JASC 5340
Service difficulty reports · 22,407
Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340' 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 = '5340' 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 HNAA2022052500193Attach Bracket · gougedE912960 - CO-PILOT BULKHEAD OTBD UPPER ATTACHMENT BRACKET IS GOUGED .... REMOVED AND INSTALLED NEW SERVICEABLE CO-PILOT BULKHEAD OTBD UPPER ATTACHMENT SHEET BRACKET IAW EMB145 SRM 51-40-02SDR SWAA2022060907002Fastener · shearedFASTENER B IS SHEARED AT B.S. 727B; R.B.L. 24.75. REFERENCE 5340-I-15202-NG. / [01] FASTENER REPLACED ON CARD 22-153-01329 (AD- N477WN- SWA- BS 727B; RBL 45.5 AND RBL 24.75 SEAT TRACK FASTENER REPLACEMENT) TTG8Q00C9GGJ;[02] VERIFIED CORRECTIVE ACTION 1.SDR IPXA2022050981906Seat Track · corrodedINSPECTION TYPE:SEG4MAIN CABIN SEAT TRACK AT STA 1100-1200, LBL 20 HAS CORROSIONREMOVED AND REPLACED SEAT TRACK IAW BOEING DWG 146N5217-1 AND SRM 51-40-02-0GSDR HNAA2022052500204None · noneE913853 - RH OUTBD CARGO FLOOR SILL IS CORRODED JUST FWD OF FR 71 .... REMOVED AND REPLACED RH OUTBD CARGO FLOOR SILL JUST FWD OF FR 71 IAW EMB145 SRM 51-40-02SDR HNAA2022052500203None · noneE913852 - RH OUTBD AFT CARGO CARGO FLOOR SILL IS CORRODED AT FWD END AT FR 71 .... REMOVED AND REPLACED RH OUTBD AFT CARGO FLOOR SILL AT FR 71 IAW EMB145 SRM 51-40-02.SDR SWAA2022051396693Angle · crackedAFT CARGO BAY LAV ENCLOSURE ANGLE IS CRACKED BS 867 LBL 11 WL 164 / [01] REMOVED AFT BAY LAV ENCLOSURE ANGLE BS 867 LBL 11 WL 164 PER SRM 51-40-02-0G-0.;[02] LOCATED; DRILLED; AND DEBURRED NEW ENCLOSURE ANGLE BS 867 LBL WL 164 PER SRM 51-40-05-0G-0; DWG 149A81SDR SWAA2022051296872Attach Angle · crackedINTERCOSTAL UPPER ATTACH ANGLE IS CRACKED STA 380-400; LBL 14; WL 208. / [01] REMOVED; LOCATED HOLES ON NEW ANGLE AND INSTALLED ; INTERCOSTA LUPPER ATTACH ANGLE AT BS 380-400 LBL14 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DRAWING # 143A5400 SHT 182 SDR SWAA2022051296874Attach Angle · crackedINTERCOSTAL UPPER ATTACH ANGLE IS CRACKED STA 380-400; RBL 40; WL 208. / [01] REMOVED; LOCATED HOLES ON NEW ANGLE AND INSTALLED ; INTERCOSTA LUPPER ATTACH ANGLE AT BS 380-400 RBL 40 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DRAWING # 143A5400 SHT 140SDR FDEA202204221028Joint · damagedFWD CARGO FRAME 40 LH HAS FASTENERS WITH DAMAGED INDICATIONS HOLES A, B, AND C. COMPLIED WITH EA 6-5710-127939 PT8: WINGS - BASIC WING STRUCTURE - ALI WORKCARD 5710390-00-11 REPAIRED CRACKED HOLES IN CTR WING JOINT - FR 40 LH / RH. MAJOR REPAIRSDR SWAA2022051196155Attach Angle · crackedB.S 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10; W.L. 163. / [01] VERIFIED THE APPLICABILITY OF SRM 57-10-10-2R-5 REPAIR 5;[02] CUT AND REMOVED THE BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 16 TO RBL 8 WL 163 IAW SRM 57-10-10-2R-5 REPAIR SDR SWAA2022051795792Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 12; W.L. 162. / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5 AND UPDATED MEASUREMENT FIELD[11] INSTALLED BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL9-LBL20 WL162; BOND CHECK GOOD IAW SRM 57-10-SDR SWAA2022042595639Bracket · brokenPANEL 192E LEFT FWD ATTACHING BRACKET BROKEN / [01] R&R PANEL 192E LEFT FWD ATTACHING BRACKET PER REF AMM 53-12-12.SDR SWAA2022042793270Attach Angle · crackedBS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT L.B.L. 12; W.L. 164. REMOVED DAMAGED SECTION OF VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5. INSPECTED ALL INITIAL FASTENER HOLES IN THE REPAIR AREA AND TRIMMED EDGE OF DAMAGE CUTOUT NDT PART 6 51SDR SWAA2022050392653Stanchion · elongatedSUPPORT STANCHION FOR SIDE WALL PANEL FOUND WITH ELONGATED HOLE IN AFT CARGO COMPARTMENT WASTE TANK AREA.. / [01] LOCATED AND DRILLED NEW SUPPORT STANCHION (PO#1766028) FOR SIDE WALL PANEL IN AFT CARGO COMPARTMENT WASTE TANK AREA IAW SRM 51-40-05-0G-0. PART WISDR SWAA2022051090802Bracket · crackedCRACK BRACKET LOCATED ON BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2022-168780 / [01] INSTALLED NEW FITTING AND FASTENERES LOCATED BS947.5 STRINGER 26L IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV - <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] INSTALLED NSDR HNAA2022041300161None · noneE908787 - LH FWD ENGINE PYLON SPAR II YOKE UPPER AFT JO-BOLT HOLE HAS INTERNAL DAMAGE .... REAMED LH FWD ENGINE PYLON UPPER AFT JO-BOLT HOLE TO 1ST OVERSIZE TO REMOVE DAMAGE AND INSTALLED REPAIR BUSHINGS IAW EMBRAER SB145-54-0008 FIGURE 2 STEPS 1-9 AND EO1-54-SDR SWAA2022042189280Support Angle · crackedCRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS691 RBL1. / [01] REMOVED DAMAGED BRACKET AT BS 691 RBL1 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS691 RBL1 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM 51-SDR SWAA2022042189281Support Angle · crackedCRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS692 RBL24. / [01] REMOVED DAMAGED BRACKET AT BS692 RBL 24 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS692 RBL24 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM SDR SWAA2022041488889Channel · abnormalAFT CARGO L/H 'Z' CHANNEL HAS OVER SIZED HOLE AT BS 727C. / [01] REMOVED DAMAGED PART OF L/H 'Z' CHANNEL AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW Z-CHANNEL IAW B 737 SRM 51-40-05-0G-0;[03] VERIFIED STEP 1 AND 2..O.K. TO TREAT AND PRIME..;SDR SWAA2022041988226Bracket · brokenWIRE SUPPORT BRACKET IS BROKEN STA 867; AT STR 3 R/H. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02;STEP 9.;[02] REMOVED WIRE SUPPORT BRACKET BROKEN STA 867;AT STR. 3 RH;IAW SRM 51-40-02.;[03SDR SWAA2022042687032Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-158279 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWINGS 141A1110 REV - AND 141A8380 REV -;[02] REPLACED TIE CLIP LOCATED BSSDR SWAA2022042687043Bracket · brokenBROKEN SUPPORT BRACKET INSULATOR LOCATED BS685 AND BETWEEN STR12R TO STR14R AT PASSENGER CABIN 2(EA) 2022-158318 / [01] REPLACED SUPPORT BRACKET INSULATOR LOCATED BS685 AND BETWEEN STR12R TO STR14R AT PASSENGER CABIN 2(EA) IAW B737-700 SRM 51-10-02; SRM 51-40-SDR YENA2022032400311None · noneDURING HEAVY MAINTENACE, REF AEM NR 2022-123689 CORR LWR DR SILL LH SIDE (SPOT 2); REF AEM NR 2022-123689 FOR ALL WORK ACP PERM RPR PER SRM 51-41-14-300SDR YENA2022032400310None · noneDURING HEAVY MAINTENACE, REF AEM NR 2022-123689 LWR DR SILL CORR LHS (SPOT 3); REF AEM NR 2022-123689 FOR ALL WORK ACP PERM RPR PER SRM 51-41-14-300SDR YENA2022032400309None · noneDURING HEAVY MAINTENACE, SCRATCH EXTERNAL SKIN BTW FR 52 -FR 53 & BTW STR 29L-STR30L LOWER FUSELAGE; REF AEROMAN N/5 2022-123562, PERFORMED PERMANENT REPAIR IAW A321 SRM 53-00-11-300-029 FIGURE 1 SHEET 001, MAJOR REPAIR, SRI ACCOMPLISHED PER FUR A321-53-00320.SDR YENA2022032400308None · noneDURING HEAVY MAINTENACE, REF AEM NR 2022-123689: CORR LWR DOOR SILL LH SIDE (SPOT 1); REF AEM NR 2022-123689 FOR ALL WORK ACP PERM RPR PER SRM 51-41-14-300. (CONSIDERED AS A MAJOR)SDR SWAA2022042090138Panel · elongatedPANEL 193AR HAS SEVERAL HOLE SCREWS ELONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 AR AS PER B 737-700 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 193AR ;AS PER B737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 AND PSDR SWAA2022040486948Attach Angle · crackedCRACK FOUND A/C BAY UPPER ATTACH ANGLE AT BS 663 LBL 8. CUT OUT DAMAGE IAW SRM 57-10-10-2R-5 FIG 202. FABRICATED REPAIR IAW SRM 57-10-10-2R-5. VERIFIED ITEMS 1 & 2. ACCOMPLISHED DVI OF REPAIR AREA & UNDERLYING STRUCTURE IAW SRM 57-10-10-2R-5 REPAIR 5 ITEM SDR CALA2022032300747None · crackedRH FR68 DOOR STOP NO. 1 LOWER IB HOLE NO. 3 HAS CRACK INDICATION IN FRAME LAYER @ 6 OCLOCK DIRECTION ON HAECO LCQ REF 9292086/34 086 AD RELATED SUPPORT TASK. NR GENERATED BY V892444 REPAIR AND REQUIRES REINSPECTION AT 19,700 FC (FH NOT RELEVANT) FIG 001 SHEET SDR CALA2022032100737Stringer · corroded(SDR) AFT CARGO LOWER BILGE. C54-55 STRINGER 44 HAS CORROSION BFM EMPLOYEE V934344. ON OR BEFORE SEP. 10, 2022 PERFORM AN 5341-01032 INSPECTION AS PER PART 2 OF THE LATEST REVISION OF ECRA PERFORMED INTERIM REPAIR OF AFT CARGO LOWER BILGE. C54-55 STRINGER 44 ASDR CALA2022032100736Stop · crackedRH FR68 DOOR STOP NO. 1 LOWER IB HOLE NO. 3 HAS CRACK INDICATION IN FRAME LAYER @ 6 OCLOCK DIRECTION ON HAECO LCQ REF 9292086/34 086 AD RELATED SUPPORT TASK. NR GENERATED BY V892444 REPAIR AND REQUIRES REINSPECTION AT 19,700 FC (FH NOT RELEVANT) FIG 001 SHEET SDR CALA2022032100715Stringer · corroded(SDR) AFT CARGO FR62-63 STRINGER 32R HAS CORROSION COMPLIED W/ EC/RA 5311-02784 NO DEVIATIONS NOTED.ACCOMPLISHED BY EMP#V934344 AT ST BFM AEROSPACE MOBILE. NR#0023443SDR SWAA2022041884239Attach Angle · crackedCRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS692 RBL1 WL207 / [01] REMOVED CRACKED ATTACH ANGLE FROM MID PASSENGER CABIN BS692 RBL1 WL207 IAW SRM 51-40-02-0G-0;[02] FABRICATED; LOCATED AND DRILL ATTACH ANGLE AT MID PASSENGER CABIN AT BS 692 RBL 1 WL 207 MAT.ISDR HNAA2022041300159None · noneE907833 - LEFT-HAND UPPER SEAT TRACK CORRODED BETWEEN FRAME 20 AND 21 .... REMOVED AND REPLACED LEFT-HAND #1 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06SDR LR7A2022031603090Fitting · corrodedDURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH SLOPING LONGERON LOWER END FITTING CORRODED AT FS737, LBL61, WL140. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0120. / PSE#53-50-12, AD 2012-0SDR LR7A2022031603082Strut · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS858 STRUT TUBE WITH DENT AT LBL63, WL210. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-24. NR# 0042. / PSE# 53-50-07, AD 2012-06-09SDR SWAA2022041284264Fitting · elongatedELONGATED HOLE UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN 2022-131780 / [01] REPLACED UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN IAW. B737-700 SRM 51-40-02; DWG # 148A2230 REV. C. SRM 51-10-02 ITEM 9.;[02] STED 1 CORRECTED. <BR>REPLACSDR SWAA2022040683835Panel · crackedCRACK ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR 2022-129778 / [01] TOOL USED CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE: 16-JAN-23;[03] TOOL USED: SCALE P/N:1863T62 SSDR FDEA202203140511Latch · brokenHAZCAN FIRE EXTINGUISHER COMPARTMENT LATCH BROKEN. OIL 14MAR22 15:28 BSL U NO RESTRICTION - ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 26-20-1 LATCH FOR DG FIRE EXTINGUISHERS COMPARTMENT INOP. RE STRICTIVE NEF: N ITEM DEFERRED PESDR SWAA2022041883074Attach Angle · crackedCRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS692 LBL1 WL207. / [01] REMOVED CRACKED ATTACH ANGLE FROM MID PASSENGER CABIN BS692 LBL1 WL207 IAW SRM 51-40-02-0G-0;[02] FABRICATED; LOCATED AND DRILL ATTACH ANGLE AT MID PASSENGER CABIN AT BS 692 LBL 1 WL 207 MAT.SDR SWAA2022032582971Shear Tie · corrodedCORROSION AT SHEAR TIE STA 360; WL 149; BETWEEN STRINGER 27L & 28L / [01] REMOVED SHEAR TIE BETWEEN STR 27L AND STR 28L AT STA 360 AS PER B737-700 SRM 51-40-02-0G-0.;[02] REMOVED CORROSION AT SHEAR TIE AS PER B737-700 SRM51-10-02-0G-0. FOUND OUT OF LIMITS AS PSDR SWAA2022041882856Attach Angle · crackedCRACKED BULKHEAD ATTACH ANGLE AT AFT CARGO BAY BS865 LBL10. MARKED. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED BULKHEAD ATTACH ANGKE CRACKED AT AFT CARGO BAY BS86SDR HNAA2022041300160None · noneE908064 - RIGHT HAND LAVATORY GUSSET CORRODED AT FORWARD AND AFT NUTPLATES AND AT POTABLE WATER OVERFLOW NIPPLE ..... REMOVED AND REPLACED RIGHT HAND LAVATORY GUSSET IAW EMB 145 SRM 51-40-02.SDR CALA2022030900616None · damaged(SUPPORT TASK) AD2018-03-12 WORK TRANSFERRED FROM NR 0023193,002 3192,0023191 FR66 DOOR STOP FITTING HAVE DAMAGE INDICATIONS AT S TOP #''S, HOLE #''S LHS #3, H4 #1, H3 AND RHS #6, H3() (GOUGES) AS PER ECRA 5341-01300. WORK ACCOMPLISHED BY VT MAE PART 2 OF THE SDR CALA2022030700597Fitting · damaged(SUPPORT TASK) AD2018-03-12 WORK TRANSFERRED FROM NR 0023193,002 3192,0023191 FR66 DOOR STOP FITTING HAVE DAMAGE INDICATIONS AT S TOP #''S, HOLE #''S LHS #3, H4 #1, H3 AND RHS #6, H3() (GOUGES) AS PER ECRA 5341-01300. WORK ACCOMPLISHED BY VT MAE PART 2 OF THE SDR AALA202203109944Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON CREASE ANGLE 1.2 IN LENGTH. LOCATION: STA 302.8 AND STR 17L. INSTALLED REPAIR PER SRM 53-10-15-2R-8.SDR SWAA2022032979627Strap · corrodedA22-22; AFT PIT STA 772; BL0; FLOOR SPLICE STRAP; UPPER SURFACE; CORROSION AT 1EA FASTENER HOLE; MRK'D. (SECONDARY STRUCTURE) ATA-53-98 / [01] VERIFIED REPLACEMENT PART AS 149A9401-4; IAW AIPC 53-42-11-26; ITEM # 955. REMOVED AND REPLACED ON A/C IAW AMM 25-52-SDR IPXA2022030279612Web · crackedINSPECTION TYPE:4CL-3 DOOR JAMB WEB/ INNER SKIN IS CRACKED AT STA. 1307 & Z= -18.REPAIRED CRACKED L-3 DOOR JAMB WEB/ INNER SKIN AT STA. 1307 & Z= -18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)SDR HNAA2022022300104Not Reported · not reportedE900513 - FUSELAGE SKIN HAS POSSIBLE CRACK AT FRAME 79 BETWEEN STRINGERS 06R AND 07R MARKED .... REPAIRED FUSELAGE SKIN CRACK AT FRAME 79 BETWEEN STRINGERS 06R AND 07R IAW PIEDMONT EO1-53-22-0025.SDR CALA2022022200479Stringer · corrodedA3NB-53-3-6186 AFT CARGO BILGE AREA FR54 TO FR55 S42L HAVE CORRO SION DOT 42-036 () FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 001 SHT 53-00-13-300-001 FIG 001 SHEET 02. REQUIRES INSPECTIONS PER SRI EMBODIMENT, SUBSEQUENT INSPECTION AND METHOD TBD.
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