JASC 5310
Service difficulty reports · 38,479
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 LR7A2026091803918Tee Fitting · crackedDURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO CARGO UNDERFLOOR SKIN HORIZONTAL ATTACH TEE AT 797.0E TO FS817.0E, RBL10, WL127-145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70SDR LR7A2026091803916Plate · crackedDURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FUSELAGE LOWER BELLY SKIN AFT SKID PLATE CRACKED AT FS797.0E, LBL10 TO RBL 10, WL126. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-7SDR LR7A2026091803906Cap · crackedDURING SCHEDULED A CHECK INSPECTION UNDER JOB CARD HA1200 THERE WAS TAIL STRIKE DAMAGE FOUND TO FS797.0E BULKHEAD LOWER CAP LBL12 - RBL12, WL128. / REPAIRED IAW LAC MEA 382-53-26-147. NR#0010.SDR JGVR20260918001Door Frame · corrodedREMOVED MULTIPLE AREAS OF CORROSION ON THE MAIN ENTRY DOOR INNER FRAME, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED BLENDED AREAS PER TECHNICAL DISPOSITION.SDR AALA202610209698Crease Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CABIN WET AREA RH CREASE ANGLE CORRODED STA 986.5 TO STA987 RBL52. REMOVED AND REPLACED IAW BOEING DRAWING 147A8501AND AARD 51-00-05-1.SDR CALA2026101220277Gusset · crackedFRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.SDR CALA2026101220275Gusset · crackedFRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.SDR CALA2026092219644Door Sill · corrodedL2 DOOR SILL HAS CORROSION JUST INBD OF AFT GIRT BAR FITTING. EVALUATED & REPAIRED L-2 DOORSILL JUST INBD OF AFT GIRT BAR FITTING, REPAIR/EVAL FOUND TO BE CATEGORY A NO FURTHER ACTION REQUIRED IAW SRM 53-41-14-300-001, & 53-41-14-283-002.SDR DALA2026092105246Door Sill · corrodedPAX CABIN, CREW DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. C/A: PERFORMED REPAIR AT PASSENGER CABIN, CREW DOOR CUTOUT LOWER SILL BEAM I/B FLANGE FROM FR67+290MM TO FR68 I/A/W DELTA ER/A #636581-14 SECTION I REV ORIGINAL DATED 11SDR DALA2026092105245Beam · corrodedPAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR67+430MM Y1292. REPLACED LONGITUDINAL BEAM P/N: D5347218820400 AT Y1292 BTW FR68 TO FR69 I/A/W A 320 SRM TASK 51-72-11-911-001 PARAG 2 REV: 158.00 DATED 01-JUN-26. AND REF DWGS: 53474180, D534SDR SWIA2026091777216Pressure Panel · scratchedTRANSFER FROM EAML 1993541 TRANSFERRED FROM CAMP 33010415 IDENTIFIED A GOUGE ON LT PRESSURE FLOOR STRUCTURE PANEL AT FS549 APPROXIMATELY 12 X 132 X 003 FLIGHT 1. BLENDED SURFACE SCRATCH ON THE PAINTED LH PRESSURE FLOOR SILL STRUCTURE PANEL AT FS549 IAW SRM 5SDR DALA2026091805214Antenna · demodificationFOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER (P/N 8485-5310-404-1) BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 636936-14. (1817872) (AIRCRAFT GROUNDED).SDR CALA2026091819548Door Frame · crackedRIGHT EMERGENCY EXIT, FWD LOAD TRANSMITTING PROFILE SHOWS SIGNS OF CRACKING. REMOVED & REPLACED THE FRAME SEGMENT IAW SRM 51-72-11-911-001, & SRM 51-42-11-001.SDR SWAA2026101282859Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75, WL 208.1. REPLACED THE CROSSBEAM, BS 540 BTWN BL0 - RBL 24.75 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG143A0060, SHEET 36, REV A.SDR SWAA2026101278616Crossbeam · crackedCRACK ON CROSSBEAM, BS 540, BL 0 - LBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A0060, SHT 36, REV A.SDR DALA2026092205308Door Frame · corrodedDURING H CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-02C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE AFT CARGO DOOR SURROUND STRUCTURE C01343028- 103 LOWER SILL WAS FOUND WITH CORROSION. THE CORROSION FOUND IS ON THE OUTER SURFSDR DALA2026092205307Door Frame · corrodedAFT SERVICE DOOR SURROUND - FR76 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A636471-14 PRI REV. 2SDR DALA2026092205306Door Frame · corrodedAFT SERVICE DOOR SURROUND - FR74 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A 636471-14 PRI REV. SDR DALA2026091705188Coupling · corrodedLEVEL 2 CORROSION, PAX CABIN LONGITUDINAL BEAM AT FR68 Y1292 COUPLING AREA, I/B UPPER COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200-337. REPLACED COUPLING AT FR68 Y1292 LOCATED I/B UPPER IAW SRM 51-72-11-911-001 PARAG 2. REV 158. AND DWGSDR 2A6R2026091675404Angle · corrodedACFT WAS FOUND TO HAVE CORROSION DAMAGE TO THE FRAME 2 ANGLE PN L533M1043427 (APPROX. FS 2675 MM). REPLACEMENT WAS NOT AVAILABLE WITHIN SCHEDULED RTS AND PART WAS FABRICATEDSDR QMLA2026091620069Deck Plate · crackedDURING INSPECTIONS THE MGB DECK WAS FOUND TO BE CRACKED FROM THE ELECTRICAL CONNECTOR AFT TO THE FIREWALL AND FORWARD OF THE ELECTRICAL CONNECTOR APPROX. 2 INCHESSDR IPXA2026100354024Gusset · corrodedWHILE EVALUATING JCW T3F18E009L4M8, FOUND CORROSION AT BS 1885, BULKHEAD FWD SIDE SERVICE DOOR LATCH FITTINGS. INSTALLED 4EA NEW GUSSETS P/N 148N6614U9 B/N 4512167, PN 148N6614U8 B/N 4512168 P/N 148N6614-7SAAU, P/N 148N6614-10SAAU AND 2EA FITTINGS AT APU LOWSDR AALA202609307326Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN, FLOORBOARD BREAK ANGLE SUPPORT CRACKED, STATION 540 RBL2. INSTALLED NEW BREAK ANGLE SUPPORT IAW IPC 53-42-11-66 AND AARD 51-00-05-1.SDR AALA202609305771Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN, FLOORBOARD SUPPORT ANGLE CRACKED, STATION 540 LBL2. INSTALLED NEW BREAK SUPPORT PN 143A5240-35 IAW IPC 53-42-11-66 AND AARD 51-00-05-1.SDR IPXA2026092350550Tee Angle · broken- BROKEN - SPLICE TEE, LOWER FACE OF KEEL BEAM AT LOWER PANEL NO.149AL FWD SUPPORT, NEAR STA 962, LBL 5. REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.96. INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO.145T8629 SH.2 REV.A.SDR DALA2026092205302Door Sill · damagedFWD CARGO DOOR SURROUND STRUCTURE, LWR SILL AREA (AREA COVERED BY SCUFF PLATES), SKIN PANEL, SILL. COMPLIED WITH ER/A 636422-14 PRI REV 0 AND FINAL ER/A 636422-14 REV ORIGINAL SECTION I PERMANENT REPAIR. PART REPLACED. (LP# 1814859; AIRCRAFT WAS GROUNDED)SDR DALA2026092205301Waste Box · corrodedWASTE BOX RIGHT SIDE INNER LIP HAS CORROSION. -M- REF. CORROSION SSI: 53-61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS .125'. MATERIAL REMOVED .034". REMAINING THICKNESS .091". (LP# 1814774; AIRCRASDR DALA2026092205300Waste Box · corrodedWASTE BOX FWD RIGHT CORNER HAS CORROSION MULTIPLE PLACES AND SURROUNDING RIGHT HINGE FITTING. -M- -P- REF. CORROSION SSI: 53- 61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS .125'. MATERIAL REMOVED .SDR SWAA2026092157039Sill Drain · odorCREW REPORTED A BAD ODOR COMING FROM ALL ENTRY AND SERVICE DOORS. REMOVED DEBRIS FROM DRAINS ON FLOOR NEAR BOTH ENTRY AND SERVICE DOORS IAW AMM 38-31-00.SDR IPXA2026091761112Floor Skin · corrodedMDC FLOOR SKIN STR AT FR26, RH SIDE OF Y1456 IS CORRODED. FAULT-STR- FAULT CREATED TO CAPTURE NEW REVISION OF EO 98291. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98291-REQ1 REV. 2 AND VT-MAE EA EA 300-5313-27-A4577, REV. A.SDR SIMA20260914003Support Rib · crackedCENTER FUSE II WFF SUPPORT RIB CRACKED, COMPLY WITH ERS-EJ-53MR-5547SDR SWAA2026101287845Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB AT RBL 40 BTW BS 663 - 675. PERFORMED PERMANENT REPAIR ON THE PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2, FIGURE 203, SHTS 2 & 3.SDR IPXA2026100338118Roller Track · corrodedFWD CARGO COMPARTMENT, FLOOR STRUCTURE FR 20 TO 25 RT AT -Y140, BALL MAT TRACK BASE OTBD AREA HAS SEVEN SPOTS OF CORROSION. THE SPOTS OF CORROSION BENEATH BALL MATS AT -Y140 BTW FR 20 & FR 25 HAVE BEEN IDENTIFIED & BLENDED OUT IAW SRM 53-10-15-101, FIG 103, ASDR IPXA2026100338127Roller Track · corrodedFWD CARGO FLOOR STRUCTURE, BALL MAT BASE HAS SEVERAL SPOTS OF CORROSION AT Y140 (LT) BETWEEN FR 20 & FR 25. BLEND OUT COMPLETED IAW A300-600 SRM 51-74-10/201, ALL SPOTS FOUND WITHIN LIMITS IAW SRM 53-10-15.SDR IPXA2026100437064Roller Track · corrodedFWD CARGO FLOOR STRUCTURE, BALL MAT BASE HAS SEVERAL SPOTS OF CORROSION AT Y140 (LT) BETWEEN FR 20 & FR 25. BLEND OUT COMPLETED IAW A300-600 SRM 51-74-10/201, ALL SPOTS FOUND WITHIN LIMITS IAW SRM 53-10-15.SDR SWAA2026100705700Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL45.5 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 143A5240, SHEET 1, REV-.SDR SWAA2026100727826Crossbeam · crackedCRACKED BREAK PANEL, BS 540 BTWN RBL 24.75 - BL 0. REPLACED THE BREAK PANEL IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, DWG 143A5240, SHEET 13, REV A.SDR SWAA2026100572681Stub Frame · crackedCRACKED R1 DOOR STUB FRAME, 0.1" ABOVE SEAL DEPRESSOR, LENGTH: 1.5". REMOVED AND REPLACED R1 DOOR UPPER STUB FRAME IAW SRM 51-40-02 AND DWG 141A8370, REV D, STEP 2, ITEM 1.SDR AALA202609174582Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED STANCHION ANGLE AT STA 867 LOWER STRUCTURE AREA. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-40-02.SDR DALA2026091505145Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66 Y765. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y 765 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT DRAWISDR DALA2026091505144Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66+70MM Y1292. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-101 AT Y1292 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NATSDR QMLA2026091520066Bracket · crackedCRACK FOUND ON REINFORCEMENT BRACKET AND ON MGB DECKSDR 2026FA0000691Panel · corrodedCORROSION WAS FOUND IN THE NOSE LANDING GEAR ACTUATOR TUNNEL AROUND A HYDRAULIC LINE STANDOFF. DURING THE REPAIR A HOLE WAS MISLOCATED NEAR THE DEFECT. THE CORROSION WAS REMOVED AND NDT WAS ACCOMPLISHED TO VERIFY REMAINING MATERIAL THICKNESS AND THAT NO CRACKSSDR SWAA2026102182814Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0060, SHT 36, REV A.SDR SWAA2026102191104Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 24.75 - 44.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5240, SHT 12, REV-.SDR SWAA2026102180435Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, REV-. SSDR CALA2026091519437Retainer · crackedRIGHT W/W FWD CUT OUT SEAL RETAINER HAD TWO CRACKS. PANEL 198BR WAS REMOVED TO GAIN ACCESS IAW SRM 51 -40-02-OG, SUPPORT CHANNEL WAS REMOVED SRM 51-40-02-OG, REPLACED SUPPORT. CHANNEL IAW SRM 51-40-02, & INSTALLED NEW BRACKET IAW SRM 51-40-02, AND REINSTALLSDR IPXA2026102206792Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 61 Y0 RH CLS HAS CORROSION. INSTALLED OF CLS ADAPTER ON MDC FR61 Y0. R/H IAW SRM 51-41-21-001.SDR IPXA2026102206731Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 65 RH BETWEEN -Y1456 AND -Y1959, CLS HAS CORROSION. VERIFIED INSTALLATION OF CLS ADAPTER ON MDC FR65 R/H -Y1456 AND -Y1959 IAW SRM 51-41-21-001.SDR SWAA2026101961698Door Frame · crackedFED UPPER DOOR SURROUND CUTOUT FRAME WAS CRACKED AT BS 312, STR 5L. THE DOOR FRAME WAS REPAIRED IAW EA M-22-153-01244 LBL 33 BETWEEN S5L & S6L.
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