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 CALA2021112902183Stringer · corrodedAFT CRG COMPT: FLOOR BILDGE STR38 RH BETWEEN FR58 AND FR59 HAS C ORROSION EVIDENCE. DOT 61-047 (A3NB-53-4-6179) () REPAIR @ STR 38 R/H FR C58-C59 ACCOMPLISHED ON FINAL EA 320-5341 -13-A2728 AND UAL EC/RA 5341-01285. REPAIR CATEGORY A. ACCOMPLIS HED BY EMP#V934SDR CALA2021112902181Stringer · corrodedAFTG CRG COMPT: FLOOR BILDGE STR37 RH BETWEEN FR59 AND FR60 HAS CORROSION EVIDENCE. DOT 61-48 (A3NB-53-4-6179) () REPAIR @ STR 37 R/H FR C59-C60, ACCOMPLISHED ON FINAL EA 320-534 1-13-A2728 AND UAL EC/RA 53-41-01285 REPAIR CATEGORY A. ACCOMPLI SHED BY EMP#V934SDR JJBA20211123037Mount · corrodedRH VERTICAL PARTITION LOWER SILL ATTACH POINT HAS SIGNS OF CORROSION AT FASTENER HOLES. ACCOMPLISHED BEAM FUSELAGE !, FRAME 61 DOUBLER REPAIR AT RH VERTICAL PARTITION LOWER.SDR SWAA2021122745981Flange · crackedFWD LT FUSELAGE FRAME SMALL CRACK AT FLANGE ABOVE L1 DOOR CUTOUT BS 312. REMOVED CRACK IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC INSP. ALONG EDGE OF CUTOUT IAW NDT PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED. LOCATED & DRILLED NEW HOLES ON LAY OUTSDR K11A2021111900093Pad · corrodedJACK PAD FITTING ADAPTER HAS CORROSIONSDR SWAA2021122744253Panel · corrodedDME#1 BASE ON PANEL 192F CORRODED ; / [01] CLEANED AREA AND FOUND OUT LIMITS IN REFERENCE B-737 SRM 53-40-70-1-A-1; [02] ADD REFERENCE B-737 SRM 51-10-02-0G-0; [03] WILL BE ACCOMPLISHED IN ITEM #TTG8Q009DQ95; [04] VERIFIED ACCOMPLISHED IN ITEM #TTG8Q009DQ95SDR SWAA2022010643233Attach Bracket · crackedP-18 ATTACH BRACKET CRACKED BS 273 AT S-8L. 8-91 ; / [01] REMOVED ATTACH BRACKET AT BS 273;S-8L AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED P-18 ATTACH BRACKET IAW. DWG #141A0720; [03] TO CORRECTING STEP # 2 DWG# 141A9502-5; [04] TREATED AND PRIME P-18 SDR SWAA2022010643234Attach Bracket · crackedP-18 ATTACH BRACKET CRACKED BS 273 AT S-10L. 8-92 ; / [01] REMOVED ATTACH BRACKET AT BS 273;S-10L AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED P-18 ATTACH BRACKET IAW. DWG. #141A9502-10; [03] VERIFIED 1-2. OK TO TREAT AND PRIME.; [04] TREATED AND PRIME PSDR SWAA2022011042546Attach Fitting · brokenRT BODY PNL 192BR ATTACH FLANGES HAVE 2 BROKENRECPTICALS IN FWD AREA. 8-81 ; / [01] REMOVED AND REPLACED 2 ATTACHED FLANGES AT RT BODY PNL 192BR IAW SRM 51-40-02-0G-0; [02] VERIFIED STEP 1.SDR SWAA2022011042548Attach Fitting · brokenLT BODY PNL 192BL ATTACH FLANGES HAVE 8 BROKEN RECPTICALS. 8-80 ; / [01] REMOVED RECPTICALS AT LT BODY PNL 192BL ATTACH FLANGES AS PER B737 SRM 51-40-02-0G-0; [02] REMOVED AND REPLACED 8 ATTACHED FLANGES AT LT BODY PNL 192BL IAW SRM 51-40-02-0G-0; [03] VERIFIESDR SWAA2021120241511Stringer Clip · crackedSTRINGER CLIP CRACKED BS 520 STR 26L. REMOVED STRINGER CLIP STR 26L BS 520 PER SRM 51-40-02. INSTALLED STRINGER CLIP IAW DWG 143A1215 REV-, AND SRM 51-40-02.SDR SWIA2022010463393Attach Fitting · corroded*CORROSION ON RH FLOOR BEAM FITTING ATTACHED TO FRAME FS 319.00 AT APPROX LBL36 STGR 18R (C CHECK RO 12-31-21) / REMOVED AND REPLACED FITTING P/N SH670-31990-1 AT FRAME FS319, RBL36 STGR 18R. REF. CRJ900 SRM 51-42-21-001-001-A01 AND DWG # SH670-31950 REV.SDR SWAA2021120741056Access Panel · crackedCRACK ACCESS PANEL 193AR AT FUSELAGE EXTERIOR ; 2021-512088 / [01] TOOL USED CALIPER P/N 500-197-30 S/N A21043164 DUE DATE 01/SEP/22.; [02] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 11-DEC-21.; [03] TOOL USED SCALE P/N SCA-301 S/N AE-412133 SDR SWAA2021120740617Fitting · elongatedSUPPLEMENTAL INFORMATION: ELONGATED HOLE STIFFENER ASSY LOCATED BS 1016 AND BL 0 UPPER POSITION AT PASSENGER CABIN ; 2021-511964 / [01] REPLACED NEW FITTING AND FASTENERS LOCATED BS 1016 AND BL 0 UPPER POSITION AT PASSENGER CABIN I.A.W B737-700 SRM 51-10- 02 ISDR SWAA2021120640495Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT AFT CARGO BAY BS807 RBL15 WL157. THERE IS NO ALLOWABLE DAMAGE FOR ATTACH ANGLE AT AFT CARGO BAY BS807 RBL15. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVE STRINGER CLIP IAW SRM 51-40-02-0G-0. VERIFIED NO ALLSDR SWAA2021120340467Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE IN FWD CARGO BAY BS 500A FWD SIDE LBL 25, WL 155. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED A NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-05 AND DWG 143A7502. INSTALLED THE NEW INTERCOSTAL ATTACSDR CALA2021110302023Stringer · corroded(A3NB-53-4-6179) AFT CRG COMPT: STR41 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE DOT 61-056. IAW SRM 51-42-11/001 AND NDT''D CUT OUT IAW NTM 51-10-08 PART 6. SRM 53-00-13-300-001 FIG 001 SHEET 5 INSTALLED STRINGER REPAIR INSPECTION THRESHOLD FROM TIME OFSDR CALA2021110302025Stringer · corroded(A3NB-53-4-6179) AFT CRG COMPT: STR42 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE. DOT 61-055 IAW SRM 51-42-11/001 AND NDT''D CUT OUT IAW NTM 51-10-08 PART 6. SRM 53-00-13-300-001 FIG 001 SHEET 5. INSTALLED STRINGER REPAIR INSPECTION THRESHOLD FROM TIME OSDR FDEA202111022758Angle · crackedRH WING FILLET FAIRING FRAME (BETWEEN PANELS 152LT/152KT) - CRACK STA. 5-113 BTW L28-L29 FABRICATED AND INSTALLED NEW ANGLE REF DWG# A5A7064.SDR HNAA2021112900585None · noneE888033 - DIAMOND GUSSET AT FR 20 CORRODED .... BLENDED AREA FOUND TO BE NOT ALLOWABLE. RAR RH OMEGA BEAM DIAMOND GUSSET AT FR 20. IAW EMB 145 SRM 53-21-10, SRM 51-40-02SDR HNAA2021112900588None · noneE888039 - LH LOWER #1 SEAT TRACK EMERGENCY STOWAGE ATTACHMENT FEET CORRODED .... REMOVED AND REPLACED L/H LOWER #1 SEAT TRACK EMERGENCY STOWAGE ATTACHMENT FEET IAW EMB 145 AMM 25-26-03.SDR HNAA2021112900591None · noneE888045 - SERVICE DOOR FORWARD SILL CORRODED AROUND GALLEY NUT PLATE HOLE .... PERFORMED BLEND OUT OF DAMAGE ON THE SERVICE DOOR FWD SILL AROUND GALLEY NUT-PLATE HOLE. BLENDED AREAS FOUND TO BE BEYOND ALLOWABLE LIMITS. RAR SERVICE DOOR FWD SILL AROUND GALLEY NSDR HNAA2021112900590None · noneE888043 - SERVICE DOOR CENTER SILL CORRODED AROUND AFT NUT PLATE HOLE ... PREPPED, FABICATED AND INSTALLED FABRICATED INTERNAL DOUBLER FOR SERVICE DOOR CENTER SILL REPAIR AROUND AFT NUT-PLATE HOLE AND APPLIED HYSOL TO AREA IAW EMB 145 SRM 53-21-02RE, ITEM 2, FSDR HNAA2021112900589None · noneE888042 - SERVICE DOOR CENTER SILL CORRODED AROUND FWD NUT PLATE HOLE .... PREPPED, FABRICATED AND INSTALLED FABRICATED INTERNAL DOUBLER FOR SERVICE DOOR CENTER SILL REPAIR AROUND FWD NUT-PLATE HOLE AND APPLIED HYSOL TO AREA IAW EMB 145 SRM 53-21-02RE, ITEM 2,SDR HNAA2021112900587None · noneE888037 - LH LOWER #1 SEAT TRACK CORRODED .... INSTALLED LH #1 LOWER SEAT TRACK IAW EMB 145 AMM 53-01-06SDR HNAA2021112900586None · noneE888036 - LH UPPER #1 SEAT TRACK CORRODED .... REMOVED AND REPLACED LH #1 UPPER SEAT TRACK IAW EMB 145 AMM 53-01-06.SDR HNAA2021112900584None · noneE888031 - OUTBD BRACKET AT FR 23 FLOORBOARD STEP DOWN CORRODED .... PERFORMED BLEND OUT OF DAMAGE ON THE OUTBD BRACKET AT FR23 FLOOR BOARD STEP DOWN. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE OUT OF LIMITS, RAR OUTBD BRACKET AT FR 23 FLOORBOARD STEP DOWN ISDR HNAA2021112900583None · noneE888030 - AFT SERVICE DOOR SILL CORRODED AROUND AT UPPER JOGGLE .... RAR SERVICE DOOR AFT SILL IAW EMB-145 SRM 51-40-02.SDR CALA2021102902002None · corroded(A3NB-53-4-6179) AFT CRG COMPT: FLOOR BILDGE STR41 LH BETWEEN FR 53 AND FR54 HAS CORROSION EVIDENCE. DOT 61-45 FOUND STR41L FR53-54 OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 003. REMOVED AND INSTALLED NEW STRINGER IAW SRM 51-42-11. P/N D5 347042020800 BATCH 0SDR CALA2021102601984Frame · corrodedFR 69-70 BETWEEN STGR 2L-2R HAS SURFACE CORROSION ON FUSELAGE CR OWN SKIN,WHERE (2EA) COAX CABLES PASS THROUGH. BEFORE THE AIRCRAFT REACHES 113,200 TOTAL AIRCRAFT FLIGHT CYCLES ALL WORK ACCOMPLISHED ON HAECO NR 9296415. ACCOMPLISHED INTERIM REPAIR AT FR 69-70 SDR CALA2021102601979None · none(A3NB-53-4-6179) AFT CRG COMPT: FLOOR BILDGE STR41 LH BETWEEN FR 53 AND FR54 HAS CORROSION EVIDENCE. DOT 61-45SDR LR7A2021091102964None · crackedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5313, FOUND FS858 STRUT ATTACHMENT PLATE CRACKED AT RBL60, WL160. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000545166.SDR CALA2021102501965Skin · corrodedFR 69-70 BETWEEN STGR 2L-2R HAS SURFACE CORROSION ON FUSELAGE CR OWN SKIN,WHERE (2EA) COAX CABLES PASS THROUGH. BEFORE THE AIRCRAFT REACHES 113,200 TOTAL AIRCRAFT FLIGHT CYCLES ALL WORK ACCOMPLISHED ON HAECO NR 9296415. ACCOMPLISHED INTERIM REPAIR AT FR 69-70 SDR HNAA2021110900532None · noneE885221 - RH OUTBD CARGO FLOOR SILL IS CORRODED AROUND 2 SCREW HOLES BTW FR 61-64 ... REMOVED AND REPLACED RH OUTBD CARGO FLOOR SILL BTW FR 61-64.IAW EMB145 SRM 51-40-02.SDR HNAA2021110900531None · noneE885218 - RH CARGO OUTBD FLOOR SILL BTW FR 65-68 IS CORRODED AROUND 3 SCREW HOLES. ...REMOVED CORRODED RH CARGO OUTBD FLOOR SILL BTW FR 65-68 POSITIONED,DRILLED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-20-03. 51-40-02.SDR HNAA2021110900530None · noneE885214 - RH CARGO OUTBD FLOOR SILL BTW FR 71-73 IS CORRODED AROUND 3 SCREW HOLES ...REMOVED AND REPLACED RH OUTBD CARGO FLOOR SILL BETWEEN FR 71-73 IAW EMB-145 SRM 51-40-02SDR MASA20220329159None · gougedGOUGES ON FWD/LWR AND AFT/LWR GUIDES FITTINGS AT BOTH FWD AND CENTER CARGO COMPARTMENT DOORS SURROUND STRUCTURES
CORRECTIVE ACTION: DAMAGE WAS REMOVED AND WAS REPAIRED PER CRJ-900 SRM 53-31-23-201-002-A01SDR MASA20220329121None · noneWEAR ON FWD/UP AND AFT/UP ROLLER GUIDES FITTINGS AT BOTH FWD AND CENTER CARGO COMPARTMENT DOORS SURROUND STRUCTURES
CORRECTIVE ACTION: DAMAGE WAS REMOVED AND WAS REPAIRED PER CRJ-900 SRM 53-31-23-201-002-A01SDR FDEA202110122515None · noneWHILE PERFORMING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND TRUNNION FITTING EXISTING TRIMMED OUT AREA FOUND NOSE LANDING GEAR RIGHT HAND TRUNNION SUPPORT FITTING ATTACH LONGERON AT APPROX STATION 595 FOUND CRACK. NOSE LANDING GEAR RIGHT HAND TRSDR SWAA2021111728691Panel · delaminatedPANEL 192BL HAS EDGES DELAMINATED IN TWO SPOTS. REMOVED DAMAGED PLIES & PREPARED THE DAMAGED AREA TO APPLY FABRIC REPAIR PLIES NO WATER NOTE AT ACCESS PANEL 192BL IAW SRM 51-70-04-2R-10 PARAGRAPH 4 B & C. APPLIED FABRIC REPAIR PLIES AT ACCESS PANEL 192BL IAW SDR FDEA202110082564Stiffener · crackedAFT FUSELAGE (TAIL CONE) BULKHEAD, STA Y 2163, LOWEST STIFFENER CRACKED AT RHS OUTBD EDGE. 0004002951 : RODRIGUEZ, HECTOR - 08-NOV-2021 06:52 INSTALLED STIFFENER AND SUPPORT -19 ON LOWER R/H SIDE OUTBOARD EDGE OF AFT FUSELAGE BULKHEAD (TAIL CONE) AT STASDR FDEA202110022443Fitting · corrodedAFT CARGO - RIGHT HAND FITTING AT STATION 1877 LONGERON 43 FOUND CORROSION CORROSION AT AFT CARGO - RIGHT HAND FITTING STATION 1877 LONGERON 43 REMOVED AND FOUND OUT LIMIT AS PER SRM 53-00-00-2R FIGURE 205.CARRIED OUT REPAIR AT STATION 1877 LONGERON 43 RIGSDR SWAA2021112425763Shear Tie · corrodedAFT CARGO BAY SHEAR TIE CORRODED BS 727C; S25L - 26L; WL 149. EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND PRIMED NEW SHEAR TIE IAW DWGS 146A3230, 146A1281 AND SRM 51-40-05SDR SWAA2021112425757Shear Tie · corrodedAFT CARGO BAY SHEAR TIE CORRODED BS 847 S26 - 27L, WL 153. EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED ACB SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND PRIMED IAW DWG 146A3230, 146A1202 AND SRM 51-40-05-0G-0. INSTSDR FDEA202109302470Bracket · corrodedAFT CARGO AT FWD LWR DOOR CUTOUT LWR JAMB BRACKET IS CORRODED BEYOND LIMITS. INSTALLED NEW BRACKET P/N: AGA7226-1 REF MD-11 SRM 51-33-01-OG, AMM 20-50-02-2 TABLE 204, AND DRWG AGA7226. MAJOR REPAIR.SDR SWAA2021102824753Flange · corrodedRT ECS EXHAUST O/B FLANGE HAS FRETTING CORROSION. BLENDED OUT CORROSION AND MEASURED MINIMUM THICKNESS REMAINING. FOUND OUT OF LIMITS IAW SRM 53-40-71-1A-1, FIG 103, DETAIL C; VIEW A-A. ORIGINAL THICKNESS 0.100'; REMOVED 0.019'; REMAINING 0.081'. REMOVED RTSDR SWAA2021102824755Flange · unknownLT ECS EXHAUST O/B FLANGE HAS FRETTING EROSION. INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-0G-0.SDR CALA2021100101736Skin · corrodedRH AIRFONE DOUBLER BETWEEN FR63-FR64 AND STRINGER 41R-42R FOUND CORROSION. UPON FURTHER EVALUATIONS, CORROSION WAS FOUND ON FASTENERS AT PERINATE REPAIR AND NO FURTHER ACTION REQUIRED. REPAIR DOUBLER LOCATED AT FR63-64, STRG40-43. FASTENERS WERE REPLACED IAW SSDR FDEA202109272765Angle · crackedRH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 L39. CRACK CONFIRMED WITH NDT HFEC. REMOVED AND REPLACED FAIRING SUPPORT RIB PER SRM 51-33-01-0G AND DOUGLAS DWG AFA7769SDR FDEA202109272769Angle · crackedRH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 BETWEEN L30-L31. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG 7769.
Back to JASC 5340