JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, newest first.
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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"
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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 SWAA2023030103314Floor Panel · pulledDOT A24-10 CENTER CABIN FLOOR PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 231ZF AND FOUND PULLED FIBERS AND DENTS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAWSDR SWAA2023030103315Floor Panel · pulledDOT A24-11 CENTER CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] WORK ACCOMPLISHED ON W.O.#TTG8Q00HU0UH;[02] VERIFIED STEP 1SDR SWAA2023030103316Floor Panel · pulledDOT A24-12 CENTER CABIN FLOOR PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE PLIES ON UPPER SURFACE FULL LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANESDR DALA2023022101273Angle · corroded(LOG 2631852) DURING INSPECTION FOUND AFT CARGO L/H Z ANGLE STA 727A-847 LBL HAS MULTIPULE AREAS OF CORROSION. REMOVED DAMAGED ZEE ANGLE FROM AFT CARGO L/H STA 727A-847 LBL 24 AND REPAIRED PER B737 S.R.M 53-00-53-2R-G PARA 4. B-N. Z ANGLE SPLICE ARE LOCATED BESDR FDEA202302140258Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009 RIGHT HAND X -8.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009 RIGHT HAND X = -8.5 CROWN WORN REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SSDR CALA2023021400436Skin · dentedFUSELAGE OUTWARD DENT BETWEEN FR26&27 AND STR37L&38L. CURRENT AIRCRAFT TIME 29120FC/66097FH. INITIATE DIP FOR INSP THRESHOLD FROM TIME OF EMBODIMENT 60000FC/ 120000FH WHICHEVER COMES FIRST. INSP INTERVALS N/A & METHOD N/A. DENT IS OUT OF LIMITS REF SRM 53-00-1SDR SWAA2023031302758Floor Panel · delaminatedFWD CABIN FLOOR PANEL 222BF HAS A DELAMINATION ON O/B EDGE APPROXIMATELY 4' AFT OF FWD EDGE<[01] IDENTIFIED 222BF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 2; TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL SDR SWAA2023031302759Floor Panel · delaminatedAFT CABIN FLOOR PANEL 242UF HAS A DELAMINATION ON THE LOWER SKIN AFT EDGE AT GIRT BAR ATTACH POINT<[01] IDENTIFIED PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIG 6; TABLE 6.<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. <BRSDR DALA2023021601211None · noneSHIP 694 CRACKED STABILIZER STRAP (2EAS) BTW STA 365.25 TO STA 395 AND LBL 24 AT ABOVE NLG W/W (E&E). CORRECTIVE ACITON: SUMMARY OF NRC 00401: STABILIZER STRAP (2EAS) BTW STA 365.25 TO STA 395 AND LBL 24 AT ABOVE NLG W/W WERE REPAIRED PER B757-200 SRM. (262685SDR DALA2023021501188None · noneAIRCRAFT 3122, CORROSION FLOOR BEAM +Y765 AT LEVEL FR68 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 AT LEVEL FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11; SRM 51-72-11 AND DWG D53472000000. (LP 2627463)SDR AALA202302155750Floor Panel · delaminatedAIRCRAFT WAS GROUNDED: CABIN FLOOR PANEL 241JF POPPING AT SEAT ROW 20 CENTER ISLE. MAINTENANCE FOUND FLOOR PANEL DELAMINATED AND REPLACED IT PER AMM 53-00-00-400-801-A01.SDR DALA2023021501180None · noneCORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=200 X=-9 TO X=-44. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.045 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00431 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00484: CORROSION LEVESDR DALA2023021501179None · noneIN REFERENCE TO NRC 00066, AFTER REMOTION OF RETAINER SEALS, CRACK WAS FOUND ON PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2. SUMMARY OF NRC 00511: PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2 WAS REPAIRED PER B7SDR SWAA2023031302378Panel · tornFWD CABIN FLOOR PANEL 222DF HAS A TORN OUT FASTENER HOLE ON THE O/B EDGE<[01] IDENTIFIED FLOOR PANEL 222DF MATERIAL IAW SRM 53-00-50-0I-1 FIG. 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS AND REQUIRES A PERMANENT REPAIR IAW SRM 53-0SDR SWAA2023031302382Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF HAS BROKEN TANG ON AFT I/B END<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>RESDR SWAA2023031302383Panel · brokenFWD CABIN FLOOR PANEL 221GF HAS BROKEN TANG ON FWD O/B END<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>RESDR SWAA2023031601762Floor Panel · peelingAFT CABIN FLOOR PANEL 241XF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 XF; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6T5;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241XF AND TO BE INSTALLED ON TTG8Q00GS6T5.SDR SWAA2023031601778Floor Panel · peelingAFT CABIN FLOOR PANEL 241YF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 YF; P/N 147A5810-77; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6UA;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241YF AND TO BE INSTALLED ON TTG8Q00GS6UA.SDR SWAA2023031601777Floor Panel · peelingAFT CABIN FLOOR PANEL 241ZF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 ZF; P/N 147A5810-98; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TY;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241 ZF AND TO BE INSTALLED ON TTG8Q00GS6TY.SDR SWAA2023031601761Floor Panel · peelingAFT CABIN FLOOR PANEL 241ABF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 ABF P/N 147A5810-88; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TU;[02] VERIFIED STEP 1 RECEIVED PANEL AND TO BE INSTALLED ON T/C TTG8Q00GS6TU.SDR SWAA2023031601775Floor Panel · peelingAFT CABIN FLOOR PANEL 241AAF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 AAF; P/N 147A5810-8; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TW;[02] VERIFIED STEP 1SDR SWAA2023031601774Floor Panel · peelingAFT CABIN FLOOR PANEL 242UF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 UF P/N 147A5810-95; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS726;[02] VERIFIED STEP 1 RECEIVED PANEL AND TO BE INSTALLED ON T/C TTG8Q00GS726.SDR SWAA2023031601772Floor Panel · peelingAFT CABIN FLOOR PANEL 241ACF UPPER SURFACE PEELING.<[01] PREPARED DAMAGE AREA AND APPLIED THE GLASS FABRIC REPAIR PLIES AT AFT CABIN FLOOR PANEL 241ACF UPPER SURFACE. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 169454SDR SWAA2023031601770Panel · crackedAFT CABIN FLOOR PANEL 242VF UPPER SURFACE CRACKED.<[01] RECEIVED NEW CABIN FLOOR PANEL 242VF; P/N 147A5810-350; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS724;[02] VERIFIED STEP 1.SDR SWAA2023031601758Floor Panel · crackedAFT CABIN FLOOR PANEL 241AEF CRACKED.<[01] PREPARED FOR REPAIR DAMAGED AREA; AT AFT CABIN FLOOR PANEL#241AEF AS PER B737 SRM 53-00-50-2R-1;[02] REPAIRED DAMAGED AREA AT AFT ABIN FLOOR PANEL #241 AEF AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO#1799598 PO#169SDR SWAA2023031601769Floor Panel · peelingAFT CABIN FLOOR PANEL 242TF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 TF; P/N 147A5810-94; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS728;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 242TF AND TO BE INSTALLED ON TTG8Q00GS728SDR SWAA2023031601768Floor Panel · peelingAFT CABIN FLOOR PANEL 242RF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 RF; P/N147A5810-2; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS72C;[02] VERIFIED STEP 1.SDR SWAA2023031502026Floor Panel · delaminatedCUSTOMER REQUEST DELAMINATED FLOOR PANEL 241RF AT PASSENGER CABIN 2023-119374<[01] TOOL USED CALIPER P/N: 500-752-20; S/N: B21038259; 22-SEP-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV. S/N:18185781; DUE DATE:24/JAN/24.;[03] TOOL USED SCALE P/N SPX621 S/N SDR DALA2023021401134Unknown · unknownCORRODED FLOOR SUPPORT STA Y=157-200 AND X=44.5, STA Y=180 AND X=12 TO X=38. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.035 IN, THEREFORE THE AREA IS OUT LIMITS IN REF NRC 00434 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00485: CORROSIONSDR HALA2023021400054Unknown · unknownSHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION LEFT SIDE FRAME 80/ 82 - FRAME 79, STRINGER LEVEL 26LH, UPPER SIDE. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT LEFT SIDE FRAME 80/82 TO FRAME 79, STRINGER LEVEL 26LH, UPPER SIDE REPLACED. (2627272)SDR HALA2023021400045Unknown · unknownSHIP 384 MAIN DECK LONGITUDINAL BEAM FOUND BADLY CORRODED AT LOCATION FRAME 75 - FR 78, -Y445 (RIGHT SIDE). CORRECTIVE ACTION: MAIN DECK LONGITUDINAL BEAM AT FRAME 75 - FRAME 78, -Y445 (RIGHT SIDE) REPLACED. (2627128)SDR HALA2023021400044Unknown · unknownSHIP 384 MAIN DECK LONGITUDINAL BEAM FOUND BADLY CORRODED AT LOCATION FRAME 75 - FRAME 80/82, -Y450 (RIGHT SIDE). CORRECTIVE ACTION: MAIN DECK LONGITUDINAL BEAM AT FRAME 75-FRMA 80/82, -Y450(RIGHT SIDE) REPLACED. (2626735)SDR HALA2023021400043Unknown · unknownSHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION FR 80/82, BETWEEN - Y1137-1. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT FR 80/82, BETWEEN -Y1137.1 AND -Y1447.8( RIGHT HAND SIDE) REPLACED. (2626729)SDR HALA2023021400057Unknown · unknownSHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION LEFT SIDE FRAME 80/ 82 - FRAME 79, STRINGER 26LH, BOTTOM SIDE. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT LEFT SIDE, FRAME 80/82-FRAME 79, STRINGER 26LH REPLACED. (2626732)SDR SWAA2023031601453Floor Panel · delaminatedCABIN FLOOR PANEL 232BF FWD SIDE DELAMINATED<[01] PREPARED FOR REPAIR CABIN FLOOR PANEL 232 BF; AS PER B 737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 232BF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473813 ASDR SWAA2023031601449Floor Panel · delaminatedCABIN FLOOR PANEL 231BF SURFACE DELAMINATED<[01] RECEIVED NEW CABIN FLOOR PANEL 231 BF; P/N 141A5810-168; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GXTW0;[02] VERIFIED STEP 1.SDR DALA2023022301364None · none(LOG 2636162) DURING INSPECTION FOUND CORROSION ON FLOOR BEAM STA 947.5 LBL 26". FLOOR BEAM STA 947.5 LBL 26 DAMAGE WAS REPAIRED I.A.W. B737-900 SRM 53-70-51-2R-5.SDR DALA2023021401124Unknown · unknownCRACK ON FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3. SUMMARY OF NRC 00294: FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2622016)SDR DALA2023021401122Unknown · unknownIN REF NRC 00294: CRACK ON FWD PAN OF FWD CARGO DOOR ON BEAM 5. SUMMARY OF NRC 00628: FWD PAN OF FWD CARGO DOOR ON BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2621821)SDR DALA2023021301083Shield · corroded(LOG 2621819) DURING INSPECTION FOUND FWD CARGO AFT SHIELD AT STA 490 RBL 25 HAS CORROSION. REMOVED AND REPLACED FWD CARGO AFT SHIELD IAW B737 SRM 51-40-02, B737 SRM 51-40-05 AND BOEING DWG # 143A8126.SDR DALA2023021001073Unknown · unknownSHIP 694 SECONDARY NRC : IN REF. NRC 00378 : CORROSION OUT OF LIMITS ON FLOOR BEAM STA. Y=365 BTW RBL 9 AND RBL10 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00556: CORROSION OUT OF LIMITS ON FLOOR BEAM STA. Y=365 BTW RBL 9 AND RBL10 WAS REPAIRED PER. B 75SDR DALA2023021001067None · noneSHIP 3307 CRACK CROSS BEAM FR74 AT LEVEL SEAT TRACK YB IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 605361-14. VALIDATED ER/A 605361-14 MATCHES PRI 605361-14. PERFORMED REPAIR INSTRUCTIONS ON CROSS BEAM YB FRAME 74 AT LEVEL OF STRINGER 26L IN PASSESDR SWAA2023032000773Floor Panel · delaminatedCABIN FLOOR PANEL 241FF FWD CORNER DELAMINATED<[01] PREPARED FOR REPAIR FLOOR PANEL 241 FF; AS PER B737 SRM 53-00-50-2R-9.;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED FLOOR PANEL 241 FF; AS PER B737; SRM 53-00-50-2R-9 MATERIAL USED PO.1473815 AND PSDR SWAA2023032000774Floor Panel · delaminatedCABIN FLOOR PANEL 242DF DELAMINATED<[01] MEASUREMENTS;[02] PREPARED DAMAGED AREA TO APPLY REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 53-00-50-2R-7;[03] VERIFIED STEPS 1 AND 2;[04] OK TO APPLY REPAIR;[05] APPLIED REPAIR AT FLOOR PANEL #242DF PER B737<BR>SRM 5SDR SWAA2023031600775Floor Panel · delaminatedCABIN FLOOR PANEL 231FF L/H AREA DELAMINATED FLOOR PANEL 231 FF<[01] PREPARED FOR REPAIR; FLOOR PANEL 221 FF; AS PER B737 SRM 53-00-50-2R-9;[02] CORRECTION #1. PREPARED FOR REPAIR FLOOR PANEL 231FF; AS PER B737 SRM 53-00-50-2R-9;[03] VERIFIED CORRECTED STEP 2.SDR DALA2023021401118Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE (PAX CAB) (W2). SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 53-20-51-0I,SDR DALA2023021001071Unknown · unknownSHIP 689 IN REF. NRC 0170. CORROSION ON RH SIDE PLATE BTW STA 1440 TO 1463 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00590: SIDE PLATE SECTION WAS REPLACED PER B757 SRM. (2620151)SDR FDEA202302080225Track · damagedCABIN - SEAT TRACK STATION 1540, X = 8.50 CROWN AREA DAMAGED. CROWN AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATSDR FDEA202302080224Track · damagedCABIN - SEAT TRACK STATION 1611, X = -8.50 CROWN AREA DAMAGED. CABIN Ï¿½ AT SEAT TRACK STATION 1611, X = -8.5 DAMAGED CROWN AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SSDR FDEA202302080223Track · corrodedCABIN - SEAT TRACK STATION 1405 TO 1436, X = -8.50 CORROSION. CABIN Ï¿½ CORROSION AT SEAT TRACK STATION 1405 TO 1436, X = -8.5 EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED
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