JASC 5310

Service difficulty reports · 38,519

Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310'
  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 YENA2026012900082Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 INSIDE OF THE INNER FRAME SEGMENT 1 IN PASSENGER CABIN (CRACK L:0.650 INCH); REF AEROMAN WO 2025 415/1 NR 2025-750907; REMOVED AND REPLACED FRAME SEGMENTS ON THE EMERGENCY EXIT DOOR 844 IAW Jan 28, 2026 · N637JB · Airbus A320232SDR YENA2026012900081Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF DOOR STOP FITTING Ñ1 FR 68 LH. CRACK DIRECTION 7 AND 12 OCLOCK LOOKING AFT. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1427178 TASKCARD: NR-00041) REF AEROMAN WO 2025 415/1 NR 2025-762622, PERFOJan 28, 2026 · N637JB · Airbus A320232SDR YENA2026012900080Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER IB HOLE OF DOOR STOP FITTING N2 FR 66 LH CRACK DIRECTION 7 OCLOCK LOOKING FWD CRACK D=0.170 INCH; REF AEROMAN WO 2025 415/1 NR 2025-762623 PERFORMED PERMANANT REPAIR LOC ON LWR IB HOLE OF DOOR STOP FITTJan 28, 2026 · N637JB · Airbus A320232SDR YENA2026012900079Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LWR IB HOLE OF DOOR STOP FITTING N1 FR68 CRACK DIRECTION 1 AND 7 OCLOCK LOOKING AFT CRACK D=0.170 INCH; REF AEROMAN WO 2025 415/1 NR 2025-762624 PERFORMED PERMANENT REPAIR LOC ON LWR IB HOLE DOOR STOP FITTINGJan 28, 2026 · N637JB · Airbus A320232SDR VNAA202601280031Floorbeam · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE ( FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WATER LINE 79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE ( FLIGHT COMPARTMENT FLJan 28, 2026 · N646NN · Cndair CL6002C10SDR VNAA202601280028Crossbeam · corrodedIN REFERENECE TO NRC 00129: AFTER REMOVAL OF ANGLE CAP, CORROSION ON LH CROSSBEAM AT FS280 WAS FOUND. LT CROSSBEAM AT FS280 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-00Jan 28, 2026 · N646NN · Cndair CL6002C10SDR VNAA202601280022Beam · corrodedCORROSION ON BEAM SIDE, RIGHT SIDE FROM FS985.00 TO FS1088.20 WL 72.00 AND LEFT SIDE FROM FS1049.00 TO FS1053.00 WL 72.00 AT AFT BAGGAGE-BAY. CORROSION ON BEAM SIDE, RIGHT SIDE FROM FS985.00 TO FS 1015.00 AND FS1069.75 TO FS1088.20 WL 72.00 AND LEFT SIDE FROJan 28, 2026 · N646NN · Cndair CL6002C10SDR VNAA202601280009Fitting · corrodedCORROSION ON FITTINGS 2EA BTW FS 349 TO FS 364 AND STRG 25LH TO STGR 27 AT AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE. CORROSION ON FITTING 1EA BTW FS 349 TO FS 364 AND STRG 26LH AT AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ 900 SRM 51Jan 28, 2026 · N646NN · Cndair CL6002C10SDR DALA2026012800654Cross Bar · corrodedRIGHT AFT CABIN 01EA FLOOR SUPPORT/CROSS BEAM AT FR 73+10 INCHES, -YB TO -YC1 FOUND HEAVY CORROSION. REPLACED THE DAMAGED SUPPORT BEAM AT -YB TO -YC1 FR73+10 INCHES PER A330 SRM 51-72-11-911-001. (1423061)Jan 28, 2026 · N820NW · Airbus A330323SDR SWIA2026012776639Structure · corrodedRBL9 SIGNS OF CORROSION FROM BS 6770 TO 693. BLENDED OUT AND EVALUATED DAMAGE ON FLOOR SUPPORT AND BULKHEAD BEAM AT RBL9 BETWEEN F.S.677 TO 693, REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE IAW SRM 51-42-10, 51-42-21, 51-41-02, 53-31-43, 53-00-41, 51-42-15 AJan 27, 2026 · N707EV · Cndair CL6002C11SDR SWIA2026012776637Support · corrodedMULTIPLE NUTPLATE HOLES HAVE SIGNS OF CORROSION ON LBL9 FROM FS579.00 TO FS661. REPAIRED DAMAGE AROUND NUTPLATE HOLES ON LBL 9 FROM BS 579 TO BS 661 IAW REO 670-53-31-1199, REV-P1, REV-- 1 AND SRM 53-31-43, 51-41-02, 51-42-06, 51-42-10, AMM 53-00-49.Jan 27, 2026 · N707EV · Cndair CL6002C11SDR HNAA2026030200159Doubler · corrodedEXTERNAL FUSELAGE POTABLE WATER HEATER NIPPLES DOUBLER HAS CORROSION. RAR EXTERNAL FUSELAGE POTABLE WATER HEATER NIPPLES DOUBLER IAW EMB 145 SRM 51-40-02.Jan 27, 2026 · N907AE · Emb EMB145LRSDR YENA2026012900085Door Frame · ground damageDURING HEAVY MAINTENANCE: FWD CARGO DOOR HIT BY BAG LOADER. DAMAGE FOUND TO DOOR JAM UPPER CORNERS AND CARGO BAY DOOR LOWER AFT CORNER; REF AVIANOR WO# JB-3139-AOG-01. NR# 3003. CARRIED OUT DVI OF FWD CARGO DOOR, SURROUND AND ATTACHMENTS, HINGE FITTINGS AND DOJan 27, 2026 · N3139J · Airbus BD5001A11SDR SWIA2026012675610Latch Catch · crackedPOSSIBLE CRACK ON LEFT TRU LANDING AFT LATCH CATCH. REMOVED AND REPLACED LEFT TRU LANDING. REF. SRM 51-42-06-001-001-A01, REO 670-53-11-2268 REV.- AND DWG CC670-33040 REV. -G SHEET 2.Jan 26, 2026 · N726SK · Cndair CL6002C10SDR SWAA2026021764716Window Frame · crackedCRACK ON UPPER CORNER R1 WINDOW FRAME. PERFORMED A REPAIR ON THE R1 WINDOW FRAME IAW EA 26-153-00290, WIP1 - WIP5.Jan 26, 2026 · N458WN · Boeing 7377H4SDR DALA2026013000728Fitting · out of limitsTIME LIMITED REPAIR ERA 596680-14AD REV A. CONTINUITY FITTING REPLACEMENT IS LIMITED TO 53,909 TFC. ACCOMPLISH ERA 596680-14AD SECTION III PRIOR TO 53,909 TFC. CONTACT LIAISON ENGINEERING FOR THE PERMANENT REPAIR. ASSOCIATED AA 5311-01226 ADDED FOR AC 3268 ASJan 26, 2026 · N368NW · Airbus A320212SDR DALA2026012900699Window Frame · damagedAD 2020-17-03 / A.A. WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. FLIGHT DECK, RT WINDSHIELD FRAMING LOWER CENTER POST, & RT CONTINUITY FITTING CRACKED. PERFORMED WING FRAMING MIRROR REPAIR & CONTJan 26, 2026 · N349NB · Airbus A319114SDR IPXA2026021974623Bracket · crackedAVIONICS COMP, FR10, BY -Y1456, ANGLE PICKUP IS CRACKED. REMOVED ANGLE PICKUP WITH CRACK AT AVIONICS COMP, FR10, BY -Y1456 IAW A300-600 SRM 51-40-21. INSTALLED NEW ANGLE P/N UPA53610814204 AT STR-Z100- AVIONICS COMP, FR10, BY -Y1456 IAW A300-600 SRM 51-40-21 Jan 25, 2026 · N145UP · Airbus A300F4622RSDR SWAA2026022364418Crossbeam · crackedCRACKED CROSSBEAM, PASSENGER CABIN, BS 540, LBL 2, WL 208. REMOVED AND REPLACED THE CROSSBEAM, BS 540, LBL 0.0 TO LBL 24.75 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B;Jan 25, 2026 · N922WN · Boeing 7377H4SDR SWAA2026022364419Crossbeam · crackedCRACKED CROSSBEAM AT PASSENGER CABIN, BS 540; LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540 LBL 24.75 - LBL 45.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B.Jan 25, 2026 · N922WN · Boeing 7377H4SDR IPXA2026020469257Brace · crackedM.C. DECK FR#38.1 RH DIAGONAL BRACE CRACKED WHERE THE FLOOR MEETS THE SIDEWALL INSTALLED SMOKE TUBE AT FR 38.1 RH MAIN DECK IAW. A300 SRM 51-40-23. REVIEWEDJan 25, 2026 · N145UP · Airbus A300F4622RSDR DALA2026020100733Window Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FR 4 WINDOW FRAME. REPAIR PERFORMED PER ER/A 631144-14AD. SECTION I IS LIMITED TO 60000FC FROM EMBODIMENT. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SERVICE. ASSOCIATED ER/A 14-631144 ADDEDJan 25, 2026 · N349NB · Airbus A319114SDR DALA2026012900707Window Frame · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR LH & RH CONTINU ITY FITTING REPLACEMENT PERFORMED PER ER/A 631144-14AD. SECTION I LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-63114Jan 25, 2026 · N349NB · Airbus A319114SDR DALA2026012900706Window Frame · damagedER/A 631144-14AD ISSUED FOR LT & RT MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-631144 ADDED. (LP: 1419073)Jan 25, 2026 · N349NB · Airbus A319114SDR DALA2026012600549Window Frame · crackedCRACK INDICATION FOUND ON RH WINDSHIELD CENTER POST, LOWER ATTACHMENT ARIA, LOWER CORNER RADIUS, CRACK IS HORIZONTAL DIRECTION, CRACK LENGTH IS 0.190 INCH. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR Jan 25, 2026 · N359NB · Airbus A319114SDR IPXA2026052763514Angle · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD FR 39-40 -Y450 UPPER SURFACE HAS EXFOLIATION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97465-REQ1 AND VT-MAE EA 300-5315-27-A4331, REV. -.Jan 24, 2026 · N145UP · Airbus A300F4622RSDR IPXA2026030367324Housing · corrodedNUMBER 4 R/A ANTENNA (5SA2) HOUSING CORRODED AROUND DOME NUT AND CUTOUT AREA. INSTALLED NEW R/A HOUSING IAW SRM 51-40-21.Jan 24, 2026 · N145UP · Airbus A300F4622RSDR AALA202602134521Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL CROSSBEAM IS CRACKED AT BS 540 RBL 2. REPLACEMENT AND INSTALL OF MAIN CABIN FLOOR CROSSBEAM COMPLIED ON NR-00618.Jan 24, 2026 · N981AN · Boeing 737823SDR AALA202602138365Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL CROSSBEAM IS CRACKED AT BS 540 LBL 2. REPLACEMENT AND INSTALL OF MAIN CABIN FLOOR SUPPORT CROSSBEAM COMPLIED ON FAS NR-00619.Jan 24, 2026 · N981AN · Boeing 737823SDR DALA2026012500537Plate · corrodedAIRCRAFT 6717, CORROSION ON SIDE PLATE LT AND BS 620 AT FWD CARGO BAY. CORROSION LEVEL 2. CORROSION ON SIDE PLATE LT AND BS 620 AT FWD CARGO BAY WAS REPAIRED IAW SRM 53-00-53-2R, PROCEDURE 2, REPAIR 2. (LP 1417580)Jan 24, 2026 · N67171 · Boeing 757232SDR HNAA2026030400166Door Sill · corrodedCORROSION ON THE MAIN DOOR SILL BTW FR 20 - 22. R & R THE DOOR SILL IAW SRM 51-40-02.Jan 23, 2026 · N642AE · Emb EMB145LRSDR ASAA2026012364091Seat Track · corrodedMAIN CABIN, LBL 45.50, 727I + 14 INCHES, SEAT TRACK CORRODED. CORROSION LEVEL 1 & NOT MAJOR REPAIR GROUNDED - YES. REMOVED CORROSION ON THE SEAT TRACK BS 727I + 14", LBL 45.50. ORIGINAL MATL. THICKNESS ON BOTTOM OF TRACK IS .230", REMOVED .027", REMAINIJan 23, 2026 · N581AS · Boeing 737890SDR JJBA20260211005Support Frame · corrodedCORROSION ON THE LT SILL FRAME 35-41. REMOVED AND REPLACED WITH NEW LT SILL FRAME 35-41.Jan 23, 2026 · N14168 · Emb EMB145XRSDR CALA2026020913627Panel · corrodedLAV SERVICE PAN SHOWS EVIDENCE OF CORROSIONREMOVED LAV ACCESS PANELS 141QW, 141PW, AND AND 141MW FOR LAV REPAIR. REMOVED LAV SERVICE DOOR AND HINGES, BAGGED AND TAGGED HARDWARE. CLEANED FUSELAGE SKIN IN PREP FOR MARKING STRINGER AND FRAME LOCATIONS. REMOVED INJan 23, 2026 · N13227 · Boeing 737824SDR DALA2026012600547Post · corrodedCORROSION ON AFT LATERAL POST LAVATORY A AT FWD GALLEY AREA. COMPLIED WITH ER/A 631052-14 REV. A. APPROVED DATE: 16-JAN-26 MATCHES WITH ALL STEPS OF ER/A 631052-14 PRI REV. 0 AND REV 1 IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON AFT LATERAL POST LJan 23, 2026 · N359NB · Airbus A319114SDR AALA202601232119Failsafe · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FAILSAFE STRAP RUNNING UNDER KICK FITTING AT STA 663.75, S18R. REPAIRED FAILSAFE PER EA 370951.Jan 23, 2026 · N919AN · Boeing 737823SDR SWIA2026012276070Door Frame · corrodedMAIN AVIONICS BAY DOOR LAND PITTED AND WITH FRETTING DAMAGE ALL AROUND. REMOVED DAMAGE ALL AROUND MAIN AVIONICS BAY DOOR LAND PER REF SRM 51-21-06-001-001-A01, AVIONICS BAY DOOR LAND IS WITHIN LIMITS PER REO 690-53-21-032, REV --. SEE CONTINUATION CARD FOR DEJan 22, 2026 · N899SK · Cndair CL6002D24SDR SWIA2026012276057Support · corrodedCORROISON ON BACKUP, SILL (STGR 21L, FS333.00 TOFS349.00) REPLACED BACKUP, SILL (STGR 21L, FS333.00 TOFS349.00) REF. SRM 51-42-06-001-001-A01 AND DWG# SH670-31810 REV: AE. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.Jan 22, 2026 · N899SK · Cndair CL6002D24SDR 2A6R2026052675601Deck Plate · dentedDURING 500-HOUR INSPECTION, A DENT WAS DISCOVERED ON THE R/H SIDE OF THE TRANSMISSION DECK (P/N: L533M1017295). THE MAXIMUM DEPTH IS APPROXIMATELY 0.022" WITH A MAXIMUM DIAMETER OF 0.8. AN APPROXIMATE LOCATION OF THE DAMAGE IS AT STA. 4600MM, W.L. 2465MM, AND Jan 22, 2026 · N831ME · Urocop EC135T2SDR VNAA20260329002Angle · corrodedCORROSION ON KICKPLATE ANGLE BTW FS310.0 TO FS 349.0 (DOOR SILL AREA) AT PASSENGER DOOR SURROUND STRUCTURE. KICKPLATE ANGLE BTW FS310.0 TO FS 349.0 (DOOR SILL AREA) AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Jan 22, 2026 · N643NN · Bombdr CL6002D15SDR VNAA20260329001Angle · corrodedCORROSION ON MID CAP ANGLE BTW FS310.0 TO FS 349.0 (DOOR SILL AREA) AT PASSENGER DOOR SURROUND STRUCTURE. MID CAP ANGLE BTW FS310.0 TO FS 349.0 (DOOR SILL AREA) AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.Jan 22, 2026 · N643NN · Bombdr CL6002D15SDR AALA202602202015Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO AUXILIARY DOOR SILL OUTER CHORD BETWEEN BS 310 AND BS 352 ALONG S23L. REPLACED CHORD PER EA 372019.Jan 22, 2026 · N982AN · Boeing 737823SDR 2A6R2026020274903Floor Skin · dentedMULTIPLE DAMAGES TO THE COCKPIT FLOOR UPPER SKIN PANEL IN THE FORM OF DENT AND CORROSION DAMAGES TO THE UPPER SKIN. ZONE 1 HAS CORROSION DAMAGE ON THE LH & RH SIDE FWD LOCATION NEAR THE PILOT & COPILOT PEDALS. THE CORROSION DAMAGE IS MEASURED TO BE APPROXIMATJan 22, 2026 · N381MS · Bolkms BK117C2SDR 2A6R2026020274902Rib · crackedDAMAGE TO THE FWD BOTTOM LBL195 RIB IN THE FORM OF A CRACK IN THE RADIUS OF THE TOP FLANGE. THE CRACK WAS FOUND BENEATH THE CENTER CONSOLE MOUNT AND WAS MEASURED TO BE APPROXIMATELY 1.0” IN LENGTH. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PJan 22, 2026 · N381MS · Bolkms BK117C2SDR JJBA20260127077Door Sill · corrodedSERVICE DOOR SURROUND STRUCTURE, FWD SILL BTW FR 17-20 FOUND CORRODED. SERVICE DOOR SURROUND STRUCTURE FWD SILL BTW FR 17-29 EXISTING REPAIR BLENDED AND FOUND OUT OF LIMITS. CF1, SERVICE DOOR SURROUND STRUCTURE FWD SILL BTW FR 17-20 REPAIR REMOVED AND REPLACEDJan 22, 2026 · N14174 · Emb EMB145XRSDR CALA2026012713325Bracket · dentedL2 DOOR EXTERNALM BRACKET ON FWD EDGE OF THE DOOR FRAME APPEARS TO HAVE A DENT. REPLACED THE BRACKET IAW 147A0010. REV.- AND SRM 51-40-02-0G-0.Jan 22, 2026 · N33289 · Boeing 737824SDR DALA2026012600596Door Frame · cracked(LOG 8092530) ON B4 CHECK, FOUND R1 & L1 OUTER DOOR FRAMES CRACKED, UPPER OTBD CORNERS. ALL WORK AND RII'S PERFORMED ARE TRANSFERRED TO WORKPAGE 7543424 AND NON-ROUTINES NR 1 AND NR 2 IAW ER/A 620146-14TR, REV ORIG, & 620147-14TR, REV ORIG.Jan 22, 2026 · N386DA · Boeing 737832SDR DALA2026012600595Window Frame · cracked(LOG 1414305) DURING B-4 CHECK, FOUND R1 WINDOW FRAME C-D POST CRACKED AT UPPER OTBD CORNER. REPAIRED THE CRACKS IAW ERA 620147-14.Jan 22, 2026 · N386DA · Boeing 737832SDR DALA2026012600594Window Frame · cracked(LOG 1414279) DURING B-4 CHECK, FOUND L1 WINDOW FRAME C-D POST CRACKED AT UPPER OTBD CORNER. REPAIRED THE CRACKS IAW ERA 620146-14.Jan 22, 2026 · N386DA · Boeing 737832SDR AALA202601261370Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BEAM AROUND 2 NUTPLATES FOR THE CENTER SHAPE FITTING AT FR 68 AND S23L. REPAIRED SILL BEAM PER SRM 53-41-14-300-001 REPAIR PRINCIPLE #3 AND EA 371804.Jan 22, 2026 · N410AN · Airbus A321253NX
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