N964DN

Part: ENGINE — MAKING METAL (LEFT) · airframe 44,885 hrs · 25,519 cycles

IFSD OF NUMBER ONE ENGINE DUE TO AN OIL STRAINER CLOGGED MESSAGE. AIRCRAFT ARRIVED SAFELY IN SAN. SAN MAINTENANCE FOUND SIGNIFICANT METAL IN MAIN OIL FILTER AND ON CHIP DETECTORS, REPLACED LEFT ENGINE. SYSTEM OPERATION IS NORMAL.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 43,452 hrs · 24,726 cycles

EMERGENCY EXIT COVER LENS DAMAGED. REPLACED THE LENS.

Part: APU — CONTAMINATED · airframe 42,601 hrs · 24,227 cycles

CREW REPORTED AN ODOR IN THE CABIN WITH HAZE. MAINTENANCE FOUND APU CONTAMINATED. CLEANED APU INLET AND INSPECTED DOOR. INSPECTED AND FOUND OVERFLOW BOTTLE FULL AND DRIPPING HYDRAULIC FLUID. EMPTIED BOTTLE AND PERFORMED DUCT BURNOUT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,473 hrs · 24,150 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY ASSEMBLY. OPERATION CHECKS OK.

Part: LONGERON — CORRODED · airframe 41,648 hrs · 23,662 cycles

CORROSION ON LONGERON 28R AND SPLICE BETWEEN 28-229 AT ELECTRONICS EQUIPMENT COMPARTMENT. REPAIRED IAW SRM 53-10-01.

Part: GUIDE VANE — PUNCTURED (LT WING TE FLAP) · airframe 41,654 hrs · 23,666 cycles

PUNCTURE ON LOWER FACE INBD FLAP INBD GUIDE VANE, LT WING. REPAIRED IAW SRM 57-20-02.

Part: TAB — UNKNOWN (RUDDER) · airframe 41,648 hrs · 23,662 cycles

FLAME SPRAY COAT ON RUDDER CONTROL TAB. REPAIRED IAW SRM 55-41-01.

Part: SKIN — DAMAGED (RUDDER) · airframe 41,648 hrs · 23,662 cycles

DAMAGED METAL OF RUDDER. REPAIRED IAW SRM 55-41-01.

Part: ANGLE — CRACKED (BS 1475) · airframe 41,645 hrs · 23,661 cycles

CRACKED CLIP JUST ABOVE LONGERON BS 1475, 19L, 16LH AT AFT ACCESSORY COMPARTMENT. FABRICATED AND INSTALLED NEW CLIPS IAW SRM 5-103 AND 51-30-05.

Part: CUSP WEB — CRACKED (BS 902) · airframe 41,645 hrs · 23,661 cycles

CRACK ON CUSP WEB BS 902, BETWEEN X=60 AND X=54. REPAIRED IAW SRM 53-20-02, FIG 8.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 41,171 hrs · 23,387 cycles

NON-STANDARD HOLE IN VERTICAL STAB FORWARD RT SPAR FORWARD FLANGE BELOW ZFS52.267. REPAIRED IAW ERA 543991-14AD.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 41,171 hrs · 23,387 cycles

NON STANDARD HOLE IN VERTICAL STAB FORWARD LT SPAR FORWARD FLANGE FASTENER HOLE BELOW ZFS 52.267. REPAIRED IAW ERA 543991-14AD.

Part: FINGER DOUBLER — CRACKED (VERTICAL STAB) · airframe 41,171 hrs · 23,387 cycles

VERTICAL L/E SKIN LOWER FINGER DOUBLER CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW DWG 5930609 AMD SG09550005.

Part: STRUCTURE — UNKNOWN (VERTICAL STAB) · airframe 41,171 hrs · 23,387 cycles

RT VERTICAL STABILIZER DIRTY HOLE INDICATION. REMOVED VERTICAL STABILIZER L/E AND REPAIRED BOTH LT AND RT STABILIZER SPAR CAP AND L/E SKIN AW SG0955005 AND ERA 543991-14AD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,143 hrs · 23,374 cycles

EMERGENCY EXIT LIGHT OUT AT PASSENGER AND SERVICE DOORS. R & R EMERGENCY BATTERY PACKS B5-240 IAW MM. OPERATION CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,092 hrs · 22,729 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-241 OVER AMM. OPERATION CHECK OK.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 38,194 hrs · 21,561 cycles

TAILCONE DISPLACEMENT BOTTLE PULL CABLE WORN. REPLACED PULL CABLE.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 36,589 hrs · 20,556 cycles

AFT EMERGENCY EXIT SIGN FLASHING ON AND OFF. R & R AFT EMERGENCY CABIN LIGHT BATTERY AND BATTERY PACK. OPERATION CHECKED GOOD.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 36,482 hrs · 20,488 cycles

DURING SERVICE CHECK, NOTED LT SLIDE PINS NOT ENGAGED. R & R L1 DOOR SLIDE IAW AMDS 2561-4641.

Part: COVER — CRACKED (TAILCONE SLIDE) · airframe 36,360 hrs · 20,412 cycles

TAIL CONE SLIDE COVER CRACKED AT HINGES. SLIDE AND COVER INSTALLED ON AMDS 5352-4491.

Part: SKIN — CRACKED (BS 1531) · airframe 36,359 hrs · 20,411 cycles

FUSELAGE EXTERIOR SKIN CRACKED 15 INCHES ABOVE VENTRAL STAIR AT CANTED FRAM BS 1531. REPAIRED IAW ERA 489806-14 MA.

Part: SKIN — CRACKED (BS 1531) · airframe 36,359 hrs · 20,411 cycles

FUSELAGE SKIN CRACKED AT CANTED FRAME BS 1531, RIGHT HAND. REPAIRED IAW ERA 489806-14MA, REV O.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 36,359 hrs · 20,411 cycles

L1 DOOR SLIDE LANYARD IS FRAYED. REMOVED AND REPLACED LANYARD IAW MM. (LP# 1435900)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,667 hrs · 19,967 cycles

EMERGENCY LIGHTS ALONG VENTRAL STAIRS INOPERATIVE. R & R BATTERY PACK, POWER SUPPLY, AND REPLACED LAMPS. OPS CHECKED NORMAL IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,600 hrs · 18,260 cycles

DURING SERVICE CHECK, MX FOUND VENTRAL STAIRS EMERGENCY LIGHTS INOPERATIVE. R & R AFT RT LAVATORY BASE AND BATTERY PACK B5-239 AND LAMPED EIGHT SIDEWALL LIGHTS. OPS CHECKED GOOD.

Part: CABLE — OUT OF RIG (TAIL) · airframe 32,242 hrs · 18,064 cycles

DURING INSPECTION AND RIG CHECK OF CATWALK, MX FOUND LATCH PLUNGER HSG OUT OF ADJUSTMENT. ADJUSTED MOVEABLE CEILING IAW AMM. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,127 hrs · 17,997 cycles

DURING SERVICE CHECK, FOUND BOTH EXTERIOR EMERGENCY LIGHTS IINOPERATIVE. R & R NEW BATTERY IN BATTERY PACKS. OPS CHECKS NORMAL.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 31,912 hrs · 17,876 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT SEAT 21B. MAINTENANCE REMOVED AND REPLACED TERMINAL LUG AT GROUND 5244 OR WIRE L841C20N PER WDM. OPERATION CHECKS GOOD.

Part: GUIDE VANE — DAMAGED (RT WING TE FLAP) · airframe 31,909 hrs · 17,873 cycles

RIGHT INBOARD FLAP OUTBOARD GUIDE VANE DAMAGED. REMOVED AND REPAIRED AND REINSTALLED RT INBOARD FLAP OUTBOARD GUIDE VANE AS PER AMM 27-50-02-020-801, 27-50-02-420-801 AND SRM 51-10-02 VOL I, 57-20-05 VOL I.

Part: FLOORBEAM — DAMAGED (BS 1395 RBL 26) · airframe 31,909 hrs · 17,873 cycles

FLOORBEAM AT STA 1395 RBL 26 HAS DOUBLE HOLE. INSTALLED REPAIR PER ERA 501342-14 REV O.

Part: DOOR FRAME — GOUGED (CARGO DOORWAY) · airframe 31,909 hrs · 17,873 cycles

MID CARGO DOOR AFT FRAME PAN GOUGED ABOVE BEARING OF LOCK MECHANISM. REMOVED BEARING OF LOCK MECHANISM AND STOP FITTINGS NR 1 AND NR 2 FOR ACCESS, REF MD90 SRM 51-30-05 VOL II. BLENDED OUT GOUGE AT MID CARGO DOOR. AFT JAMB PAN FOUND OUT OF LIMITS REF SRM 52-00-01 FIG 3 VOL I. INSTALLED REPAIR DOUBLER AND BACK UP AREA OF MID CARGO DOOR AFT FRAME IAW SRM 52-30-02 FIG 5 VOL I.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 31,909 hrs · 17,873 cycles

HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN RT AFT BARREL NUT HOLES (2 AFT HOLES) HAVE CORROSION. REMOVED AND REPLACED SKIN PANEL NR 5936113-504 AT RT HORIZONTAL STAB PER DWG 5940486.

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAPS) · airframe 31,909 hrs · 17,873 cycles

LEFT WING OTBD FLAP INBD SUPPORT FITTING UPPER ARM AFT OTBD SCREW HOLE FOR FAIRING HAS CORROSION. REMOVED CORROSION ON TWO OTBD FLAP INBD SUPPORT FITTING. UPPER HOLE STEPPED UP TO O.341 AND LOWER HOLE TO 0.391 DIAMETER. INSTALLED REPAIR BUSHINGS IN REF MD90 SRM 51-10-05 AND DELTA ER/A 503593-14.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 31,909 hrs · 17,873 cycles

REMOVED RT MLG SUPPORT FITTING BUSHING AND BEARING. NO CORROSION FOUND ON SUPPORT FITTING BUSHING BUT FOUND SCRATCHES AND CORROSION ON BEARING BORE. GENERATED AAR N/R S/N 1016456 AND REWORKED AREA PER DRAWING SR09570087-7001 AND INSTALLED OVER SIZED BEARING, SUPPORT FITTING BUSHING REMAINED STANDARD SIZED.

Part: BEAM — CORRODED (BS 1212 L19R) · airframe 31,909 hrs · 17,873 cycles

CORROSION FOUND AT AFT CARGO DOOR CUTOUT UPPER BEAM AT BS 1212 L19R. REMOVED AND REPLACED BEAM PER SRM 51-30-05 VOL II.

Part: FRAME — CRACKED (BS 1364) · airframe 31,909 hrs · 17,873 cycles

LT CABIN FUSELAGE FRAME CRACKED AT BS 1364 L15L TO L16L. REMOVED AND REPLACED FRAME BS 1364 BETWEEN L13L-L16L IN REF WITH SRM 51-30-05, 51-30-03 VOL II AND DRAWING 9912243.

Part: FRAME — CRACKED (BS 1364) · airframe 31,909 hrs · 17,873 cycles

RT AFT CABIN FUSELAGE FRAME TIE CRACKED AT STA 1364 L15R TO L16R. REMOVED AND REPLACED FORMER FROM RT AFT CABIN FUSELAGE AND BULKHEAD WEB AT BS 1364 BETWEEN LONGERONS L13R-L16R IN REF WITH SRM 51-30-05, 51-30-03 VOL II AND DRAWING NR 9912243.

Part: CARGO TRACK — CORRODED (BS 512-845) · airframe 31,909 hrs · 17,873 cycles

REMOVED AND REPLACED TIE-DOWN TRACK BETWEEN FS 845-512 FOUND OUT OF LIMITS WITH CORROSION IN REF SRM 51-10-03 AND 53-00-01. FABRICATED AND INSTALLED NEW SPLICE AT FS 720 LT IN REF SRM 53-40-01 VOL I.

Part: DOUBLER — CORRODED (BS 769) · airframe 31,909 hrs · 17,873 cycles

MID CARGO COMP ANTENNA DOUBLER BETWEEN FS 769-788 HAS CORROSION. REMOVED AND REPLACED DOUBLER AT FS 769-788 IN REF MD-90 SRM 51-30-02, 51-30-05.

Part: DOUBLER — CORRODED (BS 1395 BULKHEAD) · airframe 31,909 hrs · 17,873 cycles

AFT CARGO COMPARTMENT AFT PRESSURE BULKHEAD LOWER ANGLE CORROEDED AT BS 1395 LONGERON 30. REMOVED AND REPLACED DOUBLER AFT PRESSURE BULKHEAD AND TEE EXTRUSION AS PER SRM 53-00-01.

Part: CARGO TRACK — CORRODED (BS 218-512) · airframe 31,909 hrs · 17,873 cycles

FWD CARGO BAY LEFT TIE DOWN TRACK FS 218-512 FRAME ATTACH POINTS AND UPPER, LOWER SURFACE FLANGE CORROSION OUT OF LIMITS IN REF SRM 53-00-01. REMOVED AND INSTALLED NEW TIE DOWN TRACK WITH 2 NEW SPLICES IN REF SRM 53-40-01, 51-30-05 AND 51-30-02. TREATED AND TOP COATED IN REF SRM 51-10-03.

Part: CARGO TRACK — CORRODED (BS 598-617) · airframe 31,909 hrs · 17,873 cycles

MID CARGO COMP LT TIE DOWN TRACK SPLICE BETWEEN FS 598-617 HAS CORROSION. REMOVED AND REPLACED TIE-DOWN SPLICE AT FS 608 IN REF SRM 51-10-03, 51-10-05, 51-30-05 VOL II, 51-40-01 FIG 7 VOL I DWG NR 3936702.

Part: BEAM — CORRODED (BS 655-788) · airframe 31,909 hrs · 17,873 cycles

BEAM FOUND CORRODED. REMOVED AND REPLACED LOWER BEAM 28R BETWEEN BS 655 THRU 788 AS PER DRAWING NR 5930481 AND PER SRM 51-30-05.

Part: GUSSET — CORRODED (CARGO BAY) · airframe 31,909 hrs · 17,873 cycles

REMOVED CORROSION AT GUSSETS BS 370 AND 427 IAW SRM 51-10-03 VOL II. FOUND OUT OF LIMITS IN REF SRM53-00-01 VOL I. REMOVED AND REPLACED GUSSETS AT FS 370 AND 427 IN REF SRM 51-30-05 AND DWG NR 5910142.

Part: WEB — CORRODED (BS 362.5-434.5) · airframe 31,909 hrs · 17,873 cycles

BLENDED OUT DAMAGE AND REPLACED WEB IN FWD CARGO COMPARTMENT CUT OUT DOOR FRAME FROM FS 362.5 - 434.5 BETWEEN L29R - L24R IAW SRM NR 51-30-02 VOL II AND DRAWING 3 5910142.

Part: INTERCOSTAL — CORRODED (BS 750-757) · airframe 31,909 hrs · 17,873 cycles

MID CARGO COMPARTMENT, GUSSETS AND INTERCOSTAL BETWEEN BS 750-757.5 AND L30-L29R HAVE CORROSION. REMOVED AND REPLACED INTERCOSTAL AND GUSSETS PER 51-30-02 VOL II, 53-00-01 VOL I, 51-10-01 VOL II, 51-10-02 VOL II, AND 51-10-03 VOL II.

Part: FRAME — CORRODED (BS 1437) · airframe 31,909 hrs · 17,873 cycles

AFT ACCY LOWER FRAME SECTION BS 1437 LBL 16 TO RBL 16 HAS CORROSION ON AFT SIDE OF TEE CAP ALSO FUSELAGE SKIN JUST AFT HAS BARE SPOTS. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FRAME SECTION LOCATED AND DRILLED NEW FRAME, TREATED AND PRIMED SKIN AND FRAME. INSTALLED NEW FRAME AT BS 1437 REF MD-90 SRM 51-30-02 AND 51-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 370-427) · airframe 31,909 hrs · 17,873 cycles

FWD CARGO COMPT, SMALL FLOOR SUPPORT BRACKETS AT STA 427 AND 370 BETWEEN L28-29R HAVE SURFACE CORROSION. REMOVED AND REPLACED FLOOR SUPPORTS PER SRM 51-30-05 AND 51-30-02.

Part: GUSSET — CORRODED (BS 757 L27-30R) · airframe 31,909 hrs · 17,873 cycles

MID CARGO BAY GUSSET FROM BS 757 BETWEEN L27-30R CORRODED AND HOLE ELONGATED. REMOVED AND REPLACED GUSSET PER DWG 5936039, SRM 51-30-05 VOL II, 51-10-03 VOL II, AND 53-00-01 FIG 3 VOL I.

Part: CHANNEL — DAMAGED (BS 647) · airframe 31,909 hrs · 17,873 cycles

REMOVED AND REPLACED INTERCOSTAL CHANNEL AT STA 674 BETWEEN L-28R - L29R IN REF DRAWING 9936577.

Part: BRACKET — CORRODED (BS 1250) · airframe 31,909 hrs · 17,873 cycles

AFT CARGO BS 1250 BRACKET FOR LEFT TIE DOWN TRACK, UNDER TRACK, IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. LOCATED AND DRILLED NEW BRACKET AT STA 1250 P/N 3936595-517. INSTALLED NEW BRACKET REF MD-90 SRM 51-10-05 AND 51-30-05.

Part: WEB — CORRODED (FWD CARGO JAMB) · airframe 31,909 hrs · 17,873 cycles

LOWER DOOR FRAME CORRODED. REMOVED AND INSTALLED NEW PANEL SECTION AT FWD CARGO BAY LOWER DOOR FRAME BETWEEN BS 370 AND 427 IAW SRM 53-60-02 VOL I FIGURE 11.

Part: FLOOR SUPPORT — CORRODED (BS 1212) · airframe 31,909 hrs · 17,873 cycles

FLOOR SUPPORT AT BS 1212 HAS CORROSION TOP AND BOTTOM. REMOVED CORROSION FOUND OUT OF LIMITS LOCATED AND DRILLED NEW FLOOR SUPPORT TOP COATED NEW FLOOR SUPPORT. INSTALLED NED FLOOR SUPPORT IAW SRM 51-30-2 VOLUME II.

Part: FRAME — CORRODED (BS 1307) · airframe 31,909 hrs · 17,873 cycles

AFT CARGO BAY BS 1307 FRAME CORRODED BETWEEN LONGERON 28 RT AND LONG 28 LT. REMOVED CORROSION FOUND OUT OF LIMITS CUTOUT DAMAGED AREA. FABRICATED FRAME REPAIR TREATED PRIMED AND TOP COAT ALL PARTS. INSTALLED FRAME REPAIR. REF DWG SR09530057.

Part: INTERCOSTAL — CORRODED (BS 160-180 L28L) · airframe 31,909 hrs · 17,873 cycles

E/E BAU INTERCOSTAL BETWEEN FS 160-180 AT L28L HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-02 VOL II, 53-00-01 VOL I, 53-10-01 VOL III, AND 51-10-03 VOL II.

Part: SEAT TRACK — CORRODED (BS 200 RBL 44) · airframe 31,909 hrs · 17,873 cycles

CORROSION AT SEAT TRACK RBL 44 BS 200 INBD EDGE LWR SURFACE. REMOVED CORRODED SECTION FROM BS 200-246 AND INSTALLED REPAIR SPLICE PER SRM 53-40-01 FIG 6 VOL I.

Part: LONGERON — CORRODED (FS 170-180) · airframe 31,909 hrs · 17,873 cycles

E/E COMPARTMENT L 28 FS 170-180 HAS SPOTS OF CORROSION. REPAIRED PER SRM 53-10-01 FIG 7.

Part: LONGERON — CORRODED (FS 160-200 L30) · airframe 31,909 hrs · 17,873 cycles

E/E COMPARTMENT L30 FROM FS 160 - 200 HAS SPOTS OF CORROSION. REPAIRED LONGERON PER SRM 53-10-01-FIG 7 ON NR 1000 10417 1016163.

Part: STRINGER — CORRODED (FS 160-200) · airframe 31,909 hrs · 17,873 cycles

E/E COMPARTMENT STRINGER 29L STA 160-200 HAS SPOTS OF CORROSION. REPAIRED PER 53-10-01 FIG 7 ON NR 1000/419/1016165.

Part: CUSP WEB — CORRODED (FS 1193-1235) · airframe 31,909 hrs · 17,873 cycles

CABIN LT SIDE CUSP WEB AT BS 1193 TO 1235 HAS CORROSION. REPAIRED PER SRM 53-20-02-FIG 26 CONFIG 7041 VI NR 1015731.

Part: CUSP WEB — CRACKED (BS 1355) · airframe 31,909 hrs · 17,873 cycles

CABIN LT SIDE CUSP WEB STA 1355 CRACKED AT LIGHTENING HOLE. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-20-02 FIG 6 VOL I.

Part: SEAT TRACK — CORRODED (BS 200-265) · airframe 31,909 hrs · 17,873 cycles

CORROSION AT RT CABIN SEAT TRACK LOWER ATTACH FLANGE TO WEB AREA RBL 22 FROM BS 200-265. REPLACED SEAT TRACK PER SRM 53-40-01 VOL I.

Part: CUSP WEB — GOUGED (BS 1193) · airframe 31,909 hrs · 17,873 cycles

CABIN RT SIDE CUSP WEB FS 1193 DENTED & GOUGED. INSTALLED REPAIR DOUBLER IAW SRM 53-20-02 VOL II FIG 14 REPAIR 7017.

Part: FRAME — CORRODED (BS 1288 L28L/R) · airframe 31,909 hrs · 17,873 cycles

AFT CARGO COMPARTMENT FRAME AT BS 1288 FWD AND AFT FACE FRAME HAS CORROSION BETWEEN L28L AND L28R. FABRICATED FRAME SECTION PER DWG SR09530057 AND 9919603. INSTALLED FRAME REPAIR PER SRM 51-30-00 VOL II.

Part: CUSP WEB — DENTED (BS 792) · airframe 31,909 hrs · 17,873 cycles

CABIN RT SIDE CUSP WEB FS 792 DENTED. INSTALLED REPAIR DOUBLER PER SRM 53-20-02 FIG 21 VOL I.

Part: CUSP WEB — CRACKED (BS 739) · airframe 31,909 hrs · 17,873 cycles

CABIN RT SIDE CUSP WEB FS 739 CRACKED ON OTBD EDGE. FABRICATED DOUBLER AND FILLER AND INSTALLED PER SRM 53-20-02 FIG 19.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 31,909 hrs · 17,873 cycles

INTERCOSTAL IN MID CARGO BAY FOUND OUT OF LIMITS FOR CORROSION PER SRM 51-10-03 VOL II AND 53-00-01 VOL I. REMOVED AND REPLACE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 31,909 hrs · 17,873 cycles

INTERCOSTAL IN MID CARGO BAY FOUND OUT OF LIMITS FOR CORRSION PER SRM 51-10-03 VOL II AND 53-00-01 VOL I.