JASC 5330

Service difficulty reports · 79,329

Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330'
  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 JJBA2021082518054Doubler · corrodedCORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR AFT RADIO ALTIMETER #2 BTW FR 68-69. SKIN REPAIRED.Aug 18, 2021 · N14125 · Emb EMB145XRSDR SWAA2021092708216Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+12; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10Aug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708212Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+6; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10-Aug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708188Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+9; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-4[06] EVALUATED DAMAGED REMOVAL AT DISCREPANCY AREA L=0.5' W=0.6' ORIG. THICKAug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708225Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+13; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10Aug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708224Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+5; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] INSTALLED EWIS PROTECTION AT BS927-BS947 BL 0 PER AMM 20-60-07; [02] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT Aug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708219Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+8; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5' W=0.5'.PERFORMED VISUAL INSPECTION WITH A 10-Aug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708208Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+14; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708207Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+12; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708189Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 907+10; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [01] REMOVED 1 EA FASTENER AT DISCREPANCY AREA PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.6 W= 0.5 PERFORMED VISUAL IAug 17, 2021 · N208WN · Boeing 737SDR SWAA2021092708183Skin · corrodedCORROSION AROUND FASTENER AT BS 887+16, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6A. NO ADDITAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708215Skin · corrodedCORROSION AROUND FASTENER AT B.S. 927+11; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. ; / [11] INSTALLATION OF 1 EACH FASTENER WAS ACCOMPLISHED ON EA# 21-153-02635-WIP1; [12] REFER TO FAULT TTG8Q006DPMC WHERE EA 21-153-02635 WAS ADDED AS A SUBTASK; [Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708220Skin · corrodedCORROSION AROUND FASTENER AT BS 927+9, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. ] REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02 PARAGRAPH 15Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708217Skin · corrodedCORROSION AROUND FASTENER BS 927+14, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO MAKE SURE ALL OF THE CORROSION WAS REMOVED IAW SRM 51-Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708218Skin · corrodedCORROSION AROUND FASTENER AT BS 927+15, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02 PARAGRAPH 15.Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708213Skin · corrodedCORROSION AROUND FASTENER AT BS 927+7, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708214Skin · corrodedCORROSION AROUND FASTENER AT BS 927+10, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02, PARAGRAPH 15Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708210Skin · corrodedCORROSION AROUND FASTENER AT BS 907+17, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS, NO CORROSION IAW SRM 51-10-Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708209Skin · corrodedCORROSION AROUND FASTENER BS 907+15, BL 0, WL 306.5 ON SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.5 W= 0.5 PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS TO MAKE SUREAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708206Skin · corrodedCORROSION AROUND FASTENER AT BS 907+11, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIOAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708204Skin · corrodedCORROSION AROUND FASTENER AT BS 907+13, BL 0, WL 306.5 FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION & PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIONAL DAMAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708205Skin · corrodedCORROSION AROUND FASTENER AT BS 907+16, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. . REMOVED CORROSION, PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO ADDITIONAL DAMAGE NOTED. HFEC INSPECTED SKIN BLEAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708203Skin · corrodedCORROSION AROUND FASTENER AT BS 907+7, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONAL DAMAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708202Skin · corrodedCORROSION AROUND FASTENER AT BS 907+5, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH, 15 A 6 A. NO ADDITIAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708187Skin · corrodedCORROSION AROUND FASTENER AT BS 907+8, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708186Skin · corrodedCORROSION AROUND FASTENER AT BS 907+6, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER AT DISCREPANCY AREA IAW SRM 51-40-02. REMOVED CORROSION PERFORMED A VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708185Skin · corrodedCORROSION AROUND FASTENER AT BS 907+4, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION, PERFORMED VISUAL INSPECTION WITH 10-POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6 A. NO ADDIAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708201Skin · corrodedCORROSION AROUND FASTENER AT BS 887+15, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING, IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708199Skin · corrodedCORROSION AROUND FASTENER AT BS 887+12, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONALAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708200Skin · corrodedCORROSION AROUND FASTENER AT BS 887+14, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS, CORROSION WAS REMOVED IAW SRM 51-10-02, PARAAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708198Skin · corrodedCORROSION AROUND FASTENER AT BS 887+11, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS. CORROSION REMOVED IAW SRM 51-10-02, PARAAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708197Skin · corrodedCORROSION AROUND FASTENER AT BS 887+10, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIOAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708196Skin · corrodedCORROSION AROUND FASTENER AT BS 887+9, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA15 A 6 A. NO ADDITIONALAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708195Skin · corrodedCORROSION AROUND FASTENER AT BS 887+8, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED THE FASTENER IAW SRM 51-40-02. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708193Skin · corrodedCORROSION AROUND FASTENER AT BS 887+6, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708190Skin · corrodedCORROSION AROUND FASTENER AT BS 887+3, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION , PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A . NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAWAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708192Skin · corrodedCORROSION AROUND FASTENER AT BS 887+5, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER IAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708191Skin · corrodedCORROSION AROUND FASTENER AT BS 887+4, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION AND PERFORMED A VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARA 15 A 6 A. NO ADDITIONAL DAMAGE NOTED. REMOVED THE FASTENER Aug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708184Skin · corrodedCORROSION AROUND FASTENER AT BS 887+17, BL 0, WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02, PARAGRAPH 15 A 6 A. NO ADDIAug 17, 2021 · N208WN · Boeing 7377H4SDR SWAA2021092708182Skin · corrodedCORROSION AROUND FASTENER AT B.S. 887+13; B.L. 0; W.L. 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED ONE FASTENER IAW SRM 51-40-02. REMOVED CORROSION. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS IAW SRM 51-10-02 PARAGRAPH 15.A.6.A. NO AAug 17, 2021 · N208WN · Boeing 7377H4SDR MASA20210915441Doubler · crackedCRACK IN DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT STRUCTURE DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT STRUCTURE WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01Aug 17, 2021 · N957LR · Cndair CL6002D24SDR MASA20210915424Skin · corrodedCORROSION ON INNER FUSELAGE SKIN BTW FS280-295 STGR 25R-24R AT MAIN AVIONICS COMPARTMENT. FUSELAGE SKIN BTW FS280-295 STGR 25R-24R WAS REPAIRED PER EA 81-2021-069 REV. AAug 17, 2021 · N957LR · Cndair CL6002D24SDR IPXA2021091073782Skin · corrodedINSPECTION TYPE:3CR/H AFT FUSELAGE SKIN BETWEEN STA 2103 TO 2163.685 AND BETWEEN LONGERONS 33R TO 35R IS CORRODED.REPAIRED CORRODED R/H FUSELAGE SKIN BETWEEN STA 2103 TO 2163.685 AND BETWEEN LONGERONS 33R TO 35R IAW VT-SAA EA 011-5330-01-A9311 REV. IR AND UPS Aug 17, 2021 · N284UP · Doug MD11FSDR JJBA2021082517055Doubler · corrodedCORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR FWD RADIO ALTIMETER #2 BTW FR 65-56. SKIN REPAIRED.Aug 17, 2021 · N14125 · Emb EMB145XRSDR SWAA2021082308194Skin · corrodedCORROSION AROUND FASTENER AT BS 887+7, BL 0, WL 306.5, ON FUSELAGE SKIN UNDER DORSAL FIN. REMOVED CORROSION, L= 0.7' W=0.7'. PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO INSURE ALL CORROSION REMOVED IAW SRM 51-10-02 PARAGRAPH 15.A.6.A .NOAug 17, 2021 · N208WN · Boeing 7377H4SDR DALA2021081904837Skin · dentedSHIP 650 ER/A 593437-14, DURING HCK AT QRO, DENTS WERE NOTED ON THE FUSELAGE SKIN, STA 1400-1440, STR 27R-28L. ER/A 593437-14 SECTION I REPAIR WAS PERFORMED. FOLLOW ON ACTION IS REQUIRED FOR DTE. (1915308)Aug 17, 2021 · N650DL · Boeing 757232SDR DALA2021081904836Skin · damagedSHIP 650 DTE/MONITOR INSP. REF. ER/A 384081-14AD REV. C; FUSELAGE / SKIN / F.S. 590-661 / S14L ? S19L / REPAIR OF DAMAGE. CORRECTIVE ACTION: REF ERA 384081-14AD REV C. (1915090)Aug 17, 2021 · N650DL · Boeing 757232SDR DALA2021081904835Skin · damagedSHIP 650 AMOC/MONITOR INSP. REF. ER/A 384081-14AD REV. C; FUSELAGE / SKIN / F.S. 590-661 / S14L-S19L / REPAIR OF DAMAGE. CORRECTIVE ACTION: REF SKIN REPAIR PER ER/A 384081-14AD REV. C. (1915094)Aug 17, 2021 · N650DL · Boeing 757232SDR DALA2021081904831Skin · dentedSHIP 650 IN REF. TO NRC 00826: DENT OUT LIMITS ON FUS SKIN BTW STA 1425 AND S-28-L TO 29-L. CORRECTIVE ACTION: SUMMARY OF NRC 00828: DENTS ON FUSELAGE SKIN BTW STA 1400 TO STA 1440 AND S-27R TO S-27L WERE REPAIRED PER ETI-57-21-368 REV. 4 AND ERA 593437-14 RE.Aug 17, 2021 · N650DL · Boeing 757232SDR DALA2021081804777Skin · corrodedCORROSION ON AFT CARGO SKIN. SUMMARY SEE NRC 105-0008:5331-2001/012 00365: BLENDED AND CHECKED LIMITS IN SKIN PER B717 SRM 53-00-00- 1A. REPLACED SKIN CLIP PER DWG #9912243 AND B717 SRM 51-40-02. (LP #1915089)Aug 17, 2021 · N978AT · Boeing 717200
Back to JASC 5330