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 CALA2026081718667Frame · crackedFRAME 68, STR 22L INNER CAP & WEB FLANGE HAS A CRACK INDICATIONS 5CM LONG AND 100% SH IAW AAR LCQ N/R 9296334/20334. REFERENCE LOG PAGES 9953498, 9962986 AND 9963050 FOR DIP AND WORK ACCOMPLISHMENTS.SDR 2A6D20260814Frame · corrodedCORROSION ON THE COLLECTIVE SPLIT FRAME ON FWD AND AFT SIDE OF OPENING.SDR SWIA2026081377251Frame Splice · corrodedFOUND RT SPLICE AT FRAME, BS 605, STR 20R CORRODED. REMOVED AND REPLACED THE FRAME SPLICE IAW DWG 601R36026, REV AF, & SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026081377236Frame Angle · corrodedFOUND CORROSION ON FRAME BS 605 REINFORCEMENT ANGLE. REMOVED AND INSTALLED A NEW FRAME REINFORCEMENT ANGLE IAW DWG 601R36026, REV-AF, & SRM 51-42-06 AND COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR CALA2026082718958Frame · crackedLEFT FR16 HOLE NO.2,NO.4,NO.6 HAVE A CRACK IN FRAME LAYER AT 11 O'CLOCK POSITION AND HOLE NR 19 HAS AN OUT OF ROUN D CONDITION IN FRAME LAYER. FR 16 HOLE 19 ACCOMPLISHED ON LP 9642983, FR 16 HOLE 2 ACCOMPLISHED ON LP 9643006, AND FR 16 HOLE 4 ACCOMPLISHED ONSDR CALA2026082718956Frame · crackedLEFT FRAME 16 HOLE NR 2 REPAIRED ON NR 30576/9290576 REQUIRES DIP LOGPAGE GENERATION FOR REPETITIVE INSPECTION REQUIREMENTS. GENE RATED BY V945000 PER AAR LCQ NR 9291035/31035.ESFR INFORMATION UPDATE LH FRAME 16 HOLE #2 REPAIRED IAW 53-11-12-300-012. CRACK WASDR CALA2026082718954Frame · crackedLEFT FRAME 16, HOLE NR 4 REPAIRED ON NR 3576/9290576. LT FRAME 16 HOLE NR 4 REPAIRED IAW 53-11-12-300-012. CRACK WAS FOUND DURING THE ISBS REF FIG 1 SHT 1 STEP 2. CRACK FOUND IN FRAME LAYER PER FIG 002 REF FIG 1 SHT 1 STEP 3. CRACK WAS FOUND WITHIN CONCERNEDSDR CALA2026082718952Frame · crackedLEFT FRAME 16 HOLE NR 19, REPAIRED ON NR 30576/9290576. LH FRAME 16 HOLE NR 19, REPAIRED IAW 53-11-12-300-012. CRACK WAS FOUND DURING THE ISBS REF FIG 1 SHT 1 STEP 2. CRACK FOUND IN FRAME LAYER PER FIG 002 REF FIG 1 SHT 1 STEP 3. CRACK WAS FOUND WITHIN CONCERSDR CALA2026081418623Frame · crackedLEFT FRAME 68, STGR 22L INNER CAP AND WEB FLANGE HAD CRACK INDICATIONS, 5CM LONG AND 100% SH. PERFORMED REPAIR ON INNER CAP IAW EC/RA 5341-01580.SDR CALA2026081418621Frame · crackedFRAME 68, STRINGER 22R INNER CAP AND WEB FLANGE HAD A CRACK INDICATION, 5CM LONG AT 100% SH. PERFORMED REPAIR ON INNER CAP IAW EC/RA 5341-01580.SDR DALA2026081404665Frame · crackedFOUND CRACK IN FR16 LT, OUTBBOARD FLANGE, UPPER AREA ABOVE DOOR STOP 7, AT HOLE NR 6, COMPLIED WITH ER/A 567055-14. (1753281) (AIRCRAFT GROUNDED).SDR REXA2026090401772Frame · corrodedSTRINGER 21L CORRODED FWD OF BS 319. REMOVED CORROSION FROM FS319 BETWEEN STR 21L AND STR 20L IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS MEASUREMENTS OF REWORKED AREAS IAW NDTM PART 1, 51-20-004-270-A01, REV-37. FOUND LOWEST REMAINING THICKNESS TO SDR REXA2026081001535Frame · corrodedFS 501 FRAME IS CORRODED AT STGR 18L. REMOVED FS501 STUB FRAME BETWEEN STGR 18L - STGR 17L IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW FRAME IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR SWIA2026080877260Frame · corrodedBS 605, FRAME FLANGE CORRODED BTWN STR 23L - 26R. REMOVED AND INSTALLED THE FRAME IAW DWG 601R36026, REV AF, DWG 601R35005, REV AG, SRM 51-42-21, AND SRM 51-42-06. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWAA2026091001033Frame · corrodedCORROSION ON FRAME AT BS 303 LBL55 WL210. REWORKED PER EA 26-153-02140 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-02140-DTI.SDR SWAA2026091089137Frame · crackedCRACKED FRAME AT BS 312 WL 284 BETWEEN STR 6L AND STR 5L TASK COMPLETED I.A.W EA M-22-153-01244. BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L CCN TTG8Q01DQHBF.SDR SWIA2026080377541Frame · corrodedFS1015 FOUND TO HAVE CORROSION BETWEEN STGR 27 TO 25L, STGR 22L TO 21L REQUIRES REPLACEMENT C-CHECK RO 10062026REPLACED FRAME FS1015 BETWEEN STRINGER 26R TO 19L IAW REO 670-53-61-2744 REV-- DATED 2026-08-11 AND CRJ-700 SRM 51-42-06-001-001-A01 AND 51-24-36SDR SWAA2026090857428Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2026-457102 PERFORMED PERMANENT REPAIR FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA I.A.W B737-800 EA M-22-153-01244.SDR DALA2026080304466Frame · crackedCRACK ON CAP OF FRAME STA Y# = 1,178 BTW LONG 14RH TO 15RH AT AFT ACCESORIES COMPARTMENT. REPAIRED PER ER/A 635890-14. (1731671) AIRCRAFT WAS GROUNDED.SDR REXA2026091101819Frame · corrodedCORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT CORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CRJ 900 SRSDR CALA2026082718948Fitting · crackedBS 663.75 FRAME FITTING & FAIL SAFE STRAP AT S18A, CRACKED AT RT TOP LOWER AFT FASTENER ON FRAME FITTING, AFTER CLEAN UP LOCKED BY TOMC FOR MX FERRY TO RFD. FERRY FLIGHT COMPLETED ACCOMPLISHED REPLACEMENT OF RIGHT BS 663.75 REAR SPAR FRAME ASSEMBLY IAW ECRA SDR AALA202609058025Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA AT FR 16 BETWEEN S4R AND S14R - REPLACED FRAME PER EA 377945SDR AALA202609058236Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA AT FR 16 BETWEEN S4L AND S14L - REPLACED FRAME PER EA 377920SDR REXA2026090401771Frame · corrodedFRAME BS 379 REQUIRES REMOVAL BETWEEN S20-S25R TO ACCESS CORROSION. UPON ADDITIONAL EVALUATION BS 379 BETWEEN S20 - 25R HAS EXFOLIATE CORROSION FOUND 100 PERCENT MATERIAL LOSS, OUT LIMITS IAW SRM 53-21-23-101-003-A02. INSTALLED NEW FRAME BS 379 BTWN S20 - 2SDR REXA2026081001534Frame · corrodedFS 501 FRAME IS CORRODED BETWEEN STGR 22L AND STGR 26R. UPON FURTHER INVESTIGATION, DISCREPANCY ADDRESSES 2 SEPARATE FRAME SECTORS. BS 501 FRAME HAS WIDESPREAD CORROSION ON MULTIPLE ELEMENTS BETWEEN STGR 22L AND STGR 26L, IS FOUND TO BE OUT OF LIMITS IAW SRM SDR UIEA2026061700517Frame · cracked1EA CRACK FOUND ON BS 1000 STR 38R - STR 39R APPROX 0.750". CHORD CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A506 REV 10 PART 4. NO FURTHER DEFECTS NOTED.SDR UIEA2026063000558Doubler · crackedRH STA 820 U/D TENSION TIE ATT. FRAME DOUBLER 2EA FASTENER HOLES CRACKED. FRAME DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW FRAME DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME DOUBLER INSTALLED AS PER SRM 51-40-02.& NO FURTHER DEFECTS NOTED.SDR UIEA2026070700576Frame · crackedLH STA 880 UPPER DECK FRAME FOUND 1EA FASTENER HOLE CRACK(<P>FRAME CRACK AREA REPAIRED AS PER RI-53-20-18366 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700578Frame · crackedRH STA 880 UPPER DECK FRAME FOUND 2EA FASTENER HOLES CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18365 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700581Frame · crackedLEFT BS 840 UPPER DECK FRAME ONE EACH FASTENER HOLE CRACKED. FRAME CRACK AREA REPAIRED AS PER RI-53-20-18364 REV A. NO FURTHER DEFECTS NOTEDSDR UIEA2026072000613Frame · crackedSTA 900 LH UPPER DECK FRAME 1EA FASTENER HOLE CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18410 REV A. NO FURTHER DEFECTS NOTED</P>)SDR AALA202610022391Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOCATED ON CHORD. STA 727 STR 25L - 26L. REPAIRED IAW EA377884, EA378953, BOEING DRAWING 146A0060, AND SRM 51-40-02-0G.SDR SIMA20260728001Frame · crackedFR07 CRACKED THROUGH 2 RIVETS ON LH SIDE BETWEEN STR 12L AND STR 13L. (MAJOR REPAIR). PERFORMED PERMANENT REPAIR TO FR 07 BETWEEN STR 12L AND STR 13L IAW ERS-EJ-53MR-5487.SDR VNAA202610060029Frame · corrodedCORROSION ON FRAME STA 1088 BTW STGR 27RH AND 26RH AT AFT CARGO COMPT. FRAME STA 1088 BTW STGR 27RH AND 26RH AT AFT CARGO COMPT WAS REPAIRED PER REO 690-53-61-1809 REV. - -SDR SWAA2026082589157Frame · crackedBS 312 FRAME UPPER ANGLE CRACKED AT LBL 33 BETWEEN S5L & S6L., PERFORMED EA M-22-153-01244 IN CC TTG8Q01DDXQX.SDR SWAA2026082138473Stub Frame · crackedCRACK INDICATION FOUND ON BS 639, LBL 45.57 STUB BEAM STRAPS, REPLACED THE STRAP ASSY IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 144A1715, SHEET 9, REV A.SDR SWIA2026072577232Frame Angle · corrodedFOUND CORROSION ON FRAME BS 589 REINFORCEMENT ANGLE. REPLACED CORRODED FRAME BS 589 REINFORCEMENT ANGLE WITH NEW IAW DWG 601R36025, REV-P, & SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR CALA2026082718946Frame · crackedFRAME 16 RT DOUBLE JOGGLE HOLES NR 1, 6, & C HAD CRACK INDICATIONS DURING ACCOMPLISHMENT OF TC 17-5311-1-2837. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5311-02463, PART 1, ITEM 1. IAW ECRA PART 1 ITEM 2.SDR CALA2026082718944Frame · crackedEA 5341-01231 004, RT SIDE FRAME 68 AT STR 22 INNER CAP & WEB FLANGE IS CRACKED 6.50 INCH LONG. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01578 WITHOUT DEVIATIONS. ORIGINAL DISCREPANCY UNDER LCQ NR 9292250 AND ECRA 5341-01231. CARRIED TO ACCOMPLISHSDR AALA202608183581Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED UPPER CORNER FRAME FITTING AT FR 68 AND S8R - REPLACED UPPER CORNER FRAME FITTING PER SRM 51-42-11SDR SWIA2026072477272Frame Splice · corrodedFOUND CORROSION ON LT SPLICE AT FRAME FS 589, STR 20L. REPLACED THE FRAME SPLICE IAW DWG 601R36025, REV P, AND SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026072477264Frame Splice · corrodedFOUND CORROSION ON RT FRAME SPLICE, BS589, STR 20R. REPLACED THE FRAME SPLICE, IAW DWG 601R36025, REV P, AND SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR DALA2026072804347Frame · dentedDENT ON FRAME STA 1440 BTW S-26L TO S-25L AT AFT CARGO COMPARTMENT. REPAIRED PER PRI 635477-14AD REV. 3 AND PER ER/A 635477-14AD (1717896)(AIRCRAFT GROUNDED)SDR DALA2026072804345Frame · crackedMLG WHEEL WELL, LH SIDE, CRACK ON FRAME WEB AT BS 1147, LBL 70, WL 175. REPAIRED PER PRI 635758-14 REV. 3 AND ER/A 63578-14 (1716741)(AIRCRAFT GROUNDED)SDR VNAA20260726464Frame · corrodedFWD SIDE OF FRAME BS 319 CORRODED BETWEEN STR 24L-25L. REPLACED FRAME SECTION IAW SRM 53-00-06-201-006-A01.SDR VNAA20260726463Frame · corrodedFWD SIDE OF FRAME BS 319 CORRODED BETWEEN STR 24L-25L. REPLACED FRAME SECTION IAW SRM 53-00-06-201-006-A01.SDR VNAA2026072441Frame · corrodedBS 549 FRAME IS CORRODED BETWEEN STR 18L - 19L. REPAIRED IAW REO 670-53-31-1189, REV-.SDR VNAA2026072439Frame · corrodedBS 565 FRAME IS CORRODED BETWEEN STR 18L - 16L. REPAIRED IAW REO 670-53-31-1189, REV--, AND REO 670-53-31-1189, REV-.SDR VNAA2026072423Frame · corrodedBS 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STR 20L TO 21L. UPON REVIEW OF UT MEASUREMENTS FOUND .064 REMAINING ORIGINAL THICKNESS IS .080 REMOVED .016 FOUND DAMAGE TO BE OUT OF LIMITS OF SRM 53-00-00-101-001-A01. REPAIRED BS 280 CIRCUMFERENTIAL JOINT IASDR SWIA2026072377255Frame · corrodedBS 589, FRAME WEB AND ATTACH FLANGE ARE CORRODED BETWEEN STR 18 - 22R. REMOVED AND INSTALLED A NEW LOWER FRAME SECTION IAW DWG 601R36025, REV P, DWG 601R35005, REV AG, AND SRM 51-42-06.
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