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 QXEA9901242Stringer · corrodedPDX - STRINGER 74 HAS CORROSION ON TOP SIDE WHERE IT PASSES THROUGH FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.May 26, 1999 · N493US · Fokker F28MK4000SDR QXEA9901240Stringer · corrodedPDX - STRINGER 74 HAS TOP SURFACE CORROSION BETWEEN FRAMES 9305A AND 9305B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.May 26, 1999 · N493US · Fokker F28MK4000SDR USAA990475Stringer · corrodedTPA - DURING CX-6 CHECK, FOUND CORROSION IN STRINGER 27L APPROX 20 INCH LONG AT STATION 996 TO 1016, CORROSION LEVEL 1. REPLACED CORRODED SECTION OF STRINGER, SPLICED IN NEW STRINGER AT STATION 956 TO 1016 PER SRM 53-10-3 FIG 1. (M)May 25, 1999 · N270AU · Boeing 7372B7SDR RRXA991584Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 24 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-2. (CORROSIOMay 25, 1999 · N993CF · Doug DC862SDR RRXA991583Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 64 RIGHT, AND WL 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53May 25, 1999 · N993CF · Doug DC862SDR QXEA9901223Stringer · crackedPDX - LEFT-HAND FORWARD CABIN STRINGER 36 HAS ONE CRACK AT INSULATION FASTENER HOLE, 1.7 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.May 25, 1999 · N493US · Fokker F28MK4000SDR QXEA9901203Stringer · crackedPDX - STRINGER 35 CRACKED AT INSULATION FASTENER HOLE, 6.6 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.May 25, 1999 · N493US · Fokker F28MK4000SDR QXEA9901181Stringer · crackedPDX - STRINGER 34 CRACK/CORROSION AT HOLE, 2.6 INCHES AFT OF FRAME 5305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.May 25, 1999 · N493US · Fokker F28MK4000SDR QXEA9901175Stringer · corrodedPDX - STRINGER 34 FORWARD END, 2.5 INCHES AFT OF FRAME 4900 HAS EXFOLIATION CORROSION. REPAIRED IAW FOKKER SRM 53-02-06.May 25, 1999 · N493US · Fokker F28MK4000SDR QXEA9901163Stringer · corrodedPDX - THERE IS CORROSION ON STRINGER 43 APPROXIMATELY 3 INCHES AFT OF FRAME 12414. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9, PARAGRAPH 4B AND SRM 53-10-4 PAGE 8, PARAGRAPH 3C.May 25, 1999 · N493US · Fokker F28MK4000SDR P2EA99209Stringer · crackedSJO - DURING C-CHECK, STRINGER 17L WAS CRACKED FROM BS 727 TO BS 796. REPAIRED PER EO COO-3-53-334-99 DATED 5/28/99. (M)May 25, 1999 · N412CE · Boeing 737205SDR MWEA99306Longeron · corrodedFOUND HEAVY CORROSION ON LONGERON 24R AT STATION 1361. MTC FABRICATED AND INSTALLED NEW LONGERON.May 25, 1999 · N803ME · Doug MD88SDR CALA9900574Longeron · crackedINSPECTION FOUND A 1 CRACK IN LONGERON 2R AND FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED, NEW SECTIONS AND SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 18.May 25, 1999 · N72829 · Doug DC982SDR AALA990830Longeron · crackedTUL - FOUND CRACK IN LONGERON 2R AFT OF STATION 1418, ROUTED OUT TO .5 BY .25 PER ESO 80559, DATED 4/3/98. INSTALLED REPAIR PER AARD 53-30-00-2, LONGEORN SPLICE. (M)May 25, 1999 · N581AA · Doug DC982SDR SWAA990916Stringer · corrodedDURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT STRINGER 26L AND SPLICE, BS 318. REPAIRED STRINGER AND SPLICE PER SRM.May 24, 1999 · Boeing 7372H4SDR QXEA9901227Stringer · crackedPDX - RIGHT-HAND FORWARD CABIN STRINGER 44 HAS TWO CRACKS BETWEEN FRAMES 6805 AND 7305. ONE CRACK AT EACH INSULATION FASTENER HOLE. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901226Stringer · corrodedPDX - RIGHT-HAND CABIN STRINGER 41 HAS CORROSION DAMAGE LOCATED JUST ABOVE FRAME 6805 AND 2.9 FORWARD OF EXISTING REPAIR. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION A-A, FIGURE 1.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901207Stringer · crackedPDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901206Stringer · crackedPDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 8.8 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901192Stringer · corrodedPDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901191Stringer · corrodedPDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 2.6 FORWARD FRAME 9305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901180Stringer · crackedPDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 2.7 INCHES FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901179Stringer · crackedPDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 9.7 FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.May 24, 1999 · N493US · Fokker F28MK4000SDR QXEA9901137Stringer · crackedPDX - STRINGER 47 CORROSION/CRACK AT HOLES, 2 CRACKS ONE AT EACH HOLE 6.3 AFT OF FRAME 6805 AND 6.4 FORWARD OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06.May 24, 1999 · N493US · Fokker F28MK4000SDR CKSA99066Stringer · corrodedDURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 865 TO STA 883. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. FABRICATED AND TREATED REPAIR PARTS IAW L1011 SRM 51-21-02. REPAIR CARRMay 24, 1999 · N102CK · Lkheed 1011385115SDR CKSA99060Longeron · corrodedDURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND LONGERON CORRODED AT ZONE 110, STA 270. DETERMINED TO BE OUT OF LIMITS IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-50-02 AND 51-40-01/02. FOUND AT GAMCO MAINTENANCE FACILITY (May 24, 1999 · N102CK · Lkheed 1011385115SDR CKSA99059Stringer · corrodedDURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 649 TO STA 749. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. FOUND AT GAMCO MAINTENANCEMay 24, 1999 · N102CK · Lkheed 1011385115SDR ABXA9900516Longeron · corrodedLONGERON 22 RIGHT HAD EXFOLIATION CORROSION AT STATION 1680. REPAIRED IAW DC8 SRM 53-2-2.May 24, 1999 · N816AX · Doug DC863SDR QXEA9901209Stringer · crackedPDX - STRINGER 31 CRACKED AT INSULATION FASTENER HOLE, 6.3 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 23, 1999 · N493US · Fokker F28MK4000SDR QXEA9901208Stringer · crackedPDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.8 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 23, 1999 · N493US · Fokker F28MK4000SDR QXEA9901198Stringer · crackedPDX - STRINGER 30 IS CRACKED AT INSULATION FASTENER HOLE MID WAY BETWEEN FRAME 7305 AND 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.May 23, 1999 · N493US · Fokker F28MK4000SDR QXEA9901194Stringer · crackedPDX - LEFT-HAND CABIN STRINGER 31 HAS CRACK WITH CORROSION AT HOLE, 6.3 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 23, 1999 · N493US · Fokker F28MK4000SDR QXEA9901193Stringer · crackedPDX - LEFT-HAND CABIN STRINGER 30 HAS CRACK WITH CORROSION AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.May 23, 1999 · N493US · Fokker F28MK4000SDR ASAA9980119Longeron · corrodedOAK - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28R AT FS 1137. REPAIRED IAW ASA EA 5310-01689. (M)May 23, 1999 · N947AS · Doug DC983SDR USAA990466Stringer · crackedCLT - DURING CX CHECK, FOUND STRINGER 5 LT CRACKED 1 INCH AT STATION 1142. STOP DRILLED, USED .1875 HI-LOCK FOR REAMED HOLES FOR INSTALLED ANGLE PER SRM 51-10-02 AND EA 64489. (M)May 22, 1999 · N336US · Boeing 737301SDR USAA990459Stringer · crackedCLT - DURING Q-6 CHECK, FOUND 1 INCH CRACK IN RADIUS OF STRINGER AT STRINGER 5 LEFT AT STATION 1142. INSTALLED REPAIR ANGLE PER EA 64489. (M)May 22, 1999 · N336US · Boeing 737301SDR UPS99829779Longeron · corrodedINSPECTION TYPE:C1, FWD PIT FS 600 L36 CORRODED. FABBED SPLICE SHIMS IAW TIMCO REO-06533, ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND TIMCO REO-06533.May 22, 1999 · N851UP · Doug DC873FSDR TWAA9907512Longeron · crackedFOUND .5 INCH CRACK IN LONGERON 2L, STA 775. REPAIRED CRACKED LONGERON 2L AT STA 775 PER SRM 53-02, FIG 18. CHECK-C 10-17-98 STL.May 22, 1999 · N412EA · Doug DC951SDR TWAA9907511Longeron · crackedFOUND .5 INCH CRACKS IN LONGERON 5L AND 3L, STA 775. SPLICED LONGERON SECTIONS PER SRM 53-02, FIG 18. CHECK-C 10-17-98 STL.May 22, 1999 · N412EA · Doug DC951SDR QXEA9901219Stringer · crackedPDX - STRINGER 28 HAS CORROSION WITH CRACKS AT TWO INSULATION FASTENER HOLES BETWEEN FRAMES 7305 AND 7805. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B, FIGURE 1EE.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901218Stringer · crackedPDX - STRINGER 28 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901217Stringer · crackedPDX - STRINGER 28 CORRODED AT CRACK 8.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901215Stringer · crackedPDX - STRINGER 28 IS CRACKED AT INSULATION FASTENER HOLE, 2.7 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901202Stringer · corrodedPDX - STRINGER 28 CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.8 FORWARD FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901201Stringer · corrodedPDX - STRINGER 28 IS CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.5 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.May 22, 1999 · N493US · Fokker F28MK4000SDR QXEA9901190Stringer · corrodedPDX - LEFT-HAND CABIN STRINGER 28 CORRODED BETWEEN FRAMES 8805 AND 9305. REPAIRED IAW FOKKER SRM 53-02-0, FIGURE 1EE.May 22, 1999 · N493US · Fokker F28MK4000SDR GTIA9901013Stringer · misdrilledMHV - PASSENGER CABIN INTERNAL STATION 550 TO 570 STRINGER L-17 THERE ARE APPROX 25 HOLES WITH SHORT C/C SPACING S/B .600 IAW SRM 53-02 FIG 18 SH 6 ARE .48-.58 REF NR A092-S03-W084. REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STATION 531 TO STATION 5May 22, 1999 · N934ML · Doug DC931SDR ABXA9900522Longeron · corrodedHEAVY CORROSION ON LONGERON 35 LEFT AT STATION 1760. REPAIRED IAW DC8 SRM 53-2-2 AND DWG NR 1415997.May 22, 1999 · N816AX · Doug DC863SDR GTIA9901024Longeron · crackedMHV - PASSENGER CABIN INTERNAL STA 560 LONGERON L-17 HAS A CRACK. HOLES WERE MIS-DRILLED. REPAIR WILL BE ACCOMPLISHED ON W/C NR A092-S39-W132. W132 - REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STA 531 TO STA 588, PRODUCTION SPLICE PER ENGINEERING May 21, 1999 · N934ML · Doug DC931SDR GTIA9901023Stringer · crackedMHV - BS 207 LT, STR 13 WEB IS CRACKED. RECEIVED VERIFICATION OF REPAIR MAT'L ON P.O. NR 80319. TRIMMED CRACKED MEMBER IAW DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 AND SRM 51-30-2. (X)May 21, 1999 · N934ML · Doug DC931
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