JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320' 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 = '5320' 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 HNAA20240900838Floor Support · corrodedE051424 LH CABIN OMEGA BEAM #2 GUSSETT IS CORRODED. RAR THE LH CABIN OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.SDR SWAA2024091828988Transition Panel · corrodedAFT CARGO COMPARTMENT LEFT SIDE FROM STA 727F TO STA 807 TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES.DOT#G166<[01] REMOVED CORROSION AT STA. 727F TO 747 ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037; WITHIN LIMITS IAW B737-800 SRM 53-00-53; TOOL#SDR SWAA2024091838984Transition Panel · corrodedAFT CARGO COMPARTMENT LEFT SIDE FROM STA 727F TO STA 807 TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES.DOT#G166<[01] REMOVED CORROSION AT STA. 727F TO 747 ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037; WITHIN LIMITS IAW B737-800 SRM 53-00-53; TOOL#SDR SWAA2024091830977Transition Panel · corrodedFWD PIT; TRANSITION PANEL CORRODED ON UPPER SURFACE APPROX. RBL-24 BETWEEN BS 500 AND 500A. MARKED<[01] REMOVED AND REPLACED SIDE PLATE SHIELD IAW B737-800 SRM 52-40-02 AND BOEING DWG 143A0080 AND DWG 143A8126;[02] REMOVED AND REPLACED SIDE PLATE SHIELD IAW B7SDR SWAA2024091828990Shield · corrodedAFT CARGO COMPARTMENT RIGHT SIDE TRANSITIONAL PANEL FROM STA767 TO 807 HAS CORROSION AT MULTIPLE PLACES. DOT#G164.<[01] REMOVED CORROSION ORIGINAL THICKNESS .050 REMOVED .006 REMAINING .044 OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. NEW SHEILD INSTALLATION SDR SWAA2024091828994Channel · crackedFWD PIT R/H SIDE; CHANNEL CRACKED AT BS 500H AT STRINGER S-26R. MARKED<[01] REMOVED AND REPLACED CLIP PART NUMBER 143A7502-154 @ FWD PIT R/H SIDE; CHANNEL AT BS 500H AT STRINGER S-26R IAW 7373-800 SRM 51-40-02 AND IAW B737-800 DWG. 14A7505 REV:-;[02] REMOVED ASDR SWAA2024091828991Transition Panel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE FROM STA 767 TO STA 727F TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES. DOT#G165.<[01] REMOVED CORROSION AT STA. 727F TO 727J ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037 IN LIMITS IAW B737-800 SRM 53-00-53 TOOL#T8SDR SWAA2024091828999Angle · crackedFWD PIT; ANGLE CRACKED AT BS 500G AT STRINGER S-26L. MARKED<[01] REMOVED AND REPLACED ANGLE IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7505;[02] REMOVED AND REPLACED ANGLE IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7505. VERIFIED ALL STEPS COMPLETE.SDR SWAA2024091829002Shield · corrodedAFT CARGO COMPARTMENT; CARGO DOOR CUTOUT FORWARD SHIELD CORRODED. UPPER AND LOWER SURFACES.<[01] REMOVED AND REPLACED SHEILD PT. #146A8127U12; IAW BAC. DWG. 146A0081 B737-800 SRM 51-40-02;51-05-02.;[02] CORRECTIVE ACTION CORRECTION: REMOVED AND REPLACED SHEILDSDR AALA202409175829Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23L BETWEEN FR 69 AND FR 70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-72-11-911-001.SDR U2RA2024090800044Web · scratchedREF HAECO XMN (TX9Y778Y) NRC#: KUL9399 - FWD CARGO COMPARTMENT, STA 660-680 RBL 33-55, MULTIPLE SCRATCHES ON EXISTING REPAIR DOUBLER UPPER SURFACE OF LATERAL BEAM WEB.SDR AALA202409037566Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11.SDR CALA2024082802306Angle · corrodedCORROSION FOUND ON ALC INTERCOSTAL UPPER CHORD UNDER TRANSITION PANEL STA 1540-1560 STR 27L. FOUND ON AGING AIRCRAFT INSPECTION. REF AMES NR 172653-0100-0248 SEE PARTIAL WORK SHEET #144 PAGE 1OF1 REPLACED UPPER CHORD INTERCOSTAL P/N 146N545OU17 BATCH RC-1025 0SDR AALA202408270208Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FOUND FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 537.45, FROM BL 0 TO LBL 24. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02-0G.SDR DALA2024082608426Tie Down · corroded(LOG 0518102) CORROSION AROUND FLOOR TIE DOWN AT STA 947 RBL 26 WL 208. REMOVED CORROSION ON STA 947 FROM LBL 40 TO RBL 60 WL 208. REPAIRED AND INSTALLED NEW -1 TEE CHORD, -2 ANGLE, -3 STRAPS AND -4 FILLERS ALL IAW. B737-900 SRM 53-70-51-2R-5.SDR DALA2024082308406Tie Down · corroded(LOG 0516144) CORROSION AROUND FLOOR TIE DOWN AT STA 947 RBL 49 WL 208. REMOVED AND REPAIRED CORROSION (DAMAGE) AROUND FLOOR TIE DOWN STA 947 RBL 49 WL 208, WITH REMOVAL AND REPLACING INTERCOSTAL FROM STA 947 TO STA 967 RBL 49 WL 208. IAW B737-900 SRM 51-40-02SDR DALA2024082308405Tie Down · corroded(LOG 0516136) CORROSION AROUND FLOOR TIE DOWN AT STA 947 LBL 26 WL 208. REMOVED AND REPAIRED CORROSION (DAMAGE) AROUND FLOOR TIE DOWN AT STA 947 LBL 26 WL 208, WITH REMOVAL AND REPLACING INTERCOSTAL FROM STA 947 TO 967, LBL 26 WL 208 IAW B737-900 SRM 51-40-02-SDR CALA2024082302257Floor Support · corrodedGEN ITEM: GENERATING ITEM SUPPORT TASK: UPPER CABIN FLOOR PANEL SUPPORT HAS CORROSION UPPER SURFACE BETWEEN STA 319-321 RBL 39-41. (CUSTOMER FOUND ITEM)SDR DALA2024082208364Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM. 53-00-55-2R PROCEDURE 4 FIG. 205. (LP 0514941)SDR DALA2024082208363Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. FIGURE 210. (LP 0514913)SDR DALA2024082208362Pan · crackedAIRCRAFT 9550, INITIAL INSPECTION: CRACK ON INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. WAS REPAIRED PER PRI 619298-14 REV.SDR DALA2024082208360Pan · crackedAIRCRAFT 9527, INITIAL INSPECTION: CRACK ON LH RING PAN (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/UPPER) STA Y=851, (FWD/LOWER) STA Y= 851, (FWD/LOWER) STA Y=870, (FWD/LOWER) STA Y=908, (FWD/LOWER) STA Y=927, (FWD/UPPER/LOWER) STA Y= 946 AT CABIN PAXSDR DALA2024082208359Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 210. (LP 0514363)SDR DALA2024082208358Pan · crackedAIRCRAFT 9550, CRACK INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. CORRECTIVE ACTION: INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. WAS REPAIRED PER PRI 619304-14 REV. 3 AND ERA 619304-14 REV ORIGINAL SECTION I PERMANENT REPAIR ASSOCIATED ER/A 14-6SDR SWIA202411120820Floor Support · corrodedRH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED CLOSED)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHINSDR SWIA20241029820Floor Support · corrodedRH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED OPEN)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHIN LSDR SWAA2024100228390Sill Drain · corrodedAFT FLOOR STRUCTURE - MULTIPLE SPOTS CORROSION ON R/H MOP SILL BS 947+17.5 RBL 53/BS 967+5; BS 967+6.5; BS 967+13; BS 967+14 RBL 49; BS 967+7; BS 967+17.5 RBL 51/ BS 987+2.5; BS 987+5; BS 987+10.5 RBL<[01] REMOVED CORROSION ON ASD AT MULTIPLE SPOTS CORROSION OSDR SWAA2024100228401Sill Drain · corrodedAFT FLOOR STRUCTURE - MULTIPLE SPOTS CORROSION ON L/H MOP SILL BS 947+5.5; BS 947+7.5; BS 947+12; BS 947+17.5; LBL 51 WL<[01] REMOVED AND REPLACED MOP SILL AT BS907 - BS1006; LBL50; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG: 147A8501 REV: B.;[02] VERIFIED COSDR SWAA2024100228402Sill Drain · corrodedAFT FLOOR STRUCTURE - MULTIPLE SPOTS CORROSION ON L/H MOP SILL BS 967+2.5; BS 967+6.5; BS 967+8.25; BS 967+10; BS 967+14; BS 967+17.5 LBL 49 WL 208 (MARKED)<[01] AED MOP SILL WILL BE REPAIRED ON CUST CARD TTG8Q00VCLUM;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASDR SWAA2024100228403Sill Drain · corrodedAFT FLOOR STRUCTURE - MULTIPLE SPOTS CORROSION ON L/H MOP SILL BS 987; BS 9687+3; LBL 47 / BS 992.8 LBL 45 WL 208 (MARKED)<[01] AED MOP SILL WILL BE REPAIRED ON CUST CARD TTG8Q00VCLUM;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2024100128398Stiffener · crackedPAX CABIN FLOOR STRUCTURE STIFFENER CRACKED; STA540; WL208; LBL 3. (MARKED)<[01] RAMOVED AND REPLACED CRACKED FLOOR STRUCTURE STIFFENER AT STA540; WL208; LBL 3 IAW SRM 51-40-02 AND DWG 143A0060 ST 46.;[02] RAMOVED AND REPLACED CRACKED FLOOR STRUCTURE STIFFENERSDR SWAA2024100128406Stiffener · crackedPAX CABIN FLOOR STRUCTURE STIFFENER CRACKED; STA540; WL208; RBL 3. (MARKED)<[01] REMOVED AND REPLACED FLOOR STRUCTURE STIFFENER AT STA540; WL208; RBL 3 IAW SRM 51-40-02; DWG 143A0060 SH 46; AND DWG 143A5240 SH 14.;[02] REMOVED AND REPLACED FLOOR STRUCTURE STIFSDR AALA202409251622Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 400 TO STA 500, LBL 25. REPAIRED TRANSITION PANEL PER AARD 51-00-05-1 AND SRM 53-00-53-2R.SDR SWAA2024092428147Support Angle · crackedCRACK ANGLE - SUPPORT BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT 2024-512502<[01] REPLACED ANGLE LOCATED BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN SDR SWAA2024092428148Support Angle · crackedCRACK ANGLE - SUPPORT BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT 2024-512503<[01] REPLACED SUPPORT ANGLE LOCATED BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B.;[02] CORRECTSDR IXXA2024092003Electrical Box · damagedBONDING JUMPER STUD PULLED THROUGH P31 PANEL BOX BACK PANELSDR IPXA2024091167271Support · gougedWHILE WORKING CORROSION ON RCB WALL FOUND LIGHT SURFACE CORROSION ON TOP OF FLOOR STRUCTURE FROM STA. 320 TO 380 LBL 69" TO RBL 69". MARKED 4-030 ,ATA 53 SKILL STR. ACCOMPLISHED VT-SAA EA 757-5300-01-BO267 IR AND E0-91223-REQ1. REPOSITIONED CENTER AIR DUCT UNDSDR AALA202409098926Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500A TO STA 500I, RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR CALA2024090402375Intercostal · crackedF/S 681 STR 12L INTERCOSTAL CRACKED O/B RADIUS, TAG 35262. REF AMES NR 172653-0200-0115 REPLACED INTERCOASTAL IAW B757-200 SRM 51-40-02 AND 51-40-05 ESFR 1037121SDR CALA2024090302358Structure · corrodedSUPPORT TASK - AFT OF BULK CARGO STA 1562 BTN S39L AND S39R FAIL SHORD CHORD CORROSION CRACK AT HOLE FND AFTER SHEAR TIE REMOVED. TRANSFER REFER NON-ROUTINE WO.3616838 AND ORIGINATOR V896820 AFT OF BULK CGO STA1562 BTW STR39L AND 39R FAIL SAFE CHORD WORK ACCOMSDR YENA2024082601160Support Angle · brokenDURING HEAVY MAINTENANCE: BROKEN SUPPORT ANGLE LOCATED FRAME 69 AT LEVEL OF STRINGER 24L AT AFT GALLEY AREA; (RESOLVED ON W/O: 1310500 TASKCARD: NR-00011 ) REF AEROMAN W.O. 2024 131/1 NR 336930 - REMOVED AND REPLACED SUPPORT ANGLE LOCATED FRAME 69 AT LEVEL OFSDR YENA2024082601151Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL IN BULK CARGO COMPARTMENT (CPCP FINDING ); (RESOLVED ON W/O: 1310500 TASKCARD: NR-00015 ) REF AEROMAN WO 2024 131/1 NR 2024-336703, PERFORMED PERMANENT REPAIR LOC. ON LOWER SILL FR 61 PLUS 19 IN AT BULK CARGO IAWSDR CALA2024082602270Intercostal · crackedSTR 12R INTERCOSTAL CRACKED O/B RADIUS. REMOVED AND REPLACED THE INTERCOASTAL BS 681 STR 12R IAW SRM 51-40-02 AND B757-200 SRM 51-40-05.SDR YENA2024082201146Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL IN BULK CARGO COMPARTMENT (CPCP FINDING ); REF AEROMAN WO 2024 131/1 NR 2024-336703, PERFORMED PERMANENT REPAIR LOC. ON LOWER SILL FR 61 PLUS 19 IN AT BULK CARGO IAW A320 SRM 53-41-49-300-003 STEP 2A. THIS REPAIR SDR DALA2024082108331Cusp Web · corrodedAIRCRAFT 9510, INITIAL INSPECTION: CORROSION ON LH REPAIR DOUBLER OF CUSP WEB STA Y=841, Y=866 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2-LH CUSP WEB STA Y=866 AT PAX CABIN WAS REPAIR PER B717-200 SRM-53-00-55-2R-4 FIG. 214, LH CUSP WEB STA Y=841 WAS ASDR DALA2024082108330Web · crackedAIRCRAFT 9527, INITIAL INSPECTION: SEVERAL CRACKS BELOW INBD WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX. CORRECTIVE ACTION: WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX WAS REPAIRED PER B717-200 SRM 57-70-10-2R-2, PAR. 4 AND B717-200 SRM 51-41-02-0G.SDR AALA202408214429Cleat · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON FORWARD CARGO FR 34 CLEAT HAS 0.02" CRACK ON FASTENER HOLE. FABRICATED AND INSTALLED FR 34 CLEAT ABOVE STR 27.SDR DALA2024082008300Angle · crackedAIRCRAFT 9550, INITIAL INSPECTION: CRACKS ON ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE. CORRECTIVE ACTION: ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE WAS REPAIRED PER PRI SDR REXA2024111101459Channel · corroded"ANTENA DOUBLER F.S. 295-310 STR 27 CORRODED. UPON FURTHER INVESTIGATION, FOUND CORROSION ON ANTENNA DOUBLER AT F.S. 295-310 STR 27, ORIGINAL MATERIAL THICKNESS OF 0.050"", AFTER CORROSION REMOVAL OF 0.050"", 100% MATERIAL LOSS, DOUBLER FOUND TO BE OUT OF LIMISDR SWAA2024100227989Sill Drain · corrodedMOPSILL CORROSION; BS294+11; RBL56; WL208<[01] UPDATED STEPS 1;2;[02] STEP 2 EDIT FOR DEPTH OF REMOVAL.;[03] CERTIFY;[04] FSD MOPSILL ANGLE TO BE REPLACED ON CARD TTG8Q00VBL39;[05] VERIFIED CORRECTIVE ACTION #4
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