JASC 5310
Service difficulty reports · 38,511
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 AALA202604235638Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR LOWER SILL EXISTING REPAIR AT FR 68 AND S23L. MAINTENANCE REMOVED EXISTING REPAIR AND INSTALLED A NEW REPAIR ON LOWER SILL PER SRM 53-41-14-300-001.SDR AALA202604229403Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BREAK ASSEMBLY PANEL AT STA 540 BETWEEN LBL 24 AND LBL 45. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202604223465Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BREAK ASSEMBLY PANEL AT STA 540 AND LBL 3. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202604225158Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BREAK ASSEMBLY PANEL AT STA 540 AND RBL 3. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR DALA2026042202568Window Frame · crackedDURING CCK AT QRO, AFTER INSPECTION OF COCKPIT WINDOWS PER WC 5600-2492, LOWER FWD CORNER WAS FOUND CRACKED AT LT WINDOW FRAME. CRACK WAS REPAIRED PER ERA 633661-14AD. (LOG 1555729 - AIRCRAFT WAS GROUNDED).SDR SWIA2026042076866Pressure Deck · corrodedLEFT CABIN, PRESSURE FLOOR SKIN CORRODED AT ONE LOCATION BTWN BS 473.15, & FS 461. REPAIRED THE LT PRESSURE FLOOR SKIN IAW REO 601R-53-41-666, REV C. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042076862Pressure Deck · corrodedLEFT CABIN PRESSURE DECK CORRODED AT TWO LOCATIONS BTWN BS 449.85 & 461. REMOVED CORROSION ON LT CABIN PRESSURE DECK IAW REO 601R-53-41-666, REV-C, STEP 1.2. & 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.047" ALLOWABLE BLENSDR SWIA2026042076861Pressure Deck · corrodedRIGHT CABIN PRESSURE DECK CORRODED AT ONE LOCATION BTWN BS 484 & 499. REMOVED CORROSION ON RT PRESSURE DECK IAW REO 601R-53-41-666, REV C. & SKYCARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.047" ALLOWABLE BLEND DEPTH 0.0SDR SWIA2026042076853Pressure Deck · corrodedRIGHT PRESSURE DECK CORRODED AT ONE LOCATION, BS 449.85. REPAIRED RT PRESSURE DECK IAW REO 601R-53-41-666, REV-C. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042076851Pressure Deck · corrodedLEFT CABIN PRESSURE DECK CORRODED AT TWO LOCATIONS, BS 424. REPAIRED LT CABIN PRESSURE DECK AT BS 424 IAW REO 601R-53-41-666, REV C. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042076849Pressure Deck · corrodedLEFT CABIN, PRESSURE DECK CORRODED AT ONE LOCATION BETWEEN BS 424 & 439. REMOVED CORROSION ON THE PRESSURE DECK IAW REO 601R-53-41-666, REV C, STEP 1.2. & TASK CARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.042" ALLOWABLESDR SIMA20260420001Seal Depressor · bentFWD PAX DOOR CUTOUT FWD SEAL DEPRESSOR FRAME IS BENT IN 3 SPOTS. (MAJOR REPAIR) RAR FWD PAX DOOR CUTOUT FWD SEAL DEPRESSOR IAW ERJ 170 SRM 51-40-08SDR CALA2026042315628Angle · corrodedLEFT FLOOR CREASE BEAM AT L1 DOOR FROM STA 348 TO STA 280 HAS CORROSION AND BARE METAL IN SEVERAL AREAS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW INNER CHORD REF B737 NG SRM 51-40-05 AND BAC DWG 141A8110 REV A.SDR CALA2026042115552Door Frame · crackedRIGHT MLG CENTER DOOR FRAME CRACKED NEAR THE LOWER FORWARD ATTACH POINT. REMOVED RT MLG DOOR ASSY IAW AMM 32-13-11-000-803, REPAIR PARTS IAW SRM 52-80-02-2R-2 AND SRM 51-40-02-0G-0 .REINSTALLED RT MLG DOOR ASSY IAW AMM 32-13-11-420 -803. ACCOMPLISHED RT MLG SDR U2RA2026051200028Longeron · cracked2EA CRACK INDICATON FOUND AT BS2598 BULKHEAD R/H S-11R LONGERON P/N 65B02522-4 PER BOEING SR MUA-MUA-26-0026-22B REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12-2026 AND PER BCS 202603210023-0016SDR CALA2026042915829Fitting · crackedFLIGHT DECK, WINDSHEILD CONTINUITY FITTING LT AND RT HAS CRACK I NDICATION APROX. .40 INCH FROM CENTER POST. PERFORMED INTERIM REPAIR IAW ECRA 5311-03450 AND REO-L25896 REV IR WITH NO DEVIATIONS. PAR T 2: ACCOMPLISH INITIAL INSPECTIONS AT FRONT WINDSHIELD FSDR AALA202604280098Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE, CRACK DIRECTION: 5 OCLOCK (VIEW AFT LOOKING FWD) . D1-D2= 0.212 INCH; AD 2020-19-03 (L= 0.212 IN). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON RH LASDR SWIA2026041876277Crossbeam · crackedRIGHT CROSSBEAM AT BS 280 CRACKED ON UPPER FLANGE. REPLACED RT CROSSBEAM AT BS 280 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV K.SDR SIMA20260418003Crossbeam · corrodedSSI 53-23-005. CABIN FLOOR FR 84 CROSSBEAM CORRODED AT LH SIDE. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED PERMANENT REPAIR TO CABIN FLOOR FR 84 CROSSBEAM AT LH SIDE IAW ERS-EJ-53MR-5443SDR VNAA202606060002Striker · dented1605FH PERM REPAIR - REPAIR TO PAX DOOR SEAL STRIKER - EXTENSION TO SRM 53-21-23-201-004-A01. PAX DOOR SEAL STRIKER WAS REPAIRED PER SRM 53-21-23-201-006-A01.SDR AALA202606033294Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 RIGHT AND #7 DOORSTOP FITTING. REPAIRED FRAME PER EA 374446.SDR IPXA2026051567724Structure · corrodedAFT CARGO-FRAME 58 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED (07 EA) RECEPTACLES FROM ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN Y450 AND Y2462 ,FOR ACCESS IAW A300-600 SRM 51-40-21-001. REMOVED DAMAGE (07 SDR SWAA2026052090782Pressure Deck · crackedCRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK WEB, RBL 42, BS 663 - 675. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK, BS 663 - 675, RBL 30 - 60 IAW SRM 53-40-51-2R-2,. REPAIR 2.SDR HNAA2026052000417Door Frame · damagedMAIN DOOR LOWER FRAME AFT NUTPLATE HOLE DOUBLER HAS NO DTA INFORMATION. REPAIR WAS ACCOMPLISHED IAW ETN-EM-52-041. RE-ACCOMPLISHED DOUBLER FOR REPAIR OF MAIN DOOR LOWER FRAME AT AFT NUT-PLATE HOLE IAW SRM 52-10-04RE, ITEM 3, FIG 201, SHEET 3 AND EO1-52-26-019SDR IPXA2026050267675Crossbeam · corrodedAFT CARGO-FRAME 54.2 CEILING STRUCTURE FROM LT TO RT SIDE HAS CORROSION AROUND MULTIPLE HOLES. INTALLED NEW PROFILE-CROSS FRAME 54.2 STA Y-450 TO Y450 AND Y-450 TO Y-1959 IAW SRM 51-40-21-001.SDR VNAA20260418017Web · corrodedWEAR AND CORROSION ON WEB BTW STGR 26L TO 25L AND FS 517.00 TO FS 565.00 ALSO STGR 26L TO 25L & FS 629.00 TO FS 661.00+ 16.00 AT FWD AND CENTER BAGGAGE BAY DOOR AREA. WEB BTW STGR 26L TO 25L AND FS 517.00 TO FS 565.00 ALSO STGR 26L TO 25L AND FS 629.00 TO FSSDR VNAA20260418009Beam · crackedCRACK ON LONGITUDINAL BEAM RBL12 FS280. CRACK ON LONGITUDINAL BEAM RBL12 FS280.00 WAS REPAIRED PER REO 690-53-11-2163 REV. --SDR IPXA2026061056763Splice Angle · gougedMAIN CARGO DECK RT FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS (2 EA) SPOTS OF TOOLING DAMAGE ON AFT FACE ON SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV.SDR AALA202604249791Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: WINDSHIELD FRAMING CENTER POST LH HALF FOUND CRACKED IN AREA A. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE IAW EA 372184.SDR F3LA202604200404Door Sill · corrodedREFERENCE LTPR NR 5001479407-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON R/H AFT DOORSILL. REQUIRES TO BE EVALUATED AS PER A320N SRM 53-41-14-283-002 REV 48. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOORSILL FRSDR F3LA202604200403Door Sill · corrodedREFERENCE LTPR NR 5001479406-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON L/H AFT DOORSILL. REQUIRES TO BE EVALUATED AS PER A320N SRM 53-41-14-283-002 REV 48. CORROSION WAS REMOVED AND WAS FOUND IN ALLOWABLE LIMITS (CATSDR FDEA202604170458Crossbeam · damagedEXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA6-5310-T0306792 DUE TO A FASTENER HOLE MISS DRILL, SDR SWIA2026041676633Post · corrodedFLIGHT COMPARTMENT LT DOOR POST HAS SIGNS OF CORROSION. PERFORMED REPAIR AT FLIGHT COMPARTMENT LT DOOR POST IAW SRM 53-00-00, & 51-21-11, 51-25-06, IAW AMM 20-70-00, IAW REO 670-53-11-745 REV -A, IAW REO 670-53-11-2321 REV --.SDR HNAA2026052000414Doubler · not openedFUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 70/71 STR 16R/18R HAS NO REPAIR INFORMATION. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FOR FUSELAGE EXTERNAL SKIN REPAIR BETWEEN FR 70/71 STR 16R/18R IAW EMB 145 ETD2026-145-007284 AND EO1-53-26-0217.ER BESDR REXA2026050700525Landing · crackedCRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR. RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01SDR CALA2026042015538Angle · corrodedL1 DOOR CUTOUT LOWER SILL AREA,, ONE ANGLE ATTACHED TO THE INNER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN BS 328 AND BS 344. . REMOVED, LOCATED, DRILLED AND INSTALLED NEW INNER ANGLE IAW SRM 51-40-05 AND DWG 141A8112 REV-.SDR DALA2026042002484Door Frame · corrodedAFT PASSENGER DOOR SURROUND.FWD FRAME (FR74) HAS 4 FASTENERS HOLES WITH CORROSION .-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/003 00419 COMPLIED WITH ER/A 632912-14 PRI REV 0, REV 1, AND FINAL ER/A 632912-14 REV ORIGINAL. ORIGINAL THISDR DALA2026042002483Door Frame · corrodedAFT PASSENGER DOOR SURROUND.AFT FRAME (FR76) HAS 13 FASTENERS HOLES WITH CORROSION .-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/002 00418 COMPLIED WITH ER/A 632912-14 PRI REV 0, REV 1, AND FINAL ER/A 632912-14 REV ORIGINAL. ORIGINAL THSDR DALA2026041702436Door Frame · damagedFR68 DOOR FRAME R/H, DOOR STOP FITTINGS 1,2,3,4,5,6 AND 7 LOCATIONS WERE FOUND THE HOLES (4 HOLES IN EACH FITTING) COMMON TO THE FRAME WEB GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER (6.38MM/0.251") "ACTION REQUIRED PRIOR TO FURTHER FLIGHT, ENGINEERING EVASDR JR2R20260416662Gusset · corrodedAFT WET AREA GUSSET AT FR90 LBL10 CORRODED. REPLACEDSDR JR2R20260416653Crossbeam · corrodedFR17 CROSSBEAM AT RBL24 CORRODED. REPAIREDSDR SWIA2026041576339Angle · crackedCO-PILOT SIDE POST OTBD LWR ANGLE CRACKED. REPLACED CO-PILOT SIDE POST OTBD LOWER ANGLE IAW DWG 601R33007, REV -U, SRM 51-42-21, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SIMA20260415005Retainer · gougedFWD CARGO DOOR LOWER SEAL RETAINER IS GOUGED IN SEVERAL SPOTS. (MAJOR REPAIR) REMOVED AND REPLACED FWD CARGO DOOR LOWER SEAL RETAINER IAW ERJ 170 SRM 51-40-08.SDR REXA2026051500584Door Sill · corrodedCORROSION ON LOWER SILL BTS FS 1009 AND FS 1035 (APPROX) AT AFT CARGO COMPT DOOR CUTOUT. LOWER SILL BTS FS 1009 AND FS 1035 (APPROX) AT AFT CARGO COMPT DOOR CUTOUT WAS REPAIRED PER CRJ-900 SRM 53-61-23-201-001-A01.SDR SWAA2026051389820Strap · out of toleranceFRAME STRAP AT BS 328 STR 20R-22R DOES NOT MATCH CONFIGURATION OF FIG 5 CUSTOMER CARD 5311-I-17336NG STEP 13, FOUND REPAIR AT BS 328 FRAME BETWEEN STRINGERS S-19 R AND S-24R CARD REQUIRES CONTACT ENGINEERING USING ESR OR TSR. VERIFIED PERFORM OP TEST OF IND SDR SWAA2026051289623Crossbeam · crackedPANEL BREAK AT BS 540 CRACKED AT RBL2 WL208. REMOVED AND REPLACED PANEL BREAK AT PASSENGER BS540 RBL2, WL 208 IAW SRM 51-40-02 AND DWG 143A0060.SDR SWAA2026051289624Crossbeam · crackedPANEL BREAK AT BS 540 CRACKED AT LBL2 WL208. REMOVED AND REPLACED PANEL BREAK AT PASSENGER BS 540, LBL 2 IAW SRM 51-40-02 AND DWG 143A0060.SDR SIMA20260415003Beam · corrodedCORROSION AROUND HIGH LOCK ON RH AFT UPPER BEAM AT FR 87, Y=10.- 748" (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION AROUND HI-LOK ON RH AFT UPPER BEAM AT FR 87, Y=10.748" PER EMB 175 SRM 51-10-03, UPON EVALUATION FOUND AREA TO BE L=1.1" W=.- 800" H=.050SDR SIMA20260415004Beam · corrodedCORROSION ON AFT LH BEAM AT FR 87, Y=-10.748 (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORRODED AREA ON AFT LH BEAM AT FR 87, Y=-10.748" PER EMB-175 SRM 51-10-03. BLENDED AREA MEASURES (L=1.8?, W=.9?, H= .022?). ORIGINAL MATERIAL IS .070? REMAINING MATERIAL ISDR DALA2026042202553Door Frame · damagedER/A 633159-14AD ISSUED FOR REPAIR TO FR68 RT FRAME WEB AT DOOR STOPS. FOLLOW ON ACTION REQUIRED. PERFORM SECTION II EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1545988). AIRCRAFT
Back to JASC 5310