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 SWAA032137Bracket · looseDURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINER BRACKET LOOSE. SECURED RETAINER PER MM.Sep 23, 2003 · N380SW · Boeing 7373H4SDR UPS03841370Fitting · crackedINSPECTION TYPE: C1, STATION 1140 LONGERON 35R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM.51-1-20DSep 23, 2003 · N866UP · Doug DC873FSDR UPS03841384Support Fitting · corrodedINSPECTION TYPE: C1, A-PIT DOOR FWD. LOWER FORWARD T-BOLT SUPPORT FITTING HAS A BACKUP FITT ING CORRODED BEYOND LIMITS AT STA. 290 AT LONG. 33R. REMOVED AND REPLACED FITTING IAW DWG. 5894282,AND SRM. 53-2-0 FIG. 2DSep 22, 2003 · N866UP · Doug DC873FSDR UPS03441319Fitting · damagedINSPECTION TYPE: C, DURING PERFORMING BS 1000 RT BATH TUB FITTING REPLACEMENT AS PER EO NR B747-5310-18579A, IT WAS FOUND 3 EA OF FASTENER HOLES SEAM AT I/B VERT FLANGE AND 6 EA OF FASTENER HOLES FOUND OVERSIZED DIAMETER .309 INCH IN O/B HORIZ FLANGE. THE BASep 22, 2003 · N682UP · Boeing 747121SDR UPS03841427Fitting · crackedINSPECTION TYPE: C3, END FITTING AT STA 1766 L28R MISSING FASTENER. AFTER FURTHER INSP, CRACKED. REMOVED END FITTING AT STA 1766 L28R IAW DC8 SRM 51-1-20D. LOCATED, DRILLED, AND DEBURRED NEW PART P/N 4772397-1N PO 423837.1 IAW DC8 SRM 51-1-24. INSTALLED NSep 19, 2003 · N813UP · Doug DC873FSDR 03FDEA01590Hinge · crackedFWD EXTENDED TAILCONE LT HINGE UPPER ATTACHED FITTING MOUNTED AT FWD FACE OF AFT BULKHEAD STA Y2164 (AFT ACCESSORY COMPT) FOUND WITH 02 EA HAIR LINE CRACKS AS MARKED. FWD EXT TAILCONE LT HINGE UPPER ATTACHED CRACKED FITTING WHICH MOUNTED AT FWD FACE OF AFT Sep 19, 2003 · N603FE · Doug MD11SDR UPS03841306Fitting · crackedINSPECTION TYPE: C1, STA 834 FRAME TO LONGERON FITTING IS CRACKED AT LONG 14R. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.Sep 19, 2003 · N866UP · Doug DC873FSDR 2004F00139Fitting · corrodedAT C-CHECK, FOUND CORROSION ON FITTING AT FRAME 59 AND STRINGER 41R IN AFT CARGO BAY. FITTING AT FRAME 59, RIGHT STRINGER 41 OF FLOOR STRUCTURE REMOVED AND REPLACED. (M)Sep 16, 2003 · N951LF · Airbus A320233SDR AUS20031029Bracket · cracked(AUS) ALTERNATOR CAPACITOR BRACKET FAILED ALLOWING CAPACITOR TO SHORT CIRCUIT ON POSITIVE PLATE.Sep 16, 2003 · Cessna 404CESSNASDR IXXA060529SFitting · corrodedDURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION FS 1124 LONGERON 27 LEFT. REMOVED DAMAGED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.Sep 11, 2003 · N829BX · Doug DC871FSDR UPS03841412Fitting · crackedINSPECTION TYPE:C3 AFT FUSE INTERIOR L17LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED CRACKED LONGERON END FITTING AND INSTALLED NEW FITTING IAW UPS DC8 SRM, 51-1-20D AND 51-1-21.Sep 11, 2003 · N813UP · Doug DC873FSDR UPS03841411Fitting · crackedINSPECTION TYPE: C3, AFT FUSE INTERIOR L10LT END FITTING CRACKED BETWEEN FS 1766-1772. REMOVED L10LT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873FSDR UPS03841409Fitting · crackedINSPECTION TYPE: C3, AFT FUSE INTERIOR L17 RT END FITTING CRACKED BETWEEN FS 1766-FS 1772. REMOVED L17 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873FSDR UPS03841407Fitting · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L10 RT END FITTING CRACKED BETWEEN FS 1768-1772. REMOVED L10 RT END FITTING TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.Sep 11, 2003 · N813UP · Doug DC873FSDR IXXA060539SFitting · corrodedDURING ROUTINE C CHECK, FOUND A CORRODED FITTING UNDER NUT PLATE AT STATION 240 LONGEREON 33 RIGHT. REMOVED DAMAGED FITTING. MANUFACTURED NEW FITTING, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW TIMCO REPAIR ENGINEERING ORDSep 9, 2003 · N829BX · Doug DC871FSDR WVE2003F00014Bracket · crackedLEFT BLEED AIR DUCT SUPPORT BRACKET PN MM67080500001 AT FRAME STA 1108, LEFT BUTT LINE 27, WATER LINE 99.91 IS CRACKED APPROX 2 INCHES. PROBABLE CAUSE: STRESS.Sep 8, 2003 · N610QX · Cndair CL6002C10SDR 2003F00647Fitting · crackedDURING 4 C CHECK, FOUND RT MAIN WHEEL WELL, Y STATION 577-727, FITTING CRACKED. THE DAMAGED PART WAS REPLACED BY A NEW ONE. (M)Sep 7, 2003 · N785TW · Doug DC915FSDR UPS03841400Attach Angle · corrodedINSPECTION TYPE: C3, FWD PIT SMOKE BARRIER UPPER ATTACH ANGLE CORRODED NEAR CENTER LINE. REMOVED CORR IAW DC8 SRM 51-1-8, ORIG .063 INCH, REMOVED .014 INCH, REMAINING .049 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED 2 ANGLES AND SPLICE ANGLE IAW DC8 SRM 5Sep 7, 2003 · N813UP · Doug DC873FSDR SWIA200312452Plate · crackedFS 589.0; LBL 38; FLOOR LANDING PLATE HAS A CRACK EXTENDING FROM RIVET. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-433 REV NC.Sep 3, 2003 · N916SW · Cndair CL6002B19SDR UPS03841212Intercostal · crackedINSPECTION TYPE: C2, INTERCOSTAL BETWEEN STA. 260-280 IS CRACKED AT LONG. 33R REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG.5750726,AND SRM. 51-1-20D.Aug 31, 2003 · N809UP · Doug DC873FSDR UPS03841203Fitting · crackedINSPECTION TYPE: C2, STATION 300 LONG. 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3754041,SRM.53-2-0 FIG. 1B, DWG. 9751879.Aug 28, 2003 · N809UP · Doug DC873FSDR GTIA030672Fitting · corrodedFOUND AFT PIT CORRODED ANGLE AT FS 1155 4 INCHES RBL AND 1 CORRODED FASTENER AT FS 1145, SHORT FRAME, 4 INCHES RBL. AFTER FURTHER INSPECTION DISCOVERED FLOOR SUPPORT STATION 1148 4 INCHES RBL CRACKED. REMOVED FLOOR SUPPORT RECEIVED NEW FLOOR SUPPORT FITTING.Aug 27, 2003 · N829NK · Doug DC982SDR UPS03841222Fitting · crackedINSPECTION TYPE: C2, FLOORBEAM FITTING IS CRACKED AT STA. 340 RBL. 58 REMOVED AND REPLACED FITTING IAW DWG. 9754022,AND SRM. 51-1-20DAug 27, 2003 · N809UP · Doug DC873FSDR UPS03841209Fitting · crackedINSPECTION TYPE: C2, LONG. 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA. 1140 AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG. 3758497,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873FSDR UPS03841208Fitting · crackedINSPECTION TYPE: C2, LONG. 32L SPLICE FITTING IS CRACKED AT STA. 610. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873FSDR UPS03841206Fitting · crackedINSPECTION TYPE: C2, FLOOR SUPPORT FITTING IS CRACKED AT STA. 120 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 5758571,AND SRM. 51-1-20D.Aug 27, 2003 · N809UP · Doug DC873FSDR UPS03841210Fitting · crackedINSPECTION TYPE: C2, 2 EACH CRACKED SEAT TRACK FITTINGS ,B-PIT CEILING STA. 420,RBL 24. REMOVED DAMAGED SEAT TRACK SECTION BETWEEN STA. 300 TO 490 RBL 24-31 FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM. 53-2-3 FIG. 8A,AND REPLACED FITTINGS IAW SRM. 53Aug 26, 2003 · N809UP · Doug DC873FSDR UPS03841207Fitting · crackedINSPECTION TYPE: C2, SEAT TRACK TO FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 700 LBL. 24. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755222,AND SRM. 51-1-20D.Aug 26, 2003 · N809UP · Doug DC873FSDR CA031001006Fitting · cracked(CAN) PART REMOVED FROM SERVICE.NEW PART INSTALLED.Aug 25, 2003 · Bell 205A1SDR UPS03841198Fitting · crackedINSPECTION TYPE: C1, AFT ACCY COMPT. FS 1660 FLOORBEAM END FITTING AT RBL 48 IS CRACKED. HFEC IAW DC8 NDT SPM 06-10-01.001 NOTED TO BE CRACKED. RECEIVED, LOCATE D, AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLEAug 25, 2003 · N801UP · Doug DC873FSDR ABXA030351Fitting · crackedLT FRAME 294 ENG. FITTING CRACKED AT CARGO FLOOR ATTACH POINT. REPLACED FITTING IAW DC-9 SRM 51-10-4, 51-30-5 AND 51-30-1.Aug 18, 2003 · N905AX · Doug DC932FSDR UPS03241154Fitting · crackedINSPECTION TYPE: C, LT BS 740 FITTING CRACKED BEYOND LIMITS. LT BS 740 FITTING REPLACED IAW UPS EO B727-5310-7477-C.Aug 12, 2003 · N937UP · Boeing 72725CSDR UPS03841186Fitting · crackedINSPECTION TYPE: C1, CABIN STA 857, L19R FITTING BEHIND INTERCOSTAL CRACKED. REMOVED FITTING FROM STA 857, L19R FOR REPLACEMENT, RECEIVED SUPPORT FITTING P/N 3779498-502. LOCATED AND DRILLED IAW DC8 SRM 51-3-2. IN STALLED NEW FITTING IAW DC8 SRM 51-1-20D.Aug 8, 2003 · N801UP · Doug DC873FSDR AWXA200300938Attach Angle · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON ATTACH ANGLE UNDER PANEL 191 AT AT BS 1483. MAINTENANCE REMOVED CRACKED ATTACH ANGLE UNDER PANEL 191AT AT BS 1483; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-24-00, PG. 3, FIG.Aug 8, 2003 · N802AW · Airbus A319132SDR UPS03841181Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 L35L INTERCOSTAL ATTACH FITTING IS CRACKED. VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1, REMOVED FITTIN G IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING P/N 3758497.1N PO NR 3541 22 LOCATED AND DRILLED Aug 7, 2003 · N801UP · Doug DC873FSDR UPS03841180Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1140-1150 BETWEEN L32R-L33R INTERCOSTAL ATTACK F ITTING IS CRACKED VERIFIED CRACK IAW DYE PENETRANT TEST IAW DPS 4.707.1. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, AND DRILLED NEW FIT TING IAW DC8Aug 7, 2003 · N801UP · Doug DC873FSDR UPS03841178Fitting · crackedINSPECTION TYPE: C1, AFT CARGO PIT AT FS 1150 L32 RT-L33 RT BANANA FITTING IS CRACKED. REMOVED (2) BANANA FITTINGS STA 1152 AND 1160 L33R-L30R. UPON FURTHER INSPECTION BANANA FITTING NOTED TO BE CRACKED. REC'D, LOCATED, AND DRILLED (2) BANANA FITTINGS IAW DCAug 7, 2003 · N801UP · Doug DC873FSDR USAA030164Fitting · corrodedFOUND FITTING CORRODED .125 INCH AREA, 2 INCHES AROUND FITTING, BOTH SIDES, BS 685 LT MLG SIDE STRUT FITTING. REMOVED BUSHINGS, MACHINED FACES AND BORE OF LUG AND INSTALLED NEW BUSHINGS PER EA 76728. (M)Jul 31, 2003 · N420US · Boeing 737401SDR ASAA0340319Fitting · corrodedOAK - DURING C-CHECK, FOUND LAV ATTACH FITTING CORRODED ON FLOORBEAM AT STATION 947.5 AND WL 208. REPAIRED IAW SRM. (M)Jul 25, 2003 · N786AS · Boeing 7374S3SDR ASAA0340324Fitting · corrodedOAK - DURING C-CHECK, FOUND CORROSION ON GIRT BAR FLOOR FITTING AT STATION 334 AND STRINGER 17. REPAIRED IAW SRM. (M)Jul 25, 2003 · N786AS · Boeing 7374S3SDR EIA2003101Fitting · crackedFWD CARGO PIT AFT PRESSURE BULKHEAD STA 1000, BATH-TUB FITTING BETWEEN STA 38-39L CRACKED. REMOVED AND REPLACED TWO EACH FITTINGS BETWEEN STA 38-39L, STA 1000, P/N 65B16518-1 AND 65B16517Y3 PER B747 SRM 51-32-02, PGS 8 & 9, 51-10-01, PGS 6 & 7, 53-10-03, PG 1Jul 25, 2003 · N485EV · Boeing 747212BSDR 2003FA0000781Fitting · corrodedDURING AN ANNUAL INSPECTION, REMOVED TRIM FROM LEFT AND RIGHT WINDSHIELD POSTS. FOUND FOAM INSULATION IN CONTACT WITH STEEL FITTINGS (PN 7955300 AND 7955301). FITTINGS AND ATTACHING BOLTS (AN3) WERE RUSTED. HAVE FOUND SEVERAL A/C WITH THIS PROBLEM. RECOMMENJul 22, 2003 · N82085 · Piper PA28181SDR 2003FA0000778Fitting · corrodedDURING AN ANNUAL INSPECTION REMOVED TRIM FROM LEFT AND RIGHT WINDSHIELD POSTS. FOUND FOAM INSULATION IN CONTACT WITH STEEL FITTINGS. PN 79553-00 AND 7955301. FITTINGS AND ATTACHING AN3 BOLTS WERE CORRODED. THIS IS THE SECOND INSTANCE OF THIS CONDITION SEVEJul 18, 2003 · N9088Q · Piper PA28181SDR HEEA088077Fitting · wornEXCESSIVE WEAR FROM EARS ON CROSSTUBE PAD. REPLACED FITTINGS.Jul 8, 2003 · N8588X · Bell 206L3SDR UPS03841039Fitting · corrodedINSPECTION TYPE: C2, FWD PIT FS 272 AND L25L Z-FITTING CORRODED. REMOVED FITTING, FABBED SPLICE ANGLES 2 EA IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED HOLES ON NEW FITTING IAW DC8 SRM 53-2-0, INSTALLED NEW FITTING AND SJul 7, 2003 · N750UP · Doug DC871FSDR GTIA030574Fitting · corrodedFOUND CABIN FS 1309 FRAME TO FLOORBEAM ATTACH FITTING CORRODED AND FAST CORRODED STRINGER 18R. REMOVED OLD FITTING. INSTALLED NEW FITTING. (M)Jul 2, 2003 · N804NK · Doug DC982SDR CA030709010Attach Fitting · misinstalled(CAN) EXTERNAL PLATFORM AND COUNTERWEIGHT INSTALLATION MODIFICATION OF STRUT ATTACH FITTING IS DAMAGING UPPER CORNER OF HELICOPTER ROOF STRUCTURE AND THUS REQUIRES INSTALLATION OF NEW HARDWARE PN 95K0300-063 & 95K0300-065.Jun 28, 2003 · Hughes 369ESDR 03FDEA00995Fitting · gougedMDIS 463 53-10 0005658 24JUN03 BFM CLOSE R COMPLY WITH EA NR 7-5310-70960, FUSELAGE - MAIN CARGO DOOR ACTUATOR FITTING GOUGE REPAIR P/N 53FX1428-1. FACT 27JUN03 13:57 BFM R COMPLIED WITH EA NR 7-5310-70960,FUSELAGE-MAIN CARGO DOOR ACTUATOR FJun 28, 2003 · N463FE · Boeing 727200SDR UPS03840917Fitting · crackedINSPECTION TYPE: C, STATION 1875 AT LONGERON 36 LARGE FITTING IS CRACKED INSIDE 62 TAIL COMPARTMENT. REMOVED AND REPLACED FITTING IAW DWG 5652580 AND SRM 51-1-20D, 51-3-0.Jun 19, 2003 · N807UP · Doug DC873FSDR UPS03840943Fitting · crackedINSPECTION TYPE:C3 A/C BAY STA 8 LONG 33L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4612650 AND SRM 51-1-20D.Jun 18, 2003 · N807UP · Doug DC873F
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