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.

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 & 51-70Sep 18, 2026 · N405LC · Lkheed 382GSDR 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 & 51-7Sep 18, 2026 · N405LC · Lkheed 382GSDR 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.Sep 18, 2026 · N405LC · Lkheed 382GSDR 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.Sep 18, 2026 · N318QS · Emb EMB505SDR 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.Sep 17, 2026 · N811NN · Boeing 737823SDR 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.Sep 17, 2026 · N836UA · Airbus A319131SDR 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.Sep 17, 2026 · N836UA · Airbus A319131SDR 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.Sep 17, 2026 · N836UA · Airbus A319131SDR 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 11Sep 17, 2026 · N353NW · Airbus A320212SDR 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, D534Sep 17, 2026 · N353NW · Airbus A320212SDR 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 5Sep 17, 2026 · N957SW · Cndair CL6002B19SDR 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).Sep 17, 2026 · N981AT · Boeing 717200SDR 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.Sep 17, 2026 · N836UA · Airbus A319131SDR 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.Sep 16, 2026 · N201LV · Boeing 7377H4SDR 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.Sep 16, 2026 · N201LV · Boeing 7377H4SDR 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 SURFSep 16, 2026 · N301DU · Airbus BD5001A11SDR 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. 2Sep 16, 2026 · N301DU · Airbus BD5001A11SDR 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. Sep 16, 2026 · N301DU · Airbus BD5001A11SDR 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 DWGSep 16, 2026 · N353NW · Airbus A320212SDR 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 FABRICATEDSep 16, 2026 · N110VU · Urocop EC135T2SDR 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 INCHESSep 16, 2026 · N102HN · Urocop EC135P1SDR 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 LOWSep 15, 2026 · N463UP · Boeing 75724APFSDR 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.Sep 15, 2026 · N960NN · Boeing 737823SDR 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.Sep 15, 2026 · N960NN · Boeing 737823SDR 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.Sep 15, 2026 · N316UP · Boeing 76734AFSDR 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)Sep 15, 2026 · N301DU · Airbus BD5001A11SDR 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; AIRCRASep 15, 2026 · N301DU · Airbus BD5001A11SDR 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 .Sep 15, 2026 · N301DU · Airbus BD5001A11SDR 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.Sep 15, 2026 · N8888M · Boeing 7378SDR 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.Sep 15, 2026 · N136UP · Airbus A300F4622RSDR SIMA20260914003Support Rib · crackedCENTER FUSE II WFF SUPPORT RIB CRACKED, COMPLY WITH ERS-EJ-53MR-5547Sep 14, 2026 · N217NN · Emb ERJ170200LRSDR 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.Sep 14, 2026 · N201LV · Boeing 7377H4SDR 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, ASep 14, 2026 · N146UP · Airbus A300F4622RSDR 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.Sep 14, 2026 · N146UP · Airbus A300F4622RSDR 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.Sep 14, 2026 · N146UP · Airbus A300F4622RSDR 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-.Sep 14, 2026 · N208WN · Boeing 7377H4SDR 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.Sep 14, 2026 · N208WN · Boeing 7377H4SDR 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.Sep 14, 2026 · N8305E · Boeing 7378H4SDR AALA202609174582Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED STANCHION ANGLE AT STA 867 LOWER STRUCTURE AREA. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 51-40-02.Sep 14, 2026 · N960NN · Boeing 737823SDR 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 DRAWISep 14, 2026 · N353NW · Airbus A320212SDR 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 NATSep 14, 2026 · N353NW · Airbus A320212SDR QMLA2026091520066Bracket · crackedCRACK FOUND ON REINFORCEMENT BRACKET AND ON MGB DECKSep 14, 2026 · N102HN · Urocop EC135P1SDR 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 CRACKSSep 14, 2026 · N541QS · Cessna 680ASDR 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.Sep 13, 2026 · N8658A · Boeing 7378H4SDR 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-.Sep 12, 2026 · N8658A · Boeing 7378H4SDR SWAA2026102180435Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, REV-. SSep 12, 2026 · N8658A · Boeing 7378H4SDR 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 REINSTALLSep 12, 2026 · N18112 · Boeing 757224SDR 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.Sep 11, 2026 · N146UP · Airbus A300F4622RSDR 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.Sep 11, 2026 · N146UP · Airbus A300F4622RSDR 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.Sep 11, 2026 · N8657B · Boeing 7378H4
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