JASC 5300

Service difficulty reports · 8,206

Reports filed under 5300 · Fuselage Structure (General), 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 = '5300'
  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 2022FA0000290None · bypassingTHIS AIRCRAFT MADE AN EMERGENCY LANDING AT FORT LAUDERDALE EXECUTIVE AIRPORT AFTER SEVERAL ATTEMPTS THE RIGHT MAIN WOULD NOT FREEFALL, THE AIRCRAFT WAS BROUGHT TO US FOR MAINTENANCE AND TROUBLESHOOT AFTER THIS INCIDENT. WE FOUND THAT THE POWER PACK P/N HYC5005Jun 13, 2022 · N8415H · Piper PA32R301SDR CALA2022061301497Skin · puncturedABM CLEANING TRUCK HIT FUSELAGE AT 3 FEET BELOW DOOR 4 LEFT, PUTTING A HOLE IN THE FUSELAGE. DAMAGE IS 2 AND 1/4 INCH HORIZONTAL BY 1 INCH VIRTICAL. SHOULD READ PUNCTURE IN FUSELAGE. PUNCTURE IS LOCATED IN SECTION 47, STATION 1768, STRINGER 29L. BEHIND DAMAGE Jun 13, 2022 · N45905 · Boeing 7878SDR CALA2022061301493Unknown · vibrationPER INBOUND FLIGHT CREW - VIBRATION FELT ONLY IN FORWARD PART OF CABIN NOT AFT . REF AMM 05-51-67 CONDITIONAL INSPECTION . ALSO PER CREW OVERWEIGHT LANDING WAS SMOOTH NOT HARD . REF AMM 05- 51-35. ADDED LABOR DATA. ACCOMPLISHED CONDITIONAL INSPECTION REF AMM Jun 13, 2022 · N12216 · Boeing 737824SDR K11A2022071900146Stringer Clip · damagedDAMAGED STRINGER TIE MAIN DECK STA 420 STR 9RJun 12, 2022 · N733CK · Boeing 737436SDR K11A2022071900145Stringer Clip · damagedDAMAGED STRINGER TIE MAIN DECK STA 400 STR 9RJun 12, 2022 · N733CK · Boeing 737436SDR GTIA2022061336483None · noneFUME EVENT..."RAN CHECKLIST UNABLE TO IDENTIFY SOURCE. STARTED AT 1300 DESCENFLY ISOLATED IN THE FLIGHT DECK -PERFORMED FUME EVENT PACK BURN OUT IAW TSM 05-50-00 NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE AT THIS TIMEJun 12, 2022 · N507NK · Airbus A319132SDR IXXA2022061102Stringer · corrodedSTRINGER 39 L CORRODEDJun 11, 2022 · N255CM · Boeing 767200SDR NACA2022061000001None · noneAFT CARGO DOOR FRAME CORRODED. STA 1270 S-32R SECTION 46. PERFORMED MAJOR REPAIR CATEGORY B IN LH FUSELAGE SECTION 46 BULK CARGO DOOR SURROUND STRUCTURE WEB STA 1461.00 S-32L IAW B767 SRM 51-70-13. TYPICAL WEB REPAIR DETAIL 3, FULL DEPTH REPAIR REV 119 AND SEMJun 10, 2022 · N379CX · Boeing 767323SDR CALA2022061301485Plate · damagedRH FR68 AND FR66 INNER CAP JOINT TO THE GUSSET PLATES FROM STRIN GER 10 TO STRINGER 16 HAS DAMAGE INDICATION IN ALL HOLES NOTED. DAMAGE CLASSIFIED AS OUTROUND HOLES AND GOUGES. REAMED TO 0.1865" ALL HOLES AT RH FR66 AND FR68 FROM STR10 TO ST STA: ST ENG BFM R1Jun 10, 2022 · N805UA · Airbus A319131SDR IXXA2022061004Web · corrodedUPPER CARGO FRAME CORRODED.Jun 10, 2022 · N255CM · Boeing 767200SDR IXXA2022061002Panel · crackedP-33 PANEL CRACKEDJun 10, 2022 · N255CM · Boeing 767200SDR 2022FA0000285None · crackedTHE 1200 HOUR CYCLIC STICK INSPECTION (VISUAL INSPECTION FOR CRACKS IN MOUNTING AREA) WAS PERFORMED IAW THE BHT-407-MPI WITH NO INDICATIONS OF CRACKS SEEN. THE AIRCRAFT MAINTENANCE WAS COMPLETED AND THE AIRCRAFT WAS DELIVERED TO THE CUSTOMER. THE CUSTOMER HAS Jun 10, 2022 · N674RL · Bell 407SDR IXXA2022061001Panel Support · corrodedLPANEL SUPPORT CHORD CHORDJun 10, 2022 · N255CM · Boeing 767200SDR CALA2022061001483Exhaust Vent · corrodedFUS. LOWER SURFACE AFT VACUUM BLOWER EXHUST VENT PORT SURROUND F ND CORROSION. WERE ZERO TIMED WHICH SETS THE INITIAL INSPECTION AT 30,000 INSPECTIONS AT 4,000 FLIGHT CYCLES THEREAFTER. FLIGHT CYCLES SINCE THE REPAIR WAS INSTALLED AND REPETITIVE THE SKIN WAS RJun 10, 2022 · N772UA · Boeing 777222SDR CALA2022061001478Skin · noneNUMEROUS BLEND OUTS LOCATED ON LWR AFT FUSELAGE SKIN, STA 1300-1460, STRINGER 25R TO 26L. INFO ONLY INFO ONLY: SEE NR 5715602 (MCO) FOR PREVIOUS REPAIRS & CORRECT IVE ACTION. AREA IDENTIFIED PER GMM 06-35-05 LOG PAGE WAS CONVERTED TO ELB FORMAT ON APR 27, 2016Jun 9, 2022 · N75861 · Boeing 75733NSDR V0XD20220609001Skin · dentedDENT ON LH FUSELAGE SKIN BETWEEN FS10015.00- FS1031.00 AND BETWEEN STGR26L- STGR25L. CORRECTIVE ACTION: COLD WORKED/HAND DRESSED OUT DENT TO ORIGINAL CONTOUR IAW OLIVER WYMAN CAVOK EA 22-C9-53-0535 REV. A DATED 6/08/2022. DTE TO BE ACCOMPLISHED WITHIN 12 MONTJun 9, 2022 · N579NN · Cndair CL6002D24SDR IXXA2022060901Shear Tie · corrodedSHEAR TIE CORRODEDJun 9, 2022 · N307AZ · Boeing 767200SDR 2022FA0000284None · noneREPORT SUMMARY: DURING THE TRC (TECHNICAL REVIEW COMMITTEE) FOR ESN 10489 AT ROLLS-ROYCE EOS DERBY, THE AD (AIRWORTHINESS DIRECTIVE) CHECKLIST WAS COMPLETED WHICH COVERS AD 2021-07-11 THROUGH COMPLIANCE TO AK416. THE CRITERIA FOR THIS IN THE INTERNAL CHECKLISJun 8, 2022SDR CALA2022061001476Skin · crackedAD2019-11-02 EA 5310-06900 REV D OP 014 RH BS 1035 UNDERWING LONGERON FUSELAGE SKIN AREA FOUND 1EA CRACK APPROX 1" IN LENGTH. REF HX NR WO 817998, ORIG BY V906014 EA 5310-06900 REV.D OP.14 RH FUSELAGE SKIN AT BS 993-1035 S-35R INSPECTED BY V896888 RII V896375 Jun 8, 2022 · N206UA · Boeing 777222SDR CALA2022061001475Structure · crackedAD2019-11-02 EA 5310-06900 OP 031 REV D BS 1035 RH UNDERWING LONGERON 1EA CRACK FOUND AT CENTER TANK FRONT SPAR CHORD LAYER REF HX NR WO 816165, ORIG BY V914372 PREVIOUS ENTRY HAS A TYPO, SHOULD READ EA 5310-06900 OP 014 REV D EA 5310-06900 REV D OP 014 BS 103Jun 8, 2022 · N206UA · Boeing 777222SDR SROM060820221Skin · corrodedUPPER FUSELAGE OUTER SKIN AT FS X469 TO FS X553 BETWEEN STR. 12S AND 3S CHAFED ALONG WITH TO FUSELAGE FAIRING SEAL (AFT RG WING TO FUSELAGE FAIRING).Jun 8, 2022 · N792CP · Bombdr DHC8402SDR JR2R20220608698None · corrodedRH MOP SILL BETWEEN FR88 AND FR90 CORRODEDJun 8, 2022 · N85340 · Emb ERJ170200LRSDR JR2R20220608743Angle · corrodedSUPPORT ANGLE UNDER RH MOP SILL AT FR89 CORRODEDJun 8, 2022 · N85340 · Emb ERJ170200LRSDR FDEA202206071644Floor Panel · damagedAFT CARGO COMPT #152KF FLOOR PANEL WAS FOUND INSERTS DAMAGED. REPAIRED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005.Jun 7, 2022 · N724FD · Airbus A300*SDR SWIA202265964None · crackedFRAME 52 WING TO FUSELAGE RIB STRUCTURE HAS CRACK IN OUTBOARD SURFACE. (C-CHECK RO 6/23/2022) / REMOVED AND REPLACED FRAME 52 TO FUSELAGE RIB STRUCTURE REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06, CPM 51-25-00.Jun 7, 2022 · N205SY · Emb EMB110*SDR AALA202206153943Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: 1 INCH CRACK WAS FOUND ON STIFFENER AT STA 745 AND STR 27L. INSTALLED DOUBLER REPAIR PER SRM 53-00-63-2R.Jun 7, 2022 · N774AN · Boeing 777223SDR GTIA2022060936478None · noneFUME EVENT DIRTY SOCK SMELL IN THE CABIN DURING APPROACH-PERFORMED TROUBLESHOOTING PER TSM 05-50-00-810-831-A. OPERATED PACKS, ENGINES & APU, NO LEAKS NOTED. NO FUME OR DIRTY SOCK SMELL NOTED. A/C OK FOR CONTINUE OPERATION.Jun 7, 2022 · N679NK · Airbus A321231SDR CALA2022060801457Support · crackedFWD CARGO COMPARTMENT, FR30-FR34, AFT BULKHEAD, LH SIDE, LOWER SUPPORT STRUCTURE CRACKED.Jun 7, 2022 · N805UA · Airbus A319131SDR CALA2022060801462Stringer · crackedAD2019-11-02 EA 5310-06900 OP 04 BS 1035 RH BUILT-UP UNDERWING LONGERON FOUND CRACK REF HX NR WO 728392, ORIG BY V924732 EA 5310-06900 REV D OP 014 BS 1035 RH UNDERWING LONGERON REPLACED. WORK ACCOMPLISHED BY MECHANIC V893003 INSPECTED BY V897231. RII INSPECTEJun 7, 2022 · N206UA · Boeing 777222SDR CALA2022060801461Structure · crackedAD2019-11-02 EA 5310-06900 OP 014 REV D BS 1035 RH UNDERWING LONGERON 1EA CRACK FOUND AT RING CHORD LAYER REF HX NR WO 816170, ORIG V914372 BS 1035 RH UNDERWING LONGERON AREA 1EA CRACK AT RING CHORD REPLACED AS PER EC/RA 5710-02803 REV- PART 1 - INTERIM REPAIRJun 7, 2022 · N206UA · Boeing 777222SDR CALA2022060801460Longeron · crackedAD 2019-11-02 EA 5310-06900 OP 014 REV D BS 1035 RH UNDERWING LONGERON 1EA CRACK FOUND AT CENTER TANK FRONT SPAR WEB LAYER REF HX NR WO 816156, ORIG BY V914372) BS 1035 RH UNDERWING LONGERON AREA 1EA CRACK AT CENTER TANK FRONT SPAR WEB REPAIRED AS PER EC/RA 57Jun 7, 2022 · N206UA · Boeing 777222SDR SROM060720222Skin · corrodedUPPER FUSELAGE OUTER SKIN AT FS X321 TO FS X373 AND STR 12P AND 12S CHAFED.Jun 7, 2022 · N792CP · Bombdr DHC8402SDR EE4Y202260715774Tail Cone · corrodedTAIL CONE RIGHT SIDE LOWER AREA WITH CORROSION, LOCATED BETWEEN TAIL CONE AND AIRCRAFT STRUCTURE. NOTE: THE TAIL CONE WAS REPAIRED AS PER ETD2022-190-016685 REV. B GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER COO-EO-2022-15691 INSTUCTIONS (FOR ADDITIONAL Jun 7, 2022 · Emb EMB110*SDR SROM060720221Skin Panel · corrodedUPPER FUSELAGE OUTER SKIN AT FSX69 TO FSX553 AND STR12P TO STR3P CHAFED ALONG WING TO FUSELAGE FAIRING SEAL (AFT LH WING TO FUSE FAIRING).Jun 7, 2022 · N792CP · Bombdr DHC8402SDR EVCA0607222None · crackedTHERE IS AN APPROX. 1 INCH CRACK ON RH RIB AT INBOARD OUTER EDGE.Jun 7, 2022 · N894GT · Airbus A300*SDR EVCA0607221None · crackedTHERE IS AN APPROX. .40 INCH CRACK ON LH RIB AT INBOARD OUTER EDGE.Jun 7, 2022 · N894GT · Airbus A300*SDR EVCA060722Stabilator · crackedTHERE IS AN APPROX. 3 INCH CRACK ON THE HORIZONTAL STABILZER UPPER INBOARD RH SIDE.Jun 7, 2022 · N894GT · Airbus A300*SDR FDEA202206061515None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING STRINGER REPAIR FOUND ON FWD CARGO COMPARTMENT BTW FR30~31,STGR36L POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310.RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DJun 6, 2022 · N724FD · Airbus A300*SDR HALA2022060800220None · noneSHIP 380 DURING INSPECTION, CRACKS WERE FOUND ON HORIZONTAL STABILIZER FITTING HINGE LH LOWER LUG INNER FITTING AND RH LOWER LUG INNER AND OUTER FITTINGS. CORRECTIVE ACTION: REPAIRED CARRIED OUT AS PER ER/A 599829-14. (8456999)Jun 6, 2022 · N380HA · Airbus A330243SDR GTIA2022060936476None · noneFO AND FLIGHT ATTENDANTS REPORT AN ELECTRICAL SMELL COMING FROM FORWARD GALLEY-PER TSM 05-50-00-810-831-A . NO ODORS NOTICED FROM FWD GALLEYJun 6, 2022 · N948NK · Airbus A320271NSDR CALA2022060801451Fitting · noneSUPPORT TASK - REMOVE AND INSTALL PREVIOUSLY REPAIR PARTS FOR R/H STA 955 REPAIR REFER ECRA 5310-06966 - TRANSFER REFER NON-ROUTINE WO.774567 AND ORIGINATED BY EMP V897381 CABIN STA955-STA966 RBL85.9-RBL97.42 CLOSURE PANEL WEB COMPLETE AND PREVIOUSLY REPAIR PAJun 6, 2022 · N76055 · Boeing 767424ERSDR CALA2022060801450Bulkhead · noneSUPPORT TASK - REMOVE AND INSTALL PREVIOUSLY REPAIR PARTS FOR L/H STA 955 REPAIR REFER EC/RA 5310-06969 - TRANSFER REFER NON-ROUTINE WO.774560 - AND ORIGINATED BY EMP V897381 CABIN STA955-STA966 LBL85.9-LBL97.42 CLOSURE PANEL WEB COMPLETED AND PREVIOUSLY REPAIJun 6, 2022 · N76055 · Boeing 767424ERSDR CALA2022060801449Bulkhead · crackedAD2012-09-04 SUPPORT TASK EA 5340-01385 REV ORIG RHS STA955 REAR SPAR BULKHEAD FAILSAFE STRAP UNDER THE ATTACHED FITTING FOUND CRACK-TRANSFER REFER NON-ROUTINE WO.803292 AND ORIGINATED BY EMP V906449 STA955 RHS REAR SPAR BULKHEAD FAIL SAFE STRAP REPAIRED I.A.WJun 6, 2022 · N76055 · Boeing 767424ERSDR SWIA202265872None · crackedCRACK FOUND IN SMALL SUPPORT BRACKET LOCATED IN FWD AVIONICS BAY, ON FRONT SIDE OF BULKHEAD/CROSSBEAM FS280, 26" RBL, DIRECTLY UNDER STICK PUSHER CAPSTAN. CRACK MEASURES APPROXIMATELY 5/8" LONG, PASSING THOUGH BOTTOM MOST RIVET. (FILED CLOSED) REMOVED ANDJun 6, 2022 · N804SK · Cndair CL6002D24SDR CALA2022060601442Skin · dentedDENT FOUND ON INSPECTION OF BIRD STRIKE AFT OF AOA VANE. ACCOMPLISHED DETAILED VISUAL INSP IAW STEP 2 OF AVO 9718. NO PER AVO9718 PERFORMED STEP 3 HFEC PER PART 6 51-00-00 PROCEDURE REF STEP 2 OF AVO 9718. AOA SENSOR DAMAGED FURTHER DISCREPENCIES EXIST. NEED Jun 6, 2022 · N39728 · Boeing 737724SDR K11A2022071300144Frame Angle · crackedCRACK FOUND IN FUSELAGE SKIN AT LOWER AFT CORNER OF FWD GALLEY SERVICE DOOR CUTOUT APROXIMATE STATION 323 WL210Jun 4, 2022 · N733CK · Boeing 737436SDR COEA2022070604917Floorbeam · crackedWO 238445 NR 100033 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 21 R/H LONGITUDINAL FLOORBEAM CRACKED AT ATTACHMENT. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.Jun 4, 2022 · N917FX · Aerosp 262A12NORDSDR COEA2022070603917Floorbeam · crackedWO 238445 NR 100025 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM IS CRACKED FRAMES 26-27. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.Jun 4, 2022 · N917FX · Aerosp 262A12NORDSDR COEA2022070602917Floorbeam · crackedWO 238445 NR 100024 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM 33-34 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.Jun 4, 2022 · N917FX · Aerosp 262A12NORDSDR COEA2022070601917Floorbeam · crackedWO 238445 NR 100023 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM 38-39 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.Jun 4, 2022 · N917FX · Aerosp 262A12NORD
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