JASC 5340

Service difficulty reports · 22,411

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.

SDR UPS05845282Fitting · crackedSTA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D.Aug 15, 2005 · N750UP · Doug DC871FSDR AWXA200501011Fitting · corrodedSAL - MAJOR REPAIR - CORROSION FOUND ON C3 CHECK LOCATED AROUND FITTING AT THE LOWER SILL OF THE FORWARD CARGO DOOR CUTOUT. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE FITTING LOCATED ON THE LOWER SILL OF FORWAug 15, 2005 · N645AW · Airbus A320231SDR UPS05845256Fitting · crackedEND FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D.Aug 15, 2005 · N750UP · Doug DC871FSDR MWEA050080Attach Angle · corrodedMAIN CABIN, LEFT INBOARD SEAT TRACK ATTACH ANGLE AT STATION 1174 BROKEN AND CORRODED. REMOVED AND REPLACED CLIP.Aug 15, 2005 · N814ME · Doug DC981SDR 2005UALA00815Stringer Clip · crackedAFT PIT STA 907 STR 24R STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.Aug 14, 2005 · N327UA · Boeing 737322SDR 2005UALA00814Stringer Clip · bentAFT PIT STA 727D STR 20L STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.Aug 14, 2005 · N327UA · Boeing 737322SDR DHL2005747507Attach Angle · corrodedCORROSION ON SKIN ATTACH ANGLE FS 990 FROM STR 27R TO STR 29R. REMOVED CORROSION OFF SKIN ATTACH ANGLE FS 990 STR 27R TO 29R. PERFORMED ULT INSP ON BLENDED AREA. ATTACH ANGLE BEYOND LIMITS IAW B727 SRM 51-20-1. FABRICATED AND INSTALLED NEW ATTACH ANGLE SKIAug 14, 2005 · N747DH · Boeing 727224SDR SWAA052444Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.Aug 14, 2005 · N696SW · Boeing 7373T5SDR SWAA052443Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.Aug 14, 2005 · N696SW · Boeing 7373T5SDR UPS05845385Fitting · crackedINSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND INSTALLED FITTING AND INTERCOSTAL IAW DWG 4758514 AND DWG 9754949.Aug 13, 2005 · N750UP · Doug DC871FSDR UPS05845292Fitting · corrodedLWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED .500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTING AT FS 1230 L32R IAW SRM 51-3-2 AND 51-1-20D.Aug 13, 2005 · N750UP · Doug DC871FSDR LR7A05103Tee Fitting · corrodedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WHEEL WELL TEE AND WEB CORRODED AT FS 588 TO 596, LBL 65, WL 138. REPLACED TEE AND WEB IAW SRM SMP 583 51-60 AND 70.Aug 13, 2005 · N404LC · Lkheed 382GSDR UPS05845229Fitting · crackedMAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0 .Aug 12, 2005 · N750UP · Doug DC871FSDR UPS05845219Fitting · crackedFITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 12, 2005 · N750UP · Doug DC871FSDR SWAA052433Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM.Aug 12, 2005 · N612SW · Boeing 7373H4SDR SWIA200515864Clip · crackedMAIN AVIONICS COMPARTMENT STA 280 BL 10.5 WL 74.0 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE AND FILLER IAW CRJ200 SRM 51-42-21.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR SWIA200515863Clip · crackedMAIN AVIONICS COMPARTMENT STA280 BL 10.5 WL 74.0 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE AND FILLER IAW CRJ200 SRM 51-42-21.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR SWIA200515862Clip · crackedMAIN CABIN FS 484 RT BL 28.5 WL73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW 'CLIP' AT FS 484 RT BL 28.5 WL 73.5 IAW CRJ200 RHEO 601R-41-059 REV A.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR SWIA200515861Clip · crackedMAIN CABIN FS484 RT BL 36WL 73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW 'CLIP' PN 601R-53-41-059-2 AT FS 484 RT BL-36 WL IN MAIN CABIN IAW CRJ200 601R-53-41-059 REV 'A'.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR SWIA200515860Clip · crackedMAIN CABIN FS484 LT BL AND 28.5 WL 73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP MAIN CABIN FS484 LH BL 28.5 WL 73.5 IAW CRJ200 REO 601-53-41-059 REV A.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR SWIA200515859Clip · cracked280 BULKHEAD FLOOR SUPPORT STRUCTURE CLIPS AT LBL 9 AND RBL 9 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS IAW CRJ200 SRM 51-42-11.Aug 11, 2005 · N447SW · Cndair CL6002B19SDR IXXA05SMN178SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 6, STA 1260.000 STA 1280.000 L-34L. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51.1.20D PAGE 21. CLEANED, TRETAED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51Aug 11, 2005 · N603AL · Doug DC873FSDR IXXA05SMN179SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCY CMPT BATHTUB FITTING CRACKED 1, STA 1690.000, L-28R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9 AND DCAug 11, 2005 · N603AL · Doug DC873FSDR UPS05845371Fitting · crackedINSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG 3643110 AND 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845366Fitting · crackedINSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845293Fitting · crackedFITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845281Fitting · corrodedMAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTING AT FS 980 LBL 40 IAW SRM 51-3-0, 51-1-21, AND 51-3-2.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845280Fitting · crackedLONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845279Fitting · crackedLONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845277Fitting · crackedCRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,51-1-20D AND 51-01-23 FIG 48.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845276Fitting · crackedMAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SRM 51-1-8. REMOVED AND REPLACED "T" FITTING IAW SRM 51-3-2 AND DWG 3649114.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845274Fitting · crackedFS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845258Angle · crackedCENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845253Fitting · crackedFRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT FS 781 LONG 18R AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845233Fitting · crackedFRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT F/S 857.125 L19L. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-21D AND 51-3-2.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845232Fitting · crackedFRAME TO INTERCOSTAL ATTACHED FITTING CRACKED AT F/S 834.500 L18L. REMOVED AND REPLACED INTERCOSTAL ATTACH FITTING IAW SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845226Fitting · crackedLONGERON END FITTING CRACKED AT FS 857.125 L1 FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845221Fitting · crackedLONGERON END FITTING CRACKED FS 907 L8R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845220Fitting · crackedFITTING CRACKED FS 822 L20L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Aug 11, 2005 · N750UP · Doug DC871FSDR UPS05845202Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED (2 INCHES) STA 680 L2R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D,51-1-21,AND 51-1-23 .Aug 11, 2005 · N750UP · Doug DC871FSDR SWAA052414Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.Aug 11, 2005 · N690SW · Boeing 7373G7SDR SWAA052411Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.Aug 11, 2005 · N612SW · Boeing 7373H4SDR SWAA052400Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM.Aug 11, 2005 · N612SW · Boeing 7373H4SDR SWAA052399Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.Aug 11, 2005 · N612SW · Boeing 7373H4SDR IXXA05SMN167SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .500 INCHES, STA 300.000 , L-32R L-33R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS (HILOAug 10, 2005 · N603AL · Doug DC873FSDR IXXA05SMN166SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .5 INCHES STA 340.000 , L-32R L-33R. REMOVED AND REPLACED CRACKED FITTING ON FWD CARGO CMPT, STA 340.000, L32R-L33R IAW DC8 SRM 51.1.20D PAGES 9, 21. TORQUED IAW DC8 SRM 51-3-1.Aug 10, 2005 · N603AL · Doug DC873FSDR USAA050999Angle · corrodedCLT - FOUND ZEE ANGLE CORRODED 3.5 INCHES, SCREW HOLES ON THE SURFACE OF THE LEFT SUPPORT ZEE ANGLE AT LBL 20.20. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 53-40-01. (M)Aug 10, 2005 · N449US · Boeing 7374B7SDR SWAA052391Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.Aug 10, 2005 · N696SW · Boeing 7373T5SDR SWAA052390Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM.Aug 10, 2005 · N696SW · Boeing 7373T5SDR SWAA052380Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM.Aug 10, 2005 · N612SW · Boeing 7373H4
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