N346BC
Registered owner: NUWAY AG LLC, OH (owner ≠ operator)
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.
55 reports on file, 2015-07-16 – 2015-12-31.
Part: WEDGE — DAMAGED (RT WING TE FLAP) · airframe 29,785 hrs · 16,474 cycles
REPAIR INBD RT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA, APPROXIMATELY 15.5" X 10.5", ON RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.
Part: WEDGE — DAMAGED (LT WING TE FLAP) · airframe 29,785 hrs · 16,474 cycles
INBD LT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. REPAIRED IAW SRM 51-70-10.
Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 29,785 hrs · 16,474 cycles
LEFT INBD MAIN FLAP UPPER PANEL FROM MF BS 74.0 TO MF BS 209 FOUND DAMAGE CORE FROM INBD TO OTBD END AND FWD TO AFT SIDES AND ONE HOLE IN CORE. REPAIRED IAW SRM 51-70-10 AND ER/A 538384-14 ORIGINAL REVISION.
Part: FLOORBEAM — CORRODED (BS 1681) · airframe 29,785 hrs · 16,474 cycles
CP53-251-01-MAIN CABIN, CORROSION ON FRAME UNDER NUTPLATES BS 1681 AND BETWEEN RBL 57-LBL 57. REMOVED CORROSION UNDER NUTPLATES ON MAIN CABIN FRAME, FLOOR BEAM, UPPER CHORD AT BS 1681 BETWEEN RBL57-LBL57, REF SRM 53-00-51, FIG 101, DET III AND ACCOMPLISHED PERMANENT REPAIR ON DISTURBED FITTING, PN 140N2047-5 ATTACHED TO FLOORBEAM AT BS 1681, LBL 9.0, REF ER/A 538387-14, REV ORIGINAL.
Part: SEAT TRACK — CORRODED (BS 680-740) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN FLOOR STRUCTURE, SEAT TRACK FLANGE, BS 680 TO BS 740, RBL 45.5. REMOVED CORROSION ON MAIN CABIN FLOOR STRUCTURE SEAT TRACK FLANGE BS TO BS 740, RBL 45.5. BLENDOUT MEASURE 60" X 2" X 0.059" MIN MATERIAL REMAINING. ORIGINAL THICKNESS TO BE .070". SEAT TRACK FLANGE REWORK AREA FOUND OUT OF LIMITS REF SRM 53-00-52, FIG 101 DET VIII. ACCOMPLISHED PERMANENT REPAIR BY REPLACING SEAT TRACK SUPPORT SECTION FROM BS 640 TO BS 740, RBL 45.5, REF SRM 51-40-02, PAGE 7, DWG 143N5080 & ER/ A538374-14, REV ORIGINAL.
Part: SEAT TRACK — CORRODED (BS 641) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN FLOOR SEAT TRACK FLANGE/AROUND FASTENER HOLES AT BS 641, LBL 45.5. ACCOMPLISHED PERMANENT REPAIR ON SEAT TRACK FLANGE, AROUND FASTENER HOLES AT BS 640-780, LBL 45 REF ER/A 538367-14, REV ORIGINAL.
Part: SHUTOFF VALVE — CORRODED (APU BLEED) · airframe 29,785 hrs · 16,474 cycles
APU BLEED AIR SHUTOFF VALVE HAS SURFACE CORROSION VIEWED THRU ACCESS DOOR 313AL RLO14. R & R APU BLEED SHUTOFF VALVE IAW AMM 36-11 -10-401. LEAK AND OPS CHECK DUE. PERFORMED OPS AND LEAK CHECK OF APU BLEED SHUT OFF VALVE, OPS AND LEAK CHECK GOOD IN REF TO AMM 63-11-10-404-013.
Part: SUPPORT — CORRODED (BS 900 BULKHEAD) · airframe 29,785 hrs · 16,474 cycles
FWD CARGO BS 900 BULKHEAD VERTICAL SUPPORT AT RBL-7.5 HAS CORROSION AT BOTTOM. UPON EVALUATION, FOUND BULKHEAD VERTICAL SUPPORT BS 900, RBL 7.5 TO HAVE AN EXFOLIATION CORROSION MEASURING 3" X 1" X .060" MATERIAL LOSS, ORIGINAL MATERIAL TO BE 0.220". FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-40-08, FIG 101 ALLOWABLE DAMAGE 1. REMOVED , LOCALLY FABRICATED & REPLACED BULKHEAD VERTICAL SUPPORT IAW SRM 51-40-02 PARA 4B & DWG 111N2001.
Part: FRAME — CORRODED (CARGO DOOR) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO DOOR AFT LOWER FRAME. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO DOOR AFT LOWER FRAME IAW ER/A 538385-14, REV ORIGINAL.
Part: FRAME — CORRODED (CARGO DOOR) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON FWD CARGO DOOR AFT LOWER FRAME. REPAIRED IAW ERA 538381-14, REV ORIGINAL.
Part: KEELBEAM — CORRODED (BS 1100-1120) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON LOWER KEEL STRUCTURE TEE FITTING ABOVE LT MLG DOOR AT BS 1100 - 1120, LBL7. FOUND OUT OF LIMITS IAW SRM 53-00-71, FIG 101, DETAIL VII. REMOVED, FABRICATED & REPLACED KEEL IAW DWG 144N8180 & SRM 51-40-02, PG 10.
Part: SEAT TRACK — CORRODED (BS 640) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON SEAT TRACK FLANGE AROUND FASTENER HOLE, BS 640, RBL 45. BLENDED CORROSION ON SEAT TRACK FLANGE & ACCOMPLISHED PERMANENT REPAIR IAW ER/A 538371-14, REV ORIGINAL.
Part: SKIN — DENTED (BS 460) · airframe 29,785 hrs · 16,474 cycles
DURING INSPECTION OF DENT ON N/R 100-3 FOUND DENT AT EXT FUSELAGE 1" FWD OF BS 460 BELOW LAP AT STR 26R. MECHANICALLY MEASURED DENT ON FUS SKIN FWD OF BS 460 BELOW LAP AT STR 26R TO BE 2.2"X 1" X.002" DEEP, A/Y=500. ACCOMPLISHED PERMANENT REPAIR OF DENT IAW ER/A 538368-14, REV ORIGINAL. INSTALLED ID TAG PER PS 900-5-1, NR 04. ESTABLISHED DENT DECAL MONITOR IAW TOPP 30-10-70, PAGE 13. ASSOCIATED ER/A 14-538368 ADDED FOR AC 6819.
Part: FRAME — DENTED (BS 1340) · airframe 29,785 hrs · 16,474 cycles
TWO DENTS ON AFT CARGO FRAME AT BS 1340 BETWEEN STRINGERS 25-26L. REPAIRED IAW SRM 53-00-07, REPAIR 5.
Part: GATE — CORRODED (R1 DOOR) · airframe 29,785 hrs · 16,474 cycles
R1 DOOR LOWER GATE LOWER EDGE CORRODED. REMOVED CORROSION IAW SRM 52-10-02, FIG 101 100 PERCENT EXFOLIATED FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL XII ALLOWABLE DAMAGE 1, PAGE 107. R & R R-1 DOOR LOWER GATE IAW AMM 52-11-38-404-009, OPS CHECK GOOD.
Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 29,785 hrs · 16,474 cycles
FWD CARGO DOOR SILL LOWER REPAIR ANGLE HAS CORROSION BETWEEN BS 580 - 600. FOUND THE REPAIR TO BE 100 PERCENT CORRODED. REMOVED, FABRICATED & INSTALLED REPLACEMENT TEE ANGLE IAW SRM 51-40-02, PARA 7D & DWG 143N8522.
Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 377, BETWEEN BL 0 AND LBL 24, FOUND TO BE OUT OF LIMITS. TRIMMED-OUT THE SECTION ON MAIN CABIN FLOORBEAM LBL 32.5 - RBL 36 IAW SRM 53-00-51, REP 10. INSTALLED & ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-51, REPAIR 10, PAGE 202, PAR 4 & DWG 141N5166, REV A.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, RBL 7.55. ACCOMPLISHED ERA 332525-14MA, REV E.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, RBL 2.9. REMOVED CORROSION IAW SRM 53-00-51, REPAIRED IAW ER/A 332525-14MA, REV E.
Part: DECK PLATE — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
MAIN CABIN-CORROSION ON LT SIDE OF DECK PLATE BETWEEN BS 1681-1720 AND BETWEEN BL 0-LBL 57. REMOVED CORROSION ON MAIN CABIN DECK PLATE BS 1681 TO BS 1720, BL-0-LBL57 IAW SRM 53-00-51, FIG 101. ORIG MAT THICKNESS .071 IAW DW 141N5313. MAT LOSS .013 BS 1681 LBL-24-LBL-26. FOUND OUT OF LIMITS IAW- SRM 53-0051, FIG 101. ACOMPLISHD PERMANENT REPAIR IAW SRM 53-00-51, REPAIR 2, FIG 201, L=2.0, W=1.5, D=.013.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUPLATES AT BS 1510, LBL 7.55. ACCOMPLISHED ER/A 332525-14MA, REV E.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 3 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, LBL 2.9. ACCOMPLISHED ERA 332525-14MA, REV E DUE TO 100 PERCENT MATERIAL LOSS AT THIS LOCATION. REPAIRED IAW PS 900-5-1, NR 4 AND IAW TOPP 30-10-70, PG 13.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, LBL-12. REMOVED NUT PLATES FOR ACCESS REMOVED CORROSION IAW SRM 51-40-02. REMOVED CORROSION FROM BS 1510 LBL. 12 IAW SRM 53-00-51, FOUND MATERIAL LOSS 1" X 3" X 100 PERCENT. CUT OUT DAMAGE AND FABRICATED REPAIR WITH SHT 7075-T6-.080 BATCH 0002461636 " EXTRUDED" IAW ER/A 332525-14MA, REV E, LOCATED & DRILLED HOLES TREATED AND PRIMED AND INSTALLED FROM BS 1510, LBL-12 IAW ER/A 332525-14MA, REV E ASSOCIATED ER/A 14-332525, ADDED FOR AC 6819.
Part: SEAT TRACK — CORRODED (BS 365) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN SEAT TRACK FLANGE FWD END, BS 365, RBL 45.5. ORIGINAL MAT. THICKNESS: .070", MAT LOSS: 3"X 1"X .021". FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE I, DET VIII. REMOVED, FABRICATED & INSTALLED SEAT TRACK SUPPORT REPLACEMENT SECTION FROM BS 365 TO BS 418, RBL 45.5 IAW SRM 51-40-02 & DWG 141N5131-4.
Part: FRAME — DENTED (BS 1340) · airframe 29,785 hrs · 16,474 cycles
AFT CARGO FRAME BS 1340 STR 25R FOUND DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. TRIMED DAMAGE OUT OF FRAME INBD FLANGE AFT CARGO FRAME IAW SRM 53-00-07, REPAIR 5, FIG 201. FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-00-07, R5, FIG 201.
Part: DECK PLATE — CORRODED (BS 1681-1720) · airframe 29,785 hrs · 16,474 cycles
CORROSION FOUND ON RT SIDE OF DECK PLATE BETWEEN BS 1681 - 1720 AND BETWEEN BL 0 & RBL 57. REMOVED CORROSION IN AREA AND FOUND AREAS TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. 1 DETAIL III. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 FIG 201, REPAIR 2, PG 201.
Part: SEAT TRACK — CORRODED (BS 365) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN SEAT TRACK FLANGE FWD END, BS 365, RBL 24.7. REMOVED CORROSION ON MAIN CABIN SEAT TRACK SUPPORT AT BS RBL 24.5, L=1.4", W=.9", D=.012" ORIGINAL THICKNESS .070" FOUND OUT OF LIMITS IAW SRM 53-00-52. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-52, FIG 1 AND SRM 51-40-02 AND DWG 141N 5130.
Part: STRAP — CRACKED (BS 365-377) · airframe 29,785 hrs · 16,474 cycles
FLOOR SUPPORT STABILIZATION STRAP BS 365.25 - 377.7 LBL 24 CRACKED IN THREE PLACES AND BETWEEN TWO PREVIOUS REPAIR DOUBLERS. R & R DAMAGED SECTION OF STABILIZATION STRAP IAW SRM 51-40-02, PARA 4E, PARA 7D & DWG 141N5150.
Part: FRAME — DENTED (BS 1440) · airframe 29,785 hrs · 16,474 cycles
THREE DENTS ON AFT CARGO LT FRAME AT BS 1440 BETWEEN STRINGERS 25-26L. CUT OUT DENTS, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-00-07-R5, FIG 201.
Part: INTERCOSTAL — CORRODED (BS 1380) · airframe 29,785 hrs · 16,474 cycles
CORROSION FOUND ON AFT CARGO INTERCOSTALT BS 1380, RBL 26. REMOVED CORROSION IAW SRM 51-10-02 AND 53-00-04 ALLOWABLE DAMAGE 1. FOUND OUT OF LIMITS IAW SRM 53-00-53. R & R THE INTERCOSTAL IAW SRM 51-40-02 & DWG 146N5390.
Part: STRINGER — CORRODED (BS 1620) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON STR 30 END FITTING IN AFT CARGO BS 1620. REMOVED CORROSION IAW SRM 53-00-03. FOUND OUT OF LIMITS IAW SRM 53-00-03. R & R THE STRINGER END FITTING IAW SRM 51-40-02, PAR 4 AND 7, DWG 146N3800, REV BV AND SRM 51-40-03, PAR 4.
Part: FRAME — DENTED (BS 780) · airframe 29,785 hrs · 16,474 cycles
DENT ON FWD CARGO LT FRAME AT BS 780 JUST ABOVE STR 24L. DENT ON FWD CARGO LT FRAME AT BS 780, STR 24L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. TRIMMED OUT DENT L= 1", W=1"X 0.5" R IAW FIG 201, DETAIL III, REPAIR 5. FORMED J-SECTION REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5, PG 201. INSTALLED J-SECTION REPAIR AT LT BS 780, ABOVE STR 24L IAW SRM 51-40-02, PG 6-7 AND SRM 53-00-07, REPAIR 5. REPAIR IS PERMANENT CAT"B" WITH THRESHOLD INSPECTION TO START AT 50000, F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED INSPECTION. ACFT IS CURRENTLY AT 16474, F/C REF SRM 53-00-07, FIG 201 REPAIR 5, TABLE II.
Part: FRAME — DENTED (BS 600) · airframe 29,785 hrs · 16,474 cycles
THREE DENTS ON FWD CARGO FRAME BS 600 STRINGERS 24-25L. TRIMMED OUT THE DENTS IAW SRM 53-00-07, REP 5. ACCOMPLISHED PERMANENT CAT "B" REPAIR IAW SRM 53-00-07, REPAIR 5.
Part: FRAME — DENTED (BS 800) · airframe 29,785 hrs · 16,474 cycles
TWO DENTS ON FWD CARGO LT FRAME AT BS 800 BETWEEN STRINGERS 23 - 25L. TRIMED OUT DENTS, ACCOMPLISHED PERMANENT MAJOR REPAIR IAW SRM.
Part: FLOORBEAM — CORRODED (BS 365) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 365, BL 0 TO RBL 62. ACCOMPLISHED PERMANENT CAT"A" MAJOR REPAIR IAW SRM.
Part: FLOORBEAM — CORRODED (BS 377) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 377, BETWEEN BL 0 AND LBL 24. OUT OF LIMITS.
Part: CREASE BEAM — CORRODED (BS 438) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON LEFT CREASE BEAM BS 438. REMOVED SECTION OF CREASE BEAM BETWEEN BS 430 - 450 IAW SRM 51-40-02, PG 7. FABRICATED, LOCATED AND DRILLED THE NEW SECTION OF THE CREASE BEAM IAW SRM 51-40-05, PG 3. , INSTALLED IAW SRM 51-40-02, PG 7, AND DWG 140N0504.
Part: SKIN — DENTED (BS 443) · airframe 29,785 hrs · 16,474 cycles
BS 443 BELOW STRINGER 25R, FUSELAGE SKIN HAS APPROXIMATELY A ONE INCH DENT. REPAIRED IAW ER/A 536965-14, REV ORIGINAL.
Part: INTERCOSTAL — CORRODED (BS 1600-1620) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO INTERCOSTAL BETWEEN BS 1600-1620, LBL-2.9 AT BOTTOM ON OTBD SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, R & R INTERCOSTAL IAW DWG NR 146N3400, REV F AND SRM.
Part: INTERCOSTAL — CORRODED (BS 1413) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT CARGO INTERCOSTAL AT BS 1413, LBL 16 ON INBD SIDE OF WEB. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-04, FIG 101. DETAIL II. FABRICATED A NEW INTERCOSTAL IAW DWG 146N5517. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-40-02, PG 2-10.
Part: SEAT TRACK — CORRODED (BS 640) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON MAIN CABIN SEAT TRACK FLANGE, BS 640, LBL 24.7. REMOVED DAMAGED SEAT TRACK SECTION . FABRICATED A REPLACEMENT SEAT TRACK SECTION AND FABRICATED CHANNEL IAW SRM 53-00-52, REPAIR 3, OPTION 2, PG 201-206. INSTALLED THE SEAT TRACK SECTION AND CHANNEL IAW SRM 53-00-52, REPAIR 3, OPTION 2, PG 201-206.
Part: TEE FITTING — CORRODED (BS 1120-1140) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON AFT ATTACH POINT OF LOWER KEEL STRUCTURE TEE FITTING AT BS 1120 - 1140, LBL 5.5. R & R THE TEE FITTING IAW SRM 51-40-02, PAR 9.
Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON UPPER CAP ON FRAME BS 1661, RBL 54. TRIMMED-OUT DAMAGED SECTION OF FLOORBEAM BETWEEN RBL 49 - 65 AND ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-51, REPAIR 8, FIG 201.
Part: CREASE BEAM — CORRODED (BS 1237) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION FOUND ON RT CREASE BEAM BS 1237, RBL 65. CUTOUT DAMAGED SECTION OF CREASE BEAM FROM BS 1230 - 1250, RT & ACCOMPLISHED A PERMANENT SPLICE REPAIR IAW SRM 53-00-13, REPAIR 1.
Part: FLOOR SUPPORT — CORRODED (BS 365-377) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON FLOOR SUPPORT BS 365 - 377, BL 0. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. R & R THE FLOOR SUPPORT IAW SRM 51-40-02, PG 6 AND PG 2 AND IAW DWG 141N5190.
Part: CREASE BEAM — CORRODED (BS 1600-1607) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON CREASE BEAM BS 1600 - 1607, LBL 62. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-13, 1 FIG 101, DETAIL III. R & R THE SECTION OF THE CREASE BEAM AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-13, REPAIR 1, FIG 201.
Part: FLOOR SUPPORT — CORRODED (BS 332-336) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON FLOOR SUPPORT, BS 332 - 336, RBL 3. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, AD1, FIG 101, DETAIL VI. R & R THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 7D, PAGE 7 & DWG 141N5160.
Part: FRAME — DENTED (BS 700) · airframe 29,785 hrs · 16,474 cycles
DENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R. TRIMMED-OUT DENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R AND ACCOMPLISHED A PERMANENT CAT"B" REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT MEASURE 9.040" X 1.080" X 0.5" RT THRESHOLD INSPECTION TO START AT OR BEFORE 41474 F/C & REPEAT INSPECTION EVERY 11000 F/C THEREAFTER. ACFT IS CURRENTLY AT 16474 F/C RER SRM 53-00-07, FIG 201, REPAIR 5, TABLE II, PAGE 210. METHOD OF INSPECTION: HFEC & DETAILED INSPECTION.
Part: FRAME — DENTED (BS 800) · airframe 29,785 hrs · 16,474 cycles
DENT ON FWD CARGO RT FRAME AT BS 800 ABOVE STR 23R. ACCOMPLISHED A PERMANENT CAT"B" REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT SIZE 1.08" X 0.94" X 0.5"R. THRESHOLD INSPECTION TO START AT BEFORE 50000 F/C & REPEAT INSPECTION EVERY 12000 F/C THEREAFTER USING HFEC & DETAILED INSP IAW SRM 53-00-07, REPAIR 5, FIG 201, TABLE II, PAGE 210.
Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 29,785 hrs · 16,474 cycles
LEFT WING INBD FLAP T/E WEDGE PANEL LOWER SURFACE IS DAMAGED, DENTED, PUNCTURED, AND CRACKED MF BS 223 TO MF BS 240. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON LT WING INBD FLAP T/E WEDGE IAW SRM 51-70-10, TRIMOUT DIMENSION: 17" X 9.5". COMPLIED WITH ALL STEPS ON JIC 2034-8210-01.
Part: BOX BEAM — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 29,785 hrs · 16,474 cycles
CORROSION ON BOXBEAM BETWEEN BS 1661 AND BS 1681, LBL 54. REMOVED AND INSTALLED NEW BOX BEAM IAW SRM 51-40-02, PARA 7D, PG 6&7, 51-40-02, 4B PG2, AND DWG 146N5230.
Part: STRUCTURE — CORRODED (BS 1640-1661) · airframe 29,785 hrs · 16,474 cycles
CORROSION ON BOXBEAM BETWEEN BS 1640 AND BS 1661, LBL 54. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R BOX BEAM IAW SRM.
Part: FRAME — DENTED (BS 700) · airframe 29,785 hrs · 16,474 cycles
TWO DENTS ON FWD CARGO FRAME AT BS 700, ABOVE STR 24L. TRIMMED OUT DENTS FOUND ON FRAME IAW SRM 53-00-07, FIG 201, REPAIR 5. INSTALLED AND ACCOMPLISHED A PERMANENT CAT "B" MAJOR REPAIR.
Part: FRAME — DENTED (BS 660) · airframe 29,785 hrs · 16,474 cycles
DENT ON FWD CARGO LT FRAME AT BS 660 FROM STR 24-25L. INSTALLED & ACCOMPLISHED A PERMANENT REPAIR CAT "B" IAW SRM 53-00-07, REPAIR 5, FIG 201, DETAIL III.
Part: SKIN — DENTED (TE FLAP) · airframe 29,785 hrs · 16,474 cycles
RIGHT INBD MAIN FLAP T/E WEDGE UPPER AND LOWER SKINS HAVE 15" X 11" AREA DENTED 62"-77" FROM OTBD END. ACCOMPLISHED PERMANENT REPAIR OF THE DISCREPANT AREA ON RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.