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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2021060101230Skin · corrodedCORROSION DAMAGE FOUND DURING PERFORMING INSPECTION PER SB 747-53A28.78 ON INNER SURFACE OF FUSELAGE SKIN(<P>ACCOMPLISHED EI NO. T2021A53M-1437 REV.3</P><P>COND CK NORMAL.</P>)SDR SWAA2021070178427Access Panel · crackedCRACK DOOR CUT OUT COVER ACCESS FWD ENTRY AT BS 304 AT PASSENGER CABIN . REPLACED COVER ACCESS LOCATED DOOR CUT OUT FWD ENTRY AT BS 304 AT PASSENGER CABIN IAW B737-700 SRM:51-40-02 AND 51-10-02 ITEM 9.SDR FXGA202105282123Skin · cracked6-8 INCH CRACK @ STA 699-704 APPX. RBL 24. REPAIR OF SKIN DAMAGE CAUSED BY CARGO LOADING/UNLOADING. REPAIR DAMAGE TO FUSELAGE SKIN @ STA 699-704 RBL 24 PER STS ENGINEERING AUTHORIZATION 81-2021-039.SDR DALA2021060102985Skin · crackedSHIP 685 CRACKED INNER SKIN PROYECTION STA 1653 ON R4 ENTRY DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00825: INNER SKIN PROYECTION STA 1653 ON R4 ENTRY DOOR WAS REPAIRED PER ER/A: 591688-14 REV. ORIGINAL. (1822606)SDR SIMA20210527007Skin · crackedR/H FUSELAGE SKIN HAS A CRACK APROX 1/2 INCH LONG AT FR 75 BETWEEN STRS 1R AND 3R-C/A-REPAIRED RH FUSELAGE SKIN AT FR75 BETWEEN STR 1R AND 3R IAW SRM 53-31-01. ENTERED INTO DT # DT-EM-53-1367 AND DTEM-53-1368.SDR JJBA20210527001Skin · corrodedCORROSION ON LOWER REAR FUSE 1 SKIN, BTW FR 66-70 AND BTW STR 21L-21R, UNDER ANTENNA RADIO ALTIMETER. RADIO ALT. ANTENA 2 AFT EXT DOUBLER REMOVED FOR ACCESS TO CORROSION. DAMAGED SECTION OF FUSE SKIN REMOVED. ON LOWER REAR FUSE 1 SKIN BTW FR 68-70 AND BTW STR SDR SIMA20210527004Skin · crackedFUSELAGE SKIN IS CRACKED AT FR 77, 5TH RIVET DOWN FROM STR 3R. (1/16"LONG) - FUSELAGE SKIN IS CRACKED AT FR 77, 1ST RIVET DOWN FROM STR 4R. (1/16"LONG-C/A-C/W BUSHING REPAIR IAW SRM 53-32-01. C/W BUSHING REPAIR IAW SRM 53-32-01.SDR SIMA20210527005Skin · crackedFUSELAGE SKIN HAS 6 CRACKS AT FR 77, 1ST RIVET UP FROM STR 4L. (1/32" LONG). FUSELAGE SKIN HAS 6 CRACKS AT FR 77, 1ST RIVET DOWN FROM STR 4L. (1/32" LONG). FUSELAGE SKIN HAS 2 CRACKS AT FR 77, 1ST RIVET UP FROM STR 6L. (1/32" LONG).. FUSELAGE SKIN HAS 1 CRACK SDR MASA20210527208Skin · corrodedLOWER SKIN CORRODED IN E&E BAY FWD OF FS364 BETWEEN STGR 26R AND 27R |BLENDED OUT CORROSION ON SKIN PANEL IAW EA 79-2021-130. BLEND OUTS ARE WITHIN LIMITS.SDR CALA2021052600736Skin · damagedREFERENCE 6258300. AIRCRAFT SUSTAINED FUSELAGE BELLY SKIN DAMAGE FROM STA.857 TO 927, FROM S-27L TO S-27R. REMOVED FASTENERS PER AVO ESC200513-0523-1 STEP A.1. NEED TO PERFORM DETAILED VISUAL INSPECTIONS PER AVO ESC200513-0523-1 STEPS A.2 THRU A.4. ESC200513-0SDR CALA2021052600735Skin · crackedB767-53-3-7064 - LOWER HALF FUSELAGE STA 1438 BETWEEN S38R-S39R HAS CRACK REF NRC 9130394, SKIN DAMAGED AREA TRIMMED OFF PER SRM 53-00-01- 2R-29 REAPIR FIG 201. SKIN THICKNESS IS 0.056". HFEC CARRIED OUT PER B767 NTM PART6 51-00-19 REV 125, NO CRACK FOUND. REPSDR SWIA2021082060547Buttstrap · corrodedCIRCUMFERENTIAL JOINT BETWEEN FS. 280.00 TO 282.86 AND STRINGER 26LH TO 26RH IS CORRODED. (C-CHECK RO 8/19/2021) COMPLIED WITH DISPOSITION FOR BLENDED CORROSION DAMAGE TO FS280.00 BUTTSTRAP BETWEEN STR26L AND STR26R IAW MHIRJ REO 670-53-21-2014 REV.-- DSDR SWAA2021061480210Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / EA # 21-153-01510 COMPLETED; EA # 21-153-01510 COMPLETED RII; EA # 21-153-01510 COMPLETED RIISDR SWAA2021061480205Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510; PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510 RII; PERFORMED REPAIRSDR HNAA2021062400290Skin · crackedEXTERIOR FUSELAGE AT FR 78 BETWEEN STR 4L-7L HAS POSSIBLE CRACKS AROUND 5 RIVETS. REPAIRED EXTERIOR FUSELAGE AT FR 78 BETWEEN STR 4L-7L CRACKS AROUND3 RIVETS IAW PIEDMONT EO1-53-21-0141. TWO RIVETS FOUND NOT TO HAVE CRACKS AROUND THEM.SDR HNAA2021062400289Skin · crackedEXTERIOR FUSELAGE AT FR 77 BETWEEN STR6R-7R HAS POSSIBLE CRACKS AROUND 2 RIVETS. REPAIRED EXTERIOR FUSELAGE AT FR 77 BETWEEN STR 6R-7R CRACKS AROUND 1 RIVET IAW PIEDMONT EO1-53-21-0140. ONE RIVET FOUND NOT TO HAVE CRACKS AROUND IT.SDR HNAA2021062400284Skin · crackedEXTERIOR FUSELAGE AT FR 79 BETWEEN STR 3R-4R HAS POSSIBLE CRACKS AROUND 1 RIVET (MARKED). REPAIRED EXTERIOR FUSELAGE AT FR 79 BETWEEN STR 3R-4R CRACKS AROUND1 RIVET IAW PIEDMONT EO1-53-21-0140.SDR SWIA2021080259913Doubler · corrodedMAIN AVIONICS BAY TCAS ANTENNA DOUBLER FROM FS295.00 TO FS310.00 CORRODED (C-CHECK RO 7/28/2021) REPLACED TCAS ANTENNA DOUBLER, FS295.00-310.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-30023 REVG. SEE CONTINUATION CARD FORSDR DALA2021062403414Skin · crackedSHIP 1601 , FUSELAGE SKIN AT BS 1582, S38L-39L, CRACK AND CORROSION. C/W ERA 591671-14, (LP 181552)SDR DALA2021052502888Skin · crackedSHIP 1601 DURING INSPECTION MAINTENANCE FOUND CRACK IN SKIN BS 1582 BETWEEN STR 39L &39R. AFT EDGE OF FWD SKIN AT BUTT SPLICE, AFT OF WASTE SERVICE DOOR. REAPAIRED PER ERA 591671-14. (LP 1816836)SDR IPXA2021052269692Skin · delaminatedINSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R, FIG 201SDR IPXA2021052269691Skin · delaminatedINSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F PER SRM 53-80-01-2R, FIG 201SDR SWIA202160019Skin · dented*DENT FORWARD LH FUSELAGE APPROXIMATELY 6.5€? FORWARD OF FS250 BETWEEN STR21L AN STR22L. (C-CHECK RO 8/1/2021) REPAIRED FORWARD LH FUSELAGE APPROXIMATELY 6.5€? FORWARD OF FS250 BETWEEN STR21L AN STR22L. REF MHIRJ REO 601R-53-11-3707 REV -- DATED 2021SDR FDEA202105211346Skin · crackedCABIN - LEFT HAND STATION 1255 L3 DOOR FORWARD LOWER JAMB WEB BETWEEN LONGERON 26 LEFT AND LONGERON 27 LEFT FOUND CRACKED. CABIN - AT LEFT HAND STATION 1255 L3 DOOR FORWARD LOWER JAMB WEB BETWEEN LONGERON 26 LEFT AND 27 LEFT , CRACKED SKIN REPAIRED AS PER SDR MASA20210521207Skin · damagedFORWARD FUSELAGE EXTERNAL SKIN PANEL PN 170-20874-003 BETWEEN FRAME 22 AND X=7070.7 AND AT STRINGER 28R- LIGHTNING STRIKE DAMAGE. DAMAGE REPAIR REF: ETD2021-170-014822SDR FDEA202105201335Skin · damagedMAINFRAME - HOLE IN A/C FUSELAGE REPAIR COMPLY WITH E..A. F-5310-T0361682 REV NO. POS. P1 DURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE SDR JGVR20210520004Skin · corrodedBLENDED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTORS. FOUND CORROSION TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02. REPAIRED CORROSION ON LOWER FUSELAGE SKIN AROUND TCAS ANTENNA CARRY THRU CONNECTOR PER TEXTRON REPAIR MEMO DQ 2SDR A6WA202106077797Skin · dentedAFT FUSELAGE SKIN DENT FS 640.00 - 1Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 1Ï¿½ LH STR 26 +2Ï¿½. DAMAGE MEASURES 1.200Ï¿½L X 0.600Ï¿½W X 0.023Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PSDR A6WA202106077795Skin · gougedAFT FUSELAGE SKIN GOUGE FS 589.00 + 1Ï¿½ RH STR 25 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN GOUGE FS 589.00 + 1 RH STR 25 + 2Ï¿½. DAMAGE MEASURES 1.10Ï¿½ L X 0.007Ï¿½ W X 0.006Ï¿½ D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FISDR A6WA202106077796Skin · dentedAFT FUSELAGE SKIN DENT FS 640.00 - 2Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 2Ï¿½ LH STR 26 +2Ï¿½.DAMAGE MEASURES 0.550Ï¿½L X 0.500Ï¿½W X 0.008Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PRSDR JJBA20210519002Skin · dentedDENT FOUND ON SKIN UNDER GROUND CONNECTOR AT STR 15 BTW FR 7-8 LH. ON FUSE SKIN, UNDER GROUND CONNECTOR AT STR 15 BTW FR 7-8 (LH), DAMAGE CUT OUT PERFORMED AND RIVET PATTERN DRILLED. REPAIR PARTS LOCALLY FABRICATED AND INSTALLED.SDR A6WA202105277787Skin · dentedAFT FUSELAGE SKIN DENT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½, DIMENSION0.700Ï¿½L X 0.500Ï¿½W X 0.050Ï¿½W. DENT FOUND TO BE OUT OF LIMITS REF CRJ200SDR DALA2021052402869Access Panel · crackedSHIP 3140 - CRACK ACCESS PANEL 191KB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 191KB BELLY FAIRING AT LOWER FUSELAGE AS PER ERA AND A319 SRM 51-77. (1813212)SDR IPXA2021051969591Skin · dentedINSPECTION TYPE:SEG4DENT OUT OF LIMITS SECTION 48REPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEGREE F CURE PER SRM 53-80-01-2R FIG 201SDR MK1Y20210519009Skin · damagedDURING MAINTENANCE INSPECTION FOUND A DENT WITH CREASE ON FUSELAGE SKIN – SEC 41, STA 334, STR 38R, TO STR 39RSDR MK1Y20210519003Frame · crackedDURING MAINTENANCE INSPECTION FOUND THREE CRACKS AT FRAME'S WEB AND INNER CHORD, CRACKS DIMENSIONS: 0.70", 0.59" AND 0.78, FRAME ASSY P/N 146T1117-1.SDR MK1Y20210519002Skin · dentedDURING MAINTENANCE INSPECTION FOUND DENT AND TWO SCRATCHES ON FUSELAGE SKIN AT SEC 48, STA 1582 TO STA 1605, STR 18L TO STR 20L.SDR WX0A1900010073961None · noneNRC 2000-0001: (274-2) JUST FWD OF R/H WINDSHIELD, BTWN FR3-4, DENT FOUND. / JUST FWD OF R/H WINDSHIELD BTW FR 3-4, DENT FOUND WITHIN LIMITS IAW SRM 53-00-11-283-005. REPAIR CATEGORY B, SEE SRI 53-00-11-205-050 FOR INSPECTION REQUIREMENTS. INSPECTION THRESHOLDSDR SWAA2021061682367Skin · dentedDENT EXTERNAL SKIN LOC AT BS 294.5 MORE 2 INCHES AND 3 INCHES BELOW STR 23L AT LOWER FUSELAGE ; 2021-215661 / REPAIRED EXTERNAL SKIN LOC. BTW BS 285.6 TO BS 312 AND BTW STR 23L TO 26L I.A.W EA #21-153-01520; PART 21-153-01520-WIP1 <BR>; PART 21-153-01520-WIP2 SDR SWAA2021061682366Skin · dentedDENT EXTERNAL SKIN LOC BTW BS 285.5 TO BS 303 AND BELOW STR 24L AT LOWER FUSELAGE ; 2021-215660 / REPAIRED EXTERNAL SKIN LOC. BTW BS 285.6 AND BS 312 AND BTW STR 22L TO STR 26L I.A.W EA #21-153-01520; PART 21-153-01520-WIP1; PART 21-153-01520-WIP2 REV B.;REPAISDR FDEA202105181294Skin · damagedREFERRING TO EA # 8-5310-79837, PART # 2, STEP # 1 PAGE 6 OF 6 PERFORM A DETAILED INSPECTION OF THE WRINKLES SHOWN IN FIG 1, MEASURE LENGTH, WIDTH & DEPTH. VERIFY THAT THE WRINKLES HAVE NOT SIGNIFICANTLY (=10%) CHANGED SINCE THE INITIAL INSPECTION SDR DALA2021052302845Skin · dentedSHIP 651 DENT TO FUSELAGE SKIN @ BS200 AND RBL 12-22. REPAIRED PER ERA 591111-14. (LP 1813089)SDR DALA2021052202842Skin · damaged(LOG 1812868) DURING INSPECTION FUSELAGE SKIN AT STA 294.5 BETWEEN S-21L AND S-23L WAS FOUND WITH A BULGE AT THE JACK POINT. MAINTNENANCE REPAIRED PER ERA 591675-14.SDR DALA2021052202841Skin · damaged(LOG 1813129) DURING INSPECTION FOUND ELONGATED FUSELAGE SKIN- SCREW HOLE OF SKIN OF JACKING PAD ADAPTATOR. FUSELAGE SKIN- SCREW HOLE OF SKIN OF JACKING PAD ADAPTATOR WAS REPAIRED PER ERA 591675-14.SDR MASA20210518191Doubler · corrodedLOWER ATC ANTENNA DOUBLER CORRODED IN E&E BAY|R&R ANTENNA DOUBLERSDR SWAA2021061682365Skin · dentedDENT EXTERNAL SKIN LOC BTW BS 235.8 TO BS 243.7 AND 4 INCHES BELOW STR 24R AT LOWER FUSELAGE ; 2021-215654 / FAULT RESOLVED ON OTHER FAULT #TTG8Q0052336;P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22;TOOL USED P/N NORTEC500D S/N N500X11290U021704 DUE DASDR V6NA2021051701.0Skin · corrodedAT SCHEDULED 12 YEAR INSPECTION, DISCOVERED CORROSION ON FUSELAGE SKIN AT LAVATORY SERVICE PORTS. CORROSION WAS REMOVED. REMAINING SKIN THICKNESS DETERMINED TO BE OUR OF LIMITS. REMOVED DAMAGED AREA. INSTALLED FILLER OF 0.040 INCH THICK 2024-T3 ALUMINUM AND EXSDR SWIA202158449Skin · damagedTRANSFER FROM EAML 638626 : MULTIPLE DENT AND SCRATCH DAMAGE TO RH FUSELAGE SKIN (DWG SH670-31071, 0.047€? NOM. THICKNESS, REF) BETWEEN FS 379.00 €“ FS409.00 AND STR 15R €“ 17R. DENT #1: 1.61€? (L) X 1.35€? (W) X 0.1345(D); DENT#4: 2.78€? (L) X 3.29€? (SDR CALA2021051700685Skin · damagedREFERENCE 6258300. AIRCRAFT SUSTAINED FUSELAGE BELLY SKIN DAMAGE FROM STA.857 TO 927, FROM S-27L TO S-27R. ACCOMPLISHED DETAIL VISUAL INSPECTIONS IN ACCORDANCE WITH AVO 2000513-0523-1 STEPS A.2 THRU 5. ALL DEFECTS NOTED ON LOG ITEMS. REMOVED FASTENERS PER AVO SDR AALA202105191754Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT FUSELAGE SKIN PANEL. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER PER SRM 53-41-11-300-009 AND EA 327624.
Back to JASC 5330