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 F3LA200800521Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT TRANSITION PANEL 151FH WAS DAMAGED. MAINT REPAIRED TRANSITION PANEL 151FH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111SDR F3LA200800522Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151DH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111SDR F3LA200800523Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151CH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151CH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111SDR UPS08853010Floor Panel · crackedINSPECTION TYPE-C1, COCKPIT FLOOR PNL 680 HAS 1 FASTENER HOLE WITH IMPROPER E.D. AND 1 FASTENER HOLE CRACKED TO EDGE. CUTOUT CRACKED AREA IAW SRM 53-02-00 FIG 23, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00,51-01-21.Jul 24, 2008 · N715UP · Doug DC871FSDR UPS08152980Floor Panel · crackedINSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 262BM IS CRACKED ON THE AFT END. REPAIRED MAIN CABIN FLOOR PNL NR 262BM IAW SRM 53-10-20 TABLE 201 PARA 8A.Jul 24, 2008 · N153UP · Airbus A300F4622RSDR UPS08852973Floor Panel · damagedINSPECTION TYPE-C1, FLOOR PANEL 626D HAS DAMAGE AT 2 CORNERS AS MARKED EDGE DAMAGE OUT OF LIMITS IAW, SRM 53-2-0 FIG 1F, FABRICATED AND REPLACED FLOOR PANEL SKIN IAW DWG 3619130 AND SRM 51-1-21.Jul 24, 2008 · N715UP · Doug DC871FSDR UPS08852900Floor Panel · damagedINSPECTION TYPE-C2, COURIER AREA FLOOR PANEL F27 SPONGEY FABRICATED NEW FLOOR PANEL IAW, SRM,. 53-2-1, 51-1-8, 53-21-1, 51-1-21.Jul 24, 2008 · N752UP · Doug DC871FSDR UPS08153051Floor Panel · delaminatedINSPECTION TYPE-5YR, MAIN CARGO COMPT FLOOR PNL 231GH AT FR27 LT SIDE, FOUND DELAMINATED. REPAIRED MAIN CARGO COMPT FLOOR PNL 231GH AT FR27 LT SIDE REF SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622RSDR UPS08152982Floor Panel · delaminatedINSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL NR 231QJ AT FR 26 LT SIDE FOUND DELAMINATED. REPAIRED MAIN CABIN FLOOR PNL NR 231QJ AT FR 26 LT SIDE IAW A300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622RSDR UPS08152979Floor Panel · crackedINSPECTION TYPE-5, YR MAIN CARGO COMPT RT FLOORBOARD NR 262DM CRACKED BOTTOM SIDE AT TIE- DOWN CUT OUT. REPAIRED MAIN CABIN FLOORBOARD NR 262DM IAW SRM 53-10-20 FIG 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622RSDR UPS08152977Floor Panel · brokenINSPECTION TYPE:5 YR, MAIN CABIN COMPT, FLOOR PANEL 252BN AT FR. 72 FOUND BROKEN. REPAIRED MAIN CABIN FLOOR PANEL 252BN AT FR 72 IAW SRM 53- 10-20 FIG 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622RSDR UPS08152909Floorboard · crackedINSPECTION TYPE-5 YR MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK CRACKED AT TOP SURFACE AND BOTTOM T/E AT FR. 38.2. REPAIRED MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK AT FR.38.2 REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622RSDR UPS08152981Floor Panel · crackedINSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 231SG IS CRACKED AT THE FWD END. REPAIRED MAIN CABIN FLOOR PNL NR 231SG IAW SRM 53-10-20 TABLE 201 PARA 8A.Jul 22, 2008 · N153UP · Airbus A300F4622RSDR UPS08152978Floor Panel · crackedINSPECTION TYPE: 5 YR, MAIN CABIN FLOOR PANEL NR 252BN IS CRACKED AT FWD END. REPAIRED MAIN CABIN FLOOR PANEL NR 252BN FWD CRACK IAW SRM 53- 10-20 FIG 201 PARA 8.Jul 22, 2008 · N153UP · Airbus A300F4622RSDR F3LA200800518Floor Panel · gougedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF WAS GOUGED AND A PREVIOUS REPAIR WAS PEELING UP. MAINT REPAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPJul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800509Floor Panel · peelingDURING C-CHECK, INSP NOTED THE PREVIOUS REPAIRS PEELING LOOSE ON THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151UG. MAINT REPAIRED TRANSITION PANEL 151UG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (AJul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800510Floor Panel · puncturedDURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800511Floor Panel · puncturedDURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151BE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151BE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800512Floor Panel · gougedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT FORWARD LT LOWER TRANSITION PANEL 151AE WAS GOUGED IN THE CENTER OF THE PANEL. MAINT REPAIRED TRANSITION PANEL 151AE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLEJul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800513Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT UPPER TRANSITION PANEL 151FE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800514Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT LOWER TRANSITION PANEL 151DE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151DE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800515Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL 161NF WAS PUNCTURED SEVERAL TIMES. MAINT REPAIRED FLOOR PANEL 161NF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.(A)Jul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800516Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF WAS PUNCTURED IN THE CENTER, COVERED WITH TAPE. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPJul 22, 2008 · N942FR · Airbus A319111SDR F3LA200800517Floor Panel · puncturedDURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT LOWER TRANSITION PANEL 161BF WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 161BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 22, 2008 · N942FR · Airbus A319111SDR UPS08152907Floor Panel · crackedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL Z261BH IS CRACKED. REPAIRED MAIN CABIN FLOOR PANEL Z261BH REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 22, 2008 · N153UP · Airbus A300F4622RSDR UPS08152906Floor Panel · gougedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251XJ HAS SEVERAL GOUGES. REPAIRED CABIN FLOOR PANEL NR Z251XJ REF. A-300-600 SRM 53-10-20 TABLE 2 01 PARA. 8A.Jul 22, 2008 · N153UP · Airbus A300F4622RSDR UPS08152905Floorboard · gougedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251BN HAS SEVERAL GOUGES. REPAIRED MAIN CABIN FLOORBOARD NR Z251BN REF. A-300-600 SRM 53-10-20 TABLE 201 PARA. 8A.Jul 22, 2008 · N153UP · Airbus A300F4622RSDR F3LA200800499Floor Panel · brokenDURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION WAS COMPLETED ON EMPIRE AERO CENTER NON ROUTINE NR 9642. UPON COMPLETION OF THE REPAIR IT WAS INJul 18, 2008 · N918FR · Airbus A319111SDR F3LA200800507Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.Jul 17, 2008 · N807FR · Airbus A318111SDR F3LA200800506Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.Jul 17, 2008 · N807FR · Airbus A318111SDR F3LA200800502Floor Panel · delaminatedDURING C2 C-CHECK, INSPECTION NOTED THE TOP LAYER DELAMINATED ON FLOOR PANEL 251NF. MAINTENANCE REMOVED DELAMINATED LAYER AND APPLIED MYLAR PATCH IN ACCORDANCE WITH A319 SRM 53-02-00.Jul 17, 2008 · N943FR · Airbus A319112SDR UPS08153044Floor Panel · damagedINSPECTION TYPE:5 YR, MAIN CARGO DECK POS P4R, FLOOR INTERIM REPAIR. REPAIRED MAIN CABIN FLOOR PNL NR 241LH REF SRM 53-10-20, TABLE 201, PARA 8A.Jul 17, 2008 · N153UP · Airbus A300F4622RSDR 08FDEA02916Floor Panel · corrodedMAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .042 INCH, REMAINING .035', REMOVED .007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TOOL ID AAR 9800 CAL DJul 16, 2008 · N273FE · Boeing 727233SDR F3LA200800498Floor Panel · puncturedDURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161BF WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Jul 15, 2008 · N941FR · Airbus A319112SDR F3LA200800497Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS NON ROUTINE HAS THE PANEL NUMBER INCORRECTLY INDICATED. THE DAMAGED PANEL IS 151UG. MAINTENANCE REPAIRED DAMAGE TO PANEL 151UG IAW THE REQUIJul 15, 2008 · N943FR · Airbus A319112SDR F3LA200800496Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Jul 15, 2008 · N943FR · Airbus A319112SDR F3LA200800495Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151DE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Jul 15, 2008 · N943FR · Airbus A319112SDR F3LA200800494Floor Panel · puncturedDURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (SJul 15, 2008 · N943FR · Airbus A319112SDR F3LA200800493Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151AE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (SJul 15, 2008 · N943FR · Airbus A319112SDR F3LA200800492Floor Panel · puncturedDURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS IS EITHER A DUPLICATE WRITE-UP (161UG- NON ROUTINE C047467) OR SHOULD HAVE BEEN WRITTEN AS 152UG, WHICH HAD DAMAGE ALSO. THE DAMAGE REPAIR FOJul 15, 2008 · N943FR · Airbus A319112SDR 08FDEA02889Floorboard · damagedMAIN CARGO FLOOR PANEL 242 RG IS CRACKED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F.Jul 15, 2008 · N674FE · Airbus A300F4605RSDR ABXA080210Floor Panel · corrodedUPPER CARGO SUB FLOOR PANEL BENDED BEYOND LIMITS APPROXIMATELY STA 412, RT BUTT LINE 60. REMOVED AND REPLACED PANEL IAW B767 SRM 51-40-02. (A)Jul 11, 2008 · N773AX · Boeing 767281SDR F3LA200800463Floor Panel · damagedDURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131CG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800462Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800460Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800459Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800458Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800457Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800455Floor Panel · damagedDURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111SDR F3LA200800453Floor Panel · damagedDURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 11, 2008 · N940FR · Airbus A319111
Back to JASC 5321