767322SDR DALA2026071304093Frame · crackedCRACK AT FWD DIRECT OF THE FASTENER HOLE 555 OF FRAME 40 LEFT SIDE. REPAIRED PER ERA 634953-14 REV ORIGINAL. (1693250) AIRCRAFT WAS GROUNDED.Jul 11, 2026 · N801NW · Airbus A330323SDR DALA2026071304092Frame · corrodedFRAME LOWER CHORD AT FR53.3, BETWEEN STGR-49L AND STGR-50L OF THE AFT CARGO BILGE AREA FOUND CORROSION. REPAIRED PER ERA 635421-14. REV ORIGINAL. (1693203) AIRCRAFT WAS GROUNDED.Jul 11, 2026 · N801NW · Airbus A330323SDR IPXA2026082702249Frame · crackedRIGHT FR 47 VERTICAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE N IN ALL LAYERS AT 6 O' CLOCK POSITION. ACCOMPLISHED THE REPAIR PER EO-98116-REQ1 AND EA 300-5710-27-A4553, REV-.Jul 10, 2026 · N144UP · Airbus A300F4622RSDR HNAA2026081900735Frame · crackedLEFT FR79 BTW STR 8-9L HAS CRACKED AROUND RIVET. REPAIRED IAW SRM 53-32-01 ITEM 9.Jul 10, 2026 · N939AE · Emb EMB145LRSDR HNAA2026081900734Frame · crackedLEFT FR 78 HAD TWO CRACKS BTWN S3 - 5L AROUND RIVETS. REPAIRED IAW SRM 53-32-01, ITEM 3.Jul 10, 2026 · N939AE · Emb EMB145LRSDR DALA2026071504147Frame · damagedPERMANENT REPAIR (REPLACEMENT OF FR16 LHS) WAS ACCOMPLISHED AT PREVIOUS M2 CHECK, PER 586145-14 REV D. AT REV E STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. C/A: PER SECTION VII OF 586145-14 REV E, ACCOMPLISH SECTION VII Jul 10, 2026 · N359NB · Airbus A319114SDR DALA2026071504146Frame · damaged*DTE*PERMANENT REPAIR (REPLACEMENT OF FR16 LT) ACCOMPLISHED AT PREVIOUS M2 CHECK, PER 586145-14 REV D. AT REV E STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. *DTE* PER SECTION DTE III OF 586145-14 REV E,FR16 LHS CROSS BEAJul 10, 2026 · N359NB · Airbus A319114SDR DALA2026071504145Frame · damaged*DTE* PERMANENT REPAIR (REPLACEMENT OF FR16 LT) ACCOMPLISHED AT PREVIOUS M2 CHECK, IAW 586145-14 REV D. AT REV E, STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. *DTE* PER SECTION DTE II OF 586145-14 REV E, FR16 LHS DBL JGJul 10, 2026 · N359NB · Airbus A319114SDR DALA2026071304103Frame · corrodedCORROSION WAS FOUND ON THE FR 53.3 FRAME LOWER OUTER CHORD AT Y=819. REPAIRED PER ERA 635421-14. (1692874) AIRCRAFT WAS GROUNDED.Jul 10, 2026 · N801NW · Airbus A330323SDR DALA2026071304102Frame · crackedCRACK WAS FOUND AT HOLE 378 (LHS). REPAIRED PER ERA 635199-14AD. (1692768) AIRCRAFT WAS GROUNDED.Jul 10, 2026 · N801NW · Airbus A330323SDR DALA2026070803988Frame · corrodedCRACK ON FRAME CAP STA 1022 LONG 4LH AT PAX CABIN, COMPLIED WITH ER/A 635304-14. (1687775) (AIRCRAFT GROUNDED).Jul 8, 2026 · N608AT · Boeing 717200SDR SWAA2026081713354Frame · corrodedCORRODED FRAME, BS 303.9, BTWN STR 16L - 17L, WL 210. REPAIRED THE FRAME IAW EA 26-153-01946-WIP1, & EA 26-153-01946.Jul 7, 2026 · N8651A · Boeing 7378H4SDR SWAA2026081273592Frame · crackedCRACKED FRAME, BS 440, STR 8L - 9L. REPAIRED THE FRAME IAW EA 26-153-01892-WIP1, EA 26-153-01892-WIP2, & EA 26-153-01892.Jul 7, 2026 · N7732A · Boeing 7377BDSDR SWAA2026081282516Frame · crackedCRACKED FRAME, BS 360, STR 8R - 9R. REPAIRED THE FRAME IAW EA 26-153-01890-WIP1, EA 26-153-01890-WIP2, AND EA 26-153-01890.Jul 7, 2026 · N7732A · Boeing 7377BDSDR SWAA2026081281556Frame · crackedCRACKED FRAME, BS 400, STR 8R - 9R. REPAIRED THE FRAME IAW EA 26-153-01891-WIP1, EA 26-153-01891-WIP2, EA 26-153-01891-WIP3, AND EA 26-153-01891.Jul 7, 2026 · N7732A · Boeing 7377BDSDR CALA2026083119100Frame · crackedLEFT FRAME 68, STR 22L HORIZONTAL STIFFENER LOWER RADIUS FLANGE CRACKED. INNER FLANGE & HORIZONTAL FLANGE FILLET RADII. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01576 WITHOUT DEVIATIONS.Jul 6, 2026 · N814UA · Airbus A319131SDR IPXA2026082730862Frame · crackedCRACK NOTED AT 6 O'CLOCK AT FWD LAYER, DAMAGE (SCRATCH AND GOUGE) AT ALL LAYERS AT RT WING, FR 40 RADIUS. ACCOMPLISH THE REPAIR IAW EO-98427-REQ1, & EA 300-5710-27-A4584, REV -. MAJOR REPAIR.Jul 6, 2026 · N144UP · Airbus A300F4622RSDR YENA2026070900557Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 COUPLING AREA BULKHEAD ABOVE STR 30RH, CRACK DIREC TION: 07 OCLOCK, D1-D2= 0.073 INCH APPROX AD RELATED TASK CARD NO. A32 0-53-1372-01. ACCOMPLJul 5, 2026 · N568JB · Airbus A320232SDR YENA2026070900556Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 6, OPEN FASTENER H OLE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH , IN FWD CARGO COMPARTMENT (1 EA)(-Y1292); ACCOMPLISHED REPAIR OF CRACK DAMAGES ON THE CENTEJul 5, 2026 · N568JB · Airbus A320232SDR YENA2026070900550Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4,OPEN FASTENER HOLE ON ZONE1, CRACK DIRECTION IS 1 OCLOCK, CRACK DEPTH IS 0.095 INCH,IN FWD CARGO COMPARTMENT (1EA)(-Y254); REF AEROMAN WO 2026-196/1 NR 299010 ACCOMPLISHED PERMANENTJul 5, 2026 · N568JB · Airbus A320232SDR YENA2026070900547Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 1 CRACK LENGTH IS 0.480 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA), REF AEROMAN NR 2026 299167 WO 2026 196/1 Jul 5, 2026 · N568JB · Airbus A320232SDR YENA2026070900546Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO BAY (1 EA)(+Y765). REF AEROMAN NR 2026 299015 WO 2026 196/1 ACCOMPLISHED PERMAJul 5, 2026 · N568JB · Airbus A320232SDR DALA2026070703969Frame · damagedAIRCRAFT 0693, DURING NDT INSPECTION DISCREPANT AREAS WERE FOUND AS FOLLOW: ZONE TO BE INSPECTED BLOCKED BY INTERCOSTAL CLIPS ON FRAME BS 600 BTW LONGERONS 2-3L, ALSO PLUG WAS FOUND ON FRAME BS 620 BTW LONGERONS. 3-4L IAW TASK CARD 5330-2564 STEP: 1. FRAME BJul 5, 2026 · N693DL · Boeing 757232SDR SWAA2026081702482Angle · crackedCRACK ON ANGLE LOCATED BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 SRM 51-10-02, ITEM 9, & DWG 143A7505 SHEET 151REV-.Jul 4, 2026 · N8651A · Boeing 7378H4SDR YENA2026070900545Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.095 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y765); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00041 ) REF Jul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900544Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON TJul 4, 2026 · N568JB · Airbus A320232SDR YENA2026070900543Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON TJul 4, 2026 · N568JB · Airbus A320232
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