JASC 5230
Service difficulty reports · 13,358
Reports filed under 5230 · Cargo/Baggage Doors, 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 = '5230' 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 = '5230' 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 96FDEA00706Inner Skin · corrosionCORROSION (C53-111-02, 2) NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT EDGE 10 INCHES FROM THE BOTTOM. REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUT FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRSDR AALA960472Web · corrodedFOUND CORROSION FORWARD CARGO DOOR WEB LANDING AT FWD AND AFT ENDS. REMOVED CORRODED WEB BOTH ENDS AT FWD CARGO DOOR MANUFACTURED NEW WEBS 7075-T6 .071 AND CHORD ANGLES TREATED AND PRIMED AND INSTALLED PER SRM 51-10-1. (M)SDR 96FDEA00681Outer Skin · dentedMCD HAS 2 BULGES IN THE OUTER SKIN AT FWD AND AFT LIFT ACTUATORS. REWORKED BULGES ON MCD OUTER SKIN AT FWD AND AFT LIFT ACT TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEARANCES BETWEEN MCD OUTER SKIN AND FWD AND AFT LIFT ACT ROD ENDS IAW FEDEX MM 52SDR UPS96205786L-Angle · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 2 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 2 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-30-2, 51-30-5, 51-30-1 AND MM 51-20-151 AND 51-SDR UPS96205785L Angle · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 3 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 1 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-40-2, 51-20-21, 51-30-1 AND MM 51-20-151 AND 51SDR 96FDEA00665Skin · gougedNR 1 CARGO DOOR OUTER SKIN IS GOUGED 20 INCHES FWD THE AFT EDGE, 2 INCHES UP FROM THE BOTTOM. REMOVED GOUGE WITH A .193 DRILL BIT AND INSTALLED RIVET WET WITH SEALANT.SDR 96ZZZX2089Latch Rod · wornFORWARD BAGGAGE DOOR, FORWARD LATCH ROD IS PARTIALLY WORN THROUGH JUST BEHIND COTTER PIN HOLE.SDR 96ZZZX2061Latch Rod · wornFORWARD BAGGAGE DOOR AFT LATCH ROD IS WORN PARTIALLY THROUGH JUST BEHIND COTTER PIN HOLE.SDR VSTA9603001Seal · out of positionCOULD NOT CONTROL CABIN ALTITUDE, CABIN CLIMB TO 12,000 FEET. FOUND DOOR SEAL OUT OF CHANNEL, REINSTALLED AND SECURED. GROUND CHECKS NORMAL.SDR COMA9610106Roller · wornCARGO DOOR WILL NOT OPEN. FORWARD LOWER ROLLER CAME OUT OF THE TRACK. REPLACED DOOR ROLLER, OPERATES NORMAL.SDR CAL960421Door Pan · gougedHOU - INSPECTION FOUND A GOUGE INBOARD OF HOLD OPEN ON AFT CARGO DOOR PAN. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230C01117. (M)SDR 96FDEA00601Transverse Beam · crackedNR 0248 AND 028, FWD CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN O/B RADIUS 12 INCHES AND 24 INCHES OF FWD EDGE. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON FWD CARGO DOOR MM 52-31-61.SDR 96FDEA00600Web · crackedNR 0254 AND 029, AFT CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN RADIUS 24 INCHES AFT OF FWD EDGE OF DOOR. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON AFT CARGO DOOR.SDR 96FDEA00590Angle · crackedNR 0540 AND 045, WHILE WORKING NR 0254 FOUND AFT CARGO DOOR NR 2 FROM BOTTOM, I/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED L-ANGLE SRM 52-30-1.SDR 96FDEA00609Skin · crackedNR 3 CARGO DOOR INNER SKIN HAS A RIVNUT HOLE WITH THREE CRACKS EMANATING FROM IT 12 INCHES AFT OF THE FWD EDGE, 1.5 INCH FROM THE BOTTOM. FABRICATED AND INSTALLED EXTERNAL DOUBLER AFTER DAMAGED AREA WAS REMOVED.SDR 96FDEA00536Angle · crackedWHILE WORKING NR0254, FOUND AFT CARGO DOOR NR 3 FROM BOTTOM, O/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED AFT CARGO DOOR NR 3 O/B L-ANGLE.SDR MALA964915Corner · puncturedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR AFT LOWER CORNER PUNCTURED. REPAIRS WERE COMPLETED BY REPLACING THE LOWER AFT CORNER, PN 27-24051-003, IAW FAC SRM 51-00-00, SRM 51-30-03, AND SRM 51-40-01. (X)SDR 96FDEA00498Skin · dented(NR 0685) MAIN CARGO DOOR HAS TWO BULGES IN THE OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS. CORRECTIVE ACTION: REWORKED BULGES ON MCD OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEARANCES BETWEEN MCD OUSDR 96FDEA00493Skin · corrosion(NR 0168) CORROSION (C53-111-02-(2)), NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT, EDGE 10 INCHES FROM THE BOTTOM. ***S/D *** REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUTS. FOUND TO BE OUT OF LIMITS SDR ASOA96006Seal · defectiveMEI/ATL - INBOUND, LOST CABIN PRESSURIZATION IN CRUISE FLIGHT AT 22,000 FEET. CREW PERFORMED AN EMERGENCY DESCENT TO 5,000 FEET AND REGAINED CONTROL OF PRESSURIZATION. THE FLIGHT CONTINUED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED ASDR CAL960339Skin · dentedGSO - THE FORWARD LOWER CORNER OF FORWARD CARGO DOOR SKIN FOUND DENTED AND SCRATCHED. THE DAMAGED SKIN REMOVED OVER AN AREA OF APPROXIMATELY 6 INCHES IN DIAMETER IAW SRM 52-00-3, FIGURE 3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 52-00-3, FIGURE 3,SDR 96FDEA00482Centering Block · gougedSNRM (0690). MAIN CARGO DOOR AFT CENTERING IS GOUGED. C/A REMOVED GOUGED MAIN CARGO DOOR AFT CENTERING BLOCK, INSTALLED ONE EACH NEW BLOCK IAW FEDEX 727 SRM 51-10-1.SDR 96UAL900172Door Handle · not securedUNABLE TO CONTROL CABIN PRESSURE IN ANY MODE. AFT PIT DOOR RELEASE HANDLE UNDER PIT DOOR SEAL. SECURED HANDLE, PRESSURIZED AIRCRAFT, CHECKS NORMAL.SDR UPS96405749Latch Support · corrodedWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED FOUND CRACK IN AFT CARGO DOORWAY LOWER. SILL LATCH NR 10 INSPECTION PERFORMED ACC NDT MANUAL D6-7170, PART 6 CHAPTER 51-00-00. REPLACED TRUSS AND LATCH SUPPORT FITTING AT POS NR 10 PER EO B747-5340-0191 APP D. SDR USAA960288Pan · corrodedPIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD CARGO LOWER DOOR PAN AT STATION 370 TO 427. CORROSION TASK NR C51-53300. REMOVED AND REPLACED LOWER PAN WITH MODIFIED PAN P/N J060228-3 PER SRM 53-05 FIG 44. (M)SDR CAL960293Door Pan · crackedHOU - INSPECTION FOUND A 1.5 INCH CRACK UNDER FORWARD LOCK CAM OF AFT CARGO DOOR PAN SKIN. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. (X)SDR 96ZZZX2088Latch Rod · wornDURING INSPECTION OF AIRFRAME, FOUND EXCESSIVE PLAY IN NOSE BAGGAGE DOOR LOCK PUSHRODS. WHERE RODS ATTACH TO LOCKING MECHANISM JUST AFT OF COTTER PIN HOLE, WORN THROUGH 50 PERCENT. (AD 88-04-05 AND SB 872 AND SB 633B APPLIES TO THIS AREA.)SDR 96ZZZX2087Latch Rod · wornDURING INSPECTION OF AIRFRAME FOUND EXCESSIVE PLAY IN NOSE BAGGAGE DOOR LOCK PUSHRODS. WHERE RODS ATTACH TO LOCKING MECHANISM JUST AFT OF COTTER PIN HOLE, WORN THROUGH 50 PERCENT. (AD 88-04-05 AND SB 872 AND SB 633B APPLIES TO THIS AREA.)SDR 96ZZZX2086Door Latch · chafe doorNOSE BAGGAGE DOOR, LOWER CENTER LATCH HAS WORN A NOTCH IN FIBERGLASS DOOR, AFT OF LATCH. ALLOWS KEY TO BE REMOVED WHEN DOOR IS OPENED AND UNLOCKED. SITUATION APPLIES TO AD 88-04-05 AND SB 872.SDR 96ZZZX1779Hinge · crackedBAGGAGE DOOR WAS OPERATED AND FLIGHT CREW NOTICED BROKEN HINGE. HINGE IS WHITE METAL AND SUSPECTED TO BE OLD STYLE SLIDE LOCKS THAT CAUSED FRACTURE. CURRENTLY, S.K. KIT OF HYD ACTUATOR INSTALLED. SUBMITTER SUGGESTS WHEN LOADING, MAKE SURE BAGGAGE DOES NOT SSDR 96FDEA00406Skin · nickedMCD INNER SKIN IS NICKED AT THE AFT EDGE 46 INCHES FROM THE BOTTOM.SDR 96FDEA00405Aft Frame · nickedMCD AFT FRAME IS NICKED IN TWO PLACES. REPAIRED MCD AFT FRAME IAW FEDEX EA NR 7-5230-27785.SDR 96FDEA00404Fwd Frame · nickedMCD FWD FRAME AND INNER SKIN ARE NICKED AT CENTER OF DOOR. REPAIRED MCD FWD FRAME IAW FEDEX EA NR 7-5230-27785.SDR 96FDEA00402Inner Skin · crackedNR 3 CARGO DOOR INNER SKIN HAS A 3 INCH CRACK AFT OF THE FWD EDGE 14 INCHES FROM THE BOTTOM. REMOVED DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-2.SDR 96FDEA00401Act Supt Ftg · gougedMCD AFT ACTUATOR SUPT FITTING IS GOUGED IN THREE PLACES. MCD AFT ACTUATOR SUPT FITTING BLENDED WITHIN LIMITS PER DRW NR 65-48200 AND FEDEX SRM 51-10-6 AND 51-10-2.SDR UPS96805962Bolts · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01 (T/C 420269).SDR UPS96805821Bolts · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01.SDR UPS96205834Beam · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 5 TRANSVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 AND NR 2 SKIN VERTICAL STIFFENERS. REMOVED INNER SKIN, REMOVED NR 5 TRANSVERSE BEAM, FABRICATED NEW TRANSVERSE BEAM, AND INSTALLED IN DOOR. SDR CAL960490Frame · crackedGSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME. THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED WEB WAS CUT OUT. REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND SRM 51-30-2. (X)SDR 9605126631Seal · damagedDURING CRUISE, PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED ACCOMPANIED BY A LOSS OF PRESSURIZATION. AIRCRAFT DIVERTED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED AIR/GROUND RELAY R229, RIGHT OUTFLOW VALVE ACTUATOR AND AUTO PRESSURE CONTROLLER. REPAIRED DENTSDR 9605606601Frame · corrodedDURING P-CHECK, FOUND CORROSION ON THE BULK CARGO DOOR FORWARD LOWER CORNER FRAME. REPAIRED FRAME (P/N 65B07094-1) PER EA 66-99453.SDR USAA960214Pan · corrodedPIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SEVERAL AREAS OF LEVEL 1 CORROSION PREVIOUSLY REWORKED APPROXIMATELY 1 INCH BY 2 INCH SECTIONS FROM STATION 370 T0 427 CARGO DOOR PAN LOWER SECTION. SPLICED IN NEW LOWER PAN SECTION PER SRM 53-05 FIG 44. (M)SDR UPS96805961Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD JAMB HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0.SDR UPS96805820Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR JAMB HAS HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0.SDR ASAA9610023Upper Beam · crackedSEA - DURING D-CHECK, A 1 INCH CRACK WAS FOUND IN THE MAIN CARGO DOOR UPPER BEAM 1.3 INCHES FORWARD OF THE MAIN CARGO DOOR ACTUATOR ATTACHMENT FITTING, BS 465.5. REPAIRED PER EA 5230-01056 AND BOEING TELEX ASA-SEA-96-0069RR. (M)SDR 96014122810Door Farme · blend outFOUND DEEP BLEND-OUT AND NON-SRM REPAIR (KNIFE EDGE BLEND-OUT) ON AFT LOWER CORNER OF FORWARD CARGO DOOR FRAME. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-50-00, FIGURE 9, SHEET 1 EXCEPT EXTENDED EXTERNAL DOUBLER AFT TO PICK UP 2 ROWS BEYONSDR IXXA9631Skin · dentedDURING THE D-CHECK INSPECTION, FOUND DENTS IN THE OUTER SKIN OF THE AFT LOWER CARGO DOOR. REPAIR WAS PERFORMED PER DACO SRM 52-4-1,52-2-0, 51-1-4, 51-1-8, AND 51-1-21A. (X)SDR EISA96015Doubler · damagedTEMPORARY REPAIR AT FWD CARGO DOOR EXTERIOR. REMOVED TEMP REPAIR, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-30-02. (M)SDR EISA96011Channel · corrodedNR 3 AFT CARGO DOOR LOWER CENTER SECTION STIFFENER CHANNEL HAS CORROSION. FABRICATED NEW CHANNEL AND INSTALLED PER SRM 51-30-02. (M)SDR MWEA96047Skin · crackedDURING C-CHECK, FOUND AFT CARGO DOOR SKIN CRACKED NEXT TO DOOR HANDLE CUTOUT. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 52-05 FIG 30.
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