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 JR2R20240620527Angle · crackedANGLE CLIP CRACKED AT FWD SIDE OF FR12 LBL36 IN FLIGHT DECK.SDR JR2R20240620528Angle · crackedANGLE CLIP CRACKED AT FWD SIDE OF FR12 BL0 IN FLIGHT DECK.SDR JR2R20240620257Seal Rest · corrodedUPON REMOVAL OF FWD CARGO DOOR SCUFF PLATE, FOUND CENTER SEAL REST CORRODED. REPLACED.SDR JJBA20240918016Profile · corrodedCORROSION FOUND NEAR FR65 AND STGR 16L ON PROFILE. REMOVED AND REPLACED LOWER SECTION OF SHEAR CLIP AT FRAME 65.SDR SWAA2024080703358Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2024-404773<[01] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: SDR SWAA2024080703354Access Panel · delaminatedDELAMINATED ACCESS PANEL 194FR BODY FAIRING AT FUSELAGE EXTERIOR 2024-404754<[01] TOOL USED CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15/FEB/25.;[03] TOOL USED: SCALE P/N: CR520SDR SWAA2024080703361Intercostal · crackedCRACK ON INTERCOSTAL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2024-404783<[01] REPLACED BRAKE PANEL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 AT PASSENGER IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 36 REV.SDR VNAA20240726010Strap · corrodedCORROSION ON JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). WAS REPAIRED PER REO 690-53-21-1789 REV - -SDR SWAA2024071603318Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-357658<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23325591; DUE DATE: 11-JAN-25.;[02] TOOL USED: PHOTOMETER/RADIOMETER P/N: XRP-3000; S/N: 1859843; DUE DATE: 24-JUL-24;[03] REPAIRED FWD CORNESDR FDEA202406190985Support Web · deformedAFT FUSELAGE FOUND 2EA SUPPORT WEB GOT DEFORM AT FR86 S35R AND S38R REPLACED THE NEW SUPPORT WEBS WITH RIVETS. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 AND 51-40-21-001 PARA.6, PAGE.7B~23, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, AT AFT FUSELAGE FR86SDR ASAA2024061950835Floor Support · corrodedAFT WET AREA FLOOR SUPPORT RBL 50 STA 947 TO 967 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT AT RBL 50 FROM STA 947 TO 967 IAW BOEING 737-900 SRM 51-40-02-0G-0W-2" O-.085" R-.075" L-2" D-.010.SDR ASAA2024061950629Floor Support · corrodedAFT WET AREA FLOOR SUPPORT RBL 20 STA 967 TO 986 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FOOR SUPPORT IAW B737-900ER SRM 51-40-02-0G-0W-1.5" O-.075" R-.058" L-1.5" D-.017".SDR ASAA2024061950628Floor Support · corrodedAFT WET AREA FLOOR SUPPORT RBL 20 STA 947 TO 967 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-900ER SRM 51-40-02-0G-0W=3" O=.075 R=.012 L=4 D=.063.SDR ASAA2024061950627Transition Panel · corrodedL/H TRANSITION PANEL STA 500H TO 500L IS CORRODED. GROUNDED - YES. L/H TRANSITION PNL STA 500H TO 500L REPAIRED IAW B737-900ER SRM 53-00-53-2R-6W=2" O=.040" R=.035" L=10" D=.005".SDR ASAA2024061950626Transition Panel · corrodedR/H TRANSITION PANEL STA 500H TO 500L IS CORRODED. GROUNDED - YES. R/H TRANSITION PNL STA 500H TO 500L REPAIRED IAW B737-900ER SRM 53-00-53-2R-6W .8 O .040 R .032 L 1.8 D .008.SDR ASAA2024061950623Floor Support · crackedFWD WET AREA INTERCOSTAL CRACKED AT RBL 30 STA 312 TO 328. GROUNDED - YES. REMOVED AND REPLAED INTERCOSTAL IAW B737-900 ER SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.SDR DALA2024062506467Shield · corroded(LOG 0405602) AFT CARGO COMPARTMENT, AFT SHIELD AT AFT CARGO DOOR CORRODED. AFT CARGO DOOR WAS REPAIRED BY REPLACEMENT IAW B737-900 SRM 51-10-02-0G PAR. 9C, SRM 51-40-02-0G AND DWG 146A0081.SDR DALA2024062106303Channel · corroded(LOG 0403708) CORROSION ON AFT CARGO ZEE CHANNEL FROM STA 727A TO 827, LBL 23. REPAIRED IAW B737 SRM 53-00-53-2R-5 FROM STA 727 TO STA 847 C.SDR DALA2024062106301Baffle · corroded(LOG 0403686) FORWARD CARGO COMPARTMENT R/H FLOOR BAFFLE STA 500F-500G CRACKED. REMOVED AND REPLACED BAFFLE AT STA 500F-500G STR 26 R/H IAW B737 SRM 51-40-02-0G AND B737 SRM 53-30-53-2R.SDR DALA2024062106300Web · corroded(LOG 0403680) FORWARD CARGO BAY THRESHOLD WEB HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED FWD CARGO BAY THRESHOLD WEB. IAW B737 SRM 51-40-02-0G AND DWG 143A8330 REV A.SDR N6WA2024062102Insulation · wornBLEED DUCT WARNING MSG RIGHT SIDE. PERFORMED DETAILED PHYSICAL PNEUMATIC AND BLEED SYSTEM LEAK CHECK IN RT PYLON AND AFT EQUIPMENT BAY IAW AMM 36-10-00. R & R RT HASOV INSULATION BLANKET IAW AMM 21-61-08. RESECURED INSULATION VALVE INSULATION BLANKET IAW CRJ ASDR JJBA20240906002Door Sill · corrodedUPON REMOVAL OF BAGGAGE DOOR PROTECTOR STRIP, FOUND CORROSION ON FRAME 66 DIRECTLY UNDER REMOVED PROTECTOR STRIP AREA. REMOVED AND REPLACED BAGGAGE DOOR SILL. APPLIED TOP COAT TO BAGGAGE DOOR SILL.SDR SWAA2024080503196Gusset · crackedCRACK GUSSET LOCATED BS 500I AND S-19R AT FWD CARGO COMPARTMENT 2024-401555<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500I AND S-19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7902 SHEET 256 REV:B SEE INDIVIDUAL SIGN OFF BELOW;[02] COMPSDR SWAA2024080503197Gusset · crackedCRACK GUSSET LOCATED BS500I AND S-21L AT FWD CARGO COMPARTMENT 2024-401557<[01] REPLACED GUSSET LOCATED BS500I AND S-21L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 AND DWG 143A7902 SHEET 256 REV B.;[02] CERTIFIED STEPSDR SWAA2024080503199Angle · crackedCRACK ANGLE - CLIP LOCATED BS500H AND STR26L FWD FACE FWD CARGO COMPARTMENT 2024-401554<[01] REPLACED ANGLE- CLIP AND FASTENERS LOCATED BS500H AND STR26L FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 AND DWG 143A7505 SHEET 108 REV -. SESDR SWAA2024080503198Angle · crackedCRACK ANGLE - CLIP LOCATED BS500H AND STR26L AFT FACE FWD CARGO COMPARTMENT 2024-401556<[01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS500H AND STR26L AFT FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 DWG 143A7505; SHEET 109; REV.- SEE SDR SWAA2024080503200Angle · crackedCRACK ANGLE - CLIP LOCATED BS500H AND STR26R FWD FACE FWD CARGO COMPARTMENT 2024-401558<[01] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND STR26R FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 AND DWG 143A7505 SHEET 108;109;110; RSDR SWAA2024080503201Angle · crackedCRACK ANGLE - CLIP LOCATED BS500G AND STR26R FWD FACE FWD CARGO COMPARTMENT 2024-401559<[01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS500G AND STR26R FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 AND DWG 143A7505 SHEET 108;109; REVSDR SWAA2024080503203Web · crackedCRACK STIFFENER ASSY LOCATED BS 540 BETWEEN BL 0 TO RBL 24.75 AT CENTER WING BOX 2024-401565<[01] REPLACED ONLY UPPER WEB LOCATED ON STIFFENER BS 540 BETWEEN BL 0 TO RBL 24.75 AT CENTER WING BOX IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 143A5240 SHEET 14 REV SDR SWAA2024080503204Stiffener · crackedCRACK STIFFENER ASSY LOCATED BS 540 BETWEEN BL 0 TO LBL 24.75 AT CENTER WING BOX 2024-401566<[01] REPLACED STIFFENER ASSY LOCATED BS 540 BETWEEN BL 0 TO LBL 24.75 AT CENTER WING BOX IAW B737-800 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 143A0060 SHEET SDR SWAA2024072402674Floor Panel · pulledPANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] TRIMMED SHAPE FOR NEW FLOOR PANEL FROM BMS4-17TYVI LOT 1553922-1; LOCATED INSERT HOLES AND UP-SIZED INSERTS HOLES; ALL THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A AND PARAGRAPH 4.A; TABLE SDR ASAA2024061851091Transition Panel · corrodedFWD PIT TRANSITION LH SIDE HAS CORROSION STA 500B TO 500E. GROUNDED - YES. REMOVED AND RELACED FWD PIT TRANSITION L/H SIDE IAW B737-800 SRM 51-40-02-0G-0.W= 1" O= .040 R= .034 L= 2" D= .006.SDR SWAA2024071802968Support Bracket · crackedAFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED UNDER WASTE TANK POST @ S-26L STA 867 MKD DOT<[01] REMOVED AND REPLACED NEW BRACKET AT AFT CARGO COMPARTMENT FLOOR SUPPORT UNDER WASTE TANK S-26L STA 867 PER REF 51-40-02-0G-0 AND DWG# 149A8102.;[02] VERIFIEDSDR SWAA2024071802972Support Bracket · crackedAFT OF AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED AFT END @ S-25L STA 947.75 MKD DOT<[01] SUMMARY: REMOVED AFT CARGO FLOOR SUPPORT BRACKET AT STA 947.75 S-25L AS PER B 737 SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW BRACKET AT S-25 STA 947.75 AS PER REFSDR ASAA2024061850951Transition Panel · corrodedAFT PIT R/H TRANSITION HAS CORROSION STA 767-727D. GROUNDED - YES. REMOVED AND REPLACED TRANSITION FROM STA 767-727D IAW B737-800 SRM 51-40-02-0G-0, AFT PIT R/H TRANSITION FROM STA 727E TO STA 727B FOUND TO BE IN LIMITS IAW B737-800 SRM 53-00-53-1A-2W= 1' O= .SDR ASAA2024061850758Sidewall Support · corrodedAFT CARGO SIDEWALL SUPPORT AT STA 727I RBL 26 IS CORRODED. GROUNDED - YES. REMOVED DAMAGE SIDEWALL SUPPORT FOUND TO BE OUT LIMITS IAW B737-900ER SRM 53-00-07-1A-1 REMOVED AND REPLACED SIDEWALL SUPPORT IAW B737-900ER SRM 53-00-07-2R-4W:1" O: .063" R: .032" L: 2SDR ASAA2024061850755Strap · corrodedAFT CARGO STRAP RBL 24 STA 807 TO 827 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE AFT CARGO STRAP FOUND TO BE OUT LIMITS IAW B737-900ER SRM 53-60-15-1A-1, REMOVED AND REPLACED AFT CARGO STRAP IAW B737-900ER SRM 51-40-02-0G-0W: 2" O: .080 R: .068" L: 1" D: .0SDR SWAA2024070802758Strip · corrodedFWD CARGO CAP STRIPS HAVE SEVERAL AREAS OF CORROSION FOUND AFTER CLEANING.<[01] R+R CAP STRIPS AS REQUIRED PER AMM 25-52-06SDR ASAA2024061850688Transition Panel · corrodedAFT CARGO R/H TRANSITION AFT OF DOOR HAS AREAS OF CORROSION GROUNDED - YES. REMOVED DAMAGE TRANSITION PANEL FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2, REMOVED AND REPLACED TRANSITION PANEL IAW SRM 53-00-53-2R-5 W:1" O:.040" R:.032 L:1" D:.008SDR AALA202407024325Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD RIGHT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.SDR ASAA2024061850631Shield · corrodedAFT CARGO FWD SHIELD HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED DAMAGE, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-60-15-1A-1, REMOVED AND REPLACED SHIELD AT AFT CARGO FWD SIDE, IAW B737-900ER SRM 51-40-02-G-0W 1.5 O .050 R .000 LSDR ASAA2024061850630Transition Panel · corrodedAFT CARGO R/H TRANSITION HAS AREAS OF CORROSION STA 737A TO STA 767. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2, REPAIRED TRANSITION IAW B737-900ER SRM 53-00-53-2R-5W: 1" O: .040" R: 0 L: 1" D: .040".SDR ASAA2024061850621Angle · corrodedAFT CARGO L/H TRANSITION HAS AREAS OF CORROSION STA 727A TO 847. GROUNDED - YES. REMOVED CORROSION FOUND OUT LIMITS IAW B737-900ER SRM 53-00-53-1A-2 & FABRICATED TRANSITION IAW B737-900ER SRM 53-00-53-2R-5W=1" O=.040" R=.023" L=1" D=.017".SDR AALA202406276511Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD LEFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.SDR IPXA2024062611207Tee Angle · corrodedL/H LOWER FUSELAGE AT STA. 1240 VERTICAL T-CORD HAS CORROSION ISNTALLED T-CHORD L/H FUSELAGE AT STA 1240 VERTICAL. SRM 51-40-02.SDR IPXA2024062405953Web · corrodedL/H LOWER FUSELAGE BETWEEN STA. 1200-1260 WEB HAS CORROSION INSTALLED NEW CHANNEL, FILLER AND ANGLE, IAW SRM 51-40-02-0G.SDR AALA202406253748Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 312 AND STA 328, LBL 46. REPLACED INTERCOSTAL PER AARD 51-00-05-1 AND SRM 51-40-01-0G.SDR AALA202406246236Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 321, LBL46. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202406245374Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 335, LBL 46. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR DALA2024062106302Intercostal · corroded(LOG 0403693) CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL STA 787-794 RBL 23 WL 158. REMOVED AND REPLACED INTERCOSTAL AT STA 787-794 RBL 23 WL 158 IAW B737 SRM 51-40-02-0G-0 AND DWG# 146A8320 REV: A.
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