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 DALA2020012170440Skin · corrodedLOWER FUSELAGE HAD CORROSION ON THE SKIN BUTT JOINT AND DRAIN TUBES BS 1720 TO 1725, STRINGERS 26R & 29L. REPAIRED THE LOWER FUSELAGE SKIN IAW ER/A 584094-14, REV ORIGINAL.Jan 16, 2020 · N541US · Boeing 757251SDR DALA2020012000403Skin · crackedDURING INSPECTION FOUND CRACK ON EXTERNAL POWER RECEPTACLE CUTOUT FWD SIDE. AREA ON EXTERNAL POWER RECEPTACLE WAS REPAIRED PER SRM 53-10-15 REPAIR 5.Jan 16, 2020 · N3768 · Boeing 737832SDR SIMA2020012016004Skin · dentedREF AML 4212922 /2 TDMI 055T5310 LH FUSELAGE SKIN DENT BETWEEN FR 11-12, STR 4L-5L ERS-EJ-53DF-2993 PTC PERMANENT REPAIR.-C/A-INSTALLED REPAIR DOUBLER AND FILLER ON LH FUSELAGE SKIN BETWEEN FR 11-12, STR 4L-5L IAW ERS-EJ-53DF-2993R3 PTC PERMANENT REPAIR..Jan 16, 2020 · N255NN · Emb ERJ170200LRSDR CALA2020011900189Skin · gougedSUPPORT TASK P/R GOUGE IN LEFT FUSE SKIN APPROX STA 1075 FWD OF APU CUT OUT. REF NRS 2664N1125 DAMAGE AT LT FUSE SKIN AT STA 1075 FOUND TO BE OUT OF LIMITS DEPTH .008 W.269 L.837 GOUGE F5081 REPAIRED USING 2024 T3 .080 LOT NR EL-6205/113210 FILLER AND 2024T3.0Jan 16, 2020 · N24729 · Boeing 737724SDR SIMA202001176001Skin · dentedAIRCRAFT ARRIVED WITH TDMI 676T5345 TO REPAIR A DENT TO THE RH CENTER FUSELAGE BETWEEN FR 15-16 AND STGR 12R-13R-C/A-PERFORMED PERMANENT REPAIR ON DENT ON RH CENTER FUSELAGE BETWEEN FR 15-16 AND STGR 12R-13R IAW EMB 145 SRM 53-21-01 FIGURE 202. REPAIR MATERIALJan 16, 2020 · N676AE · Emb EMB145LRSDR SWIA2020030348946Skin · corroded*FS 559.00+112 TO 574 STR 25 LH TO 25 RH EXTERNAL SKIN AND FASTENERS HAS CORROSION AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED EXTERNAL SKIN FS 559.00+112 TO 574 STR 25L TO 25R REF REO. COMPLIED WITH SKYWEST TASK CARD.Jan 15, 2020 · N440SW · Cndair CL6002B19SDR SWIA2020030348945Skin · corroded* FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FASTENERS HAS CORROSION IN AREA (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND REPAIR TO CORROSION ON FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FASJan 15, 2020 · N440SW · Cndair CL6002B19SDR SWIA2020021848611Skin · dentedLH FUSELAGE SKIN JUST AFT OF PANEL 121AL HAS A DENT. (C-CHECK) RO 2/14/2020 THE DENTED AREA HAD MISSING MATERIAL AND COULD NOT BE DRESSED BACK TO CONTOUR. REMOVED AND REPLACED THE LH FUSELAGE NOSE HYDRAULIC BAY SURROUND SKIN PANEL REF REO AND DWG. SEE CONTJan 14, 2020 · N689CA · Cndair CL6002D24SDR R61A202001220048Skin · dented***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK COMPLETION*** DENT OUTER SKIN LOCATED BETWEEN FR 21-22 STGR 17L-18L. FOUND ACCEPTABLE AS PERMANENT ALLOWABLE DAMAGE IAW ETD2020-170-001571. A/C REMAINS OUT OF SERVICE FOR HEAVU CHECK COMPLETION.Jan 14, 2020 · N747YX · Emb ERJ170200LRSDR CALA2020011900152Skin · corroded(SUPPORT TASK) EXTERIOR SKIN FOR LAV EXHAUST VENT SHOWS SIGNS OF CORROSION. REFER TO N/R: 9827064. REMOVED DAMAGE AT LAV EXHAUST VENT BETWEEN FR69-70 RT, MAX MATERIAL LOSS .010, MAX ALLOWED .004 AND IS OUT OF LIMITS IAW SRM 53-41-11-283-006, REMOVED AND REINSTJan 14, 2020 · N470UA · Airbus A320232SDR CALA2020011900151Skin · damagedRAMP REPORTED DAMAGE TO AFT CARGO A/C CUTOUT INSPECTED AREA FOUND THREE AREAS OF DAMAGE ON FWD SIDE OF AFT CARGO DOOR CUTOUT. LOWER DAMAGE IS APPROX 24 INS FROM BOTTOM OF CUTOUT, 1.5 INCHES LONG AND DENTED IN APPROX 1/16 INCH. MID DAMAGE IS APPROX 31 INS FROM Jan 14, 2020 · N68802 · Boeing 737924ERSDR R61A202001170033Skin · out of limits***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK*** EXTERNAL FUSELAGE SKIN, UNRECORDED BLENDOUT FOUND AT SKIN FR3+12" & 2" BELOW STGR12R RVSM AREA. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW ETD2020-170-001206. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLJan 14, 2020 · N725YX · Emb ERJ170200LRSDR SWAA2020012040615Skin · corrodedEXTERIOR FUSELAGE SKIN CORRODED AT BS 350, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER SRM AND EA.Jan 13, 2020 · N746SW · Boeing 7377H4SDR DXTR2020011301Skin Panel · chafedWIMG ANTI-ICE VALVE UPPER STUDS CHAFING FUSELAGE, REPAIRED IAW CESSNA REPAIR SR-680A-ATA53-22175.Jan 13, 2020 · N543QS · Cessna 680ASDR FDEA2020011320119Skin · corrodedREFER TO WRI #53108830 W/O #00076033 TO COMPLY WITH EA # T 1-5310-T0349168 A P2 TITLE : FUSELAGE Ï¿½ MAINFRAME Ï¿½ SKIN CORROSION ADJACENT THE VHF ANTENNA STATION 1721 Ï¿½ 1741 LONGERON 50L Ï¿½ 50R, BLENDOUT REPAIR FUSELAGE - STATION 1721 - 1741 LONGERON 5Jan 12, 2020 · N576FE · Doug MD11FSDR DALA2020011500292Skin · corrodedEMPENNAGE LT SIDE EXTERIOR SKIN HAS CORROSION JUST FWD OF APU INLET DOOR BS 1780. CORRECTIVE ACTION: REMOVED DAMAGED / CORRODED PARTS FWD STRAP / AFT STRAP, UPPER, LOWER ANGLES FABRICATED TREATED, PRIMED & TOPCOATED NEW PARTS. INSTALLED NEW PARTS SEALED AREAS Jan 12, 2020 · N541US · Boeing 757251SDR CALA2020011300138Skin · dentedDENT ON FRAME 75 SRT 31 R. -SUPPORT TASK. PER HAECO LCQ REF. 929 4269. GENERATED. HAECO TECHNICIAN AND QC REPAIRED DENT BY CUTTING O UT DENT 1.6"L X 1.5"W AT FR75 STR 31R AND INSTALLING DOUBLER IAW SRM 53-00-11-300-042 FIG 001 PG10. SRI 53-0011-205-052 INSPECTJan 12, 2020 · N439UA · Airbus A320232SDR CALA2020011300140Skin Panel · chafedB757 53-3-0587 SUPPORT BRACKET CHAFING INTO FUSELAGE SKIN PANEL STA 1795 STR 17R AS VIEWED THRU ACCESS 311AL. RL0105 REF. ST. EN GINEERING N/R 0084140 FOUND FUS SKIN OUT OF LIMITS AT STA 1795 STRINGER 17R IAW B757-3 00 SRM 53-80-70-R4,.50" CRACK. CUT OUT DAMAGJan 12, 2020 · N75853 · Boeing 757324SDR FDEA202001110158Skin · damagedTHE LH SIDE OF THE FUSELAGE FROM STA 510-515 2"-4" DOWN FROM STR 26L HAS SEVERAL DEEP PITS FROM LIGHTNING STRIKE. REPAIRED DAMAGE IN FUSELAGE SKIN CAUSED BY LIGHTNING STRIKE. INSTALLED DOUBLER REPAIR PER EA F-5330- T0351859.Jan 11, 2020 · N926FD · Boeing 7572S7SDR SWIA2020031049094Skin · dentedADM#3845 - DENT FOUND ON RH SIDE OF FUSELAGE SKIN PANEL APPROXIMATELY FS 275.8 BETWEEN STGR 22R AND 23R. (C CHECK) RO 3/7/2020 HAND DRESSED TO REFORM TO ORIGINAL CONTOUR TO DISCREPANT SKIN, ENSURED NO OIL CANNING OCCURRED POST REWORK COMPLIED WITH REO. SEJan 11, 2020 · N905EV · Cndair CL6002B19SDR ASOA202002193015Skin · corrodedDURING C CHECK INSPECTION FOUND CORROSSION ON FUSELAGE SKIN AT AFT RADIO ALTIMETER AT FRAME 65 STRINGER 21L-21R. MAINTENANCE REPAIRED I/A/W ETD2020-145-001101Jan 9, 2020 · N11107 · Emb EMB145XRSDR SWIA2020021148428Skin · chafed*LOWER FUSELAGE SKIN CHAFED EXTERNALLY FROM CONTACT WITH FAIRING FASTENER AT APPROX FS969.5 STRINGER 27. (C-CHECK) RO 2/07/2020 REPAIRED LOWER SKIN PANEL AT FS969.5 PER REO.Jan 9, 2020 · N746SK · Cndair CL6002C10SDR DALA2020011300208Skin · crackedUPPER FUSELAGE APU INLET CUT OUT FWD LWR CORNER FOUND CRACKED AT STA 1725 S-7R. C/A UPPER FUSELAGE AT STA1725, S-7R APU INLET CUT OUT FWD LWR CORNER CRACKED SKIN REPAIRED AS PER B767-400 SRM53-80-01 REPAIR 5 RELEASE 59.00 19DEC19. THIS IS CATEGORY B REPAIR,INSJan 9, 2020 · N837MH · Boeing 767432ERSDR DALA2020011300207Skin · crackedHFEC INSPECTION FOUND 01EA CRACK APPROX 0.100" IN LENGTH ON THE FUSELAGE SKIN APPROX 0.150" BELOW THE 6TH STRINGER-ATTACH RIVET ALONG S-13AL AFT OF STA 1654.50 AS MARK PER W/C 5330-01229-01A STEP 4. C/A THE FUSELAGE SKIN APPROX 0.150" BELOW THE 6TH STRINGER-ATJan 9, 2020 · N837MH · Boeing 767432ERSDR SWIA2020041050077Skin · crackedRIGHT SIDE FUSELAGE SKIN FOR NOSE GEAR CUT-OUT RADIUS IS CRACKED. (C-CHECK) RO 4/9/2020 RIGHT SIDE FUSELAGE SKIN AT FS 235 FOR NOSE GEAR CUTOUT ACCOMPLISHED REF CRJ200 IAW REO.Jan 8, 2020 · N975SW · Cndair CL6002B19SDR RAIA2020012908005Skin · crackedAFT FUSELAGE EXTERIOR SKIN HAS CRACK INDICATION EXTENDING FROM RIVET AT FRAME 79 @ STR 3 LH- REMOVED RIVET FOR NDI INSP. PERFORMED HF EC INSPECTION OF INDICATED LOCATION, CRACK FOUND AND END MARKED. CUT HOLE IN AFT SKIN AT FR 79, STR 3 LH TO REMOVE CRJan 8, 2020 · N835HK · Emb EMB145LRSDR R61A202001280103Skin · corroded***AIRCRAFT IS IN HEAVY CHECK*** CORROSION ON SKIN PANEL (INTERNAL) AROUND RIVETS BTW FR 76 BTW STR 29L-29R. REPAIRED SKIN PANEL IAW ETD2020-170-001065. ***AIRCRAFT REMAINS IN HEAVY CHECK***Jan 8, 2020 · N635RW · Emb ERJ170100SESDR R61A202001250074Finger Doubler · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO DOOR FWD FINGER DOUBLER HAS CHAFFE DAMAGE AT FRAME 24. REMOVED AND REPLACED FWD CARGO DOOR FWD FINGER DOUBLER. REF: EMB SRM 51-40-08. RESTORED SURFACE PROTECTION PER SRM 51-23-04, 51-23-05, 51-23-06 CPM 51-25-00.Jan 8, 2020 · N231JQ · Emb ERJ170200LRSDR SIMA202001280007Skin · crackedL/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 78. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.Jan 8, 2020 · N667GB · Emb EMB145LRSDR SIMA202001280006Skin · crackedL/H REAR FUSELAGE II SKIN IS CRACKED AROUND A RIVET AT FR 79. (CRACK APROX 1/4 INCH LONG) -C/A-REPAIRED IAW SRM 53-32-01.Jan 8, 2020 · N667GB · Emb EMB145LRSDR RAIA2020011680004Skin · dentedFWD LOWER BELLY SKIN HAS DENT AT FRAME 25 AT 6 O'CLOCK POSITION- REPAIRED FWD LWR BELLY SKIN AT FR 25.Jan 8, 2020 · N835HK · Emb EMB145LRSDR DALA2020010900166Skin · crackedAFT EXTERIOR FUSELAGE SKIN IS CRACKED EXTENDING FROM RIVET HEAD STATION 1725 STRINGER 7R (VERIFIED WITH HFEC SURFACE SCAN). REPAIRED PER SRM 53-80-01 (LP 1436589)Jan 8, 2020 · N152DL · Boeing 7673P6SDR EE4Y2020010871479Skin · corrodedDURING THE STRUCTURE INSPECTION IT WAS FOUND IN THE AFT CARGO COMPARTMENT AREA WITH SKIN AND STRINGER 28L CORRODED FROM FR73 TO FR81, BTWN S-27L AND S-28R, AND S-28L CORRODED BTWN FR78 AND FR79.THE MENTIONED DAMAGE WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS MEJan 8, 2020 · N965AZ · Emb ERJ190100IGWSDR C77A2020010800001Doubler · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON-CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE I FORWARD CARGO SURROUND LOWER FORWARD FINGER DOUBLER P/N 170-67115-001. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIREJan 8, 2020 · N205NN · Emb ERJ170200LRSDR SWAA2020010701499Doubler · deformedEGPR CUTOUT REPAIR REQUIRES REPLACEMENT DUE TO DEFORMATION / REMOVED AND REPLACED EGPR CUTOUT AFTSIDE BY FABRICATING DOUBLER #1 MADE FROM 7075T6 CLAD LOT# 1376846-2 SURFACE TREATED AND PRIMED IAW SRM 51-20-01-0G-0 AND SRM 53-10-15-2R-4 REPAIR-4Jan 7, 2020 · N563WN · Boeing 737752SDR COEA2020032616801Skin · corrodedWO 209330 NR 200169 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE R/H LOWER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 24-25 BETWEEN STRINGERS 13AR-14R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113811_01...15875 ISSUE A, DATED 3/20/2020.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR COEA2020032615801Skin Panel · corrodedWO 209330 NR 100063 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE R/H LOWER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 23D-24 BETWEEN STRINGERS 16R-17R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113811_01...15875 ISSUE A, DATED 3/20/2020.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR COEA2020032012801Skin Splice · damagedWO 209330 NR 200208 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE SKIN SPLICE IS DAMAGED AT FRAME 42 STRINGER 4-5R. CORRECTIVE ACTION: REPLACED SPLICE WITH FABRICATION.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR COEA2020032011801Skin Panel · corrodedWO 209330 NR 200130 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H UPPER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113648_01...15859 ISSUE A, DATED 3/16/2020.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR COEA2020032010801Skin Panel · corrodedWO 209330 NR 200123 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H UPPER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 8R-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113648_01...15859 ISSUE A, DATED 3/16/2020.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR COEA2020031306801Skin Panel · corrodedWO 209330 NR 200164 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE R/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23C BETWEEN STRINGERS 5AR-6R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-806-A01.Jan 7, 2020 · N801FX · Aerosp ATR72212SDR SWIA2020031049115Skin · dented*EXTERNAL SKIN DENT/GOUGES, 2EA APPROXIMATELY FS1031.00 STGR 22RH JUST AFT OF THE LOW AIR GROUND CONNECT PANEL (MARKED) (C-CHECK) RO 3/6/2020 REPAIRED GOUGES ON EXTERNAL SKIN 2 EA AT APPROX FS1031.00 STGR 22RH JUST AFT OF THE LOW AIR GROUND CONNECT PANEL Jan 7, 2020 · N821SK · Cndair CL6002D24SDR REXA2020020570140Skin · corrodedINITIAL INSPECTION: CORROSION ON EXTERNAL LOWER SKIN OF THE TAILCONE (SM) (FUS) (TCI 300-13) SUMMARY OF NRC. 00105 CORROSION LEVEL 1: CORROSION ON EXTERNAL LOWER SKIN OF THE TAILCONE WAS REMOVED PER CRJ-900 SRM Jan 7, 2020 · N916XJ · Cndair CL6002D24SDR R61A2020011870036Doubler · corrodedWHILE IN HEAVY CHECK FOUND FWD FUSELAGE LH SIDE 5 HOLE DOUBLER AT FR19 HAS CORROSION AT FWD EDGE REMOVED AND REPLACED FWD FUSELAGE LH SIDE 5 HOLE DOUBLER AT FR19 REF SRM 51-40-08 RESTORED SURFACE PROTECTION REF. E175 SRM 51-23-04, 51-23-05, 51-23-06.Jan 7, 2020 · N408YX · Emb ERJ170200LRSDR AALA202002109008Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN AT FR 35 AND S30L. REPAIRED SKIN PER EA 301966.Jan 6, 2020 · N665AW · Airbus A320232SDR CALA2020011000111Skin · chafedB757-53-3-6075 SUPPORT CHAFING INTO AFT FUSELAGE SKIN PANEL STA 1797 STR 17R BLENDED AND CHECKED LIMITS ON CHAFING AT AFT FUSELAGE SKIN PANEL STA 1797 STR 17R; L=2.3 IN W=.70 IN D=.031,ORIGINAL MATERIAL THI CKNESS .056 IN. BLENDED AREA FOUND TO BE OUT OF LIMITJan 6, 2020 · N502UA · Boeing 757222SDR DALA2020010700089Doubler · damagedRAMP REPORTS DAMAGE AT AFT LOWER EDGE OF C1 CARGO DOOR. DAMAGE IS TO EXISTING DOUBLER EDGE. REMOVED, FABRICATED, AND DRILLED UP NEW DOUBLER AND TRIMED DAMAGE IAW B717 SRM 53-20-15-2R-5 OPTION 2. INSTALLED REPAIR DOUBLER PER B717 SRM 53-20-15 FIG 202 OPT. 2. ALJan 6, 2020 · N894AT · Boeing 717200SDR CALA2020010600101Skin · corrodedFOUND CORROSION AROUND LAV VENT AFT FUSELAGE, A/C RIGHT SIDE. VERFIED REPAIR DOUBLER ITEM 1 MATERIAL 0.071 2024T3,P.O# 9747831 , REPAIR FILLERS ITEM 2,3 MATERAIL 0.063 2024T3 P.O# 8546450 AND VERFIED INTERNAL DOUBLER P/N D5348019320401 AS REF TO SRM 53-41 -11-Jan 6, 2020 · N891UA · Airbus A319132SDR ASOA202002193016Doubler · corrodedDURING C CHECK INSPECTION FOUND CORROSSION AND MISSING RIVET ON AFT RADIO ALTIMETER BASE FRAME 68-69 AND STRINGER 21L-21R. MAINTENANCE PERFROMED REPAIR I/A/W ETD 2020-145-001101Jan 5, 2020 · N11107 · Emb EMB145XRSDR CALA2020010600100Skin · dentedRAMP REPORTED DENT FORWARD AT 2L DOOR & MEASUREMENTS APPROX 2 INCHES BY 2 INCHES WITH DEEPEST DEPTH AT 3/16 INCHES LOCATED AT APPROX BODY STA 662 & JUST ABOVE W/L 208 BEFORE STRINGER REMOVED DADO PANEL TO INSPECT INTERNALLY, NOTE STRINGER BENT & E VIDENCE OF CJan 5, 2020 · N77867 · Boeing 75733N
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