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 RRXA11432Longeron · corrodedDURING A MAINTENANCE VISIT FOUND L31L CORRODED BEYOND LIMITS AT STA 450-520. REPLACED SECTION PER DHSK 873-508SDR AWXA0002050Stiffener · corrodedD: Web support beam at R/H APU torque box BS 1098 has exfoliated corrosion on stiffener.C: Repaired web support beam stiffener IAW B737 SRM 51-40-3 Fig 1 Pgs. 1-6 and BAC DWG 65-54832SDR 2002F00723Stringer · corrodedFOUND FUSELAGE INTERIOR AT BS 294 THROUGH BS 314 STRINGER 21R HAS SURFACE CORROSION. (M)SDR RRXA11422Longeron · crackedDURING A MAINTENANCE VISIT FOUND LONGERON 30R CRACKED AND CORRODED BETWEEN STA 8-70. REPLACED LONGERON 30R DUE TO CRACK AND CORROSION FROM STA 8 - 70 PER DC8 SRM 51-1-21, 51-1-20D AND DWG 3648667SDR AWXA0002051Stiffener · crackedD: Pressure web stiffener cracked at BS 727, LBL 17, WL 202C: Removed and replaced stiffener IAW B737 SRM 51-30-2 Pg 8SDR 2001UALA01501Stringer · corrodedBS 434 STR 34R CORRODED.SDR 2001UALA01500Stringer · corrodedBS 434 STR 35R CORRODED.SDR 2001UALA01499Stringer · corrodedBS 434 STR 34R CORRODED.SDR 2001UALA01494Stringer · corrodedBS 434-478 STR 35L CORRODED.SDR 2001UALA01490Stringer · corrodedBS 434-456 STR 34L CORRODED.SDR AWXA0002086Stringer · corrodedD: S-26L STA 727-727A +10 corroded beyond limits.C: S-26L STA 727-727A +10 repaired per SRM 53-10-3 Fig 1 pg 2 and SRM 51-30-2 pg 2 & 8SDR ZW0A0105706Longeron · crackedDURING CHECK-C MAINT IN THE AFT ACCY COMPT THE LONGERON END WAS CRACKED AT STA 1418, LONGERON 2L. REPLACED CRACKED LONGERON PER SRM 53-14-4, FIG 2. REPAIRED WITH SPLICE SECTION PER SRM 53-02, FIG 7. SHIMMED REPAIR PART AS NECESSARY.SDR CALA0100672Stringer · crackedINSPECTION FOUND AN 1/8" CRACK IN STRINGER 4R SPLICE AND STRINGER 6R SPLICE AT STA 907. THE STRINGER SPLICES WERE REMOVED AND NEW STRINGER SPLICES WERE INSTALLED IAW SRM 51-10-02.SDR SWAA012171Stringer · corrodedDURING SCHEDULED D CHECK, FOUND STRINGER 25L CORRODED AT BS 352. REPAIRED STR PER SRM.SDR AWXA0002005Stringer · crackedd: Stringer 24L at STA 525C: Removed damaged area on stringer, Fabricated and installed repair per SRM 53-00-03 fig 201SDR EIA2001237Longeron · corrodedMZJ - FOUND CORROSION ON LONGERON 30 NEAR STATION 290. FABRICATED AND INSTALLED REPAIR STRAP ON LONGERON 30 AT STATION 290 PER ECRA 916-53-033-2. (M)SDR DL72L011217Stringer · corrodedSTRINGER 29L WAS FOUND BADLY CORRODED BETWEEN FS 950E AND FS 980.SDR ZW0A0105506Longeron · crackedDURING CHECK-C MAINT FOUND CRACK IN LONGERON 20L ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20L PER ARA 17776.SDR ZW0A0105505Longeron · crackedDURING CHECK-C MAINT LONGERON 20R HAD TWO CRACKS, ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20R PER ARA 17777.SDR AWXA0002038Intercostal · corrodedD: Pas. Cabin RBL 54 STA 377-420 Intercostal corroded top surface around fastner holes.C: Removed intercostal, Fabbed & Installed Intercostal per SRM 51-40-02 pg 46-47 Fig 12 & SRM 57-30-01 pg 11 step 7SDR C2XA01TY099Stringer · chafedTYS DURING A SCHEDULED INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 2412/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.SDR USAA010928Stringer · corrodedTPA - FOUND STRINGER CORRODED 4 INCHES, STRINGER 26 RIGHT AT STATION 1016. CORROSION LEVEL 2. REPAIRED STRINGER PER SRM 53-00-03 FIG 201. (M)SDR MWEA011087Longeron · damagedLONGERON 6 RIGHT DAMAGED BETWEEN STATION 503 AND 522. BLENDED DAMAGED AND ATTACHED SPLICE PLATE OVER DAMAGE.SDR AWXA0002037Intercostal · crackedD: Intercostal cracked at STA 446 between STR 22L & 23LC: Removed cracked intercostal at STA 446-460, 23L. Installed replacement intercoastal at STA 440-460, 23L IAW SRM 51-40-02 Pg 4SDR IXXA0100068SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 902 BETWEEN LONGERONS LONGERON 21R AND LONGERONS 20R. REPAIR ACCOMPLISHED REOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION REPAIR FILLERS AN EXTERNAL DOUBLERS IN ACCORDANCE WITHSDR AWXA0002062Web · crackedD: Cockpit floor web cracked, BS 180, LBL 22, WL 207 at edge of cut-outC: Removed & replaced cockpit floor web IAW AWA ER #15-5311-01186-SS3 at BS 180, WL 207, LBL 22SDR AWXA0002016Web · crackedD: HFEC Indicates 1.3" crack, BS 178 Bulkhead web, FWD side along strap, WL 226.3 RBL 6.8C: Repaired BS 178 bulkhead web at WL 226.3 RBL 6.8 & 4.9 IAW B737 SRM 53-1011 Pgs 1-7SDR AWXA0002015Web · crackedD: BS 178 Bulkhead web side cracked .200" out of button-head rivet hole, WL .234 RBL 10C: Repaired BS 178 Bulkhead web fwd side WL 234 RBL 10 IAW B737 SRM 53-10-11 Pgs 1-6 Fig 1SDR AWXA0002122Doubler · crackedD: Doubler on floor beam at BS 670 LBL 24 crackedC: Removed and replaced doubler IAW B737 SRM 51-30-5 Pg 5SDR 01FDEA00555Stringer · crackedDURING ROUTINE INSP STR 17L FOUND CRACKED AT BS 456. *S/D* REMOVED AND REPLACED STRINGER PER SRM 53-10-3, 51-30-2.SDR 2001UALA01362Stringer · corrodedSTRINGER CORRODED. STR 6L, STA 767. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE AND REPLACED TIE CLIP.SDR ZW0A0105305Longeron · crackedDURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CRACKS AT STA 160, LONGERON 3L AND 4L. REPAIRED PER SRM 53-02 FIG 18.SDR 2001UALA01356Stringer · corrodedSTRINGER CORRODED. STA 266 STR 22. MAJOR REPAIR ACCOMPLISHED.INSTALLED FILLERS AND STRINGER SPLICE.SDR COOSDR010064Stringer · crackedFUSELAGE STRINGER SECTION 27L FROM BS 960 TO BS 1016, CRACKED.SDR COOSDR010061Stringer · crackedFUSELAGE STRINGER SECTION FROM BS 306 TO BS 326 AT STR 4R, CRACKED.SDR COOSDR010060Stringer · crackedFUSELAGE STRINGER SECTION FROM BS 429 TO BS 450 AT STR 4R, CRACKED.SDR COOSDR010058Stringer · crackedFUSELAGE STRINGER SECTION 9L FROM BS 727A+7 TO BS 727B+12, CRACKED.SDR COOSDR010057Stringer · crackedFUSELAGE STRINGER SECTION 9R FROM BS 755 TO BS 780, CRACKED.SDR COOSDR010056Stringer · crackedUPPER FUSELAGE MAIN CABIN STRINGER 11R AT BS 540, CRACKED.SDR COOSDR010055Stringer · crackedUPPER FUSELAGE MAIN CABIN STRINGER 11L AT BS 540 CRACKED.SDR COOSDR010054Stringer · crackedPAX CABIN, BS 727+9INCHES, STRINGER NR 1 CRACKED.SDR COOSDR010051Stringer · corrodedAFT C/C BAY, STA967, STR 27R CORRODED.SDR AWXA0002027Web · crackedD: BS 178 Bulkhead L/H intercostal web is cracked at WL 209 LBL 27C: removed damaged intercostal web installed new web IAw SRM 51-40-02 & DRW 65-45833SDR AWXA0002026Intercostal · crackedD: BS 178 L/H intercostal is cracked WL 195.7 LBL 27C: Removed and replaced intercostal IAW SRM 53-10-08SDR AWXA0002022Intercostal · crackedD: BS 178 R/H intercostal cracked at WL 195.7 RBL 27C: Removed and replaced intercostal per SRM 53-10-08SDR LR7A01046Stiffener · bentDURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 787E LONGITUDINAL STIFFENERS BENT AT LBL 3.57 AND RBL 3.57, WL 126.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 33.SDR LR7A01045Stiffener · brokenDURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 787E - 797E LONGITUDINAL STIFFENERS BROKEN AT LBL 3.57 AND RBL 3.57, WL 127.75.FABRICATED AND REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-53-10 PG 7 D, 51-70. NR 9, CONT. SDR LR7A01044Stiffener · brokenDURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 797E LONGITUDINAL STIFFENERS BROKEN AT LBL 10 AND RBL 10, WL 127.75.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 41.SDR LR7A01043Stiffener · deformedDURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 777E - 787E LONGITUDINAL STIFFENERS DEFORMED AT LBL 20.95 AND RBL 20.95, WL 127.5.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT. SHEET ITEM 31.SDR LR7A01042Stiffener · deformedDURING POST TAIL STRIKE DAMAGE EVALUATION (REF. OPER CTRL NO. LR7A01033) FOUND FS 787E - 797E LONGITUDINAL STIFFENERS DEFORMED AT LBL 20.95 AND RBL 20.95, WL 127.5 - 128.5.REPLACED LONGINTUDINAL STIFFENERS IAW SRM SMP 583-51-70. NR 9, CONT.SHEET ITEM 42.
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