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 USAA011389Stringer · crackedPIT - FOUND STRINGER CRACKED 1.5 INCH STRINGER 5L AT FRAME JUNCTION STATION 380. DOUBLER INSTALLED PER SRM 53-00-03. (M)Dec 3, 2001 · N390US · Boeing 7373B7SDR 2002F00332Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040FSDR 2002F00317Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3 WAS ISSUED DER DERY 510314-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNDec 1, 2001 · N141WE · Doug DC1040FSDR 2002F00024Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040FSDR 2002F00020Longeron · crackedDURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-G08321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040FSDR DHL2001365519Stringer · corrodedLEVEL 2 CORROSION AT STR 47 LT BETWEEN FR 35 SRM REF 53-14-00 PG 250 ITEM 264. REMOVED FASTENERS PER SRM 51-30-29. CUT OUT DAMAGED AREA PER SRM 53-10-10. FABRICATED REPAIR PARTS PER SRM 53-10-10. CLEANED, TREATED AND PRIMED PER SRM 51-60-12. INSTALLED REPDec 1, 2001 · N365DH · Airbus A300B4203SDR DHL2001365538Stringer · corrodedSEVERAL COUPLING SECTIONS CORRODED BETWEEN FR 33-34 STRINGERS 48-50 LT, 48-50 RT. REMOVED COUPLING AT STR 49L FR 33-34 RT & LT PER SRM 51-30-30. INSTALL NEW COUPLING PER SRM 51-30-30. REMOVED COUPLING AT STR 50L, FR 33-34 PER SRM 51-30-30. INSTALLED NEW CONov 30, 2001 · N365DH · Airbus A300B4203SDR DHL2001365539Stringer · corrodedCORROSION ON STR 36L-46L AT FRAME 72. REMOVED CORROSION PER SRM 51-40-11 (NEGLIGIBLE MTL REMOVED). CUT OUT 2 FT SECTION AND REPLACED PER SRM 53-10-10.Nov 30, 2001 · N365DH · Airbus A300B4203SDR 2001UALA02353StringerSTRINGER 30L AT BODY STATION 470, STRINGER SPLICE REQUIRES REPLACEMENT REF CF9059. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED PERMANENT STRINGER REPAIR SPLICE.Nov 30, 2001 · N611UA · Boeing 767222SDR DHL20013650Stringer · corrodedCORROSION ON STR 5R BETWEEN FR 32-34. CORROSION REMOVED PER SRM 51-40-11, FOUND TO BE OUT OF SRM LIMITS. CUT OUT DAMAGED AREA PER SRM 53-10-10. FABRICATED REPAIR PARTS PER SRM 53-10-10. INSTALLED REPAIR PER SRM 51-30-20.Nov 27, 2001 · N365DH · Airbus A300B4203SDR ASAA0140158Stringer · gougedPAE - DURING SI CHECK, FOUND GOUGE ON STRINGER 16 RT ON UPPER SIDE JUST FORWARD OF 500F FRAME. REPAIRED PER SRM. (M)Nov 26, 2001 · N782AS · Boeing 7374Q8SDR ABXA010626Longeron · crackedLONGERON 17 RIGHT WAS CRACKED AT F.S. 408. CRACK WAS LOCATED AT LOWER HI-LOCK AND WAS APPROXIMATELY .50 INCHES LONG. REPAIRED LONGERON 17 RIGHT IAW DC-9 SRM 53-02.Nov 26, 2001 · N969AX · Doug DC941SDR ABXA010621Longeron · crackedLONGERON 17 LEFT WAS CRACKED ON UPPER AND LOWER FLANGE AT STATION 945 FRAME. REPAIRED AREA IAW DC-9 SRM 53-02.Nov 26, 2001 · N949AX · Doug DC931SDR GTIA012258Longeron · corrodedFTW - FOUND E/E BAY LONGERON 28 LEFT HAS CORROSION AT STATION 170-180. CUT OUT DAMAGE AND REMOVED. INSTALLED LONGERON AND SPLICE PER DC9 SRM 51-30-2. (M)Nov 24, 2001 · N12536 · Doug DC932SDR AWXA200100617Stringer · crackedMCN - MAJOR REPAIR - "C" - STR 16 L/H BS 504C HAS .5" CRACK, VISUALLY CONFIRMED BY 10X MAGIFICATION. MAINTENANCE CUT OUT CRACKED AREA ON STR 16 L/H BS 504C, FABRICATED A NEW CHANNEL AND INSTALLED IAW AWA ER 03-5312-01094-DD1.Nov 24, 2001 · N328AW · Boeing 7373B7SDR DHL2001365536Longeron · crackedCRACK FOUND ON FR 28R OUTER FLANGE BETWEEN 2 VERT FASTENERS BETWEEN STR 14-15 RT DURING NDT INSP. REMOVED FASTENERS PER SRM 51-30-30. REMOVED LONGERON PER SRM 57-30-30. INSTALLED NEW LONGERON PER SRM 57-30-30.Nov 23, 2001 · N365DH · Airbus A300B4203SDR C2XA01TY185Stringer · chafedTYS DURING A SCHEDULED INSPECTION THE EXTERNAL STRINGER 19L WAS FOUND CHAFED JUST AFT OF HYDRAULIC PUMP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR OF STRINGER 19L IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION 5310-01207, THE REPAIR WAS SANov 23, 2001 · N16511 · Emb EMB135ERSDR ASAA0140152Stringer · gougedPAE - DURING SI CHECK, FOUND STRINGER 16 RIGHT HAS GOUGE ON UPPER SIDE JUST FORWARD OF BS 500 FRAME. REPAIRED PER SRM. (M)Nov 21, 2001 · N782AS · Boeing 7374Q8SDR 2001UALA02326Stringer · bentDEEP GOUGE 2 FT AFT OF DR 2L, AND 1 FT UP FROM DOOR BOTTOM.. MAJOR REPAIR ACCOMPLISHED. FRAME 69, STRINGER 23 REMOVED. REWORKED STRINGER & MFG DOUBLER AND INSTALLED.Nov 21, 2001 · N444UA · Airbus A320232SDR 2001UALA02325Stringer · dentedLEFT HAND FUSELAGE AT BODY STATION 1587 AND STRINGER 20 LH HAS DENT IN SKIN. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS REMOVED AND SKIN LAP DOUBLER INSTALLED.Nov 21, 2001 · N521UA · Boeing 757222SDR ASAA0110643Stringer · damagedPAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 259-260, STRINGER 26R WITH AN OVERSIZED HOLE. REMOVED AND REPLACED CHORD PER SRM. (M)Nov 20, 2001 · N745AS · Boeing 737298CSDR AALA20012134Longeron · crackedTUL - FOUND LONGERON 3L CRACKED IN RADIUS INBOARD OF OUTBOARD FASTENER STATION 160. SPLICED NEW LONGERON FROM STATION 170 FORWARD IAW SRM 53-02 FIG 18 SHEETS 1-4-5-6. (M)Nov 20, 2001 · N426AA · Doug DC982SDR QXEA0101968Stringer · corrodedPDX - FUSELAGE BELLY STRINGER 1 HAS CORROSION AT TIE IN CLIP AREA AFT SIDE OF FRAME 16060. REPAIRED IAW FOKKER SRM 51-10-01, 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000SDR AALA20012135Longeron · crackedTUL - FOUND LONGERON 4L CRACKED AT FRAME STATION 160. CUT OUT DAMAGED AREA AND INSTALLED SPLICE PER SRM 53-02 FIG 18. (M)Nov 19, 2001 · N426AA · Doug DC982SDR QXEA0101917Stringer · chafedPDX - CLIP ON CASTELLATION, FRONT SIDE OF FRAME 50-2 IS CHAFING INTO STRINGER 27. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, PARAGRAPH 3E AND SRM 51-10-4.Nov 18, 2001 · N482US · Fokker F28MK4000SDR ZW0A0111302Longeron · crackedDURING CHECK-C MAINT THE NUMBER 2 RT LONGERON WAS CRACKED .125 INCH AT STA 1220. REPAIRED PER SRM 53-02, PAGES 49 THRU 53.Nov 17, 2001 · N9401W · Doug DC983SDR 2001UALA02271Stringer · dentedBODY STATION 310 STRINGER 28R LEFT HAND FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER DOUBLER REPAIR.Nov 14, 2001 · N921UA · Boeing 737522SDR 2001UALA02278Stringer · corrodedBODY STATION 286 STRINGER 20 RBL 88 UPPER T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP AND SPLICES.Nov 13, 2001 · N650UA · Boeing 767322SDR SWAA013091Stringer · corrodedDURING SCHEDULED 1/2D CHECK, FOUND STRINGER 27L CORRODED AT BS 420 TO BS 500A. REPAIRED STR PER SRM.Nov 13, 2001 · N322SW · Boeing 7373H4SDR SWAA013081Stringer · crackedDURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 495, STR 22R. REPAIRED STR PER SRM.Nov 13, 2001 · N693SW · Boeing 737317SDR GTIA012216Longeron · crackedFOUND LONGERON 13R CRACKED AT FUSELAGE FRAME STA Y-965. REMOVED DAMAGED SECTION OF STRINGER. FORMED LONGERON AND SPLICE. INSTALLED LONGERON REPAIR IAW DC9 SRM 53-02. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012189Longeron · crackedFTW - FOUND LONGERON 17L CRACKED AT FUSELAGE FRAME STATION Y=980. REMOVED DAMAGED AREA OF LONGERON. FABRICATED NEW LONGERON SECTION AND SPLICE. INSTALLED LONGERON SECTION AND SPLICE PER DC9 SRM 53-02. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012188Longeron · crackedFTW - FOUND LONGERON 12R CRACKED AT FUSELAGE FRAME STATION Y=945. REMOVED CRACKED LONGERON. FABRICATED DRILLED AND LOCATED NEW LONGERON AND SPLICE. INSTALLED NEW LONGERON AND SPLICE. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012186Longeron · crackedFOUND LONGERON 13L CRACKED AT FUSELAGE FRAME STATION Y=965. REMOVED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED LONGERON 13 ON STATION 965 2ND SPLICE PER DC9 30 SRM 51-30-2. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012240Longeron · crackedFTW - FOUND LONGERON 16L CRACKED AT FUSELAGE FRAME STATION Y 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED REPAIR IAW DC9 SRM 53-02. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012233Longeron · crackedFTW - FOUND LONGERON 17R CRACKED AT FS 965. REMOVED CRACKED LONGERON. FORMED LONGERON AND SPLICE. INSTALLED REPAIR LONGERON AND SPLICE (TWO EACH) IAW DC9 SRM 53-02. (M)Nov 12, 2001 · N12536 · Doug DC932SDR GTIA012231Longeron · crackedFOUND LONGERON 16R CRACKED AT FUSELAGE FRAME STATION 965. REMOVED LONGERON 16R CRACKED FROM STATION 955-975. DRILLED AND LOCATED LONGERON AND SPLICE. INSTALLED LONGERON REPAIR AND SPLICES (TWO EACH) IAW DC9 SRM 53-02. (M)Nov 12, 2001 · N12536 · Doug DC932SDR P2EA2001V0019Stringer · crackedDuring "C" Check Inspection.-Fuselage, BS1080, Str 22 R-H With Crack.-Fuselage Stringer Section Repaired at Str 22 R-H, From BS1050 to BS1088, IAW SRM 53-10-3, Fig 1Note: See COOPESA Work Order No. O10863 1-70, VAM100 No. 227 & 122SDA099.Nov 12, 2001 · N122NJ · Boeing 737230SDR 2001UALA02256Crease Beam · damagedLEFT CABIN CREASE BEAM FLOORBOARD SUPPORT DAMAGED. STA 1355-1383, LBL 65 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.SPLICED NEW ANGLE.Nov 12, 2001 · N517UA · Boeing 757222SDR AWXA200100632Stringer · crackedMCN - C12 CK - "C" - 1" CRACK FOUND AT FWD EDGE OF WING SCANNING LIGHT CUTOUT AT BS 500C+4, STR 16L. MAINTENANCE REMOVED STRINGER END, FABRICATED REPAIR CHANNEL AND FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1.Nov 11, 2001 · N311AW · Boeing 7373G7SDR ASOA01239Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 20 RIGHT BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM Nov 11, 2001 · N280AS · Emb EMB120RTSDR AWXA200100592Stringer · crackedMCN - C12 CK - "C" - CRACK FOUND AT FWD EDGE OF WING SCANNING LIGHT CUTOUT AT BS 500C+4, STR 16R, 1.1" LONG. MAINTENANCE REMOVED CRACKED STRINGER END, FABRICATED REPAIR CHANNEL AND FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1 REFERENCING BOEINov 11, 2001 · N311AW · Boeing 7373G7SDR 2001UALA02260Crease Beam · damagedMID CABIN CREASE BEAM BODY STATION 960 TO BODY STATION 980 STRINGER 17L HAS TOOLING DAMAGE ON WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED.Nov 11, 2001 · N521UA · Boeing 757222SDR ASOA01240Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 16. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM 51-Nov 10, 2001 · N280AS · Emb EMB120RTSDR SWAA013061Stringer · crackedDURING SCHEDULED 1/2D CHECK, FOUND STRINGER WEBS CRACKED ( 2 EA ) AT BS 294.5, STR'S 7L & 8L. R&R WEBS PER SRM.Nov 9, 2001 · N322SW · Boeing 7373H4SDR 2001UALA02240Intercostal · corrodedINTERCOSTAL AT STATION 1666 TO 1681.8 RBL 57 TO RBL 54 CORRODED ON UPPER SURFACE BELOW GUTTER IN DOORWAY 4R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW PART (J-ANGLE) INTERCOSTAL..Nov 8, 2001 · N517UA · Boeing 757222SDR AT0200018Longeron · crackedLONG 5R CRACKED AT STA 617.Nov 7, 2001 · N830AT · Doug DC932SDR AT0200017Longeron · crackedLONG 6R CRACKED AT STA 617.Nov 7, 2001 · N830AT · Doug DC932SDR AT0200016Longeron · crackedLONG 5L CRACKED AT STA 699.Nov 7, 2001 · N830AT · Doug DC932SDR 2001FA0000503Stringer · crackedTHE RIB IS CRACKED IN 3 EACH PLACES WERE IT ATTACHES TO SKIN CRACKS ORIGINATE FROM RIVETS AND CRACKING TOWARDS OTHER RIVETS.Nov 6, 2001 · N370SC · Lear 31A
Back to JASC 5313