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.

SDR DALA2024071207077Frame · not reportedSHIP 684 DTE, ERA 618976-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 1260 BETWEEN S-26R & S-27R. CORRECTIVE ACTION: REF ERA 618976-14Jul 11, 2024 · N684DA · Boeing 757232SDR CALA2024071102012Frame · corrodedB767-53-3-7036 CAB - STA977 BELOW FLOOR RH S/W O/B FRAME CHORD LWR EDGE (NEAR PRESSURE DECK AREA) FOUND CORROSION . CABIN RH STA977 FRAME OUTER CHORD AT WL186 INTERIM REPAIRED AS PER ECRA5311-03241 REV - PART 1 - INTERIM REPAIR WORK DETAIL ATTACHED FORM 44.000Jul 11, 2024 · N647UA · Boeing 767322SDR AALA202409104052Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB AFT FACE ON HORIZONTAL FLANGE RADIUS AT FR 68 AND S8R. REPAIRED FRAME PER SRM 53-41-12-300-012.Jul 10, 2024 · N189UW · Airbus A321211SDR SWAA2024080711239Frame · crackedCRACK FOUND DURING HFEC OPEN HOLE INSPECTION OF R/H BS727 INNER CHORD AT STR-18A; LOCATED AT LOWER HOLE; IN MOST O/B LAYER OF STACK-UP AT 9:00 POSITION<[01] REMOVED AND REPLACED STA 727 R/H FRAME INNER CHORD AT S-18A; AFT LOWER FITTING AS PER 51-40-02; DWG#146Jul 10, 2024 · N478WN · Boeing 7377H4SDR DALA2024071907275Stub Frame · corroded(LOG 0448923) CORROSION ON STA 320 STUB FRAME AT STR 23L. REMOVED AND REPLACED STUB FRAME AT STA 320 STR 21L TO STR 23L IAW B737 SRM 51-40-02-OG AND BOEING DWG # 141A1180.Jul 10, 2024 · N392DA · Boeing 737832SDR YENA2024071100986Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON HOLE C, FR 16 DOUBLE JOGGLE AREA, CRACK DIRECTION AT 9 OCLOCK RH SIDE, CRACK DEPTH 0.145 INCHES, CONFIRM EACH INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-00; (RESOLVED ON W/O: 1280173 TASKCARD: NR-00024)Jul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100985Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON HOLE A, FR 16 DOUBLE JOGGLE AREA, CRACK DIRECTION AT 3 OCLOCK RH SIDE, CRACK DEPTH 0.135 INCHES, CONFIRM EACH INDI CATION USING BOROSCOPE VIEW AS PER NTM 51-90-00; (RESOLVED ON W/O: 1280173 TASKCARD: NR-00025Jul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100984Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE, DOOR STOP #7 , HOLE H1. CRACK POSITION IS: 7 OCLOCK , DEPTH IS 0.177 INCHES APPROX; REF AEROMAN WO:2024 38/1 WCC:2024-332725. EVALUATED CRACK INDICATION ON FRAME 16 RH SIDE, DOOR STOP #7 , HOLE H1Jul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100983Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP #7 , HOLE H1. CRACK POSITION IS: 7 OCLOCK , DEPTH IS 0.181 INCHES APPROX; REF AEROMAN WO:2024 38/1 WCC:2024-332726. EVALUATED CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP #7 , HOLE H1Jul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100982Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP #7 , HOLE H3. CRACK POSITION IS: 6 OCLOCK , DEPTH IS 0.171 INCHES APPROX; REF AEROMAN WO:2024 38/1 WCC:2024-332727.EVALUATED CRACK INDICATION ON FRAME 16 LH SIDE, DOOR STOP #7 , HOLE H3.Jul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100977Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON INNER FRAME SEGMENTS 1 (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 843 FWD RH SIDE. CRACK LENGTH = 0.100 INCHES, ON PASSENGER CABIN; REF AEROMAN WO# 2024 38/1 WCC# 2024-332586.ACCOMPLISHED THE REINFORCEMEJul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100975Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON INNER FRAME SEGMENTS 1 (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 833 FWD LH SIDE. CRACK LENGTH = 0.120 INCHES, ON PASSENGER CABIN; REF AEROMAN WO# 2024 38/1 WCC# 2024-332585. ACCOMPLISHED THE REINFORCEMJul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100974Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON INNER FRAME SEGMENTS 1 (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 834 AFT LH SIDE. CRACK LENGTH = 0.100 INCHES, ON PASSENGER CABIN; REF AEROMAN WO: 2024 38/1 WCC# 2024-332587. ACCOMPLISHED THE REINFORCEMJul 10, 2024 · N655JB · Airbus A320232SDR YENA2024071100973Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON INNER FRAME SEGMENTS 1 (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 844 AFT RH SIDE. CRACK LENGTH = 0.110 INCHES, ON PASSENGER CABIN; REF AEROMAN WO: 2024 38/1 WCC# 2024-332588. ACCOMPLISHED THE REINFORCEMJul 10, 2024 · N655JB · Airbus A320232SDR DALA2024071107033Frame · crackedSHIP 3158 CRACK INDICATION WAS FOUND ON FR16RH, FASTENER HOLE 7. CORRECTIVE ACTION: REPAIRED PER ER/A 592899-14 . (0440092)Jul 10, 2024 · N358NB · Airbus A319114SDR DALA2024071107026Frame · crackedSHIP 3158 CRACK INDICATION WAS FOUND ON FR16RH, FASTENER HOLE 7. CORRECTIVE ACTION: REPAIRED PER ER/A 592899-14AD. (0440315)Jul 10, 2024 · N358NB · Airbus A319114SDR AALA202409042141Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RIGHT-HAND HOLE 7 ON DOUBLE JOGGLE AREA, CRACK DIRECTION AT 3 O'CLOCK. ACCOMPLISHED TIME LIMITED REPAIR ON FR 16 RIGHT-HAND BETWEEN STR 5R TO DOOR STOP #5 (PARTIAL FRAME REPLACEMENT) ON DOUBLE JOJul 9, 2024 · N746UW · Airbus A319112SDR DALA2024071006985Frame · crackedCRACK ON FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00499: FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROC 1 REPAIR 1. (LP #0438169)Jul 9, 2024 · N965AT · Boeing 717200SDR AALA202407108487Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE "A" ON DOUBLE JOGGLE AREA AT FR 16 LEFT AND DOOR STOP FITTING #7. REPLACED FRAME PER EA 354355.Jul 8, 2024 · N740UW · Airbus A319112SDR DALA2024070806926Frame · crackedSHIP 3132 CRACK INDICATION FOUND ON AROUND FASTENER HEAD LOC FR35LH AND BTW STR 30LH TO STR31LH. CORRECTIVE ACTION: REPAIRED PER ER/A 617994-14AD. (0435048)Jul 8, 2024 · N332NB · Airbus A319114SDR SWIA202409160812Frame · crackedFS 333.00 FRAME HAS CRACK AT APPROXSTR 01 (C-CHECK RO 9/15/2024) COMPLIED WITH REPAIR TO FRAME AT FS 333.00 APPROX. STR 01 REF. REO 690-53-21-1807 REV -- DATED 22-JUL-2024. ALL STEPS OF REO COMPLIED WITH. COMPILED WITH SKYWEST TASK CARD 51-900-1002-SKYJul 7, 2024 · N693CA · Cndair CL6002D24SDR SWAA2024082610227Stub Frame · crackedCRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-420826<[01] TOOL USED ON STEP 5 AND 6: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25;[02] REPAIRED STUB FRAME LOCATED ON BS 294.5 AT LEVEL STR 17R AT FJul 7, 2024 · N262WN · Boeing 7377H4SDR SWAA2024082610106Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-420816<[01] REPAIRED FRAME LOCATED STA 312 BTW STR5L TO STR6L FWD GALLEY AREA IAW EA NO M-22-153-01244 REV B . SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPAIRED FRAME LOCATED STA 312 BTW STRJul 7, 2024 · N262WN · Boeing 7377H4SDR IPXA2024072202331Frame · dentedDENT ON FRAME IN STA 720 RH BETWEEN STR 23R AND 25R. INSTALLED FRAME REPAIR, IAW SRM 53-00-07-2R-5, DETAIL I, MAT.Jul 7, 2024 · N418UP · Boeing 75724APFSDR DALA2024070906944Frame · damaged(LOG 0433894) BURN DAMAGE AT FRAME 500I STR 6L 2".0 DWN .035W .075L .005D. REPAIRED PER ERA 619139-14.Jul 7, 2024 · N802DN · Boeing 737932ERSDR SWI202409160808Frame · corrodedCABIN INTERIOR FS847.00+32 BETWEEN STGR26L AND STGR26R HAS CORROSION ON AFT SIDE FLANGE AS MARKED (C-CHECK RO 9/15/2024) REMOVED AND REPLACED LOWER FRAME FS847.00+32. BETWEEN STGR20L AND STGR20R REF. CRJ900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-00Jul 6, 2024 · N693CA · Cndair CL6002D24SDR DALA2024070806901Frame · crackedSHIP 3132 CRACK INDICATION FOUND OPEN HOLE 19 FRAME 16LH. DOUBLE JOGGLE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 617934-14AD REV. ORIGINAL. (0431213)Jul 6, 2024 · N332NB · Airbus A319114SDR DALA2024070806900Frame · crackedSHIP 3132 CRACK INDICATION FOUND OPEN HOLE 5 FRAME 16LH. DOUBLE JOGGLE AREA. CORRECTIVE ACTION: REPLACED PER ER/A 617934-14AD REV. ORIGINAL. (0431196)Jul 6, 2024 · N332NB · Airbus A319114SDR WX0A2024081932158Frame · cracked(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0082: S/M PASSENGER CABIN, CRACK FOUND AT FR 68 STR 22 RH CRACK FOUND ON WEB HORIZONTAL FLANGE / PASSENGER CABIN FR 68 AT STR 22R/H & STOP FITTING #1 REPAIRED AS PER AIRJul 5, 2024 · N220NV · Airbus A320214SDR SWAA2024080909411Frame · crackedCRACK FRAME STA 312 AND BETWEEN S-5L TO S-6L ON UPPER FWD CORNER THE FORWARD GALLEY SERVICE DOOR 841 AT PASSENGER CABIN 2024-415005. CORRECTED DESCRIPTION: CRACK FRAME STA 312 AND BETWEEN S-5L TO S-6L ON UPPER FWD CORNER THE FORWARD ENTRY DOOR 831 AT PASSENGERJul 5, 2024 · N8322X · Boeing 7378H4SDR DALA2024070806919Frame · crackedSHIP 3137 CRACK INDICATION ON FRAME 68 RH SIDE ON OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE #4 LOWER INBOARD LOC. DOOR STOP FITTING #1 FR68 RH AS PER A319 SRM 53-41-12-300-008 AND SRM 53-41-1Jul 5, 2024 · N337NB · Airbus A319114SDR SWAA2024081309153Frame · corrodedCORROSION ON 303 FRAME; LBL 58; WL 209-211.<[01] REMOVED CORROSION ON FRAME BS 303.9 LBL 55 WL 209-211 IN A 3.1' X 1.4' X .037' FROM ORIGINAL THICKNESS OF .330'. FOUND TO BE OUT OF LIMITS. ACCOMPLISHED REPAIR TO BS 303.9 FRAME IAW EA 24-153-01913;[02] VERIFIEDJul 4, 2024 · N257WN · Boeing 7377H4SDR DALA2024070806871Frame · corrodedSHIP 684 CORROSION ON FRAME STA. 1620 BTW S-28L TO S-28R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00730 NEW SECTION FRAME STA. 1620 BTW BTW S-25L TO S-25R WAS FABRICATED PER B757-200 SRM 51- 40-05-0G AND DWG 146N1031 REV.G. AND REPLACED PER Jul 4, 2024 · N684DA · Boeing 757232SDR SWIA20240809703Frame Splice · damagedFRAME 319 SPLICE REPAIR REQUIRED FOR FOM OF STR 25R REPLACEMENT (C-CHECK RO 8/7/2024) PERFORMED REPAIR ON DAMAGE FRAME 319 BETWEEN STR 25L TO STR 24R IAW CRJ 700 SRM 51-41-02,SRM -51-42-06,SRM 53-00-06,REO 670-53-21-1308 REV -- DATED 2016-09-06,SRM 51-4Jul 3, 2024 · N705SK · Cndair CL6002C10SDR YENA2024071100959Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME LOC DOOR STOP 7 FR16RH HOLE H1. CRACK DEPTH 0.063 INCH AND DIRECTION 9 O'CLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00025) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR STOP 7 FR16 RJul 3, 2024 · N569JB · Airbus A320232SDR DALA2024070506802Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACKED ON CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-20Jul 3, 2024 · N942AT · Boeing 717200SDR YENA2024070800959Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 7 O'CLOCK AND CRACK DEPTH IS 0.092 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00026) REF AEROMAN WO 2024 1Jul 2, 2024 · N566JB · Airbus A320232SDR YENA2024070800958Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.076 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00027) REF AEROMAN WO 2024 1Jul 2, 2024 · N566JB · Airbus A320232SDR YENA2024070800957Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.076 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00027) REF AEROMAN WO 2024 1Jul 2, 2024 · N566JB · Airbus A320232SDR YENA2024070800955Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE CROSSBEAM SPLICING AREA, AT OPEN FASTENER HOLE H2, CRACK DIRECTION IS 1 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00046) REF AEROMAN WO 2024 159/1 NR 2024-277058, PEJul 2, 2024 · N566JB · Airbus A320232SDR YENA2024070800954Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE UPPER DOUBLE JOGGLE AREA, AT OPEN FASTENER HOLE C, CRACK DIRECTION IS 3 OCLOCK, CONFIRM INDICATION USIN G BOROSCOPE VIEW AS PER NTM 51-90-00, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1301763 TAJul 2, 2024 · N566JB · Airbus A320232SDR YENA2024070800953Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FACE OF FR35 AT LEVEL OF STGR 30L. CRACK LENGTH 1.5 INCH APPROX; (RESOLVED ON W/O: 1301763 TASKCARD: NR-00052) REF AEROMAN WO 2024 159/1 NR 2024-277195 PERFORMED REPAIR AT FRAME 35 BTW STGR 30L TO STGR 31Jul 2, 2024 · N566JB · Airbus A320232SDR WX0A2024070532106Frame · cracked(AIRCRAFT NOT GROUNDED) FOUND .125IN CRACK EMMINATING FROM THE NUMBER 10 RIVET BETWEEN STRG Z+780 AND Z+950 / ACCOMPLISHED REPAIR OF CRACK IAW TD/81428247/006/2024#A"Jul 2, 2024 · N307NV · Airbus A319112SDR DALA2024070506782Frame · crackedCRACK (0.100IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 907 BTW S-8L & S-9L. FUSELAGE FRAME STA 907 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-03A.Jul 2, 2024 · N399DA · Boeing 737832SDR DALA2024070306743Frame · crackedCRACK ON CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT. CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.Jul 2, 2024 · N942AT · Boeing 717200SDR DALA2024070306742Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK ON CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.Jul 2, 2024 · N942AT · Boeing 717200SDR DALA2024070306741Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK AT FRAME STA 715 AND L27R CANTED KEEL AREA. CORRECTIVE ACTION: FRAME STA 715 AND L27R CANTED KEEL AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP 0425118)Jul 2, 2024 · N942AT · Boeing 717200SDR DALA2024070206724Frame · crackedCRACKS ON FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 1 TABLE 203 FIG 201.Jul 2, 2024 · N942AT · Boeing 717200SDR DALA2024070306736Window Frame · crackedSHIP 3140 CRACK INDICATION WAS FOUND AFFECTING THE RH WINDSHIELD FRAMING. CORRECTIVE ACTION: REPAIRED PER ERA 617687-14AD. (0425745)Jul 2, 2024 · N340NB · Airbus A319114SDR SWAA2024080707754Frame · crackedCRACK ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN 2024-405134<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED REPAIR ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN IAW EA 24-Jul 1, 2024 · N482WN · Boeing 7377H4
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