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 SWAA2021060943984Former · chafedFAIRING FORMER BS 657-665 LBL 28 HAS CHAFE DAMAGE / REMOVED AND REPLACED FAIRING FORMER BS657-665 LBL28 IAW SRM 51-40-05; SRM 51-40-02; SRM 53-40-71-1A-1 AND AIPC 53-42-00-91BSDR IPXA2020052645696Support Frame · crackedINSPECTION TYPE:3CR/H WING TO BODY AT STRINGER 31 RH HAS VERTICAL ATTACHMENT SUPPORT FRAME CRACKED.REMOVED, FABRICATED CRACKED SUPPORT FRAME AND INSTALLED AT RH WING TO BODY AT STRINGER 31 IAW DRAWING ANB7143 AND SRM 51-35-01. (MINOR)SDR IPXA2020051155173Angle · crackedINSPECTION TYPE:3CL/H UPPER WING TO BODY FAIRING ATTACH FRAME HAS BOTTOM L-ANGLE CRACKED AT STA 1401.REMOVED FABRICATED AND INSTALLED L-ANGLE AT L/H WING TO BODY FRAME AT STA 1401 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)SDR IPXA2020052055483Frame · wornINSPECTION TYPE:3CTAILCONE FRAME AT LH MIDDLE GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR IPXA2020052055479Frame · crackedINSPECTION TYPE:3CTAILCONE RH FRAME CRACKED AT MIDDLE GUIDE PIN.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-01 REPAIR 1 FIG 201. (MINOR).SDR IPXA2020051555336Frame · wornINSPECTION TYPE:C3TAILCONE FRAME AT LH UPPER GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR IPXA2020051555335Frame · wornINSPECTION TYPE:3CTAIL CONE FRAME AT RH UPPER GUIDE PIN WORN THRU.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR IPXA2020041354146Support · corrodedINSPECTION TYPE:N/ASUPPORT STRUCTURE UNDERNEATH TAILCONE ON A/C SIDE CORRODEDREPAIRED PER DWG 148N1606 & SRM 51-40-02SDR SWIA20205110560Diaphragm · cracked*DIAPHRAGM CRACKED JUST AFT OF FS909.00 STGR 24L AT BOTTOM (MARKED (C-CHECK) RO 5/7/2020 REPAIRED WING TO FUSELAGE AFT FAIRING SUP. FS909.00, LBL17. COMPLIED WITH BOMBARDIER REO AND COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)SDR SWIA20205060521Support · corrodedFORWARD WING-TO-FUSELAGE FAIRING LONGITUDINAL SUPPORT STRUCTURE BETWEEN FS629 AND FS661 HAS CORROSION AROUND FASTENERS (C-CHECK) RO 5/4/2020 INSTALLED NEW LONGITUDINAL SUPPORT STRUCTURE BETWEEN FS 629 TO FS 661 P/N SH670-39063-1 P/O 10207-0011/79 . REFSDR SWIA20205060520Splice Angle · corrodedAFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE AT FS939 IS CORRODED (C-CHECK) RO 5/4/2020 REMOVED, REPLACED AND INSTALLED NEW AFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE REF CRJ 700 SRMSDR SWAA2021082782262Panel · damagedWING TO BODY FAIRING 193B PANEL HAS SEVERAL ELONGATED SCREW HOLES. / REMOVED AND REPLACED PER AMM 53-51-21SDR IPXA2020050454884Longeron · crackedINSPECTION TYPE:2CTAIL CONE R/H UPPER LONGERON BEAM IS CRACKED AT THE FWD. END.REPAIRED TAIL CONE R/H UPPER LONGERON BEAM IAW UPS EO MD11-5350-66790-A. (MINOR)SDR IPXA2020050154830Doubler · wornINSPECTION TYPE:2CTAIL CONE LH UPPER LONGERON @ PRODUTION DOUBLER IS WORN THRU.REPAIRED TAILCONE LONGERON / INTERNAL DOUBLER IAW EO MD11-5350-66790-A. (MINOR)SDR IPXA2020050154829Frame · crackedINSPECTION TYPE:2CTAIL CONE FWD. R/H FRAME IS CRACKED AT THE CENTER GUIDE PIN HOLE.REPAIRED TAIL CONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG. 201. (MINOR)SDR IPXA2020050454885Doubler · chafedINSPECTION TYPE:2CTAIL CONE R/H UPPER PRODUCTION DOUBLER HAS CHAFE DAMAGE.REPAIRED TAIL CONE R/H PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-A. (MINOR)SDR CALA2020040300783Skin · dentedFUSELAGE TAIL CONE UPPER SKIN UPPER SURFACE AT FR85-86 STRINGER 1R-2R FOUND 1EA DENT MARK REF NON-ROUTINE NO.9410324 -ORIGINATED, SPEC NO.A3NB-06-3-6001. FUSE TAILCONE FR85-FR86 STR1R-STR2R REPAIRED AS PER SRM 53-51-30 0-011 REV 132. THIS IS A CATAGORY A REPAISDR DALA2020040602193Support · corrodedSHIP 5803 CORROSION ON LH/RH BODY FAIRING FRAME SUPPORT LOWER AREA AT STA 860 (FUS). CORRECTIVE ACTION: SUMMARY OF NRC S/N 00682, LH/RH BODY FAIRING FRAME SUPPORT LOWER AREA AT STA 860 (FUS), WERE REPAIRED PER ER/A 586288-14 REV ORIG SECTION 1, PERMANENT REPAISDR DALA2020033102108Panel · puncturedSHIP 3836 FILLET PANEL 193AL FWD OF LMLG HAS SMALL PUNCTURE. CORRECTIVE ACTION: REMOVED DAMAGE AND POTTED CORE PER B737-900 SRM 53-40-70. INSTALLED PERMANENT REPAIR PER B737-900 SRM 53-40-70-2R PROCEDURE 1. (6736887).SDR VNAA202003249992Drag Angle · crackedSUSPECT CRACK AT LH AFT TAIL CONE DRAG ANGLE. REMOVED LH AFT TAIL CONE DRAG ANGLE (PART #AV670-21186-003) IAW CRJ 900 SRM 51-40-00-001-001-A01. INSTALLED NEW LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-21-001-001-A01, AND 51-42-22-001-001-A01.SDR VNAA202003249991Drag Angle · crackedSUSPECT CRACK AT RH AFT TAIL CONE DRAG ANGLE. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH AFT DRY ANGLE PN:AV670-21186-004 IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR SWAA2021082781882Panel · damagedWING TO BODY FAIRING PANEL 193B HAS ENLARGED HOLES AT FASTNER LOCATION 6;9;10;11;21;24;25;36;+37 / REMOVED AND REPLACED PANEL 193B PER MM 53-21-400-802 AND 51-20-07-0G-0SDR SWAA2021082732892Panel · delaminatedWING TO BODY FAIRING PANEL 193B HAS DELAMINATION AT FASTNER HOLE LOCATION 2;3;4;5;6;+8 / REMOMED AND REPLACED PANEL 193B PER MM 53-21-400-802 AND 51-20-07-OG-0SDR SWAA2020032442643Panel · delaminatedWING TO BODY PANEL 193B RT FWD CORNER DELAMINATED AND SEVERAL SCREW HOLES ENLARGED. REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B PER AMM 53-51-21.SDR HALA2020031900066Cable · out of positionTAIL CONE JETTISON KEVLAR CABLE ROUTED INCORRECTLY FROM PAINT. // RE-ROUTED TAIL CONE RELEASE KEVLAR CABLE PER AMM 53-52-01, SECURITY CHECK OK.SDR SWAA2021060987113Support · chafedCHAFING ON 193AR BODY FARING PANEL I/B SUPPORT BS667 RBL27. / REMOVED AND REPLACED FAIRING FORMER SUPPORT BS 667 RBL 27 FOR 193AR BODY FAIRING PANEL IAW SRM 51-40-05; SRM 51-40-02 AND AIPC 53-42-00-91BSDR SWAA2021060987112Support · chafedCHAFING ON 193AL BODY FARING PANEL I/B SUPPORT BS667 LBL27. / REMOVED AND REPLACED FAIRING FORMER SUPPORT BS 667 LBL 27 FOR 193AL BODY FAIRING PANEL IAW SRM 51-40-05; SRM 51-40-02 AND AIPC 53-42-00-91B.SDR SWAA2021082510138Panel · delaminatedLOWER WTB PANEL 193B HAS MISSING MATERIAL AND WEAR ON UPPER SURFACE PERIMETER FROM CONTACT WITH STRUCTURE. L/H O/B FWD CORNER DELAMINATED APPROX. .2' DEEP AND .7' LONG. / REMOVED AND REPLACED LOWER WTB PANEL 193B PER AMM 53-51-21.SDR UIEA2020031300384Skin · dentedTWO DENTS ON FUSELAGE TAIL CONE SKIN BETWEEN STA 1873.40 / STA 1881.75 AND LBL 3.4 / LBL 7.5.(<DIV> / </DIV><P ><SPAN>ONE DENT WAS FOUND WITHIN / SRM LIMITS. THE OTHER DENT WAS REPAIRED PER B767-300 SRM 53-00-01-2R-10 / REPAIR 10. SEE RAM FORM N662GT-20-03.</SSDR 7C7A2020032700022Tail Cone · damagedFORWARD TAILCONE ASSEMBLY (P/N 85560061) HAS MULTIPLE AREAS OF BUBBLED PAINT AND SOFT COMPOSITE ALONG RIGHT SIDE OF FUSELAGE.SDR FDEA2020042390766Stiffener · crackedAFT BULKHEAD TAIL CONE AT UPPER R/H SUPPORT STIFFNER (3RD FROM THE TOP, MARKED IN RED) O/B IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR HAT CHANNEL PER E.A. 8-5310- T0353336 AND SRM 51-31-01 VOL. 1.SDR SWIA2020032749471Angle · corrodedEXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS939.00 ANGLE IS CORRORED (AS MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED NEW ANGLE P/N SH670-39189-1 AT EXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS932.00 REF CRJ700 SRM.SDR DALA2020031701907Panel · damagedSHIP 3871 ON WALK AROUND FOUND DAMAGE ON PANEL 149A7556 . CORRECTIVE ACTION: INSTALLED PERMANENT REPAIR PER B737 SRM 53-60-70. (7139179).SDR DALA2020030701692Latch · out of adjustTAILCONE RELEASE TEST FAILED USING AFT BULKHEAD DOOR. ADJUSTED RIGHT UPPER AND LEFT LOWER TAILCONE LATCHES PER MD88 AMM 5353 OPS CHK NML. (LP1519691)SDR SWAA2020032442670Support · chafedCHAFING ON 193AR BODY FARING PANEL IB SUPPORT BS667 RBL27. REMOVED AND REPLACED FAIRING FORMER COMMON TO PANEL 193AR RBL27 IAW SRM 51-40-02 AND DWG 149A7210, P/N 7531195 PO# 784910 89004U 18MAR20SDR DALA2020031001744Cable · out of adjustTHE TAIL CONE RELEASE TEST FAILED WITH THE AFT BULKHEAD DOOR. MAINTENANCE ADJUSTED THE AFT BULKHEAD DOOR ARM ASSEMBLY PULL CABLE REF B717 AMM 53- 52. OPERATIONAL CHECK IS NOW FUNCTIONAL. (LP #1518530)SDR DALA2020030901735Splice · corrodedCORROSION LEVEL: 2 CORROSION WTB FAIRING 139CL HAS CORROSION ON SPLICE. ( ATTACHED TO PANEL) FOUND TO BE OUT OF LIMITS. REPLACED SPLICE. (LP 1519139)SDR DALA2020030901734Splice · corrodedCORROSION LEVEL: 2 CORROSION*** WTB FAIRING 139DL HAS CORROSION ON SPLICE. ( ATTACHED TO PANEL) OUT OF LIMITS. REPAIRED SPLICE. (LP 1519129)SDR EBVR20200306001Stinger · corrodedTAIL STINGER HAD SOME CORROSION BEYOND LIMITS, COMPLIED WITH MINOR REPAIR TO TAIL STINGER IAW AQRD ERO-966015,REV.IR DATED 03-02-2020SDR DALA2020030701693Latch · wornTAILCONE ATTACH LATCH @0800 POSITION LOOSE AND WORN. REPLACED TAILCONE ATTACH LATCH AT 0800 POSITION PER MD88 AMM 53-53 NEEDS ADJUSTMENT AT TAILCONE INST.(481754) TAILCONE LATCH ADJUSTED OPS NML. (LP1519811)SDR REXA2020033000373Channel · crackedFOUND AFT FAIRING CHANNEL BROKEN
REMOVED & REPLACED & MODIFIED AFT FAIRING CHANNEL IAW CRJ 900 SRM 51-42-13-001-001-A01 & IS670538200021 & ENDEAVOR EO# R53573. WCACSDR SWAA2021082720905Panel · delaminatedWING-TOBODY FAIRING #194DL; LOWER SIDE OF PANEL; 6.00' BY 1.00' AREA OF DELAMINATION; 13.0' FROM FWD EDGE; 12.0' FROM O/B EDGE OF PANEL; AREA MARKED IN BLACK / REPAIRED AND APPLIED DECRATIVE FINISH ON WING TO BODY FAIRING 194DL LWR SIDE OF PANEL 6' X 1' AREA OSDR SWAA2021082520904Fairing · delaminatedWING-TO-BODY FAIRING #194DL; LOWER SIDE ; .750' BY .750' DENT WITH DELAMINATION ON PANEL; AREA MARKED IN BLACK; 7.0' FROM AFT EDGE; 10.50' FROM I/B EDGE OF PANEL / EVALUATED AND FOUND DAMAGE ON WING TO BODY FAIRING PANEL 194 DL TO BE DELAMINATION WITH MINOR COSDR SWAA2021082781173Panel · damagedWING TO BODY FAIRING PANEL 193B HAS SEVERAL ELONGATED FASTENER HOLES. / REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B PER AMM 53-51-21.SDR SWAA2021081218855Radome · damagedNOSE RADOME HAS MULTIPLE SPOTS OF DAMAGE WITHIN 10' OF EACH OTHER / REMOVED AND REPLACED NOSE RADOME IAW AMM 53-52-00-000-801 AND AMM 53-52-00-400-801 WN7935 AAR TOOL # 34005 DUE 11/22/20 AAR TOOL # 34005 DUE 11/22/20 TW # 39119 DUE 07/22/20 POS: P TAG/GRB NO.SDR RAIA2020040160006Angle · crackedL/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE NUTPLATE SUPPORT IS CRACKED....R&R L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE.SDR RAIA2020040106005Angle · crackedL/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE NUTPLATE SUPPORT IS CRACKED....R&R L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE.SDR RAIA2020032760003Angle · crackedLH W/W FWD O/B CORNER CENTER BELLY FAIRING 'L' ANGLE NUTPLATE SUPPORT IS CRACKED - FABRICATED AND PARTIALLY INSTALLED REPAIR FOR LH W/W FWD O/B CORNER CENTER BELLY FAIRING L ANGLE. BELLY FAIRING NEEDS TO BE TEMP INSTAALED TO PICK UP NUTPLATE POSITIONSDR DALA2020022701454Receptacle · looseVARIOUS PIN RECEPTACLES ON TAIL CONE LOOSE. REPLACED HARDWARE AS NEEDED REF MD88 SRM 51-30-02. (LP1506012)SDR DALA2020022501395Rivet · missing2 RIVETS MISSING @ UPPER AND LOWER CLIPS FWD OF LOWER R/H TAILCONE LOCK PIN. INSTALLED 2EA RIVETS UPPER AND LOWER CLIPS FWD OF LOWER R/H TAIL CONE LOCK PIN. IAW MD88 SRM 51-30-0. (LP1503328)
Back to JASC 5350