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 DALA2024101009916Vapor Barrier · cracked(LOG 0598314) VAPOR BARRIER LH UPPER ANGLE TO FUEL TANK HAS CRACK AT LBL 8 STA 663. REMOVED, FABRICATED AND INSTALLED VAPOR BARRIER L/H UPPER ANGLE AT STA 663 BETWEEN LBL 6.13 TO LBL 19 IAW B737-800 SRM 57-10-10-2R-5.Oct 7, 2024 · N3730B · Boeing 737832SDR DALA2024100809829Crossbeam · crackedSHIP 3133 CRACKED HOLE #26 CROSSBEAM JUNCTION AREA AT FR20 LH. CORRECTIVE ACTION: PERFORMED REPAIR AS PER 620265-14AD. (0596606)Oct 7, 2024 · N333NB · Airbus A319114SDR DALA2024100809828Post · corrodedSHIP 3144 CORROSION ON LATERAL POST LOWER AREA IN LAV A. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON LAVATORY A AS PER ER/A 620623-14 REV. (0597105)Oct 7, 2024 · N344NB · Airbus A319114SDR CALA2024100802605Crease Beam · corrodedMAIN CABIN RH CREASE BEAM STA 827 I/B END CORROSION REF AAR N/R 9903430 REMOVED AND REPLACED R/H CREASE BEAM WEB AT MAIN CABIN STA 827 TO STA 807 RBL 60 REF SRM 51-40-02-0G-0.Oct 7, 2024 · N39461 · Boeing 737924ERSDR CALA2024100802604Crease Beam · corrodedMAIN CABIN RH CREASE BEAM STA 787 I/B END CORROSION REF AAR N/R 9903429 REMOVED AND REPLACED RT CREASE BEAM WEB AT MAIN CABIN STA 787 TO STA 767 RBL 60 REF SRM 51-40-02-0G-0.Oct 7, 2024 · N39461 · Boeing 737924ERSDR REXA2024120201519Crossbeam · chafedAFT CARGO DOOR CROSSBEAM CHAFED/CUT FROM COUNTER BALANCE CABLES. REPAIREDD AFT CARGO DOOR CROSSBEAM IAW ENDEAVOR AIR EA CRJ753-17469 REV. IR DATED 11/8/2024.Oct 6, 2024 · N371CA · Cndair CL6002C10SDR REXA2024101700882Pressure Deck · misalignedWHILE INCORPORATING SB 670SH-53-043 REV C, WE HAVE ENCOUNTERED MISMATCHED FACTORY PILOT HOLES @FS 843 LBL 18 COMMON TO THE LBL18 FLOOR BEAM AND PRESSURE BOX EXISTING HOLES. REPAIRED BY INSTALLING A FREEZE PLUG IAW MHIRJ REO 690-53-41-502 REV -- DATED 2024-10-Oct 6, 2024 · N582CA · Cndair CL6002D24SDR DALA2024101009902Window Frame · crackedCRACK EVIDENCE ON EXTERNAL CUT OUT OUTBD/INBD UPPER CORNERS OF WINDOW NO. 1 LH AT EXTERNAL FUSELAGE AREA. PERMANENT REPAIR LHS ON EXTERNAL CUT OUT OUTBD/INBD UPPER CORNERS OF LH WINDOW NO. 1 WAS PERFORMED PER ERA NO.619132-14.Oct 6, 2024 · N3733Z · Boeing 737832SDR R61A2024102200468Crossbeam · corrodedCORROSION ON FR17 CROSSBEAM. PERFORMED PERMANENT REPAIR ON CROSSBEAM 17 PER REF SRM-53-00-10/10 REPAIR 03P.Oct 5, 2024 · N403YX · Emb ERJ170200LRSDR R61A2024100800462Window Post · damagedWHILE IN HEAVY CHECK - WHILE ACCOMPLISHING 170EO-53-10-0023 (REPLACE FORWARD FUSELAGE LATERAL POST T SHAPES), 2 EA HOLES WERE MIS-DRILLED ON THE UPPER LH SIDE OF FWD FUSELAGE LATERAL POST. PERFORMED PERMANENT BUSHING REPAIR ON 2 EA HOLES ON THE UPPER LH SIDE Oct 5, 2024 · N227JQ · Emb ERJ170200LRSDR CALA2024100900796Window Post · crackedSUSPECT 2 CRACKS ON L3 FWD WINDOW POST 2ND SCREW UP FROM BOTTOM FWD. SEE ATTACHED PHOTO HFEC INSPECTION REQUIRED, REF SRM 56-10-02-1A-3 PARA. 4 A. FIG 102. CRACK ON 2ND SCREW UP ON LEFT WINDOW POST BETWEEN WINDOWS L2 AND L3. VERIFIED WITH HFEC 1 EA CRACK THAT Oct 5, 2024 · N26232 · Boeing 737824SDR YENA2024100801353Crossbeam · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 2, LOCATED ON CROSSBEAM SPLICING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.106 INCHES, CRACK DIRECTION: 1 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00051) REF AE W/OOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801352Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE A OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00052) REF AE W/O# 2024-214/1. N/R# 2024 - 446434.PERFORMED PERMANENT REPOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801351Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00053) REF AE W/O# 2024-214/1. N/R# 2024 - 446435. PERFORMED PERMANENT REOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801350Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00054) REF AE W/O# 2024-214/1. N/R# 2024 - 446436. PERFORMED PERMANENT REOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801349Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00048) REF AE W/O# 2024-214/1. N/R# 2024 - 446433. PERFORMED PERMANENT REOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801348Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL FITTING LAYER AT THE UPPER AND LOWER INBOARD HOLES OF DOOR STOP FITTING 7 LOCATED FRAME 16 RH AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00055) REF AE W/O# 2024-214/1. N/R# 2024 - 446432Oct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801347Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00056) REF AE W/O# 2024-214/1. N/R# 2024 - 446437. PERFORMED PERMANENT REOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801346Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC, BWT FR, 55 TO FR, 57 IN AFT CARGO COMPARTMENT (CPCP FINDING);(RESOLVED ON W/O: 1311389 TASKCARD: NR-00057) REF AE W/O# 2024-214/1. N/R# 2024 - 446603. REMOVED AND REPLACED STRINGER 43L LOC, BET FR 55 TO FR Oct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801345Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA RH SIDE FROM UPPER TENSION BOLT IN INBORD VERTICAL FLANGE. CRACK DIRECTION IS 10 O'CLOCK, CRACK LENGTH IS 0.080 INCH APPROX IN COCKPIT; (RESOLVED OOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801344Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA LH SIDE FROM UPPER TENSION BOLT IN I/B VERTICAL FLANGE. CRACK DIRECTION IS 2 O'CLOCK LENGTH IS 0.140 INCH APPROX IN COCKPIT; ARM W/O 2024 214/1 N/ROct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801343Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68RH SIDE AT LOWER I/B HOLE OF DOOR STOP FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00066) REF: ARM W/O 2024 214/1 N/R 2024-446438. PERFORMED REPAIR ON FRAME 68 RH SIDE AT LOWER INBOOct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801342Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STO P FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00067) PERFORMED REPAIR ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STOP FITTING 1 AT Oct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801340Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH & RH LOWER FASTENERS AREA / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9035-24 COVER REV.0 & PART 1-6 /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03Oct 5, 2024 · N559JB · Airbus A320232SDR YENA2024100801339Door Frame · damagedDURING HEAVY MAINTENANCE, REAR FUSELAGESB53-1491 DOOR STOP FITTING NR 1 STR 22L FR 68 HOLE FILLET RADIUS CRACKED PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS 1-4) /2/ AIRBUS RDAF 81468047/003/2024#B /3/ AIRBUS DOSSIER 81468047 /4/ AIOct 5, 2024 · N559JB · Airbus A320232SDR SWIA20250124004Door Frame · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA29701-690-53-21-032 170PQ-DTI - MAIN AVIONICS DOOR CUT-OUT FROM APPROX. F.S. 364.00 TO F.S. 394.00 HAS SEVERAL GOUGES & CORROSION ON FWD & AFT SIDES & ON L/H & R/H SIDE.REMOVED ALL DAMAGE REF 690-53-21-032. PEOct 4, 2024 · N170PQ · Cndair CL6002D24SDR AALA202412099973Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN FASTENER HOLES AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 358669.Oct 4, 2024 · N748UW · Airbus A319112SDR AALA202412094716Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN FASTENER HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 358669.Oct 4, 2024 · N748UW · Airbus A319112SDR SWI2024F01256Crossbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 14 BELOW FORWARD GALLEY AREA. (C-CHECK RO 10/30/2024) (FILED CLOSED) PERFORMED PERMANENT DOUBLER REPAIR ON FR 14 CROSS BEAM REF. SRM 53-00-10 /REPAIR 03P. CHANGE IN WEIGHT 563.26 GRAMS. CAL. TOOL I.D.#Oct 4, 2024 · N610CZ · Emb ERJ170200LRSDR SWI2024F01255Crossbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 17 UNDER WARDROBE AREA. (C-CHECK RO 10/30/2024) (FILED CLOSED) REMOVED DAMAGE SECTION OF MAIN CABIN FORWARD WET AREA CROSS BEAM FR 17 UNDER WARDROBE AREA BY CUTTING AWAY DAMAGE. FABRICATED AND INSTALLEOct 4, 2024 · N610CZ · Emb ERJ170200LRSDR SWI2024F01177Crossbeam · corrodedCORROSION FOUND ON RH CROSSBEAM AT F.S 280.00 BULKHEAD #28943546 (C-CHECK RO 11/6/2024) RH CROSSBEAM AT F.S 280.00 FOUND OUT OF LIMITS, REPLACED WITH NEW CROSSBEAM. REF. CRJ700 SRM SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51Oct 4, 2024 · N787SK · Cndair CL6002C10SDR SWI2024F01176Crossbeam · corrodedLH CROSSBEAM AT FS 280.00 HAS CORROSION TRANS# 28943506 (C-CHECK RO 11/6/2024) REPLACED THE CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-340Oct 4, 2024 · N787SK · Cndair CL6002C10SDR FDEA202410041470Crossbeam · corrodedMAIN DECK FLOOR STRUCTURE FOUND CROSSBEAM CORROSION AT FR47 AND Y370 AREA. REMOVED CORROSION CROSSBEAM AND INSTALLED NEW CROSSBEAM I.A.W A300-600F SRM 51- 72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT Oct 4, 2024 · N671FE · Airbus A300F4605RSDR REXA2024100700856Door Frame · crackedL/H AFT OVER WING EMERGENCY EXIT DOOR (SN SB1485) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED L/H AFT OVER WING EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-17346 REV. IR DATED 9/25/2024.Oct 4, 2024 · N325PQ · Cndair CL6002D24SDR REXA2024100700855Door Frame · crackedL/H FWD OVER WING EMERGENCY EXIT DOOR (SN SB1487) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED L/H FWD OVER WING EMERGENCY. EXIT DOOR IAW ENDEAVOR EA CRJ952-17345 REV. IR DATED 9/25/2024Oct 4, 2024 · N325PQ · Cndair CL6002D24SDR CALA2024100702589Window Frame · crackedREF EA 5310-08195 OP002 CRACK FOUND ON SECOND LOWER FASTNER AT R/ H NO.3 WINDOW FRAME REF AAR N/R 9909581 ACCOMPLISHED R/H SIDE NO.3 WINDOW FRAME POST PERMANENT REPAIR. EA 5310-08195 REV ORIG OP004 WHICH CONSIST ON R/H NO.3 WINDOW FRAME INSP COLD WORKING ANDOct 4, 2024 · N37408 · Boeing 737924SDR CALA2024100702586Window Frame · crackedREF EA 5310-08195 OP001 CRACK FOUND ON SECOND LOWER FASTNERB AT L/H NO.3 WINDOW FRAME REF AAR N/R 9909580 ACCOMPLISHED L/H SIDE NO.3 WINDOW FRAME POST PERMANENT REPAIR PATTERN PERMANENT REPAIR INSTALLATION I.A.W EA 5310-08195 REV ORIG OP003 WHICH CONSIST ON L/Oct 4, 2024 · N37408 · Boeing 737924SDR CALA2024100702571Fitting · crackedFLIGHT DECK, WINDSHIELD CONTINUITY FTG HAS CRACK INDICATION APPR OX .400 INCH OUT FROM CTR POST ON HORIZONTAL LEG ON LH AND RH SI DE. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLI GHT". RECEIVED FINAL RFTS #4 OPS 60006 WITH INSTRUCTION TO ACCOMOct 4, 2024 · N882UA · Airbus A319132SDR DALA2024100509717Window Frame · crackedSHIP 3133 FUSELAGE NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH & RH CRACK DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 620123-14AD. (0591827)Oct 4, 2024 · N333NB · Airbus A319114SDR DALA2024100509716Window Frame · crackedSHIP 3133 FUSELAGE NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH & RH CRACK DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 620123-14AD. (0591818)Oct 4, 2024 · N333NB · Airbus A319114SDR VNAA202410030022Support Frame · corrodedHN00177438 DISCREPANCY: FS 794 BELLY FAIRING SUPPORT FRAME IS CORRODED. CORRECTIVE ACTION: REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-82-660 REV. -- DATED 2024-09-03.Oct 4, 2024 · N716PS · Cndair CL6002C10SDR JR2R20241004206Doubler · corrodedINTERNAL SIDE OF POTABLE WATER DRAIN MAST STRUCTURE AND DRAIN MAST DOULBER CORRODED AT FR86 TO FR87 BETWEEN STR27R AND STR28R. REPLACED INTERCOSTALOct 4, 2024 · N87303 · Emb ERJ170200LRSDR JR2R20241004480Crossbeam · corrodedCROSSBEAM AT FR84 RBL14 - RBL30 HAS AREAS OF CORROSION. REPAIREDOct 4, 2024 · N87303 · Emb ERJ170200LRSDR AALA202412113987Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 2 ZONE 2. CRACK DEPTH IS 0.219 INCH AND CRACK DIRECTION IS 9 OCLOCK. MAINTENANCE PERFORMED INTERIM REPAIR ON FASTENER HOLE OOct 3, 2024 · N748UW · Airbus A319112SDR AALA202412117770Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 5 ZONE 2. (CRACK DEPTH: 0.202 INCHES). MAINTENANCE ACCOMPLISHED REPAIR LOC. HORIZONTAL FLOOR BEAM AND VERTICAL STRINGER IN CENOct 3, 2024 · N748UW · Airbus A319112SDR AALA202412116958Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 4 ZONE 1 (CRACK DEPTH:0.212 INCHES). MAINTENANCE ACCOMPLISHED REPAIR ON HORIZONTAL FLOOR BEAM AND VERTICAL STRINGER IN CENTER Oct 3, 2024 · N748UW · Airbus A319112SDR CALA2024120503020Door Frame · corrodedAPU DOOR INTERNAL SURROUND STRUCTURE HAS SEVERAL AREAS OF CORROSION FWD, AFT & O/B.Oct 3, 2024 · N14121 · Boeing 757224SDR SWI2024112701296Striker · dentedPASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN IS DENTED STGR4L & STGR5L. (MARKED IN RED) (C-CHECK RO 11/26/2024) PERFORMED REPAIR OF PASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN STGR4L & STGR5L BY COMPLYING WITH ALL Oct 3, 2024 · N706SK · Cndair CL6002C10SDR SIMA20241003008Crossbeam · corrodedFWD GALLEY, THERE IS CORROSION ON THE RH FLOOR CROSS BEAM AT FR 14. SSI 53-10-027 (MAJOR REPAIR) (LEVEL 2 CORROSION). PERFORMED REPAIR OF RH FLOOR CROSSBEAM AT FR.14 IN FWD GALLEY IAW EMB 175 SRM 53-00-10, RE-03P, ITEM 6, TABLE204, FIGURE 203Oct 3, 2024 · N323ED · Emb ERJ170200LRSDR SIMA2024102303006Crossbeam · corrodedFWD GALLEY, THERE IS CORROSION ON THE CENTER CROSS BEAM AT FR 17. SSI 53-10-027. (MAJOR REPAIR) (LEVEL 2 CORROSION). REPAIRED CORROSION ON CENTER CROSS BEAM AT FR.17 IN FWD GALLEY IAW EMB 175 SRM 53-00-10Oct 3, 2024 · N323ED · Emb ERJ170200LR
Back to JASC 5310