JASC 5313

Service difficulty reports · 36,313

Reports filed under 5313 · Fuselage Main, Longeron/Stringer, 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 = '5313'
  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 UPS02439582Longeron · crackedDURING C CHECK, LT BLG OVERWING LONGERON BS 1413 FOUND TWO CRACKS BOTH CRACKS THROUGH THICKNESS ONE CRACK IS 5.5 INCH INLENGTH ANOTHER ONE CRACK IS 3 INCH IN LENGTH . BS 1413 LT OVERWING LONGERON ANGLE REPAIR CARRIED OUT AS PER HX RS R-53-43-34909 AND RASep 15, 2002 · N683UP · Boeing 747121SDR UPS02439581Longeron · crackedDURING C CHECK, CRACK FOUND AT RT SIDE OF BS 1350 OVERWING LONGERON, THE CRACK FOUND INITIATED FROM FWD EDGE OF VERTICAL FLANGE RUNNING TOWARD AFT TO I/B HORI FLANGE, TOTAL LENGTH OF CRACK 2 INCH LONG APPROXIMATELY. BS 1350 RT OVERWING LONGERON UPPER CHSep 14, 2002 · N683UP · Boeing 747121SDR GTIA021072Longeron · corrodedAFT PIT STA 1136, HAS CORROSION AT LONGERON 28R. FABRICATED LONGERON AND LONGERON SPLICE. REMOVED DAMAGED LONGERON SECTION, INSTALLED NEW SPLICE AND NEW LONGERON SECTION.Sep 13, 2002 · N815NK · Doug DC983SDR GTIA021064Longeron · corrodedAFT PIT, STA 1174 TO STA 1155 HAVE CORROSION AT LONGERON 30. MATERIAL LOSS OUT OF LIMITS COMPLIED WITH E.A. 5310-0252.Sep 13, 2002 · N815NK · Doug DC983SDR IXXA0200137SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON LONGERON 36 AT STATION 380. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED LONGERON FROM STATION 360 TO 450, FABRICATION AND INSTALLATION OF NEW LONGERON IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MASep 12, 2002 · N828BX · Doug DC871FSDR GTIA021063Longeron · corrodedMID PIT STA 768 LONGERON 29 LT CORROSION ON LONGERON INBOARD FLANGE/LOWER SURFACE AT LONGERON TO FRAME FASTENER. REMOVED DAMAGED SECTION, FABRICATED NEW LONGERON REPAIR SECTION/SPLICE INSTALLED LONGERON AND SPLICE.Sep 12, 2002 · N815NK · Doug DC983SDR GTIA021060Skin · damagedCREASE OVER FRAME AT FS 220 BETWEEN LONGERONS 17L AND 18L. LOCATED, FABRICATED AND DRILLED DOUBLER INSTALLED REPAIR DOUBLER.Sep 12, 2002 · N815NK · Doug DC983SDR IXXA0200135SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LONGERON 33R AT STATION 350 AFT OF THE C-1 DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED LONGERON FROM STATION 340 TO 450, FABRICATION AND INSTALLATION OF NEW LONGERON IN ACCORDANCE WITH TSep 11, 2002 · N828BX · Doug DC871FSDR AALA20021317Longeron · crackedTUL - FOUND L2R CRACKED AT END FITTING. REMOVED DAMAGED SECTION OF 2R. INSTALLED SPLICE AND DOUBLER PER AARD 53-30-00-2. (M)Sep 10, 2002 · N596AA · Doug DC983SDR ZW0A0209201Stringer · crackedDURING CHECK-C MAINT LONGERON 2L WAS CRACKED AT STA 1418, .25 INCH LONG. INSTALLED REPAIR SPLICE PER SRM 53-02, FIG 18.Sep 9, 2002 · N9402W · Doug DC983SDR 2002UALA01431Stringer · damagedFWD CABIN STR 2R IS DRILLED INTO ABOVE STRINGER CLIP AT STA 380. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SECTION.Sep 8, 2002 · N343UA · Boeing 737322SDR 2002UALA01428Stringer · crackedCABIN STA 907, STR 4L. FOUND 2 EA CRACKS IN STRINGER AROUND FASTENERS. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER.Sep 8, 2002 · N343UA · Boeing 737322SDR AWXA200200944Stringer · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H, BS 1006-1012, AFT SIDE OF WASTE SERVICE COMPARTMENT. MAINTENANCE FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED CORRODED STRINGER 26 R/H, BS 1006-1012; FABRICASep 6, 2002 · N325AW · Boeing 737301SDR 02FDEA00627Stringer · crackedSTR 15L IS CRACKED AT BS 720B+16. R&R STRINGER PER SRM 53-10-3.Sep 5, 2002 · N496FE · Boeing 727200SDR 2002UALA01404Crease Beam · corrodedCABIN FLOOR STATION 773, RBL 62, INBOARD CREASE BEAM HAS CORROSION AT FLOOR BOARD FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. CORROSION CUT OUT AND DOUBLER INSTALLED.Sep 5, 2002 · N543UA · Boeing 757222SDR GTIA020969Longeron · corrodedMID B/B LONGERON 29L CORRODED AT STA 636, 648 AND 654. REMOVED L29L AT STA 589 TO 664.5 AND SPLICES. FABRICATED LONGERON IAW EA. INSTALLED SPLICES AT STA 589 TO 664.5.Sep 4, 2002 · N817NK · Doug DC982SDR AWXA200200949Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STRINGER 5 R/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727E, STRINGER 5 R/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW DWG 69Sep 4, 2002 · N336AW · Boeing 737375SDR MWEA020534Strap · misalignedRIGHT FRAME AT STATION 362 HAS 3 EXISTING PILOT HOLES NOT LINING UP WITH EXISTING FASTENER HOLES PATTERN. -- LOCATED AND DRILLED STRAP FABRICATED AND INSTALLED STRAP.Sep 4, 2002 · N809ME · Doug DC982SDR MWEA020536Doubler · damagedFORWARD CARGO DOOR DOUBLER DAMAGED AT STATION 362 LONGERON 20&21 RIGHT. -- FABRICATED AND INSTALLED DOUBLER.Sep 4, 2002 · N809ME · Doug DC982SDR MWEA020535Shear Tie · damagedSHEAR CLIP DAMAGED AT LONGERON 20 RIGHT STATION 332. -- LOCATED AND DRILLED SHEAR TIE. REMOVED AND INSTALLED SHEAR TIE AND SPLICE.Sep 4, 2002 · N809ME · Doug DC982SDR GAIA02085STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE MAIN CARGO COMPARTMENT INTERIOR AT BS 720B HAD A CRACK AT STRINGER S15L FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED NEW PART IAW B727 SRM 53-10-3, FIG 5. THE AIRCRAFT WAS RETURNEDSep 3, 2002 · N79748 · Boeing 727224SDR GAIA02086STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO COMPARTMENT INTERIOR BS 720B HAD A CRACK AT STRINGER S15R END, FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW PART IAW B727 SRM 53-10-3, FIGURE 5. THE AIRCRASep 3, 2002 · N79748 · Boeing 727224SDR USAA020331Stringer · crackedPIT - FOUND WEB BEAM CRACKED .25 INCH, FS 727, S18A RIGHT WEB BEAM FIRST INBOARD FAST HOLE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Sep 3, 2002 · N531AU · Boeing 7373B7SDR AWXA200200874Stringer ClipMCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 663, STRINGER 10 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 663, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200Sep 3, 2002 · N187AW · Boeing 737277SDR AWXA200200873Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 597, STRINGER 9 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 597, STRINGER 9 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200 SSep 3, 2002 · N187AW · Boeing 737277SDR AWXA200200872Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A 1/2" CRACK WAS FOUND ON STRINGER CLIP AT BS 559, STRINGER 10 R/H. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 559, STRINGER 10 R/H, FABRICATED A NEW STRINGER CLIP, AND INSTALLED REPAIR IAW DWG 69-35352, AND B737-200Sep 3, 2002 · N187AW · Boeing 737277SDR MWEA020523Doubler · damagedWHILE AIRCRAFT PARKED AT GATE, BAGGAGE CART STRUCK AIRCRAFT ON RIGHT HAND SIDE FORWARD OF THE FORWARD CARGO DOOR JAMB. -- LOCATED AND DRILLED HOLES REMOVED AND INSTALLED SKIN.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020533Skin · tool damageMISDRILLED HOLES IN NEW SKIN AT STATION 392 ABOVE LONGERON 19 RIGHT. -- PLUGED MISDRILLED HOLES.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020532Clip · damagedSHOVEL CLIP DAMAGED AT STATION 362 LONGERON 21 RIGHT. -- LOCATED AND DRILLED HOLES IN NEW SHOVEL AND REINSTALLED CLIP.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020531Clip · damagedSHOVEL CLIP DAMAGED AT STATION 362 LONGERON 20 RIGHT. -- LOCATED AND DRILLED SHOVEL CLIP AND REINSTALLED CLIP.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020530Clip · damagedSHEAR CLIP DAMAGED AT STATION 294 LONGERON 21 RIGHT. -- FABRICATED AND INSTALLED SHEAR CLIP.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020529Longeron · damagedLONGERON 22 RIGHT IS DAMAGED AT STATION 351. -- LOCATED AND DRILLED NEW LONGERON AND REINSTALLED LONGERON.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020528Clip · damagedSHEAR CLIP DAMAGED AT LONGERON 21 RIGHT AT STATION 351. -- FABRICATED AND INSTALLED SHEAR CLIP AND SPLICE.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020527Longeron · damagedLONGERON 21 RIGHT DAMAGED AT STATION 351. -- FABRICATED AND INSTALLED LONGERON.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020526Longeron · damagedLONGERON 20 RIGHT DAMAGED AT STATION 351. -- FABRICATED AND INSTALLED LONGERON.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020525Frame · damagedFRAME DAMAGED AT STATION 362 LONGERON 20 RIGHT AND 21 RIGHT. -- DRILLED FRAME REMOVED AND INSTALLED FRAME.Sep 3, 2002 · N809ME · Doug DC982SDR MWEA020524Splice · damagedFRAME DAMAGED STATION 351 LONGERON 20 RIGHT-21 RIGHT. -- FABRICATED AND INSTALLED FRAME REPAIR SPLICES.Sep 3, 2002 · N809ME · Doug DC982SDR AUS20021131Stringer · corroded(AUS) FUSELAGE STRINGER LOCATED AT STN 107.00 CONTAINED SEVEREEXFOLIATION CORROSION. EVIDENCE OF WATER ENTRY OVER AN EXTENDED PERIOD.Sep 1, 2002 · Beech 95C55SDR GTIA020968Longeron · corrodedCORROSION HEAVY PITTING IN MID CARGO PIT F 674 AND 693 LONG 29L. REMOVED LONG 29L FROM 664.5 TO 740.5 FABRICATED LONGERON 29L AND 2 EACH LONGERON SPLICES , INSTALLED LONGERON AND SPLICES.Sep 1, 2002 · N817NK · Doug DC982SDR AWXA200200948Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STRINGER 4 L/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727B, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-3Sep 1, 2002 · N336AW · Boeing 737375SDR AWXA200200947Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 5/16" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727C, STRINGER 4 L/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727C, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-Sep 1, 2002 · N336AW · Boeing 737375SDR 2002UALA01396Crease Beam · corrodedCABIN CREASE BEAM IB CHORD BODY STATION 734 TO BODY STATION 740 LBL 65 UPPER SURFACE HAS EXCESS MAT LOSS. MAJOR REPAIR ACCOMPLISHED.CREASE BEAM INNER CHORD REPLACED. PARTS SEALED AND FASTENERS INSTALLED.Sep 1, 2002 · N543UA · Boeing 757222SDR CALA0200450Longeron · crackedINSPECTION FOUND A 1.5" CRACK IN LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18.Aug 31, 2002 · N71828 · Doug DC982SDR 02FDEA00617Stringer · crackedFOUND STR 27 RT CRACKED IN INBOARD RADIUS AT BS 1111-1116. REMOVED AND REPLACED STRINGER PER SRM 51-40-4.Aug 30, 2002 · N127FE · Boeing 727100SDR 2002UALA01394Stringer · corrodedAFT PIT STATION 1468 STRINGER 29L UPPER INBOARD FLANGE HAS EXCESSIVE MATERIAL LOSS AFTER CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND EXTENDED PRODUCTION STRINGER SPLICE AS REPAIR.Aug 30, 2002 · N546UA · Boeing 757222SDR UPS02839473Longeron · crackedINSPECTION TYPE:C1 STA 1755 LONG 15L CRACKED AT I/B FLANGES. REMOVED DAMAGED SECTION OF LONGERON PER DC8 SRM 53-2-2 FIG 11. FABRICATED REPAIR PER DC8 SRM 53-2-2 FIG 11. INSTALLED PER DC8 SRM 51-1-20DAug 29, 2002 · N755UP · Doug DC871FSDR IXXA0200129SDoubler · inadequateDURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR AT FUSELAGE STATION 45 LONGERON 29L WAS DETECTED. REPAIR ACCOMPLISHED, REMOVAL OF TEMPORARY REPAIR, DAMAGE. FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MAAug 27, 2002 · N828BX · Doug DC871FSDR UPS02839465Longeron · crackedINSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17L IS CRACKED. REMOVED AND REPLACED LONG 17L FS 1766-1790 IAW DC8 SRM 51-1-20D AND 51-1-21.Aug 27, 2002 · N755UP · Doug DC871FSDR UPS02839460Longeron · crackedINSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17R IS CRACKED. REMOVED LONG & ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21. INSTALLED NEW LONG AND ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21.Aug 27, 2002 · N755UP · Doug DC871FSDR UPS02839434Longeron · crackedINSPECTION TYPE:C-1 LONG 17L AND END FITTING CRACKED AT STA 1772. REMOVED LONG AND END FITTING, FABRICATED LONGERON SLICE AND DRILLED UP NEW END FITTING IAW DRAWING 5649327 AND SRM 51-1-24, INSTALLED REPAIR PARTS IAW SRM 51-1-20D.Aug 27, 2002 · N708UP · Doug DC871F
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