JASC 5321

Service difficulty reports · 49,402

Reports filed under 5321 · Fuselage Floor Panel, 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 = '5321'
  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 08FDEA03289Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 UM, IS CRUSHED, CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03288Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 TH, LOWER SURFACE IS CRACKED AND PUNCTURED ON THE UPPER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03287Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 UH, IS CRACKED AND CRUSHED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03286Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 WH, IS CRACKED AND HAS A HOLE IN THE LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03285Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 YG, IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03284Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 XG; IS CRACKED; HAS EDGE DAMAGE AND PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03283Floor Panel · damagedMAIN CARGO DOOR PANEL NR 252 VF; IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03282Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 VF; FWD END IS CRACKED AND HAS SEVERAL PUNCTURES. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03280Floor Panel · damagedMAIN CARGO DOOR PANEL NR 251 BH, CENTER CUT-OUT IS CRACKED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03279Floor Panel · crackedMAIN CARGO DOOR PANEL NR 251 AH; UPPER AND LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03278Floor Panel · puncturedMAIN CARGO DOOR PANEL NR 261 UF, LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03277Floor Panel · puncturedMAIN CARGO DOOR PANEL NR 261 RF, FWD OUTBD LOWER SURFACE IS PUNCTURED. FABRICATED PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G".Aug 6, 2008 · N664FE · Airbus A300F4605RSDR FDEA200808053254Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Aug 5, 2008 · N318FE · Doug DC1030FSDR FDEA200808053253Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Aug 5, 2008 · N318FE · Doug DC1030FSDR UPS08853152Floor Panel · gougedINSPECTION TYPE:C1 FLOOR PANEL FROM STA 660 TO STA 760 RBL 24 TO 44 HAS 14 INCH GOUGE PENETRATING OUTER SKIN. FABRICATED AND REPLACED FLOOR PANEL IAW EO DC8-5320-9691C.Aug 5, 2008 · N715UP · Doug DC871FSDR UPS08153043Floor Panel · puncturedINSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL APPROX FR26 IN AFT CABIN HAS PUNCTURE. REPAIRED MAIN CABIN FLOOR PNL, NR 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A.Aug 5, 2008 · N153UP · Airbus A300F4622RSDR 08FDEA03254Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.Aug 5, 2008 · N318FE · Doug DC1030FSDR 08FDEA03253Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.Aug 5, 2008 · N318FE · Doug DC1030SDR 08FDEA03214Floor Panel · damagedMAIN DECK FLOOR BOARD 232 LG IS PUNCTURED. REMOVED DAMAGE; PREPPED FOR LAY UP. MAT ID'D; LAYED UP REPAIR PLYS AND STARTED CURE. COMPLETED CURE AND SANDED IAW A300-600 SRM 53-10-21.Aug 1, 2008 · N728FD · Airbus A300B4622RSDR UPS08M53094Floor Panel · corrodedINSPECTION TYPE:2C RCB FLOOR PANEL PART NUMBER WSPO785-501 HAS AREAS OF CORROSION. REMOVED AND REPLACED FLOOR PANEL IAW UPS EO MD11-5330-27218-C.Jul 31, 2008 · N281UP · Doug MD11FSDR F3LA200800537Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 161CF WAS PUNCTURED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 161CF IAW SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE FLOOR PANEL 161CF IAW THE REQUIREMENTS OF AMM 25-00-00-370-001.Jul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800536Floor Panel · puncturedDURING C3 C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 162CF, WAS PUNCTURED IN SEVERAL PLACES. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 162CF IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE FLOOR PANEL IAW THE RJul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800535Floor Panel · puncturedDURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT TRANSITION PANEL, 152AE, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152AE IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITIJul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800534Floor Panel · puncturedDURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152XG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANJul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800533Floor Panel · puncturedDURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152WG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANJul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800532Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT PIT FLOOR PANEL, 151VG, WAS DAMAGED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 151VG IAW SRM 53-02-00 FIGURE 204. MAINT PAINTED THE FLOOR PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE RJul 31, 2008 · N927FR · Airbus A319111SDR F3LA200800531Floor Panel · scratchedDURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT LOWER TRANSITION PANEL 131BF HAS DEEP SCRATCHES ALONG BOTTOM EDGE. MAINTENANCE REMOVED DAMAGED AREA AND CLEANED IAW THE REQUIREMENTS OF SRM 53-02-00 PAGE 214. MAINTENANCE FILLED DAMAGED AREA IAW THJul 31, 2008 · N927FR · Airbus A319111SDR UPS08853089Floor Panel · damagedINSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 880-1000 LBL 44.60 HAS 3EA MISSING & 1 EA DAMAGED INSERT. REPLACED 4EA INSERTS IAW DPS 1.9023 REPAIR 4.3-1 PAGE 4.Jul 30, 2008 · N715UP · Doug DC871FSDR UPS08853088Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 RBL 44.60 HAS 2 EA CRUSHED AREAS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691.Jul 30, 2008 · N715UP · Doug DC871FSDR UPS08853083Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 LBL 25.44 IS CRUSHED AT FWD & AFT ENDS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691.Jul 30, 2008 · N715UP · Doug DC871FSDR UPS08853069Floorboard · damagedINSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 800-1000 RBL 25.44 HAS 1 EA MISSING & 3EA DAMAGED INSERTS. REMOVED AND REPLACED 4EA INSERTS PER B DPS 1902-3 REPAIR 4.3.1 PG 4.Jul 30, 2008 · N715UP · Doug DC871FSDR UPS08853067Floorboard · crackedINSPECTION TYPE:C1 COURIER AREA FLOORBOARDS 2EA ARE DELAMINATED AND CRACKING. SANDED, CLEANED AND REPAIRED 2EA COURIER AREA FLOORBOARDS AT DELAMINATED AND CRACKED AREAS IAW SRM 51-01-19.Jul 30, 2008 · N715UP · Doug DC871FSDR 08FDEA03169Floor Panel · damagedMAIN CABIN FLOOR PANEL NR 242 HK IS CRACKED. FABRICATED NEW FLOORBOARD NR 242 HK IAW FEDEX DWG SRZ 25-005; REV "G".Jul 30, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03141Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCHES TO 97 INCHES IS BROKEN. THIS SDR WAS GENERATED IN ERROR. FOR DETAILS SEE SDR TRACKING NR 08-3140.Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03147Floorboard · damagedCABIN FLOOR BOARD HAS A DENT FROM FRAME 26 TO 28 AND RBL 47 INCHES TO 67 INCHES. FABRICATED NEW FLOORBOARD NR 232 VH IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03145Floor Panel · damagedMAIN DECK FLOORBOARD NR 232 TG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 TG IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03144Floor Panel · damagedMAIN DECK FLOOR BOARD NR 232 YG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 YG IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03143Floor Panel · damagedMAIN DECK FLOORBOARD, RIGHT SIDE NR 252 CF IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 CF IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03142Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 30; LBL 30 INCH IS CRUSHED. FABRICATED NEW FLOORBOARD NR 231 YG IAW DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03140Floor Panel · damagedMAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCH TO 97 INCH IS BROKEN. FABRICATED NEW FLOORBOARD NR 241 LK IAW FEDEX DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03138Floor Panel · damagedMAIN CABIN FLOOR PANEL BETWEEN FRAMES 40 TO 43 AND LBL 57 INCH TO 77 INCH IS BROKEN. FABRICATED NEW FLOOR BOARD NR 241 TH IAW DWG SRZ 25-005; REV "G".Jul 29, 2008 · N664FE · Airbus A300F4605RSDR F3LA200800528Floor Panel · damagedDURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 242FF WAS DAMAGED IN SEVERAL PLACES. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, PARAGRAPH 3, SOLUTION B, PAGE 245.Jul 28, 2008 · N927FR · Airbus A319111SDR F3LA200800526Floor Panel · damagedDURING C-CHECK, INSP NOTED THE FLOOR PANEL 251FF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAIRED FLOOR PANEL 251FF IAW SRM 53-02-00 FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 28, 2008 · N927FR · Airbus A319111SDR F3LA200800527Floor Panel · damagedDURING C-CHECK, INSP, NOTED THE FLOOR PANEL 251LF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAIRED FLOOR PANEL 251LF IAW SRM 53-02-00 PARAGRAPH 8.A FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 28, 2008 · N927FR · Airbus A319111SDR UPS08853155Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1120 RBL 14. FABRICATED AND REPLACED FLOOR PNL IAW EO DC8-5320-9691C.Jul 27, 2008 · N715UP · Doug DC871FSDR UPS08853086Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1180 RBL 14. REMOVED FLOOR PANEL IAW MM 53-21-02, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW EO DC8-5320-9691C, AND MM 53-21-02.Jul 27, 2008 · N715UP · Doug DC871FSDR UPS08853080Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 57. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW MM 53-21-02, EO DC8-5320-9691.Jul 27, 2008 · N715UP · Doug DC871FSDR UPS08853079Floor Panel · puncturedINSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL PUNCTURED STA 1220 RBL 58. REMOVED FLOOR PANEL IAW MM 53-21-02, REPAIRED PER SRM 51-01-19, REINSTALLED PANEL IAW 53-21-02.Jul 27, 2008 · N715UP · Doug DC871FSDR UPS08853077Floor Panel · crushedINSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 36. REMOVED PANEL, FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW MM 53-21-02, AND EO DC8-5320-9691C.Jul 27, 2008 · N715UP · Doug DC871FSDR UPS08853076Floor Panel · damagedINSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1500 LBL 29. REMOVED PNL, FABRICATED AND INSTALLED REPLACEMENT FLOOR PNL IAW MM 53-21-02, EO DC8-5320-9691C.Jul 27, 2008 · N715UP · Doug DC871F
Back to JASC 5321