N762BC
Registered owner: STEELE RAYMOND M, PA (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.
58 reports on file, 2016-02-28 – 2016-04-29.
Part: INTERCOSTAL — CORRODED (BS 1280-1300) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO, RT INTERCOSTAL UPPER ANGLE BETWEEN BS 1280-1300 BELOW OTBD SIDE OF TRANSITION PANEL. R & R 1 EA INTERCOSTAL WEB AND 1EA UPPER ANGLE IAW SRM.
Part: SUPPORT — CORRODED (BS 900) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
LOWER WTB FAIRING SUPPORT FS 900/LBL 14-RBL 24; T EXTRUSION AND SPLICE ANGLES ON FWD AND AFT SIDES CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED PERMANENT EXTRUSION REPAIR REF SRM.
Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
LEFT BS 820-840 UPON REMOVEL OF TRANSITION PANEL. INTERCOSTAL HAS CORROSION ON LOWER FLANGE THAT ATTACHES TO SKIN. LOCATED BETWEEN LT STR 27 AND LT STR 28. FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL IAW SRM.
Part: SLIDE — DAMAGED (L1 DOOR) · airframe 28,319 hrs · 16,502 cycles
L1 DOOR SLIDE PACKBOARD FWD BLADE SLOT TORN AT INBD SIDE. ESCAPE SLIDE L-1 DOOR TO BE INSTALLED ON TASK-CARD.
Part: FLOOR SUPPORT — CORRODED (BS 1450) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION UNDER 1 EA NUTPLATE IN AFT CARGO UPPER FLOOR SUPPORT AT BS 1450 RBL-13. ACCOMPLISHED AFT CARGO UPPER FLOOR SUPPORT AT BS 1450, RBL 13 BY REPLACEMENT IAW SRM.
Part: TORQUE SHAFT — CORRODED (RUDDER PCU) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
VERTICAL STABILIZER, LT SYS RUDDER PCU BELLCRANK TORQUE SHAFT HAS SURFACE CORROSION. ASSY LT SYS RUDDER PCU AREA IAW AMM 20-11, SRM AND AMM 27-21 OPS CHECK GOOD IAW AMM 27 -21.
Part: FRAME — DENTED (BS 1360) · airframe 28,319 hrs · 16,502 cycles
DENT ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1360 ABOVE STR 26L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED REPAIR IAW SRM.
Part: FLOORBEAM — DAMAGED (BS 310) · airframe 28,319 hrs · 16,502 cycles
TOILET FLUSH LINE BRACKET RIVET HAS ELONGATED HOLE AND TOOLING DAMAGE ON MAIN CABIN FLOORBEAM WEB AT BS 310.5, LBL 53. ACCOMPLISHED PERMANENT REPAIR FOR TOOLING MARKS ON MAIN CABIN FLOORBEAM WEB AT BS 310.5, LBL 53, REF ER/A 544726-14, REV. ORIG. R & R TOILET FLUSH LINE BRACKET DUE TO HOLE ELONGATION REF SRM REF. THIS NON-ROUTINE, 100-397 FOR REPAIR ACCOMPLISHMENT REF LOGPAGE 2459601.
Part: SLIDE — DAMAGED (R2 DOOR) · airframe 28,319 hrs · 16,502 cycles
R2 DOOR ESCAPE SLIDE DAMAGED AT UPPER RT CORNER. PROCURED FROM STOCK R-2 DOOR ESCAPE SLIDE O/H TO BE INSTALLED ON TASK CARD.
Part: BEARING — CORRODED (RT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
RT WING OTBD, MAIN FLAP OTBD BALL SCREW GIMBAL UPPER PIVOT BEARING AND IMMEDIATE AREA SHOWING RUST. PROCURED PART. INSTALLATION AND OP'S CHECK ACCOMPLISHED ON T/C NR 2751-2542, FOR REPLACEMENT OF RT, OTBD, FLAP BALLSCREW.
Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE FLOOR SUPPORT LOWER FLANGE BETWEEN BS 1460-1480, RBL-13. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACEMENT IAW SRM.
Part: FRAME — DENTED (BS 1320) · airframe 28,319 hrs · 16,502 cycles
THREE DENTS ON AFT CARGO LT FRAME AT BS 1320 BETWEEN STR 25-26L. TRIMMED-OUT DENTS IAW SRM 53-00-07, FIG 201 REPAIR 5. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07 REPAIR 5 FIG 201.
Part: INTERCOSTAL — CORRODED (BS 1360-1380) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO INTERCOSTAL ON OTBD SIDE OF WEB, LOWER FLANGE AND UPPER ANGLE BETWEEN BS 1360-1380 BELOW OTBD SIDE OFTRANSITION PANEL ACP 0600-156-01Z. REMOVED CORROSION ON INTERCOSTAL AND 3 EA ANGLES FOUND TO BE EXFOLIATED OUT OF LIMITS IAW SRM 53-00-04, FIG 101 ALLOWABLE DAMAGE 1. R & R INTERCOSTAL AND 3 EA ANGLES AT BS 1360-BS 1380, RT IAW SRM 51-40-02, PARA 4 AND 7 DWG 146N5390-AND 146N3300 SHT 76, REV C.
Part: FRAME — GOUGED (BS 1280) · airframe 28,319 hrs · 16,502 cycles
MAIN CABIN RT SIDE BS 1280 FRAME HAS 2 EA GOUGE MARKS. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN RT SIDE BS 1280 FRAME STR 9R TO STR 14R IAW ER/A 544719-14AD REV ORIGINAL REF NRC 200-219 & THIS LOG FOR REPAIR ACCOMPLISHMENT, REF LOG PAGE 2451799.
Part: FRAME — DENTED (BS 680) · airframe 28,319 hrs · 16,502 cycles
FWD CARGO COMPARTMENT LT SIDE FRAME BS 680 HAS 2 EA DENTS BETWEEN STR 23L AND 25L. TRIMMED OUT AND ACCOMPLISHED PERMANENT REPAIR REF SRM.
Part: HINGE — CORRODED (MLG DOOR) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CASTING FOR MLG DOOR AFT HINGE HAS SEVERAL CORROSION PITS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R KEELBEAM SUPPORT CASTING REF DWG & SRM.
Part: FRAME — DENTED (BS 580) · airframe 28,319 hrs · 16,502 cycles
FWD CARGO COMPARTMENT LT SIDE FRAME BS 580 HAS TWO DENTS BETWEEN STR 23L AND 25L. EVALUATED DAMAGE, FABRICATED AND INSTALLED. REPAIR IAW SRM.
Part: GIRT BAR — WORN (R4 DOOR SLIDE) · airframe 28,319 hrs · 16,502 cycles
R-4 DOOR GIRT BAR ACTUATION SYS HAS GIRT BAR LIFTER BUSHINGS WORN FWD AND AFT CAM LIFTER BUSHINGS WORN. FWD AND AFT REMOVED AND INSTALLED R4 DOOR GIRT BAR ACTUATING SYS GIRT BAR LIFTER , CRANK ASSY AND BUSHINGS IAW CMM 52-11-05 AND IAW SOPM 20-50-03 AND CMM 52-11-25, ADJUSTMENT CHECK TO BE COMPLIED ON JOB CARD 5211-9001-4R.
Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL OTBD LOWER FLANGE BETWEEN BS 1320-1340, RBL-10.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL AND REMOVED AND REINSTALLED 4 EA BRACKETS, ANGLES IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 1520-1540) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL ON BOTH SIDES OF WEBAND ON LOWER FLANGE BETWEEN BS 1520-1540, RBL-3. REMOVED AFT CARGO BILGE INTERCOSTAL ON BS 1520-1540, RBL=3 IAW SRM 51-40-02, PG 2-11, EVALUATED CORROSION ON INTERCOSTAL IS OUT OF LIMITS IAW SRM 53-00-04 ALLOWABLE DAMAGE 1, FIG 101, DETAIL II. REPLACED INTERCOSTAL IAW DWG NR 146N8900.
Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320 LBL-17. REMOVED CORROSION IAW SRM 53-00-04, FIG 101 AD 1, PG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-04, FIG 101, DETAIL II, AD 1 PG 103. R & R THE INTERCOSTAL IAW SRM 51-40-02 GENERAL AND DWG NR 146N5700.
Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN STR 1300-1320, RBL-17. REMOVED CORROSION BLEND OUT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04 ALLOWABLE DAMAGE 1, DETAIL 1. ACCOMPLISHED REPLACEMENT OF AFT CARGO BILGE INTERCOSTAL IAW SRM 51-40-05 & 51-40-02.
Part: HINGE — CORRODED (MLG DOOR) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
SUPPORT CASTING FOR MLG DOOR CENTER HINGE HAS CORROSION ON FWD SIDE LOWER FLANGE, AND AFT SIDE TOP OF MID FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED REPLACEMENT OF KEEL SUPPORT CASTING FOR MLG DOOR CENTER HINGE AT KEEL BS 1120, LBL 0 IAW SRM.
Part: FRAME — DENTED (BS 620) · airframe 28,319 hrs · 16,502 cycles
FWD CARGO COMPARTMENT L/T SIDE FRAME BD 620 HAS ONE DENT, STR 23L. TRIMMED OUT DAMAGE, ACCOMPLISHED PERMANENT REPAIR IAW SRM.
Part: HINGE — CORRODED (RT MLG DOOR) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CASTING CORRODED TOP AND BOTTOM OF FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R MLG DOOR FWD HINGE AT KEEL BS 1072 LBL6-RBL6 IAW SRM.
Part: STIFFENER — CORRODED (BS 900 BULKHEAD) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON BULKHEAD STIFFENER LOWER SIDE BS 900 LBL 8. REMOVED CORROSION ON STIFFENER AT LOWER SIDE STA 900, LBL 7.5. ORIGINAL THICKNESS IS .180", MATERIAL LOSS WAS .049" WHICH WAS OUT OF LIMITS IAW SRM 51-10-10 ALLOWABLE DAMAGE PG 103, FIG 101, DETAIL V. R & R WITH NEW STIFFENER, VTSAA 111N2020-8 IAW SRM 51-40-02, PG 1-5 AND REF DWG 111N2001.
Part: STIFFENER — CORRODED (BS 900 BULKHEAD) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON BULKHEAD STIFFENER LOWER SIDE BS 900, RBL 10. REMOVED CORROSION ON STIFFENER AT LOWER SIDE BS 900, RBL 7.5 ORIGINAL THICKNESS IS .180", MATERIAL LOSS WAS .038 WHICH WAS OUT OF LIMITS IAW SRM 51-10-10 ALLOWABLE DAMAGE, PG 103, FIG 101, DETAIL V. R & R WITH NEW STIFFENER, PN 111N2020-7 IAW SRM 51-40-02 PG 1-5 AND REF DWG 111N2001.
Part: FRAME — DENTED (BS 700) · airframe 28,319 hrs · 16,502 cycles
FWD CARGO COMPARTMENT RT SIDE FRAME BS 700 HAS 2 EA DENTS STR 23R TO STR 24R. TRIMMED-OUT 2 EA DENTS ON FRAME AT BS 700, STR 23R-STR 24R REF SRM 53-00-07, REPAIR 5. TRIMOUT 1 MEASURE 1.08" X 1.04" X 0.5"R, TRIMOUT NR 2 MEASURE 1.78" X 1.04" X 0.5"R. ACCOMPLISHED PERMANENT REPAIR REF SRM 53-00-07, REPAIR 5.
Part: FRAME — DENTED (BS 1340) · airframe 28,319 hrs · 16,502 cycles
DENT ON AFT CARGO, LT FRAME UPPER FLANGE AT BS 1340 ABOVE STR 26L. TRIMMED-OUT 1 EA DENT ON FRAME UPPER FLANGE AT BS 1340, ABOVE STR 26L REF SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT MEASURE 1.38" X 0.94" X 0.5"R. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201.
Part: CASE — CORRODED (RUDDER ACTUATOR) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
RUDDER TRIM ACTUATOR CASE HARDWARE BADLY RUSTED. R & R VERTICAL STABILIZER RUDDER TRIM ACTUATOR IAW AMM 27-21. OPS CK GOOD.
Part: KEELBEAM — CORRODED (BS 1060-1072) · airframe 28,319 hrs · 16,502 cycles
KEELBEAM BS 1060-1072 LBL5 AND FASTENERS CORRODED AT SEVERAL SPOTS. R & R NEW FASTENERS AND STIFFENERS, PN 70016533830001, BS 1060-1072, LBL5-RBL5 IAW DWG 149N8110 AND SRM 51-40-02. REMOVED CORROSION FROM STIFFENER IAW SRM 53-40-12, ORIGINAL MATERIAL THICKNESS IS .435" MECHANICALLY MEASURED MATERIAL LOSS FOUND TO BE .055, MAX ALLOWABLE IS .043 IAW SRM 53-40-12, ALLOWABLE DAMAGE 1, FIG 101, FOUND TO BE OUT OF LIMITS FABRICATED NEW STIFFENER LOCATED AND DRILLED AND INSTALLED AT BS 1060-1072/LBL5 IAW SRM 51-40-02, PAGE 2. CORROSION ON STIFFENER FOUND DURING CORROSION REMOVEL ON KEEL BEAM, REMOVED CORROSION FROM KEELBEAM AT BS 1060-1072, LBL5 IAW SRM 53-40-12, FIG 101 ORIGINAL MATERIAL THK .250 MAT REMOVED FROM 2 EA AREAS, L=5.5 X W=1.4 D=.025 AND L=2.3 W=1.4 D= .011 FOUND 2 EA AREA TO BE IN LIMITS IAW SRM 53-40-12, FIG 101.
Part: INTERCOSTAL — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL ON INBD LOWER FLANGE AND OTBD FWD CHANNEL BETWEEN BS 1500-1520, LBL-2.9. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.
Part: SKIN — CORRODED (BS 1883-1885) · airframe 28,319 hrs · 16,502 cycles
AFT FUSELAGE TAIL COMPARTMENT, BS 1883-1885, LBL10-RBL10, SKIN AND FASTENERS CORRODED. REMOVED SKIN STRAP AFT LOWER BS 1885, STR 25L TO 25R. ORIG MATERIAL THICKNESS .011" IAW DWG 148N3601, MATERIAL LOSS .025" FOUND OUT OF LIMITS IAW SRM 53-80-01, FIG 101. FABRICATED SKIN STRAP IAW DWG 148N3601 AND SRM 51-40-05, PG 3. R & R FASTENERS IAW SRM 51-40-02 PARA 4B, PG2.
Part: ANGLE — CORRODED (BS 1480-1500) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1480-1500, LBL 24.5 UNDER OTBD SIDE OF TRANSITION PANEL. REMOVED CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE FOUND TO BE EXFOLIATED 50 PERCENT AND CRACKED OUT OF LIMITS IAW SRM 53-00-04. ALLOWABLE DAMAGE 1 DETAIL II. ORIGINAL MATERIAL .050 IAW DWG 146N5448, REV K 4" L X 1" W X .025. R & R IAW SRM 51-40-05, PG 3, FIG 1 AND SRM 51-40-02, PG 21.
Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL-3. REMOVED CORROSION AT INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL3. ORIGINAL MATTERIAL THICKNESS .032-MATTERIAL LOSS: 50 PERCNET =.016", FOUND OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DETAIL II. ALLOWABLE DAMAGE 1 L=3.6", W=1.5" D=.016. R & R INTERCOSTAL BETWEEN BS 1300-1320, LBL 3 IAW SRM 51-40-02, FIG 4, PG 21, PG 7, PARA 7D AND DWG 146N5399, REV B.
Part: FLOORBEAM — CORRODED (BS 310) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON FLOORBEAM UPPER TEE BS 310, LBL 17 TO LBL 21. COMPLIED WITH ERA 544722-14, REV ORIGINAL ON FUSELAGE FLOOR BEAM UPPER TEE AT BS 310.5, LBL 17-LBL 21.
Part: FLOORBEAM — CORRODED (BS 310) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON FLOORBEAM LOWER CHORD BS 310, LBL 51 TO LBL 60. COMPLIED WITH ERA 544723-14, REV ORIGINAL.
Part: CREASE BEAM — CORRODED (BS 800-880) · airframe 28,319 hrs · 16,502 cycles
UPON REMOVAL OF FLOORBOARD 230-41 IAW JIC 2020-2376 MAIN CABIN LT CREASE BEAM INBD CHORD CORRODED IN MULTIPLE SPOTS BETWEEN BS 800 AND BS 880. COMPLIED WITH ERA 544733-14, REV-0 PERMANENT REPAIR IN MAIN CABIN LT CREASE BEAM AT BS 760-898 INBD CHORD.
Part: SEAT TRACK — CORRODED (BS 1320-1350) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON MAIN CABIN SEAT TRACK BS 1320-1350, RBL 24. BLENDED AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED PERMANENT REPAIR IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 1200-1220) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1200 - 1220, LBL 24.5 JUST BELOW OTBD SIDE OF LT TRANSITION PANEL. REMOVED UPPER ANGLE IAW SRM 51-40-02, PG 1-10. LOCATED AND DRILLED UPPER ANGLE ON INTERCOSTAL IAW DWG 146N5390. INSTALLED NEW UPPER ANGLE ON INTERCOSTAL IAW SRM 51-40-02. PREVIOUS UPPER ANGLE FOUND 100 PERCENT EXFOLIATED AND OUT OF LIMITS, REF SRM 53-00-53, FIG 101, DET V.
Part: SKIN — DENTED (LT WING TE FLAPS) · airframe 28,319 hrs · 16,502 cycles
LT WING INBD MAIN FLAP UPPER SURFACE HAS 2 GOUGED DENTS 53" FROM INBD END/ 19"-22" FROM T/E. ACCOMPLISHED PERMANENT REPAIR ON LT WING INBD MAIN FLAP UPPER SURFACE AT 2 EA GOUGED DENTS 53" FROM INBD END 19"-22" FROM T/E, DAMAGE AREAS MEASURED 2." DIA IAW SRM 51-70-10.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
LEFT INBD MAIN FLAP UPPER OTBD PANEL HAS CHAFE DAMAGE 0-36" FROM THE OTBD END. ACCOMPLISHED REPAIR, DAMAGE DIMENSION IS APPROXIMATELY 1" X 11" OF THE DISCREPANT AREAS ON LT INBD MAIN FLAP UPPER OTBD PANEL IAW ER/A 514121-14MA, ORIGINAL REVISION.
Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
RT WING INBD MAIN FLAP UPPER SKIN HAS 2 EA CREASES 47"-49" FROM INBD END/ 18.5"-22.5" FROM T/E. ON RT WING INBD MAIN FLAP UPPER SKIN REPAIRED 2 EA CREASES 47"-49" FROM INBD END 18.5"-22.5" IAW SRM 51-70-10.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
LEFT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5"-77" FROM OTBD END. ACCOMPLISHED REPAIR OT THE DISCREPANT AREA ON THE UPPER SURFACE, APPROX 1" X 10" AND THE LOWER SURFACE, APPROX 10" X14" OF THE LT WING INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.
Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON MAIN CABIN SEAT TRACK SUPPORT BS 1640, RBL 45. R & R NEW SEAT TRACK SUPPORT BETWEEN BS 1600-BS 1640, RBL 45 IAW DWG 146N5120.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
RIGHT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5 - 77" FROM OTBD END. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON RT WING INBD MAINFLAP T/E WEDGE LOWER SKIN IAW SRM 51-70-10.
Part: SEAT TRACK — GOUGED (BS 1545) · airframe 28,319 hrs · 16,502 cycles
MAIN CABIN SEAT TRACK CROWN LBL 45 AT BS 1545 HAS A DEEP GOUGED. BLENDED GOUGED ON MAIN CABIN SEAT TRACK CROWN AT BS 1545, LBL 45. MATERIAL LOSS OF 0.033", FOUND TO BE OUT OFF LIMITS IAW SRM 53-00-52. ALLOWABLE DAMAGE DETAIL 1., ACCOMPLISHED REPLACEMENT OF MAIN CABIN SEAT TRACK FROM BS 1540-1600, LBL 45, IAW DWG NR 146N5120 SRM 51-40-02 & 51-40-05.
Part: STRAP — CORRODED (BS 740) · airframe 28,319 hrs · 16,502 cycles
CORROSION MAIN CABIN FLOOR STABILIZER STRAP, BS 740, LBL 26. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.
Part: STRAP — CRACKED (BS 365) · airframe 28,319 hrs · 16,502 cycles
MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP LBL 45, BS 365 CRACKED. REMOVED AND INSTALLED NEW SECCION OF STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP, LBL 45, STA 365.25 TO STA 377.7 IAW SRM.
Part: STRAP — CRACKED (BS 365-377) · airframe 28,319 hrs · 16,502 cycles
MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP BS LBL 26, BS 365 TO BS 377 CRACKED MIDSPAN. REMOVED AND INSTALLED NEW SECTION OF STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP, LBL 26, BS 365.25 TO BS 377.7 IAW SRM.
Part: SUPPORT STRAP — CORRODED (BS 1681) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
CORROSION ON SUPPORT STRAP BS 1681, BL0. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED.
Part: SUPPORT — CORRODED (BS 1678) · airframe 28,319 hrs · 16,502 cycles
CORROSION ON MAIN CABIN BOX BEAM SUPPORT LBL 52, BS 1678. R & R THE SUPPORT IAW SRM'S 51-40-02, PG 31 AND 51-40-02, PG 21.
Part: NUT — CORRODED (TE FLAP) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
NR 6 T/E FLAP TRACK BALL NUT TRUNNION HAS CORROSION AND BOTH BALLNUT BUSHING ARE WORN OUT OF LIMITS. REMOVED RT WING NR 6 T/E FLAP BALL SCREW IAW AMM 27-51-11-029-001. INSTALLATION OF SERVICEABLE NR 6 T/E FLAP BALLSCREW AND 2 EA NEW BALLNUT BUSHINGS AND TEST WILL BE ACCOMPLISHED ON TC 2751-2542.
Part: BALL SCREW — SPALLED (LT WING TE FLAP) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
LT WING INBD FLAP OTBD BALLSCREW THREADS SPALLING AND BALLNUT GREASE FILLED WITH RUST. R & R INBD FLAP, OTBD BALLSCREW IAW AMM 27-51.
Part: BALL SCREW — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
NR 5 T/E FLAP BALL NUT TRUNNION HAS CORROSION AND BOTH BALL NUT BUSHINGS ARE WORN OUT OF LIMITS. R & R RT WING NR 5 T/E FLAP BALLSCREW IAW AMM 27-51. NEW BUSHINGS WILL BE ACCOMPLISHED ON T/C 271-2542.
Part: BALL SCREW — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 28,319 hrs · 16,502 cycles
LT WING INBD MAIN FLAP INBD BALLSCREW NUT CORRODED AND BUSHINGS ARE WORN. R & R LT WING INBD MAIN FLAP INBD BALLSCREW AND 2 EA NEW BUSHINGS WILL BE ACCOMPLISHED ON T/C 2751-2538.
Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
RT WING INBD MAIN FLAP UPPER SKIN PUNCTURED 62" FROM INBD END/ 13" FROM T/E. ACCOMPLISHED REPAIR OF RT WING INBD MAIN FLAP UPPER SKIN, APPROXIMATELY A .5" CIRCLE, 62" FROM THE INBD END AND 13" FROM THE T/E IAW SRM 51-70-17.
Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 28,319 hrs · 16,502 cycles
LT WING INBD MAIN FLAP UPPER SURFACE PUNCTURED 53" FROM INBD END 14" FROM T/E. ON LT WING INBD MAIN FLAP UPPER SURFACE 53" FROM INBD END 14" FROM T/E. REPAIRED IAW SRM 51-70-17, REPAIR 4B, FIG 24.