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 DALA2022060103812Frame · crackedSHIP 3102 - CRACK INDICATION ON FRAME 20 RH SIDE ON DOUBLE JOGGLE AREA IN HOLE 5 AT LEVEL DOOR STOP 7 CRACK DIRECTION 9 O'CLOCK IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION FRAME 20 RH SIDE ON DOUBLE JOGGLE AREA IN HOLE 5 AT LEVEL DOOR SSDR SWAA2022071112443Receptacle · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER LOC AT RECEPTACLE SURROUND CUTOUT AT LOWER FUSELAGE 2022-267900 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X12101V022235; CAL DUE DATE: 03-JUN-22;[02] REPAIRED EXTERNAL GROUND ELECTRICAL POWER LOC ATSDR FDEA202205271308Skin · corrodedEMPENNAGE - AFT FUSELAGE SKIN RIGHT HAND SIDE AT APPROXIMATE STATION 2160 LONGERON 33 RIGHT TO LONGERON 35 RIGHT AREA FOUND CORROSION. EMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE AT APPROXIMATE STATION 2160 LONGERON 33 RIGHT TO LONGERON 35 RIGHT SKIN CORROSIOSDR DALA2022053103731Doubler · damaged(LOG 8646063) PEFORMED FWD FUSE DOUBLER REPAIR. REF SRM 53-00-01-2R #3 TABLE 204.SDR A6WA202205268221Skin · dentedR/H AFT LOWER SKIN IS DENTED AND HAS SCRATCHED ON FS 589 - FS 605 AT S-24R TO S-25R. ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER TO REPAIR AREA ON AIRCRAFT SKIN EXTERIOR IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-1SDR FDEA202205261298None · noneAGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN EXTERIOR STATION 595 TO 615, LONGERON 27 LEFT TO 29 LEFT. EXISTING REPAIR AT FUSELAGE SKIN EXTERIOR STATION 595 TO 615, LONGERON 27 LEFT TO 29 LEFT EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53SDR DALA2022052703702Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN FR3 AND FR4. SKIN REPAIRED IN MSP DURING C CHECK W/REF. TO ERA 582205-14, REV . C, REFERENCE LOG PAGE 5841746. THIS REPAIR SHOULD HAVE BEEN CLASSIFIED AS A MAJOR REPAIR AND THERFORE SDR RECORDABLE. THIS LOG IS TO IDENTIFY IT AS SUSDR SWAA2022072111545Angle · crackedCRACK ANGLE - CLIP LOCATED BS 500B STRINGER 26L FWD CARGO COMPARTMENT 2022-274516 / [01] REPLACED ANGLE - CLIP LOCATED BS 500B STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700-51-10-02 ITEM 9; 51-40-02 AND DRAWING 143A7505 REV.9;[02] REPLACED ANGLE - CLIP LSDR SWAA2022072111546Angle · crackedCRACK ANGLE - CLIP LOCATED BS 500C STRINGER 26R FWD CARGO COMPARTMENT 2022-274517 / [01] REPLACED ANGLE - CLIP LOCATED BS 500C STRINGER 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 ;51-40-02 AND DRW 143A7505 SHEET 5 REV B. SEE INDIVIDUAL SIGNOFSDR SWAA2022072011543Angle · crackedCRACK ANGLE - CLIP LOCATED BS 400 STRINGER 26R FWD CARGO COMPARTMENT 2022-274512 / [01] REPLACED ANGLE - CLIP LOCATED BS 400 STRINGER 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 ;51-40-02 AND DWG 143A7505 SHEET 2 REV B. SEE INDIVIDUAL SIGNOFFSSDR SWAA2022072011541Angle · crackedCRACK ANGLE - CLIP LOCATED BS 400 STRINGER 26L FWD CARGO COMPARTMENT 2022-274513 / [01] REPLACED ANGLE - CLIP LOCATED BS 400 STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SHEET 2 REV B. SEE INDIVIDUAL SING-OFFS BELOW.;[02] REPLASDR AC2A2022060813901Sidewall Panel · crackedR/H LONGERON AT STA5700 HAS CRACK COMING FROM RIVET TO CORNER WEBBING. CORRECTIVE ACTION - REMOVED LOWER 3 ANGLES CUT DAMAGED WEBBING (WALL) . CUT ACCESS PANEL INTO FRONT OF THE DRY BAY REMOVED WALL . FABRICATED INBOARD AND OUTBOARD DOUBLER FOR SPLICE REPAIR SDR CALA2022052701360Fitting · damagedUPON REMOVAL LH FWD KEEL BEAM REINFORCEMENT ANGLE FOUND TO HAVE DAMAGED HOLES AND LH AFT KEEL BEAM REINFORCEMENT ANGLE FOUND TO HAVE DAMAGED HOLES. AT LH KEEL BEAM AFT INTERNAL WEB HOLES L21,L 81,L82,L83,L84,L85 SHOW ELONGATION ON W10 RIB. HOLES L72,L73,L75 ,LSDR SWAA2022070110914Shield · crackedCRACK ON AFT CARGO DOOR CUTOUT SHIELD AT LEVEL BS 492 TO BS 500A AND STRINGER 25R OF FWD CARGO COMPARTMENT 2022-265980 CRACK ON FWD CARGO DOOR CUT OUT SHIELD AT LEVEL BS 492 TO BS 500A AND STR 25R OF FWD CARGO COMPARTMENT / [01] REPLACED SHIELD AND FASTENERS LSDR DALA2022062204361Skin · noneERA 582205-14 REV C SECTION IV ISSUED FOR PERMANENT REPAIR TO LH NOSE SKIN DENT. REF LOGPAGE 5841746FOR ORIGINAL DEFERRAL FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION VI WITHIN 10 DAYS OF SECTION IV COMPLETION AND ACCOMPLISH SECTION VII WITHIN 30 DAYS OF SECTSDR AALA202206069877Access Door · unsecureAIRCRAFT WAS GROUNDED: DURING WALKAROUND FOUND POTABLE WATER SERVICE DOOR MISSING. FOUND DAMAGE TO BELLY PANEL. ACCOMPLISHED TIME LIMITED REPAIR IPER AARD 52-40-12-1. RE-INSPECTION REQUIRED EVERY FLIGHT CYCLE. FINAL RESTORATION TO BE ACCOMPLISHED NO LATER THANSDR AALA202205279877None · noneAIRCRAFT WAS GROUNDED: DURING WALKAROUND FOUND POTABLE WATER SERVICE DOOR MISSING. FOUND DAMAGE TO BELLY PANEL. ACCOMPLISHED TIME LIMITED REPAIR IPER AARD 52-40-12-1. RE-INSPECTION REQUIRED EVERY FLIGHT CYCLE. FINAL RESTORATION TO BE ACCOMPLISHED NO LATER THANSDR DALA2023052304126Unknown · unknownSHIP 5806 ER/A 599502-14 ISSUED TO REPAIR SKIN AND STRINGER HOLE AT S-1, STA 1180+80. CORRECTIVE ACTION: REF ERA 599502-14. (2247472)SDR V0XD202206200101Skin · gougedAFT FUSELAGE SKIN AT F.S 10151.30 AND 1069.75 BETWEEN STGR 21L AND 22L THERE IS A GOUGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR TO THE AFT LOWER FUSELAGE SKIN AT F.S 10151.30 AND 1069.75 BETWEEN STGR 21L AND 22L BY CUTTING OUT DAMAGE FABRICATING AND INSSDR IPXA2022061483109Doubler · gougedINSPECTION TYPE:1CTAILCONE LH PRODUCTION DOUBLER GOUGE AT STA. Y=2165.REPAIRED GOUGED DOUBLER IAW SRM 51-31-01,51-21-02 AND UPS EO MD11-5350-66790-B (MINOR).SDR IPXA2022061483108Doubler · gougedINSPECTION TYPE:1CTAILCONE RH INTERNAL PRODUCTION DOUBLER GOUGE AT STA. Y=2165.REPAIRED GOUGED PRODUCTION DOUBLER IAW SRM 51-31-01,51-21-02 AND UPS EO MD11-5350-66790-B (MINOR).SDR P5CA2022051800122Skin · gougedGOUGE DAMAGE ON IAI MAIN DECK CARGO DOOR SURROUND LOWER SKIN BETWEEN STA 500 AND STRINGER S-26LH (LAP JOINT AREA)(IT WAS REPAIRED BY MXA EO NO. TRE6753493)SDR FDEA202205221275Skin · dentedEXTERIOR FUSELAGE SKIN HAS A PROTRUDING DENT AT APPROX STA 602 APPROX 1.5IN BELOW THE LAP SEAM AT S26L REPAIRED PER FEDEX EA # F-5330-T0368480SDR FDEA202205221274Skin · dentedEXTERIOR FUSELAGE SKIN HAS A PROTRUDING DENT AT APPROX STA 642 APPROX 2IN BELOW THE LAP SEAM AT S26L REPAIRED PER FEDEX EA # F-5330-T0368479SDR SWAA2022070109938Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-265790 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29/SEP/22.;[02] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIRSDR IPXA2022060482801Skin Panel · crackedINSPECTION TYPE:C14CRACK ON FUESLAGE SKIN (P/N:148T3121-2) ON STA 1725.5,NEAR S-7R.REPAIR I.A.W UPS EO B767-5330-83872-A AND BOEING SR 4-5502355762SDR DALA2022052303527None · noneSHIP 3224 CORROSION INTERNAL STRUCTURE LOCATED DOOR OUTFLOW VALVE AREA FR 65 TO FR 66 AT LEVEL STR 28R TO STR 29R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 599398-14 REV ORIGINAL. (2245117)SDR SWAA2022062709647Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN AT: STA 1016+2 TO STA 1016+9; B.L. 0; WL 306.5; STA 1016+2 TO STA 1016+11; LBL 8 TO LBL 13; WL 306; STA 1016+3 TO STA 1016+12; RBL 8 TO RBL 13; WL 306. / [01] REMOVED CORROSION ON FUSELAGE SKIN;[02] VERIFIED SRM 53-00-01-1A-1 ASDR REXA2022062001240Panel · crackedPANEL 443BT SKIN IS CRACKED. REMOVED & REPLACED PANEL SKIN IAW CRJ 900 SRM 51-42-10-001-001-A01 & 51-42-06-001-001-A01.SDR SWAA2022053109740Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H / [01] NOT FOUND ALLOWABLE DAMAGE LIMITS ON FOR FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H IAW SRMSDR SWAA2022053109742Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H / [01] NOT FOUND ALLOWABLE DAMAGE LIMITS ON FOR FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H IAW SRMSDR DALA2022052403548Skin · crackedCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1022 BTW LONG 13RH-14 RH (FUS). SUMMARY OF NRC 00029: FUSELAGE SKIN STA Y=1022 WAS REPAIRED PER PRI 599215-14 REV. 2 AND ER/A 599215-14 REV ORIGINAL SECTION I: PERMANENET REPAIR. ACCOMPLISH REPETITIVE INSPECTION WITHIN EVSDR SWAA2022061409517Threshold Web · crackedFWD CARGO THRESHOLD WEB CRACKED AT FASTENER HOLE. 8-81 / [01] RECEIVED; LOCATED AND DRILLED NEW THRESHOLD WEB AT FWD CARGO AS PER B737-700 SRM 51-40-05-0G-0. INSTALLATION WILL BE ACCOMPLISHED ON MOC TTG8Q004E9LR.;[02] VERIFIED STEP 1;[03] COMPLETESDR CALA2022052001293Floor Support · corrodedFOR ESFR ENTRY PURPOSES ONLY. FLOOR DECK CORRODED AT STA 1714.8 RBL 8-RBL 31. SEE FLEET CYCLE LOG PAGE 9812182 FOR WORK PERFORMED.SDR SWAA2022060809158Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2022-284030 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED <SDR DALA2022052003457Battery Pack · inoperativeER/A 599216-14, FUSELAGE SKIN AT Y=1076 AND Y=1087, L-13R TO L-14R HAS CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. ACCOMPLISH ER/A 599216-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTH INTERVAL AFTER 17MAY22. ASSOCIATED ER/A 1SDR SWAA2022051908682Frame · crackedDURING WALK AROUND INSPECTION; FOUND A CRACK LOCATED ON CENTRAL BOTTOM SIDE OF THE GPU DOOR / [01] REMOVED DAMAGED SECTION OF ELECTRICAL GROUND POWER RECEPTACLE SURROUND PER SRM 53-10-15-2R-4 REPAIR 4.;[02] ACCOMPLISHED AN HIGH FREQUENCY EDDY CURRENT (HFEC) INSDR DALA2022051903434None · noneCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH (FUS). SUMMARY OF NRC 00030: EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH WAS REPAIRED PER ER/A 599216-14 REV. ORIGINAL SECTION L: PERMANENT REPAIR AND PRI 599216-14 RSDR SWAA2022061608759Intercostal · crackedFWD CARGO BAY INTERCOSTAL UNDER FLOOR TO SIDEWALL SUPPORT BS 400-420 RBL 25 IS CRACKED / [01] VERIFIED APPLICABILITY NOT ALLOWABLE DAMAGE PART THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED FWD CARGO BAY INTSDR SWAA2022061308506Shield · corrodedFWD CARGO COMPARTMENT FLOOR AREA STA 500 TO STA 500A; RBL 24; WL 156; SHIELD IS CORRODED. A177-009 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15;[02] EVALUATED ALLOWABLE LIMITS. 040 ORIGINAL 'T' .031 REMAINING .009 LOSS; FOUND OUT OF LIMITSSDR SWAA2022060908522Angle · corrodedFWD CARGO COMPARTMENT FLOOR AREA STA 500D TO STA 500E; RBL 24 WL 156; Z-ANGLE IS CORRODED. A177-015 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM15;[02] EVALUATED ALLOWABLE LIMITS; .040 ORIGINAL 'T' .032 REMAINING .008 LOSS FOUND OUT OF LIMITSSDR SWAA2022060908513Angle · corrodedFWD CARGO COMPARTMENT FLOOR AREA STA 500E TO STA 500F; RBL 24 WL 156; Z-ANGLE IS CORRODED. A177-017 / [01] EVALUATED ALLOWABLE LIMITS OF CORROSION (Z ANGLE) 100% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] VERIFIED STEPS 1 AND 2 ARE COMPLETE;[SDR SWAA2022060908516Angle · corrodedFWD CARGO COMPARTMENT FLOOR AREA STA 500H TO STA 500I; RBL 24 WL 156; Z-ANGLE IS CORRODED. A177-022 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15;[02] EVALUATED ALLOWABLE LIMITS .040 ORIGINAL 'T' .023 REMAINING.017 LOSS FOUND OUT OF LIMITS SDR SWAA2022060908520Angle · corrodedFWD CARGO COMPARTMENT FLOOR AREA STA 500C TO STA 500D; RBL 24 WL 156; Z-ANGLE IS CORRODED. A177-013 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15;[02] EVALUATED ALLOWABLE LIMITS; .040 ORIGINAL 'T' .028 REMAINING .012 LOSS ;FOUND OUT OF LIMISDR SWAA2022060808753Support · crackedCRACK SUPPORT ZEE LOCATED BS500A STR26L AND WL156 AT FWD CARGO COMPARTMENT 2022-284007 / [01] INSTALLED SUPPORT ZEE AND FASTENERS LOC. BS400 AT 500D STR26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG 143A7500 REV A <BR>SEE INDIVSDR ASAA2022051738366Transition Panel · corrodedFWD PIT L/H TRANSITION HAS AREAS OF CORROSION STA 500D TO STA 500I. GROUNDED - YES. FWD PIT L/H TRANSITION CORROSION FOUND OUT OF LIMITS FROM 500D TO 500Z IAW B737-800 SRM 53-30-53-01-2 REPAIRED TRANSITION IAW B737-800 SRM 53-00-53-2R-5.W= 1" O= .040" R= .032 SDR DALA2022052103512None · noneSHIP 671 AMOC, ER/A 501945-14AD REV. A; FUSELAGE / SKIN / STA. 620, S-26L & S-27L / PREVIOUS REPAIR / CORROSION. CORRECTIVE ACTION: REF ERA 501945-14AD REV A. (2237921)SDR DALA2022052103511None · noneSHIP 671 DENT ON FUSELAGE SKIN BTW STA 1500 TO STA 1505 AND BTW S30 AND S29 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00059: DENT ON FUSELAJE SKIN BTW STA 1500 TO STA 1505 AND BTW S30 AND S29 LH AT LOWER FUSELAJE WAS REPAIRED PER PRI 599012-14 RESDR DALA2022052103508None · noneSHIP 671 CORROSION ON REPAIR DOUBLER BTW STA 620 TO STA 630 AND S26 AND S27 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00053: FUSELAGE SKIN BTW STA 620 TO STA 630 AND S26 AND S27 LH WAS REPAIRED PER PRI 501945-14 REV. 0 AND ER/A 501945-14AD REV. (SDR DALA2022052103507None · noneSHIP 666 CORROSION ON ANTENNA PLATE AT AFT CARGO COMPARTMENT, STA. 1510, BTW S-28R AND S-29R. CORRECTIVE ACTION: SUMMARY OF NRC 00224, ANTENNA PLATE AT AFT CARGO COMPARTMENT, STA. 1510, BTW S-28R AND S-29R. WAS REPLACED PER ERA NO. 480021-14 REV.A. (2238159)
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