JASC 5310

Service difficulty reports · 38,548

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"

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SDR SWAA2020013140931Crease Beam · corrodedAFT CABIN INNER CREASE BEAM UPPER SURFACE HAD CORROSION BETWEEN BS 947+17 TO BS 967+17, RBL 52. R&R CREASE BEAM PER SRM & DWG.Jan 26, 2020 · N8603F · Boeing 7378H4SDR DALA2020012970679Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE. (CPAX) SUMMARY OF NRC 00281: RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462880)Jan 26, 2020 · N908DA · Doug MD9030SDR DALA2020012970678Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE. (CPAX) SUMMARY OF NRC 00292: RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462863)Jan 26, 2020 · N908DA · Doug MD9030SDR DALA2020012970677Frame · crackedCRACK ON RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE. (CPAX) SUMMARY OF NRC 00282: RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462766)Jan 26, 2020 · N908DA · Doug MD9030SDR DALA2020012960676Frame · crackedCRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00138:RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461939)Jan 26, 2020 · N908DA · Doug MD9030SDR DALA2020012960675Frame · crackedINITIAL INSPECTION: CRACK ON RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00137:RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461934)Jan 26, 2020 · N908DA · Doug MD9030SDR DALA2020012960674Frame · crackedCRACK ON RING PAN LOWER AFT EDGE AT STA Y= 943, Y=674 AND Y= 845 LH SIDE. (CPAX) SUMMARY OF NRC 00136:RING PAN LOWER AFT EDGE AT STA Y=943, Y=674 AND Y= 845 LH SIDE. WERE REPAIRED PER MD-90 SRM-56-20-02 FIGURE 2 (1461887)Jan 26, 2020 · N908DA · Doug MD9030SDR SWAA2020012840794Structure · crackedPOWER ACCESS DOOR STRUCTURE AROUND DOOR LOWER SIDE CRACKED AND SECTION MISSING. / REPAIRED GROUND POWER ACCESS DOOR STRUCTURE LOWER SIDE IAW SRM 53-10-15-2R-4.Jan 26, 2020 · N8310C · Boeing 7378H4SDR REXA2020020500177Bulkhead Web · crackedFS202.75 BULKHEAD FWD SIDE @BL23.71 HAS MULTIPLE INDICATORS AROUND ENTIRE CIRCUMFERENCE OF THE PARKING BRAKE CABLE CUTOUT .15"" LONG BY 80% FSH. FAILED NDT INSPECTION COMPLIED WITH REMAINING STEPS OF REO 601R-53-11Jan 25, 2020 · N8970D · Cndair CL6002B19SDR AALA2020020549065Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED VERTICAL PRESSURE DECK WEB AT BS 639 BETWEEN RBL 31.83 AND RBL 40. REPAIRED VERTICAL PRESSURE DECK WEB PER SRM 57-10-10-2R.Jan 25, 2020 · N981AN · Boeing 737823SDR DALA2020012750661Doubler · corrodedDURING INSPECTION FOUND CORROSION ON FITTING DOUBLER BS 797 BTW S-27L TO S-27R IN THE AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED IAW ETI-37-20-300, REV 1, AND ERA 584735-14, SECTION 1, REV ORIG.Jan 24, 2020 · N3769L · Boeing 737832SDR DALA2020012750660Doubler · corrodedDURING INSPECTION FOUND CORROSION ON FITTING DOUBLER BS 757 BTW STRINGERS 27L - 27R IN THE AFT CARGO COMPARTMENT. FITTING DOUBLER WAS REPAIRED IAW ETI-37-20-300, REV 1, AND ERA 584735-14, SECTION 1, REV ORIG.Jan 24, 2020 · N3769L · Boeing 737832SDR YENA2020012840054Crossbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE CROSS BEAM LOCATED FRAME 17RH SIDE AT FWD GALLEY AREA; ACCOMPLISHED REPAIR OF CORROSION DAMAGE FOUND ON THE FLOOR CROSSBEAM (P/N 170-21769-403) FR 17RH AT THE FWD FUSELAGE IN ACCORDANCE WITH AEROMAN E/A 53-0Jan 24, 2020 · N374JB · Emb ERJ190100IGWSDR SWAA2021080920117Retainer · crackedSEAL RETAINER IS CRACKED BS 663 LBL 20 WL 140 / REMOVED AND REPLACED SEAL RETAINER B.S.663 LBL20 WL140 PER SRM 51-40-02-0G-0 DWG 111A1000 AND DWG 111A1001Jan 23, 2020 · N426WN · Boeing 7377H4SDR VNAA202002299991Crossbeam · corrodedFS 280 CROSSBEAM IS CORRODED OB OF RBL 9 LOCATED,AND DRILLED NEW SERVICEABLE RH FS280 CROSSBEAM IAW CRJ 700 SRM 51-21-06-001-001-A01 AND 51-40-11-001-001-A01.Jan 23, 2020 · N540EG · Cndair CL6002C10SDR FDEA202001230211Spar · crackedINSPECTION OF CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, FOUND HOLE D WITH CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, CRACKED HOLE D PER EA: 6-5710-T0352050 PJan 23, 2020 · N686FE · Airbus A300F4605RSDR DALA2020012740609Box Beam · crackedCRACKS FOUND ON THE BOX BEAM BETWEEN BS 345 - 365, RBL 24 IN THE PAX CABIN FLOOR STRUCTURE. REPLACED THE BOX BEAM IAW DWG 141N5160-3, REV E, AND SRM 51-40-02-0G, PAR 4 AND 7.Jan 23, 2020 · N547US · Boeing 757251SDR DALA2020012300516Stiffener · crackedMFEC INSPECTION FOUND ONE CRACK AT NOSE WHEEL WELL, RT VERTICAL STIFFENER FILLET RADIUS. BS 287, WL 170. THE LENGTH OF CRACK IS ABOUT 0.5 INCH. CRACK REPAIRED.Jan 23, 2020 · N838MH · Boeing 767432ERSDR SWAA2021072129112Crease Beam · corroded***CORROSION*** ON UPPER FLANGE OF I/B CREASE BEAM CORD AT STA 951+12-986; LBL56; WL207 / REMOVED AND REPLACED INNER CHORD BETWEEN BSTA. 893 AND BSTA 1006; IAW. DWG. 147A8501; SRM. 51-40-02-0G-0 LIMIT STATEMENT L3.0' X W0.75' X D.030' INNER CHORD FOUND TO BE OJan 22, 2020 · N8602F · Boeing 7378H4SDR SWAA2021072129111Crease Beam · corroded***CORROSION***ON UPPER FLANGE OF I/B CREASE BEAM CORD AT STA 951+12-986; RBL56; WL207 / REMOVED AND REPLACED NEW REPLACEMENT INNER CHORD ON STA 890 TO STA 1006 RBL 56; WL 207; PART # 147A8540U8; LOT # PO 765207; IAW SRM-51-40-02-0G-0; DWG. 142A8501 CORROSION Jan 22, 2020 · N8602F · Boeing 7378H4SDR SWAA2021070720109Pressure Deck · damagedCOCKPIT FLOOR DAMAGED AT BS 257 BL0 -LBL13 WL 208 / REMOVED DAMAGED WEB SECTION AND INSTALLED REPAIR PARTS AT BS220-250 RBL10-LBL20 WL208 IAW EA 1-A53-33179 REV.IRJan 22, 2020 · N426WN · Boeing 7377H4SDR AALA2020020549064Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK FIRST OFFICERS #1 WINDOW POST UPPER OUTBOARD CORNER CRACKED AT BS 214 AND S10R. REPAIRED WINDOW POST PER EA 302085.Jan 22, 2020 · N981AN · Boeing 737823SDR AALA2020020549063Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CAPTAINS #1 WINDOW POST UPPER OUTBOARD CORNER CRACKED AT BS 214 AND S10L. REPAIRED WINDOW POST PER EA 302084.Jan 22, 2020 · N981AN · Boeing 737823SDR SWAA2020012940862Crease Beam · corrodedUPPER FLANGE OF INBOARD CREASE BEAM CHORD CORRODED AT BS. 890 TO BS. 1006, RBL 56. R&R INNER CHORD IAW SRM & DWG.Jan 22, 2020 · N8602F · Boeing 7378H4SDR 2020FA0000079Structure · crackedWE HAVE EXPERIENCED MULTIPLE OCCURRENCES OF CRACKING IN THE CONTROL PEDESTAL STRUCTURE OF C208 AND C208B'S. THE PARTS FROM THE C208 IPC 53-22-00 FIG 1 ARE: PANEL ASSY-LH 2613247-7, PANEL ASSY - RH 2613247-1, AND SUPPORT ASSY 2613010-11. THE CRACKS OCCUR IN TJan 22, 2020 · Cessna 208BSDR REXA2020012810062Angle · corroded"INITIAL INSPECTION: CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE (W1)"ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED FOR ANEW ONE PER CRJ-900 SRM 51-41-02-001-001-A01 (LEVEL CORROSION 2) "Jan 21, 2020 · N147PQ · Cndair CL6002D24SDR V0XD202001261101Support · crackedLH ANGLE ON FRAME SUPPORT CRACKED AT F.S.793.00 CORRECTIVE ACTION: REMOVED DAMAGED AREA BY CUTTING OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO670-53-82-478 REV:A DATED 2014/11/12, CRJ 700 SRM 51-42-06, 51-42-21, 51-21-11, 51-25-06, 51-25-16 TR Jan 21, 2020 · N340CA · Cndair CL6002C10SDR AALA202001249020Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CAPTAINS #3 WINDOW CUT OUT E-F WINDOW POST FORWARD EDGE #2 FASTENER HOLE CRACKED AT BS 240 AND S11L. REPAIRED WINDOW POST PER EA 302088.Jan 21, 2020 · N981AN · Boeing 737823SDR AALA202001249019Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: FIRST OFFICERS #3 WINDOW CUT OUT E-F WINDOW POST FORWARD EDGE #2 FASTENER HOLE CRACKED AT BS 240 AND S11R. REPAIRED WINDOW POST PER EA 302089.Jan 21, 2020 · N981AN · Boeing 737823SDR SIMA202001231006Doubler · damagedDAMAGE ON NOSE WHEEL WELL FOUND TO BE OUT OF LIMITS PER EMBREAER "TRANSFERRED TO NRWC 663-ABI-04309"-C/A-FOUND DOUBLER ON RH SIDE OF NLG WHEEL WELL DAMAGED. REMOVED AND REPLACED DOUBLER IAW EMB 145 SRM 51-40-02, 51-20-03Jan 21, 2020 · N663AR · Emb EMB145LRSDR A6WA2020012247122Post · crackedFOUND A CRACK LOCATED AT 409+128, LBL 18, ON THE LOWER END OF STRUT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE POST STRUT IAW REO 601R-53-41, 56, REV E.Jan 21, 2020 · N428AW · Cndair CL6002B19SDR COEA2020030408819Crease Beam · corrodedWO 211121 NR 200060 HEAVY CHECK COE/MINOR REPAIR: R/H CREASE BEAM WEB HAS LEVEL 2 CORROSION FRAMES 28A-28B. CORRECTIVE ACTION: REPLACED WITH OEM PART.Jan 20, 2020 · N819FX · Aerosp ATR72212SDR VNAA2020012301101Window Frame · crackedDURING REMOVAL OF PILOTS SIDE WINDOW FOUND A CRACK IN THE PRIMARY STRUCTURE OF THE FRAME BETWEEN THE SIDE WINDOW AND WINDSHELD. MX REMOVED AND REPLACED PILOTS SIDE WINDOW POST.Jan 20, 2020 · N708PS · Cndair CL6002C10SDR VNAA202002299994Crossbeam · corrodedFS 280 CROSSBEAM IS CORRODED BETWEEN LBL9 AND LBL18 LOCATED AND DRILLED NEW SERVICEABLE LH FS280 CROSSBEAM IAW CRJ 700 SRM 51-40-11-001-001-A01.Jan 19, 2020 · N540EG · Cndair CL6002C10SDR SIMA2020012019006Shunt · corrodedDURING ACCOMPLISHMENT OF EO-2400-018 (APU SHUNT GROUND IMPROVEMENT), FOUND THE APU SHUNT AREA ON FR 80 TO BE CORRODED-C/A-ACCOMPLISHED APU SHUNT REPAIR ON FR 80 IAW EMB 145 SRM 53-32-04 STEP 3 AND DET. E, SECTION A-A PAGE 208. REPAIR MATERIALS;DOUBLER: AL CLADJan 19, 2020 · N676AE · Emb EMB145LRSDR SWIA2020020548222Beam · corrodedCORROSION IN L/H BEAM FROM FR.12-21. (C-CHECK) RO 2/03/2020 REMOVED AND REPLACED L/H BEAM FROM FR 12-21. REF. SRM . RESTORED SURFACE PROTECTION PER SRM AND CPM PO# 259007, 252104Jan 18, 2020 · N134SY · Emb ERJ170200LRSDR SWIA202020548221Beam · corrodedCORROSION IN R/H BEAM AT FR.17. (C-CHECK) RO 2/03/2020 REMOVED AND REPLACED R/H BEAM FROM FR 12-20. REF. SRM . RESTORED SURFACE PROTECTION PER SRM AND CIC PER CPM PO# 259007, 252104Jan 18, 2020 · N134SY · Emb ERJ170200LRSDR SWIA2020020548220Beam · corrodedCORROSION IN L/H BEAM FR.86-89. (C-CHECK) RO 2/03/2020 REMOVED AND REPLACED L/H BEAM FR.86-89 REF SRM. RESTORED SURFACE PROTECTION REF EMB SRM. APPLIED CIC REF EMB CPM.Jan 18, 2020 · N134SY · Emb ERJ170200LRSDR SWIA2020020548219Beam · corrodedCORROSION IN R/H BEAM FR.86-89. (C-CHECK) RO 2/03/2020 REMOVED AND REPLACED R/H BEAM FR.86-89 REF EMB SRM. RESTORED SURFACE PROTECTION REF EMB SRM.Jan 18, 2020 · N134SY · Emb ERJ170200LRSDR DALA2020012180450Box Beam · corrodedCORROSION ON BOX BEAM BETWEEN BS 720 - 740, LBL 62 AT PAX CABIN FLOOR STRUCTURE. THE CORROSION WAS REMOVED IAW SRM, INSP AND WAS FOUND TO BE OUT OF LIMITS PER SRM. BOX BEAM WAS REPLACED IAW SRM.Jan 18, 2020 · N547US · Boeing 757251SDR CALA2020012300202Door Frame · crackedLEFT FWD EMERGENCY EXIT HATCH AFT VERTICAL FRAME WAS CRACKED AT FASTENER AREAS, REMOVED & REPLACED IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232SDR CALA2020012300201Door Frame · crackedLEFT FWD EMERGENCY EXIT HATCH FWD VERTICAL FRAME WAS CRACKED AT FASTENE R AREAS, REMOVED & REPLACED THE VERTICAL SEGMENT IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232SDR CALA2020012300199Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR FWD WEB & AFT FRAME CRACKED, REMOVED & REPLACED IAW SRM 51-72-11-910-002.Jan 18, 2020 · N438UA · Airbus A320232SDR REXA2020012870122Electrical Box · cracked"INITIAL INSPECTION: CRACK IN BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE. (FUS) ""BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, CRJ900 SJan 17, 2020 · N296PQ · Cndair CL6002D24SDR CALA2020012300198Pressure Panel · crackedC-4 CHECK, RT PRESSURE PANEL FR35-36 ROTO SCAN INSPECTI ON HOLES 16,18,22, AND 24 HAVE CRACK INDICATIONS. HAECO TECHNICIAN V052041 AND QC LC-32 REPAIRED RH PRESSURE PANEL FR35-36 IAW ECRA 5331-02567 PART 1. DTA LP ACCOMPLISH THE INITIA L INSPECTION REQUIREMENTJan 17, 2020 · N439UA · Airbus A320232SDR C77A2020011700003Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED IN THE FORWARD FUSELAGE AT THE RH COCKPIT FLOOR DOUBLER (P/N 170-03238-005) DURING INSPECTION IN THE AREA. THE DAMAGE EXCEEDED THE LIMITS PROVIDED IN THE SRM BECAUSE OF ITS DEPTH. EAMS REQUESTEJan 17, 2020 · N622CZ · Emb ERJ170200LRSDR SWIA2020021848650Joint · corroded* CORROSION ON CIRCUMFERENTIAL JOINT FS 280 AND FS 282.86 BETWEEN STR27 AND STR26R. (C-CHECK) RO 2/14/2020 REMOVED CORROSION ON FS280.00 BUTTSTRAP BETWEEN STGR 27 AND STGR 26R REF CRJ700 SRM. ORIGINAL MATERIAL THICKNESS OF FS280.00 BUTTSTRAP BETWEEN STGR Jan 16, 2020 · N730SK · Cndair CL6002C10SDR SWIA202002048213Beam · corrodedCORROSION ON INTERCOSTAL BEAM BEHIND FR 90 Y=+10.748" (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED INTERCOASTAL BEAM BEHIND FR 90 Y=+10.748". REF SRM.Jan 16, 2020 · N138SY · Emb ERJ170200LRSDR SWIA202002048209Rib · crackedFR 52 SUPPORT RIB UPPER ATTACHMENT ANGLE IS CRACKED AT LH MLG WHEEL WELL AREA. (C-CHECK) RO 2/02/2020 REMOVED AND REPLACED FR52 SUPPORT RIB UPPER ATTACHMENT ANGLE AT FR52 LH MLG WHEEL WELL, REF. SRM.Jan 16, 2020 · N138SY · Emb ERJ170200LRSDR REXA2020012860063Tube · corroded"INITIAL INSPECTION: CORROSION ON TUBE AT PASSENGER DOOR SURROUND STRUCTURE (FUS) "TUBE WAS REPLACED FOR A NEW ONE PER CRJ-900 AMM 52-11-00-400-802-A01.LEVEL CORROSION: 1Jan 16, 2020 · N147PQ · Cndair CL6002D24
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