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 SWIA200312042Attach Fitting · crackedFS 625 RIGHT INTERCOSTAL ANGLE CRACKED STR 14R. REPLACED ANGLE IAW CRJ SRM 51-40-11.Apr 15, 2003 · N432SW · Cndair CL6002B19SDR GTIA030319Fitting · corrodedAFT PIT LT FITTING SUPPORT LOWER DOOR JAMB, 2 EA CORRODED STA 1155, STA 1211. REMOVED 2EA LT FITTINGS. LOCATED AND DRILLED NEW FITTINGS. INSTALLED NEW FITTING.Apr 15, 2003 · N823NK · Doug DC982SDR ASAA0380312Attach Bracket · crackedOAK - FOUND DURING 15K CHECK, E/E ATTACH ANGLE BRACKET IS CRACKED AT AFT SIDE OF TERMINAL END OF LONGERON 7R AT FS 1463. REPLACED BRACKET PER SRM 51-10-2 AND 30-5. (M)Apr 14, 2003 · N947AS · Doug DC983SDR ASAA0380314Attach Bracket · crackedOAK - DURING 15K CHECK, FOUND TRIM AND LOAD FEEL CENTERING SPRING ACTUATOR ATTACH BRACKET IS CRACKED AT FS 1485. REPLACED BRACKET PER SRM 51-10-3 AND 10-4. (M)Apr 14, 2003 · N947AS · Doug DC983SDR ASAA0380317Attach Angle · corrodedOAK - FOUND 15K CHECK, ATTACH ANGLE IS CORRODED BETWEEN FS 1212 AND 1222 OUTBOARD OF LONGERON 30 IN AFT CARGO BAY. REPLACED ATTACH ANGLE PER SRM 51-10-3 AND 4. (M)Apr 14, 2003 · N947AS · Doug DC983SDR UPS03840676Fitting · crackedINSPECTION TYPE: C1, STA. 45-70 AT APPROX. LBL. 48 AT OVERHEAD IN AC BAY HAS A CRACKED FITTING. REMOVED,FABRICATED AND INSTALLED FITTING IAW DWG. 5890314,AND SRM 51-1-20D,51-3-0Apr 13, 2003 · N808UP · Doug DC873FSDR QXEA0300477Clip · damagedAT FS 1108 LEFT HAND SIDE LOOKING FORWARD CLIP LOWER FASTENER HOLE ELONGATED. REPAIRED IAW HORIZON AIR EO R-53-44B, EA 53-89 AND EO 601R-53-3923.Apr 7, 2003 · N607QX · Cndair CL6002C10SDR QXEA0300478Fitting · damagedAT FS 1126 STRINGER 11 RIGHT SIDE AT FITTING MM670-36545-002 EXISTING HOLES NR 5AD NEEDS STEPPED UP TO NR 6AD. REPAIRED IAW HORIZON AIR EA 601R-53-3912 AND EA R-53-84.Apr 4, 2003 · N607QX · Cndair CL6002C10SDR ASAA0380278Fitting · crackedOAK - DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M)Apr 2, 2003 · N947AS · Doug DC983SDR ASAA0380279Fitting · crackedOAK DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M)Apr 2, 2003 · N947AS · Doug DC983SDR DHL2003741548Fitting · corrodedDURING C-CHECK, BS 1050 STR 27R END FITTING CORRODED. REMOVED FITTING BS 1050 STR 26R FOR REPAIR. REMOVED FASTENERS FOR ACCESS ON STR 27R KEEL BEAM EXTENSION ANGLE. UPON REMOVAL OF STR FITTING FOUND KEELBEAM T-ANGLE CORRODED AND CRACKED. REMOVED PREVIOUS KApr 1, 2003 · N741DH · Boeing 727200SDR ASAA0240166Channel · crackedPAE - DURING C-CHECK, FOUND RADAR MOUNT SHELF CHANNEL IS CRACKED AT BS 204. REPAIRED IAW SRM. (M)Mar 22, 2003 · N774AS · Boeing 7374Q8SDR ASAA0310208Fitting · corrodedPAE - DURING C-CHECK, FOUND LT UPLOCK SUPPORT FITTING AT BS 685, LT BUTTOCK LINE 70 CORRODED. REMOVED AND REPLACED SUPPORT FITTING IAW MFG DWG. (M)Mar 22, 2003 · N744AS · Boeing 737210CSDR ASAA0310200Attach Angle · corrodedOKC - DURING D-CHECK, FOUND ATTACH ANGLES AT BS 947, STRINGER 25L-25R CORRODED. REMOVED AND REPLACED ANGLES PER SRM. (M)Mar 21, 2003 · N745AS · Boeing 737298CSDR 2003FA0000384Bracket · wornDURING A ROUTINE INSPECTION THE NOSE GEAR ACTUATOR ATTACH BRACKETT WAS FOUND LOOSE. ALL ATTACH RIVETS AND HARDWARE WERE FOUND TO BE WORKING. THE NOSE GEAR ACTUATOR ROD END CLEVIS ATTACH BOLT WAS ALSO FOUND BENT. THE BRACKETT AND CLEVIS BOLT WERE REPLACED. Mar 14, 2003 · N5326U · Piper PA28R201SDR GTIA030153Bracket · crackedMAIN CABIN UNDER FLOOR STA 864 LT FLOORBEAM TO FUSELAGE ATTACH BRACKET CRACKED. REMOVED CRACKED BRACKET. LOCATED AND DRILLED NEW BRACKET. INSTALLED BRACKET.Mar 12, 2003 · N809NK · Doug DC983SDR ASAA0380205Attach Angle · crackedOKC - DURING 30K CHECK, FOUND GILLINER ATTACH ANGLE IS CRACKED AT FS 617. REPAIRED CRACKED ANGLE WITH COLD BOND FIBERGLASS OVERLAY PER SRM 51-70-1. (M)Mar 4, 2003 · N935AS · Doug DC982SDR UPS03840314Fitting · crackedINSPECTION TYPE:C2 LONG 31L SPLICE FITTING IS CRACKED AT STA 600-640. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.Mar 3, 2003 · N880UP · Doug DC873FSDR ASAA0380186Fitting · brokenOKC - FOUND DURING 30K CHECK, LEFT OVERHEAD STOWAGE BIN MOUNT FITTING IS BROKEN. REPLACED MOUNT FITTING PER MM 20-10-12 AND 30-01. (M)Mar 2, 2003 · N935AS · Doug DC982SDR UPS03440398Bracket · corrodedINSPECTION TYPE: C, LT MLG WW - BS 1241 LBL 1 TO 8 HORIZONTAL BRACKET FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PAGE 8 TOTALLY 2 EA (P/N: 65B82011-3 AND 69B11570-1).Mar 2, 2003 · N520UP · Boeing 747200SDR MWEA030110Support Fitting · crackedPAX DOOR INERCOSTAL SUPPORT FITTINGS AT DOOR CENTER LINE ABOVE BEAM #1 CRACKED. -- LOCATED, DRILLED AND INSTLALLED SUPPORT FITTINGS.Feb 21, 2003 · N803ME · Doug DC981SDR GTIA030098Fitting · corrodedFTW - FOUND MAIN CABIN FS 1022 STATION 181 T-FITTING CORRODED. REMOVED T-FITTING, LOCATED AND DRILLED NEW PART. INSTALLED FITTING. (M)Feb 10, 2003 · N811NK · Doug DC981SDR UPS03840170Fitting · crackedINSPECTION TYPE: C3, ALC STA 1490 L34R SPLICE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Feb 6, 2003 · N805UP · Doug DC873FSDR UPS03840168Fitting · crackedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1160 BETWEEN L33R-34R Z-FITTING IS CRACKED. REMOVED CRACKED FITTING. FABRICATED REPAIR DOUBLER & SHIM IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING REPAIR DOUBLER AND SHIM IAW DFeb 6, 2003 · N805UP · Doug DC873FSDR DHL2003804893Fitting · crackedAFT CARGO COMPT FITTING CRACKED 3.000 BETWEEN STA 1040.000 AND 1060.000 NEAR TO L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 AND FAX BOEING-SEV-LIM-03-00-0003H, DATE: JAN. 20, 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANEDFeb 5, 2003 · N804DH · Doug DC873FSDR AWXA200300165Fitting · corrodedLCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON R/H FORWARD VERTICAL TO FUSELAGE ATTACH FITTING BS 1088. MAINTENANCE REMOVED CORRODED ATTACH FITTING BS 1088; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW B737-Feb 3, 2003 · N175AW · Boeing 73733ASDR UPS03840169Fitting · crackedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1040-1060 AT L28R SPLICE FITTING IS CRACKED. REMOVED CRACK FITTING. LOCATE NEW FITTING, DRILL EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. REMOVED LOWER FILLET PANEL FOR ACCESS IAW DC8 SRM 51-3-0. INSTAFeb 3, 2003 · N805UP · Doug DC873FSDR DHL2003804666Fitting · crackedAFT CARGO COMPT. SPLICE FITTING CRACKED 3.000 INCH BETWEEN STA. 1040.000-1060.000 , L31R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1 AND FAX BOEING -SEU-LIM - 03-00003H DATE 20TH 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED , TREATED ANDFeb 2, 2003 · N804DH · Doug DC873FSDR DHL2003740514Channel · chafedCABIN BS 1166 STR 10.3 LT ATTACHING GILLINER SUPPORT SHOWS CHAFE MARK. CUT OUT DAMAGED AREA (2.5 X 1 INCH) AND FABRICATED DOUBLER (7075-T6 .090) PER SRM 53-10-2 AND 51-40-3. TREATED AND PRIMED PARTS PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-30-2.Feb 2, 2003 · N740DH · Boeing 7272Q9SDR DHL2003740511Channel · chafedCABIN BS 1166 AND 1148 STR 7.5 LT EACH HAVE GILLINER ATTACHING SUPPORT CHAFE MARKS INTO FRAME. CUT OUT DAMAGED AREA AT STA 1166 3 X 1 INCH, AND 1148 3 X 1 INCH PER SRM 51-40-3. FABRICATED DOUBLERS (7075-T6 .100) PER SRM 53-10-2 FIG 5. TREATED PARTS AND AREAFeb 2, 2003 · N740DH · Boeing 7272Q9SDR F3LA200300054Attach Angle · wornDURING C-4 CHECK, INSPECTION REPORTED SEVERAL FASTENER HOLES WORN AND DAMAGED ON RT MLG WHEEL WELL CUTOUT AFT FAIRING ATTACH ANGLE. REPLACED ATTACH ANGLE PER SRM 51-40-02.Feb 1, 2003 · N303FL · Boeing 7373M8SDR UPS03840149Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN FITTING IS CRACKED AT STA 680 FWD SIDE AT LONG 12R. REMOVED AND REPLACED FITTING IAW DWG 3779762, AND SRM 51-1-20D.Feb 1, 2003 · N811UP · Doug DC873FSDR AWXA200300163Fitting · corrodedLCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LAVATORY AREA FLOOR BOARD ATTACH HOLE BS 986, RBL 20. MAINTENANCE REMOVED AND REPLACED ATTACH FITTING AT BS 986, RBL 20 IAW B737-300 SRM 51-40-02, PG. 6-9.Jan 31, 2003 · N175AW · Boeing 73733ASDR UPS03840167Fitting · corrodedINSPECTION TYPE: C3, AFT CARGO PIT AT FS 1210 BETWEEN L33R-34R T-BOLT LATCH BACKUP FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2 -0. LOCATED, TRIMMED AND DRILLED UP FITTING 3754930-1 AND REPAIR FITTINGS 5894282-5Jan 29, 2003 · N805UP · Doug DC873FSDR IXXA060500SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACKED END FITTING FROM STATION 1767 TO 1772 AT LONGERON 10 LEFT. REMOVED CRACKED END FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D, 51-1-21, 21-3-0, AND 51-1-24.Jan 23, 2003 · N820BX · Doug DC871FSDR ABXA030070Fitting · crackedFLOOR BEAM TO KEEL FITTING, STA. 775 WAS CRACKED. REPLACED FITTING, STA. 775, IAW DC-9 SRM 51-30-5 AND 51-30-1.Jan 23, 2003 · N957AX · Doug DC941SDR F3LA200300024Attach Angle · damagedDURING C-4 CHECK, INSPECTION REPORTED LT MLG WHEELWELL CUTOUT AFT FAIRING ATTACH ANGLE HAD SEVERAL FASTENER HOLES WORN AND DAMAGED. REPLACED FAIRING ATTACH ANGLE PER SRM 53-43-01.Jan 22, 2003 · N303FL · Boeing 7373M8SDR C2XA03TY005Angle · corrodedTYS, During a scheduled inspection corrosion was found on the center ramp angle between frames 19 and 20. Maintenance removed and replaced the center ramp angle, alodined, primed and painted. I/A/W-EMB-135/145-SRM-51-40-02. The repair was satisfactory and the Jan 18, 2003 · N18982 · Emb EMB145LRSDR C2XA03TY009Doubler · corrodedTYS, During a scheduled inspection corrosion was found on the galley spar joint caps by the sevice door. Maintenance removed and replaced the doubler on galley forward sill, alodined, primed and painted. I/A/W-EMB-135/145-GST-1927/02A, CMP-51-21-04/05/06. The Jan 18, 2003 · N18982 · Emb EMB145LRSDR C2XA03TY008Doubler · corrodedTYS, During a scheduled inspection corrosion was found on doubler of right omega beam at frame 20 and 22. Maintenance cleaned doubler at FR20 and found to be within limits and removed and replaced the doubler for omega beam at FR22, alodined, primed and painteJan 18, 2003 · N18982 · Emb EMB145LRSDR UPS03840078Fitting · corrodedINSPECTION TYPE: C-2, AFT PIT DOOR SLIDE AREA STA 1210 BETWEEN LONG 31R-32R END FITTING CORRODED. REMOVED EXISTING FITTINGS, LOCATED, DRILLED AND DEBURRED NEW FITTINGS P/N 3754930-1N, 5894282-501, & 5894282-502 IAW DC8 SRM 51-3-2 AND INSTALLED FITTINGS IAW DJan 16, 2003 · N868UP · Doug DC873FSDR UPS03240056Fitting · crackedINSPECTION TYPE: C, CRACK INDICATION IN ONE HOLE BS 870 LT HOLE LOCATED 2ND FASTENER ROW FROM FWD EDGE OF FITTING TOP FASTENER HOLE OF LWR FITTING. REPAIRED IAW UPS EO B727-5310-3057-H.Jan 7, 2003 · N934UP · Boeing 72721CSDR UPS03840017Fitting · corrodedINSPECTION TYPE: C2, ALL STA 1400 L30R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVEED CORRODED FITTING IAW DC8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Dec 29, 2002 · N868UP · Doug DC873FSDR ASA0280670Attach Fitting · crackedOKC - FOUND DURING 30K CHECK, UPPER LEFT TAILCONE ATTACH BRACKETS TWO CRACKED. REPLACED BRACKETS PER SRM 51-10-2, 51-10-4, 51-30-1, AND DAC DWG 9911957. (M)Dec 23, 2002 · N972AS · Doug DC983SDR DLM90021403Attach Angle · crackedDURING HMV-1, THE FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT CANTED STA 1520.225 AND LONGERON L-2L. THE HORIZONTAL LEG WAS TRIMMED SIMILAR TO MD80 SRM 53-05-D, FIGURE 23. FILLER WAS ADDED TO THE TRIMMED OUT AREA AND A REPAIR ANGLE INSTALDec 1, 2002 · N916DN · Doug MD9030SDR SWIA200211645Channel · crackedCARGO DOOR FORWARD TRACK CHANNEL STR 16L IS CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGED CHANNEL IAW CRJ SRM 53-61-23, 51-24-16, 51-40-11, 51-25-06, 51-25-00, 51-42-06 & 51-24-11.Nov 26, 2002 · N907SW · Cndair CL6002B19SDR UPS02239947Fitting · crackedINSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956Nov 13, 2002 · N905UP · Boeing 72751CSDR DLM88021319Attach Angle · crackedFUSELAGE / VERT STAB TO FUSELAGE ATTACH ANGLE / RH : CRACK REPAIR THE RH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FRAME STA. 1474. THE CRACK WAS .75" LONG IN THENov 13, 2002 · N990DL · Doug MD88SDR 2002UALA01723Fitting · gougedAFT CARGO DOOR CUT OUT LOWER SILL 3RD FROM FRONT LUG HAS GOUGE AFT LOWER END. MAJOR REPAIR ACCOMPLISHED. 3RD FROM FRONT LOWER LUG BLENDED & ROTO PEENED.Nov 13, 2002 · N467UA · Airbus A320232SDR C7WA200200035Fitting · crackedDURING CPCP INSPECTION WITH JOB CARD C5322401 FOUND 8 INCH CRACK IN MAIN DECK HORIZONTAL FITTING BETWEEN BS 930 AND BS 950 AT STR 14L. C/A: REMOVED AND REPLACED HORIZONTAL FITTING AT STRINGER 14L. BETWEEN BS 930 AND BS 950 IAW SRM.Oct 19, 2002 · N220NE · Boeing 72731
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