JASC 5321
Service difficulty reports · 49,350
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.
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
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 SWAA2023060143258Floor Panel · pulledFLOOR PANEL 231EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #SDR SWAA2023060143259Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231GF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; APPLIED TAPE AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 THEN CURED USING HEAT LAMPS AND THERMOSDR SWAA2023060143267Floor Panel · pulledFLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231JF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; APPLIED TAPE AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 THEN CURED USING HEAT LAMPS AND THERMOSDR SWAA2023060143268Floor Panel · pulledFLOOR PANEL 231UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231UF OUT OF BMS 4-23 TY2 LOT#1525675-1. INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K-1 AND CURED UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/23. PART MARKED SDR SWAA2023060143271Floor Panel · pulledFLOOR PANEL 241KF UPPER SKIN HAS ARAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241KF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND ECONOMICAL RSDR SWAA2023060143262Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241SF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETSDR SWAA2023060143263Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241UF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1525675-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETSDR SWAA2023060143264Floor Panel · pulledFLOOR PANEL 242MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 5 TABLE 5 SECTION 46.UPPER SKIN STRAND DAMAGE EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1. PARA 4. F. <BR>MULTIPLE AREAS OF STRASDR SWAA2023052342909Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL (AFT WET AREA) HAS DELAMINATION 242QF<[01] REMOVED & REPLACED CABIN FLOOR PANEL 242QF AS PER AMM 53-21-00.;[02] INSP C/WSDR SWAA2023052342910Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL (AFT WET AREA) HAS DELAMINATION 242PF<[01] REMOVED & REPLACED CABIN FLOOR PANEL 242PF AS PER AMM 53-21-00.;[02] INSP C/WSDR SWAA2023052342907Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL (AFT WET AREA) HAS DELAMINATION 241UF<[01] REMOVED & REPLACED CABIN FLOOR PANEL 241UF AS PER AMM 53-21-00.;[02] INSP C/WSDR SWAA2023052342911Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL (AFT WET AREA) HAS DELAMINATION 241VF<[01] REMOVED & REPLACED CABIN FLOOR PANEL 241VF AS PER AMM 53-21-00.;[02] INSP C/WSDR SWAA2023052342912Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL (AFT WET AREA) HAS DELAMINATION 241WF<[01] REMOVED & REPLACED CABIN FLOOR PANEL 241WF AS PER AMM 53-21-00.;[02] INSP C/WSDR DALA2023050203421Unknown · unknownSHIP 672 SECONDARY FINDING: AFTER FASTENERS OF ANGLE REMOVAL, CRACK WAS FOUND ON WEB BTW STA 1180-1200 AND STGR 17R AT PAX CABIN FLOOR STRUCTURE. IN REF NRC 00331. CORRECTIVE ACTION: SUMMARY OF NRC 00655: WEB BTW STA 1180-1200 AND STGR 17R AT PAX CABIN FLOOR SSDR DALA2023050103368Unknown · unknownSHIP 3351 CORROSION FLOOR BEAM -Y953 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y953 LOC. FR31 TO FR37 RH SIDE IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2743749)SDR DALA2023050103367Unknown · unknownSHIP 3351 CORROSION FLOOR BEAM -Y450 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y450 LOC. FR31 TO FR37 RH SIDE IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2743747)SDR CALA2023050101304Floorboard · brokenSUPPORT TASK: MAIN CABIN FLOORBOARD 221ZBF IS BROKEN ON EDGE. TRANSCRIBED FROM HAECO GSO NRC# 9286433 REPAIRED BROKEN EDGE ON PANEL 221ZBF IAW B737-900ER SRM 53-00-50 -2R-1.SDR CALA2023050101303Floorboard · tornSUPPORT TASK: MAIN CABIN FLOORBOARD 222ZAF HAS TORN FIBERS. TRA NSCRIBED FROM HAECO GSO NRC# 9286439 REPAIRED TORN FIBERS ON PANEL 222ZAF IAW B737-900ER SRM 53-00-50 -2R-1 REF HAECO GSO MECH V934866 INSP QC357SDR SWAA2023060142663Floor Panel · crackedFWD FLOOR PANEL 221BF O/B TANG IS CRACKED.<[01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2 FOUND CRACKE ALONG BOTH UPPER AND LOWER SKINS OF TANG TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.<BR><BR>COMPLETELY REMOVED TANG; PRESDR SWAA2023060142675Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] IDENTIFIED FLOORBOARD MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1 FIG 6 TABLE 6<BR><BR>PANEL UPPER SKIN DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4.F.<BR><BR>PANEL SKIN DASDR SWAA2023060142672Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241AAF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. DAMAGE TO UPPER SURFACE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PANEL 241AASDR SWAA2023060142677Skin · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE IS REPAIRABLE IAWSDR SWAA2023051142918Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221DF FOUND DELAMINATED: P/N 141A5810-59<[01] RECEIVED MAIN CABIN FLOOR PANEL 221DF P/N 141A5810-59; PANEL WILL BE INSTALLED ON T/C TTG8Q00JCQTE;[02] VERIFIED STEP 1SDR DALA2023050203390Unknown · unknownCRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS (3 EA) ON FWD PAN FROM BEAM #1 AND BEAM #4 OF FWD CARGO DOOR. ALSO CRACK (1 EA) ON UPPER PAN CLOSE OF AFT HINGE. SUMMARY OF NRC 00093: CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKSSDR FDEA202304280779Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222AFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280778Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222CFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280777Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 222BFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280776Access Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 221CFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 221 CFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304280775Panel · dentedMAIN CARGO COMPARTMENT, ACCESS FLOOR PANEL 221DFF WITH DENTS. MDCC, ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2. REV. 85 DEC15/2022SDR SWAA2023060142228Panel · crackedCRACKED BREAK PANEL STA 540; BL0-LBL 25; WL 208.<[01] UPDATED MEASUREMENT TABLE;[02] LOCATED AND DRILLED NEW BREAK PANEL AT STA 540; BL 0 - LBL 25; WL 208 IAW SRM 51-40-05-0G-0 AND AIPC 53-42-11-66. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2<BR>OK TO INSTSDR SWAA2023052442216Splice · corrodedAFT CARGO; FLOOR PANEL SPLICE AT STA. 727I+4 HAS CORROSION.<[01] BLENDED CORROSION ON AFT CARGO FLOOR PANEL SPLICE AT STA. 727I+4? PER SRM 51-10-02. REMOVED .028? OF MATERIAL. REMAINING THICKNESS IS .042? DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-00-53-1A-2. SDR AALA202304281689Floorboard · damagedAIRCRAFT WAS GROUNDED: ISLE FLOOR BOARD BEHIND ROW 1 AND ROW 2 SOFT. REMOVED AND REPLACED AISLE FLOORBOARD BEHIND ROW 1 AND ROW 2.SDR DALA2023042703302Unknown · unknown(LOG 2738558) DURING INSPECTION FOUND AFT CARGO BOTTOM SIDE OF FLOOR BEAM AT STA 947 RBL 10 WL202 HAS CORROSION. COMPLIED WITH ER/A 607863-14 REV ORIGINAL.SDR DALA2023042703271Unknown · unknownSHIP 3351 CRACK SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 RH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 RH AT AFT GALLEY AREA. RII INSPECTION COMELETE. (2738765)SDR DALA2023042703270Unknown · unknownSHIP 3351 CRACK SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 LH AT AFT GALLEY AREA. (2738757)SDR DALA2023042603250Unknown · unknownDURING ATTENTION OF NRC 00399, FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FOUND CORRODED OUT OF LIMITS. SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FABRICATED AND REPLACED PER B717-200 SRM 51-30-07-0G FIGSDR DALA2023042603249Unknown · unknownCORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 AT PAX CABIN. (W1). SUMMARY OF NRC 00526: CORROSION LEVEL 2. FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2737864)SDR SWAA2023052531323Floor Panel · pulledPASSENGER FLOOR PANEL 241VF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW FLOOR PANEL IAW AMM 53-21-00;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR FLOOR PANEL REPLACEMENT.SDR SWAA2023052431338Floor Panel · pulledPASSENGER FLOOR PANEL 231TF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL WAS INSTALLED ON TASK CARD TTG8Q00HJQ7V.;[02] ADDED P/N & B/N;[03] C/W INSPECTION.SDR SWAA2023052431337Floor Panel · pulledPASSENGER FLOOR PANEL 232LF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PNL IAW AMM 53-21-00SDR SWAA2023052431334Floor Panel · pulledPASSENGER FLOOR PANEL 232NF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PNL IAW AMM 53-21-00SDR SWAA2023052431333Floor Panel · pulledPASSENGER FLOOR PANEL 231FF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231FF PER A.M.M. 53-21-00SDR SWAA2023052431330Floor Panel · pulledPASSENGER FLOOR PANEL 231RF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PANEL IAW AMM 53-21-00.;[02] CWSDR SWAA2023052431329Floor Panel · pulledPASSENGER FLOOR PANEL 242AF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00K86G8;[02] C/W INSPECTIONSDR SWAA2023052431328Floor Panel · pulledPASSENGER FLOOR PANEL 231YF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231YF PER A.M.M. 53-21-00SDR SWAA2023052431327Floor Panel · pulledPASSENGER FLOOR PANEL 231ZF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231ZF PER A.M.M. 53-21-00SDR SWAA2023052431326Floor Panel · pulledPASSENGER FLOOR PANEL 232DF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PNL IAW AMM 53-21-00SDR SWAA2023052431325Floor Panel · pulledPASSENGER FLOOR PANEL 232FF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PNL IAW AMM 53-21-00SDR SWAA2023052431324Floor Panel · pulledPASSENGER FLOOR PANEL 232JF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REPLACED WITH NEW PNL IAW AMM 53-21-00SDR SWAA2023052431322Floor Panel · pulledPASSENGER FLOOR PANEL 231MF HAS MULTIPLE DENTS/ PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231MF PER A.M.M. 53-21-00
Back to JASC 5321