JASC 5714

Service difficulty reports · 1,451

Reports filed under 5714 · Wing, Center Box, 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 = '5714'
  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.

SDR DALA2021092305724None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 1 Y254 LOCATED ON FLOOR BEAM IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957917)Sep 22, 2021 · N350NA · Airbus A320212SDR DALA2021092305723None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 2 Y254 LOCATED ON FLOOR BEAM IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957916)Sep 22, 2021 · N350NA · Airbus A320212SDR DALA2021092305722None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 2 -Y254 LOCATED ON FLOOR BEAM IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957915)Sep 22, 2021 · N350NA · Airbus A320212SDR SWAA2021092111960Angle · crackedCRACK ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX ; 2021-384461 / [01] REMOVED ANGLE LOCATED BS 695 AND RBL 24 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700 ANGLE MUST BE REPLACED ; PERFORMED VISUAL INSAug 25, 2021 · N758SW · Boeing 7377H4SDR SWAA2021092210390Angle · crackedCRACK ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX ; 2021-392080 / [15] REPLACED ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 4 REV - AND DWG 111A6000 SHEET 2 REV. B. MATERIAL USED: BAC1490-2782; PO#2021Aug 24, 2021 · N228WN · Boeing 737*SDR FDEA202104121189Angle · corrodedAUX TANK PANEL LAND UPPER T CHORD AYB7080-5 SHOWS CORROSION UNDER RUB STRIP STA1366 X-28. REPAIRED UPPER ANGLE AYB7080-5 REF EA 8-5710-T0361291 "LOWER AUX FUEL CELL CORROSION UPPER CHORD" MAJOR REPAIR.Apr 12, 2021 · N319FE · Doug MD1030FSDR YENA2021041600247Skin · corrodedDURING HMV, EA A21-330-01 WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / Y1468 & STIFF 16-17 / CORROSION DAMAGE - PERMANENT REPAIR (THIS IS CONSIDERED A MAJOR REPAIR)Apr 11, 2021 · N509JB · Airbus A320232SDR YENA2021041600238Skin · corrodedDURING HMV, RER AEROMAN NR 2021-113286 CORROSION UPPER SURFACE OF UPPER SKIN CENTER WING BOX AT LEVEL FR41 AND FR42 BTW Y1292 AND Y1732 IN PASSENGER CABIN; "PERFORMED PERMANENT REPAIR ON UPPER SURFACE OF UPPER SKIN CENTER WING BOX AT FR41 TO FR42 BTW Y1292 ANDApr 11, 2021 · N509JB · Airbus A320232SDR CALA2021022200205Fitting · crackedSHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED LP 5866779 B737-57- 4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW UNITED EC/RA 5714-01201 REV ORIGINAL SSFR REPORT, FORM 46-0024 ENTERED BY UAL, 2/19/2021 ACCOMPLISHED INSPECTION.Feb 19, 2021 · N15710 · Boeing 737724SDR CALA2021022200204Fitting · crackedSHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED LP 5867921 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT FORM 46-0024 ENTERED BY UAL, 2-19-2021 ACCOMPLISHED INSPECTION.Feb 19, 2021 · N15710 · Boeing 737724SDR CALA2021022200203Fitting · crackedSHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED LP 5867920 B737-57 -4-1262. REMOVED AND REPLACED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED, 2-19-2021 ACCOMPLISHED INSPECTION.Feb 19, 2021 · N15710 · Boeing 737724SDR CALA2021022200202Fitting · crackedSHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED LP 5867918 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW UNITED ERIRA 5717-01201. SSFR REPORT, FORM 46-0024 ENTERED, ACCOMPLISHED INSPECTION.Feb 19, 2021 · N15710 · Boeing 737724SDR CALA2021022200201Fitting · crackedSHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED LP 5867917 B737-57 -4-1262. REMOVED AND REPLACED SHEAR FITTING IAW UNITED EC/RA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024 ENTERED, ACCOMPLISHED INSPECTION.Feb 19, 2021 · N15710 · Boeing 737724SDR CALA2021022200200Fitting · crackedSHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED LP 5867916 B737-57- 4-1262. REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAN UNITED ECIRA 5714-01201 REV ORIGINAL. SSFR REPORT, FORM 46-0024 ENTERED.Feb 19, 2021 · N15710 · Boeing 737724SDR DALA2021020400668Stringer · crackedSHIP 3239 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36. R. CORRECTIVE ACTION PERFORMED PERMANENT REPAIR PER ER/A 589108-14AD REV. ORIGINAL PRI 589108-14AD REV.0 AND REV. 1.Feb 3, 2021 · N339NW · Airbus A320212SDR SWIA202055671Nut · corrodedRIGHT OUTBOARD FLAP CENTER HINGEBOX CENTER MOUNT NUTS CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED RIGHT OUTBOARD FLAP CENTER HINGEBOX CENTER MOUNT CORRODED NUTS, IAW CRJ200 AMM REF 57-21-35-400-802.Dec 9, 2020 · N957SW · Cndair CL6002B19SDR SWIA202055670Nut · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGEBOX CENTER MOUNT NUTS CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED RIGHT OUTBOARD FLAP OUTBOARD HINGEBOX CENTER MOUNT NUTS, IAW CRJ200 AMM REF 57-21-35-400-803.Dec 9, 2020 · N957SW · Cndair CL6002B19SDR DALA2020041502262Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 4 HOLE 2 (INB SIDE) -Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINAApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502261Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 HOLE ZONE 2 FR 36 (INB SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502260Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 FR 36 -Y765 ZONE 1 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502259Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT HOLE ZONE 2 (O/B SIDE) Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV Apr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502258Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502257Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502255Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 3 AT ZONE 2 (O/B SIDE) Y254 AT FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502254Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT ZONE 1 Y254 (INB SIDE) FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502253Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 FR36 AT ZONE 1 Y254 INB ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211SDR DALA2020041502252Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 5 AT HOLE ZONE 1 FR 36 (O/B SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211SDR DALA2020031601875Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR36 FASTENER HOLE ZONE 2 (Y765) REPAIR PRIOR TO FURTHER FLIGHT WC 5711- 01036- 03B,AD 2018-13-08.CRACK POSTION 12 OCLOCK. (1 EA), PEFORMED REPAIR INSTRUCTIONS AT FRONT SPAR VERTICAL STRINGER AT FR Mar 15, 2020 · N337NW · Airbus A320212SDR DALA2020031401847Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36 FASTENER HOLE ZONE 2 (-Y254), PERFORMED REPAIR INSTRUCTION AT FRONT SPAR VERTICAL STRINGER FR36 ZONE 2 (-Y254) ASPER PRI 585381-14AD. REV.0, REV.1 REV.2 AND ERA 585381-14AD REV. ORIGINAL SECTIMar 13, 2020 · N337NW · Airbus A320212SDR DALA2020031401846Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36 FASTENER HOLE ZONE 1.(Y254), PERFORMED REPAIR INSTRUCTION AT FRONT SPAR VERTICAL STRINGER FR 36 ZONE 1 (Y254) ASPER PRI 585381-14AD REV. 0, REV.1 REV.2 AND ERA 585381-14AD, REV-ORIGINAL SECTIOMar 13, 2020 · N337NW · Airbus A320212SDR DALA2020031401845Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36 FASTENER HOLE ZONE 2(Y254), PERFORMED REPAIR INSTRUCTIONS AT FRONT SPAR VERTICAL STRINGER FR 36 ZONE 2 (Y254) ASPER PRI 585381-14AD REV. 0, REV.1 REV.2 AND ERA 585381-14AD REV. ORIGINAL SECTIOMar 13, 2020 · N337NW · Airbus A320212SDR DALA2020031401844Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36 FA STENER HOLE ZONE 1 (-Y765), PERFORMED REPAIR INSTRUCTIONS AT FRONT SPAR VERTICAL STRINGER AT FR 36 -Y765 ASPER PRI 585381-14AD REV.0, REV.1 AND REV.2 AND ERA 585381-14AD REV. ORIGINAL SECTIMar 13, 2020 · N337NW · Airbus A320212SDR DALA2020031401843Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36 FA STENER HOLE ZONE 1.(Y765), PERFORMED REPAIR INSTRUCTION AT FRONT SPAR VERTICAL STRINGER AT FR 36 ZONE 1 (Y765) ASPER PRI 585381-14AD REV. 0, REV.1 REV.2 AND ERA 585381-14AD REV. ORIGINAL SEMar 13, 2020 · N337NW · Airbus A320212SDR DALA2020031401842Stringer · crackedCRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36 FASTENER HOLE ZONE 2(-Y765), PERFORMED REPAIR INSTRUCTION AT FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36 HOLE ZONE 2 (-Y765) ASPER PRI 585381-14AD REV. 0, REV.1 AND REV.2 AND ERA 585381-1Mar 13, 2020 · N337NW · Airbus A320212SDR SWAA2022041154533Support Angle · crackedFLOOR ANGLE SUPPORT CRACKED AT APPROX. STA 540 LBL1 / REPLACED FLOOR PANEL BREAK ASSEMBLY PER SRM 51-40-02.Dec 5, 2019 · N466WN · Boeing 7377H4SDR SWAA2022040620807Attach Angle · crackedL\H WING TO BODY FAIRING STRUCTURE; STA 500D; STR 19L AT WING BULL NOSE HAS CHORD CRACKED. / REMOVED L/H WING TO BODY FAIRING STA 500D STR 19L FRAME CHORD IAW SRM 51-40-02-0G-0 VERIFIED NEW PART AS P/N 116A3118-9 FRAME ATAG A58549 IAW AIPC 57-40-00-48 PG 45. LNov 4, 2019 · N7863A · Boeing 7377Q8SDR HKGA20191008022Skin · crackedRH NACELLE FLAP TRAILING EDGE LOWER SKIN ATTACH FLANGE IS CRACKED. LOCATED AND DRILLED NEW RH NACELLE FLAP TRAIILING EDGE LOWER SKIN ATTACH FLANGE (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED ATTACH FLANGE (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ERSDR SWAA2022031047912Floor Panel · brokenCTR WING BOX AREA; FLOOR PANEL 241BF; LWR SURFACE HAS DEEP GROOVES / BROKEN COMPOSITE MATERIAL. / EVALUATED; PREPPED; CLEANED AND REPAIRED MULTIPLE AREAS OF DAMAGE COMPOSITE AT LWR SURFACE ON FLOORBOARD 241BF IAW B737 SRM 53-0-50-2R-1 PAR 3 (A; C-F; K1; L1; M1Jul 29, 2019 · N442WN · Boeing 7377H4SDR LR7A2019062401994Attach Angle · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CENTERWING LEADING EDGE TO OUTBOARD WING JOINT ATTACH ANGLE CRACKED CWS84.3 TO CWS178.8 FS497 WL272. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6381.Jun 24, 2019 · N409LC · Lkheed 382GSDR LR7A2019062401993Bracket · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CWS191 TO CWS200 BRACKET CRACKED DURING REMOVAL OF SPAR WEB REPLACEMENT ACCESS. CWS191R TO CWS200R WL272 FS517. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 638Jun 24, 2019 · N409LC · Lkheed 382GSDR LR7A2019062401991Cap · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CENTER WING FRONT WEB UPPER CAP CORROSION AND OVERSIZED HOLES CWS157.5 TO 209.5L FS517 WL257. REPAIRED IAW MEA 382-57-18-193 DWG #5730LH2527 NR #6377Jun 24, 2019 · N409LC · Lkheed 382GSDR LR7A2019062401990Cap · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CWS178R VERTICAL ATTACH TEE CAP CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6376.Jun 24, 2019 · N409LC · Lkheed 382GSDR LR7A2019062841667Structure · damagedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTERWING LOWER FWD #1 PLANK REQUIRES REPLACEMENT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.Jun 24, 2019 · N409LC · Lkheed 382GSDR CA190716002Pressure Deck · cracked(CAN) UPON INSPECTION, CRACK FOUND ON PRESSURE FLOOR STRUCTURE AT FS459 - RBL 0.0 - 9.0 (TC# 20190716002)Jun 23, 2019 · Cndair CL6002B19SDR FDEA201903190676Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR HOLE C NDT INSPECTION FOUND CRACK (LT) COMPLIED WITH EA: 6-5710-T0345244 P1, TITLE: WINGS - BASIC WING STRUCTURE - EO 6-5710-7-3305E3 P3 & P4 - CRACK HOLES AT FR47 REAR SPAR AREA. REPAIRED FUSELAGE CTR WING BOX REAR SPAR LH HOMar 19, 2019 · N659FE · Airbus A300F4605RSDR FDEA201903190674Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR RH HOLE F NDT INSPECTION FOUND CRACK COMPLIED WITH EA: 6-5710-T0345244 P1, TITLE: WINGS - BASIC WING STRUCTURE - EO 6- 5710-7-3305E3 P3 & P4 - CRACK HOLES AT FR47 REAR SPAR AREA. REPAIRED FUSELAGE CTR WING BOX REAR SPAR RT HOLEMar 19, 2019 · N659FE · Airbus A300F4605RSDR SWAA2022030369790Strap · crackedL/H W/W CENTER WING RIB STIFFENER; TO UPPER WING TO BODY STRAP CRACKED ABOVE #1 AFT FUEL BOOST PUMP. / R&R BODY STRAP AT L/H W/W CENTER WING RIB STIFFENER TO UPPER WING TO BODY ABOVE THE #1 AFT FUEL BOOST PUMP PER SRM 51-40-02Feb 14, 2019 · N952WN · Boeing 7377H4SDR SWAA2022030323666Vapor Barrier · crackedWHILE WORKING CUSTOMER CARD# T885736 FOUND R/H VAPOR BARRIER DBLR CRACKED / USING 2024-T3 .040 CLAD LOT #1372384-2 FABRICATED R/H VAPOR BARRIER DBLR. ALL WORK ACCOMPLISHED IAW DWG 65-88700; DWG 111A1511-28 DWG 111A1000. SRM 51-20-01-0G-0 DBLR IS REMOVED AND INFeb 11, 2019 · N272WN · Boeing 7377H4SDR SWAA2022022521965Intercostal · crackedPASSENGER CABIN FLOOR STRUCTURE; AREA ABOVE WING BOX CENTER SECTION; BS 540; BL 0 TO LBL 2; INTERCOSTAL CRACKED THROUGH LOWER ANGLE. / REMOVED AND REPLACED WITH NEW INTERCOSTAL PER SRM 51-40-02Jan 24, 2019 · N267WN · Boeing 7377H4SDR DALA2019010200007Skin · corrodedWHILE ON THE LINE IN ATL MTC WAS SEARCHING FOR THE SOURCE OF A FUEL SMELL IN THE AIRCRAFT CABIN AND FOUND CORROSION WHICH HAD CREATED A HOLE IN THE LT SIDE OF THE CENTER WING BOX AFT UPPER SKIN BETWEEN STA 87 AND STA994. THE MAIN AREA OF CORROSION AS A RESULT Jan 1, 2019 · N951DN · Doug MD9030
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