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 ASAA0580431Longeron · corrodedOKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)Aug 7, 2005 · N935AS · Doug DC982SDR DHL2005748503Stringer · corrodedAFT CARGO COMPT LOWER FUSELAGE STR 29L IS CORRODED BETWEEN STA 970 AND STA 990. REMOVED STR 29L KEEL BEAM CHORD FROM BS 950-1010 DRILLED AND LOCATED NEW KEEL BEAM CHORD P/N 65-56441-7 PO NR 53143 IAW S/B 727-53-179 FIG 12 TREATED AND PRIMED AREA AND CHORD IAWAug 7, 2005 · N748DH · Boeing 727225SDR AWXA200501026Stringer · crackedDURING C15 CHECK DISCOVERED STRINGER 18A SHEAR BEAM CRACKED 2.0 INCHES IN LENGTH AT THE AFT END. MAINTENANCE TRIMMED OUT EXISTING CRACK IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5361-05241-RC1. FABRICATED FILLER AND RADIUS FILLER IAW AWA ER 03-5361-052Aug 7, 2005 · N311AW · Boeing 7373G7SDR ASAA0580428Longeron · damagedOKC - DURING C-CHECK, FREEZE PLUG IN OVERSIZED HOLE IN LONGERON. REMOVED DAMAGED SECTION. SPLICED IN NEW LONGERON SECTION. (M)Aug 5, 2005 · N947AS · Doug DC983SDR 05FDEA02287Stringer · unknownEVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, (STRINGER REPAIR STR 28L, BS 700, WL 148). REMOVED PREVIOUS STR. REPAIR SPLICE AND REPAIR SECTION BS 700 720 2" STR 28L WL 148, PER SRM 51-30-2. FABRICATEAug 5, 2005 · N489FE · Boeing 727200SDR 05FDEA02281Longeron · corrodedCENTER CARGO FOUND EXFOLIATION CORROSION ON LONG 48 LT SIDE BETWEEN STA 1601 AND 1621. REPAIR IAW SRM 53-10-00 FIG 2 VOL 1.Aug 5, 2005 · N624FE · Doug MD11SDR 05FDEA02280Longeron · corrodedFWD CARGO COMPT FOUND EXFOLIATION CORROSION ON LONG 52 AT STA 1039. REPAIR SRM 53-10-00 FIG 1 & 2 VOL 1.Aug 5, 2005 · N624FE · Doug MD11SDR 05FDEA02278Longeron · corrodedFWD CARGO COMPT FOUND SEVERE CORROSION ON LONGERON 48 LEFT AT STA 6-60. REPAIR IAW SRM 53-10-00 FIG 2 VOL I.Aug 5, 2005 · N624FE · Doug MD11SDR 173Stringer · corrodedCORROSION AT STR. 28R AT BS 650. S/O 283001, DELTA N//R NR 22590Aug 5, 2005 · N624DL · Boeing 757232SDR USAA050973Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 8R AT STATION 500. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-03. (M)Aug 4, 2005 · N588US · Boeing 7373B7SDR SWAA052304Stringer · corrodedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 795, STR 26R. REPAIRED STRINGER PER SWA EA.Aug 3, 2005 · N307SW · Boeing 7373H4SDR 05FDEA02182Longeron · crackedONE CRACK 4 INCHES LONG ON LONGERON INSIDE APU COMPT RT SIDE STA 2050. REPAIRED CRACK PER SRM 53-17-01 VOL 3 FIG 4, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2.Aug 2, 2005 · N381FE · Doug MD1010FSDR 05FDEA02175Longeron · crackedONE CRACK 1 INCH LONG ON LONGERON INSIDE APU COMPT STA 2050. REPAIRED CRACK PER SRM 53-17-01 FIG 4 VOL 3, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2.Aug 2, 2005 · N381FE · Doug MD1010FSDR FQW2006F00000Longeron · brokenTOP LT LONGERON BROKE JUST FWD OF HORIZONTAL STABILIZER FORWARD FITTING. (K)Aug 1, 2005 · N12BS · Wsk PZLM18BSDR 05FDEA02167Longeron · corrodedCENTER CARGO STATION 5-93 TO STATION 5-113 LONGERON 46R CORROSION FOUND AT TWO LOCATION AS MARKED. CORRODED LONGERON AT 46R CTR CARGO STA 5-93 TO STA 5-113 ON TWO LOCATION CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG. 2. VOL. I. AND FEDEX EA 1-5310-87568 (TAug 1, 2005 · N579FE · Doug MD11SDR 05FDEA02162Longeron · crackedCENTER CARGO COMPARTMENT HAS STA 1787 RT LONGERON 45 CRACKED. REMOVED AND REPLACED AS PER DRAWING AFA7097 AND SRM 51-31-01.Aug 1, 2005 · N575FE · Doug MD11SDR 05FDEA02151Longeron · corrodedCENTER CARGO BILGE STATION 1601 LONGERON 45R CORROSION FOUND AS MARKED. CORRODED LONGERON ON CENTER CARGO STATION 1601 LONGERON 45RH TRIMMED OUT AT STATION 1591 AND STATION 1611 AND REPAIR CARRIED OUT AS PER SRM 53-10-00 FIGURE 1 VOLUME I AND FEDEX EA 1Jul 31, 2005 · N579FE · Doug MD11SDR 05FDEA02150Longeron · corrodedCENTER CARGO BILGE STATION 1751 LONGERON 46R CORROSION FOUND AS MARKED. CORROSION ON CENTER CARGO BILGE STATION 1751 LONGERON 46 R/H REMOVED AS PER SRM 51-21-01 VOL II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01, FIG 3, VOL I. ORIGINAL THICKNESS=0.145", Jul 31, 2005 · N579FE · Doug MD11SDR 05FDEA02149Longeron · corrodedCENTER CARGO BILGE STATION 1661 LONGERON 48L FOUND CORRODED. CORROSION AT CENTER CARGO BILGE STATION 1661 LONGERON 48L CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG. 2 SHT 5 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jul 31, 2005 · N579FE · Doug MD11SDR 2005UALA00734Stringer Clip · crackedCABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 685, STR 4 LT. REMOVED AND REPLACED STRINGER CLIP.Jul 29, 2005 · N914UA · Boeing 737522SDR COMA057088Stringer · dentedAFT RT FUSE AT FS1057 STR 14R-15R HAS 2.6L X 1.6W X .040D DENT. TRIMMED OUT DAMAGED AREA, LPI OR EDDY CURRENT TO ENSURE NO CRACKS EXIST. FABRICATE AND INSTALL DOUBLER (2024-T3 .063) IAW BRAS EO 601R-53-6952.Jul 29, 2005 · N354CA · Cndair CL6002C10SDR SIMA200521611Stringer · chafedABI - FOUND STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, 145/1142 REV 29 CHAPTER 53-24-02. (M)Jul 28, 2005 · N815AE · Emb EMB135KLSDR SIMA200521601Stringer · chafedSTRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM 145/1142 REV 30, CHAPTER 53-24-02. (M)Jul 28, 2005 · N815AE · Emb EMB135KLSDR SIMA200521603Stringer · chafedABI - STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUT OUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-24-02. (M)Jul 28, 2005 · N815AE · Emb EMB135KLSDR SWAA052220Stringer · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 330, STR 11R. REPAIRED STRINGER PER SRM.Jul 28, 2005 · N307SW · Boeing 7373H4SDR SWAA052248Stringer · corrodedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 805, STR 26L. REPAIRED STRINGER PER SRM.Jul 28, 2005 · N307SW · Boeing 7373H4SDR 05FDEA02111Longeron · corrodedFORWARD CARGO: BILGE AREA STA 6-10 L51L LONGERON FOUND CORRODED. CORROSION AT LONGERON END FWD CARGO BILGE STA 6-10 L51R TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 VOL. I FIG. 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 27, 2005 · N579FE · Doug MD11FSDR UPS05445019Stringer · crackedBS 560 S9L STRINGER END FOUND CRACK, CRACK LENGTH 7/16". BS 560 STR 9L STR END REPAIRED AS PER SRM 53-10-03 FIG 2.Jul 26, 2005 · N683UP · Boeing 747121SDR 2005FA0001091Longeron · crackedBOTH UPPER LONGERON WAS CRACKED APPROXIMATELY 54 INCHES AFT OF DATUM. THE AREA IS DIFFICULT TO INSPECT AS IT IS 75 PERCENT COVERED BY THE HOPPER. THIS IS A VERY UNUSUAL AREA TO FIND SUCH A DEFECT. THE AC HAS NO DAMAGE HISTORY AND HAS NOT BEEN ABUSED. (K)Jul 26, 2005 · N4020Q · Ayres STRT34SDR ASAA0580398Longeron · damagedOKC - FOUND DURING C-CHECK, FREEZE PLUG IN LONGERON. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION. (M)Jul 25, 2005 · N947AS · Doug DC983SDR UPS05445174Stringer · crackedM/D BS 1740-1760 S3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.5". M/D BS 1740-1760 STR 3R STRINGER END REPAIRED AS PER HX RS R53-61-35355. FOLLOW UP INSPECTION FOR THIS REPAIR IS REQUIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445173Stringer · crackedBS 1740-1760 S2R STRINGER END FOUND CRACK, CRACK LENGTH 2". M/DECK BS 1740-1760 STR 2R STRINGER END REPAIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445063Stringer · crackedBS 2180-2200 S25R STRINGER FOUND CRACKED, CRACK LENGTH 5/8". BS 2180 TO BS 2208 STR 25R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445025Stringer · crackedBS 1940-1960 STR 11R STRINGER END FOUND CRACKED, CRACK LENGTH 1 INCH. BS 1930 TO BS 1960 STR 11R REPAIRED AS PER SRM 53-10-03 FIG 4.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445024Stringer · crackedBS 1940-1960 STR 3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.25 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3R BETWEEN BS 1930 AND 1960.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445023Stringer · crackedBS 1958-1960 STR 3L STRINGER END FOUND CRACKED, CRACK LENGTH 1.625 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3L BETWEEN BS 1930 AND 1960.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445022Stringer · crackedBS 1958-1960 STR 1L STRINGER END FOUND CRACKED, CRACK LENGTH 3.875 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR - 1L BETWEEN BS 1930 AND 1960.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445021Stringer · crackedBS 1940-1960 S1R STRINGER END FOUND CRACKED, CRACK LENGTH 1.125. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 1R BETWEEN BS 1930 & 1960.Jul 23, 2005 · N683UP · Boeing 747121SDR UPS05445018Stringer · crackedBS 1958-1960 STR 2L STRINGER END FOUND CRACK, CRACK LENGTH 1.5". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR-2L BETWEEN BS 1930 AND 1960.Jul 23, 2005 · N683UP · Boeing 747121SDR AWXA200500949Stringer · corrodedMCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION IN SEVERAL LOCATION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6". MAINTENANCE REMOVED CORROSION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6", IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMJul 21, 2005 · N627AW · Airbus A320231SDR UPS05M45582Longeron · corrodedINSPECTION TYPE:C, CABIN ANGLE FITTING BETWEEN STA 1239-1256 LONGERON 27 RT FOUND CORRODED. CORROSION REMOVED AT CABIN AREA STA 1239 TO 1256, FOUND OUT OF LIMIT. ORIG THK 0.238" & MAT REMOVED IS 0.090" PER SRM 53-00-01 F3.V1 R.37. ANGLE FITTING BRACKET REMJul 20, 2005 · N256UP · Doug MD11FSDR SIMA200520604Stringer · chafedA PREVIOUS REPAIR ANGLE ON STRINGER 19R WAS FOUND CHAFED. REMOVED THE EXISTING REPAIR ANGLE AND CLEANED THE AREA. FABRICATED AN INSTALLED A NEW REPAIR ANGLE. REPAIR DONE IAW SRM. (K)Jul 20, 2005 · N813AE · Emb EMB135KLSDR 2005UALA00679Stringer · corrodedSTRINGER 42L HAS CORROSION BETWEEN FRAME 57 AND 58. REPLACEMENT OF STRINGER (PSE) ACCOMPLISHED.Jul 20, 2005 · N418UA · Airbus A320232SDR 2005UALA00678Stringer · corrodedSTRINGER 43L HAS CORROSION AT FRAME 58. REPLACEMENT OF STRINGER (PSE) ACCOMPLISHED.Jul 20, 2005 · N418UA · Airbus A320232SDR YNT2005F00000Stringer · corrodedCORROSION ON STRINGER L17, FS 336, CORROSION REMOVED AND A REPAIR STRAP INSTALLED OVER REPAIRED AREA. (SW05200510589) (K)Jul 19, 2005 · N188JS · Gulstm G1159SDR 05FDEA01995Longeron · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: ON FWD CARGO COMPARTMENT BTW STA 808-821 L 52, CORROSION ON SHOVEL END AND LONGERON. ACCOMPLISHED REMOVAL OF SHOVEL END, SPLICES. REMOVED CORROSION. REPAIRED IAW SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAG 1-Jul 19, 2005 · N571FE · Doug DC1010SDR AWXA200500926Stringer · crackedDURING C18 CHECK DISCOVERED STRINGER 8L CRACKED, 1.125 INCHES IN LENGTH, AT BS 380. MAINTENANCE CUT OUT CRACK ON STRINGER 8L, BS 380, IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. FABRICATED TWO ZEE ANGLES AND FILLER IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. Jul 17, 2005 · N313AW · Boeing 7373S3SDR UPS05844965Longeron · corrodedINSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8 SRM 53-2-2 FABRICATED AND INSTALLED LONGERON 34R AT STA 1350-1490 IAW DRWG 3646937Jul 16, 2005 · N807UP · Doug DC873FSDR AWXA200500905Stringer · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION AT STRINGER 31R, FS 65, INTERNAL STRUCTURE UNDER FLOOR COMPARTMENT. MAINTENANCE REMOVED CORROSION AND NO ALLOWABLE DAMAGE WAS FOUND IN SRM. MAINTENANCE REMOVED STRINGER 31R FROM FS 64 TO FS 67 IAW AIRBUS SRM 51-42-1Jul 14, 2005 · N627AW · Airbus A320231SDR 05FDEA01949Longeron · corrodedCORROSION FOUND IN VERTICAL LEG OF LONGERON 47L STATION 1764, LEAVING A HOLE .5 HIGH BY 3.0 LONG AFTER CORROSION REMOVAL WITH REDUCED MATERIAL THICKNESS ON BOTH SIDES OF SUBJECT HOLE. COMPLIED WITH FED EX EA 8-5310-91240 FUSELAGE LONGERON 47L STA 1764 CORROSJul 14, 2005 · N373FE · Doug DC1010
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