JASC 5311

Service difficulty reports · 61,537

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 IPXA2025040998346Frame · crackedNLG W/W FRAME ON THE LANDING GEAR DOOR, RIGHT SIDE AFT OF THE HINGE N2 WITH A CRACK DOT 07-043.REMOVED FRAME ON THE LANDING GEAR DOOR, RIGHT SIDE AFT OF THE HINGE N2 IAW B757-200 SRM 51-40-02-0G-0.INSTALLED NEW FRAME ON LANDING GEAR RH SIDE AFT OF THE HINGE N2Mar 27, 2025 · N443UP · Boeing 75724APFSDR HALA20250331021Frame · corrodedNUMEROUS CORROSION ON FRAME 1138 (M). CUTOUT APPROX 4 INCHES OF OUT OF LIMITS CORROSION ON STA 1138 FRAME BETWEEN LEFT L29 AND L30, HFC CUTOUT NO CRACKS NOTED. REMOVED REMAINING S/C AT STA 1138 FRAME , CLEANED AND TREATED PRIME AND PAINTED PER SRM 51-10-04 MMar 27, 2025 · N486HA · Boeing 717200SDR REXA2025032800362Frame · corrodedFS 549 IS CORRODED BETWEEN STGR 26L AND STGR 27 IN THE FWD BAGGAGE BAY REMOVED AND REPLACED FRAME SECTION BETWEEN STGR 26L AND STGR 27 IAW ENDEAVOR EA CRJ753-18457 REV--IR DATE 02/19/2025.Mar 27, 2025 · N669CA · Cndair CL6002C10SDR SWAA2025050553967Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 0.875 INCH AT PASSENGER CABIN 2025-232168<[01] REPLACED STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND BTW STR 6R TO STR 10R AT FWD Mar 26, 2025 · N290WN · Boeing 7377H4SDR SWAA2025042109838Stub Frame · crackedMAIN CABIN R1 DOOR CUTOUT FORWARD UPPER CORNER CRACK INDICATION AT STUB FRAME MEASURING .7 INCHES IN LENGTH<[01] INSTALLED STUB FRAME IAW B737-700 SRM 51-40-02; B737-700 AIPC 53-11-00-80; AND BOEING DWG NO. 141A8370 REV.C.;[02] INSTALLED STUB FRAME IAW B737-70Mar 26, 2025 · N956WN · Boeing 7377H4SDR IPXA2025041681038Frame · dentedAFT CARGO COMPARTMENT BS1500 / S25L-S27L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-27, ENRIQUE BARREIRO. INSTALLED J SECTION REPAIR PER SRM 53-00-07-2R-5 DETAIL I. REVIEWEDMar 26, 2025 · N443UP · Boeing 75724APFSDR IPXA2025041680829Frame · dentedAFT CARGO COMPARTMENT BS1600 / S26L-S25L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-25, ENRIQUE BARREIRO. INSTALLED STRIGER CLIP (2EA) AND REPAIR SPLICE ON AFT CARGO COMPARTMENT BS1600 / S26L-S25L FUSELAGE FRAME IAW B757-200 SRM 53-00-07-2R-5 MATERIAL USMar 26, 2025 · N443UP · Boeing 75724APFSDR IPXA2025041480002Frame · corrodedFAULT - STR - Z162- AFT CARGO COMPARTMENT BS1300 / S26R FRAME HAS A DENT. DOT 95-22, ENRIQUE BARREIRO. INSTALLED NEW J SECTION. IAW SRM 51-40-02. MATERIAL USED 21EA BOLT P/N BACB30MY6K4X BATCH 0004365542, 21EA COLLAR P/N BACC30AC6 BATCH 0004198709 AND SEAL P/Mar 26, 2025 · N443UP · Boeing 75724APFSDR IPXA2025041580671Frame · dentedFAULT - STR - Z162 - AFT CARGO COMPARTMENT BS1480 / S25R FUSELAGE FRAME HAS A DENT. DOT 95-24, ENRIQUE BARREIRO. INSTALLED SUPPORT PANEL AT AFT CARGO COMPARTMENT BS1480 FUSELAGE FRAME IAW B757-200 SRM 51-40-02-0G MATERIAL USED P/N:BAC330NX6K3 BTCH:0004325741 Mar 26, 2025 · N443UP · Boeing 75724APFSDR IPXA2025041580950Frame · dentedFAULT - STR - Z161 - AFT CARGO COMPARTMENT BS1580 / S26L-S25L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-26, ENRIQUE BARREIRO. INSTALLED 1EA REPAIR SPLICE AND 2EA STRINGER CLIPS IAW B757-200PF SRM 51-40-02-0G FOR ACCOMPLISH REPAIR IAW SRM 53-00-07-2R-5 DMar 26, 2025 · N443UP · Boeing 75724APFSDR DALA2025040102468Frame · corrodedFS 1022, LOWER PRIOR FRAME REPAIR AT STR 29LT-30 IS CORRODED. SUMMARY SEE NRC 001-0545:5331-2001/010 01244: CORROSION LEVEL 2. REPAIRED 3 ROLLED Z-FRAME REPAIR SPLICE PER B717-200 SRM 53-20-07-2R. (LP #0879160)Mar 26, 2025 · N925AT · Boeing 717200SDR FDEA202503260498Frame · corrodedLOWER FUSELAGE FRAME AT STA 410 AT STRINGER 52 HAS CORROSION AT INTERCOSTAL INTERSECTION. REMOVED & REPLACED FRAME AT LOWER FUSELAGE STA 410 IAW SRM 51-35-01. PART MARKED IAW GMM 07-0-1000. MAJOR REPAIR CATOGORY A. STG 45L TO STG 45R.Mar 26, 2025 · N618FE · Doug MD11FSDR FDEA202503260497Frame · corrodedLOWER FUSELAGE STA 421 FRAME AT STRINGER 52 HAS CORROSION AT INTERCOSTAL INTERSECTION. REMOVED & REPLACED LOWER FUSELAGE STA 421 FRAME AT STRINGER 52 IAW SRM 51-35-01. MAJOR REPAIR CATOGORY A. STGR 45L TO STG 45R.Mar 26, 2025 · N618FE · Doug MD11FSDR SWI2025F01265Frame · corrodedCORROSION ON FRAME AT FS927.00 BETWEEN STGR 25L AND STGR 26L (MARKED) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW LOWER FRAME SECTOR FS927 BETWEEN STR 20L - STR23R REF: CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01 AND DWG SH690Mar 25, 2025 · N896SK · Cndair CL6002D24SDR SWI2025F01262Frame · corrodedCORROSION ON FRAME AT FS969.00 BETWEEN STGR 25L AND STGR 26L (MARKED) (C-CHECK RO 09/07/2025)INSTALLED NEW FRAME SECTOR FS969.00, P/N SH690-37074-3S. REF: CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01, AND DRAWING SH690-37060 REV AC. COMPMar 25, 2025 · N896SK · Cndair CL6002D24SDR SWI2025F01155Frame · corrodedFRAME AT FS333 HAS HEAVY CORROSION BETWEEN STGR21L - STGR 25L. REMOVED AND INSTALLED NEW FRAME AT FS333 REF SRM 51-42-06-001-001 A01, SRM 51-42-21-001-001 A01 AND DWG SH670-32420 REV E. LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY.Mar 25, 2025 · N614SK · Cndair CL6002C10SDR SWIA202509020010Frame · damagedUPON REMOVAL OF FS333 FRAME FOUND ELONGATED HOLES (2 EA) ON FRAME SUPPORT ANGLE BETWEEN STGR 21L - STGR 22L. REPLACED FRAME SUPPORT ANGLE OF FRAME FS333 BETWEEN STGR 21L - STGR22L WITH NEW FABRICATED FRAME SUPPORT ANGLE .REF DWG SH670-31810 REV : AE AND SRM Mar 25, 2025 · N614SK · Cndair CL6002C10SDR SWAA2025043054298Frame · crackedCRACK FRAME LOCATED BS259.5 BTW STR8R TO STR9R AT PASSENGER CABIN 2025-224171<[01] STEP 4 TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 210138003 DUE DATE: 11-JUN-25;[02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 5Mar 24, 2025 · N221WN · Boeing 7377H4SDR N6WA2025032402Frame · corrodedFRAME 364.00 HAS CORROSION AT STGR26R. REPAIRED FRAME 364.00 BETWEEN STRINGERS 24L TO 24R IAW GOJET EO C550/700-53MR-006.Mar 24, 2025 · N544GJ · Cndair CL6002C11SDR SWI2025F01281Frame · corrodedCORROSION ON AFT SIDE FS1015.00 BETWEEN STGR23R - STGR24R AS MARKED (C-CHECK RO 09/07/2025)REMOVED AND REPLACED INTERCOSTAL AT FS1015 & STGR23R - STGR 24R IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-42-21-001-001-A01 AND DRAWING MM690-35007 REV.U. CMar 22, 2025 · N896SK · Cndair CL6002D24SDR REXA2025072400754Frame · corrodedFOUND CORROSION ON FRAME SECTION P/N SH670-32033-1 AT F.S. 333 BETWEEN STR 19 AND STR 20. INSTALLED NEW SERVICEABLE FRAME SECTION P/N SH670-32033-1 TO TIE FITTING AT FS 333 BETWEEN STGR 19R AND STGR 20R IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-00Mar 22, 2025 · N379CA · Cndair CL6002C10SDR REXA2025051400586Frame · corrodedFS319 FRAME IS CORRODED BETWEEN STGR20L AND STGR21L. REMOVED AND REPLACED FRAME P/N SH670-31891-3 AT FS319 BETWEEN STR18L AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Mar 22, 2025 · N379CA · Cndair CL6002C10SDR REXA2025051400585Frame · corrodedFS319 FRAME IS CORRODED BETWEEN STGR26L AND STGR26R. INSTALLED NEW FRAME AT FS319 (P/N:SH670-31355-1S) BETWEEN STR23R AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01Mar 22, 2025 · N379CA · Cndair CL6002C10SDR REXA2025051300583Frame · corrodedFS319 FRAME IS CORRODED BETWEEN STGR20L AND STGR21L. REMOVED AND REPLACED FRAME P/N SH670-31891-3 AT FS319 BETWEEN STR18L AND STR21L IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Mar 22, 2025 · N379CA · Cndair CL6002C10SDR DALA2025032402170Frame · gouged(LOG 0871228) MAIN CABIN OVHD FRAME GOUGED AT BS 727A. ACCOMPLISHED FRAME REPAIR IAW SRM 53-00-07-2R REPAIR 1.Mar 22, 2025 · N3749D · Boeing 737832SDR DALA2025032102134Frame · crackedCRACK OF 0.093 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #090-0004, STEP 10). SUMMARY OF NRC 00281: FRAME TAB ON THE OVERWING FRAME AT STA Y= 696.000 RH WAS REPAIRED PER CARMar 21, 2025 · N938AT · Boeing 717200SDR FDEA202503200460Fitting · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 D P1 TO REPAIR THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGEMar 20, 2025 · N674FE · Airbus A300F4605RSDR VNAA20250320104Frame · crackedHN00205392 SN: 00600 DISCREPANCY: F.S. 333 FRAME IS CRACKED BETWEEN STGR 0 TO STGR 1R. CORRECTIVE ACTION: REPAIRED FRAME AT F.S.333 STRINGER 0 AND 2R IAW MHIRJ REO 670-53-21-2533 REV-- DATED 2025-01-20Mar 19, 2025 · N509AE · Cndair CL6002C10SDR VNAA20250320074Frame · dentedHN00198732 SN: 00166 DISCREPANCY: EXTERNAL FRAME IS DENTED @FS 280 BETWEEN 23R AND 24R CORRECTIVE ACTION: REPAIRED EXTERNAL FRAME AT FS 280 BETWEEN 23R AND 24R IAW REO 670-53-21-2514 REV -- DATED 2025-01-10Mar 19, 2025 · N509AE · Cndair CL6002C10SDR VNAA20250320049Frame · corrodedFRAME SECTOR FS 379.00 CORRODED BETWEEN STR 22R AND 23R REMOVED FS 379 FRAME SECTOR IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW FRAME SECTOR PN# SH670-32118-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-Mar 19, 2025 · N508AE · Cndair CL6002C10SDR VNAA20250320016Frame · corrodedFURTHER INVESTIGATION FINDS CORROSION ON EXISTING REPAIR IN THE FS295.00 FRAME BETWEEN FRAME AND SKIN BETWEEN RH STGR 26-22 CORRECTIVE ACTION: REMOVED EXISTING REPAIR IN THE FS295.00 FROM STGR L26-R23 IAW CRJ700 SRM 51-42-21-001-001-A01 & 51-23-00-001-001-A01.Mar 19, 2025 · N509AE · Cndair CL6002C10SDR YENA2025032000297Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE FWD LH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 833. MAXIMUM CRACK LENGTH: 0.500 I NCHES; REF AEROMAN N/R 2025- 125818, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCYMar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000296Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE FWD RH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 843. MAXIMUM CRACK LENGTH: 0.450 I NCHES; REF AEROMAN N/R 2025-125819, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY Mar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000295Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE AFT LH SIDE OVERWING EMERGENCY EXIT HATCH DOOR 834. MAXIMUM CRACK LENGTH: 0.400 INCHES; REF AEROMAN N/R 20250125820, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXMar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000294Frame · crackedDURING HEAVY MAINTENANCE: SEVERAL CRACK INDICATIONS FOUND ON FRAME SEGMENT 1 OF THE AFT RH SIDE OVER WING EMERGENCY EXIT HATCH DOOR 844. MAXIMUM CRACK LENGTH: 0.400 I NCHES; REF AEROMAN N/R 2025-125821, ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY Mar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000292Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE C FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 3 OCLOCK; REF AEROMAN N/R 2025- 125698, PERFORMED PERMANENTE REPAIR ON HOLE C FR16LH JOGGLE AREA I.A.W A320 SRM 53-11-12-300-012Mar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000291Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 9 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00021) FUR-A320-53-02090, REF AEROMAN N/R 2025-125700, MESURE OF DIAMETER ON OPEMar 19, 2025 · N766JB · Airbus A320232SDR YENA2025032000290Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 9 OCLOCK; REF AEROMAN N/R 20250125700, PERFORMED PERMANENTE REPAIR ON HOLE D FR16LH JOGGLE AREA I.A.W A320 SRM 53-11-12-300-012 FMar 19, 2025 · N766JB · Airbus A320232SDR DALA2025032002096Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN. SUMMARY OF NRC 00360: CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN WAS REPAIRED PER B717-200 53-20-07-2R REPAIR 4. (LP #0866910)Mar 19, 2025 · N938AT · Boeing 717200SDR DALA2025031902065Frame · corrodedCORROSION FOUND ON FRAME AT F.S. 889 BETWEEN STRINGER 29L. SUMMARY SEE NRC 001-0508:2550-2001/008 01228: CLEANED UP FRAME REF B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL. FOUND TO BE OUT OF LIMITS. REPAIRED REF B717-200 SRM 53-20-07-2R REPAIR 3 ROLLED Z-Mar 19, 2025 · N925AT · Boeing 717200SDR HNAA2025043000281Frame · crackedF034720 FRAME 66 CRACKED AT STR 16R. REMOVED CRACKED FR 66 LOWER FRAME SECTION AND INSTALLED SERVICEABLE FRAME 66 SECTION IAW EMB 145 SRM 51-40-02.Mar 18, 2025 · N677AE · Emb EMB145LRSDR SWAA2025042854155Frame · crackedCRACK ON WEB FRAME LOCATED BS 259.5 BTW STR 8R TO STR 9R AT FWD GALLEY AREA 2025-204596<[01] ET EQUIPMENT USED P/N: NORTEC 600D; S/N: 240494307; DUE DATE: 27-AUG-25;[02] PERFORMED PERMANENT REPAIR ON WEB FRAME LOCATED BS 259.5 BTW STR 6R TO STR 11R AT FWD GALLMar 18, 2025 · N220WN · Boeing 7377H4SDR SWAA2025040806858Frame · crackedPASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] ACCOMPLISHED REPAIR PER EA#M-22-153-01244 AND 'EA-GENERAL' REPAIR REFERENCE IS SELECTED;[02] VERIFIED CORRECTIVE ACTION 1Mar 18, 2025 · N280WN · Boeing 7377H4SDR DALA2025031902067Frame · corrodedCORROSION AT STA 1083 BETWEEN STRG 38R AND STRG 39R ON AFT CARGO BILGE SKIN REF TO CPCP 53-558-00. CORROSION ON AFT CARGO BILGE SKIN AT STA 1083 S38R-S39R WAS REPAIRED PER PRI 624890-14 REV 0. COMPARED AND COMPLIED WITH ER/A 624890-14 REV ORIGINAL. NO DEVIATIOMar 18, 2025 · N828MH · Boeing 767432ERSDR SWI2025F01144Frame · corrodedCORROSION ON FS863.00 AFT SIDE AT STGR27. REMOVED CORROSION ON FRAME AT BS 863, S27 AND FOUND REWORKED AREA TO BE ACCEPTABLE REF REO 670-53-51-345 REV -, STEPS 1 - 7 COMPLIED WITH. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 17, 2025 · N614SK · Cndair CL6002C10SDR SWI2025F01143Frame · corrodedFRAME AT FS280.00 HAS CORROSION ON AFT SIDE OF FRAME BETWEEN STR.27 AND STR.26R. PERFORMED CUTOUT AND APPLIED DOUBLER TO FRAME AT FS280, STGR 27 - STGR26R IN REF TO REO 670-53-11-2113 REV --. COMPLIED WITH TASK CARD 51-900-1002-SKYMar 17, 2025 · N614SK · Cndair CL6002C10SDR SWIA202507210317Frame · corrodedCORROSION FOUND ON INBOARD UPPER FLANGE OF RBL9 AT FS 549. PERFORMED FLANGE REPAIR ON INBOARD UPPER FLANGE OF RBL9 AT FS 549 INSTALLED ANGLE (18) , FILLER (23) AND SHIM (19) REF CRJ700 SRM 53-00-41-201-001-A01AND COMPLIED WITH ALL THE STEPS OF THE REO 670-53Mar 17, 2025 · N723EV · Cndair CL6002C10SDR DALA2025031802057Frame · misrepairedSHIP 683 ER/A 564553-14 / AMOC APPROVAL LIMIT FUSELAGE / FRAME / FS 440-460 / S-2R - S-3R / 2KU / ACL POWER SUPPLY RELOCATION / INSUFFICIENT EDGE DISTANCE. CORRECTIVE ACTION: REF ERA 564553-14AD. (0863152)Mar 17, 2025 · N683DA · Boeing 757232SDR DALA2025031702029Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN. SUMMARY OF NRC 00361: FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0861190)Mar 16, 2025 · N938AT · Boeing 717200SDR UIEA2025022500164Frame · corrodedBULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME WITH CORROSION (L=2" W=1.5").(<P>BULK CARGO COMPARTMENT, AT STA 1518, BTW STRG 28L AND 29L FRAME, CORROSION LEVEL 1 WAS EVALUATED. REWORKED, AND INSPECTED, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMIMar 15, 2025 · N1373A · Boeing 76731K
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