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 DALA2025011300242Skin · gougedSHIP 3147 SECONDARY FINDING GOUGE EXTERNAL SKIN LOCATED BTW FR 54 TO FR 55 AND BTW STR 41L TO STR 43L AT LOWER FUSELAGE (2 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A 623315-14. (0757774)SDR DALA2025011300241Skin · dentedSHIP 3147 DENT EXTERNAL SKIN LOCATED AT FR 58 AND BTW STR 41L TO STR 42L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 622576-14. (0757753)SDR SWI2025F00162Skin · damagedADM N603CZ-7577 EVALUATE AND IMPROVE APPEARANCE OF DAMAGE AT 5.5" ABOVE STRG 14R. 14" AFT OF RADOME AFT DEGE. 6.5" FWD OF RH ICE DETECTOR LEADING EDGE. (C-CHECK RO 2/21/2025) PERFORMED PERMANENT DOUBLER REPAIR ON RH UPPER FWD FUSELAGE SKIN FR 02-03 STGRSDR SWIA20250221111Skin · damagedADM N603CZ-6874 EVALUATE AND IMPROVE APPREARANCE OF DAMAGE AT LH SIDE OF A/C 9" AFT OF FR10 AND 1.5" ABOVE STGR16L (C-CHECK RO 2/21/2025) REMOVED AND REPLACED FWD FUSELAGE LH SKIN PANEL REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. NO CSDR DALA2025012400612Skin · ground damage(LOG 0756499) BELT LOADER CONTACTED FORWARD CARGO SKIN AREA 7 TO 9 INCHES UP FROM FLOOR THRESHOLD ON FORWARD SIDE OF CARGO OPENING. REPAIRED DAMAGE PER ERA 623563-14.SDR DALA2025011300243Skin · damagedSHIP 3147 LIGHTNING STRIKE FASTENER HEAD LOCATED FR15 AT LEVEL STR36R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR FOR LIGHTNING STRIKE AS PER A319 SRM 53-11-11-300-034. (0755594)SDR DALA2025011300239Skin · dentedSHIP 3147 DENT EXTERNAL SKIN LOCATED BTW FR 11 TO FR 12 AND 14 INCHES ABOVE LH S IDE STR LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AS PER A319 SRM 53-11-11-300-041. (0756534)SDR ASAA2025011055193Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN I/B OF DRAIN MAST BETWEEN STA 989-1006 STGR 24L-25L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT STA 986.5 TO STA 1006 STGR 24L-25L IAW EA 800-53EA-28059 REV 00 SRXR430XSDR ASAA2025011055191Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN AROUND WATER SEVICE PANEL CUTOUT BETWEEN STA 907-927 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT STA 907-927 STGR 25R TO STGR 27R IAW EA 800-53EA-28068 REV 00 SRXR430X.SDR ASAA2025011055192Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN AT SERVICE INTERPHONE JACK AT STA 1043 STGR 24L-25L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN AT STA 1043 BETWEEN STGR 24L-25L IAW EA 800-53EA-28070 REV 00 SRXR430X.SDR SWAA2025011384740Seal · crackedR/H HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED FWD EDGE<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.SDR DALA2025011300286Skin · corrodedCORROSION SSI: 53-60-02-03. CORROSION FOUND BETWEEN FR 70 AND FR71 AND BETWEEN STGR 36L AND STGR 35L. REPAIRED PER PRI 622727-14 REV 0,1,2,3 AND ERA 622727-14 REV ORIGINAL. (LP# 0754712)SDR DALA2025011300258Skin · corroded(LOG 0755265) CORROSION ON FWD CARGO BAY, INSTALLED DOUBLER BETWEEN STA 500C-500D BETWENN S-27R TO S-27L. REMOVED AND REPLACED DOUBLERS ON FWD CARGO BAY BETWEEN STA 500C- 500D BETWEEN S - 27R TO 27L PER B737-900 SRM 51-40-02-0G AND DWG P36028 REV: A AND P20184SDR DALA2025011300248Skin · dentedSHIP 3147 A DENT WAS FOUND AFFECTING THE LOWER SKIN PANEL BETWEEN FR66 & FR67 AT STRINGER 41RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 622561-14. (0754936)SDR N6WA2025011202Doubler · corrodedCORROSION ON TCAS OMNI DIRECTIONAL ANTENNA DOUBLER. REPLACED TCAS ANTENNA DOUBLER IAW CRJ SRM 51-42-06.SDR JJBA20250225008Skin · damagedDAMAGE TO THE LH REAR FUSELAGE 1 AT FRAMES 70 TO 72 AND STRINGERS 16L-18L. PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION ON AND AROUND DAMAGED AREA OF LH REAR FUSELAGE I FROM FRAMES 70-72, STRINGERS 16L-18L. NO INDICATION OF CRACKS FOUND AT THIS TIME. REMOVSDR SWAA2025021884799Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] REPAIRED EGPR SURROUND DOUBLER AT BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(A-M) FIG. 204 SHT.(3-4);[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLSDR SWAA2025020584632Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-779426<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:146A7901 SHEET:66 REV.A LENGSDR IPXA2025012012393Skin · damagedFUSELAJE ZONE 200 HAS EVIDENCE LIGHTNING STRIKE BETWEEN STA. 1320 TO 1440 (S11-S26). ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-00-01-2R, REPAIR 28 PER SRM 53-60-01-2R-0.SDR IPXA2025012496294Skin · damagedDAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND FOR CORRECTIVE ACTION PLEASE SEE REF: EO-92470-REQ1 (SECTION 48 FUSELAGE SKIN PANEL DENT, GOUGE, AND CRACK DAMAGE FORWARD OF STA 2598; BETWEEN STR 38R AND 46R - CATEGORY B REPAIR) COMPLIED WITH EO-92470SDR DALA2025011300270Skin · damaged-AD- ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50, ALSO ON SAME ANGLE BTW X=44 AND X=50 (4 EA) AT WINGBOX AREA. (CPAX). SUMMARY OF NRC 00750: ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50 AT SDR CALA2025011300110Skin · crackedSUPPORT TASK - EA 5310-07557 REV B OP 002 (AD 2019-11-02) LH UNDERWING LONGERON FUS SKIN 2EA HOLE FOUND CRACK (DETAIL REF NDT INSP FINDING RECORD). FUSELAGE LH SKIN AT STA 993-1035 BETWEEN STR-35L AND STR-37L MODIFICATION WITH DOUBLER AND REPAIR FILLER INSTALSDR CALA2025011300109Skin · crackedSUPPORT TASK - EA 5330-07074 REV B OP 001 STEP 3, CRACK FOUND ON L/H FUSELAGE SKIN. ACCOMPLISH EA 5310-07557 OP1 AND OP2 FOR MODIFICATION. FUSELAGE LH SKIN AT STA 993-1035 BETWEEN STR-35L AND STR-37L MODIFICATION WITH DOUBLER AND REPAIR FILLER INSTALLATION ASSDR FDEA202501090049Doubler · damagedLOWER FORWARD CARGO DOOR LOWER FORWARD JAMB EXISTING REPAIR DOUBLER EDGE FOUND WITH CHAFED MARKS AT STATION 899 LOWER FORWARD CARGO DOOR LOWER FORWARD JAMB AT STATION 899 CHAFFED EXISTING REPAIR DOUBLER REMOVED AS PER MD11 SRM 51-33-01-0G. REPAIR CARRIED OSDR FDEA202501090048Doubler · damagedLOWER FORWARD CARGO DOOR CUTOUT LOWER AFT JAMB EXISTING REPAIR DOUBLER LOWER CORNER FOUND CHIPPED OFF AT STATION 999 LOWER FORWARD CARGO DOOR CUTOUT LOWER AFT JAMB LOWER CORNER AT STATION 999 CHIPPED OFF EXISTING REPAIR DOUBLER REMOVED AS PER MD11 SRM 51-3SDR EE4Y2025010921512Skin · corrodedDURING THE STRUCTURE INSPECTION, WAS FOUND THE FUSELAGE SKIN WITH CORROSION AT THE INTERNAL SURFACE, BETWEEN FRAME 73 AND 74 AND BETWEEN STRINGER 29L AND 29R, SINCE NOT TECHNICAL DATA WAS FOUND TO REPAIR THE REPORTED DAMAGES, EMBRAER HAS BEEN CONTACTED TO PROVSDR SWIA2025011400008Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA96223-ETD 2025-170-000104 RA96186-ETD2025 MXCODEID106942-PR - RAMP REPORTS POSSIBLE DENT FORWARD PAX DOOR. FOUND TO BE OUT OF LIMITS PER SRM 53-10-01/AD02. COMPLIED WITH ETD2025-170-000104. DETAILED VISUAL INSPECTION CSDR DALA2025011300282Skin · corrodedFWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION BETWEEN HOLES 5OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 179-0001:5331-01297- 02C/004 00259 REPAIRED REF ER/A 622538-14 PRI REV 0, REV 1 AND ER/A 622538-1SDR DALA2025011300281Skin · corrodedFWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 0.75" ABOVE HOLE 3OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 179-0001:5331-01297- 02C/003 00258 REPAIRED REF ER/A 622538-14 PRI REV 0, REV 1 AND ER/A 62253SDR DALA2025011300278Skin · corrodedAFT RIGHT PASSENGER/SERVICE DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 1.5" ABOVE/FWD OF HOLE 12OL. MARKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 048-0001:5331-01297- 02B/001 00246 REPAIRED PER PRI 622574-14 REV 0,REV1 AND ERSDR SWIA20250109043Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA96223-ETD 2025-170-000104 RA96186-ETD2025 MXCODEID106942-PR - RAMP REPORTS POSSIBLE DENT FORWARD PAX DOOR. FOUND TO BE OUT OF LIMITS PER SRM 53-10-01/AD02. COMPLIED WITH ETD2025-170-000104 (ATTACHED). DETAILED VISUAL ISDR VNAA20250108038Skin · chafedCHAFING FOUND ON EXTERIOR SKIN OF FUSELAGE AT STRINGER 27 BETWEEN FS969 AND FS985. REPAIRED CHAFE BY COMPLYING WITH BOMBARDIER REO 670-53-00-290 REV -F.SDR DALA2025010800171Skin · gougedSHIP 3421 FUSELAGE SKIN HAS A GOUGE ABOVE THE BULK CARGO DOOR APPROX MIDDLE OF THE DOOR OPENING. CORRECTIVE ACTION: REPAIRED PER A330 SRM NEO 53-41-11. (0750389)SDR IPXA2025013059623Skin · dentedFUSELAGE BETWEEN STA.1896.20 AND STA 1918.9 LEFT UPPER SIDE SKIN HAS DENT (NOT MAPPED). DOT 62-06. EA-62.ACCOMPLISH PERMANENT REPAIR PER 757-200PF SRM REV 121 CHAPTER 51-70-10-2R-4 FIGURE 201 SHEET 1 (REPAIRS TO LARGE DAMAGE) PER SRM 53-80-01-2R. OSD: 2/4/202SDR BAGA2025012700008Doubler · corroded(HEAVY CHECK) WASTE BOX FOUND CORROSDED AT FR75/FR76. REMOVED AND REPLACED WASTE BOX WITH REPAIR. REPAIR VALID FOR 10000 FH.SDR SWAA2025012383733Seal · crackedLEFT STABILIZER UPPER SLIDING SEAL WORN / CRACKED.<[01] REMOVED AND REPLACED SLIDING SEAL IAW B737-NG AMM 53-31-31;[02] VERIFIED REMOVED AND REPLACED SLIDING SEAL IAW B737-NG AMM 53-31-31SDR CALA2025011300111Skin · crackedFR 35 STR 30 RH HOLE #2 HAS CRACK INDICATION APPEARS TO BE IN AFT SKIN LAYER AT 60%SH. PERFORMED REPAIR OF HOLE #2 AT FR 35 STR 30 R IAW ECRA 5330-0737 THERE IS NO TERMINATING ACTION FOR THESE REPETITIVE INSPECTION R 1/ HAECO REO L25265 REV IR PART1 THE REPASDR DALA2025011000226Skin · corrodedWHILE ACCOMPLISHING AFT LEFT PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-02A, FOUND CORROSION AT/AROUND HOLES 12OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297- 02A/002 00247 REPAIRED PER ER/A 622582-14 PRI REV 0, REV 1, AND ER/A SDR DALA2025011000225Skin · corrodedWHILE ACCOMPLISHING FWD CARGO DOOR CORROSION INSPECTION PER AMDS 5331-01297-01C, FOUND CORROSION AT/AROUND HOLES 13OL, 14OL, 16OL, 17OL, 18OL, 19OL, 20OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 046-0001:5331-01297-01C/001 00241 REPAIRED PER ER/A 623164-14 PSDR FDEA202501070027Skin · crackedFUSELAGE: #1 AIRCON COMPARTMENT CUTOUT UPPER AFT CORNER SUSPECT CRACK STATION 587.250 LONGERON 31 - LONGERON 33. FUSELAGE: #1 AIRCON COMPARTMENT CUTOUT UPPER AFT CORNER CRACK STATION 587.250 LONGERON 31 - LONGERON 33 CARRIED OUT REPAIR IN ACCORDANCE WITH SSDR COEA2025060607913Skin · corrodedWO 262004 NR 200041 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE SKIN HAS LEVEL 2 CORROSION BELOW F/O'S FWD SIDE WINDOW BETWEEN FRAMES 6-7 CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 51-25-01 AND 530000-300-803-A01.SDR SWIA20250430106Skin · chafedLH EXTERNAL FUSELAGE, CHAFFING ON SKIN PANEL, FS961, BETWEEN LH STR# 23-24 (C-CHECK RO 04/30/2025)COMPLIED WITH REO N# 670-53-51-339 REV. -- 2025-02-15, AT L/H EXTERNAL FUSELAGE SKIN BLENDED CORROSION DAMAGE BTW FS 953.00 - FS 969.00 & STR 23- STR 24L. (FOR WOSDR SWIA20250331106Skin · gougedADM# N962SW-7829 FS 640.00--FS 654.5 RH STRINGER 4-5. FOUND GOUGE 1.6" AFT OF FS 640.00 AND 1.5" ABOVE RH STRINGER 5. GOUGE IS .0019" DEEP, WIDTH .44", LENGTH .58". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USISDR AALA202502128514Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER WING LOWER SKIN, ON EXTERIOR OF FUEL TANK AT STA 540, S22L. REPAIRED SKIN PER SRM 51-10-02-0G AND EA 361103.SDR BAGA2025012500006Skin · corrodedFWD CARGO DOOR LOWER SKIN UNDERNEATH SCUFF PLATE AT FRAME 24-27 HAD CORROSION AROUND ATTACHMENT HOLES. ACCOMPLISHED TEMP REPAIR. REPAIR VALID FOR 10000 FH (HEAVY CHECK)SDR BAGA2025012500005Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN AT JUNCTION OF TAIL CONE BTW STR 35L AND 36L AT FR 78-79. ACCOMPLISED TEMP REPAIR . REPAIR VALID FOR 10000FHSDR BAGA2025012500004Skin · corrodedFWD PASSENGER DOOR LOWER SKIN UNDERNEATH SCUFF PLATES, FOUND CORROSION AROUND ATTACHMENT HOLES. ACCOMPLISHED TEMP REPAIR. REPAIR VALID FOR 10000 FH.SDR BAGA2025012300002Skin · corrodedAFT CARGO DOOR LOWER SKIN UNDERNEATH SCUFF PLATE FOUND CORROSION AROUND ATTACHMENT HOLES. ACCOMPLISED REPAIR. REPAIR VALID FOR 10,000 FH.SDR R61A2024012200043Doubler · cracked****MAJOR****DMI R1250573/1 DENTS FOUND AT FR11-12 STR5-6L REPAIRED CRACK IAW SRM 53-10-01 REPAIR 12.SDR 2A6R2025010672306Angle · crackedDURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK ROOF ANGLE (PN: L533M1017266). THE CRACK WAS LESS THAN 3.25” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-135-53-061
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