Boeing 747-2B4B
Service difficulty reports · 509
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '7472B4B' 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 aircraft_model_key = '7472B4B' 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 CKSA98680Frame · corrodedCHORD VERT FLANGE AT ZONE 100, STA 1394 TO STA 1480, WL 152, RBL 127 HAS AREA APPROX 18 INCHES OF EXFOLIATED CORROSION. REPAIRED IAW BOEING ASA CKF-EXB-223 SUPP SHTS 6 AND 7. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENSDR CKSA98679Web · corrodedOUTBOARD SIDE OF WEB ASSY LOCATED ZONE 100, STA 1372 TO STA 1416, WL 152, RBL 127 HAS NUMEROUS AREAS OF SEVERE CORROSION AND PITTING. REPAIRED IAW BOEING DOCUMENT ASA CKF-EXB-223 SUPP SHTS 6 AND 7. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CSDR CKSA98678Spar · corrodedRT ELEVATOR REAR OUTBD SPAR, ZONE 300, HAS 6 AREAS 6 TO 8 INCHES OF SEVERE CORROSION WITH EXFOLIATION. REMOVED AND REPLACED SPAR IAW BOEING DWG ASA CKF-EXB-217 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OSDR CKSA98677Longeron · corrodedLONGERON CHORD AT LWG ZONE 100, STA 1372 TO STA 1460, WL 152, LBL 127 (LT OVERWING) REPLACED FOR LEVEL 2 CORROSION. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NSDR CKSA98676Frame · corrodedFWD AND AFT SIDE OF THE 65B06740-44 FRAME ASSY AT STA 920, WL 92, BL 0 TO LBL 20 HAS AREA OF LEVEL 2 CORROSION COVERING APPROX 10 PERCENT OF SFC. REPAIRED IAW BOEING ASA CKF-EXB-239 SUPP SHT 2 ITEM 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROSDR CKSA98675Channel · corrodedSTA 840, WL 91, RBL 21, THE AFT I/B FLANGE OF THE 69B01835-1 BODY FAIRING CHANNEL HAS AN AREA APPROX 1.50 SQ INCH WITH MODERATE CORROSION. REPAIRED IAW BOEING ASA CKF-EXB-239 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK,SDR CKSA98674Skin · corrodedSKIN PANEL ASSY AT ZONES 100-200 (EXT SKINS) STA 2360, STR 46L TO 46R, RBL 8 TO LBL 8, HAS APPROX 4 SQ INCH AREA OF LEVEL 2 CORROSION NEAR LAV SVC DOOR. REPAIRED IAW BOEING ASA CKF-EXB-069 SUPP SHT 6. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE SDR CKSA98673Structure · corrodedKEEL BEAM AREA ZONE 129-204, STA 1267 TO STA 1480, BRACKETS, FITTINGS, FASTENERS, FRAMES AND WEBS HAVE SIGNS OF CORROSION. REPAIRED ALL IAW SRM 51-10-01, SRM 51-10-02 AND ASA AMD-CKF-EXB-136 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINSDR CKSA98672Structure · corrodedLAV LEAK CAUSED LEVEL 2 CORROSION TO BRACKETS, FITTINGS, WEBS, CLIPS, ANGLES AND FASTENERS IN AREA BETWEEN LANDING GEAR DOORS. ZONE 191, STA 1322 WL 96 LBL 5. REPAIRED IAW ASA CKF-EXB-136 SUPP SHT 2, SRM D6-13592, CHAPTER 51-30-02 AND ASA CKF-EXB-172. FOUNDSDR CKSA98671Bulkhead Ring · corrodedZONE 310, PRESSURE BLKHD STA 2360 WL 185 BL 0 TO RBL 6, THE AFT FACE OF RING SEGMENT 65B02634-328 HAS 4 SQUARE INCH AREA OF LEVEL 2 CORROSION. REPAIRED IAW ASA CKF-6XB-065 SUPP SHT 2, 3, 4. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, ANSDR CKSA98670Skin · corrodedSKIN PANEL ASSY AT SEC 48 RT FS, ZONE 310 STA 2598 STR 46R JUST ABOVE TAIL JACK PAD, HAS AREA 1.5 SQUARE OF LEVEL 2 CORROSION. REPAIRED IAW SRM 51-10-01, 51-10-02, SRM 51-30-02, DWG 65B02701 SH 6. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHSDR CKSA98669Frame · corrodedINSIDE SKIN AFT NR 3 RT DOOR FRAME STA 139 WL 212 RBL 127 HAS 2 X 6 AREA OF EXFOLIATED CORROSION. REPAIRED IAW D6-41910 PART 1, 747 SRM 53-30-01 DETAIL 2 OF FIG 1, AND ASA AMD-CA-014 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECSDR CKSA98668Web · corrodedUPPER SURFACE OF PRESSURE DECK, WEB 65B13375-9 LOCATED STA 1340 TO 1350, WL 186, RBL 2-11, HAS 10 X 8 AREA OF LEVEL 2 CORROSION. REPAIRED IAW ASA CKF-CA-017 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CSDR CKSA98667Skin · corrodedUPPER WING SKIN PANEL AT STA 1125 WL 200 RBL 127 HAS AN AREA 6.0 X 2.0 OF LEVEL 2 CORROSION. AREA IS NEAR UPPER WING TO BODY. REPAIRED IAW SRM 51-10-01, FIG 18.01 PER D6-5000 AND ASA CKF-CF-010 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSISDR CKSA98666Skin · corrodedUPPER WING SKIN PANEL AT STA 1090 WL 200 RBL 127, HAS AN AREA 2.0 X 2.0 OF LEVEL 2 CORROSION. REPAIRED IAW SRM 51-10-01, FIG 18.01 PER D6-5000 AND ASA CKF-CF-009 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENTSDR CKSA98665Floorbeam · corrodedFLOORBEAM UPPER CAP 65B38085 AT AFT MAIN DECK ZONE 200, STA 1700 WL 199 LBL 18 TO LBL 23 HAS LEVEL 2 EXFOLIATED CORROSION ON AFT EDGE OF -3 CAP. REPAIRED IAW ASA CKF-AMD-127 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, SDR CKSA98664Seat Track · corrodedAT ZONE 200 AFT MAIN DECK, STATION 2258 WL 199 LBL 33, THE INBD FLANGE OF 65B38271-1 SEAT TRACK HAS 1 SQAURE AREA OF LEVEL 2 EXFOLIATED CORROSION. REPAIRED IAW 747 SRM 53-10-05 ALT 1 DETAIL 1 AND ASA CKF-AMD-121. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSISDR CKSA98663Frame · corrodedFLOORBEAM CAP LOCATED AT ZONE 200 AFT MAIN DECK, STA 2260, WL 199, RBL 44 HAS SCREW HOLE SHOWING CORROSION AREA OF 0.60 DIAMETER. REPAIRED IAW ASA CKF-AMD-115 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OFSDR CKSA98662Seat Track · corrodedIN AFT CARGO AREA ZONE 100, STA 1770 RBL 24 WL 118 HAS AN AREA 0.4 X 0.6 OF EXFOLIATED CORROSION ON SEAT TRACK 65B06548-6. REPAIRED IAW ASA CKF-AMD-096 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TSDR CKSA98661Floorbeam · corrodedFLOORBEAM UPPER CAP AT ZONE 200, STA 2349 WL 199 LBL 32 HAS AREA 1 X 1 OF SEVERE CORROSION. DEPTH OF CORROSION EXCEEDS 20 PERCENT OF MATERIAL. REMOVED AND REPLACED THE 65B06161-7 UPPER CAP IAW BOEING DWG 65B06161 SHTS PL & 2. FOUND DURING ACCOMPLISHMENT OF SDR CKSA98660Skin · corrodedSKIN PANEL LOCATED AT ZONE 100, STA 1960 STR 51R TO 51L WL 125 HAS AREA APPROX 4.0 SQ INCHES OF MODERATE CORROSION. REPAIRED IAW 747 SRM 53-30-03, FIG 47 DETAIL 1 AND ASA CKF-AMD-068 SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHESDR CKSA98659Skin · corrodedSKIN PANEL LOCATED BETWEEN STA 2183 AND 2187, STRINGER 44R AND 46R, HAS AN AREA OF APPROX 3 X 6 OF LEVEL 2 CORROSION. REPAIRED IAW ASA CKF-AMD-053 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CSDR CKSA98658Stringer · corrodedUPPER FLANGE OF STRINGER LOCATED ZONE 100 STA 2064 STR 28R WL 185 HAS .5 AREA OF SEVERE CORROSION. REMOVED CORROSION IAW SRM 51-10-01, TREATED PER SRM 51-10-02 AND DWG 65B04154. REPAIRED IAW ASA CKF-AMD-088. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, SDR CKSA98657Seat Track · corrodedTOP SURFACE OF SEAT TRACK LOCATED ZONE 200 STA 1780 TO STA 1940 WL 200 RBL 11 HAS MOD TO SEVERE CORROSION. AREA OF CORROSION APPROX 15 PERCENT. REPAIRED IAW DWG 65B38253 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHSDR CKSA98656Seat Track · crackedSTA 2110 WL 200 LBL 33, THE CROWN AREA OF THE 65B38265-1 SEAT TRACK HAS 2 CRACKS. ONE CRACK RUNS FROM AFT EDGE OF -1 SEAT TRACK FWD FOR .80 LONG. THE OTHER CRACK RUNS FROM AFT EDGE OF -1 SEAT TRACK FWD FOR 5 LONG. REPAIRED IAW ASA CKF-AMD-032 SUPP SHT 2. FSDR CKSA98655Floorbeam · corrodedUPPER CAP OF FLOORBEAM LOCATED ZONE 200 STA 1820 WL 200 FROM LBL 11 TO RBL 25, HAS AREA OF EXFOLIATED CORROSION COVERING APPROX 40 PERCENT OF CAP. REPLACED IAW SRM 51-30-02 DWG 65B17767. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ASDR CKSA98654Seat Track · corrodedSEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 1946 TO STA 2280 WL 199.5 RBL 11.33 HAS AREA APPROX 24 OF LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND SDR CKSA98653Seat Track · corrodedSEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 1770 TO STA 2110 WL 199.5 RBL 33.99 HAS AREA APPROX 24 OF LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND SDR CKSA98652Seat Track · corrodedSEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 2100 WL 199.5 RBL 89 HAS AREA APPROX 24 OF LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT SDR CKSA98651Shear Tie · corrodedSHEAR TIE AT ZONE 100, STA 1720, STR 51R TO STR 51L, WL 91 BL 0, HAS APPROX 6 SQ AREA OF LEVEL 2 CORROSION. REPAIRED IAW CKF-AMD-025 SUPP SHT 1, 2, 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT SDR CKSA98650Seat Track · corrodedSEAT TRACK AT ZONE 200, STA 1620, WL 200, LBL 11 HAS AREA 1 X 2.5 OF EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38253 SHT 1 AND ATTACHMENT SHEETS 1-3 AND ASA-CKF-AMD-023 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, ANDSDR CKSA98649Seat Track · corrodedSEAT TRACK AT ZONE 200, STA 1680 TO STA 1703, WL 200, HAS AREA 1.2 X 3 WITH LEVEL 2 PITTING CORROSION. REPAIRED IAW AMENDMENT CKF-AMD-109 SHT 2 AND DWG 65B38251 SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPSDR CKSA98647Floorbeam · corrodedTOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1740, WL 200, LBL 8 TO LBL 38 HAS 4 AREAS 1-2 DIAMETER WITH EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38087 SHT 4. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP SDR CKSA98646Floorbeam · corrodedTOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1660, WL 200, LBL 33-39 HAS AREA 6 X 2.5 WITH EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38083 SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT SDR CKSA98644Floorbeam · corrodedSTA 1780 WL 200 RBL 24 THE TOP SURFACE OF UPPER CAP HAS AREA 1.20 X 2.50 OF LEVEL 2 CORROSION. REPAIRED IAW SRM 51-10-01 FIG 18.01. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIASDR CKSA98643Skin · corrodedSKIN (ONLY) AT ZONE 100, STA 2200, BETWEEN STR 48 AND 49 HAS AREA OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-30-03 FIG 1 AND CKF-AMD-053 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING SDR CKSA98641Chord · corrodedMAIN DECK CARGO DOOR UPPER CHORD CORRODED UNDER HINGES FULL LENGTH OF DOOR, INTERIOR WEB CORRODED BEYOND LIMITS (NOT CONNECTED TO DOOR). REPAIRED IAW MM 52-34-01 AND DWG 65B17895-1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPSDR CKSA98640Skin · corrodedMACHINED SKIN AT STA 1484 BETWEEN STR 10 LT AND 11 LT HAS AREA OF EXFOLIATED CORROSION 2 INCH DIAMETER, APPROX .050 DEEP. REPAIRED IAW SRM 53-30-03 FIG 47. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDSDR CKSA98639Upper Chord · corrodedAT UPPER DECK ZONE 230, STA 440, RBL 46-49, WL 309, UPPER CHORD HAS AREA OF LEVEL 2 CORROSION 3.5 X 1.5. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280SDR CKSA98638Seat Track · corrodedLEVEL 2 CORROSION FOUND ON SEAT TRACK AT ZONE 230, STA 520 TO 600, WL 307, LBL 27.99. REPAIRED IAW 747 SRM 53-10-05, ALTERNATIVE 1, PAGE 2A. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICSDR CKSA98637Floorbeam · corrodedTOP CHORD OF FLOORBEAM AT UPPER DECK ZONE 230, STA 520, WL 307, LBL 27.99 TO LBL 46.65 HAS AREA 20 X 2 OF LEVEL 2 CORROSION. REPAIRED IAW DRAWING 65B10936 SUPP SHEET 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENSDR CKSA89648Floorbeam · corrodedTOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1720, WL 200, BL 0 TO LBL 108 HAS SEVERAL AREAS 1 INCH DIAMETER WITH EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38134-6 ITEMS 2 AND 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOSDR CKS98642Stringer · corrodedSTRINGER 51R AT STA 2176 TO STA 2180 HAS AREA OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-30-03 FIG 1 AND CKF-AMD-053 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORKSDR CKSA98605Stiffener · corrodedNR 2 STIFFENER IN RT NR 1 PYLON HAS NUMEROUS AREAS OF CORROSION. NDT VERIFIED OUT OF LIMITS. REPAIRED IAW ASA CKF-PYL-017, CKF-PYL-029 & CKF-PYL-031 INCL ALL SUPP SHEETS. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBSDR CKSA98604Stringer · corrodedSTRINGER NEAR FWD LAV SVC PANEL ZONE 120, STA 550, STR 46L, WL 95, LBL 15 HAD AREA 7 X 2 CORRODED. REPAIRED IAW ASA CKF-K1-051 SUPP SHEETS 1 & 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CSDR CKSA98603Skin · corrodedSKIN PANEL AT STA 550, LBL 15-18, WL 95 HAD AREA 3.5 X 6 CORRODED. REPAIRED IAW ASA CKF-KI-51 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125-01-01.SDR CKSA98602Skin · corrodedFWD CARGO DOOR AT ZONE 120, STA 592, INTERIOR DOOR SKIN/WEB HAD AREA 1 X 3 OF CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ASA CKF-K1-026 SUPP SHEETS 3 & 4. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280SDR CKSA98601Splice · corrodedON WING TO BODY FAIRING SUPPORT STRUCTURE, STA 960, WL 95 TO 98, RBL 1-RBL 22 SPLICE WEBS FOUND AREA 3 X 22 CORRODED. BLEND OUT BEYOND SRM LIMITS. REPAIRED IAW ASA CKF-K1-031 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB)SDR CKSA98600Shear Tie · corrodedSHEAR TIE AT ZONE 120, STA 980, STR 47L, WL 95, LBL 0, HAD AREA OF CORROSION APPROX 3 X 4. ALSO STR 47R AT SAME LOCATION HAD AREA OF CORROSION APPROX 2 X 6. REPAIRED IAW SRM 747-51-10-01 AND ASA CKF KI-022. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOESDR CKSA98599Ground Strap · disbondedRT AILERON O/B GROUND STRAPS AT T/E CORRODED AND DISBONDED AT STATIC DISCHARGERS. REPAIRED IAW ASA CKF-EXW-090 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C57-560-01
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