JASC 5311
Service difficulty reports · 61,504
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 DALA2026101905719Frame · crackedCRACKED FRAME, BS 1580 BTWN S8R & S9R IN THE PAX CABIN. REPAIRED IAW SRM 53-00-07-2R. (1868625)(AIRCRAFT GROUNDED)SDR 2A6R2026101375412Frame · gougedDAMAGE WAS FOUND TO THE SURFACE OF THE RH SIDE WINDOW FRAME PN: L533M1207205 IN THE FORM OF MULTIPLE GOUGES AND CRACKS, REQUIRING REPLACEMENT OF THE WINDOW FRAMESDR 2A6R2026101275802Frame · corrodedDAMAGE TO THE LT EDGE FRAME, IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OTBD FACES OF THE FRAME.SDR 2A6R2026101275801Frame · corrodedDAMAGE TO THE RT EDGE FRAME IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACES OF THE FRAME.SDR YENA2026101500979Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450767. CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED AT FR35 AT LEVEL OF STR30 LH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.156 INCHES APPROX, CRACK POSITION: 6 AND 12 OCLOCK LOSDR YENA2026101500977Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450712. CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 6, CRACK DIRECTION IS 10 O'CLOCK, CRACK DEPTH IS 0.110 INCH, AT FWD GALLEY AREA (1 EA ); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-SDR YENA2026101500956Frame · damagedDURING HEAVY MAINTENANCE, EA A26-843-01 FUSELAGE / NOSE FWD FUSELAGE / FR16 RHS / DOUBLE JOGGLE AREA / HOLE #6 / CRACK DAMAGE – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR DALA2026101305622Frame · crackedCRACK ON OVERWING FRAME STA Y= 674 RH SIDE. OVERWING FRAME STA Y= 674 RH SIDE WAS REPLACED PER CARD 5310-01436-03B. (1857798) AIRCRAFT WAS GROUNDED.SDR DALA2026101905707Frame · damagedTOOL MARK ON FRAME STA. 1280 BTW S-11L TO S-12L AT PAX CABIN. REPAIRED IAW SRM 53-00-07 AND SRM 51-30-01. (1856865)(AIRCRAFT GROUNDED)SDR UIEA2026093000927Frame · damagedPER DWG 624U0072 SHEET 13, 08 FASTENERS ARE SHOWN BETWEEN STR-7 AND STR-8, BUT AT STA 2598 BLKHD HORIZONTAL STABILIZER FWD SIDE, ONLY 04 EA FASTENERS ARE INSTALLED PER SIDE OF BOTH LHS AND RHS FRAME . REWORK CARRIED OUT AT STA 2598 BULKHEAD HORIZONTAL STABILISDR UIEA2026093000929Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 04 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 7 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT LHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORKS CARRIED OUT AT THE LT STA 2598 BULKHEAD FWD ASDR UIEA2026093000930Frame · damagedUNABLE TO PERFORM HFEC INSPECTION FULLY AROUND 06 EA FASTENERS AND 01 EDGE PER SB747-53A2837 PART 8 R0 STEP 1 & 2 OF FIGURE 42 AND DWG 624U0072 SHEET 13 AT RHS STA 2598 BLKHD FWD AND AFT FRAME OUTER CHORD. REWORK CARRIED OUT AT RHS STA 2598 BULKHEAD FWD AND ASDR UIEA2026100300941Frame · crackedDURING HFEC OPEN HOLE INSPECTION ON RHS STA 940 TENSION TIE AND FRAME, FOUND 02 EA FASTENER HOLE ON FRAME AND CHORD WITH CRACK(<P >FRAME SPLICE REPAIR CARRIED OUT ON RHS STA 940 TENSION TIE AND FRAME CRACK 02 FASTENER HOLES AREAS AS PER SRM 53-20-07-2R-8 FIGURSDR DALA2026100905576Frame · damagedFOUND TOOLING DAMAGE ON FUSELAGE FRAME Y908, STR 2R-3R, COMPLIED WITH ER/A 637401-14. (1855981) (AICRAFT GROUNDED).SDR DALA2026100905575Frame · damagedFOUND TOOLING DAMAGE ON FUSELAGE FRAME Y927 BETWEEN STRG L3R TO L4R, ADDITIONAL ENGINEERING AUTHORIZATION ER/A REVISION IS REQUIRED. (1855903) (AICRAFT GROUNDED).SDR CALA2026100920246Frame · crackedRIGHT FRAME 16 DOUBLE JOGGLE AREA HOLE 5, HAS A CRACK INDICATION IN CORNER DOUBLER LAYER AT 6 OCLOCK DIRECTION 100%. ACCOMPLISHED A REPAIR IAW REO L26059, REV IR, AND ECRA 5311-03084, REV A.SDR IPXA2026101946534Fitting · crackedFRAME 12A LT FITTING. 2 EA CRACK NOTED IN ZONE "A" (0.100") & (0.205") AND 1 EA CRACK NOTED IN ZONE "B" (0.130"). REPLACE THE DISCREPANT FITTING PRIOR TO FURTHER FLIGHT IAW EO-23539-REQ003. VERIFIED REMOVAL OF AIR CONDITION DUCTS TWO FR 12A LT. IAW SRM 51-40-SDR DALA2026100905572Frame · crackedCRACK INDICATION FOUND ON FR 68, STRINGER 22R, INNER CAP AREA, COMPLIED WITH ER/A 637146-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 637146-14AD PRI REV 0,1 ITS HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FUSELAGE FRAME, FR 68, STR 22R IAW ER/A SDR UIEA2026092900921Frame · corrodedFRAME AT STATION 400 RBL 60 FOUND WITH SURFACE CORROSION.(<P>WORK ACCOMPLISHED ON SURFACE CORROSION AREA AT MAIN E/E EQUIPMENT CTR CMPT FRAME STA 400 RBL 60 PER EN NO.3779-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2026101305611Frame · not reportedEXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT FRAME BS 1640. REPAIRED IAW ERA 623478-14. (1852278)(AIRCRAFT GROUNDED)SDR CALA2026100620151Frame · cracked1EA HOLE FOUND CRACK ON LH RING CHORD LAYER. LT RING CHORD (1EA) FASTENER HOLE REPAIRED AS PER EC/RA 5711-01240 REV ORIG PART 1 INTERIM REPAIR.SDR REXA2026101601934Frame · corrodedAFTER CORROSION REMOVAL ON FRAME BS 794 FOUND OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-42-21-001-001-A01.SDR 2A6R2026100275410Frame · mechanic errorTWO DRILL MARKS ON THE STRUCTURE UNDERNEATH OF THE TRANSMISSION DECK. THE MARK IS 0.129" IN DIAMETER WITH A DEPTH OF 0.016". THE DAMAGE TO THE FRAME IS 0.128" IN DIAMETER WITH A MAX DEPTH OF 0.018"SDR DALA2026100505497Frame · corrodedCORROSION, SECTION 48 FRAME HAS EVIDENCE OF CORROSION AT FR 81 STGR 19L. REMOVED AND REPLACED CENTER SECTION FRAME AT FR 81 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG: C01401201 REV:-R. (LP# 1839389; AIRCRAFT WAS GROUNDED)SDR CALA2026101320342Frame · crackedFRAME 68, STR 8R, ABOVE TOP FASTENER IN WEB HORIZONTAL CRACK ALONG RADIUS APPROX .400 LONG IAW LCQ N/R 9292113/40113. REPAIRED AFT CABIN RT FRAME 68, STR 8R UPPER FRAME IAW SRM 53-41-12-300-012, PAGE 5, FIG 3. PERFORMED HFEC IAW NTM 51-10-08, WITH CRACK INDICASDR AALA202610142385Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FRAME CRACKED JUST ABOVE L1 DOOR AT STA 312. INSTALL REPAIR PART ANGLE AT STA 312 IAW SRM 53-10-07-2R REPAIR 1.SDR LR7A2026092403950Frame · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND AFT FUSELAGE UPPER FRAME CRACKED AT FS836, RBL12, WL284. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2026092403940Frame · corrodedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MLG WHEEL WELL FRAME ASSEMBLY CORRODED AT FS597, RBL61-66, WL139-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0409.SDR LR7A2026092403923Frame · deformedDURING SCHEDULED C-15 CHECK UNDER WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 777.0E BULKHEAD LOWER CAP FLANGE DEFORMED AT LBL10 TO RBL18, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 IAW SRM 51-60 & 51-70.SDR AALA202610167328Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER INBOARD HOLE DOOR STOP 1 FR 68 RH SIDE CRACK DEPTH 0.125 CRACK DIRECTION 9 OCLOCK. MAINTENANCE ACCOMPLISHMENT PERMANENT REPAIR LOCATED LOWER IB HOLE DOOR STOP 1 FRAME 68 AT LEVEL STRG 22 RH IAW A319SDR REXA2026101601901Frame · crackedCRACKED FRAME, INTERNAL FUSELAGE STRUCTURE BS 333 AND BTWN STR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE OVER BS 333 AND BTWN STRINGERS 2L TO 2R WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR DALA2026092305323Frame · dentedFWD CARGO FRAME DENTED STA 500A BY STRG S24. PERFORMED FRAME REPAIR ON FRAME 500A IAW B737-900 SRM 53-30-07- 2R-1 CAT B REPAIR. (1826194) AIRCRAFT WAS GROUNDEDSDR ABXA20260922431Frame · damagedDURING T/S OF R IDG, FOUND FRAME AT BS 698, STR 22R DAMAGED FROM ELECTRICAL DISCHARGE AC GROUNDED AND TEMP REPAIR WAS ACCOMPLISHED IAW ABX REA-5330-66263-01 AND DEFERRED FOR TRACKING IAW GMM 07.04 FOR 25 FC. INSTALLED PERMANANT REPAIR IAW ABX-REA-66268-00. DSDR REXA2026092301872Frame · corrodedFS 533 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L. RECEIVED AND COMPLIED WITH EA CRJ953-22906 REV IR DATED 09/09/2026.SDR YENA2026092300895Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 RT SIDE. CRACK DIRECTION IS 9 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERFORMED SDR YENA2026092300894Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE 7 LOCATED AT DOUBLE JOGGLE AREA, FR 20 R H SIDE. CRACK DIRECTION IS 3 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERMANESDR YENA2026092300893Frame · crackedDURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN DOUBLE JOGGLE AREA, FR 16. CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00. PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53SDR ABXA20260918425Frame · crackedDURING AIRCRAFT C-5 CHECK, MAINTENANCE DISCOVERED A CRACK IN THE BS 1809.5 BULKHEAD AFT OUTER FRAME BETWEEN S-5L AND S-6L. THIS CRACK IS OUT OF LIMITS IAW SRM AND NO APPLICABLE REPAIR IS GIVEN IN THE SRM. THE BS 1809.5 BULKHEAD AFT OUTER FRAME IS CONSIDERED SDR ABXA20260918421Frame · crackedDURING AIRCRAFT C5 CHECK, MAINTENANCE DISCOVERED CRACK INDICATIONS ON THE RT INNER FRAME AT STA 903.5 WHILE ACCOMPLISHING AN HFEC SURFACE SCAN IAW REF D. AN OPEN HOLE HFEC WAS COMPLETED IAW REF D WHERE IT WAS DISCOVERED THAT THE UPPER MOST FASTENER HOLE HADSDR CALA2026092119626Frame · corrodedAFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.SDR YENA2026091800851Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACKED DIRECTION IS 9OCLOCK, CRACK DEPTH IS 0.120 INCH APPROX., IN FWD CARGO COMPARTMENT (1EA); (RESOSDR YENA2026091800850Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESDR YENA2026091800849Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 2 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TSDR YENA2026091800848Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 11 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456SDR YENA2026091800847Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14SDR YENA2026091800846Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435SDR YENA2026091800845Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FASTENER HOLE 5 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143SDR YENA2026091800844Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 20, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00058 ) ACCOMSDR YENA2026091800843Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 19, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.081 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00059 ) ACCOMPSDR YENA2026091800842Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 14, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.094 IN CH APPROX., IN FWD CARGO COMPARTMENT ALL WORK ACCOMPLISHED ON AEROMAN WO 2026 279/1 NR2026-3
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