JASC 5340

Service difficulty reports · 22,407

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 ASOA2013051403543Attach Angle · corrodedATTACH ANGLE FOR FLIGHT COMPARTMENT FLOOR PANEL 221ALF IS CORRODED AT FS280. RECEIVED NEW SERVICEABLE PART PN CL670-33292-13S, LOCATED AND DRILLED TO MATCH ACFT IAW SRM 51-40-11-001-001-A01. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLEApr 8, 2013 · N398CA · Cndair CL6002C10SDR CALA2013040800210Mount · corrodedCORROSION AROUND LAVATORY MOUNT BLOCK AT BS 947.5, RBL 51 REPAIRED IN IAW ECRA 5321-01840.Apr 8, 2013 · N16713 · Boeing 737724SDR DALA1308396802Mount · corrodedCORROSION ON GALLEY MOUNT FITTING . REMOVED AND REPLACED GALLEY MOUNTS PER SRM 51-40-02 PG 10 PAR 9.Apr 8, 2013 · N703TW · Boeing 7572Q8SDR ASOA2013051403542Bracket · corrodedCORROSION ON TOP OF PLATE ATTACHED TO FS 533 FRAME AND STR 26L. REMOVED BRACKET IAW SRM 51-42-21-001-001 AND 51-42-06-001-001 BY REMOVING RIVETS AND HILITES. INSTALLED BRACKET, PN SH670-33389-1 AT F/S533 STR 26L IAW SRM 51-42-21-001-001-A01 AND 51-42-13-001-Apr 6, 2013 · N398CA · Cndair CL6002C10SDR UALA2013040802320Strap · missingCRASH AX HOLD DOWN STRAP MISSING. INSTALLED CRASH AXE STRAP.Apr 5, 2013 · N821UA · Airbus A319131SDR QXEA2013040500772Plate · corrodedFWD DRAFT BULKHEAD LOWER MOUNTING PLATE AT BS 32.4 HAS CORROSION. REMOVED DRAFT HEAD MOUNTING PLATE IAW SRM 51-42-05-02-01 & 51-42-45-02-01 REV 12. FOUND OUT OF LIMITS IAW SRM 51-21-00-00-02 REV12. LOCATED AND DRILLED FABRICATED MOUNTING BRACKET IAW SRM 51-Apr 5, 2013 · N410QX · Bombdr DHC8402SDR DALA13015043215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.750",W=0.250", D=0.002". REPLACE CLEAT AT FR 33 AND BETWEEN, STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 5, 2013 · N315US · Airbus A320211SDR DALA13015033215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FORWARD CARGO COMPARTMENT L=0.800", W=0.250", D=0.002" MEASURES APPROX SSI 532180. REPLACED CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FWD CARGO COMPARTMENT IAW SRM 51Apr 5, 2013 · N315US · Airbus A320211SDR DALA13015023215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=2.00", W=0.310", D=0.002". REPLACED CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 5, 2013 · N315US · Airbus A320211SDR QXEA2013040400736Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT STA 529.5. STRINGER CLIP AT STA 529.5 STR 24S WAS REMOVED IAW SRM 51-42-05-02-01, REV 12. PRIOR TO REMOVAL STRINGER CLIP, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. RECIEVED NEW PART, MATCH DRILLED TO AC IAW SRMApr 4, 2013 · N410QX · Bombdr DHC8402SDR QXEA2013040400735Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT STA 401. REMOVED 2EA SETS OF PILLOW BLOCKS TO FOM IAW SRM 51-41-05-00-01 REV 12. REMOVED 24S STRINGER CLIP AT STA 401 FOR REPLACEMENT IAW SRM 51-42-05-02-01, REV 12. MATCH DRILLED NEW CLIP IAW SRM 51-40-07-02-01, REV 12. OK TApr 4, 2013 · N410QX · Bombdr DHC8402SDR DALA13014993215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.375" D=0.002". REPLACED CLEAT AT FR 33 AND BTW STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-7Apr 4, 2013 · N315US · Airbus A320211SDR DALA13014683215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=1.300" W=0.350" D=0.003". REPLACED CEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COApr 4, 2013 · N315US · Airbus A320211SDR HNAA2013040400206Bracket · corrodedBAG BAY COVE AREA BRACKET IS CORRODED. REMOVED FASTENERS FROM COVE AREA, REMOVED COVER AND BRACKET. INSTALLED NEW BRACKET IAW DWG 85330119. INSTALLED COVE PANEL.Apr 4, 2013 · N837EX · Dhav DHC8102SDR SWAA2013041814998Fitting · crackedCLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.Apr 3, 2013 · N653SW · Boeing 7373H4SDR DALA1309650195Tee Fitting · damagedDENT AND DAMAGED TEE FITTING ON FUSELAGE SKIN BETWEEN BS 266 AND 276, BELOW WL 207.48. REPAIRED IAW PRI 512812-14, REV O, ER/A 512812-14 REV ORIG.Apr 3, 2013 · N195DN · Boeing 767332SDR 7AHR20130416002Attach Angle · corrodedLEFT LAV FLOOR TO WALL ATTACH ANGLES HAVE SURFACE CORROSION. R & R 3 EA ATTACH ANGLES IAW SRM 51-30-1.Apr 3, 2013 · N836RA · Doug DC983SDR SWAA2013040914574Attach Angle · corrodedFWD GALLEY DOOR THRESHOLD ATTACH ANGLE CORRODED BETWEEN BS 294 TO BS 328. REPAIRED ANGLE IAW SRM.Apr 3, 2013 · N213WN · Boeing 7377H4SDR DALA13014713215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" =0.800" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 31 AND BETWEEN STR 42L TO STR 43L IN FWD CARGO COMPARTMENT IAWApr 3, 2013 · N315US · Airbus A320211SDR DALA13014673215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=2.100" W=0.300" D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 34 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMApr 3, 2013 · N315US · Airbus A320211SDR DALA13014663215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=3.00" W=0.375" D=0.003". REPLACED CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014653215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=0.750" W=0.210" D=0.002". REPLACED CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014633215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APPROX. L=0.800" W=0.300" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT IAW SRM A320 51-72-11.Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014623215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" W=0.300" D=0.002". REPLACED CLEAT ON FWD CARGO COMP FR 30 BETWEEN STR 41R AND STR 42R IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014613215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.00" W=0.310" D=0.002". REPLACED CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-1Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014603215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.750" W=0.210 " D=0.002". REPLACED CLEAT AND FASTENERS LOCATED FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGOApr 3, 2013 · N315US · Airbus A320211SDR DALA13014583215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 39R TO STR 40R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.210" W=0.105" D=0.002" REPLACED CLEAT AT FR 31 AND BETWEEN STR 39R TO STR 40R IN FWD CARGO COMPARTMENT IAW SRM A320 Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014573215Attach Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=0.900"W=0.340" D=0.001". REPLACED CLEAT AT FR 31 AND BTW STR 42R TO STR 43R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11.Apr 3, 2013 · N315US · Airbus A320211SDR DALA13014500945Attach Angle · corrodedDURING SCHEDULED INSPECTION, THE RT LAVATORY AREA FS 1328 FLOOR ATTACH ANGLE HAS INTERGRANULAR CORROSION AT FUSELAGE ATTACHMENT. REPAIRED IAW SRM 53-05, FIG 24A ID REPAIR IAW PS 900-5-1 N4.Apr 3, 2013 · N945DL · Doug MD88SDR SWAA2013041514839Attach Angle · crackedKEEL BEAM TO FRAME ATTACH ANGLE CRACKED AT STA 500D, LBL 7. REMOVED AND REPLACED ANGLE IAW BOEING DWG IAW SRM.Apr 1, 2013 · N608SW · Boeing 7373H4SDR DALA1308026806Fitting · crackedAFT CARGO DOOR FRAME UPPER FWD FITTING STA 1400 AT DOOR LOCKED SWITCH CRACKED. R & R UPPER FWD DOOR FRAME FITTING NEAR DOOR LOCKED SWITCH IAW SRM 53-30.Apr 1, 2013 · N709TW · Boeing 7572Q8SDR DALA13014070944Fitting · corrodedCORROSION ON FITTINGS AT BS 1155 TO 1157 AND 1212 TO 1210 BETWEEN LONGERON PROTECTION 26 TO 29R FITTINGS WERE REPLACED IAW SRM 51-30-5.Mar 30, 2013 · N944DL · Doug MD88SDR QXEA2013032900709Stringer Clip · corrodedSTRINGER 24P CLIP IS CORRODED AT STA 763.6. REMOVED STRINGER CLIP DUE TO CORROSION IAW SRM 51-42-45-02-01, 51-42-05-02-01, REV 12, MATCH DRILLED NEW STR CLIP IAW SRM 51-40-07-02-01, REV 12. INSTALLED STRINGER CLIP IAW SRM 51-42-05-02-01 AND SRM 51-42-45-02-0Mar 29, 2013 · N410QX · Bombdr DHC8402SDR DALA13014289233Stringer Clip · crackedAFT AIR STAIR AREA UPPER RT SIDE BS 1488 LONGERON 2R, STRINGER CLIP CRACKED. R & R STRINGER CLIP IAW SRM 51-30-05 VOL II, PAGE 1, DWG 9464460.Mar 29, 2013 · N933DN · Doug MD9030SDR DALA13014279233Attach Angle · crackedEMPENAGE LT SIDE BS 1520 UPPER AFT CORNER OF VENT BOX LOUVERS, VERTICAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM 51-31-00 VOL II.Mar 29, 2013 · N933DN · Doug MD9030SDR SWAA2013041014663Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.Mar 28, 2013 · N374SW · Boeing 7373H4SDR QXEA2013032800692Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT BS 547. STRINGER CLIP 24S AT STA 547 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. REMOVED STRINGER CLIP AT STA 547 STR 24S IAW SRM 51-42-05-02-01, REV 12. NEW CLIP MATCH DRILLED TO ACFT IAW SRM REV 12 51-40-07-0Mar 28, 2013 · N410QX · Bombdr DHC8402SDR QXEA2013032800691Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT BS 509.5. STRINGER CLIP AT STA 509.5 STR 24S WAS REMOVED IAW SRM 51-42-05-02-01, REV 12. PRIOR TO REMOVAL STRINGER CLIP 24S AT STA 509.5 WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. MATCH DRILLED TO ACFT IAW Mar 28, 2013 · N410QX · Bombdr DHC8402SDR QXEA2013032800690Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT STA 489.5. REMOVED STRINGER CLIP 24S AT STA 489.5 IAW Q400 SRM 51-42-05-02-01 REV 12. FOUND STRINGER CLIP 24S AT STA 489.5 TO BE OUT OF LIMITS PRIOR TO REMOVAL IAW SRM 53-30-03-00-01, REV 12. MATCH DRILLED TO ACFT IAW SRM REVMar 28, 2013 · N410QX · Bombdr DHC8402SDR QXEA2013032800689Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT STA 469.5. STRINGER CLIP 24S AT STA 469.5 IS CORRODED OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. STRINGER CLIP WAS REMOVED IAW SRM REV 12, 51-42-05-02-01, RECEIVED NEW PART AND MATCH DRILLED TO AC IAW SRM REV 12, 51-40-07-0Mar 28, 2013 · N410QX · Bombdr DHC8402SDR QXEA2013032800688Stringer Clip · corrodedSTRINGER 24S CLIP IS CORRODED AT STA 449.5. STRINGER CLIP AT 24S STA 449.5 IS CORRODED OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. STRINGER CLIP WAS REMOVED IAW SRM REV 12, 51-42-05-02-01. RECEIVED NEW PART AND MATCH DRILED TO AC IAW SRM REV 12, 51-40-07-0Mar 28, 2013 · N410QX · Bombdr DHC8402SDR SWAA2013040414481Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.Mar 28, 2013 · N612SW · Boeing 7373H4SDR SWAA2013041714899Attach Fitting · crackedATTACH CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.Mar 27, 2013 · N374SW · Boeing 7373H4SDR UALA2013032801989Attach Bracket · missingAFT GALLEY OXYGEN BOTTLE BRACKET LATCH MISSING. REPLACED BRACKET AND WALK AROUND O2 BOTTLE.Mar 27, 2013 · N589UA · Boeing 757222SDR DALA13014299233Attach Angle · crackedEMPENAGE LT SIDE BS 1520 VENT BOX FORWARD OF INTERIOR UPPER LOUVER VERTICAL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM 51-30-00, PG 1, VOL II.Mar 27, 2013 · N933DN · Doug MD9030SDR EE4Y2013032700037Tee Fitting · crackedUPPER FUSELAGE AFT PRESSURE BULKHEAD TEE BETWEEN L15 AND 17L, AT Z=14 AND Z=24 TEE CRACKED. REPLACED PRESSURE BULKHEAD TEE SECTION IAW S/B A53-232 ACCOMPLISHMENT INSTRUCTIONS OPTION II CONDITION 2, FIG 4, REV 2, DATE APRIL 28,95.Mar 27, 2013 · N930CE · Doug DC933FSDR SWAA2013040914557Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 1006, STR 15R. REMOVED AND REPLACED CLIP IAW SRM.Mar 26, 2013 · N524SW · Boeing 7375H4SDR EE4Y201303270040Fitting · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT, BS 237, ON L24R, FRAME AREA AFT FITTING CRACKED. REPLACED, FRAME FITTING IAW SRM 51-01 PARA 2D.Mar 26, 2013 · N930CE · Doug DC933FSDR ASAA2013032594538Stringer Clip · gougedFWD CARGO BS 480, STR 22L, STRINGER CLIP GOUGED R & R STRINGER CLIP IAW SRM 51 40 02 0G 0.Mar 25, 2013 · N764AS · Boeing 7374Q8SDR ASOA2013041703401Attach Fitting · damagedUPON REMOVAL OF BS 280 BEAM AT RBL 9 (OTBD LOCATION) CLIP. FOUND TO HAVE ELONGATED HOLES. REMOVED CLIP FROM OTBD OF RBL9 IAW SRM 51-42-20-001-001-A01, 51-42-22-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE OTBD OF RBL9 IAW SRM 51-42-20-0Mar 25, 2013 · N133EV · Cndair CL6002D24
Back to JASC 5340