L/H AN - [SDR UIEA2026081200745](https://openairdocs.org/sdr/UIEA2026081200745.md): Structure · abnormal · Oct 9, 2026 · N419MC · Boeing 74748EF > WHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 RH, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN- FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U508.(
R/H ANGL - [SDR IXXA20260928001](https://openairdocs.org/sdr/IXXA20260928001.md): Skin · corroded · Sep 28, 2026 · N337AZ · Boeing 767323 > AREA FWD OF ALC, INTERNAL SKIN IS CORRODED BETWEEN STRINGERS 37L-38L APPROX STA 1087. REFERENCE AMES WO N337AZ-44 NR 194024-0100-0093. - [SDR HNAA2026092500911](https://openairdocs.org/sdr/HNAA2026092500911.md): Structure · damaged · Sep 21, 2026 · N932AE · Emb EMB145LR > BIRD STRIKE TO L/H SIDE OF NOSE. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. SEE LOGPAGE 380834-3 FOR DAMAGE MAPPING. - [SDR IPXA2026092251034](https://openairdocs.org/sdr/IPXA2026092251034.md): Unknown · vibration · Sep 21, 2026 · N570UP · Boeing 74744AF > ATB, UNKNOWN NOISE & VIBRATION FROM AIRCRAFT DURING CLIMBOUT. RESULTED IN AIR TURN BACK. - [SDR R61A2026100900298](https://openairdocs.org/sdr/R61A2026100900298.md): Stringer · corroded · Sep 18, 2026 · N221JQ · Emb ERJ170200LR > CENTER FUSELAGE 3 STINGER23R HAS CORROSION AROUND RIVET HEAD AT FRAME 89-90.PERFORMED PERMANENT REINFORCING REPAIR AT CENTER FUSELAGE 3 STINGER 23R FRAME 89-90 REF. ETD2026-170-016498 REV. C - [SDR FDEA202609071273](https://openairdocs.org/sdr/FDEA202609071273.md): Floor Panel · punctured · Sep 7, 2026 · N168FE · Boeing 7673S2F > PUNCTURED FLOOR PANEL 251KFF IN THE MAIN DECK CARGO COMPARTMENT. (ONE LOCATION) FLOOR PANEL 251 KFF, MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025 - [SDR CNMA20260910003](https://openairdocs.org/sdr/CNMA20260910003.md): Fastener · misinstalled · Sep 1, 2026 · N225NE · Boeing 767323 > IMPROPER INSTALLATION OF FASTENER LOWER FUSELAGE STATION 1217 STRINGER 39R - [SDR ABXR2026082800015](https://openairdocs.org/sdr/ABXR2026082800015.md): Support · corroded · Aug 28, 2026 · N1373A · Boeing 76731K > CORROSION ON THE CUTOUT/ SUPPORT STRUCTURE FOR PANEL 195ML, AT THE LEFT UPPER FILLET AREA, AS VIEWED WITH DOOR OPEN. REMOVED CORROSION FROM PNL 195ML'S SUPPORT STRUCTURE, LH UPR FILLET AREA LOST.037 FROM.080 MATERIAL IS FOUND TO BE OUT OF LIMITS. REPAIRED IN - [SDR SWAA2026090191566](https://openairdocs.org/sdr/SWAA2026090191566.md): Panel · delaminated · Aug 25, 2026 · N8546V · Boeing 7378H4 > PANEL 193CR LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R&R 193CR PER AMM 53-51-21. INSPECTED C/A 1. R&R 193CR PER AMM 53-51-21. - [SDR UIEA2026061300476](https://openairdocs.org/sdr/UIEA2026061300476.md): Doubler · corroded · Jul 29, 2026 · N485MC · Boeing 74745EF > NR 3 FUEL AFT BOOST PUMP FOUND CUTOUT DOUBLER CORROSION. DOUBLER FABRICATED AS PER BOEING DWG 65B19560 AND PL, NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED
) - [SDR HNAA2026090100841](https://openairdocs.org/sdr/HNAA2026090100841.md): Floor Support · corroded · Jul 28, 2026 · N664MS · Emb EMB145LR > LEFT FLOOR SUPPORT FROM FR 29 TO FR 35 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, STEP 2.B AND 3.B. - [SDR FDEA202607281046](https://openairdocs.org/sdr/FDEA202607281046.md): Floor Panel · punctured · Jul 28, 2026 · N265FE · Boeing 767300 > PUNCTURE ON 241AGF FLOOR PANEL, MAIN DECK CARGO COMPARTMENT ON 241AGF FLOOR PANEL, MAIN DECK CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025 - [SDR DALA2026071304096](https://openairdocs.org/sdr/DALA2026071304096.md): Not Reported · not reported · Jul 12, 2026 · N801NW · Airbus A330323 > PERFORM SB 57-3081 INSPECTION AT FASTENER HOLE A AND B AT LH FR40 STG 1 AREA. COMPLIED WITH ERA 635419-14 REV ORIGINAL. (1694971) AIRCRAFT WAS GROUNDED. - [SDR FDEA202607070849](https://openairdocs.org/sdr/FDEA202607070849.md): Floor Panel · damaged · Jul 7, 2026 · N298FE · Boeing 76732LF > PUNCTURED FLOOR PANEL 232HFF AT MDCC FLOOR PANEL 232HFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV. 94 DEC 15/2025 - [SDR DALA2026070603921](https://openairdocs.org/sdr/DALA2026070603921.md): Repair · not reported · Jul 3, 2026 · N352NW · Airbus A320212 > ER/A 635410-14 PERFORMS A REPAIR AT FR29 & S-1 LH & RH PER SRM T ASK 53-21-11-300-087. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN THE SOONER OF 40000FC OR 80000FH FROM SECTION I AND EVERY SOONER OF 2900FC OR 5800FH THEREAFTER. ASSOCIATED ER/A 14- - [SDR REXA2026082401568](https://openairdocs.org/sdr/REXA2026082401568.md): Access Panel · corroded · Jul 1, 2026 · N928XJ · Cndair CL6002D24 > CORROSION ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET AND 832FT ALSO ENLOGANTED SUPPORT ANGLE AND BROKEN ACCESS PANEL 832FT. CORROSION WAS REMOVED ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 52-11 - [SDR CALA2026062517341](https://openairdocs.org/sdr/CALA2026062517341.md): Adapter · damaged · Jun 24, 2026 · N12221 · Boeing 737824 > UPPER FUSELAGE STA 385, NR 2 TCAS ANTENNA MOUNTING SURFACE HAS MULTIPLE TOOLING MARKS. REQUIRES EVALUATION. REMOVED AND REPLACED TCAS ANTENNA ADAPTER AT UPPER FUSELAGE IAW DWG: 143A3180 REV V, PL:143A3180 REV J, SRM 51-40-02-0G -0 STEP 4, 51-40-05--0G-0, AMM - [SDR SWAA2026071417058](https://openairdocs.org/sdr/SWAA2026071417058.md): Strap · no discrepancy · Jun 23, 2026 · N555LV · Boeing 7377BD > BS 328 FRAME STRAP CONFIGURATION LOCATED ON S20R TO S22R DOES NOT MATCH WITH FIGURE 15. IAW EA 26-153-01702; THE CONFIGURATION IS ACCEPTABLE. - [SDR YENA2026072900632](https://openairdocs.org/sdr/YENA2026072900632.md): Structure · worn · Jun 21, 2026 · N636JB · Airbus A320232 > DURING HEAVY MAINTENANCE, WEAR VERTICAL MEMBER Y254 FR24A ON FWD CARGO BAY. WO 2026 312/1 NR 2026-391904, REPLACED VERTICAL MEMBER Y254, FR 24A IN FWD CARGO BAY IAW SRM-51-72-11. - [SDR FDEA202606160756](https://openairdocs.org/sdr/FDEA202606160756.md): Floor Panel · punctured · Jun 16, 2026 · N166FE · Boeing 7673S2F > PUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025. - [SDR SWIA2026071476646](https://openairdocs.org/sdr/SWIA2026071476646.md): Antenna · damaged · Jun 15, 2026 · N405SY · Emb ERJ170200LR > COMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 07/13/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO - [SDR SWIA2026071476645](https://openairdocs.org/sdr/SWIA2026071476645.md): Antenna · damaged · Jun 15, 2026 · N405SY · Emb ERJ170200LR > COMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO CHANGE TO WEIGHT AND BALA - [SDR SWIA2026071476643](https://openairdocs.org/sdr/SWIA2026071476643.md): Antenna · damaged · Jun 15, 2026 · N405SY · Emb ERJ170200LR > COMPLY WITH RT SIDE ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT DOUBLER REPAIR TO PREVIOS ANTENNA INSTALLATION AREA REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-5 - [SDR SWIA2026071476642](https://openairdocs.org/sdr/SWIA2026071476642.md): Antenna · damaged · Jun 15, 2026 · N405SY · Emb ERJ170200LR > COMPLY WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) COMPLIED WITH LT SIDE ATG ANTENNA PERMANENT REPAIR. IAW DWG 170-2365-02-314 APPENDIX A. NO CHANGE TO WEIGHT AND BALANCE. - [SDR DALA2026060903436](https://openairdocs.org/sdr/DALA2026060903436.md): Not Reported · corroded · Jun 3, 2026 · N932AT · Boeing 717200 > IN REFERENCE TO NRC 706 WIP NR 9, CORROSION OUT OF LIMITS AT RT SIDE. REPAIRED IAW SRM 53-00-55 (1628543) (AIRCRAFT GROUNDED) - [SDR CALA2026060816920](https://openairdocs.org/sdr/CALA2026060816920.md): Skin · damaged · Jun 3, 2026 · N61886 · Boeing 737924ER > FUSELAGE SKIN DAMAGE AT STR20L- STA847-867. REMOVED DAMAGE TO EVALUTE 11.75 L X 5.125 W REMOVED DAMAGE AREA OF THE FUSELAGE SKIN. RECTANGLE WITH THE SIDES PARALLEL AND PERPENDICULAR TO THE STRINGER SRM 53-00-01-2R-36 REPAIR INSTRUCTIONS 4. (C) ADD EMP:U347143 - [SDR SWIA2026052676303](https://openairdocs.org/sdr/SWIA2026052676303.md): Antenna · out of limits · May 26, 2026 · N181SY · Emb ERJ170200LR > COMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 06/20/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO EF - [SDR UIEA2026040800165](https://openairdocs.org/sdr/UIEA2026040800165.md): Skin · corroded · May 23, 2026 · N477MC · Boeing 74747UF > M/D STA 1241 FWD STR-16R - STR 17R INT SKIN FOUND CORROSION(CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.290" L:4" X W:1" X D: 0.015", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FU - [SDR DALA2026052803225](https://openairdocs.org/sdr/DALA2026052803225.md): Not Reported · cracked · May 22, 2026 · N891AT · Boeing 717200 > REF STEP #8 RC AA5530-01048-02 AND AD 2018-10-08 4 CRACK INDICATIONS BELOW ZFS = 52.267. REPAIRED ON ERA 564482-14AD (8342877) (AIRCRAFT GROUNDED) - [SDR FDEA202605150612](https://openairdocs.org/sdr/FDEA202605150612.md): Floor Panel · cracked · May 15, 2026 · N289FE · Boeing 7673S2F > PUNCTURES ON FLOOR PANEL 231DFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 231DFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R REPAIR GENERAL PARAG 4B FIG 201 SHEET 2 REV. 94 DEC15/2025 - [SDR VNAA20260512012](https://openairdocs.org/sdr/VNAA20260512012.md): Panel · cracked · May 12, 2026 · N541EA · Cndair CL6002C10 > CORROSION AND CRACK ON DIVERTER PANELS (3EAS). REPAIRED PER EA 5321-2026-0502 REV - -, EA 5321-2026-0501 REV - - AND EA 5321-2026-0488 REV -. - [SDR SCNA20260504180](https://openairdocs.org/sdr/SCNA20260504180.md): Door Frame · damaged · May 3, 2026 · N8011A · Boeing 737800* > FWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING WITH SHARP EDGES. DEBURRED SHARP EGES LOCATED AT FWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING IAW AC5300-1 SECTION 11-2-2 REV K DATED 05-11-2018 - [SDR QXEA2026051100108](https://openairdocs.org/sdr/QXEA2026051100108.md): Seat Track · corroded · Apr 27, 2026 · N635QX · Emb ERJ170200LR > RIGHT HAND SEAT TRACK AT STATION 17-23 HAS CORROSION IN MULTIPLE SPOTS. REMOVED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-40-08 AND RESTORED FINISH. - [SDR QXEA2026051100113](https://openairdocs.org/sdr/QXEA2026051100113.md): Not Reported · corroded · Apr 20, 2026 · N635QX · Emb ERJ170200LR > FRAME 19 LBL 11 CORROSION AT SCRFW HOLE ON BEAM. AFTER REWORK FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW ARM 53-10-10-02-01. RESTORED FINISH. - [SDR FDEA202604180486](https://openairdocs.org/sdr/FDEA202604180486.md): Fitting · cracked · Apr 18, 2026 · N669FE · Airbus A300F4605R > UPPER FUSELAGE - RH "N" HOLD FOUND CRACKED AT FR47 BTW STGR25 AND STGR26. REPAIRED THE CRACKED RH HOLE N IN UPPER FUSELAGE FR47 BTW STGR25 AND STGR26 PER EA 6-5310-T0387082. TITLE: FUSELAGE - MAINFRAME - FR47 RH HOLE N CRACK REPAIR BETWEEN S-24R AND S-26R - [SDR IXXA20260408001](https://openairdocs.org/sdr/IXXA20260408001.md): Skin · dented · Apr 8, 2026 · N255CM · Boeing 767223 > DENT NOTED AT FUSELAGE SKIN LOWER SIDE BETWEEN BS 390 TO BS 412. AND BETWEEN STRINGERS S-38R AND S-37R. REF XTREME AVIATION NRC 166 - [SDR MASA20260406061](https://openairdocs.org/sdr/MASA20260406061.md): Floorbeam · corroded · Apr 1, 2026 · N87318 · Emb ERJ170200LR > LH FLOORBEAM SPLICE PLATE AT FR 89, LBL 11 FOUND CORRODED. CORRODED CFIII LH FLOOR BEAM SPLICE PLATE AT FR 89, LBL 11 REPLACED WITH NEW AND INSTALLED IAW SRM 51-43-03 RELATED TO YQG- NRC#4502579_2000_0286 - [SDR VNAA202604010050](https://openairdocs.org/sdr/VNAA202604010050.md): Bracket · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 > FWD CARGO MACHINED BRACKET IS CORRODED AT FS 533, BETWEEN STGR 27 AND STGR 26L. REMOVED AND REPLACED FWD CARGO BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. - [SDR VNAA202604010060](https://openairdocs.org/sdr/VNAA202604010060.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 > HN00250014 DISCREPANCY: RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 847 AND FS 977. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 850.55-977.00 IAW CRJ 700 AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01. - [SDR CALA2026033014920](https://openairdocs.org/sdr/CALA2026033014920.md): Paint · missing · Mar 23, 2026 · N67052 · Boeing 767424ER > DURING INSPECTION FOUND MISSING PAINT ON NOSE RADOME. DURING PHASE 2 INSPECTION FOR LIGHTNING STRIKE. FOUND MISSING PAINT ON RADOME MEASURING APPROX. 1 SQ INCH. NO STRUCTURAL DAMAGE FOUND. APPLIED CLEAR TAPE TO EXPOSED AREA PER EC/RA 5350-02074. ACCOMPLISH A - [SDR VNAA20260501006](https://openairdocs.org/sdr/VNAA20260501006.md): Skin · dented · Mar 15, 2026 · N617NN · Bombdr CL6002D15 > FUSELAGE SKIN DENT WITHIN 6341.13 FH AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DENT DAMAGE ON FUSELAGE SKIN BTW FS942.00 - FS954.00 AND STR21L - STR22L WAS REPAIRED PER CRJ-900 REO 690-53-51-539 REV.-- - [SDR FDEA202603100332](https://openairdocs.org/sdr/FDEA202603100332.md): Floor Panel · cracked · Mar 10, 2026 · N162FE · Boeing 7673S2F > CRACK ON 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4-B FIG. 201 SHEET REV.94. - [SDR VNAA2026031013903](https://openairdocs.org/sdr/VNAA2026031013903.md): Not Reported · not reported · Mar 6, 2026 · N617NN · Cndair CL6002D24 > FUSELAGE STRUCTURE BETWEEN FS333.0 - FS265.0 AND STR 17R- 26R. / PERFORMED REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-00-638. - [SDR TSAA2026022800002](https://openairdocs.org/sdr/TSAA2026022800002.md): Not Reported · cracked · Feb 28, 2026 · N360WA · Boeing 737301 > CRACK FOUND 3 INCH FWD OF BS 727E ALONG STR 22R - [SDR IPXA2026030611423](https://openairdocs.org/sdr/IPXA2026030611423.md): Floor Support · corroded · Feb 9, 2026 · N581UP · Boeing 7474R7F > MAJOR REPAIR, CORRODED SUPPORT, MAIN DECK FLOOR SUPPORT AT BS 1580, LBL 110. REMOVED MAIN DECK CARGO FLOOR PANEL IAW AMM 53-21-02-404-006, REV 115. INSTALLED MAIN DECK CARGO FLOOR PANEL. - [SDR SWIA2026022575315](https://openairdocs.org/sdr/SWIA2026022575315.md): Dome Nut · damaged · Feb 5, 2026 · N613SK · Cndair CL6002C10 > SCREW SHANK STUCK IN THE RH ATC L-BAND ANTENNA DOME NUT (MARKED). (C-CHECK RO 02/22/2026)REMOVED THE RH ATC L-BAND ANTENNA INNER DOUBLER. COMPLIED WITH REO 670-53-21-2810 DATED: 2026-02-08 REV: -A REPAIR FOR ELONGATED HOLE AND TOOLING & CORROSIOIN DAMAGE TO - [SDR UIEA2026013000024](https://openairdocs.org/sdr/UIEA2026013000024.md): Junction Box · corroded · Feb 5, 2026 · N439GT · Boeing 747409F > JUNCTION BOX COVER FOR RIGHT HAND BODY GEAR HAS CORROSION ON LOWER EDGE.(
REPAIRED AREA OF CORROSION ON RH BODY GEAR LOWER EDGE OF JUNCTION BOX PER SRM 51-70-13-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
) Next page: https://openairdocs.org/jasc/5300/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 = '5300' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/jasc/5300/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.