JASC 5313

Service difficulty reports · 36,310

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"

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SDR DU4R2006457Stringer · corrodedFOUND CORROSION ON STRINGER 22 LT IN AFT BAGGAGE PIT. REPAIRED BY FABRICATING AND INSTALLING NEW SECTION LONGERON 18.75" X 3" X .75" FROM 1242886 7075 T6, 626520 EXTRUSION AND 2 EACH SPLICES P/N 3914677-501N IAW DC-9/MD-80 53-02 PG 45 & 46 AND 53-02 FIG 15.May 15, 2006 · N930DL · Doug MD88SDR 06FDEA1930Stringer · corrodedFOUND FWD CARGO BAY, STRINGER L28 CORRODED AT BS 527. REPAIRED STRINGER PER SRM 53-10-3.May 15, 2006 · N493FE · Boeing 727227SDR 06FDEA1932Longeron · crackedFOUND CRACKED LONGERON 7L ON INTERCOSTAL AT BS 518 RT. INTERCOSTAL REPLACED AS PER SRM 51-35-01 VOL2 AND DRAWING AFA3086.May 15, 2006 · N526FE · Doug MD11SDR 06FDEA1931Stringer · damagedFOUND MECHANICAL DAMAGE ON STR 7 LT AT BS 783. REPAIRED STR 7 LT AT BS 783 IAW SRM 53-10-3 FIG 3.May 15, 2006 · N493FE · Boeing 727227SDR DHL2006754512Stringer · corrodedAFT CARGO COMPT STR 29L IS CORRODED WITH EXFOLIATION BETWEEN STA 950E & 950F. REMOVED AND REPLACED STR 29 LEFT FROM BS 950 TO 1010 P/N 65-56441-7 PO 626034 IAW SB 727-53-0179 FIG 12.May 14, 2006 · N754DH · Boeing 727223SDR 2006UALA00948Stringer Clip · bentSTRINGER 19R AT STATION 328 HAS BENT STRINGER CLIP.May 14, 2006 · N375UA · Boeing 737322SDR SWAA061631Stringer · crackedDURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 501, STR 14R. REMOVED AND REPLACED STRINGER SECTION PER SRM.May 14, 2006 · N303SW · Boeing 7373H4SDR QXEA200601369Stringer · corrodedPDX: C3. CORROSION ON CLIP X176 AND STRINGER 31L. MAINTENANCE REPAIRED IAW Q400 SRM 51-21-00-350-801, SRM 53-20-15-990-802, SRM 51-21-10, RD 8/4-53-017, AND SRM 51-42-00.May 13, 2006 · N406QX · Bombdr DHC8402SDR UPS06846981Longeron · crackedINSPECTION TYPE:C1 60 HOLE LONGERON 17L HAS PREVIOUS REPAIR, HOWEVER CRACK HAS EXTENDED PAST STOP DRILL. REMOVED DAMAGED L17L AT STA 1776 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON 17L AT STA 1766 IAW SRM 53-02-02-0, 51-3-02, AND SRM 51-1-20D.May 13, 2006 · N818UP · Doug DC873FSDR 06FDEA1915Longeron · crackedMAIN DECK COMPARTMENT FOUND LONGERON 17R CRACKED BETWEEN STA 1239 TO 1247. FOUND LONGERON 17R BETWEEN STA 1239 TO 1247 AT MAIN DECK COMPARTMENT. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.May 13, 2006 · N599FE · Doug MD11SDR DU4R2006462Longeron · corrodedCORROSION ON LONGERON 22L BETWEEN FS 1231 AND FS 1250. REMOVED CORRODED STRAP. FABRICATED AND INSTALLED STRAP 20" X .5" FROM 7075-T6 PER DWG 5911423 IAW DC-9/MD-80 SRM 51-10-3D AND 51-30-2.May 12, 2006 · N930DL · Doug MD88SDR DU4R2006451Stringer · corrodedFOUND CORROSION ON STRINGER 30 BETWEEN FS 1287 AND 1307. REPAIRED BY REMOVING STRINGER SPLICE, FABRICATED AND INSTALLED REPAIR SPLICE 11.5" X 2.7" FROM 7075-T6 IAW DOUGLAS DWG 3914677 AND DC-9/MD-80 SRM 51-30-05 AND 51-10-3D.May 12, 2006 · N930DL · Doug MD88SDR DU4R2006446Longeron · crackedFOUND LONGERON 29L CRACKED AT ATTACH POINT AT FS 218. REPAIRED LONGERON 29 LT CRACKED AT ATTACH POINT AT FS 218 BY REMOVING CRACKED LONGERON. FABRICATED AND INSTALLED REPAIR LONGERON 57-1/4" FROM P/N 2777922-4 IAW MD-80 SRM 51-30-2 AND DELTA DC-9/MD-80 SRM 5May 12, 2006 · N930DL · Doug MD88SDR 06FDEA1832Stringer · corrodedDURING CONVERSION FROM P TO F/ACF, FOUND IN FWD CARGO COMPT B/T STA 1059 AND STA 1079 CORROSION AT STR 52. PERFORMED SKIN REPAIR PER SRM 53-20-00 FIG 7 VOL I. NEW BLANKET HAS BEEN INSTALLED PER SRM 51-35-01 VOL IIMay 12, 2006 · N568FE · Doug DC1010SDR 06FDEA1831Stringer · corrodedDURING CONVERSION FROM P TO F/ACF FOUND IN FWD CARGO COMPT B/T STA 1059 AND STA 1079 CORROSION AT STR 52. PERFOMED SKIN REPAIR PER SRM 53-20-00 FIG 47 VOL I. NEW BLANKET HAS BEEN INSTALLED PER SRM 51-35-01 VOL II.May 12, 2006 · N568FE · Doug DC1010SDR IXXA06SMN128SLongeron · misrepairedDURING ROUTINE C CHECK FOUND RIGHT HAND MAIN LANDING GEAR LONGERON 24 HAS NON STANDARD REPAIR FROM STATION 940.000 TO STATION 960.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG 5 TEMPORARY REVISION 53-123 DATE 05-15-01. REMOVED REPAIR IAW DC-8 SRM 51-1-May 11, 2006 · N830BX · Doug DC871FSDR UPS06847118Fitting · crackedFOUND A/C COMPT RT SIDE L33R END FITTING CRACKED AT FS 8.00. REMOVED AND REPLACED END FITTING ON LONGERON END FITTING L33R IAW SRM 51-1-21, 51-01-27 AND 51-1-8.May 11, 2006 · N818UP · Doug DC873FSDR UPS06846865Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 670 L6L. REMOVED END FITTING AT STA 670 L6L IAW SRM 51-1-20D, DRILLED UP AND INSTALLED END FITTING AT STA 670 L6L IAW SRM 51-03-02, AND SRM 51-1-20D.May 10, 2006 · N818UP · Doug DC873FSDR SWAA061589Stringer Splice · crackedDURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14 L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.May 10, 2006 · N676SW · Boeing 7373A4SDR UPS06446954Stringer · corrodedINSPECTION TYPE:C BULK CARGO STR CORROSION FROM BS 1945-1960 S50R. CORROSION BLEND OUT 0.055" BY 1" BY 6" EXCEED SRM LIMIT. BULK CARGO COMPT BS 1930-1960 STR 50R AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 8.May 9, 2006 · N521UP · Boeing 747212BSDR 06FDEA1759Stringer · crackedFOUND STRINGER CLIP AT BS 600 LT STR 24 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-5.May 9, 2006 · N493FE · Boeing 727227SDR 06FDEA1755Stringer · corrodedCORROSION FOUND AT STRINGER 26R BETWEEN STA 700 TO STA 720 WAS OUT OF LIMITS AFTER CORROSION REMOVAL. REMOVED DAMAGED AREA (SECTION OF STRINGER) IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR PART IAW SRM 53-10-3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2. REPAMay 9, 2006 · N491FE · Boeing 727227SDR USAA060679Stringer · corrodedBS 1640-1680 STRINGER 29R CORRODED. REMOVED & REPLACED DAMAGED SECTION PER SRM 53-00-03, DEFECT SIZE: 21 X 1.0 INCH.May 9, 2006 · N604AU · Boeing 757225SDR USAA060667Stringer · crackedBS 400 NR 3R CRACKED. INSTALLED REPAIR ANGLES AND FILLERS IAW SRM 53-00-03, DEFECT SIZE: .5 INCH.May 9, 2006 · N531AU · Boeing 7373B7SDR USAA060666Stringer Splice · crackedSTA 907, STR 5 CRACKED. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-10-02 AND 51-40-03, DEFECT SIZE: .25 INCH.May 9, 2006 · N531AU · Boeing 7373B7SDR UPS06446906Stringer Splice · crackedINSPECTION TYPE:C AFT CARGO STR SPLICE CRACKED ON BS 1740 S49L. CRACK LENGTH .25 INCH. AFT CARGO COMPT BS 1740 STR 49L SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 8, 2006 · N521UP · Boeing 747200SDR ASAA0680566Longeron · corrodedFOUND LONGERON 28L CORRODED. REPLACED DAMAGED SECTION WITH REPAIR SPLICE PER SRM 53 02 FIG 18.May 8, 2006 · N943AS · Doug DC983SDR ASAA0680563Longeron · corrodedFOUND LONGERON 29R CORRODED. REPLACED DAMAGED SECTION BY INSTALLING NEW SECTION AND A REPAIR SPLICE PER SRM 53 02 FIG 18.May 8, 2006 · N943AS · Doug DC983SDR ASAA0680562Longeron · corrodedFOUND LONGERON 30 CORRODED. REPLACED DAMAGED SECTION OF LONGERON PER SRM 51 10 4 51 30 2 AND 51 30 5.May 8, 2006 · N943AS · Doug DC983SDR UPS06446894Stringer · crackedINSPECTION TYPE:C FWD CARGO LT SIDEWALL BS 500 STR 38 FOUND CRACKED AT RIVET AREA. CRACK LENGTH .5 INCH. FWD CARGO LT BS 473 TO BS 500 STR 38 REPAIRED AS PER SRM 53-10-03 FIG 3.May 6, 2006 · N521UP · Boeing 747200SDR UPS06246858Stringer · corrodedFOUND STRINGER AT FRAME 540 RBL22 HAS CORROSION, PLS. REMOVE CORROSION AND CHECK WITHIN LIMITS. DAMAGED PART OF STR FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. DAMAGED STR REMOVED IAW SRM 51-40-4. NEW SPLICES FABRICATED IAW SRM 51-4 0-4. REPROTECTED NEW SMay 6, 2006 · N954UP · Boeing 727185CSDR DU4R2006466Longeron · crackedLONGERON 3L CRACKED IN 2 EACH PLACES AT FS 160. REMOVED CRACKED SECTION OF LONGERON. DRILLED UP AND INSTALLED 17.5" X 2.25" SECTION FROM P/N S2777922-1-26500 AND 15.25" X 2.5" FROM P/N 7637813-3 IAW DC-9/MD-80 SRM 53-02 FIG 18.May 5, 2006 · N930DL · Doug MD88SDR UPS06446933Stringer · corrodedRT LOWER FUSELAGE EXTERNAL SKIN SURFACE FOUND BILGE UP AT STA 2160 TO STA 2170 STR 45R. BULK CARGO BS 2150 TO BS 2180 S45R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.May 5, 2006 · N521UP · Boeing 747211BSDR 06FDEA1720Stringer · corrodedCORROSION IN STRINGER CHANNEL STA 1070 - 1110 STR 29R. INSTALLED REPAIR HAT SPLICE SECTIONS BETWEEN 1080-1120 IAW SRM 53-10-3.May 5, 2006 · N493FE · Boeing 727200SDR USAA060664Stringer · crackedFOUND CRACK STA 1470 RBL 16.00 STRINGER. REMOVED AND REPLACED STRINGER PER SRM 53-60-53, DEFECT SIZE: 2".May 5, 2006 · N633AU · Boeing 7572B7SDR SROM200600005Stringer · corrodedDURING HEAVY MAINTENANCE INSPECTION FOUND CORROSION AT STR 28 LT, STA 1000 TO 1006. CORROSION FOUND TO BE BEYOND LIMITS. STRINGER REPLACED I.A.W. B737 SRM 53-10-2 AND 51-10-1 PG. 9 PARA 7. STRINGER REPLACED STA 986 - 1016 PLUS/MINUS 28". ORIGINAL SPLICE REMay 3, 2006 · N245US · Boeing 737201SDR 2006UALA00880Stringer · damagedPASSENGER CABIN STRINGER 8L AT STA 787 HAS DAMAGE IN LIP RADIUS.May 3, 2006 · N934UA · Boeing 737522SDR SWAA061480Stringer · crackedDURING SCHEDULED SERVICE CHECK, FOUND STRINGER 25R CRACKED AT BS 885. REPAIRED STRINGER PER SWA EA.May 3, 2006 · N519SW · Boeing 7375H4SDR 2006UALA00859Stringer · corrodedFOUND BULK CARGO COMPT BILGE AREA, STRINGER 51L CORRODED BS 1930-1960.May 2, 2006 · N178UA · Boeing 747422SDR DOSS13Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N410BA · Let L23SUPERBLANSDR DOSS12Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE REAR COCKPIT (RCP) LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDSMay 2, 2006 · N422BA · Let L13ACBLANIKSDR DOSS11Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS ASMay 2, 2006 · N419BA · Let L23SUPERBLANSDR DOSS10Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N438BA · Let L23SUPERBLANSDR DOSS08Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LH RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N433BA · Let L23SUPERBLANSDR DOSS07Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N431BA · Let L23SUPERBLANSDR DOSS06Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS ASMay 2, 2006 · N430BA · Let L23SUPERBLANSDR DOSS04Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N427BA · Let L23SUPERBLANSDR D20060502Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LH RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N420BA · Let L23SUPERBLANSDR DOSS102Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS ASMay 2, 2006 · N420BA · Let L23SUPERBLANSDR DOSS002Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LH RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IMay 2, 2006 · N420BA · Let L23SUPERBLAN
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