N434BC
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
52 reports on file, 2015-08-26 – 2015-12-31.
Part: WEDGE — DENTED (RT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
RIGHT INBD MAIN FLAP T/E WEDGE UPPER SURFACE HAS TWO DENTS WITH SHARP CREASES. ACCOMPLISHED REPAIR OF THE TWO DISCREPANT DENTS, APPROX 1" EACH, ON RT INBD MAIN FLAP T/E WEDGE UPPER SURFACE IAW SRM 51-70-10.
Part: WEDGE — DENTED (NR 10 SLAT) · airframe 29,224 hrs · 17,053 cycles
NR 10 L/E SLAT T/E WEDGE UPPER SURFACE HAS SHARP DENT AT INBD END. HOT BOND REPAIRED IAW SRM 51-70-10.
Part: SKIN — DENTED (BS 700) · airframe 29,224 hrs · 17,053 cycles
1 EA DENT ON FWD CARGO LT FRAME UPPER FLANGE AND ONE DENT ON SIDE OF FRAME AT BS 700 BETWEEN STR 23L-25L. TRIMMED OUT THE DENTS. ACCOMPLISHED PERMANENT REPAIR REF SRM.
Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 29,224 hrs · 17,053 cycles
AFT CARGO DOOR LOWER AFT EDGE SIDE FRAME HAS CORROSION. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO DOOR LOWER AFT EDGE SIDE FRAME REF ER/A 541042-14, REV ORIGINAL.
Part: SEAT TRACK — CORRODED (BS 695-733) · airframe 29,224 hrs · 17,053 cycles
CABIN FLOOR STRUCTURE BS 695-733, RBL 45, SEAT TRACK SUPPORT CORRODED. REMOVED CORRODED AREA FROM BS 695-733 CABIN FLOOR STRUCTURE, RBL 45, FOUND 8, AREAS, L-3.5" W-0.090, D-0.025", L-1.3" W- 0.070" D-0.010", L-1.4 W-0.070 D-0.015, L-1.5" W-0.085" D- 0.019", L-1.5" W-0.070" D-0.009", L-1.6 W-0.080 D-0.025", L-1.8 W-0.070, D 0.010 8, L-.050", W-0.040, D 0.040. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-57, FIG 101, DETAIL VII. R & R SEAT TRACK SUPPORT AT MAIN CABIN BETWEEN BS 640 TO 780, RBL 45 IN REF SRM 51-40-02, AND DWG 143N5099, ER/A 541040-14, REV ORIGINAL.
Part: FRAME — DENTED (BS 1320) · airframe 29,224 hrs · 17,053 cycles
WHILE WORKING NRC 100-41, DISCOVERED 2 EA DENTS ON AFT CARGO FRAME BS 1320 BETWEEN STR 24R AND STR 26R. CUTOUT 2 EA DAMAGED AREAS AT BS 1320 BETWEEN STR 24R & 26R IAW SRM 53-00-07, REPAIR 5. DIMENTIONS OF BOTH CUTOUTS W=1.0 " X L=1.125" X 0.5"R ORIGINAL MATERIAL THICKNESS .071". ACCOMPLISHED REPAIR IAW SRM 53-00-07, REPAIR 5. REPAIR IS CAT B, ZONE 1 WITH THRESHOLD INSPECTION TO START AT 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION. ACFT IS CURRENTLY AT 17053 F/C REF. SRM 53- 00-07, REPAIR 5, FIG 201, TABLE II, PAGE 210. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: DECK PLATE — CORRODED (BS 1680) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN DECK PLATE AT BS 1680, BL-0 TO LBL-54 AND BETWEEN BS 1700-1710, LBL-51. REMOVED CORROSION ON DECK PLATE BS 1681, BL0 TO LBL 54 AND STA 1700-1710 AT LBL 51 IAW SRM 51-10-02, PARA 15 AND 53-60- 51 ALLOW. DAMAGE 2, PARA 2, STEP C. BLENDED AREA AT BS 1681 BL0 TO LBL 54 MEASURES 54.0" IN LONG X 2.0" IN WIDE. BLENDED AREA AT BS 1700 TO 1710 AT LBL 51, MEASURES 10.0", LONG X 1.0" WIDE. ORIGINAL MATERIAL THICKNESS OF DECK PLATE IS .071" IAW DWG 146N5318. MATERIAL LOSS IN BOTH AREAS IS .006" AND IS WITHIN LIMITS REF SRM 53-60-51 PARA 4, TABLE 101 AND 102. ADDITIONAL CORROSION FOUND ON ATTACH PLATE 146N5230-40 IAW SRM 51-10- 02, PARA 15. BLENDED AREA MEASURED 2.0" L X 2.0" W, ORIGINAL MATERIAL THICKNESS IS .063" REF DWG 146N5230-40, MATERIAL LOSS IS .015" AND IS OUT OF LIMITS IAW SRM 53-60-51 ALLOWABLE DAMAGE 2. R & R ATTACH PLATE AT BS 1680, BL 0 IAW DWG 146N5230 & SRM 51-40-02, PARA. 4.
Part: HINGE — DAMAGED (MLG DOOR) · airframe 29,224 hrs · 17,053 cycles
UPON REMOVAL OF CORROSION ON NR 100-124, FOUND ELONGATED, DAMAGED FASTENER HOLE, FWD-RT POSITION AT BS 1120, CENTER MLG DOOR HINGE ATTACH FITTING. R & R DAMAGED CENTER MLG DOOR HINGE ATTACH SUPPORT FITTING AT BS 1120 IAW SRM 51-40-02 PARA 9, PG 10 & DWGS 144N8180, 144N8110.
Part: FRAME — CORRODED (BS 1040) · airframe 29,224 hrs · 17,053 cycles
LOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24, CORROSION AROUND NUTPLATES. REMOVED CORROSION ON LOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24 IAW SRM 53-00-71. ALLOW-DAMAGE 1, FIG 101 DETAIL IX FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71. ALLOW-DAMAGE, 1 FIG 101, DET IX, BLENDED AREA NR 1, 2.6"L X 10.6" W WITH MRT 0.068" AND BLENDED AREA NR 2, 2.6" L X 2.6" W WITH MRT 0.075". ACCOMPLISHED REPAIR IAW ER/A 541038-14, REV ORIGINAL PERMANENT REPAIR.
Part: FRAME — DAMAGED (BS 700) · airframe 29,224 hrs · 17,053 cycles
FWD CARGO RT FRAME DENTED AND GOUGED ON UPPER FLANGE AT BS 700 BETWEEN STR 23R-25R. TRIMMED OUT 3 DAMMAGED SECTIONS AND PERMANTLY REPAIRED IAW SRM.
Part: STRAP — MISREPAIRED (BS 365-377) · airframe 29,224 hrs · 17,053 cycles
CABIN FLOOR STRUCTURE BS 365-377, LBL 25, FLOOR BEAM STABILIZATION STRAP HAS IMPROPER PREVIOUS REPAIR INSTALLED AT BS 365 AND STRAP IS CRACKED ABOVE REPAIR AT BS 375.5. FLOORBEAM STABILIZATION STRAP AT BS 365-377, LBL 25 HAS IMPROPER PREVIOUS REPAIR INSTALLED AND 2 EA ADDITIONAL CRACKS AT BS 365, LBL 24.75 CRACK NR 1 IS .950" IN LENGTH, CRACK NR 2 IS .850" IN LENGTH. R & R FLOORBEAM STABILIZATION STRAP FROM BS 345 TO BS 418 AT LBL 25 REF DWG 141N5150, SRM 51-40-02, PG 21.
Part: FRAME — DENTED (BS 1520) · airframe 29,224 hrs · 17,053 cycles
AFT CARGO BS 1520 BETWEEN STR 25L-26L TOP OF FRAME HAS DENT, GOUGE. FRAME AT BS 1520 BETWEEN STR 25L AND 26L HAS 2 EACH DENTS ON TOP OF FRAME, LOWER DENT MEASURES .63"W X .95"L, UPPER DENT MEASURES .85" W X .95" L, BOTH DENTS ARE OUT OF LIMITS REF SRM 53-00-07 PG 101, ALLOWABLE DAMAGE 1, FIG 101. PERFORMED REPAIR TO FRAME AT BS 1520, STR 25L TO 26L REF SRM 53- 00-07, REPAIR 5, DETAIL 2 AND SRM 51-40-02. 2 EA TRIMOUT ON FRAME MEASURE: NR 1: 1.130"X 1.035"X 0.5"R, NR 2: 1.080"X 1.035" X 0.5 "R. REPAIR IS PERMANENT CAT "B", ZONE 1 WITH THRESHOLD INSPECTION TO START AT OR BEFORE 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION. ACFT IS CURRENTLY AT 17053, F/C REF SRM 53-00-07, REPAIR 5, FIG 201, TABLE II, PAGE 210. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: FRAME — DENTED (BS 1540) · airframe 29,224 hrs · 17,053 cycles
AFT CARGO, BS 1540, STR 25L TOP OF FRAME HAS DENT. FRAME AT BS 1540, STR 25L HAS A DENTS ON TOP OF FRAME, LWR DENT MEASURES .95" W X 1.23" L , UPPER DENT MEASURES .76" W X 1.0" L BOTH DENTS ARE OUT OF LIMITS REF SRM 53-00-07, PG 101. ALLOWABLE DAMAGE 1, FIG 101. PERFORMED FRAME REPAIR AT BS 1540, STR 24L TO STR 26L, SRM 53-00-07, REPAIR 5, DETAIL III, FIG 201. 2 EA TRIMOUT ON FRAME MEASURE: NR 1: 1.30" X 0.95" X 0.5"R, NR2: 1.05" X 0.95"X 0.5"R. REPAIR IS PERMANENT CAT "B" WITH THRESHOLD INSPECTION TO START AT OR BEFORE 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED VISUAL INSPECTION. ACFT IS CURRENTLY AT 17053 F/C REF SRM 53-00-07, REPAIR 5, FIG 201, TABLE II, PAGE 201.
Part: FRAME — DENTED (BS 660) · airframe 29,224 hrs · 17,053 cycles
TWO DENTS ON FWD CARGO RT FRAME UPPER FLANGE AT BS 660 BETWEEN STRINGERS 22-25R. TRIMMED OUT DAMAGE IAW SRM. INSTALLED PERMANENT REPAIR IAW SRM.
Part: SUPPORT ANGLE — CORRODED · airframe 29,224 hrs · 17,053 cycles
CORROSION ON FWD CARGO DOOR LOWER SECTION OF FRAME SUPPORT ANGLE, 2ND FROM FWD END. R & R SUPPORT ANGLE AT FWD CARGO DOOR LOWER SECTION OF FRAME IAW DWG 143N6603 AND SRM 51-40-02, ORIGINAL MATERIAL .094", MATERIAL LOSS IS 1" X 1"X.022" FOUND OUT OF LIMITS REF SRM 52-30-02, ALLOWABLE DAMAGE 1, FIG 101 & DWG DAL 1505-100424.
Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN FLOORBEAM UPPER SURFACE AT BS 1640, RBL 46 - 58. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. AREA REPAIRED SRM.
Part: FRAME — DENTED (BS 1500) · airframe 29,224 hrs · 17,053 cycles
AFT CARGO BS 1500 BETWEEN STR 23-27L FRAME HAS DENTS. PERFORMED FRAME REPAIR AT BS 1500 STR 23L TO 27L REF SRM.
Part: FRAME — DENTED (BS 1400) · airframe 29,224 hrs · 17,053 cycles
DENT ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1400, BETWEEN STR 23L, 25L AND 26L. DENTS ON FRAME AT BS 1400 BETWEEN STR 23L, 25L AND 26L FOUND OUT OF LIMITS REF SRM. PERFORMED FRAME REPAIR BS 1400, STR 23L, 25L AND 26L REF SRM.
Part: SKIN — CORRODED (BS 1464-1477) · airframe 29,224 hrs · 17,053 cycles
FUSELAGE EXTERIOR SKIN STA 1464.5-1477.5, RBL 1.5-5, ANTENNA MOUNT LOCATION PITTED AND HAS TOOLING MARKS. BLENDED OUT CORROSION AND TOOLING MARKS ON FUSELAGE EXTERIOR SKIN AND ANTENNA MOUNT AT BS 1464.5-1477.5, RBL 1.5-5 IAW SRM 53-00-01, FIG 101 ORIGINAL MATERIAL THICKNESS .090" IAW DWG 146N3531 UT THICKNESS INSP IAW NDTM PT4, 51-00-10 .058" BETWEEN 1464-1477 BETWEEN S 30R, S29R L 13.3" X W=3.3" D= .032" MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-01, DAMAGE 1. ALL REPAIRS COMPLETED IAW ER/A 539842-14, REV ORIGINAL AS PERMANENT REPAIR.
Part: FRAME — GOUGED (BS 1280) · airframe 29,224 hrs · 17,053 cycles
FUSELAGE BS 1280 STR 11R-14R, FRAME GOUGED IN 2 PLACES. BLENDED 2 EA GOUGES ON FRAME BS 1280/STR 11R-14R IAW SRM 53-00-07, FIG 101, DETAIL II. MECHANICAL MEASUREMENTS OF BLENDED AREAS, AT FRAME BS 1280, STR 14R, NR 1: L=1.55" X W=0.4" X D=.023"; BELOW STR 11R, NR 2: L=1.0" X W=0.25" X D=.005", DEPTH GAUGE 08-746, CAL DUE: 01-22-16. ORIGINAL THICKNESS .071" IAW SRM 53-60-07, FIG 1 AND DWG BAC 1517-2159. MATERIAL LOSS IS OUT OF LIMITS IAW SRM 53-00-07, ALLOWABLE DAMAGE 1, FIG 101. NO FASTENERS REMOVED AT REWORKED AREAS. NO CRACKS NOTED AT BLENDED AREAS IAW NDTM PT 6, 51-00-19. PERFORMED DVI, ENSURED NO FURTHER DAMAGE AT UNDERLYING STRUCTURE. APPLIED ALODINE AND 2 COATS BMS10.11, TYPE 1 PRIMER. COMPLIED WITH PRI 541033-14, REV 0, ER/A 541033-14, REV ORIG FOR PERMANENT REPAIR.
Part: SKIN — DENTED (BS 666) · airframe 29,224 hrs · 17,053 cycles
3 EA PROTRUDING DENTS ON LOWER FUSELAGE SKIN AT APPROXIMATELY BS 666, 1 EA ABOVE S27R AND 2 EA BELOW S27R 3 EA PROTRUDING DENTS ON LOWER FUSELAGE SKIN AT BS 666, 1 EA ABOVE 27R AND 2 BELOW 27R HAVE BEEN REPAIRED BY COMPLYING WITH PRI 539825-14, REV 0 AND ER/A 539825-14, REV A PERMANENT REPAIR. INSTALLED DENT DECAL IAW PS 900-5-1 NR 04. ESTABLISHED DENT DECAL MONITOR REF 30-10-70, TOPP PAGE 13. ASSOCIATED ER/A 14-539825 ADDED FOR AC 6821.
Part: DECK PLATE — CORRODED (BS 1680-1691) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN DECK PLATE AT BS 1680 BL-0 TO RBL=54 AND AT BS 1691 RBL-51. REMOVED CORROSION ON MAIN CABIN DECK PLATE AT BS 1680, BL-0 TO RBL 54 AND BS 1691, RBL-51. REPAIR AREA REF PRI 541027-14, REV 0, ER/A 541027-14, REV A. ACCOMPLISHED PERMANENT REPAIR REF ER/A 541027-14, REV A.
Part: CREASE BEAM — CORRODED (BS 1236-1290) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN RT CREASE BEAM INNER CHORD, BS 1236 TO BS 1290. CORROSION ON MAIN CABIN RT CREASE BEAM INNER CHORD, BS 1236 TO BS 1290 FOUND OUT OF LIMITS IAW SRM 53-60-13. R & R CREASE BEAM ON MAIN CABIN RT BS 1180 TO BS 1290 IAW SRM 51-40-02 AND DWG 146N 5590.
Part: FRAME — DENTED (BS 1420) · airframe 29,224 hrs · 17,053 cycles
DENT ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1420, BETWEEN STRINGER 25L AND 26L. REPAIRED FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1420 BETWEEN STRINGERS 25L AND 26L IAW SRM 53-00-07, FIG 201, PAGE 201. ORIGINAL MATERIAL 7075-T6 .063", REPAIR AREA IS 12" X 2" X .071". TRIMOUT: 1.5" X 1.0" X 0.5" R . REPAIR IS PERMANENT CAT "B" IN ZONE 2 WITH THRESHOLD INSPECTION TO START AT OR BEFORE 42053, F/C & REPEAT INSPECTION EVERY 11000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION . ACFT IS CURRENTLY AT 17053 F/C REF SRM 53-00-07, REPAIR 5, FIG 201, TABLE II, PAGE 210.
Part: FRAME — DENTED (BS 600) · airframe 29,224 hrs · 17,053 cycles
2 EA DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 600 BETWEEN STR 23L-25L. REPAIRED FWD CARGO LT FRAME UPPER FLANGE AT BS 600 BETWEEN STR 23L AND STR 25L IAW DWG 143N1009 AND SRM 53-00-07, FIG 201, PAGE 201. TRIMOUTS, 2 EA, MEASURE NR 1: 1.54" X 0.94" X 0.5"R, NR 2: 1.49" X 0.94" X 0.5"R. REPAIR IS PERMANENT CAT "B" ON ZONE 2 WITH THRESHOLD INSPECTION TO START AT OR BEFORE 42053 F/C & REPEAT INSPECTION EVERY 11000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION . ACFT IS CURRENTLY AT 17053, FC REF SRM 53-00-07, FIG 201, REPAIR 5, TABLE II, PAGE 210.
Part: SEAT TRACK — CORRODED (BS 1276-1320) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON SEAT TRACK, BS 1276 - 1320, RBL 45.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, PAGE 102, FIG 101. R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 3, FIGURE 201.
Part: FRAME — DENTED (BS 740) · airframe 29,224 hrs · 17,053 cycles
DENT ON FWD CARGO LT FRAME UPPER FLANGE AT BS 740 ABOVE STR 23L. PERFORMED REPAIR TO FRAME AT BS 740 AND STR 23L. REF SRM 53-00-07, FIG 201, REPAIR 5. TRIMOUT OF DENT MEASURE 1.64" X 0.94" X 0.5"R. REPAIR IS PERMANENT CAT "B" WITH THRESHOLD INSPECTION TO START AT OR BEFORE 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION . ACFT IS CURRENTLY AT 17053, F/C REF SRM 53-00-07, FIG 201, REPAIR 5, TABLE II, PAGE 210.
Part: FRAME — DENTED (BS 680) · airframe 29,224 hrs · 17,053 cycles
DENT ON FWD CARGO FRAME UPPER FLANGE AT BS 680 BETWEEN STR 24-25R. REMOVED DAMAGE FABRICATED REPAIR AND INSTALLED IAW SRM.
Part: FRAME — DENTED (BS 680) · airframe 29,224 hrs · 17,053 cycles
THREE DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 680 BETWEEN STR 23L-25L. FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED FRAME IAW SRM.
Part: SEAT TRACK — CORRODED (BS 1280-1320) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN SEAT TRACK, BS 1280 TO 1320, LBL 24.7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA OF SEAT TRACK AND REPAIRED IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 720-740) · airframe 29,224 hrs · 17,053 cycles
FWD CARGO BS 720-740 LBL 7.5, INTERCOSTAL LOWER FLANGE AT BELLY SKIN CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL IAW DWG.
Part: SEAT TRACK — CORRODED (BS 1320-1327) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN SEAT TRACK, BS 1327 TO 1320, LBL 45.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED DAMAGED SEAT TRACK AND REPLACED SEAT TRACK AND INSTALLED SPLICE CHANNEL IAW SRM.
Part: SEAT TRACK — CORRODED (BS 1280-1320) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN SEAT TRACK, BS 1280 - 1320, LBL 45.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK AND INSTALLED SPLICE IAW SRM.
Part: SEAT TRACK — CORRODED (BS 1320-1350) · airframe 29,224 hrs · 17,053 cycles
CORROSION ON MAIN CABIN SEAT TRACK, BS 1350 TO 1320, LBL 24.7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AREA OF SEAT TRACK AND SPLICED REPAIR IAW SRM.
Part: SEAT TRACK — CORRODED (BS 365-400) · airframe 29,224 hrs · 17,053 cycles
SEAT TRACK BS 365-400 RBL 25, CORROSION IN SEVERAL SPOTS. FOUND CORROSION DAMAGE ON SEAT TRACK SUPPORT BS 365-400, RBL 25 TO BE OUT OF ALLOWABLE LIMITS. R & R SEAT TRACK SUPPORT. ORIGINAL MATERIAL THICKNESS IS .070 MAX MATERIAL LOSS IS 2" X 1" X .022". MAXIMUM ALLOWABLE MATERIAL LOSS IS 10 PERCENT. REF SRM 51-10-02 PAR 14 & 15 SRM 53-00-52 ALLOWABLE DAMAGE I, SRM 51-40-02, PG 6, 7, 30-31 SRM 51-40-05, PG 2 AND DWG 141N5130.
Part: FLOOR SUPPORT — CORRODED (BS 704-736) · airframe 29,224 hrs · 17,053 cycles
CABIN FLOOR STRUCTURE BS 704-714 AND 729-736/RBL 65, CUSP BEAM CORRODED. R & R INNER CUSP CHORD THAT WAS CORRODED BEYOND LIMITS IAW DWG 143N8328 AND SRM 51-40-02 (100 PERCENT MATERIAL LOSS X 2" X 1".
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
RT INBD MAIN FLAP AFT OF NR 6 FLAP TRACK, FLAP LWR T/E WEDGE SKIN HAS DENTS. ACCOMPLSHED REPAIR OF THE DISCREPANT DENTS ON RT INBD MAIN FLAP AFT OF NR 6 FLAP LOWER T/E WEDGE SKIN IAW SRM 51-70-10, PN 113N2603.
Part: CLEVIS — CORRODED (NR 8 SLAT) · airframe 29,224 hrs · 17,053 cycles
RIGHT WING NR 8 SLAT INBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-17. R & R HARDWARE AT RT WING NR 8 SLAT INBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-13-024-006, AMM 27-81-13-424-008 AND AMM 27-81-02-424-021.
Part: CLEVIS — CORRODED (NR 3 SLAT) · airframe 29,224 hrs · 17,053 cycles
LEFT WING NR 3 SLAT OTBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-07. R & R HARDWARE AT NR 3 SLAT OTBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-13-024-006, AND AMM 27-81-13-424-008 AND AMM 27-81-12-424-021.
Part: TRACK — CORRODED (NR 4 SLAT) · airframe 29,224 hrs · 17,053 cycles
LEFT WING NR 4 SLAT OTBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-08. R & R HARDWARE AT LT WING NR 4 SLAT OTBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-02-424-021 AND AMM 27-81-13-024-006.
Part: STRUT — CORRODED (NLG) · airframe 29,224 hrs · 17,053 cycles
AFTER INSPECTION OF NLG DRAG STRUT IAW T/C 2020-2435, STEP 7, REF N/R 700-27, FOUND CORROSION AT LWR BEARING AREA ISSUE OF CARD 3221-4999 REQUIRED. R & R NLG LWR DRAG STRUT IAW 3221-4999.
Part: SKIN — DENTED (NR 2 SLAT) · airframe 29,224 hrs · 17,053 cycles
WHILE PERFORMING INSPECTION , FOUND A DENT ON LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE. REPAIRED IAW SRM 51- 70-10, REPAIR 2.
Part: SKIN — BENT (LT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
LT INBD FLAP T/E AFT OF NR 3 FLAP TRACK T/E SKIN IS BENT, LWR SKIN IS BUCKLED/SCRATCHED AND SIDE HAS CRACKS. ACCOMPLISHED REPAIR OF THE 3 EA DISCREPANT AREAS ON L/E INBD MAINFLAP T/E WEDGE LOWER SKIN IAW SRM 51-70-10. DAMAGE DIMENSIONS ARE 14" X 10.5", .8750" CIRCLE AND A 1" CIRCLE. PN 113N2603.
Part: SKIN — DENTED (LT WING SLAT NR2) · airframe 29,224 hrs · 17,053 cycles
LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE 33" FROM INBD EDGE, 1.5" FWD OF AFT EDGE, SKIN HAS DENT. FOUND AND MEASURED 1 EA DENT ON LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE 33" FROM INBD EDGE 1.5" FWD OF AFT EDGE, MEASURED 1 EA DENT A=1.130, WIDE Y=.014, DEPTH A/Y=80. 1 EA DENT FOUND WITHIN LIMIT IAW SRM 57-43-02 ALLOWABLE DAMAGE FOR DENT DETAIL III, FIGURE 101, PAGE 104-105, NOTE J. PERFORMED TAP TEST NO DELAMINATION NOTED IAW NDTM PART 1, 51-05-01, I PARA 5, PN 114N4003-221, SN 000072. INSTALLED ID TAG IAW PS 900-5-1 NR 04.
Part: SKIN — DENTED (LT WING SLAT 3) · airframe 29,224 hrs · 17,053 cycles
LT WING NR 3 SLAT T/E WEDGE UPPER SURFACE 8" FROM OTBD EDGE, 8.5" FWD OF AFT EDGE, SKIN HAS DENT. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 3 SLAT T/E WEDGE UPPER SURFACE 8" FROM OTBD EDGE 8.5" FWD OF AFT EDGE IAW SRM 51-70-10, PN 114N4004-215, SN 000071. INSTALLED ID TAG IAW PS 900-5-1, NR 04. DENT TRIMOUT: 1.0" DIA.
Part: SKIN — DENTED (LT WING SLAT 4) · airframe 29,224 hrs · 17,053 cycles
LEFT WING NR 4 SLAT T/E WEDGE UPPER SURFACE 9" FROM INBD EDGE , 4" FWD OF AFT EDGE, SKIN HAS DENT. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 4 SLAT T/E WEDGE UPPER SURFACE 9" FROM INBD EDGE, 4" FWD OF AFT EDGE IAW SRM 51-70-10, PN 114N4005-229, SN 000071, TRIMOUT DIA: 2" DIAMETER. INSTALLED ID TAG IAW PS 900-5-1, NR 04.
Part: JACKSCREW — CORRODED (RT WING TE FLAPS) · airframe 29,224 hrs · 17,053 cycles
RIGHT WING NR 7 FLAP JACKSCREW HAS PITTING CORROSION. REMOVED RT WING T/E OTBD FLAP INBD BALLSCREW NR 7 IAW CARD 2751-2542. PROCURED AND INSTALLED NR 7, RT OTBD FLAP INBD BALLSCREW ON CARD 2751-2542, INSTALLED PN 7829996, SN 5112, OPS CHECK TO BE COMPLIED ON CARD 2751-2542.
Part: JACKSCREW — CORRODED (RT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
RT WING NR 8 FLAP JACKSCREW HAS PITTING CORROSION. REMOVED NR 8 RT WING T/E OTBD FLAP OTBD BALLSCREW IAW CARD 2751-2542. PROCURED AND INSTALLED SERVICEABLE NR 8 RT T/E OTBD FLAP OTBD BALLSCREW.
Part: BALL SCREW — CORRODED (LT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
LT WING FLAP TRACK NR 3 BALLSCREW HAS CORROSION FORMING ON THE BALL NUT 008-41. REMOVED NR 3 LT T/E INBD FLAP OTBD BALLSCREW IAW CARD 2751-2538. PROCURED AND INSTALLED SERVICEABLE NR 3 LT T/E INBD FLAP OTBD BALLSCREW ON CARD 2751-2538.
Part: BALLSCREW — CORRODED (RT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
RT WING NR 5 BALLSCREW HAS PITTING CORROSION. REMOVED RT WING T/E INBD FLAP INBD BALLSCREW IAW CARD 2751-2542. PROCURED AND INSTALLED SERVICEABLE NR 5 RT INBD FLAP INBD BALLSCREW ON CARD 2751-2542. OPS CHECK TO BE COMPLIED ON CARD 2751-2542.
Part: BALL SCREW — DAMAGED (RT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
RT WING NR 6 FLAP BALLSCREW DAMAGED AND GIMBLE HAD PITTING CORROSION. REMOVED NR 6 RT T/E INBD FLAP OTBD BALLSCREW IAW CARD 2751-2542. PROCURED AND INSTALLED SERVICEABLE NR 6 RT INBD FLAP OTBD BALLSCREW. OPS CHECK TO BE COMPLIED ON CARD 2751-2542.
Part: BALLSCREW — CORRODED (LT WING TE FLAP) · airframe 29,224 hrs · 17,053 cycles
LT WING FLAP TRACK BALLSCREW PITTING CORROSION FOUND ON BALL NUT ID AND OD 008-38. REMOVED NR 4 LT WING T/E INBD FLAP INBD BALLSCREW IAW CARD 2751-2538.