JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 SWAA2022011861662Panel · elongated193D PANEL HAS 2 ELONGATED FASTENER HOLES. (MARKED) / [01] R&R 193D PANEL PER AMM 53-51-21.SDR SWAA2022011861668Panel · crackedAFT EDGE OF 193D PANEL HAS 8 FASTENER HOLES WITH CRACKS RADIATING FROM FASTENER HOLE ON BACKSIDE OF PANEL ; AFT EDGE OF 193D PANEL HAS 8 FASTENER HOLES WITH CRACKS RADIATING FROM FASTENER HOLE ON ACKSIDE OF PANEL / [01] REMOVED AND REPLACED PANEL 193D PER SRM SDR SWAA2022011861773Panel · crackedRH WING TO BODY FAIRING PANEL NUMBER 195CR BOTTOM TRAILING EDGE CRACKED. ; / [01] REPAIRED PER EA 22-153-00144SDR SWAA2022011861300Panel · elongated193D PANEL HAS THREE ELONGATED HOLES AND ONE AREA OF DAMAGE ON THE INBOARD SURFACE. / [01] INSTALLED PANEL 193D AS REQUIRED REF AMM 53-51-21.SDR SWAA2022011761196Panel · elongated193D PANEL HAS 5 ELONGATED FASTENER HOLES. (MARKED) / [01] PANEL WAS REMOVED AND INSTALLED ON TTG8Q003F0MK. NEW PANEL PROCURED AND RETURNED DAMAGED PANEL TO STOCK ROOM FOR REPAIR ROUTINGSDR SWAA2022011761006Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02SDR DALA2022011400283None · none(LOG 2084980) DURING INSPECTION FOUND WEAR AND ELONGATED HOLES ON CENTER WHEEL-WELL PANEL 193D. REPAIRED PER B737-800 S.R.M. 51-70-05-2R-8 PAR. 4. ON REFERENCE OF B-737-800 S.R.M. 53-40-70-2R-1.SDR SWAA2022020360698Panel · elongatedAFT WING-TO-BODY FAIRING PANEL 194E HAS SEVERAL ELONGATED HOLES. ; / [01] PREPARED DAMAGED AREA; NO WATER NOTE AND FULL THE ELONGATED HOLES WITH LAMINATING RESIN AND CHOPPED FIBERS. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4 AND SRM 51-70-04SDR SWAA2022011360680Panel · elongatedPANEL 193D HAS ELONGATED HOLES ; / [01] INSTALLED NEW 193D PANEL REF AMM 53-51-21-499-804SDR SWAA2022011360681Panel · elongatedPANEL 194E HAS ELONGATED HOLES ; / [01] INSTALLED NEW 194E PANEL REF AMM 53-51-21-499-803-NGSDR SWAA2022011360665Panel · delaminatedWING TO BODY FAIRING PANEL 193B IS DELIMITATED ON CORNER AT HOLE LOCATION 20 TO 21; ALSO FASTENER HOLES ARE ENLARGED AT LOCATIONS 1; 3; 4; 5; 24; 25; 28; 29; 30; 31; 33 AND 34 ; WING TO ODY FAIRING PANEL 193B IS DELIMITATED ON CORNER AT HOLE LOCATION 20 TO 21;SDR SWAA2022011360863Panel · elongatedPANEL 194E HAS SEVERAL OBLONGED HOLES ; ' / [01] INSTALLED NEW PANEL IAW AMM 53-51-21<BR>REF TSR TRACKING # 202200277SDR SWAA2022011360711Panel · elongated193 B PANEL HAS 2 EACH OBLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO BE CHANGED ; 193 B PANEL HAS 2 EACH OLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO E CHANGED / [01] R&R 193 PANEL REF. SRM 51-40-02SDR SWAA2022021460700Plate · elongatedELONGATED HOLE FLOOR STRUCTURE PLATE LOCATED ON BS 847 AT RBBL 17 AT AFT CARGO COMPARTMENT ; 2022-11377 / [01] REPLACED FLOOR STRUCTURE PLATE(STRAP) LOCATED ON BS 847 AT RBBL 17 AT AFT CARGO COMPARTMENT. I.A.W B737-700 SRM 51-40-02 AND DRAWING 146A8120 REV?; [SDR SWAA2022021460583Track · crackedCRACK TRACK RBBL 13.80 LOCATED ON BS 727E AT AFT CARGO COMPARTMENT ; 2022-11372 / [01] TOOL USED: ELECTRONIC CALIPER; P/N: 500-196-30; S/N: A21033416; DUE DATE: 07-OCT-22.; [02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 05-MAR-22.; [SDR SWAA2022021460582Bracket · crackedCRACK BRACKET LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT ; 2022-11374 / [01] REPLACED BRACKET AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9; SEE INDIVIDUAL SINGOFFS BELOW.SDR SWAA2022011360660Panel · delaminatedWING TO BODY PANEL 193D HAS 7(EA) DISCREPANT FASTENER HOLES: SIX DELAMINATED AND ONE DELAMINATED AND ELONGATED (MARKED). ; / [01] INSTALLED NEW 193D PANEL IAW AMM 53-51-21. ORDERED PANEL UNDER REFERENCE TTG8Q001XKXNSDR DALA2022011200239None · noneTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN TO LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52SDR SWAA2022021162777Panel · crackedPANEL 194CL AFT UPPER THE COMPOSITE IS CRACK (228-001) ; PANEL 194CL AFT PPER THE COMPOSITE IS CRACK (228-001) / [01] MEASUREMENTS; [02] PREPARED DAMAGED AREA AT PANEL #194CL AS PER B737 SRM 51-70-04-2R-1 AND 53-60-70-2R-1; [03] VERIFIED 1;AND 2 COMPLETE;OK TOSDR SWAA2022011359742Panel · elongated193D PANEL FRETTING WEAR. ; FRETTING WEAR AND DAMAGEDELONGATED FASTENERS HOLES ALONG TRAILING EDGE OF 193D PANEL. / [01] INSTALLED NEW PANEL (193D). REFERENCE AMM 53-51-21SDR SWAA2022011259741None · cracked193D STRUCTURE STA 727. ; SPPORT STRCTRE T-CAP CRACKED STA 727 PANEL 193D RIGHT SIDE; FORWARD END OF WEING. / [01] C/W; [02] REMOVED AND REPLACED TEE CLIP 149A7678-8; [03] C/W; [04] C/WSDR SWAA2022021459613Panel · elongatedELONGATED HOLE ACCESS PANEL 431AT BRAKET LOCATED AFT POSITION INTERNAL AREA AT LT PYLON (2 EA) ; 2022-11270. / [01] REPLACED 2 E/A BRACKET LOCATED AFT POSITION INTERNAL AREA ON ACCESS PANEL 431AT IAW B737-700 SRM 51-40-02.; [02] REPLACED 2 E/A BRACKET LOCATED SDR SWAA2022020860323Panel · delaminatedFAIRING PANEL 193AR HAS 2EA DELAMINATIONS ON OUTER SURFACE (MARKED) ; / [01] PART/MATERIAL IDENTIFIED PER SRM 53-40-70-0I-1 FIGURE 2 TABLE 2 ITEM 18.<BR><BR>2 EA DELAMINATION'S OUTER SURFACE EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-40-70-1A-1 PARA 4 A .<SDR SWAA2022020359926Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 193D HAS 1 EACH SCREW HOLE CRACKED AT AFT END OF PANEL. PER GENERATING DOC REPAIR PER SRM 53-40-70. SIGN OFF STEP 18 OF GENERATING DOC AFTER REPAIR (SEQ 168) 8-26 ; / [01] MEASUREMENTS; [02] PERFORMED TAP TEST ON PANEL #193D ON SDR SWAA2022020359925Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 194E HAS 5 EACH SCREW HOLES CRACKED AT FWD END OF PANEL. PER GENERATING DOC REPAIR PER SRM 53-60-70. SIGN OF STEP 9 OF GENERATING DOC AFTER REPAIR (SEQ 168) ; DOT 8-25 / [01] MEASUREMENTS; [02] PERFORMED TAP TEST ON PANEL #194E SDR SWAA2022012759251Panel · elongatedSUPPLEMENTAL INFORMATION: PANEL 194E FWD EDGE; MIDDLE FASTENER HOLE SHOWS EVIDENCE OF STRESS CRACKS ; / [01] MEASURMENTS; [02] PERFORMED TAP TEST ON PANEL #194E AND FOUND NO WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL; ONLY DAMAGED FASTNER HOLE AS PER B737 NDSDR SWAA2022020259253Panel · delaminatedPANEL 195CL IS DELAMINATED ON OUTER SURFACE; 20' FROM UPPER EDGE; 9.5' FROM AFT EDGE. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4A(6C). REMOVED DAMAGE, PREPARED AREA, & CLEANED IAW SRM 51-70-05-2R-2 PARA 4A-C. FABRICATED REPAIR PSDR DALA2022011000159None · none(LOG 2077526) DURING INSPECTION FOUND DAMAGED FASTENER HOLES BS 727 + 2.7( 7 EAS) ON AFT SECTION SUPPORT STRUCTURE OF PANEL WHEEL WELL 193D AT FUSELAGE FAIRING BODY. FASTENER HOLES BS 727 + 2.7( 7 EAS) ON AFT SECTION SUPPORT STRUCTURE OF PANEL WHEEL WELL 193D SDR SWAA2022010658875Panel · damagedAFT WING-TO-BODY FAIRING PANEL 194E HAS MULTIPLE ELONGATED FASTENER HOLES. ; / [01] REMOVED AND REPLACED 194E PANEL IAW EO 5351-I-14642-NGSDR SWAA2022021157989Access Panel · elongatedELONGATED HOLE ACCESS PANEL 194BR AT LOWER FUSELAGE ; 2021-576315 / [01] HOT BONDER P/N:HCS9000B; S/N: 18175469; DUE DATE: 05-AUG-22.; [02] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 31980129 ; DUE DATE: 11-DEC-22; [03] TOOL USED CALIPER PN:500-464; SN: 15331SDR SWAA2022013157604Panel · crackedPANEL 194BL CORNER IS CRACKED AND BROKEN ; / [01] EVALUATED DAMAGE; PANEL CORNER IS REPAIRABLE IAW B737 SRM 53-60-70-2R-1 TABLE 203.<BR><BR>REMOVED DAMAGE; CLEANED AND PREPPED REPAIR AREA. BONDED REPAIR PLIES IAW B737 SRM 51-70-05-2R-10 REPAIR 10 PAR 4 STEPS ASDR SWAA2022020257538Fairing · crackedFAIRING PANEL 195CL AFT CORNER CRACKED AT RADIUS ; / [01] CRACK ON AFT CORNER AT RADIUS OF PANEL 195CL IS BEING REPAIRED ON FAULT TTG8Q009VQLV; [02] VERIFIEDSDR IPXA2022012678311Beam · chafedINSPECTION TYPE:3CTAIL CONE HORZ. BEAM REPAIR DOUBLER HAS CHAFE DAMAGE.REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-00-00 REPAIR 1, FIG. 201. (MINOR)SDR DALA2022010300032None · none(LOG 2071882) DURING INSPECTION FOUND WEAR AND CORROSION ON FASTENER HOLES WHERE NUT PLATE WERE REMOVED AT WING TO BODY FAIRING SUPPORT BS 727+2.7". WING TO BODY FAIRING SUPPORT BS 727+2.7" WERE REPAIRED PER ETI-37-21-541 REV.2 AND ERA 596387-14 REV. ORIGINAL.SDR SWAA2022012456256Fairing · delaminatedSUPPLEMENTAL INFORMATION: FAIRING 195CL HAS DELAMINATIONS OVER CORE AREA NEXT TO EDGEBAND OF PANEL SEE FAULT TTG8Q009PY4M. ; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 5. <BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-SDR SWAA2022021055433Panel · delaminatedSUPPLEMENTAL INFORMATION: INNER LIMNER MATERIAL SHOWS EVIDENCE OF DELAMINATION & OVER (0% OF MATERIAL DETERIORATION ; INNER LIMNER MATERIAL SHOWS EVIDENCE OF DELAMINATION & OVER 90% OF MATERIAL DETERIORATION PANEL 441DR / [01] REMOVED AND REPLACED ALUMINIUM FOSDR SWAA2022021054777Panel · elongatedSUPPLEMENTAL INFORMATION: LOWER FUSELAGE PANEL 193D HAS 2 HOLE ELONGATED. (WORK WITH N/R TTG8Q009W5HD) ; / [01] PREPARED THE DAMAGED FASTENERS HOLES AND FILLED THE HOLE WITH RESIN AND CHOPPED FIBERS; MADE THE SURFACE CONTOUR OF THE REPAIR EQUAL TO INITIAL SURFSDR FDEA202112203107Panel · delaminatedWING TO BODY PANEL 195EL IS DELAMINATED ON THE EDGE REPAIRED PER B757 SRM 53-00-70-2R-1 AND 53-60-70-2RSDR DALA2021122007876None · noneSHIP 3248 ELONGATED HOLE OFFWING ESCAPE SLIDE BELLY FAIRING CHANNEL LEFT SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED OFFWING SCAPE SLIDE BELLY FAIRING CHANNEL PER SRM A320 51-72-11. (2056752)SDR DALA2021122007875None · noneSHIP 3248 WEAR ON OFFWING SCAPE SLIDE BELLY FAIRING CHANNEL RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED OFFWING SCAPE SLIDE PER SRM A320 51-72-11. (2056746)SDR SWAA2022020254173Fairing · crackedFAIRING 195CL RADIUS IS CRACKED AT AFT EDGE. DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101, PARA 4.B. REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 53-40-70-2R-1 PARA 4.B(2) AND 4.D(1); TABLE 202. VALIDATED REPAIR PER SRM 51-SDR UIEA2021121402451Door · none# 2 ENG. STRUT I/B SERVICE PANEL HAS LATCH DON'T CLOSE PROPERLY .(<P>REMOVED & REPLACED DAMAGED LATCH AT #2 ENG STRUT I/B FAIRING ACCESS DOOR IAW B767-300</P> / <P>AMM 54-53-02.</P>)SDR SWAA2021122053486Panel · elongatedSUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES. ; / [01] TRIMMED; DRILLED; AND PAINTED NEW PNL; [02] REMOVED & REPLACED PANEL PER AMM 53-51-21SDR SWAA2021122053240Panel · elongatedSUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E FASTENER HOLES ELONGATED. ; / [01] FABRICATED AND PAINTED NEW PANEL PER EA 5351-I-14642-NG AND AMM 53-51-21; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21SDR SWAA2021122053205Panel · elongatedCENTER WHEEL WELL PANEL 193D FASTENER HOLES ELONGATED. ; / [01] TRIMMED; DRILLED AND PAINTED NEW PNL; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21SDR SWAA2021122053210Panel · delaminated193D PANEL NEEDS TO BE REPLACED DUE TO IT BEING DELAMINATED ; 193D PANEL NEEDS TO E REPLACED DE TO DELAMINATED / [01] REMOVED AND REPLACED PANEL REF. B737 AMM 53-51-21 .SDR SWAA2021122053242Panel · delaminatedCENTER WHEEL WELL PANEL 193D DELAMINATED AND HOLES ELONGATED. ; / [01] FABRICATED AND PAINTED NEW 193D PANEL IAW AD 5351-I-14642-NG AND 53-51-21; [02] REMOVED & REPLACE PANEL PER AMM 53-51-21SDR SWAA2022011253148Fairing · delaminatedFUSELAGE FAIRING 192BR; L/E HAS EROSION WITH DELAM. DOT A034-06 ; / [01] EVALUATED AND FOUND 2 EACH AREAS OF DELAM ON L/E AND BOTH ARE REPAIRABLE IAW SRM 53-40-70-2R-1 TABLE 202 AND SRM 51-70-04<BR>REMOVED DAMAGED PLIES; CLEANED AND PREPPED AREAS FOR REPAIR IASDR SWAA2022011253159Fairing · delaminatedFUSELAGE FAIRING 192BL; L/E HAS EROSION WITH DELAM. DOT A034-08 ; / [01] EVALUATED AND FOUND DAMAGE TO EDGE TO BE REPAIRABLE IAW SRM 53-40-70-1A-1 PARAGRAPH 4B(8) AND FIGURE 105. <BR>CLEANED; PREPPED AND APPLIED SEALER RESIN TO AREA; CURED 2 HOURS AT 125 DEGRESDR SWAA2022011253398Fairing · delaminatedUPPER AFT CORNER OF FAIRING 191AL DELAMINATED. ; / [01] EVALUATED AND FOUND EDGE DELAMINATION AND IS REPAIRABLE IAW SRM 53-30-70-2R-1 TABLE 202 AND SRM 51-70-04<BR>CLEANED; PREPPED AND RESIN INJECTION REPAIR IAW SRM 51-70-04-2R-13 REPAIR 13 PARAGRAPH 4A-H. TAP
Back to JASC 5350