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 SWIA202312080002Unknown · gougedUPON REPLACEMENT OF THE RH SIDE WINDOW, FOUND GOUGE DAMAGE AT 3 LOCATIONS ON THE WINDOW SILL (AIRFRAME SIDE). ALL 3 LOCATIONS COINCIDE WITH THE 3 MOUNTING SLING HOLES ON THE WINDOW (1 UPPER, AND 2 LOWR HOLES). SUSPECT DAMAGE WAS CAUSED BY THE SLING DURING PREVDec 2, 2023 · N548CA · Cndair CL6002D24SDR AALA202312065643Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR LOWER FORWARD FRAME DOUBLER AT BS 344, S17R. REPAIRED FRAME PER SRM 51-70-11-2R.Dec 2, 2023 · N932AN · Boeing 737823SDR SWAA2023120526975Door Frame · crackedEXT. POWER DOOR FRAME CRACKED AT APPROX 6OCLOCK POSITION.<[01] REMOVED DAMAGED SECTION OF SURROUND DOUBLER PER SRM 53-10-15-2R-4; REPAIR 4;[02] ACCOMPLISHED HFEC OF CUTOUT PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] REPAIRED PER SRM 53-10-15-Dec 2, 2023 · N8601C · Boeing 7378H4SDR AALA202402017025Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.Dec 1, 2023 · N659AW · Airbus A320232SDR SWIA202401301201Door Frame · corrodedCORROSION NOTED ON 3EA CHORD INNER REINFORCEMENTS AT AFT CARGO DOOR SURROUND STRUCTURE BETWEEN FS 1000.00 - FS 1051.00 #27497074 (C-CHECK RO 1/30/2024) INSTALLED 3EA NEW CHORD INNER REINFORCEMENTS AT AFT CARGO DOOR SURROUND STRUCTURE BETWEEN FS 1000.00 - FDec 1, 2023 · N746SK · Cndair CL6002C10SDR VNA2023F00010Frame · corrodedHN 118841 DISCREPANCY: CIRCUMFERENTIAL JOINT INTERFACE IS CORRODED BETWEEN FS 280 AND FS 286.86 BETWEEN STGR 25L AND STGR 25R. CORRECTIVE ACTION: COMPLIED WITH OLIVER WYMAN EA 23-C9-53-1623 REV IR DATED 11/02/2023.Dec 1, 2023 · N558NN · Cndair CL6002D24SDR VNAA202312010021Former · corrodedHN116503 DISCREPANCY: FWD FORMER AT PAX DOOR IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-021-001-001-A01.Dec 1, 2023 · N535EA · Cndair CL6002C10SDR VNAA202312010013Access Panel · corrodedHN 116286 DISCREPANCY: PANEL 542BZ HAS LIGHT CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PANEL.Dec 1, 2023 · N535EA · Cndair CL6002C10SDR VNAA202312010009Drag Angle · crackedHN 115604 DISCREPANCY: PASSENGER DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST CABLE PULLEY MOUNT CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-14-001-001-A01.Dec 1, 2023 · N535EA · Cndair CL6002C10SDR YENA2023120501545Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHEM ENT INTERNAL AREA FROM UPPER TENSION BOLT LH SIDE, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGTH IS 0.135 INCH, IN COCKPIT (1 EA); ALL WORK ACCMPLISHED ON AE WO 2023-2Nov 30, 2023 · N535JB · Airbus A320232SDR YENA2023120501544Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA FROM UPPER TENSION BOLT RH SIDE, CRACK DIRECTION IS 10 OCLOCK, CRACK LENGTH IS 0.105 INCH, IN COCKPIT (1 EA); ALL WORK ACCOMPLISHED ON AE WO # 2023Nov 30, 2023 · N535JB · Airbus A320232SDR YENA2023120501529Window Frame · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST UPPER FASTENERS LH & RH AREA / CRACKS - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)Nov 30, 2023 · N535JB · Airbus A320232SDR DALA2023113009840Unknown · unknownCORROSION ON DOOR JAMB LOWER AT AFT CARGO DOOR. SUMMARY OF NRC 00067: CORROSION LEVEL 2. DOOR JAMB LOWER AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 53-20-15-2R REP 7. (LP #0088493)Nov 30, 2023 · N892AT · Boeing 717200SDR SWIA2024020231129Door Frame · damagedPERFORM PERMANENT REPAIR TO FWD LOWER CORNER OF CARGO DOOR CUT OUT (C-CHECK RO 2/1/2024) REPAIRED FWD LOWER CORNER OF CARGO DOOR CUT-OUT IAW CRJ200 SRM 53-61-31 AND MHIRJ REO 601R-53-61-8128 REV.-- 2023-12-20, NDT PERFORMED BY BARON NDT,LLC, FAA CRS#5NDR54Nov 29, 2023 · N464SW · Cndair CL6002B19SDR AALA202402017716Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP FITTING #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.Nov 29, 2023 · N752US · Airbus A319112SDR SWAA2024010325975Pressure Deck · cracked.5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 LBL 41. CORRECTION ==.5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 RBL 41<[01] CORRECTION TO TITLE:<BR>INCORRECTLY PUT 'LBL 41'<BR>CORRECT LOCATION IS RBL 41.;[02] REPAIRED HORIZONTAL PRESSURE DNov 29, 2023 · N7730A · Boeing 7377BDSDR LR7A2023112903334Fitting · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT UNDERFLOOR LH FS537 BULKHEAD FITTING CORRODED LBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0435. / PSE# 53-40-11, Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903333Fitting · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT RH FS457 RING SEGMENT TO FLOOR BULKHEAD FITTING CORRODED, RBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0434. / PSNov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903332Fitting · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT RH FS437 RING SEGMENT TO FLOOR BULKHEAD FITTING CORRODED, RBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0433. / PSE#Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903331Fitting · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT RH FS297 RING SEGMENT TO FLOOR BULKHEAD FITTING CORRODED, RBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0432. / PSENov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903330Fitting · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT RH FS277 RING SEGMENT TO FLOOR BULKHEAD FITTING CORRODED, RBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0431. / PSE#Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903329Beam · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD FUSELAGE BEAM UPPER CAP CORRODED AT FS132, RBL40, WL195. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-30-13. NR# 0430 / PSE# 53-30-14, AD 2012-06-09Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903318Beam · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5323, FOUND LH MLG WHEEL WELL WL200 BEAM WEB HAS MULTIPLE CRACKS AT FS573 AND FS591 LBL61-85 APPROXIMATELY 1.25 TO 1.75 INCHES IN THOSE SPOTS. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 &Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903314Beam · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5324, FOUND RH MLG WHEEL WELL WL200 BEAM CRACKED AT FS573, RBL74. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0100. / PSE# 53-40-16, AD 2012-06-09Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903313Fitting · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HCHC5314, FOUND CARGO COMPARTMENT FS577 UNDERFLOOR BULKHEAD END FITTING CRACKED AT LBL61, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0094. / PSE# 53-40-18, AD 2012-06Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903310Stiffener · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC3215, FOUND STIFFENER IN THE NLG WHEEL WELL FOUND CRACKED IN CUT OUT RADIUS AT FS206, WL142, BL0. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0091.Nov 29, 2023 · N410LC · Lkheed 382GSDR LR7A2023112903304Riser Panel · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5324, FOUND RH MLG WHEEL WELL FS477 WEB RISER CRACKED AT RBL82, WL210. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0063. / PSE# 53-40-17, AD 2012-06-09Nov 29, 2023 · N410LC · Lkheed 382GSDR DALA2023113009839Unknown · unknownINAPPROPRIATE HOLES ON VERTICAL BEAMS STA Y=817 AND STA X=0, X=13, 25, X=-13, -25 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00184: VERTICAL BEAMS ON STA Y=817, X=13, X=25, X=-13, X=-25 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B717 SRM 51-70-11-2R-2. BEAMNov 29, 2023 · N934AT · Boeing 717200SDR DALA2023113009838Unknown · unknownCRACK FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R. SUMMARY OF NRC 00259: PERMANENT REPAIR ON FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R WAS PERFORMED PER PRI 613338-14Nov 29, 2023 · N934AT · Boeing 717200SDR DALA2023112909802Unknown · unknownCORROSION ON LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 AT AFT PAX CABIN. SUMMARY OF NRC 00250: CORROSION LEVEL 2. LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 WAS REPAIRED PER ER/A 613464-14 REV ORIGINALNov 29, 2023 · N934AT · Boeing 717200SDR HNAA2024011700025Crossbeam · crackedE011531 NLG UPLOCK BOX CROSSBEAM LH SUPPORT P/N 123-02685-001 IS CRACKED. REPLACED IAW PIEDMONT FCD1-53-20-0237Nov 28, 2023 · N648AE · Emb EMB145LRSDR DALA2023120109879Unknown · unknownSHIP 1602 MEC ACCESS DOOR CUTOUT FWD FRAME FOUND PUNCTURE. CORRECTIVE ACTION: FOR FUTURE INSPECTION CARRY OUT AS PER ERA 613820-14AD (0085099)Nov 28, 2023 · N1602 · Boeing 767332SDR SWAA2023113025476Panel · delaminated193 B PANEL HAS DELAM AND CHIP OUT AREA MISSING ON INNER MATERIAL EDGE ON THE SAME FORWARD LEFT HAND CORNER LEADING EDGE.<[01] VERIFIED REPLACEMENT OF 193 B PANEL IAW SRM 53-40-70.;[02] DRILLED AND INSTALLED NEW 193B PANEL; REF. SRM 51-40-02.Nov 28, 2023 · N928WN · Boeing 7377H4SDR IPXA2023112901346Unknown · unknown*SDR FILED OPEN* FOUND DAMAGE ON PANEL 194BR.Nov 28, 2023 · N610UP · Boeing 7478FSDR IPXA2023112901352Unknown · unknown*SDR FILED OPEN* FOUND DAMAGE ON PANEL 194CRNov 28, 2023 · N610UP · Boeing 7478FSDR IPXA2023112901370Unknown · unknown*SDR FILED OPEN* FOUND DAMAGE ON PANEL 194FR.Nov 28, 2023 · N610UP · Boeing 7478FSDR IPXA01354Unknown · unknown*SDR FILED OPEN* FOUND DAMAGE ON PANEL 194DR.Nov 28, 2023 · N610UP · Boeing 7478FSDR YENA2023113001515Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00012 ) FUR-A320-53-00976, REF ANov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001514Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; REF AEROMAN N/R 20232-631118, PERFORMED REPAIR ON DOOR STOP FITTING #7 FR Nov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001512Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA LH SIDE CONTINUITY FITTING, CRACK LENGTH IS 0.180 INCH, IN COC KPIT (1 EA); ROTOTEST INSPECTION IN OPEN FASTENER 3 HOLES OF LH AND RH SIDES IAW NTM 51-10-0Nov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001511Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK LENGTH IS 0. 100 INCH, CRACK DIRECTION IS 2 OCLOCK, IN COCKPIT (1 EA); REMOVED AND REPLACED MIRROR FITTINNov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001510Unknown · unknownDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 RH SIDE, FRAME 68; CRACK LOCATION: 06 OCLOCK , CRACK DEPTH: 0.145 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00024 ) PENov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001509Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 LH SIDE, FRAME 68; CRACK LOCATION: 06 AND 12 OCLOCK , CRACK DEPTH:0.187 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00025 ) PERFORMED REPAIR ON FNov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001505Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON UPPER SURFACE OF THE UPPER SKIN OF THE C ENTER WING BOX FR41 TO FR42 ON LH SIDE IN PASSENGER CABIN (CPCP RELATE D REFER MPD TASK 571157-01); REF AEROMAN NR 2023-631067 WO 2023 358/1 PERFORMED PERMANENT REPNov 27, 2023 · N562JB · Airbus A320232SDR YENA2023113001504Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER ATTACHMENT AREA AND CONTINUITY FITTING / CRACKS - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Nov 27, 2023 · N562JB · Airbus A320232SDR AALA202403127083Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE LEFT HAND PRESSURE DECK PANEL CRACKED AT FR 36 BETWEEN +Y1292 AND +Y1523. REPAIRED PRESSURE DECK PANEL PER EA 349780.Nov 26, 2023 · N752US · Airbus A319112SDR AALA202403122975Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER FUSELAGE RIGHT HAND PRESSURE DECK PANEL CRACKED AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK PANEL PER EA 349780.Nov 26, 2023 · N752US · Airbus A319112SDR YENA2023112901479Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT POCKET RH SIDE, UPPER TENSION BOLT, CRACK DIRECTION IS 10 OCLOCK, C RACK LENGTH IS 0.090 INCH APPROX, IN COCKPIT (1 EA); REF AEROMAN 2023 - 556997 W/O:2023 275/1Nov 26, 2023 · N552JB · Airbus A320232SDR YENA2023112901478Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT POCKET LH SIDE, UPPER TENSION BOLT, CRACK DIRECTION IS 2 OCLOCK, CR ACK LENGTH IS 0.130 INCH APPROX, IN COCKPIT (1 EA); REF AEROMAN NR 2023 - 556996 W/O:2023 27Nov 26, 2023 · N552JB · Airbus A320232SDR YENA2023112901477Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT POCKET RH SIDE, LOWER INBOARD RADIUS, CRACK LENGTH IS 0.200 INCH AP PROX, IN COCKPIT (1 EA); REF AEROMAN NR 2023-556885 WO 2023 275/1, ACCOMPLISHED THE REPAIR ONov 26, 2023 · N552JB · Airbus A320232
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