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.
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
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 MASA20210923451Skin · corrodedLOWER FUSELAGE SKIN BETWEEN FS485.00 - FS501.00 & STGR26R - STGR26L WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1C, EA 72-2021-169SDR KCSA202109221107Intercostal · crackedAPPROX 6.5" CRACK ON VERTICAL STABILIZER SKIN TO FUSELAGE INTERCOSTAL AT FWD EDGE OF AFT VERT STAB BLADE SEAL APPROX STA 2521 RIGHT HAND SIDE SKIN OF STAB IAW SB 747-532651 R1SDR MASA20210922450Skin · dentedFWD FUSELAGE SKIN PANEL BETWEEN FS485.0 -FS501.0, STGR23R -STGR24R WAS FOUND TO HAVE A DENT. PERFOMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, ITEM 1, 53-31-01-101-003-A04, EA81-2021-074.SDR JJBA2021092200021None · noneTHE PASSENGER FWD CABIN LH FLOOR OMEGA DOUBLER HAS CORROSION ON THE FWD SURFACE BETWEEN FR 14 TO FR 18. REMOVED AND REPLACED DIGITAL PLATE ON PASSENGER FWD CABIN LH FLOOR BETWEEN FR 14 TO FR 18.SDR JJBA20210922020None · noneCORROSION AT MULTIPLE LOCATONS FOUND ON RH CENTER AISLE LONGITUDINAL BEAM LOCATED BETWEEN FR29-FR36 Y.00+8. REMOVED AND REPLACED BEAM ASSEMBLY ON RH CENTER AISLE LOCATED BETWEEN FR29-FR36 Y.00+8.SDR JJBA20210922014None · noneAFT CARGO COMPARTMENT AT DOOR CUT-OUT LOWER FRAME HAS 3 SCREW HOLES SHOWING SIGNS OF CORROSION BETWEEN FRAME 65 - 68. REMOVED AND REPLACED AFT CARGO COMPARTMENT, DOOR CUT-OUT LOWER FRAME BEAM BETWEEN FRAME 65-68SDR JJBA20210922013None · noneTHE PASSENGER ENTRY DOOR WAY FWD FRAME LOWER SPLICE TO FLOOR BEAM IS CRACKED. REMOVED AND REPLACED LOWER REINFORCEMENT SPLICE TO FLOOR BEAM PASSENGER ENTRY DOOR WAY FWD FRAME.SDR A6WA202111157970None · corrodedR/H FLOOR SILL AT FS 559+88, FS 559+101.75, AND FS 600 AT RBL 41 AROUND NUT PLATE HOLES HAVE CORROSION. FAA IDENTIFIED DURING AGING AIRCRAFT INSPECTION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION AT 4 EACH AREAS RBL 41: FS 559+88 (P1)= 1.4"L X 1"WSDR SWIA202162446None · corrodedENTRANCE STORAGE COMPARTMENT FWD MOUNT FITTING CORRODED, FS280.00+8, LBL-36 (C-CHECK RO 11-05-2021) REMOVED, REPLACED AND INSTALLED NEW MOUNT FITTING P/N SH670-32148-3 REF. CRJ700 SRM 51-42-21-001-001-A01, AND DWG SH670-32120 REV. D COMPLIED WITH TASK CARSDR SWIA202162443None · cracked*POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN BETWEEN FS 169.00 €“ 202.00, PANEL 212AR CUTOUT ON LOWER AFT CORNER (C-CHECK RO 11-05-2021) REPLACED SKIN WITH NEW REF BOMBARDIER DWG# CC670-33035 REV D, CRJ700 SRM'S 51-42-06-001-001 A01, 51-42-21-001-001 A01, 5SDR IPXA2021101975114Beam · crackedINSPECTION TYPE:3CL-3 DOOR PLUG TOP HORZ. BEAM IS CRACKED AT THE FWD. END.REMOVED AND REPLACED BEAM IAW SRM 51-35-01 & 51-33-01. (MINOR)SDR IPXA2021101975113Beam · crackedINSPECTION TYPE:3CR-3 DOOR PLUG TOP HORZ. BEAM IS CRACKED AT THE AFT END.REMOVED AND REPLACED BEAM IAW SRM 51-35-01 & 51-33-01. (MINOR)SDR IXXA20211017068None · crackedRIGHT STUB BEAM CRACKED AT STATION 903.5 RBL89.REPAIRED RIGHT CRACKED STUB BEAM AT STATION 903.5 RBL 89 IAW
ENGINEERING ORDER 53-767-7702.SDR JJBA20210921011None · noneCENTER FUSE IV, UNDER FLOOR, LH GUSSET BTW FRAME 59-61 CORRODED. OMEGA BEAM BLENDED OUT OF LIMITS BTW FR 60-61. CENTER FUSE IV BTW FR 60-61, LH OMEGA BEAM REPAIRED AND GUSSET REPLACED. NO CORROSION FOUND.SDR JJBA20210921033None · noneLH FUSELAGE AT FR60 SILL AREA, SMALL PLATE FOR WATER SUPPLY HAS A CRACK AT NUT PLATE. INSTALLED EWIS PROTECTION ON LH FUSELAGE AT FR60 TO FR 59. REMOVED CABLE AND DUCT FAIRING FOR ACCESS. REMOVED DAMAGED SMALL PLATE, LOCATED AND DRILLED NEW PLATE. RE-INSTALLEDSDR CALA2021092201651Frame · corrodedBULK CARGO COMPARTMENT FR 61-62 STR33R HAS LIGHT SURFACE CORROSION (REMOVE CORROSION AND CHECK LIMITS) DAMAGE LOCATED AT STR 33R FR 60 - 62 BLENDED IAW SRM 51-74-00. BLENDED AREA MEASURES L=15" W= 1.5" D=.047", ORIGINAL THICKNESS .063", REMAINING MATERIAL .016SDR CALA2021092201650Stiffener · crackedAD2017-17-16 - EA5310-07143 REV D - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 OT 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 1" IN LENGTH. PLS PRINT AND ACCOMPLISHED REPAIR PER OP003 TRANSFER REF. NON-ROUTINE LP 9130578 AND ORIGINATED BY SDR CALA2021092201649Stiffener · crackedAD 2017-17-16 - EA 5310-07143 REV D ,RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 1" IN LENGTH. PLS PRINT AND ACCOMPLISH REPAIR PER OP004 TRANSFER REF. NON-ROUTINE LP 9130574 AND ORIGINATED BY SDR CALA2021092201648Stringer · corrodedA3BN-05-3-6013 DURING INSPECTION OF THE FWD CARGO COMPARTMENT, FOUND CORRODED FLOOR RIVETS FROM STRINGER 38 L/H TO STRINGER 38 R/H FROM FRAME 24 TO FRAME 34, FURTHER EVALUATION REQUIRED. REMOVED AND REPLACED CLEATS ON FRAME 32 FROM STRINGER 41-42R PER AIRBUS SDR CALA2021092201645Frame · dentedFWD CARGO BELTFRAME DENTED AT STA 500H, BETWEEN S24R & S25R. REF FLEET CYCLE LOG PAGE 9784721, LOG PAGE FOR DIP ONLY SEE FLEET CYCLE LOG PAGE 9784721 FOR DETAILS OF WORK ACCOMPLISHE D. TRIMMED OUT DENT AREA AND REPAIRED FRAME PER SRM 53-30-07-2R- 2 REPAIR 2 ALSDR CALA2021092201644Frame · corrodedAFT CARGO FR67 AFT SIDE BETWEEN STR 41R-42L HAS CORROSION ON OUT ER FLANGE PER NR 9296815 / 20815 GEN BY N078570. REMOVED CORROSION FROM FR67 AFT SIDE BETWEEN STR 41R-42L AND REP AIRED FRAME IAW SRM 53-41-12-300-014. INSTALLED ALTERNATIVE FAST ENERS IAW SRM 51SDR A6WA202109217884Frame · corrodedFWD AND AFT FACE, AND LWR LEG OF FRAME AT FS 605.00 CORROSION BETWEEN STR 26R AND 23R ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM FWD AND AFT FACE OF FRAME AT FS 605.00 BETWEEN STR 26R AND 23R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS .050,SDR A6WA202109217883Frame · corrodedAFT FACE OF FRAME AT FS 589.0 SEVERAL SPOTS OF CORROSION BETWEEN STR 25R AND 27. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM AFT FACE AT FS 589.0 BETWEEN STR 25R AND 27R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS .050, THICKNESS REMAINING .SDR SWIA202163779None · crackedWINDSHIELD SUPPORT POST BETWEEN CO- PILOTS LEFT SIDE WINDSHIELD AND FORWARD CO- PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) REMOVED CRACKED CO-PILOT WINDSHIELD SUPPORT POST AND REPLACED WITH NEW WINDSHIELD SUPPORT POST PER SDR SWIA202163778None · crackedWINDSHIELD SUPPORT POST BETWEEN PILOTS LEFT SIDE WINDSHIELD AND FORWARD PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) COMPLETED STRUCTURAL MAJOR REPAIR (**RII**) TASK CARD 51-900-1002-SKY MTCM REV: REV DATE:06 OCT 20 . / REMOSDR A6WA202110217921Skin · dentedAFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + 8Ï¿½ RH STR24 + 1.75Ï¿½, FS640.00 + 9Ï¿½ RH STR24 + 1.25Ï¿½ AND FS640.00 + 10Ï¿½ RH STR24 + 2.70Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + SDR HNAA2021101800515None · noneFUSELAGE FRAME 25 CRACKED BETWEEN STRINGERS 15R AND 16R EVALUATION .... REMOVED, FABRICATED AND INSTALLED NEW SERVICEABLE FR25 FRAME SECTION (LOCATED FROM STR 15R TO STR 20R ) AND INSTALLED INTERNAL "U" SHAPED SPLICE DOUBLER IAW EMB145 SRM 53-00-04RE, ITEM 4, SDR HNAA2021101800505None · noneSUPPLEMENTAL INFORMATION - DUPLICATE DISCREPANCY - NEW DISCREPANCY - CENTER BEAM SEAT TRACK #5 IS CORRODED AT NUMEROUS AREA'S .... PERFORMED BLEND OUT OF DAMAGE IAW EMB 145 SRM 51-10-03 AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW EMB 145 SRM 53-00-11. ESDR A6WA202110187906Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.200Ï¿½ X W = 1.100Ï¿½ X DSDR A6WA202110187903Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 9.00Ï¿½ X W = 0.600Ï¿½ X D = 0.016Ï¿½. PERFSDR HNAA2021101800504None · noneSERVICE DOOR ENTRANCE SILL HAS CORROSION .... PERFORMED DOUBLER REPAIR ON SERVICE DOOR ENTRANCE SILL CENTER AND AFT NUTPLATES IAW EMB-145 SRM 53-21-02.SDR QMLA2021101120051Tail Boom · crackedFOUND 16MM CRACK IN L/H SIDE OF TAIL ROTOR GEARBOX MOUNTING ACCESS HOLE ON TAILBOOM VERTCAL FINSDR R61A2021100600787Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CENTER FUSELAGE II LH IB CABIN SEAT TRACK UPPER IB FLANGE BETWEEN FR53 AND FR54. REPLACED CENTER FUSELAGE II LH IB CABIN SEAT TRACK BETWEEN FR43 AND FR59 WITH NEW IAW SRM 51-41-02, 51-42-01, 51-42-02 AND 51-43-SDR CALA2021092201629Fitting · corrodedCORROSION UNDER NUTPLATE LOCATED AT FWD CARGO DOOR THRESHOLD (AF T END) FR 28, STR 39R (A3NB-05-3-6016). GENERATED BY V925611, AT HAECO LCQ PER NR 9296486 (20486). REMOVED AND REPLACED 1EA CORNER SUPPORT FITTING PART NO. D532313 3520000, PO NO. 1100049.1 IAW ASDR SWIA202162883None · corrodedCORRODED DOUBLERS AT FS 533 AND FS 581 STGR 25L-26L (C-CHECK RO 11/28/2021) CORROSION ON DOUBLERS AT FS 533 AND FS 581 STGR 25L-26L WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DOUBLERS WITH NEW SERVICEABLE PARTS IAW CRJ 700 SRM 51-42-22-001-00SDR HNAA2021101800500None · noneCARGO ENTRANCE SILL HAS CORROSION .... REMOVED AND REPLACED CARGO ENTRANCE SILL IAW EMB 145 SRM 51-40-02.SDR JJBA20210919027None · noneRH FR19, Y=479 SUSPECT CORROSION ON HAT-BEAM. REMOVED AND REPLACED HAT BEAM AT Y=479 RH FR19 CORROSION LEVEL 2SDR IXXA20211007062None · corrodedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT IN COMPLIANCE OF ATI TASK CARD 53-556-00-01 MAINTENANCE IDENTIFIED CORROSION AT AFT LOWER CARGO DOOR CUTOUT LOWER FAIL SAFE CORD AT APPROXIMATELY RBL 44 STA 1250-1275 CORROSION OUT OF LIMITS-LEVEL 2.
SDR CALA2021092001612Seat Track · corrodedB777-53-3-0139 - BULK CGO AREA STA1937 TO STA1958 S-35L TO S-36L VACUUM BLOWER EXHAUST VENT SKIN FOUND CORROSION. TRANSFER REF. NON-ROUTINE LP 9131017 AND ORIGINATED BY V897008. BULK CARGO AREA STA 1937 TO STA 1958 STR 35L TO STR 36L VACUUM BLOWER EXHAUST VENTSDR SWIA202162125None · chafedAFT BELLY EXTERNAL SKIN EXISTING DOUBLER REPAIR HAD CHAFE APPROX. LOCATION FS977 STGR 27 (C-CHECK RO 10/30/2021) EXISTING REPAIR FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR AT FS977 STGR 27 IAW REO 670-53-00-290 REV-F, DATED 2019-04-26. COMPLIED WITH TASK SDR R61A2021100600785Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CENTER FUSELAGE I RH IB CABIN SEAT TRACK IN MULTIPLE AREAS BETWEEN FR23 AND FR34. REMOVED AND REPLACED SEAT TRACK ON CFI RH IB SIDE BETWEEN FR23 AND FR34 IAW EMB SRM 51-43-03 AND 51-43-04.SDR R61A2021100400780Support · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III CORROSION ON PANEL SUPPORT AT FR84 RBL 46. CENTER FUSELAGE III PANEL SUPPORT AT FR84 RBL 46 REPLACED WITH NEW IAW EMB SRM 51-41-01, 51-41-02 AND 51-43-02.SDR SWIA202164054None · mislocatedUPPER FORWARD ROLLER ON CARGO DOOR IS MISSING THE ROLLING PART (C CHECK RO 1/20/22) / REPLACED UPPER FORWARD ROLLER ASSEMBLY ON CARGO DOOR IAW CRJ 200 AMM 52-31-00 / TORQUE WRENCH-AG1132-5AUG2022SDR SWIA202162458None · elongatedELONGATED FASTENER HOLE, FS280.00 BULKHEAD ANGLE STIFFENER RBL-38.50 (C-CHECK RO 11-05-2021) REMOVED, REPLACED AND INSTALLED NEW ANGLE SUPPORT FS280.00, RBL-38.50 P/N CC670-34106-4 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, ANDSDR R61A2021100600788Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK CORROSION FOUND ON FWD LOWER FUSELAGE SHEAR CLIP AT FR 17 AND BTWN STR 28-27L. MX REPLACED SHEAR CLIP PN 170-03870-001 IAW SRM 51-41-01. SEE AAR NRC# 4500961-1000-0055. AC REMAINS IN YQG FOR COMPLETION.SDR QMLA2021092220046Angle · crackedON 9-17-2021 VICCA-5002 11088 N7UC CENTRAL FUSELAGE CRACK L/H SIDE ACFT TT 6202+04
WHILE PERFORMING THE 06-5300-EO-3328 A109-INSP OF CENTRAL FUSELAGE FRAME ASSY AT STA 1815, I DISCOVERED A CRACK ON THE INBOARD L/H SIDE, PICS HAVE BEEN SENT OUT. THIS CRACK SDR QXEA2021092000444Panel · damagedHEARD NOISE AT CRUISE, ASSURED IT TO BE SPEED TAPE OVER GROUND POWER PLUG . SUSPICION CONFIRMED ON POST FLIGHT WALK AROUND. REMOVED FROM SERVICE. REMOVED & REAPPLIED SPEED TAPE OVER EXTERNAL POWER ACCESS DOOR AS REQUIRED. CDL CLEARED ON LOGPAGE 918622 BY REMOSDR SWIA202163283None · dentedEXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 621 AND FS 640, STGR 4L TO STGR 5L. (C CHECK RO 12/28/2021) REPAIRED EXTERNAL FUSELAGE SKIN DENT BETWEEN FS 621 AND FS 640, STGR 4L TO STGR 5L.IAW MHIRJ REO 601R-53-61-7729 REV -- DATED 10-25-2021, FORM 337 AND MAJOSDR SWIA202162236None · gougedLARGE GOUGE IN A/C EXTERIOR SKIN AT APPROX FS913,STGR 27. (C-CHECK RO 11/04/2021) COMPLIED WITH THE REPAIR AT A/C EXTERIOR SKIN APPROX FS913 STGR27 REF-CRJ-900 MHIRJ REO 690-53-51-309 REV -- DATE 2021-09-28 AND REO 670-53-00-290 REV--F DATE 2019-04-26. / CSDR A6WA202110227924Skin · dentedTWO DENTS ON AFT FUSELAGE SKIN FS755.00 - 67.50 DATUM AND STR26L AND STR26R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED TWO DOUBLER REPAIRS TO THE AFT FUSELAGE SKIN AT FS755.00 - 67.50 DATUM AND STR26L AND STR26R. DENT DIMENSION LH S26 L= 2.300Ï¿½ X W =
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