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 IPXA2022042181363Channel · crackedINSPECTION TYPE:3CLOWER VERTICAL STAB UNDER PICKLE BARREL SUPPORT ANGLE IS CRACKED AT BOTH END.REMOVED, FABRICATED AND REPLACED ANGLE/CHANNEL IAW DWG. AJC7372 AND SRM 51-35-01. (MINOR)Apr 9, 2022 · N285UP · Doug MD11FSDR CALA2022041100951Failsafe · crackedSUPPORT TASK - EA5340-01385 OP001, AD2012-09-04, 2EA CRACK INDICATION: FOUND ON FAIL SAFE STRAP RUNNING FWD AND AFT OF THE FASTENER HOLE ON LH STA955 REAR SPAR BULK HEAD FAIL SAFE STRAP. TRANSFER REF. NON - ROUTINE WO.637932 AND ORIGINATED BY EMP V925917 FUSELApr 9, 2022 · N78060 · Boeing 767424ERSDR CALA2022041100950Failsafe · crackedSUPPORT TASK - EA5340-01385 OP002, AD2012-09-04, 2EA CRACK INDICATIONS FOUND ON FAIL SAFE STRAP RUNNING FWD AND AFT OF THE FASTENER HOLE ON RH STA955 REAR SPAR BULK HEAD FAIL SAFE STRAP. TRANSFER REF. NON - ROUTINE WO.637883 AND ORIGINATED BY EMP V925917 FX RHApr 9, 2022 · N78060 · Boeing 767424ERSDR CALA2022041100945Fitting · damagedREF LP 8282032 PLANNING TO CONTACT ENGINEERING BEFORE AC4010 REA CHES 60391TFC / 130942TFH WHICHEVER OCCURS FIRST PER STEP 37 OF ECRA 5321-02067 LATEST REV OF ECRA 5321-02067 INTERIM REPAIR ACCOMPLISHED PER ECRA 5321-02067 PART 1. PLANNING TO CONTACT ENGINEERIApr 9, 2022 · N810UA · Airbus A319131SDR IPXA2022042181364None · crackedINSPECTION TYPE:3CLONG. 27R TRUSS FITTING IS CRACKED AT STA. 1159.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. AFA7605 AND SRM 51-33-01. (MINOR)Apr 8, 2022 · N285UP · Doug MD11FSDR IPXA2022042181353Splice · crackedINSPECTION TYPE:4CFOUND LONGERON 49R PRODUCTION SPLICE FITTING CRACKED BETWEEN STA 5-113 AND 1541.REPLACED PRODUCTION SPLICE P/N A5A7114-511 IAW MD11 SRM 51-31-01. (MINOR)Apr 8, 2022 · N281UP · Doug MD11FSDR IPXA2022041881284Frame · crackedINSPECTION TYPE:SEG1DENT AT AFT CARGO FRAME STA 1340, S-26RACCOMPLISHED REPAIR IAW UPS RCD 251327 AND SRM 53-00-07-2R-5 DETAIL I, PER SRM 53-60-07-02RApr 8, 2022 · N421UP · Boeing 75724APFSDR N6WA2022041202Beam · crackedR/H FS280.00 BEAM HAS CRACK. FABRICATED AND INSTALLED NEW 280 BEAM IAW CRJ 700 SRM 51-47-00 AND 51-40-11.Apr 8, 2022 · N551GJ · Cndair CL600*SDR COEA2022052501911Floorbeam · crackedWO 235607 NR 200025 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE, L/H LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 31.CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.Apr 7, 2022 · N911FX · Aerosp 262A12NORDSDR IPXA2022042181362Tee Fitting · crackedINSPECTION TYPE:3CCENTER AUX TANK FWD. SPAR FITTING BETWEEN STA. X=46 & X=81 IS CRACKED.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. APB7351 AND SRM 51-31-01. (MINOR)Apr 7, 2022 · N285UP · Doug MD11FSDR IPXA2022042181361None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 46R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)Apr 7, 2022 · N285UP · Doug MD11FSDR IPXA2022042181360None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49L.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)Apr 7, 2022 · N285UP · Doug MD11FSDR IPXA2022042181359None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 48R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)Apr 7, 2022 · N285UP · Doug MD11FSDR IPXA2022042181358None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)Apr 7, 2022 · N285UP · Doug MD11FSDR IPXA2022041881283Frame · dentedINSPECTION TYPE:SEG1FRAME AT STA 1560, HAS 2 DENTS ON INNER CHORD, O/B OF S-26RACCOMPLISHED REPAIR IAW UPS RCD 251229 AND SRM 53-00-07-2R-5 DETAIL I, PER SRM 53-60-07-02RApr 7, 2022 · N421UP · Boeing 75724APFSDR IPXA2022041881282Frame · dentedINSPECTION TYPE:SEG1FRAME AT STA 1600, HAS A DENT AT S-25RACCOMPLISHED REPAIR IAW UPS RCD 251228 AND SRM 53-00-07-2R-5 DETAIL III, PER SRM 53-60-07-02RApr 7, 2022 · N421UP · Boeing 75724APFSDR MASA20220413189Skin · corrodedIN REF NRC S/N 00352, DURING STRINGER 21RH REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R). IT WAS REPAIRED PER EA 81-2022-044 REV. IRApr 7, 2022 · N904FJ · Cndair CL6002D24SDR SIMA20220407003Panel Support · corrodedSSI 53-23-005 AFT GALLEY RH PANEL SUPPORT CORRODED AT FR 89 (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY RH SUPPORT AT FR 89 IAW EMB 175 SRM 51-40-08Apr 7, 2022 · N226NN · Emb ERJ170200LRSDR SIMA20220407002None · corrodedSSI 53-23-005 AFT GALLEY RH BEAM SPLICE CORRODED AT FR 90 (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY RH BEAM SPLICE AT FR 90 IAW EMB 175 SRM 51-40-08Apr 7, 2022 · N226NN · Emb ERJ170200LRSDR JR2R8463518Crossbeam · corrodedCROSSBEAM 17 CORRODEDApr 7, 2022 · N88301 · Emb ERJ170200LRSDR IPXA2022042581436Longeron · corrodedINSPECTION TYPE:2CCENTER CARGO LONGERON 49R HAS CORROSION AT STA. 5-93/1541.REPAIRED CORRODED CENTER CARGO LONGERON 49R BETWEEN STA. 5-103 TO 5-123 IAW VT-SAA EA 011-5310-01-A9540 REV. I/R AND UPS EO MD11-5310-83411-A. (MAJOR) REF FAA FORM 8100-9 BY. S. KANG (Apr 6, 2022 · N281UP · Doug MD11FSDR IPXA2022042181352Longeron · corrodedINSPECTION TYPE:4CEXTERIOR FUSELAGE LONGERON 28R P/N AEA7545-2 HAS CORROSION BETWEEN STA Y=1207 - Y=1305.5.REPAIRED CORRODED LONGERON 28R P/N AEA7545-2 IAW EA 011-5300-01-A9541 REV I/R AND UPS EO MD11-5310-83430-A (MINOR)Apr 6, 2022 · N281UP · Doug MD11FSDR FDEA202204060879None · noneBODY STATION 16401 STRINGER 14L INTERCOSTAL TEE CLIP HAS A CRACK INDICATION AT THE LOWER INNER FASTENER HOLE. ACCOMPLISHED FEDEX EA# F-5310-T0367855 P1 - FUSELAGE - MAINFRAME - FRAME WEB - STA 1640 S-14L, CRACK INDICATION* THIS EA DEVIATES FROM EO# F-5310Apr 6, 2022 · N793FD · Boeing 757SDR IPXA2022041881255Stiffener · crackedINSPECTION TYPE:1CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 LON 49R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-33-01 AND 51-35-01 (MINOR).Apr 6, 2022 · N281UP · Doug MD11FSDR IPXA2022041681208Stiffener · crackedINSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-11 HAS A CRACK AT STA 1841.REMOVED, FAB AND REPAIRED THE CRACKED STIFFENER P/N AGA7170-11 IAW MD11 51-31-01 AND 51-35-01 (MINOR)Apr 6, 2022 · N281UP · Doug MD11FSDR IPXA2022041681207Stiffener · crackedINSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-9 THAT IS CRACKED AT STA 1841.REMOVED,FAB AND REPLACED THE CRACKED STIFFENER P/N AGA7170-9 IAW MD11 SRM 51-31-01 AND 51-35-01 (MINOR)Apr 6, 2022 · N281UP · Doug MD11FSDR IPXA2022041681206Longeron · corrodedINSPECTION TYPE:4CEXTERIOR FUSELAGE , LONGERON 28L P/N AEA7545-1 HAS CORROSION BETWEEN STA 1304-1309.REPAIRED CORRODED LONGERON 28L P/N AEA7545-1 IAW EA 011-5300-01-A9539 I/R AND UPS EO MD11-5310-83429-A (MINOR)Apr 6, 2022 · N281UP · Doug MD11FSDR SIMA20220406001Floorbeam · corrodedFOUND RH CENTER FLOOR BEAM TO HAVE CORRODED GUSSET PLATE AT FR 90 (LEVEL 2 CORROSION)-C/A-RAR RH CENTER FLOOR BEAM GUSSET PLATE AT FR 90 IAW EMB 175 SRM 51-40-08Apr 6, 2022 · N226NN · Emb ERJ170200LRSDR CALA2022040800911Skin · stainedFLOOR SUPPORT STRUCTURE BELOW AFT R/H LAV HAS BLUE WATER RESUIDU E AT STA 1620-1681 S29R - S29L. CLEANED FLOOR SUPPORT STRUCTURE BELOW RH LAV STA 1620-1681 S29R- 29L IAW SOPM 20-30-03 AND ECRA 2011-01000.Apr 6, 2022 · N29124 · Boeing 757224SDR FDEA202204060871Longeron · crackedCENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT SUSPECT CRACK. CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT REPAIR CARRIED OUT AS PER SRM 53-00-05-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.Apr 6, 2022 · N623FE · Doug MD11FSDR IPXA2022041681205Stiffener · crackedINSPECTION TYPE:3CL/H MLG WHEEL WELL HAS A STIFFENER THAT IS CRACK AT AFT O/B WEB.REMOVED, FAB, AND REPLACED THE CRACK STIFFENER IAW DWG ANB7203, MD11 SRM 51-31-01 AND 51-35-01. (MINOR)Apr 5, 2022 · N285UP · Doug MD11FSDR SIMA20220405003Shear Tie · corrodedSHEAR CLIP LOCATED AT FR 88 JUST OTBD OF STR 28R HAS CORROSION ON INBD SIDE (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED SHEAR CLIP AT FR 88 JUST OUTBOARD OF STRG 28R IAW EMB 175 SRM 51-40-08. SEE WIPS AND TASKS FOR DETAILSApr 5, 2022 · N222NS · Emb ERJ170200LRSDR CALA2022040600892Beam · corrodedCORROSION ON CABIN FLOOR STRUCTURE RH DOOR SILL BEAM AT FR68 PER HAECO LCQ N/R 9296748/28748 GENERATED BY V061619. REPAIRED R2 DOOR SILL BEAM IAW A319 SRM 53-41-14-300-001. MECH B Y V061619 INSP BY V901665Apr 5, 2022 · N807UA · Airbus A319131SDR CALA2022040600891Beam · corrodedCORROSION ON CABIN FLOOR STRUCTURE LH DOOR SILL AT FR 68 A3NB-53 -3-6187.PER HAECO LCQ N/R 9296661/ 28661 GENERATED BY V892443. REPAIRED L2 DOOR SILL BEAM IAW SRM53-41-14-300-001.) MECH BY V06 1619 INSP BY V901665.Apr 5, 2022 · N807UA · Airbus A319131SDR SWAA2022050391175Intercostal · brokenBROKEN WEB - INTERCOSTAL LOCATED BS500C TO BS50D AND STR25R AT FWD CARGO COMPARTMENT 2022-165372 / [01] FAULT RAISED IN ERROR DESCRIPTION ENTER BY ERROR RAISED NEW FAULT TTG8Q00BNXRF TO REPLACED WEB;[02] FAULT RAISED IN ERROR DESCRIPTION ENTER BY ERROR RAISED Apr 4, 2022 · N427WN · Boeing 7377H4SDR SWAA2022050391176Intercostal · brokenBROKEN WEB - INTERCOSTAL LOCATED BS500D TO BS520 AND STR25R AT FWD CARGO COMPARTMENT 2022-165372 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED BS500D TO BS520 AND STR25R AT FWD CARGO Apr 4, 2022 · N427WN · Boeing 7377H4SDR SWAA2022050391014Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV 2022-168797 / [01] INSTALLED INTERCOSTAL AND FASTENERS LOCATED BS277 TO BS294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV -<BR>SEE INDIVApr 4, 2022 · N948WN · Boeing 7377H4SDR SWAA2022050391020Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2022-168799 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND DRAWING 141A54Apr 4, 2022 · N948WN · Boeing 7377H4SDR SWAA2022050391021Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV 2022-168801 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV IA W B737-700 SRM 51-40-02 AND DRAWING 141A5400 Apr 4, 2022 · N948WN · Boeing 7377H4SDR SWAA2022050391022Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 11 FWD GALLEY AND LAV 2022-168803 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWGApr 4, 2022 · N948WN · Boeing 7377H4SDR FDEA202204040833Splice · corrodedFORWARD CARGO BILGE FROM STATION 1119 - 6-10 LONGERON 52 SPLICE FITTING FOUND CORROSION. FORWARD CARGO BILGE FROM STATION 1119 TO STATION 6-10 AT LONGERON 52 SPLICE , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-52- 2R FIGURApr 4, 2022 · N602FE · Doug MD11SDR IPXA2022041281097Stiffener · crackedINSPECTION TYPE:C13CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL25.REPAIR I.A.W UPS EO B767-5310-20118-H AND 767-300F SRM 51-70-12 GENERAL,FIGURE 1,REV 82.01.Apr 4, 2022 · N320UP · Boeing 76734AFSDR CALA2022040600883Stop Fitting · crackedRH AFT DOOR FR68 STOP FITTING #1 LWR I/B HOLE CRACK AT FRAME LAY ER 6 O''CLOCK POS. AD RELATED TASK EA 5343-01724 001 PER HAECO LC Q NON ROUTINE 9298354/30354 GENERATED BY V061682Apr 4, 2022 · N491UA · Airbus A320232SDR CALA2022040600882Fitting · crackedLH AFT DOOR FR68 STOP FITTING #1 LWR I/B HOLE CRACK AT FRAME LAY ER 6 O''CLOCK POS. AD RELATED TASK EA 5343-01724 001 PER HAECO LC Q NON ROUTINE 9298355/30355 GENERATED BY V061682Apr 4, 2022 · N491UA · Airbus A320232SDR SWAA2022051090811Crease Beam · corrodedCORROSION CREASE BEAM FLOOR STRUCTURE LOCATED BS867 AT LEVEL LBL69 AND WL208.1 AT PASSENGER CABIN 2022-168789 / [01] TOOL USED: ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; DUE DATE: 26-JAN-23<BR>TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/NApr 3, 2022 · N948WN · Boeing 7377H4SDR AALA202204137701Channel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 67 AND FR 68 AT S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.Apr 2, 2022 · N987AM · Airbus A321231SDR JR2R20220402516Doubler · corrodedFLOOR DOUBLER CORRODED BETWEEN FR19 THRU FR19A AND RBL44 THRU RBL51Apr 2, 2022 · N88301 · Emb ERJ170200LRSDR JR2R20220402514Doubler · corrodedFLOOR WEB PANEL HAS CORROSION BETWEEN FR12 THRU FR14 AND RBL37 THRU RBL50Apr 2, 2022 · N88301 · Emb ERJ170200LRSDR SWAA2022050490498Frame · crackedCRACK FRAME BS 259.5 AT STR 8LH AT PASSENGER CABIN 2022-165308 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X12101V022236; DUE DATE: 02-JUN-22;[02] TOOL USED: ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22;[03] REPApr 1, 2022 · N427WN · Boeing 7377H4SDR FDEA202204010985None · corrodedLOWER FUSELAGE - FRAME ATTACHED OUTER CHORD CORRODED, AT STA1380, BETWEEN STGR27RH AND STGR29RH COMPLIED WITH FEDEX EA: F-5310-T0367786 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 1380 FRAME OUTER CHORD PARTIAL REPLACEMENT AND SPLICE REPAIR BETWEEN S-26R AApr 1, 2022 · N903FD · Boeing 757200
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