N921DN

Part: WEB — CORRODED (VENTRAL STAIRS) · airframe 47,937 hrs · 31,979 cycles

CORROSION ON WEB ON STEP 5 AT VENTRAL STAIRWAY. WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR 5 FIG 3; ORIGINAL THICKNESS IS 0.040" AND MINIMUM REMAINING THICKNESS IS 0.024" THEREFORE AREA IS OUT OF LIMITS PER ER/A: 511165-14MA REV D. WEB ON STEP 5 AT VENTRAL STAIRWAY WAS REPAIRED (PERMANENT REPAIR) PER SRM VOL. I 52-00-01 FIG 5.

Part: ROD — CORRODED (RUDDER) · airframe 47,937 hrs · 31,979 cycles

CORROSION ON ROD P/N NAS354-4-270 AND ROD-END P/N XREP3F4S181. ROD AND ROD-END 2EA WERE REPLACED PER AMM 27-26-01-420-801. ROD AND ROD-END 2EA WERE ADJUSTED PER AMM 27-26-01-820-801 FUNCTIONAL TEST OF THE RUDDER THROW LIMITER WAS PERFORMED PER MD90 AMM 27-26-01-720-801 TEST OK. (LP0616914)

Part: WIRE — BURNED (HYDRAULIC SYS) · airframe 47,394 hrs · 31,642 cycles

AUX HYD PUMP CB TRIPPED. FOUND WIRE BURNED AT LOC B1-110 ON RT AUX HYD PUMP CB T1. REMOVED SAFETY WIRE FROM RT AUX HYS PUMP. REPLACED BUS BA5R T1-SEE 24-50-00-19 SHEET 2 ITEM 55-A PHASE. REPLACED RT AUX HYD PUMP CB B1 764 50 A. SEE WDM 29-21-00 PG 1. PERFORMED WORK CARD 2920-01077-02 AD RELATED. NO SUBSTITUTIONS OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,680 hrs · 31,205 cycles

EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REMOVED AND REPLACED POWER BATTERY AT STA 170. OPERATIONS CHECK GOOD. (LP# 9827760)

Part: BRAKE SYS — FAILED (MLG) · airframe 44,173 hrs · 29,802 cycles

DURING TAXI OUT, THE AIRCRAFT'S MAIN BRAKES LOCKED, CAUSING THE AIRCRAFT TO STOP UN-COMMANDED, AND CAUSING FLIGHT ATTENDANT CREW INJURIES REQUIRING MEDICAL ATTENTION. THE FLIGHT CREW ALSO REPORTED THAT THE AUTO-BRAKE SYSTEM FAILED TO ARM. CORRECTIVE ACTION: MAINTENANCE FOUND THE NO.3 BRAKE ASSEMBLY INBOARD ROTOR FALLING BETWEEN THE STATORS AND LOCKING UP THE NO.3 BRAKE. THE NR 3 BRAKE ASSEMBLY WAS REMOVED AND REPLACED PER THE MD90 AMM. MAINTENANCE ALSO PERFORMED AN ANTI-SKID SYSTEM RETURN-TO-SERVICE TEST WITH NO PRESENT STATUS FAULTS, AND AN AUTO-BRAKE SYSTEM RTS TEST THAT PASSED. THE AUTO-BRAKE SYSTEM ARMED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP# 9690726)

Part: SKIN — CORRODED (BS 1193-1200) · airframe 43,338 hrs · 29,263 cycles

AFT CARGO COMPARTMENT BILGE AREA RIGHT SIDE SKIN, BS 1193 - 1200 BETWEEN LONGERONS 29 - 30R CORRODED. REPAIRED IAW PRI/ERA 549063-14.

Part: FRAME — CRACKED (BS 1458) · airframe 43,323 hrs · 29,253 cycles

AFT FUSELAGE, BS 1458 LONGERON 2L OUTBOARD FRAME FLANGE CRACKED AT FRAME ATTACH POINT. REPAIRED IAW PRI/ERA 549071-14, REV O.

Part: RETAINER — GOUGED (CARGO DOOR) · airframe 43,324 hrs · 29,254 cycles

AFT CARGO DOOR AFT LOWER CORNER, SKIN AND SEAL RETAINER GOUGED. OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW ERA 549070-14, REV O. (LP# 2633154)

Part: SKIN — GOUGED (CARGO DOOR) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO DOOR FORWARD LOWER CORNER SKIN AND SEAL RETAINER GOUGED. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW PRI/ERA 549070-14. (LP# 2633150)

Part: STRUCTURE — CRACKED (BS 1520) · airframe 43,323 hrs · 29,253 cycles

PREVIOUS REPAIR BS 1520, LONGERON L9 TO 10 HAS INDICATION OF CRACK. REMOVED PREVIOUS REPAIR. INSTALLED REPAIR PARTS IAW SRM 53-10-03.

Part: FRAME — CRACKED (RT MLG WW) · airframe 43,323 hrs · 29,253 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL LOWER FRAME CRACKED IN THE RADIUS. FABRICATED DOUBLER REPAIR AND FRAME ASSEMBLY IAW SRM 53-60-02 AND DWG 5930584.

Part: ANGLE — CORRODED (BS 1463) · airframe 43,323 hrs · 29,253 cycles

AFT TAIL CONE COMPARTMENT RIGHT BS 1463 LOWER BILGE AREA HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE ANGLE IAW DWG 9911991, REV K AND SRM 51-30-01.

Part: SHEAR TIE — CORRODED (BS 1344) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, BS 1344 BETWEEN LONGERON 28L AND 26R SHEAR TIE CORRODED. FOUND TO BE OUT OF LIMITS. INSTALLED A NEW SHEAR TIE IAW DWG 9957739, REV DD.

Part: DOOR FRAME — CRACKED (BS 966-983) · airframe 43,323 hrs · 29,253 cycles

RIGHT MLG WHEEL WELL BS 966 TO 983 INTERCOSTAL CRACKED. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-30-05 AND DWG 5930584.

Part: LONGERON SPLICE — CORRODED (BS 1344-1364) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA BETWEEN BS 1344 - 1364 LONGERON 28L CORRODED IN CHANNEL. FOUND TO BE OUT LIMITS. REMOVED AND REPLACED LONGERON SPLICE IAW SRM 53-10-01.

Part: LONGERON SPLICE — CORRODED (BS 1340-1364) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY BILGE AREA BETWEEN BS 1340 AND 1364, LONGERON 28L CORRODED IN CHANNEL. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 53-10-01.

Part: FILLER — CRACKED · airframe 43,323 hrs · 29,253 cycles

CATWALK LEFT FORWARD FILLER CRACKED. REPAIRED IAW ER 549064-14, REV O.

Part: STRUCTURE — CORRODED (BS 1364) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY BILGE, BS 1364, ABOVE LONGERON 29L IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW DWG 9912243 AND SRM 53-00-01.

Part: FRAME — CORRODED (BS 1328) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, BS 1328, BETWEEN LONGERON 29L AND 29R, FRAME IS CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED THE FRAME SECTION IAW SRM 53-10-02.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 43,323 hrs · 29,253 cycles

CENTER CARGO DOOR LOWER EDGED DAMAGED. REPAIRED IAW PRI/ERA 549072-14.

Part: FRAME — CORRODED (BS 1344) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY BILGE AREA, BS 1344 BETWEEN LONGERONS 29L AND 29R, FRAME CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-30-02 AND 51-30-05.

Part: DOUBLER — CORRODED (BS 807) · airframe 43,323 hrs · 29,253 cycles

CENTER CARGO BAY, BS 807, X -1 TO X -2 STRAP AT SKIN INNER SURFACE CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED DOUBLER IAW PRI/ERA 544338-14, REV O.

Part: SHEAR TIE — CORRODED (BS 1307) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY BILGE AREA LEFT SIDE BS 1307, BETWEEN LONGERONS 29 AND 30L SHEAR TIE CORRODED. INSTALLED A REPAIR IAW SRM 53-10-02.

Part: LONGERON — CORRODED (BS 1364-1395) · airframe 43,323 hrs · 29,253 cycles

CARGO BAY RIGHT SIDE BETWEEN, BS 1364 - 1395 CORRODED ON LONGERON 27R. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01.

Part: LONGERON — CORRODED (BS 1395) · airframe 43,323 hrs · 29,253 cycles

CARGO BAY RIGHT HAND SIDE BS 1395 LONGERON 27R TERMINAL FITTING CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED THE LONGERON FITTING IAW SRM 51-30-05 AND 53-00-01.

Part: LONGERON — CORRODED (BS 1379-1395) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY RIGHT SIDE, BETWEEN BS 1379 - 1395, LONGERON 28R TERMINAL FITTING IS CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED FITTING IAW SRM 51-30-05 AND 53-00-01.

Part: ANGLE — CORRODED (BS 1212) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, RIGHT SIDE, BS 1212, LONGERON 28R ANGLE CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW ANGLE IAW WDG 5965790, REV J. AND SRM 51-10-03.

Part: DOUBLER — DAMAGED (BS 1165-1168) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, BS 1165 - 1168 BETWEEN STRINGERS 27 AND 28R. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-30-02 AND DWG 5936022.

Part: CARGO TRACK — CORRODED (BS 1269) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, RIGHT SIDE, BS 1269, LONGERON 28R CARGO TRACK CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-30-01. (LP# 2622321)

Part: FRAME — CORRODED (BS 1250) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO BAY BILGE AREA LEFT SIDE, BS 1250 BETWEEN LONGERONS 27 AND 36L. FRAME SPLICE CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FRAME STRAP IAW SRM 51-30-05, 53-30-05 AND DWG 9936073.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 43,323 hrs · 29,253 cycles

CARGO BAY RIGHT SIDE BS 1344 - 1364 LONGERON 27R CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-30-02 AND 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 1212-1269) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA DOOR CUTOUT, BS 1212 - 1269 LOWER SILL WEB CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT FROM IAW SRM 51-30-02 AND DWG 5936442.

Part: FLOORBEAM — CRACKED (BS 1212) · airframe 43,323 hrs · 29,253 cycles

FLOORBEAM ANGLE CRACKED , BS 1212 BETWEEN LBL 28 AND RBL 30. REMOVED AND REPLACED IAW DWG 5965790 AND SRM 51-30-02.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 43,323 hrs · 29,253 cycles

RIGHT HORIZONTAL STABILIZER OUTBOARD RIB, XHR 209.215 HAS CORRODED INTERNAL FASTENERS. REPAIRED IAW PRI/ERA 549062-14.

Part: FLOOR SUPPORT — CORRODED (BS 1144-1147) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, BS 1144 - 1147 BETWEEN LONGERONS 29-30L CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT SPLICE IAW SRM 51-30-01 AND DWG 5956157, REV AB. (LP# 2620899)

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 43,323 hrs · 29,253 cycles

LEFT WING RIB ATTACH ANGLE CRACKED. JUST OUTBOARD OF THE NR 1 SLAT TRACK. REPAIRED IAW ERA 544333-14.

Part: LONGERON — CORRODED (BS 1307-1328) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA, BS 1307 - 1328, FOUND LONGERON 28L CORRODED OUT OF LIMITS. REPLACED LONGERON IAW SRM 51-10-01.

Part: STRUCTURE — CORRODED (BS 1328-1344) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA BETWEEN BS 1344 - 1328 L28L CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-01.

Part: CUSP WEB — CORRODED (BS 1250-1269) · airframe 43,345 hrs · 29,268 cycles

CUSP WEB CORRODED, BS 1250 - 1269. FOUND TO BE OUT OF LIMITS. REPAIRED IAW PRI/ERA 549059-14.

Part: WEB — CRACKED (BS 220) · airframe 43,323 hrs · 29,253 cycles

FLOOR WEB RIGHT SIDE, BS 220, RBL 22 CRACKED. REMOVED AND REPLACED THE FLOOR WEB IAW SRM 51-11-01 AND DWG 9936535.

Part: SEAT TRACK — CORRODED (BS 210-275) · airframe 43,323 hrs · 29,253 cycles

RIGHT SIDE SEAT TRACK, RBL 22. BS 210 - 275 CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-40-01.

Part: FLOOR SUPPORT — CORRODED (BS 1269) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT BILGE AREA RIGHT SIDE, BS 1269 BETWEEN L28 - 29R CORRODED. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 5965790.

Part: SEAT TRACK — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

FLOOR STRUCTURE FORWARD WET AREA RIGHT SIDE, BS 200, RBL 44 - 46 SEAT TRACK CORRODED ON UPPER SURFACE, FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-10-03.

Part: WEB — CORRODED (BS 200-220) · airframe 43,323 hrs · 29,253 cycles

CABIN FORWARD WET AREA WEB, BS 200-220, RBL 26-50 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-01 AND DWG 9936535, REV CS.

Part: WEB — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

FORWARD CABIN FLOOR WEB, BS 200, LBL 6 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01.

Part: CHANNEL — CORRODED (BS 256) · airframe 43,323 hrs · 29,253 cycles

FORWARD PASSENGER COMPARTMENT, BS 256, LBL 33 CHANNEL CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-05 AND DWG 5930544, REV N.

Part: FITTING — CORRODED (BS 1370-1395) · airframe 43,323 hrs · 29,253 cycles

AFT CARGO COMPARTMENT RIGH SIDE BETWEEN, BS 1370 - 1395 L29R TERMINAL FITTING CORRODE. REPLACED IAW SRM 51-30-02.

Part: WEB — CORRODED (BS 195-200) · airframe 43,323 hrs · 29,253 cycles

CABIN FLOOR WEB FORWARD WET AREA RIGHT SIDE, BS 195 - 200, RBL 44 - 46 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01.

Part: WEB — CORRODED (BS 175-180) · airframe 43,323 hrs · 29,253 cycles

FLOOR WEB FORWARD WET AREA, RIGHT SIDE, BS 175-180, RBL 40-44. CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 984-1003) · airframe 43,323 hrs · 29,253 cycles

CABIN FLOOR SUPPORT, BS 984 - 1003 CUSP WEB CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW 51-42-00.

Part: WEB — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

FORWARD CABIN FLOOR WEB, BS 200, LBL 10 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-0001.

Part: CUSP WEB — CORRODED (BS 693-712) · airframe 43,323 hrs · 29,253 cycles

CABIN RIGHT SIDE, BS 693 -712, CUSP WEB CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-20-02.

Part: STRUCTURE — CORRODED (BS 180-200) · airframe 43,323 hrs · 29,253 cycles

FLOOR STRUCTURE FORWARD WET AREA, RIGHT SIDE, BS 180-200, RBL 11 - 44 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 232-256) · airframe 43,323 hrs · 29,253 cycles

FLOOR SUPPORT, BS 232-256, LBL 33 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-00-01 AND DWG 5930544.

Part: WEB — CORRODED (BS 160-200) · airframe 43,323 hrs · 29,253 cycles

FORWARD WEB , BS 160-200, X -54 TO X 54 CORRODED. REMOVED AND REPLACED IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 43,323 hrs · 29,253 cycles

FLOOR STRUCTURE, FORWARD WET AREA, RIGHT SIDE CHANNEL CORRODED, BS 180, RBL 44. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-00-01 AND DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 43,323 hrs · 29,253 cycles

FORWARD CABIN FLOOR SUPPORT CORRODED, BS 180, LBL 45. TASK# 53-211-01. FOUND TO BE OUT OF LIMITS. REPLACED THE FLOOR SUPPORT IAW DWG 9936534, REV RW.

Part: FLOOR SUPPORT — CRACKED · airframe 43,323 hrs · 29,253 cycles

FORWARD ENTRY DOOR FLOOR SUPPORT CRACKED, LBL 54. FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW DWG 9936534.

Part: SKIN — CRACKED (APU INLET DOOR) · airframe 43,323 hrs · 29,253 cycles

APU INLET DOOR SKIN IS CRACKED AT DOOR HINGE. INSTALLED REPAIR DOUBLER IAW SRM 52-00-01, 51-30-02 AND DWG 5916333.

Part: ANGLE — CORRODED (BS 160) · airframe 43,323 hrs · 29,253 cycles

FORWARD CABIN ANGLE CORRODED, BS 160, LBL 36. FOUND TO BE OUT OF LIMITS. REPLACED IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

CABIN FLOOR STRUCTURE FORWARD WET AREA , BS 200, RBL 44, FLOOR SUPPORT CHANNEL CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (FWD LAVATORY) · airframe 43,323 hrs · 29,253 cycles

FORWARD LAVATORY, BS 200 LB FLOOR SUPPORT CORRODED. TASK 53-211-01. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 43,323 hrs · 29,253 cycles

RIGHT FLOOR CHANNEL, BS 148-200, CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED FLOOR CHANNEL IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 43,323 hrs · 29,253 cycles

FORWARD FLOOR SUPPORT, BS 180, LBL 36, CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 43,323 hrs · 29,253 cycles

FORWARD LEFT FLOOR CHANNEL, BS 148-200, CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

FORWARD FLOOR CHANNEL, BS 200, LBL 8 CORRODED. FOUND TO BE OUT OF LIMITS. REPLACED IAW DWG 9936534, REV BW.

Part: SUPPORT CHANNEL — CORRODED (BS 180) · airframe 43,323 hrs · 29,253 cycles

FORWARD WET AREA SUPPORT CHANNEL CORRODED, BS 180, RBL 11. FOUND TO BE OUT OF LIMITS. REPLACED IAW DWG 9936534, REV BW.

Part: MOUNT — CORRODED (BS 160) · airframe 43,323 hrs · 29,253 cycles

GALLEY MOUNT FITTING CORRODED, BS 160, RBL 13. FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW DWG 9936534, BT.

Part: PAN — CRACKED (BS 1154) · airframe 43,323 hrs · 29,253 cycles

LEFT PASSENGER WINDOW PAN BS 1154, IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: SEAT TRACK — CORRODED · airframe 43,323 hrs · 29,253 cycles

SEAT TRACK BS 10-256, LBL 22 IS CORRODED.

Part: PAN — CRACKED (BS 1076) · airframe 43,323 hrs · 29,253 cycles

LEFT PASSENGER WINDOW PAN AT BS 1076 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1135) · airframe 43,323 hrs · 29,253 cycles

RIGHT PASSENGER WINDOW PAN IS CRACKED BS 1135. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1136-1155) · airframe 43,323 hrs · 29,253 cycles

RIGHT PASSENGER WINDOW PAN, 1136 - 1155 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1116) · airframe 43,323 hrs · 29,253 cycles

LEFT WINDOW PAN BS 1116 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1116) · airframe 43,323 hrs · 29,253 cycles

RIGHT PASSENGER WINDOW PAN BS 1116 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: SEAT TRACK — CORRODED (BS 210-275) · airframe 43,323 hrs · 29,253 cycles

SEAT TRACK, RBL 22, BETWEEN BS 210 - 275 IS CORRODED.

Part: PAN — CRACKED (BS 984) · airframe 43,323 hrs · 29,253 cycles

LEFT PASSENGER WINDOW PAN, BS 984 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1230) · airframe 43,323 hrs · 29,253 cycles

RIGHT PASSENGER WINDOW PAN, BS 1230 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: PAN — CRACKED (BS 1135) · airframe 43,323 hrs · 29,253 cycles

LEFT WINDOW PAN, BS 1135 IS CRACKED. REPAIRED IAW SRM 56-20-02.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 43,323 hrs · 29,253 cycles

FORWARD PASSENGER CABIN, BS 200 BL 0 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 9936534 AND SRM 51-30-02 AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (BS 148) · airframe 43,323 hrs · 29,253 cycles

CABIN FLOOR STRUCTURE FORWARD WET AREA RIGHT SIDE, BS 148, RBL 22 FLOOR SUPPORT CHANNEL CORRODED. 100% MATERIAL LOSS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 9936533.

Part: SUPPORT — WORN (VERTICAL STAB) · airframe 43,323 hrs · 29,253 cycles

VERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE BEARING SUPPORT HAS RADIAL PLAY AT BOTH ATTACH BOLTS. REMOVED AND REPLACED HINGE BEARING SUPPORT IAW DWG 5930608, REV AJ.

Part: CLAMP — BROKEN (TAILCONE) · airframe 41,900 hrs · 28,389 cycles

FORWARD CABLE RELEASE FOR TAILCONE SUPPORT CLAMP BROKE AND WORN. ACCOMPLISHED APPROVED TIME LIMITED REPAIR IAW ERA 541501-14 AND PS 900-5-1, NR 4.

Part: LONGERON SPLICE — NOT REPORTED (FUSELAGE) · airframe 40,737 hrs · 27,700 cycles

FUSELAGE, LONGERON L2L AND L2R, SPLICE REPAIR, STATION 1475537329-14MA.

Part: SLIDE — LOW PRESSURE (TAILCONE) · airframe 38,678 hrs · 26,379 cycles

TAIL CONE LIFE RAFT PRESSURE LOW. R & R TAILCONE SLIDE IAW AMDS CARD 2561-4643.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,522 hrs · 23,899 cycles

DURING SERVICE CHECK, MX FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE THROUGHOUT CABIN AND TAIL COMPARTMENT. RELAMPED LIGHTS AS REQUIRED. OPS CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 32,698 hrs · 22,895 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. FOUND LOWER EMERGENCY LIGHTS DISCONNECTED. RECONNECTED, OPERATION CHECKS NORMAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO INTERCOSTAL CORRODED 1206-1212. REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: FLOOR SUPPORT — BROKEN (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO T-BRACKET STA 1155 BROKEN BETWEEN RBL 16 AND LBL 16. REPLACED FLOOR SUPPORT PER SRM 51-30-02.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 PANEL 160SR SUPPORT FRAME CORRODED. REPAIR PER SRM 51-10-3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 WING TO BODY FAIRING 160SR LOWER SUPPORT CORRODED STA 1098 RBL 3. REPAIR PER SRM 53-00-01.

Part: PAN — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 FWD CARGO DOOR JAMB CORRODED STA 376-427. REPLACED DOOR PAN PER SRM 53-05 FIG 44.

Part: DOOR — CRACKED (LT MLG) · airframe 30,317 hrs · 21,676 cycles

HMV2 LT MLG DOOR AFT EDGE REPAIR CRACKED. REPLACED REPAIR PER SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 FLOOR SUPPORT CORRODED STA 788. REPLACED SUPPORT PER SRM 51-30-02.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 MID CARGO 655 L30 CORRODED. REPLACED SPLICE PER SRM 53-00-01.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 MID CARGO STA 655 L29L FASTENERS AND SPLICE CORRODED. REPLACED SPLICE AND FASTENERS PER SRM 53-00-01 51-30-00.

Part: FRAME — WORN (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT ASSY COMP FRAME 1437 LT WORN. REPAIR PER SRM 53-00-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT BILGE AREA STA 1231 HAS CORROSION ON FRAME. REPAIR PER SRM 53-10-02 FIG 3.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 INTERCOSTAL STA 826-845 CORRODED BETWEEN L27R AND L28R. REPLACED INTERCOSTAL PER SRM 51-30-02.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 L20R CRACKED STA 1060. REPAIR PER SRM 51-10-03 AND DRAWING SG09530021.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 30,317 hrs · 21,676 cycles

HMV2 RT MLG DOOR OUTER SKIN CRACKED. INSTALLED NEW REPAIR PER SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT FUSELAGE INTERNAL LT SIDE BETWEEN CANT 1531.604 AND 1542.019 AT STR L19 INTERCOSTAL CRACKED. REPAIR PER SRM 51-70-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 MID CARGO RT TIE DOWN RAIL CORRODED STA 522-845. REPLACED RAIL PER SRM 51-30-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 LT LONGERON 20L CRACKED STA 1060. REPAIR PER SRM 51-10-03 AND DRAWING SG09530021.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO L30 STA 1395-1379 CORRODED. REPAIR PER SRM 53-10-0.

Part: BEAM — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO L29R BEAM CORRODED. REPLACED BEAM PER SRM 51-30-05.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 EPC ACCESS PANEL LWR ATTACH BRACKET CORRODED. REPLACED BRACKET PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO TIE DOWN RAIL CORRODED STA 1146-1212 RT. REPLACED TIE DOWN RAIL PER SRM 51-30-01.

Part: SPLICE — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 STR 29L SPLICE AT STA 1136-1156 CORRODED. REPLACED SPLICE PER SRM 51-30-05.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT BILGE AREA 5 EACH INTERCOSTALS ABOVE STR 30 CORRODED AT STA 1274-1288 1288-1307 1326-1344 1269-1274, 1307-1326. REPLACED INTERCOSTALS 1274-1288, 1288-1307, 1307-1326, 1326-1344 PER SRM 51-30-05, INTERCOSTAL 1269-1274 FOUND WITHIN LIMITS PER SRM 53-00-01.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 FLOOR SUPPORT TIE DOWN RAIL IN AFT CARGO STA 1146-1064 CRACKED. REPLACE TIE DOWN TRACK PER SRM 51-30-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT BILGE SKIN SPLICE CORRODED STA 1241 26L-29R. REPLACED SPLICE PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 FLOOR SUPPORT CORRODED STA 1212 IN AFT CARGO. REPLACED SUPPORT PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO FLOOR SUPPORT CORRODED STA 1231. REPLACED FLOOR SUPPORT PER SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 AFT CARGO FLOOR SUPPORT CORRODED STA 1212-1218 RBL 8. REPLACED FLOOR SUPPORT PER SRM 51-30-02.

Part: SUPPORT ANGLE — CORRODED (RT MLG WW) · airframe 30,317 hrs · 21,676 cycles

HMV2 RT WHEEL WELL AFT OF DOOR HINGE SUPPORT ANGLE CORRODED. REPLACED ANGLE PER SRM 51-10-05.

Part: BEAM — CORRODED (CARGO BAY) · airframe 30,317 hrs · 21,676 cycles

HMV2 L29R CORRODED AT STA 1193-1202. REPLACED BEAM PER SRM 51-30-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,317 hrs · 21,676 cycles

HMV2 FRAME CORRODED STA 1212 L28L AND L28R. REPLACED NEW FRAME PER SRM 51-30-05.

Part: DOUBLER — CRACKED (RT MLG DOOR) · airframe 30,317 hrs · 21,676 cycles

HMV2 RT MLG DOOR INNER SURFACE O/B AFT CORNER REPAIR CRACKED. REPLACED DOUBLER PER SRM 51-10-05.

Part: SKIN — CRACKED (NR 1 INLET) · airframe 27,992 hrs · 19,969 cycles

CRACKS ON THE NR 1 ENGINE INLET COWL LIP SKIN (S/N 0216001).

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 25,118 hrs · 17,777 cycles

CRACKED AND BROKEN ON THE SKIN OF LT AND RT HORIZONTAL STABILIZER FAIRING REPAIRED PER MESSAGE 1-565796525-2

Part: CARGO TRACK — CORRODED (STA 579 & 598) · airframe 25,118 hrs · 17,777 cycles

CORROSION ON LOWER CARGO TRACK SPLICE BAR BETWEEN STA 579 AND STA 598 SRM 53-40-01, VOL I FIG 7.

Part: SUPPORT — CRACKED (VENTRAL STAIRWAY) · airframe 25,118 hrs · 17,777 cycles

CRACK ON LEFT CANTED SUPPORT OF VENTRAL STAIRWAY SHROUD SRM 51-70-01, VOL I FIG 1.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 25,118 hrs · 17,777 cycles

RT INBOARD FLAP VANE LOWER SKIN REPAIR SRM 57-20-05 VOL I FIG 5.

Part: SKIN — DENTED (BS 207-229) · airframe 25,119 hrs · 17,777 cycles

FUSELAGE SKIN, DENT DAMAGE REPAIR AT STA 207-229, L16-18 SRM 53-30-01 VOL I.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 23,339 hrs · 16,582 cycles

CRACK ON LT DORSAL FIN ATTACH ANGLE. REPAIRED PER MESSAGE 1-207926631-2.

Part: SKIN — DENTED (RT I/B FLAP) · airframe 22,273 hrs · 15,896 cycles

DENT ON LOWER SKIN OF RT INBOARD FLAP SRM 57-53-01 VOL I FIG 1.