JASC 5310

Service difficulty reports · 38,528

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 CALA2025081407747Window Frame · crackedCRACK FOUND AT L3 WINDOW POST AT HOLE NR 3. CRACKED AT 3 0'CLOCK, CRACK LENGTH - 0.030". REPAIRED L3 WINDOW FRAME IAW ESR-WI NO:2023573-20-12432 AND EC/RA 5310-08653 REV. ORIGINAL, INTERIM REPAIR. PERFORMED THE INTERIM REPAIR TO L3 WINDOW FRAME E-F POST PERJul 27, 2025 · N17229 · Boeing 737824SDR CALA2025080407229Rib · dentedDENT ON RIB AT STA 700 L/H SIDE STRINGER 23 IN FWD PIT. REPAIRED FRAME AT STA 700 BETWEEN 5-22L AND 5-25L IAW B757-200 S RM 53-00-07-2R-5 FIG 201 SFR# 1464 REPAIRED FRAME AT STA 700 BETWEEN S-22L AND S-25L IAW B757-200 S RM 53-00-07-2R-5 FIG 201. ADD EMP:V951Jul 27, 2025 · N14120 · Boeing 757224SDR DALA2025080205797Pan · corrodedSEVERAL AREAS OF CORROSION AROUND FASTENES. REPLACED FORWARD CARGO DOOR LOWER JAMB PAN IAW B717-200 SRM 53- 20-15-2R (1108952)Jul 27, 2025 · N957AT · Boeing 717200SDR JJBA20251024079Web · crackedRH MLG BAY AFT WEB CRACKED AT SPAR III LOWER OB CORNER. REMOVED AND REPLACED RH MLG BAY AFT WEB AT SPAR III LOWER OB CORNERJul 26, 2025 · N12135 · Emb EMB145XRSDR AALA202508196862Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON CONNECTING PLATE LOC. ON RH MAIN LANDING GEAR MEASURE OF CRACK D1-D2=0.069 INCH. MAINTENANCE REPLACED CONNECTING PLATE LOC AT FR 42 BTW STR 41RH AND 42RH MAIN LANDING GEAR IAW EA #366188 PART B STEP 2.B, DWG D53370790, A3Jul 26, 2025 · N763US · Airbus A319112SDR JJBA20251111057Bracket · corrodedL-CLIP IN BOTTOM LEADING EDGE OF AFT CARGO DOOR CUT-OUT IS CORRODED. REMOVED CRACKED L-BRACKET AND INSTALLED NEW FROM STOCK AT FR65 STR 17LJul 25, 2025 · N12135 · Emb EMB145XRSDR JJBA20251024075Crossbeam · corrodedFOUND CORROSION ON CROSS MEMBER AT FRAME 20. REMOVED AND REPLACED 1EA CROSS MEMBER IN PAX CABIN FR20Jul 25, 2025 · N12135 · Emb EMB145XRSDR 9WGA2025091954660Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091954659Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT LH APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091954658Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1205, XCW 4.0 AS S-18. AFTER FURTHER EVALUATION , BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091954657Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAWJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091854656Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091854655Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 34.5 AT S-15. AFTER FURHTER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETE WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPRJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025091854654Panel · corrodedDURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1226, XCW 80.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025090954647Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19. AFTER FURHTER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINGJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025090954646Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINGJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082654645Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WINJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082654644Panel · corrodedDURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082654643Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 0.5 AT 5-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082654642Panel · corrodedDURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA. 1182, XCW 8.5 AT 5-21. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX. STA. 1182, XCW 8.5 AT S-21 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11 MJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082254630Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MEJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082254629Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH AAPROX STA. 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPJul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082254628Panel · corrodedDURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1229, XCW 34.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING Jul 25, 2025 · N546JN · Doug MD11FSDR 9WGA2025082254627Panel · corrodedDURING HEAVY CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1226 XCW 80.5 AT S-15. AFTER FURTHER EVALUATION BOING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANELJul 25, 2025 · N546JN · Doug MD11FSDR AALA202508134533Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON DOOR FRAME LOC. BTW FR67 AND FR68 AT LEVEL STRG 8R, PASSENGER CABIN, AFT GALLEY AREA. CRACK L=0.538 IN. MAINTENANCE REPLACED DOOR FRAME LOC. BTW FR67 AND FR68 AT LEVEL STRG 8R, PASSENGER CABIN, AFT GALLEY AREA IAW A319 SRJul 25, 2025 · N763US · Airbus A319112SDR AALA202508019065Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON HOLE H1 INSTERCOSTAL FITTING LOC. ON FR 20 LH SIDE AT LEVEL DOOR STOP 7, FWD GALLEY AREA, MEASURE OF CRACK IS L=0.103 IN. MAINTENANCE REPLACED INSTERCOSTAL FITTING LOC. ON FR 20 LH SIDE AT LEVEL DOOR STOP 7, FWD GALLEY AJul 25, 2025 · N763US · Airbus A319112SDR DALA2025072505592Door Frame · misinstalledSHIP 3360 FR 64 L2-R2 HAS INCORRECT FASTENERS. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV ORIGINAL. (1104867)Jul 25, 2025 · N860NW · Airbus A330223SDR DALA2025072505591Door Frame · misinstalledSHIP 3360 FR 63 - R2 HAS INCORRECT FASTENERS. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV ORIGINAL. (1104860)Jul 25, 2025 · N860NW · Airbus A330223SDR SWIA20251110724Door Frame · corrodedRIGHT DOOR POST AT FS280 HAS SIGNS OF CORROSION AT FLOOR LEVEL (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH DOOR POST AT FS280 FLOOR LEVEL IAW CRJ900 SRM 53-11-10, 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-13. NDT PERFORMEDJul 24, 2025 · N249LR · Cndair CL6002D24SDR AALA202508013798Support Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON WING TO BODY FAIRING SUPPORT FRAME AT BS 727 FROM LBL 15 TO RBL 15. REPLACED FRAME PER SRM 53-60-71.Jul 24, 2025 · N855NN · Boeing 737823SDR HNAA2025091100620Door Frame · corrodedFUSELAGE SERVICE DOOR CUT-OUT AT FR-22 AND BETWEEN STGR 15R/16R HAS CORROSION. REPAIRED FUSELAGE SERVICE DOOR CUT-OUT AT FR-22 BETWEEN STGR 15R/16R IAW EMB 145 SRM 53-00-04 REF ITEM 16, FIG 208.Jul 23, 2025 · N646AE · Emb EMB145LRSDR AALA202509058698Fork · wornAIRCRAFT IN BASE MAINTENANCE: FOUND RACK 80VU LATERAL FITTING IN CONTACT WITH STRUCTUR RH SIDE IN AFT AVIONIC COMPARTMENT. DAMAGED AREA: 0.080 IN. MAINTENANCE PERFORMED INTERIM REPAIR AT LOWER LATERAL SUPPORT RH OF 80VU RACK LOC BTW FR23 TO FR24 AT LEVEL STR 3Jul 23, 2025 · N768US · Airbus A319112SDR QMLA2025072520076Profile · crackedDURING 500HR AIRFRAME INSPECTION FOUND THE LH AND RH A-PROFILES CRACKED AND A CRACK IN THE TRANSMISSION DECK FLOOR .Jul 23, 2025 · N953AL · Urocop EC135T2SDR IXXA20250723035Ball Screw · shearedFIRST OFFICER'S R2 WINDOW WILL NOT CLOSE. UPON INSPECTION FOUND BALLSCREW SHAFT SHEARED AT FORWARD END. REMOVED AND REPLACED R2 WINDOW BALLSCREW ASSEMBLY AND REINSTALLED ORIGINAL LOWER R2 WINDOW TRACK AND R2 WINDOW IN ACCORDANCE WITH BOEING 767 AIRCRAFT MAINTJul 23, 2025 · N479AZ · Boeing 767323SDR DALA2025072405569Reinforcement · damagedSHIP 3416 TOOLING DAMAGE ON REINFORCEMENT FR63 BETWEEN STR 2R AND STR 3R. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-11. (1101322)Jul 23, 2025 · N416DX · Airbus A330941SDR CALA2025080107211Plate · damagedFRAME 68, S10 - 16. INNER CAP GUSSET PLATE JOINT, ALL FASTENER HOLES HAVE REJECTABLE INDICATIONS. ACP INITIAL INSPECTION OF THE GUSSET HOLES IAW PART 2 OF THE LATEST REV OF ECRA 5341-01508. ACCOMPLISHED REPAIR IAW RCO-L25500.Jul 22, 2025 · N834UA · Airbus A319131SDR DALA2025072905696Pan · scratchedWASTE WATER SERVICE PAN HAS SCRATCHES. REMOVED AND REPLACED WASTE WATER SERVICE PAN IAW A220 ASRP BD500 -J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01342100 REV. -W. (LP# 1099809)Jul 22, 2025 · N118DU · Airbus BD5001A10SDR DALA2025072905694Door Sill · corrodedCORROSION ON FWD CARGO COMPARTMENT DOOR LWR SILL FASTENER HOLES, BETWEEN FR-24 AND FR-29. COMPLIED WITH ER/A 627804-14 REV. ORIGINAL. (LP# 1099778)Jul 22, 2025 · N118DU · Airbus BD5001A10SDR DALA2025072405561Window Frame · cracked(LOG 1099012) CRACK OF 0.150IN ON INNER CORNER RADIUS OF NO. 1 LH WINDOW FRAME. FRAME WAS REPAIRED PER ER/A 619132-14ADTR REV. A.Jul 22, 2025 · N3757D · Boeing 737832SDR DALA2025072405560Window Frame · cracked(LOG 1098988) CRACK ON LH/RH NO.3 WINDOW FRAME FWD LOWER CORNER AT FWD FUSELAGE. CRACK ON LH NO.3 WINDOW FRAME FWD LOWER CORNER AT FWD FUSELAGE WAS REPAIRED PER ER/A 627247-14AD REV. ORIGINAL SECTION I PERMANENT REPAIR AND PRI 627247-14 REV. 4, AND RH NO.3 WINJul 22, 2025 · N3757D · Boeing 737832SDR DALA2025072405558Window Frame · cracked(LOG 1098678) CRACK OF 0.220IN ON INNER CORNER RADIUS OF NO. 1 RH WINDOW FRAME. FRAME WAS REPAIRED PER ER/A 619132-14ADTR REV. A.Jul 22, 2025 · N3757D · Boeing 737832SDR VNA2025F00034Fitting · corrodedCORROSION ON SILL PASSENGER DOOR, CORROSION ON ANGLE KICKPLATE BETWEEN FS319/FS349 AND MID CAP CORROSION ON AFT LOWER FITTING FLOOR BEAN FS349.Jul 21, 2025 · N640NN · Bombdr CL6002D15SDR AALA202509023251Sill Drain · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL AT LEVEL STR 23R BTW FR 66 AND FR 68 AT AFT GALLEY AREA L=2.450 INCH W=2.037 INCH D=0.013 INCH. MAINTENANCE REPLACED LOWER SILL RH SIDE BTW FR66 TO FR68 AND STR23R AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A3Jul 21, 2025 · N767UW · Airbus A319112SDR SWI2025F01077Beam · corrodedAFT WET AREA L/H BEAM BETWEEN FR 86 - FR 89 CORRODED. (C-CHECK RO 08/10/2025)REMOVED AND REPLACED AFT WET AREA L/H BEAM BETWEEN FR 86 - FR 89. REF EMB SRM 51-40-08.REPLACED WIRH OEM PART AND DOES NOT EFFECT WEIGHT AND BALANCE.Jul 21, 2025 · N106SY · Emb ERJ170200LRSDR JJBA20250806004Door Sill · corrodedSERVICE DOOR CENTER SILL BTW FR 20-22 FOUND CORRODED. SERVICE DOOR CENTER SILL BTW FR 20-22 REMOVED FOR REPLACEMENT. SERVICE DOOR CENTER SILL BTW FR 20-22 REPLACEDJul 21, 2025 · N11199 · Emb EMB145XRSDR AALA202508051232Roller · wornAIRCRAFT IN BASE MAINTENANCE: CABIN FORWARD SERVICE DOOR AFT DOOR FRAME, CENTERING ROLLER FITTING HAS WEAR ON UPPER LEG. INSTALLED NEW CENTERING ROLLER FITTING. PER AMM 52-41-00.Jul 21, 2025 · N972AN · Boeing 737823SDR JJBA20250730117Cup · corrodedCF4, TOILET WASTE CUP EXTERNAL SIDE FOUND CORRODED. CF4 TOILET WASTE CUP BLENDED OUT OF LIMITS. TOILET WASTE CUP REMOVED AND REPLACEDJul 21, 2025 · N16147 · Emb EMB145XRSDR CALA2025072406866Seal Depressor · crackedR1 DOOR CUTOUT UPPER FWD CORNER SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED CORNER SEAL DEPRESSOR AT R 1 DOOR CUTOUT UPPER IAW SRM 51-40-02 SRM AND AIPC 53-11--00-80,TREATED AND APPLIED PRIMER IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804, APPLIED TOP COJul 21, 2025 · N17229 · Boeing 737824SDR DALA2025072205518Stiffener · crackedSHIP 3126 CRACK INDICATION FOUND IN HORIZONTAL STIFFENER OF LHS LATERAL WINDOW FR4. CORRECTIVE ACTION: COMPLIED WITH ER/A 569917-14AD. (1097526).Jul 21, 2025 · N326NB · Airbus A319114SDR DALA2025072205515Stiffener · crackedSHIP 3126, CRACK INDICATION FOUND IN HORIZONTAL UPPER STIFFENER OF THE LATERAL WINDOW FRAME AT FR4 LH SIDE. COMPLIED WITH ER/A 569917-14AD. (1097870).Jul 21, 2025 · N326NB · Airbus A319114
Back to JASC 5310