JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320' 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 = '5320' 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 DALA2024072207334Channel · corroded(LOG 0452506) CORROSION ON REPAIR REINFORCEMENT CHANEL AT STA 727I+5", LBL13.1 AND WL155. REMOVED AND REPLACED REPAIR REINFORCEMENT CHANNEL PER B737-800 SRM 53-00-53-2R.SDR DALA2024072207331Channel · corroded(LOG 0452417) CORROSION ON REPAIR REINFORCEMENT CHANEL AT STA 727I+5", LBL3 AND WL155. REMOVED AND REPLACED REPAIR REINFORCEMENT CHANNEL PER B737-800 SRM 53-00-53-2R-2.SDR DALA2024072207330Channel · corroded(LOG 0452397) CORROSION ON REPAIR REINFORCEMENT CHANEL AT STA 727I+5", LBL8.1 AND WL155. REMOVED AND REPLACED REPAIR REINFORCEMENT CHANNEL PER B737-800 SRM 53-00-53-2R-2.SDR IPXA2024071976451Angle · crackedCRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60. (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MSDR IPXA2024071976402Angle · crackedCRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MAIN DECK SDR DALA2024071907277Channel · corroded(LOG 0448985) CORROSION ON REPAIR REINFORCING CHANNEL AT STA 727I+5 RBL 8 WL 155. REMOVED AND REPLACED REPAIR REINFORCEMENT CHANNEL PER B737-800 SRM 53-00-53-2R-2.SDR AALA202407166126Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER FITTING LOCATED AT LEVEL STRINGER 23L BETWEEN FR 66 TO FR 68 AREA OF LOWER SILL AT AFT GALLEY AREA. REPLACED CENTER FITTING PER SRM 51-42-11-801.SDR YENA2024071601010Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FRAME 60 AND FRAME 62 IN BULK CARGO COMPARTMENT; PERFORMED REPAIR ON LOWER SILL BULK CARGO COMPARTMENT LOACTED BTW FR 60 PLUS 19 IN IAW A320 SRM 53-41-49-300-003. THIS REPAIR IS CATEGORY B AT DEFINED ISDR YENA2024071601009Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL EXISTING REPAIR LOCATED AT STR 23L FR 68 AFT GALLEY AREA; PERFORMED REPAIR LOCATED ON LOWER SILL AT STR 23L AND BETWEEN FR 67 TO FR 68 AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001 FIGURE 001(SHEET) 3. REF AEROMANSDR DALA2024071507155Cusp Web · crackedTHE CUSP WEB WAS FOUND CRACKED STA Y=218-220 / -X=44.5. SUMMARY OF NRC 00762: CUSP WEB STA Y=218-220 / -X=44.5. WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0443614)SDR CALA2024071502040Support · crackedFWD CABIN WET AREA L-1 CUTOUT FWD LOWER SILL INNER CHORD CRACKED AT SUPPORT FRAME ATTACHMENT FASTENER HEAD STA 303.9 LBL 59 REF. AAR N/R:9894904SDR DALA2024071207073Cusp Web · corrodedSHIP 684 IN REF NIRC 00460: CORROSION ON CUPS WEB BTW STA 1160 TO STA 1170 RBL.70 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00694: CUPS WEB BTW STA 1160 TO STA 1170 RBL.70 AT CPAX. WAS REPAIRED PER ERA 618766-14 REV ORIGINAL SECTION I (0442610)SDR IXXA20240712001Support · corrodedCORROSION ON THE UPPER AND LOWER SURFACES OF THE LOWER PANEL SUPPORT COMMON TO THE LEFT BULK CARGO SLOPING SIDEWALLSDR SWIA2024092000014Floor Support · corrodedR/H FLOOR SILL BETWEEN FS349.00 TO FS364.00 HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) REPAIRED R/H FLOOR SILL BETWEEN FS349.00 TO FS364 REF REO 670-53-21-1806 REV--2020-08-27 AND DWG SH670-32170 REV V COMPLIED WITH TASK CARD 51-900-1002-SKY LEAK SDR VNAA202409010024Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPPORTLBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORT LBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1435 REV: - -SDR VNAA202409010023Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPPORT LBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORTLBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1434 REV - -SDR VNAA202409010018Fitting · corrodedCORROSION ON JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E). JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E) WERE REPAIRED PER REO 690-53-11-1831 REV. --SDR VNAA202409010013Floor Support · corrodedCORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT. CORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. ON FLOOR SUPPORT LBL12.0 BTW FS26SDR AALA202408271661Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT AFT GALLEY AREA BETWEEN FR 69 AND FR 70 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.SDR AALA202408270712Channel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL STRUCTURE SUPPORT CHANNEL IN BULK CARGO COMPARTMENT BETWEEN FR 59 AND FR 60, BETWEEN S42L AND S43L. REPLACED CHANNEL PER SRM 51-42-11.SDR SWAA2024082211690Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE LOCATED ON FWD CARGO COMPARTMENT 2024-443481<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:A23325549;DUE DATE:03-JAN-25.;[02] TOOL USED ON STEP 4 RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1859843; CAL DUE DATE: 24-JUL-24;[03SDR AALA202408143684Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23L AND BETWEEN FR 69 AND FR 70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS PER SRM 51-42-11-801.SDR SWAA2024080511472Angle · crackedCRACK ANGLE LOC BS500H AFT FACE AND STRINGER 26R AT FWD CARGO COMPARTMENT 2024-402194<[01] REPLACED ANGLE - CLIP AND FASTENERS LOC. BS500H AFT FACE AND STRINGER 26R AT FWD CARGO COMPARTMENT B737-800 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 DWG 143A7505; SHEET 109; SDR SWAA2024080511635Angle · crackedCRACK ON ANGLE LOC BS500G AFT FACE AND STR26R AT FWD CARGO COMPARTMENT 2024-402195<[01] REPLACED ANGLE - CLIP AND FASTENERS LOC BS500G AFT FACE AND STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 DWG 143A7505; SHEET 109; REV.- SDR SWAA2024080511465Channel · corrodedFOUND CHANNEL TIE WITH PITTING CORROSION AT E&E COMP INTERNAL SIDE STA 351.2+8 BL0<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL TIE AT SKIN BS 351.2+8 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG 141A1160;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02SDR SWAA2024080511464Support · wornKEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E HAS SUPPORT WITH FRETTING AT STA 600. 8-48<[01] REMOVED AND INSTALLED NEW SUPPORT AT KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E AS PER SRM-51-40-02-0G-0;[02] VERIFIED STEP:1SDR SWAA2024080211569Strap · damagedELONGATE HOLE ON STRAP FAIL SAFE BS 440 BETWEEN S-20R S-21R 9(MARKED) CORRECTION SHOULD BE = ELONGATE HOLE ON STRAP FAIL SAFE BS 440 BETWEEN S-21R S-22R (MARKED)<[01] REPAIRED ELONGATED HOLE IAW EA 24-153-01926.;[02] REPAIRED ELONGATED HOLE IAW EA 24-153-01926SDR AALA202407262828Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER /CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.SDR IPXA2024072268125Web · crackedMAIN CABIN CARGO, AT FR 75, LEFT WEB HAS EVIDENCE OF CRACKING. DOT 72-044.REMOVED LEFT WEB AT MAIN CABIN CARGO AT FR75 I.A.W. A300-600 S.R.M. 51-40-21.FABRICATED LEFT WEB OF MATERIAL ALUMINUM SHEET 2024-T3 .071C", P/N: 2024-T3 .071C", BATCH: 0004148808 I.A.W. SDR DALA2024071807253Baffle · corroded(LOG 0447615) FWD CARGO BAY FOUND BAFFLE @STA. 500B TO 500C L/H CORRODED. REMOVED AND REPLACED FWD CARGO BAY BAFFLE AT STA. 500B TO 500C L/H IAW B737 SRM 51-40-02-0G AND DWG 143A7505.SDR DALA2024071607188Baffle · corroded(LOG 0447619) FWD CARGO BAY FOUND BAFFLE @STA. 500 TO 500A L/H CORRODED. REMOVED AND REPLACED FWD CARGO BAY BAFFLE AT STA. 500 TO 500A L/H IAW B737 SRM 51-40-02-0G AND DWG 143A7505.SDR DALA2024071607187Baffle · corroded(LOG 0447601) FWD CARGO BAY FOUND BAFFLE @STA. 500A TO 500B L/H CORRODED. REMOVED AND REPLACED FWD CARGO BAY BAFFLE AT STA. 500A TO 500B L/H IAW B737 SRM 51-40-02-0G AND DWG 143A7505.SDR AALA202407122311Profile · crackedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844 AFT TRANSMITTING PROFILE / SEGMENT CRACKED BETWEEN FR 38 AND FR 41. REPLACED SEGMENT PER SRM 51-42-11.SDR DALA2024071207051Pan · crackedAFT REMOVAL ANGLE CRACK ON INNER AND OUTER PAN WAS FOUND BTW BEAM 1-2 AND STA Y=954 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00665: INNER AND OUTER PAN BTW BEAM 1 TO BEAM 2 AND STA Y=954 AT AFT CARGO COMPARTMENT DOOR WERE REPAIRED PER B717-200 SRM 52-30-0SDR DALA2024071207050Cusp Web · wornWEAR ON CUSP WEB STA Y=256, 275, AND BTW STA X=44/54 (UPPER FACE) AT PAX CABIN. SUMMARY 00441: CUSP WEB STA Y=256, 275, AND BTW STA X=44/54 (UPPER FACE) AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0442199)SDR IXXA202407110002Door Sill · corrodedCORROSION ON THE LOWER SURFACE OF THE LOWER SILL, AT THE BULK CARGO DOOR FUSELAGE CUTOUT, UNDER THE AFT I/B NUTPLATE, AS VIEWED INSIDE OF THE FWD LIGHTENING, AT STA.1426.SDR IXXA20240711001Floor Support · corrodedCORROSION UNDER 8 NUTPLATES, ON THE LOWER SURFACES OF THE 4 GREEN PANEL SUPPORT CHANNEL REPAIRS, FOR THE BULK CARGO FLOOR SUPPORTS, FROM STA.1415 TO STA.1422, AT LBL23, LBL16, LBL9, AND RBL9.SDR VNAA202409010015Bracket · corrodedCORROSION ON BRACKETS, MACHINED (10EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (2EAS) (P/N:SH670-33389-1) WERE CLEANED AND NO DAMAGES WERE FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, AND BRACKETS MACHINED (8EAS) WERE EVALUATED OUT SDR VNAA202409010010Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STSDR VNAA202409010008Intercostal · wornWORN INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-SDR SWAA2024082211164Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED STA 727E AT LEVEL CEILING AREA LH SIDE AT AFT CARGO COMPARTMENT. REPAIRED RACK ANGLE - SUPPORT LOCATED STA 727E AT LEVEL CEILING AREA LH SIDE AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0 FIGURE 201 SHEET 2.SDR SWAA2024082211173Panel · elongatedELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT. FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 ITEM F AND DWG 453A2510 SHEET:8 REV: A.SDR SWAA2024082211165Panel · damagedELONGATED HOLE BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT. FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801 ITEM F AND DWG 453A2510 SHEET:9 REV: A.SDR AALA202408210691Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING FASTENER HOLE AT FR 16 RIGHT AND DOOR STOP FITTING #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.SDR SWAA2024081511120Support Angle · crackedBS 727 BULKHEAD SUPPORT ANGLE IS CRACKED AT RBL 5; WL 164<[01] REMOVED AND REMPLACED BULKHEAD SUPPORT ANGLE<BR>BS 727 RBL5 WL164 IAW SRM 51-40-02 AND DWG 144A2600 REV A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024081411117Support · corrodedAFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED AT BS 874 AND 881; RBL 17 WL 156<[01] NO DAMAGE NOTED; CLEANED AND INSPECTED IAW SRM 51-10-02;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024081411116Support · corrodedAFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED 727+5-767; RBL 21; WL 156<[01] REMOVED AND REPLACED NEW ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV:A;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024081311118Support · corrodedAFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED BS 727+5-847; LBL 21; WL 156<[01] AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT WITH CORROSION OUT OF LIMITS REMOVED AND REMPLACED IAW SRM 53-00-53-1A-2<BR>AND DWG 146A7500 REV A;[02] VERIFIED COMPLETION CORRECTISDR CALA2024073002141Stiffener · damagedREFER TAR 33 ACCOMPLISHMENT DRAFT RI 53-00-16938 REV A FIG.8, ITEM 15 - CUT STIFFENER AND INSTALL SPLICE BUT PRESSURE DECK O/B SIDE PREVIOUSLY DOUBLER REPAIRED INTERFRENCE NEW SPLICE INSTALL. TRANSFER REF. NON-ROUTINE HX NRC WO.3376315 CABIN STA 955 LBL 85.9 PSDR SWIA202407101Web · corrodedCORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED CLOSED) PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF FRAME FS 574.00 BETWEEN STR20L - 21L WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CU
Back to JASC 5320