JASC 5330

Service difficulty reports · 79,329

Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330'
  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 SWAA2019120939402Bear Strap · crackedPASSENGER CABIN FORWARD OF R1 DOOR CUTOUT BEAR STRAP CRACKED AT BS. 294, BETWEEN STR. 8R TO STR. 9R. / REPAIRED BEAR STRAP IAW EA AND EA.Nov 8, 2019 · N7863A · Boeing 7377Q8SDR R61A2019112480330Doubler · corroded***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR19-20 STR26-27L, ANTENNA INTERNAL DOUBLER FOUND CORRODED. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.Nov 8, 2019 · N656RW · Emb ERJ170100SESDR AALA201911139019Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT HAND FUSELAGE EXTERIOR SKIN AT BS 917 BETWEEN S21L AND S22L AT THE LAVATORY VENT AREA. REPAIRED SKIN PER EA 299998.Nov 8, 2019 · N860NN · Boeing 737823SDR DALA2019111286599Doubler · corrodedSHIP 6715 CORROSION ON DOUBLER OF AFT LAVATORY ACCESS PANEL. CORRECTIVE ACTION:SUMMARY OF NRC 00442 (CORROSION LEVEL 2):DOUBLER OF AFT LAVATORY ACCESS PANEL WAS REPLACED PER B757-200 SRM. (1350565)Nov 8, 2019 · N6715C · Boeing 757232SDR C77A2020012700019Finger Doubler · corrodedCORROSION OR DAMAGE HAS BEEN DISCOVERED ON THE FWD CARGO (FWD P/N 170-67115-001) AND/OR (AFT P/N 170-67115-002) FINGER DOUBLERS ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS AS PSES, COMPASS HAS CLASSIFIED REPLACEMENNov 7, 2019 · N617CZ · Emb ERJ170200LRSDR SWIA2019122747191Skin · crackedSKIN IS CRACKED AT THE TRU DOOR AFT LATCH. CRACK IS APPROX 3/4 INCH LONG. REMOVED AND REPLACED SKIN AT THE TRU DOOR AFT LATCH. BS 169 AND 173.5 IAW SRM. AND DRAWING.Nov 7, 2019 · N879AS · Cndair CL6002B19SDR C77A2019110700002Finger Doubler · damagedCORROSION OR DAMAGE HAS BEEN DISCOVERED ON THE FWD CARGO (FWD P/N 170-67115-001) AND/OR (AFT P/N 170-67115-002) FINGER DOUBLERS ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS AS PSES, COMPASS HAS CLASSIFIED REPLACEMENNov 7, 2019 · N617CZ · Emb ERJ170200LRSDR V6NA20191230604Skin · corrodedAT INSPECTION DETERMINED SKIN CORROSION AT UPPER FORWARD TCAS ANTENNA. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE.Nov 6, 2019 · N777QL · Lear 45LEARSDR V6NA20191230602Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED CORROSION ON SKIN AFT OF LEFT MAIN LANDING GEAR WELL. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE PER FAA DER.Nov 6, 2019 · N777QL · Lear 45LEARSDR V6NA2019123010601Skin Panel · corrodedAT SCHEDULED INSPECTION DISCOVERED CORROSION FORWARD OF PANEL 510AL. REMOVED CORROSION. DETERMINED REMAINING THICKNESS BY ULTRASONIC INSPECTION. REMAINING THICKNESS DETERMINED TO BE ACCEPTABLE.Nov 6, 2019 · N777QL · Lear 45LEARSDR SWIA2019121846956Skin · corrodedSKIN CORROSION LOCATED IN MULTIPLE LOCATION ON EXTERNAL FUSELAGE SKIN BETWEEN FS 559.00+80.00 AND FS559.00+112.00 @ STGR 24R COMMON TO BEAM, AFT BL 17.50. MARKED WITH RED TAPE. (C-CHECK) RO 12/14/2019 REPAIRED FUSELAGE SKIN CORROSION IAW REO. REPAIRED FAIRINGNov 6, 2019 · N437SW · Cndair CL6002B19SDR REXA2019116601701Skin · damaged"DAMAGE T: CREASE ON FUSELAGE SKIN BTW STA FS:280 AND FS:295 STGR 17RH TO 18RH . (FUS) "SUMMARY: CREASE ON FUSELAGE SKIN BTW STA FS:280 AND FS:295 STGR 17RH TO 18RH,THE DAMAGE MEASURES L:5.600"",W:0.300"" AND D:0.027"" WAS REPAIRED AND WAS FOUND WITHIN LIMITNov 6, 2019 · N607LR · Cndair CL6002D24SDR R61A2019112461327Skin · none***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** "MAJOR REPAIR" FWD FUSELAGE EXTERNAL SKIN FR19-20 STGR23-24, 17 UNRECORDED FLUSH RIVETS FOUND. FWD FUSELAGE SKIN REPAIRED IAW SRM 53-10-01 REPAIR 12P. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.Nov 6, 2019 · N656RW · Emb ERJ170100SESDR R61A2019112461325Skin · dented***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** FWD FUSELAGE EXTERNAL SKIN FR1-2, STGR20-22L, 4 PROTRUDING DENTS AT RVSM AREA. 4 EA DENTS IN LH RVSM AREA WERE FOUND TO BE WITHIN LIMITS IAW ETD2019-170-157004. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMNov 6, 2019 · N656RW · Emb ERJ170100SESDR 7C7A2019110600517Skin · dentedDENT WITH SCRATCHES IN FUSELAGE SKIN 85311825-101 BEYOND MFG. LIMITS 2.0X1.6X0.11 SCRATCHES MAX DEPTH OF 0.01Nov 6, 2019 · N880EA · Dhav DHC8106SDR 2020F00062Skin Panel · dentedDENT ON FORWARD FUSLEAGE BEYOND ALLOWABLE LIMITS LOCATED BETWEEN FS280 TO FS295 AND STR24R TO STR25R.Nov 6, 2019 · N54EA · Cndair CL6002C10SDR SWAA2022040653506Skin · corroded***CORROSION*** AROUND MAJORITY OF FASTENERS THROUGH FUSELAGE SKIN EXTERNALLY; COVERED BY DORSAL FIN FROM STA 867 TO STA 1006; APPROXIMATELY STR 2R TO STR 2L. / REPAIRED FUSELAGE SKIN B.S 867-1006 STR 2R-2L IAW EA 1-753-36041 REV IR AND ATS ER 19-05567 REV IRNov 5, 2019 · N461WN · Boeing 7377H4SDR CALA2019111101943Skin · crackedREF LP 3522239 LIGHTNING STRIKE DEFERRED PER OPERATIONAL LIMITS WILL NEED SRM REPAIR INSTALLED HFEC PERFORMED REF STEP B (2) PERFORMED STEPS A,B AND C OF SRM 53-00-01 REPAIR 4 PARA 4, NEED INSPECTED AREA PER SRM 53-00-01 REPAIR 4 PARA 4 STEPS A, B,C. HFEC C/W Nov 5, 2019 · N78008 · Boeing 777224SDR DALA2019110766461Skin · canning(LOG 1346798) DURING INSPECTION FOUND OIL CANNING ON FUSELAGE SKIN, 6 INCH ABOVE S24L BTW STA 188 TO 196. REPAIR WAS ACCOMPLISHED PER ERA 582765-14 REV. ORIG. AND ETI-37-19-340 REV. 2.Nov 5, 2019 · N3767 · Boeing 737832SDR 21GA20191107008Skin · crackedLOWER FUSELAGE SKIN SECTION 43 SKIN CRACKED AT STRINGER 38R AT BS786.Nov 5, 2019 · N999YV · Boeing 767241SDR 21GA20191107003Skin · crackedRH R1 DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED 4” LONG AT STATION 347 BETWEEN STRINGERS 19 & 20 R.Nov 5, 2019 · N999YV · Boeing 767241SDR DXTR2019110501Skin · chafedWING ANTI-ICE CROSS FEED VALVE BOLT IS CONTACTING CABIN SKIN, REPAIRED IAW CESSNA MAJOR REPAIR SR-680A-ATA53-22175. NDT PERFORMED BY TOLEDO JET CENTER, LLC. CRS# 2TJR420B ON WORK ORDER TOL80793.Nov 5, 2019 · N508QS · Cessna 680ASDR SWAA2022041965584Skin · corrodedT996953 CORROSION ON SKIN AT BS-907+10'; 2.5' ABOVE STR-22L AT LAV TANK VENT HOLE ; / B><U>ACTUALSLOADER; 24-APR-2021 11:51:13</U></B><BR>T996953 CORROSION ON SKIN AT BS-907+10'; 2.5' ABOVE STR-22L AT LAV TANK VENT HOLE<Nov 4, 2019 · N562WN · Boeing 737790SDR R61A2019112401329Skin · damaged***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** "MAJOR REPAIR" CF I EXTERNAL SKIN FR23-24 STGR16-17L, UNRECORDED RIVET FOUND. REPAIRED SKIN IAW ETD2019-170-158221. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.Nov 4, 2019 · N656RW · Emb ERJ170100SESDR 9WGA2019110401Skin · corrodedCENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 50L F.S.1621-1721. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 52 F.S. 1561-1601. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 48R F.S.1561-1581. CENTER CARGO INTENov 4, 2019 · N435KD · Doug MD11FSDR SWAA2019112039000Skin · delaminatedPANEL 191D OUTER SKIN DELAMINATED, BETWEEN BS. 482A TO BS. 540. / REPAIRED PANEL 191D OUTER SKIN IAW SRM.Nov 3, 2019 · N7846A · Boeing 73776NSDR SWAA2019110538611Skin · corrodedR/H SIDE FUSELAGE SKIN INNER SURFACE AROUND HOLES CORRODED STA 667, RBL 70. / REPAIRED SKIN IAW EA.Nov 3, 2019 · N7822A · Boeing 73776NSDR SWAA2019110538610Skin · corrodedFUSELAGE INNER SURFACE OF SKIN AROUND HOLES CORRODED AT BS. 667, LBL 70. / REPAIRED SKIN PER EA.Nov 3, 2019 · N7822A · Boeing 73776NSDR UIEA2019110105827Skin · bulgedBULGE ON THE RH SIDE FUSELAGE SKIN AT STA 730, BETWEEN S-43R TO S-44R. (<P>REPAIRED THE DAMAGED AREA IAW SRM 53-00-01-2R-1 REPAIR 1 REV. 43 AND EI NO. T2019A53M-4039 REV. 1. REPAINTED THE RE-WORKED AREA IAW AMM 51-24-11-477-083 REV. 96. JOB COMPLETED AND CONDINov 2, 2019 · N747BC · Boeing 7474J6SDR SWIA2019121846958Skin · corrodedAFT LAVATORY EXTERNAL SURROUND STRUCTURE CORRODED IN MULTIPULE LOCATIONS AROUND FASTENERS BETWEEN FS559.00+80.00 AND FS559.00+112.00 AND BETWEEN STGR20R AND STGR23R. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETE AND Nov 1, 2019 · N437SW · Cndair CL6002B19SDR SWIA2019121746915Skin · corrodedFUSELAGE OUTER SKIN HAS NUMEROUS AREAS OF CORROSION BETWEEN FS 559 TO FS 559+64 STR 26L TO STR 26R (C-CHECK) RO 12/14/2019 REMOVED CORROSION BETWWEEN FS 559 TO FS 559 +64 STR 262 TO STR 26R.WITH IN ALLOWABLE LIMITS IAW BOMBA REO.Oct 31, 2019 · N927SW · Cndair CL6002B19SDR ASAA2019112613441Skin · dentedFOUND A/C DAMAGE FROM STAIRS APPROX 6FT AFT OF LWR STATIC PORT L/H SIDE APPROX 12" ABOVE LAP JOINT. GROUNDED - YES. (RESOLVED ON W/O: 419860 TASKCARD: N/R-00009 ) REPAIRED DAMAGE 6FT AFT OF LWER STATIC PORT LH SIDE APPROX 12" ABOVE LAP JOINT IAW ASA EA 800 53EOct 31, 2019 · N551AS · Boeing 737890SDR CALA2019110301894Skin · damagedEXISTING FASTENER HOLES AT FR20-21 S41R-42R ARE VISUALLY OUT OF ROUND. REF HAECO NR 9292317. DTA REQUIRED. INTERIM REPAIR ACP PER ECRA 5331-02494 PART 1 STEP 1 INTERIM REPAIR INSTRUCTIONS. REF PART 1 STEP 2, ACCOMPLISH A PERMANENT REPAIR AT THE CENTER FUSELAGEOct 31, 2019 · N844UA · Airbus A319131SDR SWAA2022032321509Skin · corrodedSUPPLEMENTAL INFORMATION: FOLLOWING REMOVAL OF LH PICKLE FORK ASSY. 65AA0004- 1593; CORROSION WAS FOUND ON INNER SURFACE OF 144A3311-51 FUSELAGE SKIN AROUND 4 EACH FASTENER HOLES; BS 665-669; WL 195-200; LBL 70. ( CORROSION DOCUMENTED IN FRR-9 UNDER BOEING AOGOct 30, 2019 · N7865A · Boeing 7377Q8SDR RAIA2019112830046Skin · gouged#1 ENGINE PYLON INSIDE ACCESS PANEL 414DB FUSELAGE SKIN IS GOUGED BETWEEN FRAME 67 & 68- REMOVED #1 PYLON BLEED VALVE TO F.O.M. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, DRILLED-UP, ALODINE & PRIMED NEW DOUBLER. FABRICATED FILLER, LOCATED, DRILLED, INOct 30, 2019 · N14153 · Emb EMB145XRSDR IPXA2019111328936Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT STR. 15 AND BETWEEN X=46.5 TO X-80.REPAIRED CENTER WING BOX UPPER SKIN AT STR. 15 AND BETWEEN X=46.5 TO X=80 IAW VT-SAA EA 011-5730-01-A7945 REV. I/R AND UPS EO MD11-5730-74604-A. (MINOR)Oct 30, 2019 · N252UP · Doug MD11FSDR IPXA2019111328934Skin · corrodedINSPECTION TYPE:2CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN STA. XCW=101 & XCW=118 AT APPROX. FUSELAGE STA. 1256.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN STA. XCW=101 & XCW-118 AT STRINGER 12 IAW VT-SAA EA 011-5730-01-A7944 REV. IR AND UPSOct 30, 2019 · N252UP · Doug MD11FSDR SWAA2019110438527Skin · corrodedFUSELAGE SKIN AROUND 4 EACH FASTENER HOLES CORRODED BETWEEN BS. 665 TO BS. 669, RBL 70. / REPAIRED SKIN IAW EA.Oct 30, 2019 · N7865A · Boeing 7377Q8SDR DALA2019103106314Skin · crackedRH FUSELAGE SKIN S-13AR BETWEEN FRAMS 1629-1678 FOUND 4.7 INCHS CRACK. REPAIRED PER SERM 53-80-01. (LP 1338626)Oct 30, 2019 · N834MH · Boeing 767432ERSDR DALA2019103106313Skin · crackedRH FUSELAGE SKIN S-13AR BETWEEN FRAMS 1629-1678 FOUND 4.7 INCHS CRACK. REPAIRED PER SRM 53-80-01. (LP 1338623)Oct 30, 2019 · N834MH · Boeing 767432ERSDR DALA2019103106312Skin · crackedRH FUSELAGE SKIN S-13AR BETWEEN FRAMS 1629-1678 FOUND 4.7 INCHS CRACK. REPAIRED PER SRM 53-80-01. (LP 1338621)Oct 30, 2019 · N834MH · Boeing 767432ERSDR HNAA2019120460345Skin · damagedCOULD NOT LOCATE ORIGINAL - FUSELAGE SKIN HAS A BURN MARK AT FR63 BETWEEN STR 20R-21R.....INSTALLED FILLER AND REPAIR DOUBLER IAW EMB 145 SRM 53-31-01, ITEM 4, FIG. 204, SHEET 1 AND EO1-53-19-0500Oct 29, 2019 · N626AE · Emb EMB145LRSDR CALA2019110101876Pressure Panel · crackedLH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. CRACKS IN PANEL CUT OUT AREA HOLE 13. CONTACT ENGINEERING INSTRUCTIONS AND REPAIR BE FORE NEXT FLIGHT. SUPPORT TASK, AD 2018-06-04 PER HAECO LCQ NR 9 296309 REFERENCE LOG PAGE 3692863. INTERIM REPAIR ACCOMPLISHED PEROct 29, 2019 · N452UA · Airbus A320232SDR CALA2019110101875Pressure Panel · crackedLH SIDE PRESSURE PANEL BETWEEN FR 35-36 HOLES 3,4,6,7,20 AND 21 CRACKED IN TITANIUM ANGLE. HOLE 7 CRACKED IN CORNER FITTING. CON TACT ENGINEERING REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXDT FLI GHT. CRACKS LIMITED TO CUTOUT AREA. SUPPORT TASK, AD 2018-06-04 PEOct 29, 2019 · N452UA · Airbus A320232SDR CALA2019110101873Pressure Panel · crackedLH SIDE PRESSURE PANEL BETWEEN FRAME 35-36 CRACKS IN LH SIDE PRE SSURE PANEL OUTSIDE CUTOUT AREA FR35-36 HOLES 2,3,4,5,14,17, 20, 21,25 & 25.ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFOR E FLIGHT. CRACKS LIMITED TO CUTOUT AREA. SUPPORT TASK AD2018-06- 0Oct 29, 2019 · N452UA · Airbus A320232SDR CALA2019110101874Pressure Panel · crackedLH PRESSURE PANEL BETWEEN FRAME 35-36. ASSIGN AND ACCOMPLISH REP AIR PER EA 5330-05216 OP 2 BEFORE NEXT FLIGHT. SUPPORT TASK, AD 2018-06-04 PER HAECO LCQ 9296082 INTERIM REPAIR ACCOMPLISHED PER ECRA 5331-02493 PART 1. NEED TO ACCOMPLISH THE PERMANENT REPAIR ATOct 29, 2019 · N452UA · Airbus A320232SDR ABXA2019103128163Skin · corrodedCORROSION ON FUSELAGE SKIN AT FUSELAGE STATION 1330, STRINGER 33L. THE SKIN WAS REPAIRED, THE AIRPLANE WAS GROUNDED.Oct 28, 2019 · N749AX · Boeing 767232SDR CALA2019102901854Skin · dentedDENT AT BOTTOM OF FUSELAGE JUST AFT BEHIND NLG - LP 3133264 NEED S RE-EVALUATION SUPPORT TASK PER HAECO LCQ NR 9292021 GENERATED BY V061588 DENT LOCATED BOTTOM OF FUSELAGE JUST AFT BEHIND NLG AT FR20-21, STR 41R-42R. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-1Oct 28, 2019 · N844UA · Airbus A319131SDR RAIA2019103170001Skin · corrodedAFT FUSELAGE EXTERIOR SKIN HAS CORROSION UNDER AND AROUND DATA PLATE BETWEEN FRAME 80 & 81 BETWEEN STR 20 & 21 LT- REMOVED CORROSION FROM THE AFT FUSELAGE EXTERNAL SKIN BETWEEN FR80-FR81 ON THE BELLY & REMOVED DATA PLATES. AWAITING TECHNICAL DISPOSITIOct 27, 2019 · N14153 · Emb EMB145XRSDR SWAA2019112739198Skin · corrodedPRESSURE BULKHEAD WEB CORRODED BETWEEN BS. 1016 TO BS. 1040, BETWEEN STR. 24L TO STR. 25R, LOWER AREA. / REPAIRED SKIN PER EA.Oct 26, 2019 · N765SW · Boeing 7377H4
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