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 FIGUR - [SDR DALA2026100905576](https://openairdocs.org/sdr/DALA2026100905576.md): Frame · damaged · Oct 9, 2026 · N920AT · Boeing 717200 > FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y908, STR 2R-3R, COMPLIED WITH ER/A 637401-14. (1855981) (AICRAFT GROUNDED). - [SDR DALA2026100905575](https://openairdocs.org/sdr/DALA2026100905575.md): Frame · damaged · Oct 9, 2026 · N920AT · Boeing 717200 > FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y927 BETWEEN STRG L3R TO L4R, ADDITIONAL ENGINEERING AUTHORIZATION ER/A REVISION IS REQUIRED. (1855903) (AICRAFT GROUNDED). - [SDR CALA2026100920246](https://openairdocs.org/sdr/CALA2026100920246.md): Frame · cracked · Oct 8, 2026 · N824UA · Airbus A319131 > RIGHT 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 IPXA2026101946534](https://openairdocs.org/sdr/IPXA2026101946534.md): Fitting · cracked · Oct 7, 2026 · N146UP · Airbus A300F4622R > FRAME 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 DALA2026100905572](https://openairdocs.org/sdr/DALA2026100905572.md): Frame · cracked · Oct 7, 2026 · N357NW · Airbus A320212 > CRACK 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 UIEA2026092900921](https://openairdocs.org/sdr/UIEA2026092900921.md): Frame · corroded · Oct 7, 2026 · N486MC · Boeing 74745EF > FRAME AT STATION 400 RBL 60 FOUND WITH SURFACE CORROSION.(
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.
) - [SDR DALA2026101305611](https://openairdocs.org/sdr/DALA2026101305611.md): Frame · not reported · Oct 6, 2026 · N593NW · Boeing 757351 > EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT FRAME BS 1640. REPAIRED IAW ERA 623478-14. (1852278)(AIRCRAFT GROUNDED) - [SDR CALA2026100620151](https://openairdocs.org/sdr/CALA2026100620151.md): Frame · cracked · Oct 4, 2026 · N78008 · Boeing 777224 > 1EA 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 REXA2026101601934](https://openairdocs.org/sdr/REXA2026101601934.md): Frame · corroded · Oct 3, 2026 · N296PQ · Cndair CL6002D24 > AFTER CORROSION REMOVAL ON FRAME BS 794 FOUND OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-42-21-001-001-A01. - [SDR 2A6R2026100275410](https://openairdocs.org/sdr/2A6R2026100275410.md): Frame · mechanic error · Oct 2, 2026 · N110VU · Urocop EC135T2 > TWO 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 DALA2026100505497](https://openairdocs.org/sdr/DALA2026100505497.md): Frame · corroded · Sep 29, 2026 · N310DU · Airbus BD5001A11 > CORROSION, 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 CALA2026101320342](https://openairdocs.org/sdr/CALA2026101320342.md): Frame · cracked · Sep 28, 2026 · N479UA · Airbus A320232 > FRAME 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 INDICA - [SDR AALA202610142385](https://openairdocs.org/sdr/AALA202610142385.md): Frame · cracked · Sep 26, 2026 · N959NN · Boeing 737823 > AIRCRAFT 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 LR7A2026092403950](https://openairdocs.org/sdr/LR7A2026092403950.md): Frame · cracked · Sep 24, 2026 · N403LC · Lkheed 382G > DURING 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 LR7A2026092403940](https://openairdocs.org/sdr/LR7A2026092403940.md): Frame · corroded · Sep 24, 2026 · N403LC · Lkheed 382G > DURING 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 LR7A2026092403923](https://openairdocs.org/sdr/LR7A2026092403923.md): Frame · deformed · Sep 24, 2026 · N403LC · Lkheed 382G > DURING 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 AALA202610167328](https://openairdocs.org/sdr/AALA202610167328.md): Frame · cracked · Sep 23, 2026 · N12028 · Airbus A319115 > AIRCRAFT 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 A319 - [SDR REXA2026101601901](https://openairdocs.org/sdr/REXA2026101601901.md): Frame · cracked · Sep 22, 2026 · N296PQ · Cndair CL6002D24 > CRACKED 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 DALA2026092305323](https://openairdocs.org/sdr/DALA2026092305323.md): Frame · dented · Sep 22, 2026 · N888DU · Boeing 737900ER > FWD 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 GROUNDED - [SDR ABXA20260922431](https://openairdocs.org/sdr/ABXA20260922431.md): Frame · damaged · Sep 22, 2026 · N220CY · Boeing 767383 > DURING 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. D - [SDR REXA2026092301872](https://openairdocs.org/sdr/REXA2026092301872.md): Frame · corroded · Sep 22, 2026 · N810SK · Cndair CL6002D24 > FS 533 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L. RECEIVED AND COMPLIED WITH EA CRJ953-22906 REV IR DATED 09/09/2026. - [SDR YENA2026092300895](https://openairdocs.org/sdr/YENA2026092300895.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 > DURING 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 YENA2026092300894](https://openairdocs.org/sdr/YENA2026092300894.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 > DURING 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. PERMANE - [SDR YENA2026092300893](https://openairdocs.org/sdr/YENA2026092300893.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 > DURING 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 53 - [SDR ABXA20260918425](https://openairdocs.org/sdr/ABXA20260918425.md): Frame · cracked · Sep 18, 2026 · N762CK · Boeing 7673P6 > DURING 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 ABXA20260918421](https://openairdocs.org/sdr/ABXA20260918421.md): Frame · cracked · Sep 18, 2026 · N762CK · Boeing 7673P6 > DURING 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 HAD - [SDR CALA2026092119626](https://openairdocs.org/sdr/CALA2026092119626.md): Frame · corroded · Sep 18, 2026 · N819UA · Airbus A319131 > AFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583. - [SDR YENA2026091800851](https://openairdocs.org/sdr/YENA2026091800851.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 > DURING 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); (RESO - [SDR YENA2026091800850](https://openairdocs.org/sdr/YENA2026091800850.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 > DURING 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); (RE - [SDR YENA2026091800849](https://openairdocs.org/sdr/YENA2026091800849.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 > DURING 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 T Next page: https://openairdocs.org/jasc/5311/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/jasc/5311/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.