JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 SWAA2022051093014Stringer Clip · crackedAT STATION 500I; THE STRINGER CLIP BELOW THE RIGHT HAND TRANSITION ANGLE HAS EVIDENCE OF CRACKS AROUND THE TWO VERTICAL FASTENERS. PICTURE ATTACHED / [01] STRINGER CLIP WAS REMOVED AND REPLACE PER EA-22-153-01161; FAULT CODE TTG8Q00C2DF6.;[02] C/W INSPECTION.SDR SWAA2022042693284None · crackedFWD CARGO COMPARMENT L/H WL 156.4 LBL22 STA 500A Z-CHANNEL CRACKED / [01] CUTOUT DMG SECTION OF THE Z CHANNEL FROM STA 492.5 TO 500D AS PER SRM 51-10-02-0G-0 AND 53-00-53-2R-6 REPAIR 6;[02] REMOVED NUTPLATES IN THE REPAIR AREA AS PER B737-700 SRM 53-00-53-2R-6SDR IPXA2022041357167None · noneRIGHT SIDE FUSELAGE SKIN DENT FORWARD OF THE AFT CARGO DOOR BETWEEN STR. 31R-32R PROVIDED EO-83419-REQ1SDR CALA2022041400957Skin · corroded(B757-06-3-0246) LOWER FUSELAGE SKIN INTERNAL ANTENNA DOUBLER HA S CORROSION IN BULK PIT AT STA 1510 BETWEEN S28L AND 29L (MARKED ). TRANSCRIBED FROM N/R 9284791SDR SWAA2022041992884Angle · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 380 TO BS 400 BL 0 FLOOR STRUCTURE OF PASSENGER CABIN 2022-148402 / [01] REPLACED ANGLE LOC BTW BS 380 TO BS 400 BL0 FLOOR STRUCTURE OF PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG 143A5400; SHEET 38 AND REV A.;[02SDR V0XR20220516AV6Skin · corrodedFUSELAGE SKIN CORRODED AT FRAME 81 BETWEEN STRINGER 21 LEFT AND 21 RIGHT REPAIRED USING AQRD ENGINEERING REPAIR ORDER NO. ERO-971795SDR DALA2022041202575None · noneSHIP 691 DENT ON FUSELAGE SKIN BTW STA 540- 560 BELOW S-26 LH. CORRECTIVE ACTION: SUMMARY OF NRC 00513: DENT ON FUSELAGE SKIN BTW STA 540-560 BELOW S-26 LH WAS REPAIRED PER ER/A 598654-14 REV. ORIG. SECTION I AND PRI 598654-14 REV 0. (2189730)SDR DALA2022041202523None · noneHIDDEN CORROSION IN REF NRC 013: CORROSION ON INTERNAL PRODUCTION DOUBLER BELOW PAN ON AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 00091: LEVEL CORROSION 2, INTERNAL PRODUCTION DOUBLER CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PER PRI 598420-14 SDR DALA2022041102466None · noneSHIP 3259 EVIDENCE OF REWORK SUPPORT STRUCTURE BELLY FAIRING LOCATED FR 47 AND BTW STR 32L TO STR 34L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED SUPPORT STRUCTURE BELLY FAIRING LOCATED FR 47 AND BTW STR 32L TO STR 34L AT LOWER FUSELAGES AS PER A320 SRM 51-SDR CALA2022041100947Skin · crackedFRAM 35 STR 30 LH HOLE #2 HAS CRACK INDICATION IN AFT SKIN LAYER AT 11 AND 5 O''CLOCK DIRECTIONS ON HAECO LCQ REF 9296337/28337 S UPPORT TASK. TO ACCMP INITIAL INSPECTIONS OF THE FR35 STR30LH HOLE#2 IN AFT S BEFORE THE ACFT REACHES 41,126 TOTAL ACFT FC/93,240SDR DALA2024042504705Skin · noneSHIP 3259 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BT W FR 60 TO FR 61 AND STR 43R TO STR 44 LOWER FUSELAGE (REFERENCE DOC N UMBER A CARD 5100-01821-01A. C/A: PERFORMED ULTRASONIC INSPECTION AND EDDY CURRENT INSPECTION ON EXTERSDR R61A2022050500322Access Door · corrodedWASTE WATER ACCESS DOOR CORROSION FOUND. R&R IAW EMB 170 SRM 51-41-02 & 51-43-04.SDR R61A2022050500321Panel · corrodedCFIII WATER ACCESS DOOR FOUND CORROSION ON EXTERNAL SKIN. CFIII WATER ACCESS DOOR WITH CORROSION ON EXTERNAL SKIN REPLACED WITH NEW IAW EMB 170 AMM 20-10-01.SDR SWAA2022050292535Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE(EGPR) SURROUND DOUBLER IS CRACKED AT AFT VERT. MID. FLANGE BS 235.8; WL 190-170. / [01] REMOVED THE INITIAL RUBBING BLOCK & LAMINATED SHIM AS PER B737-7 SRM 51-40-02-0G-0.;[02] TRIMMED OUT DAMAGE AREA OF EGPR SURROUNDING DOUBSDR SWAA2022042992545Gusset · crackedFWD CARGO COMP STA 500D STR 18L GUSSET CRACKED / [01] REMOVED AT FWD CARG0 COMP. STA 500D STR.18L GUSSET PER B 737-700 IN REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET AT FWD CARGO COMPT. STA 500D; STRG. 18L ASSDR DALA2022041202565None · noneSHIP 3356 FWD CARGO DOOR SURROUNDING, FWD SIDE. LOCATION FR20A BETWEEN STRGR 40RH & 41RH. CORRECTIVE ACTION: DAMAGE OUT OF LIMITS OF A330 SRM53-21-11-283-004. DAMAGE ASSESED BY ENGINEERING. REF ER/A 598664-14 FOR WORK PERFORMED. (8865468)SDR DALA2022041202564None · noneSHIP 3356 FWD CARGO DOOR SURROUNDING, AFT SIDE. LOCATION: FR 25A BEWTEEN STRGR 40RH & 41RH. CXORRECTIVE ACTION: DAMAGE OUT OF LIMITS OF A330 SRM 53-21-11-283-004. DAMAGE ASSESED BY ENGINEERING. REF ER/A 598664-14 FOR WORK PERFORMED. (8865469)SDR DALA2022041202530None · none(LOG 2188065) DURING INSPECTION FOUND LIGHTNING STRIKE DAMAGE RH LOWER FUSELAGE BETWEEN STA: 277-285 STG:26R 2" BELLOW AT STA:285. REPAIRED PER B737 SRM 53-00-01 REINSTALLED 2 RIVETS PER B737 SRM 53-00-01-MON TERMINATING AT 50 FH- PER B737 SRM 53-00-01.SDR DALA2022041202529None · none(LOG 2188036) DURING INSPECTION FOUND LIGHTNING STRIKE DAMAGE RH SIDE NOSE WW STA: 259.5 BETWEEN STG:26R-27R. REPAIRED PER B737 SRM 53-00-01 REINSTALLED HI-LOK PER B737 SRM 53-00-01.SDR FDEA202204080896Floorboard · delaminatedMAIN DECK FLOORBOARD PANEL #241AF HAS IMPACT DAMAGE AND SIGN OF DELAMINATION FABRICATED FLOORBOARD REF FEDEX DRAWING SRZ-25-005SDR CALA2022041100941Skin · puncturedFUS SKIN BODY STA 2390 - STA 2412 STRG 34L-38L FOUND PUNCTURE REFER HAECO NON-ROUTINE NO.9480969- ORIGINATED BY EMP V905539 SPEC NO.B777-06-3-7179 PERFORMED BY EMP V907805, FUS SKIN BODY STA2390-STA2412 STR34L- AT 16000FC INTERVALS REFER TO ELB NO.8312145. 38LSDR SWAA2022042992219None · crackedFWD CARGO COMP STA 500C STR 25L CLIP UNDER ZEE CHANNEL CRACKED / [01] REMOVED CLIP AT FWD CARGO CONP STA 500C STR 25L AS PER B-737-7-SRM-51-40-02-0G-0;[02] VERIFIED STEP 1 OK TO INSTALL NEW CLIP;[03] INSTALLED NEW CLIP AT FWD CARGO COMP STA 500 C STR 25L IAW BSDR SWAA2022042992220Gusset · crackedFWD CARGO COMP STA 500D STR 18R GUSSET CRACKED / [01] REMOVED GUSSET AT FWD CARGO COMP STA 500 D ST 18 R IAW B737 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET;[03] INSTALLED NEW GUSSET AT FWD. CARGO COMPT. STA. 500D; S-18R; AS PER B737-7 SRSDR SWAA2022042992252Gusset · crackedCRACK GUSSET LOCATED ON BS500D AND STR19R FWD CARGO COMPARTMENT 2022-194862 / [01] REPLACED GUSSET LOCATED ON BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 143A7902 SHEET 174 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK COMPLETSDR SWAA2022042992253None · crackedCRACK STRINGER 26R LOCATED BS540 AND WL153.5 AT FWD CARGO COMPARTMENT 2022-194866 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-SDR DALA2022041202577Skin · damagedSHIP 691 DTE, ER/A 535372-14 REV. B; FUSELAGE / SKIN / STA. 1554, S-7R / TEAR STRAP / LIGHTNING STRIKE DAMAGE / FASTENER. CORRECTIVE ACTION: REF ERA 535372-14 REV B. (2187582)SDR DALA2022040802419Skin · corrodedSHIP 3101 - CORROSION INTERNAL STRUCTURE SKIN LOCATED BTW FR 30 TO FR 34 AND STR 40R TO ST42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION INTERNAL SKIN FR30 TO FR34 AND BTW STR 40R/42R AT FWD CARGO COMPARTMENT AS PER ER/A 598047.(SDR SWAA2022050391708Baffle · crackedFWD CARGO COMP RH BAFFLE BETWEEN BS500A AND BS500B FOUND CRACKED APPRX RBL 23 / REMOVED DAMAGE BAFFLE AT FWD CARGO RH BS 500A TO BS 500B RBL 23 PER REF B737 SRM 51-40-02-0G-0;RECEIVED NEW BAFFLE PN 143A7510-12; WILL BE MODIFIED PER SRM 53-30-53-2R-1 TO ACCOMMOSDR SWAA2022050391706Baffle · crackedFWD CARGO COMP RH BAFFLE BETWEEN BS500B AND BS500C FOUND CRACKED APPRX RBL 23 / [01] REMOVED RH BAFFLE AT FWD CARGO COMP. STA 500B TO 500C RBL 23 AS PER REF B737-700 SRM 51-40-02-OG-0;[02] RECEIVED ; LOCATED AND DRILLED RH BAFFLE AT FWD CARGO COMP. STA 500B TOSDR SWAA2022050391709Baffle · crackedFWD CARGO COMP LH BAFFLE BETWEEN BS500B AND BS500C FOUND CRACKED APPRX LBL 23 / [01] REMOVED FWD CARGO LH BAFFLE BETWEEN STA 500B AND 500C LBL23 PER REF B737 SRM 51-4-02-0G-0;[02] LOCATED AND DRILLED NEW BAFFLE AT CARGO LH BETWEEN STA 500B AND 500C LBL23 PER RSDR SWAA2022050391710Baffle · crackedFWD CARGO COMP LH BAFFLE BETWEEN BS500C AND BS500D FOUND CRACKED APPRX LBL 23 / [01] REMOVED BAFFLE AT FWD CARGO COMP. STA 500C TO 500D L/H AS PER REF B737-700 SRM 51-40-02-0G-0;[02] RECEIVED NEW BAFFLE ; LOCATED AND DRILLED BAFFLE AT FWD CARGO COMP. STA 500C SDR SWAA2022050391711Baffle · crackedFWD CARGO COMP RH BAFFLE CLIP CRACKED FWD OD BS500B APPROX RBL 23 / [01] REMOVED CLIP AT FWD. CARGO COMP. R/H BAFFLE FWD. BS 500B APPRX RBL 23 AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED CLIP AS PER REF B737-700 SRM 51-40-05-0G-0;[03] VERIFISDR SWAA2022050391707Baffle · crackedFWD CARGO COMP RH BAFFLE CLIP CRACKED FWD OF BS500C APPROX RBL 23 / [01] REMOVED RH BAFFLE CLIP AT FWD CARGO COMP. STA 500C RBL 23 AS PER REF B737-700 SRM 51-40-02-OG-0;[02] RECEIVED ; LOCATED AND DRILLED RH BAFFLE CLIP AT FWD CARGO COMP. STA 500C RBL 23 AS PESDR SWAA2022042991832Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-192805 / [01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV. - . SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS5SDR SWAA2022042991831Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2022-192806 / [01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV.- . SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS50SDR SWAA2022042991833Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR21R FWD CARGO COMPARTMENT 2022-192807 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] RSDR DALA2022041102493None · noneSHIP 698 DENT ON FUSELAGE SKIN STA 1735 BTW STR 24R- 25R. CORRECTIVE ACTION: SUMMARY OF NRC 00070: DENT ON FUSELAGE SKIN STA 1735 BTW STR 24R -25R WAS REPAIR PER ER/A 598575-14 REV. ORIGINAL. (2185316)SDR DALA2022041102491None · noneSHIP 681 LT SIDE FUSELAGE REPAIR AT STA 590 STRINGER L14. CORRECTIVE ACTION: ACCOMPLISHED REPAIRS AT STA 590-661L STR 14 AND STR 19L, IAW B757 SRM 53-30-01-2R REPAIR 2 AND ER/A 512671-14AD REV B SECTION IV. REFERENCE LOG PAGES 1143996 AND 0915957 FOR FOLLOW ONSDR SWAA2022041192085Doubler · crackedDURING HEFC INSPECTION CRACK INDUCTION AT FIRST RIVET ABOVE LOWER AFT BLEND OUT ON EGPR DOUBLER 'MARKED' / [01] REMOVED DAMAGE IAW SRM 53-10-15-2R-4 SECTION 4.C;[02] HFEC ACCOMPLISHED AT TRIMOUT EDGE AND REMOVED FASTENERS COMMON TO SKIN AND INTERIOR STRUCTURE SDR DALA2022040702396None · noneSHIP 3101 - REMOVE EXISTING REPAIR LOC ON FR 62 TO FR 63 BTW STR 40L TO STR 43L ON LOWER FUSELAGE . CORRECTIVE ACTION: INSTALLED NEW REPAIR LOC. ON FR62 TO FR63 BTW STR40L TO STR43L ON LOWER FUSELAGE (1 EA) AS PER A319 SRM 53-00-11(2186086)SDR A6WA202204058162Stiffener · crackedANGLE STIFFENER AT FS 516, ON RH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON RH BL 45.00 IAW ED# AWAC-CRJ 253-01816SDR A6WA202204058163Stiffener · crackedANGLE STIFFENER AT FS 516, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817SDR IPXA2022042281387Skin · damagedINSPECTION TYPE:4CCENTER FUSELAGE LOWER SKIN PANEL HAS EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L .REMOVED, REPAIRED EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L IAW VTSAA EA 011-5340-01-A9535 REV I/R AND UPS EO MD11-5330-83452-A FAA FORM 810SDR DALA2022040602319Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH. SUMMARY OF NRC 00114: CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH WAS REPAIRED PER ER/A 598251-14 REV. ORIGINAL / PRI REV. 0 AND PRI REV. 1, SECTION I: PERMANENT REPAIR. ASSOCIATESDR DALA2022040502307None · noneSHIP 3311 2 EACH SCRATCHES ON AFT FUSLAGE. CORRECTIVE ACTION: LOCATION 6" AFT OF FR 64 AT STR 44L. 1 SCRATCH 2"L X .012 DEPTH. 2ND 1.5"L X .010 DEPTH BLENDED DAMAGE WITHIN LIMITS PER A330 SRM 53-41-11. (7928222)SDR DALA2022040502305None · noneSHIP 3225 CORROSION WAS FOUND ON THE AFT FUSELAGE STRAP. CORRECTIVE ACTION: COMPLIED WITH ERA 597960-14AD. (2183921)SDR DALA2022040502301None · noneSHIP 3225 CRACK WEB AT LEVEL FR 47 AND STR 41L BELLY FAIRING AREA AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597796-14 REV ORIGINAL. (2183764)SDR FDEA202204040827Skin · crackedEMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHT FOUND SKIN CRACK 2.2 INCH. EMPENNAGE -AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHSDR IPXA2022040380790Splice Strap · corrodedINSPECTION TYPE:S-4AFT CARGO SHEAR TIE AND BUTT SPLICE BEAR STRAP AT STA 1400, BETWEEN S-30R AND S-29L HAS CORROSIONREPAIRED IAW UPS EO B757-5330-83317-A AND VT MAE EA 757-5360-27-A2882 REV-SDR VNAA202204039995Floorbeam · corrodedCORROSION ON UPPER FACE OF FLOOR SUPPORT BEAM AT LBL 9 BETWEEN FS. 581.00 AND FS. 597.00 AT PAX CABIN.
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