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 IPXA0563689Floor Panel · damagedREF BILL OF WORK TS2930 MAIN CARGO DECK FLOOR PANEL, PN 143N5457-85, PO POSTION 2 6TH FROM THE LT HAS DAMAGE BEYOND LIMITS IAW SRM B757-53-0 0-50-1A1, MFG NEW PANEL IAW EO B757-5320-9692 AND INSTALLED FLOOR PANEL IAW AMM 53-01-01-04.Nov 27, 2010 · N464UP · Boeing 75724APFSDR DALA1033783211Floor Panel · damagedDURING L CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131HF DAMAGED. REMOVED FLOOR PNL 131HF IAW AMM 53-22-14-020-050. FLOOR PNL 131HF FABRICATED IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 131HF IAW AMM 53-22-14-400-001.Nov 26, 2010 · N311US · Airbus A320211SDR IPXA0663704Floor Panel · damagedMAIN CARGO FLOOR PANEL REQUIRES FABRICATION IAW EO B767-5320-9693E. THIS IS A MAJOR REPAIR. ACCOMPLISHED FABRICATION OF MAIN CARGO FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693E.Nov 25, 2010 · N310UP · Boeing 76734AFSDR IPXA0663686Floor Panel · damagedMAIN DECK FLOOR PANEL, PN 145T5876-68 IS DAMAGED. FABRICATED NEW FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693-G.Nov 25, 2010 · N310UP · Boeing 76734AFSDR DALA1033773211Floor Panel · damagedDURING L-CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131AF DAMAGED. REMOVED FLOOR PNL 131AF IAW AMM 53-42-14-020-050. FABRICATED NEW FLOOR 131AF IAW SRM 53-02-00.Nov 24, 2010 · N311US · Airbus A320211SDR DALA1100829864Floor Panel · crackedAFT CARGO CTR FLOOR PANEL NR 3 HAS A CRACK IN RADIUS OF DOOR CUTOUT AREA. REMOVED CRACK BY TRIMMING AREA. NDT VERIFIED NO CRACK EXIST IAW NDT SPM 06-10-01. FABRICATED DOUBLER SEALED & INSTALLED REPAIR PARTS. ALL WORK ACCOMPLISHED IAW EA98-201837 & SRM (51-1Nov 23, 2010 · N773NC · Doug DC951SDR DALA1033649855Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN CORROSION IN SEVERAL PLACES ON FLOOR PANEL 63. CUT OUT DAMAGED AREA 1.5 SQ IN NDT VERIFIED DAMAGE REMOVAL IAW NDT SPM 06-10-01. FABRICATED & INSTALLED FILLER & DOUBLER FROM7075-T6 .020 THICK PO 1022528 IAW DC9 SRM 53Nov 23, 2010 · N764NC · Doug DC951SDR DALA1033519853Floor Panel · corrodedDURING M-CHECK FOUND COCKPIT, FLOOR PANEL NR15 HAS CORROSION SEVERAL PLACES ON TOP OF PANEL. REMOVED CORROSION ORIG MAT .025 REMOVED .014 REMAINING .011 OUT OF LIMITS IAW SRM 53-01 FIG 1 LOCATED DRILLED AND INSTALLED NEW CUSTOMER FURNISHED PANEL IAW SRM 51-10Nov 23, 2010 · N762NC · Doug DC951SDR DALA1033373211Floor Panel · delaminatedDURING L-CHECK FOUND AFT PIT FLOOR PANEL 151LF IS DELAMINATED, 3 X 3 INCH AREA. REMOVED FLOOR PNL 151LF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PNL 151LF IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 151LF IAW AMM 53-42-14-14-400-001.Nov 23, 2010 · N311US · Airbus A320211SDR DALA1033363211Floor Panel · delaminatedDURING L-CHECK FOUND AFT PIT FLOOR PANEL 151DF IS DELAMINATED, 5" X 3" AREA. REMOVED FLOOR PNL 151DF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PANEL 151DF ON TRAVELER NR T10/860791 MATERIAL NR A402 AB-60X144, BATCH NR 1910500 IAW SRM 53-02-00 FIG 209. INSTNov 23, 2010 · N311US · Airbus A320211SDR USAA2010120792897Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24 & BETWEEN -Y1732 TO -Y1782. REPLACED FLOOR PANEL 232FF BETWEEN FR20 TO FR24 & BETWEEN -Y1732 TO -Y1782 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 22, 2010 · N104UW · Airbus A320214SDR USAA2010120792896Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232EF BETWEEN FR20 TO FR24 & BETWEEN -Y1040 TO -Y1532. REPLACED FLOOR PANEL 232EF BETWEEN FR20 TO FR24 & BETWEEN -Y1040 TO -Y1532 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 22, 2010 · N104UW · Airbus A320214SDR USAA2010120792895Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231CF BETWEEN FR20 TO FR24 & BETWEEN Y502 TO -Y502. REPLACED FLOOR PANEL 231CF BETWEEN FR20 TO FR24 & BETWEEN Y502 TO -Y502 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 22, 2010 · N104UW · Airbus A320214SDR USAA2010120792893Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR20 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 221DF BETWEEN FR16 TO FR20 & BETWEEN -Y765 TO -Y254 IAW A320 SRM 53-02-00 & MCGILL I.R.M. 9701 REV G.Nov 22, 2010 · N104UW · Airbus A320214SDR DALA1034579855Floor Panel · bentDURING M-CHECK, FOUND CABIN FLOOR PANEL NR 99, CORNER BENT AT EXISTING REPAIR. REPAIRED IAW SRM 51-30-2, 51-20-0 & 53-23-0, FIG 6, PAGE 9.Nov 22, 2010 · N764NC · Doug DC951SDR DALA1033159855Floor Panel · damagedDURING M-CHECK FOUND DAMAGE TO MAIN CABIN FLOOR PANEL 47. REPAIRED PER SRM 53-01 FIGURE 4, SRM 53-03-FIGURE 1, SRM 51-10-3 & SRM 53-05 FIGURE 1.Nov 22, 2010 · N764NC · Doug DC951SDR DALA1033149864Floor Panel · debondedDURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL 56 DISBONDED FORWARD CENTER. REMOVED AND REPAIRED FLOOR PANEL IAW DC-9/MD-80 SRM 51-30-1 AND DC-9/MD-80 51-70-1. INSTALLED FLOOR PANEL IAW DC-9-A-53-20-01-201-925A-A.P-177.Nov 22, 2010 · N773NC · Doug DC951SDR DALA1033119853Floor Panel · damagedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 41 I/B HAT CHANNEL NUMEROUS FASTENER HEADS PULLING IN SKIN. REMOVED, LOCATED AND DRILLED NEW FLOOR PANEL IAW DC-9 SRM 51-10-4. INSTALLED IAW DC-9 SRM 51-30-1.Nov 22, 2010 · N762NC · Doug DC951SDR DALA1033109853Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR 92 FORWARD END SKIN CORRODED AND RIVET HEAD PULLING. CUT OUT DAMAGE 4.4 INCH BY 11.5 INCH FABRICATED AND INSTALLED REPAIR DOUBLER FROM 7075 T6 .025" PO 1022211 IAW DC-9 SRM 51-70-4.Nov 22, 2010 · N762NC · Doug DC951SDR USAA2010120792894Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y1732 TO -Y765. REPLACED FLOOR PANEL 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y1732 TO -Y765 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 21, 2010 · N104UW · Airbus A320214SDR USAA2010120792892Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF BETWEEN FR20 TO FR24 & BETWEEN -Y765 TO -Y254 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 21, 2010 · N104UW · Airbus A320214SDR USAA2010120792891Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1292 TO Y1732 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.Nov 21, 2010 · N104UW · Airbus A320214SDR UIEA2010112000182Floorboard · gougedDURING WALK AROUND INSP, MX FOUND GOUGES/DAMAGE TO THE MAIN DECK - FLOORBOARDS (2 EA) BS1520 - BS1580, LBL68.0 (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 1000Nov 20, 2010 · N496MC · Boeing 74747UFSDR DALA1032629853Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 37 TOP SKIN CORRODED FWD TO AFT END. LOCATED HOLES AND DRILLED HOLES ON NEW FLOOR PANEL P/N 9957918-20 IAW DC9 SRM 51-10-4.Nov 16, 2010 · N762NC · Doug DC951SDR DALA1032619853Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 102C HAS CORROSION TOP AND BOTTOM AROUND FASTENER HOLES. LOCATED, DRILLED AND DEBURRED FASTENER HOLES IN NEW FLOOR P/N 09-5300-3-3431 IAW DC9 SRM 51-10-4.Nov 16, 2010 · N762NC · Doug DC951SDR USAA2010121293001Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261PF ON AFT RIGHT SECTION BETWEEN FR68 TO FR70 & BETWEEN -Y1732 TO Y1292. REPLACED FLOOR PANEL 261PF ON AFT RIGHT SECTION BETWEEN FR68 TO FR70 & BETWEEN -Y1732 TO Y1292 IAW JOB CARD 26C26053014.Nov 15, 2010 · N104UW · Airbus A320214SDR USAA2010121293000Floor Panel · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732 IAW JOB CARD 26C26053014.Nov 15, 2010 · N104UW · Airbus A320214SDR USAA2010112292640Floor Panel · debondedPIT - C11 - MAJOR REPAIR - UPPER SURFACE OF FLOOR PANEL 261DF DISBONDED BETWEEN FR64 TO FR70. REPLACED FLOOR PANEL 261DF BETWEEN FR64 TO FR70 IAW MCGILL IRM 9701 REV G.Nov 15, 2010 · N673AW · Airbus A320232SDR DALA1032119853Floor Panel · corrodedDURING M-CHECK FOUND MAIN PAX CABIN/GALLEY FLOOR PANEL 16 HAS CORROSION ON AFT END, ON REPAIR DOUBLER TOP SIDE. REMOVED AND FABRICATED NEW ATTACH PLATE FROM P/N-.080X48X1447075-T6 LOT 102 2531 AND NEW SPACER FROM P/N 7075-T6 LOT 0923042 INSTALLED IAW DC9 SRM Nov 15, 2010 · N762NC · Doug DC951SDR DALA1035479855Floor Panel · corrodedDURING M-CHECK, FOUND COCKPIT FLOOR PANEL NR15 HAS CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS WAS .020. REMOVED .005 OUT OF LIMITS IAW SRM 53- 01 FIG.1. RECEIVED NEW PANEL DRILLED IAW SRM 51-10-4. TRANSFERRED ATTACH BRACKETS FROM OLD PANEL TO NEW PANENov 14, 2010 · N765NC · Doug DC951SDR DALA1034335533Floor Panel · corrodedDURING M-CHECK FOUND MAIN CABIN AFT DECK PLATE UPPER SURFACE CORRODED. STA 1680-1720, BL 0-RBL 54. REMOVED CORROSION IAW SRM 53-00-51, PG 103, DETAIL III. ORIGINAL THICKNESS .071 IAW SRM 53-60-51, PG 7. MAIN CABIN AFT DECK PLATE UPPER SURFACE FOUND TO BE WINov 14, 2010 · N533US · Boeing 757251SDR USAA2010111692613Floor Panel · delaminatedCWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 272BF BETWEEN FR74 TO FR75 & BETWEEN -Y794.3 TO -Y1137. REPLACED CABIN FLOOR PANEL 272BF BETWEEN FR74 TO FR75 & BETWEEN -Y794.3 TO -Y1137 IAW EA 102315.Nov 14, 2010 · N279AY · Airbus A330323SDR DALA1031909853Floor Panel · crackedDURING M-CHECK FOUND CABIN FLOOR PANEL NR78 IS CRACKED AT AFT END SCREW HOLE APR 1.5 IN CUT OUT CRACK (ZAE) FLOOR PANEL NR78 1.5"X 4.7" IAW SRM 53-05. MATERIAL IS 7075-T6 .025 PO122211 FILLER, DOUBLER 7075-T6.032, PO1022537. FABRICATED DOUBLER & FILLER IAW SNov 14, 2010 · N762NC · Doug DC951SDR DALA1031899853Floor Panel · crackedDURING M-CHECK FOUND MAIN CABIN FLOOR PANEL 73 CRACKED AT AFT END. FABRICATED REPAIR DOUBLER & FILLER IAW DC9 SRM 53-01 FIG 4 SHEET 4. INSTALLED DOUBLER & FILLER IAW DC9 SRM 53-01 SHEET4 FIG 4. ALODINED & PRIMED REPAIR IAW DC9 SRM 51-10-3.Nov 14, 2010 · N762NC · Doug DC951SDR F3LA2010111400543Floor Panel · delaminatedC-CHECK: NON ROUTINE N0401; FLOORBOARD UNDER LAV E IS DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.Nov 14, 2010 · N203FR · Airbus A320214SDR F3LA2010111400540Floor Panel · corrodedC-CHECK: FWD CARGO PIT TRANSITION FLOOR PANEL 131BF UPPER SURFACE AFT END DISBOUNDED 8 SQUARE INCHES. FABRICATED TRANSITION PANEL IAW MCW IRM 9701 REV G.Nov 14, 2010 · N203FR · Airbus A320214SDR F3LA2010111400539Floor Panel · puncturedC-CHECK: NON ROUTINE N0286; FWD CARGO TRANSITION FLOOR PANEL 131BF HAS A 1 SQUARE IN PUNCTURE. FABRICATED REPLACEMENT PANEL IAW MCG 9701, REV G.Nov 14, 2010 · N203FR · Airbus A320214SDR DALA1033199855Floor Panel · crackedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR PANEL 52 FASTENER PULLED THROUGH FLOOR PANEL SKIN CRACKED APPROXIMATELY .25 INCH REMOVED DAMAGE 2.2" X 1.4" IAW SRM 53-01 FIG 4. HFEC INSPECTION IAW NDT SPM 06-10-01 REVEALED ALL DAMAGE REMOVED. FABRICATED FILLERNov 13, 2010 · N764NC · Doug DC951SDR DALA1033189855Floor Panel · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN CORROSION ON FLOOR PANEL 36 SEVERAL PLACES. REMOVED CORROSION ON 3 AREAS, CHECK LIMITS, FOUNDED OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1 SHEET 3. CUTOUT DAMAGED AREAS (3 EA), NDT VERIFY NO CRACKS IAW NDT SPM 06-10-01, Nov 13, 2010 · N764NC · Doug DC951SDR DALA1031889853Channel · crackedDURING M-CHECK FOUND MAIN CABIN FLOOR PANEL 77 HAS 1EA HAT CHANNEL CRACKED AT END APPROX .5 INCH. ORDERED REPLACEMENT PANEL 77 P/N 09-5300-3-2456 LOCATED DRILLED DEBURRED HOLES IN PANEL 77 IAW DC9 SRM 51-10-4.Nov 13, 2010 · N762NC · Doug DC951SDR DALA1031869853Floor Panel · crackedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR67 CRACKED AT END. REMOVED FASTENERS AND SECTION OF SKIN AT DAMAGED AREA FABRICATED FILLER FROM 7075T6 .025 AND DOUBLER FROM 7075T6 .032 USED NDT TO VERIFY NO CRACK EXISTS IAW NDT SPM 06-10-01.001 PRIMED PARTS IANov 13, 2010 · N762NC · Doug DC951SDR DALA1031859853Floor Panel · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN FLOOR PANEL NR70 HAS CORROSION ON TOP OF PANEL AROUND FASTENER HOLES. BLENDED CORROSION AROUND FASTNER HOLES ON CABIN FLOOR PANEL NR70 ORIG MAT .025. REMOVED .008, REMAINING .017 DETERMINED TO BE OUT OF LIMITS IAW SNov 13, 2010 · N762NC · Doug DC951SDR DALA1031849853Floor Panel · damagedDURING M-CHECK FOUND MAIN PASSENGER CABIN FLOOR 102C AFT I/B SIDE SKIN LOOSE AND FASTENERS MISSING. FOUND SEVERAL HOLES CRACKED AND OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. RECEIVED NEW PANEL 102C P/N 9957928-21N LOCATED AND DRILLED HOLES IAW DC9 SRM 51-10-4.Nov 13, 2010 · N762NC · Doug DC951SDR DALA1031839853Floor Panel · crackedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR51 CRACKED AT FWD END FASTENER HOLE. TRIMMED OUT CRACK FROM FLOOR PANEL NR51 WEB (1.7"X 2.2") IAW SRM 53-01 FIG 4 SHT.4 PERFORMED HFEC INSP OF CUTOUT AREA IAW NDT SPM 06-10-01.001 NO CRACKS NOTED. FABBED REPAIR Nov 13, 2010 · N762NC · Doug DC951SDR FDEA201011124324Pressure Panel · corrodedFWD CARGO COMPARTMENT HORIZ PRESSURE DECK UPPER SURFACE AT FRAME 40/41 IS CORRODED AT THE SPLICE. REPAIRED PER FEDEX EA 6-5310-136722, TITLE " FUSELAGE - PRESSURIZED FLOOR BETWEEN FR 39 AND FR 40 AT Y-95.3". REMOVED AND RE-INSTALLED 1 EA. SUPPORT BRACKET Nov 12, 2010 · N455FE · Airbus A310222SDR DALA1033929864Floor Panel · dentedDURING M-CHECK FOUND MAIN CABIN METAL FLOOR PANEL 71 HAS DENT. CUT OUT DAMAGE PER DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-01 FIG 4.Nov 12, 2010 · N773NC · Doug DC951SDR USAA2010111692614Floor Panel · delaminatedCWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 272CF BETWEEN FR74 TO FR75 & BETWEEN -Y450 TO -Y794.3. REPLACED CABIN FLOOR PANEL 272CF BETWEEN FR74 TO FR75 & BETWEEN -Y450 TO -Y794.3 IAW EA 102315.Nov 12, 2010 · N279AY · Airbus A330323SDR WX0A070661Floor Panel · crackedCABIN FLOOR PANEL EDGES CRACKED OUT STA 313 TO STA 389, LBL 23 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05.Nov 11, 2010 · N869GA · Doug MD83SDR IXXA110039SFloor Panel · corrodedDURING ROUTINE C-CK INSP FOUND MAIN CARGO COMPARTMENT FLOOR PANEL SKIN CORRODED BETWEEN STA 1060.000 LT BOTTOM LINE10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLERS AND FILNov 10, 2010 · N602AL · Doug DC873FSDR WX0A070660Floor Panel · crackedCABIN FLOOR PANEL B5 CORNERS CRACKED OUT STA 617 TO STA 639, LBL 23 TO LBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05.Nov 10, 2010 · N869GA · Doug MD83
Back to JASC 5321