JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 SWAA2021111538826Panel · pulledPANEL 193B HAS SEVERAL PULLED THROUGH CRACKED FASTENER HOLES ; / [01] IDENTIFIED PANEL / MATERIAL 193B IAW SRM 53-40-70-0I-1 FIG. 2. TABLE 2. ITEM (13).<BR><BR>FOUND 3EA. CRACKED FASTENER HOLE DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4. SDR DALA2021110106703None · none(LOG 2000381) DURING INSPECTION FOUND ELONGATED HOLES (10 EA) AND WEAR ON SETLEMENT ON ACCESS PANEL 193D AT LOWER FUSELAGE. REPAIRED PER B737-800 SRM 51-70-05-2R PROCEDURE 1 REPAIR 1 AND B737-800 SRM 51-70-05-2R PROCEDURE REPAIR GENERAL AND B737-800 SRM 53-40-SDR SWAA2021112933837Access Panel · delaminatedDELAMINATION ON FWD EDGE LOWER SURFACE OF ACCESS PANEL 193D LOWER FUSELAGE ; 2021-487813 / [01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE: 01-OCT-22; [02] HOT BONDER P/N HCS9200B-AV S/N 18196126 DUE DATE: 27-JAN-22.; [03] SCALE P/N SCA-301 S/N AE-4SDR SWAA2021112933838Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR ; 2021-487805 / [01] TOOL USED: CALIPER P/N: 500-197-30; S/N:A18229508; DUE DATE: 29-SEP-22.; [02] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 SDR SWAA2021110133339Panel · elongatedPANEL 193D HAS SEVERAL ELONGATED FASTENER HOLES. ; / [01] LOCATED HOLE IN NEW PANEL PER EO 5351-I-14642-NG; [02] REMOVED AND REPLACED PANEL PER SRM 51-10-02 AND 51-40-02.; [03] C/WSDR SWAA2021111733586Panel · delaminatedFUSELAGE FAIRING 192BR; FWD EDGE HAS EROSION AND DELAM. / REPAIRED DAMAGE TO FORWARD EDGE FAIRING 192BR IAW SRM 53-40-70-2R-1; SRM 51-70-04-2R-6; NDT PT. 4; 51-00-02; AMM 51-21-99-300-801 AND BAC 5064SDR SWAA2021102832709Panel · elongated193B PANEL HOLE #19 IS ELONGATED. (REF TASK CARD 5351-I-14108-NG FIG. 2 SHEET 1 FOR LOCATION IDENTIFICATION) ; / [01] INSTALLED WASHER PER SRM 51-10-05.SDR DALA2021102706652None · noneVAULT DOOR TAILCONE RELEASE PUSH-PULL CABLE TEFLON SHEATHING TORN AT RELEASE BLOCK STA 1212 AND AT THE 8 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE DEPSDR DALA2021102606627None · noneSHIP 1801 DURING INSPECTION FOUND LOWER AFT FAIRING FLAP DRIVE ASSEMBLY CLOSE-OUT PANEL WAS WITH DELAMINATION AND CRACK DAMAGE DAMAGE. REPAIRED PER SRM 51-70. (LP 1994929)SDR SWAA2021112232792Panel · delaminatedPANEL 193CR OUTER SKIN HAS A LARGE DISBOND IN CENTER OF PANEL. (MARKED) ; / [01] IDENTIFIED PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2 ITEM 9. <BR><BR>DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-40-1A-1 PARA 4.A.(6)(A).<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM SDR SWAA2021102632586Panel · crackedFOUND 3 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 1 FASTENER HOLE OVERSIZED ON 194E PANEL AS MARKED ON PANEL. ; FOND 3 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 1 FASTENER HOLE OVERSIZED ON 194E PANEL. ACCOMPLISH EA 21-153-03141 ASSIGNED ASDR SWAA2021102532345Panel · crackedFOUND 6 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 2 FASTENER HOLES ELONGATED AND OVERSIZED ON TRAILING EDGE OF 193D PANEL. ; FOND 6 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 2 FASTENER HOLES ELONGATED AND OVERSIZED ON TRAILING EDGE OF 193D SDR SWAA2021102531977Panel · elongatedWING TO BODY PANEL 194E HAS ONE FASTENER HOLE ELONGATED (MARKED) ; / [01] EA 21-153-03126 ADDED AS SUBTASK.; [02] REPAIRED PER EA 21-153-03126SDR SWAA2021102531917Panel · delaminatedWORKING MX NOTE MDDR/AUTH # 119759LT WING TO BODY FAIRING PNL 192BL US DELAMINATED ALONG FWD LEADING EDGE / ACCOMPLISHED NOISTURE REMOVAL AS REQUIRED BY EA 21-153-03106 IAW SRM 51-70-04 RE-APPLIED SPEED TAPE PER SIPSDR SWAA2021102530697Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED WING TO BODY FAIRING PANEL 193B PER SRM 51-40-02 AND SRM 51-40-05; [02] C/W INSPSDR DALA2021101906443None · noneSUPPLEMENTAL INFORMATION SHIP 3308 ON WALK FOUND PUNCTURE ON PANEL 191AB. CORRECTIVE ACTION: REFERENCE ER/A 594915-14 FOR REPAIR. REPLACED ACCESS PANEL 191AB. (8098146)SDR SWAA2021102030853Panel · elongatedSUPPLEMENTAL INFORMATION: 194E PANEL HOLES ; THE 194E PANEL HAS SEVERAL HOLES ELONGATED AND CRACKED. / [01] REMOVED AND REPLACED 194E PANEL IAW AMM 53-51-21SDR SWAA2021102030852Panel · elongatedSUPPLEMENTAL INFORMATION: 193D PANEL HOLES ; THE 193D PANEL HAS SEVERAL CRACKED AND ELONGATED HOLES. / [01] REMOVED AND REPLACED 193E IAW AMM 53-51-21SDR SWAA2021112230807Panel · delaminatedPANEL 193CR HAS DELAMINATED FWD UPPER CORNER ; / [01] IDENTIFIED PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2 ITEM [9] AND TABLE 2 ITEM [9]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-40-1A-1 PARA 4.B.(6).(A-B) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRSDR DALA2021101806393None · none(LOG 1984534) DURING INSPECTION FOUND ELONGATED HOLE AT AFT WING-TO-BODY FAIRING PANEL 193D SUPPORT STRUCTURE BTW STA BS 725. PERMANENT REPAIR ON ELONGATED HOLE AT AFT WING-TO-BODY FAIRING PANEL 193D SUPPORT STRUCTURE BTW STATION BS 725 WAS PERFORMED PER ETI-3SDR DALA2021101806392None · none(LOG 1984317) DURING INSPECTION FOUND WORN SETTLEMET AREA OF NUTPLATES ON SUPPORT STRUCTURE. PERMANENT REPAIR ON SETTLEMET AREA OF NUTPLATES ON SUPPORT STRUCTURE STA BS 727+2.7. WAS PERFORMED PER STEP NO.1 UNTIL STEP NO.17 OF ETI-37-21-500 REVISION. 2 AND ER/ASDR SWAA2021101829575Panel · elongatedSUPPLEMENTAL INFORMATION: SEVERAL ELONGATED HOLES IN 193B PANEL. ; / [01] REMOVED AND REPLACED THE CENTER WING TO BODY FAIRING PANEL 193B PER AMM 53-51-21.SDR 2021F00203Skin · damagedTAIL CONE SKIN (LEFT SIDE) DAMAGE. ACCOMPLISHED ENGINEERING DQ31887M1 DATED OCTOBER 13TH, 2021, 680A-0041 (N504QS) TAILCONE SKIN (LEFT SIDE) DAMAGE (FASTENER REMOVAL NICKED SKIN)SDR DALA2021101406357None · none(LOG 1981318) DURING INSPECTION FOUND ELONGATED HOLES (7 EA) AT AFT WING-TO-BODY FAIRING PANEL 193D. ELONGATED HOLES (7 EA) AT AFT WING-TO-BODY FAIRING PANEL 193D WERE REPAIRED PER B737-800 S.R.M 51-70-05-2R PROCEDURE 8 PAR. 4. AND B737-800 S.R.M. 51-70-05-2R SDR SWAA2021112328540Bracket · elongatedELONGATED HOLE ON BRACKET AFT MODULATION PANEL ON FAIRING AREA ; 2021-460672 / [01] REPLACED NEW BRACKET AND FASTENERS ON AFT MODULATION PANEL FAIRING AREA IAW B737-700 SRM 51-40-02.SEE INDIVIDUAL SIGN OFFS BELLOW.; [02] REPLACED BRACKET AND FASTENERS ON AFT MSDR SWAA2021111528817Access Panel · crackedCRACK ACCESS PANEL 194E BODY FAIRING AROUND FASTENERS HOLES AT LOWER FUSELAGE ; 2021-466191 / [01] TOOL USED HOT BONDER P/N:HCS9200B-AV; S/N: 18196021; DUE DATE: 14-DEC-21.; [02] REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-SDR SWAA2021101227837Panel · elongatedWING TO BODY PANEL 194E HAS ONE FASTENER HOLE ELONGATED (MARKED) ; / [01] ADDED DAMAGE RECORD <BR>EA 21-153-02981SDR SWAA2021101227836Panel · elongatedWING TO BODY PANEL 194E HAS ONE DELAMINATED FASTENER HOLE (MARKED) ; / [01] ACCOMPLISH EA ASSIGNED AS SUBTASK; [02] C/W EA 21-153-02981; [03] ADDED DAMAGE RECORD; [04] INCORRECT SELECT REFERENCE ENTERED. CHANGED TO 'EA-GENERAL' PER EA 21-153-02981SDR SWAA2021111528045Panel · elongatedELONGATED HOLE ACCESS PANEL 193B AT LOWER FUSELAGE ; 2021-466063 / [01] TOOL USED: CALIPER P/N:500-197-30; S/N:A18234364; DUE DATE: 25-SEP-22.; [02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 15-FEB-22; [03] TOOL USED: MULTIMETER P/N: FLUKE 8SDR SWAA2021111528047Panel · elongatedELONGATED HOLE ACCESS PANEL 194E AT LOWER FUSELAGE ; 2021-466076 / [01] REPAIRED ACCESS PANEL 194E AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. TOOL USED: CALIPER P/N:500-197-30; S/N:A18234364; DUE DATE: 25-SEP-22; HOT BONDER P/N:HCS9200B-AV; SDR SWAA2021111528049Panel · delaminatedDELAMINATED ACCESS PANEL 192AR AT LOWER FUSELAGE ; 2021-466054 / [01] APPLIED CONDUCTIVE COATING ON REPAIR AREAS ON ACCESS PANEL 192AR AS PER B737-700 SRM 51-70-05-2R-1 REPAIR 1 PARA. 4.G. AND B737-700 SRM 51-70-05-2R-0 REPAIR GENERAL PARA. 4.O. TOOL USED: MULSDR SWAA2021101127215Panel · elongatedCENTER WHEEL WELL PANEL 193D HAS MULTIPLE WORN AND/OR ELONGATED HOLES. ; / [01] TSR 2021006242 SUBMITTED WITH PICS.; [02] EA 21-153-02953 ADDED TO FAULT.; [03] C/W EA 21-153-02953SDR SWAA2021100826167Panel · cracked194E PANEL HAS 3 HOLES WITH CRACKS / [01] REMOVED AND REPLACED PANEL 194E PER AMM 53-51-21SDR SWAA2021100826168Panel · elongated193D PANEL HAS 5 ELONGATED HOLES ; 193D PANEL HAS 5 ELONGATED HOLES. / [01] REMOVED AND REPLACED PANEL 193D PER AMM 53-51-21.SDR SWAA2021100625872Panel · cracked194E PNL HAS 1 CRACKED FASTENER HOLE ON THE TRAILING EDGE ; / [01] INSTALLED NEW PANEL PER 53-51-21SDR SWAA2021100625873Panel · elongated193D PNL HAS 6 ELONGATED FASTENER HOLES ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR SWAA2021100625874Panel · cracked193D PNL HAS 2 CRACKED AND DIMPLED FASTENER HOLES ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR SWAA2021100625875Panel · corroded193D PANEL HAS EXISTING REPAIR THAT IS PITTED ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR DALA2021100606109None · none(LOG 1969778) DURING INSPECTION FOUND L/H FAIRING SUPPORT STRUCTURE FOR PANELS 193D AND 194E HAS DAMAGE AT NUT PLATE HOLES. C/W ER/A 594467-14AD REV ORIGINAL .SDR DALA2021100606108None · none(LOG 1969789) DURING INSPECTION FOUND R/H FAIRING SUPPORT STRUCTURE POR PANELS 193D AND 194E HAS DAMAGE AT NUT PLATE HOLES. C/W ER/A 594467-14AD REV ORIGINAL.SDR SWAA2021100625863Panel · elongated193D PANEL ATTACH HOLES ELONGATED ; WHILE PERFORMING VISAL INSP. OF 193D PANEL FOND SEVERAL HOLES CRACKED AND ELONGATED. / [01] REMOVED AND REPLACED WING TO BODY FAIRING 193D PER MM 53-51-21.SDR SWAA2021111725191Panel · delaminatedACCESS PANEL 193D AFT EDGE DELAMINATED. / [01] PREPARED FOR REPAIR PLIES THE AREA AT PANEL 193D AS PER B737-700 SRM51-70-04-2R-9; [02] OK TO INSTALL REPAIR.; [03] REPAIRED AT PANEL 193 D AS PER B737-700 SRM 51-70-04-2R-9 . MATERIAL USED PO.1731939 AND PO. 1694SDR DALA2021093005938None · noneSHIP 3304 A FACESHEET PUNCTURE WITH PARTIAL CORE DAMAGE COMMON TO WING-TO-BODY FAIRING PANEL 191AB. THE 'W' DISTANCE TO THE SANDWICH EDGE IS NOT MAINTAINED. CORRECTIVE ACTION: REFERENCE ER/A 594455-14. (8074794)SDR SWAA2021111724113Panel · crackedACCESS PANEL 193D AFT EDGE SEVERAL FASTENER HOLES CRACKED . ; / [01] CORRECTION FOR REFERENCE SRM 51-70-04-2R-9; [02] REPAIRED AT PANEL 193D AS PER B737- 700 SRM. 51-70-04-2R-9 .MATERIAL USED PO.1731939 AND PO 1694548; [03] VERIFIED ITEM 1 AND 2.; [04] RESTORESDR SWAA2021111724112Panel · elongatedFOUND SEVERAL FASTENER HOLES ELONGATED ON PANEL 194E ; / [01] PREPARED ON DAMAGED AREA ON PANEL 194E FOR REPAIR AS PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.C.; [02] VERIFIED PREPARATION<BR>OK TO INSTALL REPAIR; [03] REPAIRED DAMAGED AREA ON PANEL #194E AS PER B7SDR SWAA2021100424294Panel · cracked194E PANEL HAS 10 HOLES WITH CRACKS / [01] LOCATED AND DRILLED NEW FUSELAGE PANEL PN 149A555-8 PER <BR>SRM 51-40-05 AND SRM 51-40-08.; [02] INSTALLED NEW SERVICEABLE PANEL 194E PER AMM 53-51-21SDR SWAA2021100424295Panel · cracked193D PANEL HAS 4 HOLES WITH CRACKS / [01] INSTALLED PANEL PER AMM 53-51-21SDR SWAA2021111724101Panel · crackedPANEL 194E FWD EDGE 2EA FASTENER HOLES CRACKED. ; / [01] PERFORMED NDT INSPECTION ON PANEL #194E AS PER B737 NDTM 51-05-01 AND FOUND NO WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL.; [02] PREPARED DAMAGED AREA ON PANEL 194E FOR REPAIR AS PER B737 SRM 53-60-70-SDR MASA20211004452Plate · damagedSACRIFICIAL PLATE OF THE LAVATORY WASTE SERVICING SURROUND STRUCTURE WAS FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 3-51-23-001-001-A02, FIGURE 53-51-23-991-802, ITEM 6,EA 79-2021-237.SDR MASA20211004454Doubler · corrodedPOTABLE WATER SERVICING DOUBLER BETWEEN FS913.00 & FS881.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23, FIGURE 53-51-23-991-803, ITEM 3, EA 83-2021-042.
Back to JASC 5350