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 DALA2024050905067Skin · damaged(LOG 0331283) APU DOOR FORWARD HINGE APPEARS TO HAVE DAMAGED THE EXTERNAL FUSELAGE SKIN. TRIMMED OUT DAMAGE ON FUSELAGE SKIN IAW B737 SRM 53-80-01-2R REPAIR 1 PAR. B. INSTALLED DOUBLER REPAIR AND FILLER ON EXTERNAL FUSELAGE SKIN AT APU DOOR FWD HINGE RH IAW B7May 6, 2024 · N393DA · Boeing 737832SDR DALA2025091806856Skin · puncturedSTRINGER 1R TO 2R, SKIN PUNCTURED. SINCE THE COMPLIANCE TO PART 26.43 IS REQUIRED, THE AIRCRAFT IS LIMITED TO 12 MONTHS SERVICE AFTER REPAIR AND FATIGUE AND DAMAGE TOLERANCE EVALUATION (DTE) ARE REQUIRED WITHIN THIS TIME LIMIT IN ACCORDANCE WITH FAA ADVISORY May 5, 2024 · N132DU · Airbus BD5001A10SDR SWIA2024F00554Skin · dentedEXTERNAL FUSELAGE APPROXIMATELY FS913.0 STG27 DENT (C-CHECK RO 7/9/2024) EVALUATED. ORIGINAL THICKNESS .118" MINIMUM REMAINING THICKNESS .077" TOTAL MATERIAL LOSS .041" MAXIMUM ALLOWED BLEND .040". THEREFORE IS OUT LIMITS. REPAIRED PER REO 690-53-51-414May 5, 2024 · N679CA · Cndair CL6002D24SDR DALA2024050705001Skin · corrodedSHIP 171 DURING CCK AT STAG, CORROSION WAS NOTED ON THE CENTER WING UPPER SKIN, STA 955, RBL 86. CORRECTIVE ACTION: ER/A 616860-14AD SECTION I REPAIR WAS COMPLETED. (0329727)May 5, 2024 · N171DN · Boeing 767332SDR GTIA2024050738105Access Door · bentTHS MAINTENANCE ACCESS DOOR 314AR HAS BENT FWD CORNER-ACCOMPLISHED REPAIR OF THS ACCESS DOR 314AR ON HAECO S.O. 122198 OPS 22436 CAT A REPAIR. NO RE-INSPECT REQUIRED PER RDAF 813 93666/010/2024 #AMay 5, 2024 · N655NK · Airbus A320232SDR SWIA20240808504Skin · dentedADM # 8219- FWD FUSELAGE BELOW CA SIDE WINDOW. JUST FWD FS280.00. DENT 1.81" LONG .71" HIGH .018" DEEP JUST FWD FS 280.00. SRM 53-00-01-101-A01. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD AMay 4, 2024 · N719EV · Cndair CL6002C10SDR AALA202405077597Skin · crackedAIRCRAFT IN BASE MAINTENANCE: R3 DOOR INTERIOR UPPER DOOR CUT OUT TRIM CRACKED. REMOVED, REPAIRED AND RE-INSTALLED R3 DOOR INSTERIOR UPPER DOOR CUT-OUT. PER AMM DMC-B787-A-25-21-02-00A-520A-A, AMM DMC-B787-A-25-00-00-01-663A-A AND AMM DMC-B787-A-25-21-02-00A-7May 4, 2024 · N837AN · Boeing 7879SDR YENA2024050700719Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN AT FR 1 CUT OUT SKIN AND 6 INCH BELOW LOWER LATERAL STRINGER AT LOWER FUSELAGE; (RESOLVED ON W/O: 1274338 TASKCARD: NR-00038) REF WO# 2024 44/1 NR# 2024-148745. ACCOMPLISHED THE REPAIR OF THE DENT DAMAGES ON NOSE FOMay 4, 2024 · N554JB · Airbus A320232SDR YENA2024050700712Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / TOP SKIN PANEL / UPPER SURFACE / BTWN FR41-42 @ Y1292 EDGE / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)May 4, 2024 · N554JB · Airbus A320232SDR YENA2024050700711Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / LOWER SKIN PANEL AT FR1 AND Y-330 / DENT - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)May 4, 2024 · N554JB · Airbus A320232SDR ABXA2024050489Skin · crackedDURING ROUTINE LINE OPERATIONS IN MIA, MAINTENANCE DISCOVERED TWO CRACKS AT THE RH EMPENNAGE SECTION AT STA. 1654.5. AT APPROXIMATELY STRINGER 15R. BOTH CRACKS MEASURE APPROXIMATELY 2¿¿ IN LENGTH. MIA INDICATED THAT THERE WAS NO DENT ASSOCIATED WITH THE CRACK.May 4, 2024 · N763CK · Boeing 7673P6SDR IPXA2024101206466Skin · delaminatedPANEL ABOVE APU EXHAUST STATION 1941.0-1963.8 HAS DELAM ON INNER SKIN TOP CENTER. (148N3730-47). INSTALLED NEW SKIN ASSY PANEL (P/N 148N3730Y47 BATCH: 0004316631) ABOVE APU EXHAUST STATION 1941.0-1963.8 REF B757-200PF SRM 51-40-02-0G-0 AND DWG: 148N3730. RE-INMay 3, 2024 · N453UP · Boeing 75724APFSDR SWIA20240503Skin · dentedDENT ON FUSELAGE EXTERNAL SKIN AFT OF FS220.00 ALONG STGR12L. (MARKED) (C-CHECK RO 7/17/2024) REPAIRED DENT ON FUSELAGE EXTERNAL SKIN AFT OF FS220.00 ALONG STGR12L. REF REO 670-53-11-1978 REV -- DATED 2024-06-16 , REO 670-51-00-085 REV -A DATED 2017-08May 3, 2024 · N760SK · Cndair CL6002C10SDR AALA202406048390Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT STA 540, S22L. REPAIRED SKIN PER EA 353519.May 3, 2024 · N943AN · Boeing 737823SDR AALA2024052060772Skin · bulgedAIRCRAFT IN BASE MAINTENANCE: OUTWARD BULGE IN FUSELAGE SKIN ABOVE AFT CARGO DOOR AT STA 807, S14R. ACCOMPLISHED DOUBLER REPAIR PER EA 353444.May 3, 2024 · N939AN · Boeing 737823SDR ABXA2024050787Bear Strap · corrodedAIRBORNE MAINTENANCE AT CVG DISCOVERED CORROSION ON THE INTERNAL BEARSTRAP (P/N 146T8521-1) LOCATED AT THE AFT LOWER CARGO CONTROL PANEL SKIN CUTOUT AT APPROXIMATE STATION 1260 BETWEEN S-23R TO S-24R.THE CORROSION WAS REMOVED PER 767-200 SRM 53-30-15, REPAIR 1May 3, 2024 · N650GT · Boeing 767231SDR SIMA202405073001Skin · gougedFOUND GOUGE RH SIDE FORWARD FUSELAGE. BETWEEN FRAME 1 AND 2 RIGHT BELOW RVSM AREA, BLEND OUT OF LIMITS OF SRM 53-10-01 "MAJOR REPAIR" PERFORMED PERMANENT REPAIR OF FORWARD FUSELAGE BETWEEN FRAME 1 AND 2 RIGHT BELOW RVSM AREA IAW ENVOY ERS EJ-53-MR-4983 PART A.May 3, 2024 · N225NN · Emb ERJ170200LRSDR DALA2024050604960Skin · damagedSHIP 178 LIGHTENING STRIKE STA 654 + 16 AT FASTENER ON STRINGER 7L. CORRECTIVE ACTION: EVALUATE AND REPAIR AS REQUIRED PER B767-300 SRM 53-00-01. INSTALLED REPAIR DECAL PER PS 900-5-1 NO. 4 (0325202)May 3, 2024 · N178DN · Boeing 767332SDR DALA2024050604959Skin · damagedSHIP 178 LIGHTENING STRIKE AT FASTENER ST 592 ABOVE STRINGER 6L. CORRECTIVE ACTION: REPAIRED REF B767-300 SRM 53-00-01 REPAIR 14. (0325067)May 3, 2024 · N178DN · Boeing 767332SDR AALA202405062898Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN PANEL BETWEEN FR 69 AND FR 70, BETWEEN S31R AND S32R AT THE AFT LAVATORY VENT AREA. REPAIRED FUSELAGE SKIN PANEL PER EA 354089.May 2, 2024 · N823AW · Airbus A319132SDR DALA2024050604933Skin · cracked(LOG 0323574) HOLE WITH CRACK INDICATION. HOLE IS LOCATED JUST BELOW STR 22R JUST FWD OF STA 540. ENSURE ALL 617540-14 REV. ORIG. PRI "0", "1" INSTRUCTIONAL STEPS ARE COMPLETED AND MATCHED FINAL - STA. 540 BULKHEAD CHORD / LOWER RH SPLICE REPAIR CRACK INDICATIMay 2, 2024 · N3739P · Boeing 737832SDR DALA2024050604927Skin · corroded(LOG 0323577) SKIN CORRODED AT GROUND AIR CONNECTOR. COMPLIED WITH ER/A 617453-14.May 2, 2024 · N3739P · Boeing 737832SDR DALA2024050304920Skin · crackedCRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA WAS REPAIRED PER PRI 617480-14 REV 1 AND ERA 617480-14 REV ORIGINAL SECTION I: PERMANENT REPMay 2, 2024 · N993AT · Boeing 717200SDR DALA2024050304910Skin · scratchedSHIP 6700 SCRATCH STA 1400 & 1420 AND BTW. S30L AND S29L AT LOWER FUSELAGE, ZONE 100. CORRECTIVE ACTION: SUMMARY OF NRC 00097: SCRATCH STA 1400 & 1420 AND BTW. S30L AND S29L AT EXTERNAL SKIN LOWER FUSELAGE, ZONE 100 WAS REPAIRED PER B757-200 SRM 53-00-01-2R REMay 2, 2024 · N6700 · Boeing 757232SDR IXXA2024050205Skin · damagedACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 412, STR 30RMay 2, 2024 · N457AZ · Boeing 767323SDR SWIA202405150001Skin · chafedRH SLAT PANEL #3 NOSE SKIN HAS CHAFES IN TWO SPOTS AS MARKED. (C-CHECK RO 5/14/2024) BLENDED OUT THE CHAFES ON RH WING #3 SLAT LEADING EDGE NOSE SKIN. BLEND DIMENSIONS AS FOLLOWS; D= .010", L= 1.747", W= 1.498", NOMINAL THICKNESS= .087", MAXIMUM ALLOWABLE May 1, 2024 · N160SY · Emb ERJ170200LRSDR YENA2024050200681Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR 41 TO FR 42 AND BTW -Y1292 TO -Y1732 PASSENGER CABIN; REF AEROMANM NR 2023-168921 WO 2024 45/1 PERFORMED PERMANENT REPAIR LOC.TOP EXTERNAL SKIN CENTER FUEL TANK BTW FR41 TO FR42 OMay 1, 2024 · N649JB · Airbus A320232SDR YENA2024050200679Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / RH TOP SKIN BTWN FR 41-42 & BTWN BEAM -Y1292 - RIB 1 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)May 1, 2024 · N649JB · Airbus A320232SDR DALA2024050204878Skin · corroded(LOG 0321597) SKIN CORRODED AT GROUND AIR CONNECTOR. COMPLIED WITH ERA 617453-14.May 1, 2024 · N3739P · Boeing 737832SDR JJBA20240523055Skin · crackedLH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND STR 3L-9L, CRACKS (X5) FOUND AROUND FASTENERS. LH EXTERNAL FUSE, PAINT REMOVED BTW FR 77-80 AND BTW STR 3L-9L. LH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND STR 3L-9L. LH EXTERNAL FUSELAGE BTW FR 77-80 STR 3L-9L FOUR REPAIApr 30, 2024 · N21197 · Emb EMB145XRSDR CALA2024051301458Skin · crackedEA5315-01152 REV ORIG OP001 - 2EA CRACKS WERE FOUND ON THE FASTENER HOLE AT LH FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AREA TRANSFER REF HXWO 3037333. LH FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN REV - PART 1 ITEM B , CREATED LP 7859487 AND CApr 30, 2024 · N654UA · Boeing 767322SDR CALA2024050701370Skin · corrodedREF AMES NON ROUTINE 168798-0100-0205.GENERATING ITEM:63-5300-1- 2516.(B767-53-3-7121) CORROSION ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN, AT STA.1083, BETWEEN STR.39L AND STR.39R.#91038 REMOVED CORROSION ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN A T STApr 30, 2024 · N643UA · Boeing 767322SDR CALA2024050101289Skin · damagedFOUND DAMAGE ON EXTERNAL SURFACE OF SKIN JUST AFT OF LIVE TV DOUBLER LOCATED AT 727E S-3L. DAMAGED AREA IS APPROXIMATELY 2 1/ 2 INCHED LONG. SEE BAM N/R 001867632 FOR REPAIR OF AREA. READ "ACCOMPLISH INSPECTION REQUIREMENTS OF THE CROWN SKIN EC/RA 5331-03088 OApr 30, 2024 · N36280 · Boeing 737824SDR CALA2024050101288Skin · dentedLIVE TV DOUBLER LOCATED ON EXTERNAL SURFACE AT 727C BETWEEN S-2L AND S-3L IS DIFFERENT THAN WHAT IS SHOWN OF T-CARD T29-4430-1-0057. ALL 3 END FASTENERS AT FWD END ARE UNDER THE DOUBLER SO THE TWO FWD FASTENERS SHOWN ON THE ILLUSTRATION CAN NOT BE HFEC INSPECTApr 30, 2024 · N36280 · Boeing 737824SDR DALA2024050104835Skin · corrodedCORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDUREApr 30, 2024 · N988AT · Boeing 717200SDR DALA2024051705314Skin · dentedSHIP 176 FOUND DENT IN DAMAGED AREA # 2, LABELED 2Q, BET STA 1197+44 AND STA 1197+66 AND STR 28R AND STR 29R WITH AN INITIAL DEPTH OF .104" AND APPROX WIDTH OF 6.125". CORRECTIVE ACTION: REPAIRED ON ERA 617766-14 REV B (0318539)Apr 29, 2024 · N176DN · Boeing 767332SDR CALA2024050701338Skin · corroded(B767-53-3-7121) CORROSION ON THE INTERIOR SURFACE OF THE FUSELA GE SKIN, AT STA.1090, JUST AFT OF THE FUSELAGE MOISTURE DRAIN, B ETWEEN STR.39L AND STR.39R.#91040 REMOVED AND REPLACED DRAIN VALVE ASSY IN ALC AT STA 1090 S-39L-S -39R IAW B767 SRM 51-40-02 PARAApr 29, 2024 · N643UA · Boeing 767322SDR CALA2024050701337Skin · corroded(B767-53-3-7121) CORROSION ON THE INTERIOR SURFACE OF THE FUSELA GE SKIN, AT STA.1084, BETWEEN STR.38R AND STR.37R.#91039 REMOVED AND REPLACED DRAIN VALVE ASSY IN ALC AT STA 1084 S-35R-S -37R IAW B767 SRM 51-40-03 PARA 4. SEE NR 168798-0100-0205 FOR R EPAIR OFApr 29, 2024 · N643UA · Boeing 767322SDR CALA2024050701336Skin · corroded(B767-53-3-7121) CORROSION ON THE INTERIOR SURFACE OF THE FUSELA GE SKIN, AT STA.1084, BETWEEN STR.37L AND STR.38L.#91041 REMOVED AND REPLACED DRAIN VALVE ASSY IN ALC AR STA 1084 STR 37L -S38L IAW B767 SRM 51-40-02 PARA 4. SEE NR 168798-0100-0205 FOR REPAIR OFApr 29, 2024 · N643UA · Boeing 767322SDR DALA2024050104848Skin · corrodedSHIP 6809 CORROSION ON SEVERAL POINTS BTW STA 680 TO STA 760 AND BTW S-3R TO S-3L ALSO DETERIORATION OF PROTECTIVE TREATMENT ON EXTERNAL DOUBLER. CORRECTIVE ACTION: SUMMARY OF NRC 00526: GO GO KU EXTERNAL DOUBLER WAS REPAIRED PER ER/A 617006-14 REV. ORIGINAL SApr 29, 2024 · N713TW · Boeing 7572Q8SDR 9WGA2026013035601Skin · damagedNR# 13 - DURING HEAVY MAINTENANCE CHECK EXTENSIVE FUSELAGE DAMAGE LH SIDE BELOW CREW CABIN (STORM DAMAGE). REFERENCE BOEING REPAIR ORDER WGN-RE-2403216 FOR CORRECTIVE ACTION, DATED 8/24/25. REFERENCE 337 FOR CORRECTIVE ACTION DATED 7/31/25. REFERENCE 8100-9 Apr 28, 2024 · N356KD · Boeing 747446SDR CALA2024050801401Skin · misrepairedFUSELAGE AT STA 1540, STR 39R MISDRILL THE REPAIR DOUBLER. FUSELAGE SKIN STA 1540 BETWEEN STR 38L AND STR 38R REPAIRED AS PER EC/RA 5360-01798 REV.- PART 1 ATTACH FORM 44-0008 ITEM 1 TO ITEM 29Apr 27, 2024 · N653UA · Boeing 767322SDR CALA2024050701354Skin · crackedFUSELAGE SKIN DOUBLER FOUND CRACK AT WASTE SYSTEM SERVICE PANEL #163AL CUTOUT AREA. FUSELAGE SKIN STA 1562 TO STA 1582 BETWEEN STR 38L AND STR 38R INTERNAL DOUBLER REPLACED AS PER SRM 51-10-02.Apr 27, 2024 · N653UA · Boeing 767322SDR CALA2024050701363Skin · crackedEA 5315-01152 OP002, STEP B(4), 2EA HOLES FOUND CRACK ON SKIN LAYER. DOOR 1R CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP INTERIM REPAIRED AS PER EC/RA 5315-01212 REV. ORIG PART 1Apr 27, 2024 · N653UA · Boeing 767322SDR CALA2024050701361Skin · crackedEA 5315-01152 OP 001, STEP B(4), 1EA HOLE FOUND THROUGH THICKNESS CRACK ON SKIN LAYER. TRANSFER REF NR HX WO.3049623. FX-DOOR 1L CUTOUT AFT LOWER CORNER FUSELAGE SKIN INTERIM WORK REPAIRED AS PER EC/RA 5315-01213 REV.- PART 1. ATTACHED FORM 44-0008 ITEM 1 TApr 27, 2024 · N653UA · Boeing 767322SDR DALA2024050204873Doubler · corroded(LOG 0321559) CORROSION ON EQUIP COOLING OVERBOARD EXHAUST VALVE DOUBLER STA 360+3-360+16 STR 28L. REMOVED AND REPLACED DOUBLER DAMAGED ON EQUIP COOLING OVERBOARD EXHAUST VALVE STA 360+2-380+4 STR 28L PER B737-800 DWG 143A3233 REV. F AND SRM 51-40-02-0G.Apr 27, 2024 · N393DA · Boeing 737832SDR CALA2024050801395Skin · crackedFUSELAGE SKIN AND BEAR STRAP A T THE L1 DOOR CUTOUT LOWER AFT CORNER STA 335 JUST ABOVE STRINGE R 20L SECOND HOLE FROM BOTTOM HAS CRACK INDICATION WITH HFEC OPE N HOLE SCAN. REPAIRED SKIN AND BEAR STRAP AT L1 DOOR CUTOUT LOWER AFT CORNER STA 355 IAW B767 SRM Apr 26, 2024 · N643UA · Boeing 767322SDR CALA2024050101287Skin · crackedFUSELAGE SKIN AND BEAR STRAP A T THE R1 LWR DOOR CORNER STA 335 JUST ABOVE STR 20R SECOND FASTE NER FROM BOTTOM HAS CRACK INDICATION WITH HFEC OPEN HOLE SCAN.Apr 26, 2024 · N643UA · Boeing 767322SDR CALA2024050101284Skin · crackedAFT LH FUSELAGE STA 1732 LOWER HORSE COLLAR AREA FWD SLIDER RUB STRIPS UPPER AND LOWER WORN THRU AND CRACKED. THIS REPAIR IS A CATEGORY A REPAIR. REPLACED FWD SKIN AND REPAIR ED LOWER SKIN IAW B767-300 SRM 53-80-01-2R-3 REPAIR 3. TRANSCRIBED FROM AMES NON ROUApr 26, 2024 · N643UA · Boeing 767322SDR DALA2024042904776Skin · crackedSHIP 6809 ERA 472891-14AD, FUSELAGE / SKIN / STA 1220, STR 4L / SKIN REPAIR / INSPECTION. CORRECTIVE ACTION: REF ERA 472891-14AD. (0313439)Apr 26, 2024 · N713TW · Boeing 7572Q8
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