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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 95ZZZZ273Stringer · crackedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT STRINGER (P/N 65-56441 WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZZ270Stringer · crackedIN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZX5345Stringer · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE RT AFT FUSELAGE CANTED BULKHEAD AREA, STA 1143, STR 9, EXFOLIATED BEYOND LIMITS. REMOVED 18.025 INCHES OF EXFOLIATED LONGERON, FABRICATED REPAIR LONGERON OF 7075T6-.063SDR 95ZZZX5338Longeron · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE FWD CARGO COMPT. LONGERON NR 30L FROM FS 332 TO FS 450. INSTALLED NEW LONGERON FS 294-FS 450 IAW DC9 SRM 53-02. INSTALLED NEW SPLICES IAW DC9, SRM 53-02. N/R NR 027NSDR 95ZZZX5335Longeron · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FWD CARGO COMPARTMENT, LONGERON 29L FROM FS 332 TO FS 450. INSTALLED NEW LONGERON, FS 332-FS 450 AND FS 332-FS 294, AND INSTALLED NEW SPLICES IAW DC9 SRM 53-02. N/R NRSDR 95ZZZX5334Longeron · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE E AND E COMPARTMENT, LONGERON 22, BETWEEN STA 160 TO STA 180, LOWER LEG. REMOVED DAMAGED LONGERON AND REPAIRED IAW E.O. 95-159. N/R NR 027F1-0007.SDR 9507679916Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 23R END FITTING FS 980 TO 996. REPLACED FITTING AND REPAIRED LONGERON PER SRM 53-02 PG 3.SDR USAA950483Longeron · crackedPIT - WHILE ACCOMPLISHING PRODUCTION CONTROL ITEM 949, FOUND A .5 INCH CRACK RADIALLY IN LONGERON 2R STATION 680 VISUAL INSPECTION. ACCOMPLISHED SPLICE REPAIR PER SRM53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17. (W)SDR DLL10952104Stringer · damagedDURING SERVICE CHECK FOUND TOOLING DAMAGE ON STR 14 RT AT STA 1023. REPAIRED PER SRM 53-13-00 PG. 806.SDR USAA950580Stringer · crackedPIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND .5 INCH CRACK (RADICAL) AT STRINGER NR 68 RT SIDE FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 RT SIDE AFT OF FRAME STATION SDR USAA950579Stringer · crackedPIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A .5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 PER SRM 51-70-06. (M)SDR UPS803175Longeron · cracked(SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND TWO CRACKS APPROX 1.5 INCHES LONG EACH AT STA 81, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 51-1-20.SDR UPS803162Longeron · corrodedDURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32L AT FS 1746. REPLACED LONGERON PER SRM 51-1-20D.SDR 95ZZZZ256Longeron · corrodedLEVEL 2 CORROSION, INSIDE OF NR 1 HEAT EXCHANGER COMPT FWD BULKHEAD AT FS 315 LOWER I/B CORNER NEAR GEAR DOOR HINGE HOUSING, LONGERON 36. REMOVED DAMAGED AREA, TREATED AND PRIMED, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00.SDR CAL950365Stringer · crackedGSO - INSPECTION FOUND, CRACKS AND CORROSION IN STRINGER 20R AT STA 500 TO 520. THE CRACKS WERE .125 INCH TO .25 INCH IN LENGTH. THE DAMAGED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (Z)SDR 9507309886Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 25R FROM FS 1258 TO 1292 AND ON ATTACH FITTING. REPLACED LONGERON AND FITTING PER SRM 51-00.SDR SWAA950353Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950338Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND STRINGER GOUGED AT BS 864, S15L, AND AT BS 928 TO 935, S14R, STRINGER CRACKED AT BS 1140, 12L, AT BS 787, S10R, AT BS 1016, S7L, AT BS 907, AT S4R AND L, AT BS 467, AT S22L, STRINGER CORRODED AT BS 1138, S13L, AND AT BS 520 TO SDR SWAA950335Stringer · damagedDURING SCHEDULED D-CHECK, FOUND TOOLING MARKS ON STRINGER AND SKIN DOUBLER AT BS 727B AND S7R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR DL72S952015Stringer · crackedAT HMV, FOUND STRINGER 15R CRACKED AT ITS END JUST FWD OF WING ICE LIGHT HOUSING AT FS 720B. REPAIRED PER SRM 53-10-3 FIG 1.SDR 9507022703Longeron · crackedDURING PERIODIC CHECK, MAINTENANCE FOUND FUSELAGE BELLY SKIN AND SURROUNDING STRUCTURE STR 29R, FS 980 TO 1015 CORRODED AND CRACKED. REPAIRED PER NWA EA 27-096533 (MFG PART NUMBER 65C1391-1).SDR DL72S951973Stringer · crackedA HMV, STRINGER CRACKED, .25 INCH CRACK IN STGR 20R JUST FWD OF STA 344. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED REPAIRS PER SRM 53-10-3.SDR 9507093208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41L AND 43L. CORROSION IS LOCALIZED AROUND FASTENERS COMMON TO FUSELAGE SKIN. CORROSION ON STR 41L EXISTS BETWEEN FRAMES 25 AND 35. CORROSION ON STR 43L IS LOCATED BETWEEN FRAMES 29 AND 34. REPAIREDSDR DL72S952207Stringer · corrodedSTRINGER 27L BETWEEN STA 560 AND STA 580 FWD CARGO CORRODED. REMOVED DAMAGED SECTION OF STRINGER, SPLICED PER SRM 53-10-3 PG 3, FOUND AT HMV.SDR DL72S951936Stringer · corrodedAT HMV, FOUND CORROSION DAMAGE TO STRINGER 27R AT FS 740. REPAIRED PER SRM 53-10-3 FIG 1.SDR DL72S951934Stringer · corrosionAT HMV, FOUND FUSELAGE STRINGER 26R WITH CORROSION DAMAGE AT FS 1144. REPAIRED PER SRM 53-10-3 FIG 1.SDR 9507603208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON LONGERON 44 OUTER FLANGE BETWEEN FR 33 TO 34. REPLACED LONGERON 44 PER EA 32-97859.SDR 9507313208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE RIVETS COMMON TO STR 44 BETWEEN FRAMES 33 AND 34. AFTER REMOVING THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE OF THE STRINGER FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA ESDR 9507103208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON RIVETS COMMON TO STR 40L BETWEEN FRAMES 29 AND 30. AFTER REMOVAL OF THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EA 32-97855. SERISDR 95ZZZZ257Longeron · corrodedLEVEL 2 CORROSION, C1 CARGO LONGERON, DOUBLER AFT OF FS 449 BULKHEAD BELOW CARGO FLOOR BBL-0 HAS CORROSION. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00.SDR 95ZZZX4111Stringer · damagedATW - C/W E.O. E95/005/653. ORIGINAL ISSUE ON LT AND RT FRAME 29 STRINGERS AT STA 25.94 FOUND DAMAGED. REPAIRED RT FRAME 29 STRINGER AT STA 29.54 IAW E.O. E95/005/653. ORIGINAL ISSUE. REPAIRED LT FRAME 29 STRINGER AT STA 25.94 IAW E.O. E95/005/653. ORIGINSDR 9507073208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 AND 34. CORROSION IS LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF THE CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97847. SERIAL NRSDR AALA950741Stringer · disbondedTULE - THE FOLLOWING STRINGERS IN ZONE 310 DISBONDED, STA 25016 - STA 25516. LEFT STRINGERS (21 EACH) NR 7 THROUGH NRS 17, 19, 20, 21A, AND NR 23 THROUGH NR 30. RIGHT STRINGERS (15 EACH) NR 45 THROUGH NRS 52, 53A, 55, 56, 58, 60, 61, 62, AND 64. TOTAL CYCLESDR 95FDEA00479Stringer · crackedCRACKED STR 6L AT BS 990 WL 288. REPAIRED STR 6L AT BS 990 WL 288 PER FEDEX SRM 53-10-3.SDR 95FDEA00460Stringer · crackedCRACKED STR 22L, BS 1030. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS NET WITH SEAL AND INSTALLED FASTENERS, ALL WORK DONE IN ACCORDANCE WITH FEDEX SRM 53-10-3 AT BS 1030 STR 22L. MFG P/N M377459, BAC1498132, M424422.SDR 95FDEA00457Stringer · corrodedCORROSION ON STR 22L, BS 1165. REPAIRED STR 22L AT BS 1165 PER FEDEX SRM 53-10-3 FIG 1.SDR 9507053208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 32 AND 33. CORROSION IN LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97845. SERIAL NR 32 SDR USAA950584Longeron · crackedPIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK AT HI-LOK AT LONGERON 3 LEFT STATION 180. INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2. (M)SDR UPS203073Stringer · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 17L AT STATION 742 AND WL 208. MAINTENANCE REMOVED THE CRACK AND REPAIRED THE STRINGER PER UPS 727-52-1580.SDR UPS203070Stringer · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 18A ON THE RIGHT HAND LOWER VERTICAL FLANGE AT STATION 860 TO 865. MAINTENANCE REMOVED THE CORROSION AND REPAIRED IAW UPS EO 727-53-1575.SDR UPS203056Stringer · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 17R AT STATION 757, RBL 70.5 AND WL 207. MAINTENANCE REMOVED THE CORROSION AND REPAIRED AREA PER UPS EO 727-53-1576.SDR ABXA9500435Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 415. REPLACED LONGERON IAW DC-9 SRM 51-30-5, 51-30-7 AND 51-30-1.SDR HEEA954830Longeron · corrodedLONGERON CORRODED DEEP AT STATION 101.38 SPLICE AS SEEN IN UPPER R/H AFT CORNER OF BAGGAGE COMPARTMENT, JUST OUTBOARD OF WHERE THE BAGGAGE COMPARTMENT CEILING PANEL ATTACHES TO LONGERON.SDR HAL95048Stringer · corrosionSBA - ITEM FROM SBA NR 18N00907 C-CHECK, LEVEL 2 CORROSION ON STRINGER AND AROUND FASTENERS STA 699 - STA 770, RBL 13 (KEEL BEAM AREA). REMOVED CORROSION, CLEANED AND TREATED PER SRM 51-10-3. INSTALLED REPAIRED SPLICE PER SRM 53-02. (X)SDR ABXA9500437Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 579. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR USAA950486Longeron · crackedIND - DURING CX-2 INSPECTION ACCOMPLISHED SID INSPECTION PSE REF 53.09.001, FOUND .5 INCH CRACK ACROSS LONGERON AT STATION 408 LONGERON 17 RIGHT. ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 PG 2A AND USAIR EA 30247. (W)SDR P5CA9500049Stringer · corrodedDURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION BETWEEN FASTENER HOLES STRINGER 4L AT BS 1539. CLEANED CORROSION AND FOUND WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, ALODINED AND PRIMED.SDR P5CA9500048Stringer · corrodedDURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION STRINGER 4L AT BS 1595, LEVEL 2. REPLACED STRINGER SECTION PER BOEING SRM 53-10-3 FIGURE 5.SDR DL72L951767Stringer · corrodedFOUND ON CV2 CHECK, CORROSION ON TOP OF STR 30 BETWEEN STA 1148 AND 1166 BL 0. REPAIRED AS PER SRM 53-10-3 AND ID PER PS 900-5-1 FIG 4.SDR 95ZZZX2832Stringer · crackedDURING AN 'ANNUAL' INSPECTION, FOUND NLG SUPPORT STRINGER CRACKED ACROSS OPENING FOR THE LT NLG DOOR ROD. LOOKING CLOSER, FOUND BOTH DOUBLERS CRACKED AT SAME LOCATION.
Back to JASC 5313