N913DN

Part: UNKNOWN — ODOR (COCKPIT) · airframe 61,701 hrs · 34,075 cycles

ON DESCENT, PASSING THROUGH 15000; NOTED A BURNING OIL ODOR IN COCKPIT. IT CAME ON SUDDENLY AND IT WAS STRONG ENOUGH TO CONSIDER PUTTING ON OUR O2 MASKS. IT THEN QUICKLY DISSIPATED WHEN THE THROTTLES MOVED FORWARD OUT OF IDLE. /A T/S PER MD90 FIM 21-22. NO APU CONTAMINATION FOUND. NO OBVIOUS HYD LEAKS NOTED. BOROSCOPED #1 & 2 ENG #3 BEARING COMPT AND BLEED AIR DUCTS. NO OIL CONTAMINATION FOUND. INSPECTED L+R ACM INLET + OUTLETS. NO OIL CONTAMINATION. RAN PACK WITH ENGS + APU. NO ODORS NOTED. ALSO OPERATING RECIRC FAN DOES NOT CAUSE ODOR. PERFORMED HIGH PRESS DUCT BURNOUT IAW MD90 AMM 21-53. REPLACED COALESCER BAG IAW MD90 AMM 21-54. THIS COMPLIES WITH THE ATA 2172 SMOKE/ODOR ODI CK LIST. RAN PACKS WITH APU + ENGINE AGAIN. NO SMOKE, OIL SMELLS NOTED. OK FOR SVC.(6612144)

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 61,692 hrs · 34,067 cycles

SHIP 9213 RIGHT WHEEL WELL FWD DOOR JAMB CRACKED. REMOVED AND REPLACED RT FWD WHEEL WELL FRAME PER BOEING DWG 5930584 (6612127)

Part: DOOR — MISSING (LT WING) · airframe 59,738 hrs · 32,758 cycles

LEFT WING #7 LEADING EDGE SLAT TRACK CUTOUT DOOR MISSING. DEFERRED AS PER MD90 CDL 57-30-01 CDL/PLACARD INSTALLED DISPATCH APPROVED. (LP# 3788178)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,983 hrs · 32,273 cycles

EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK B5-232 IAW AMM 33-51-03 OPS CK GOOD. (LP#4253574)

Part: WEB — DAMAGED (NLG WW) · airframe 58,672 hrs · 32,075 cycles

STEERING ACTUATOR MADE CONTACT WITH LEFT NOSE GEAR SUPPORT WEB. REMOVED DAMAGE ON NLG SUPPORT WEB IAW SRM 53-90-01. PERFORMED DVI OF REPAIR AREA PER MD-90 SRM 53-90-01, NO OTHER DAMAGE NOTED. FABRICATED DOUBLERS & FILLER PER MD-90 SRM 53-90-01. INSTALLED DOUBLERS, FILLER AND TAPERED SHIM PER MD-90 SRM 53-90-01.

Part: CABLE — BURNED (DC POWER) · airframe 58,221 hrs · 31,804 cycles

DURING INSPECTION OF BATTERY CABLE CONNECTORS, BURNED BATTERY CABLE TERMINAL AND BURNED CONNECTOR WERE FOUND IAW AMDS 4944-4001, STEP 2. THE CONNECTOR ASSEMBLY WAS REPLACED SWPM 20-20-01. CABLE WAS FABRICATED IAW ERA 569217-14, REV ORIGINAL. THE CABLE WAS INSTALLED IAW ERA 569217-14, REV.ORIGINAL. FUNCTIONAL TEST OF THE EMERGENCY DC POWER SYSTEM WAS PERFORMED. TESTED OK. THE APU WAS STARTED AND DID NOT FOUND SIGNS OF OVERHEATING ON THE NEW INSTALLED BATTERY CABLE IAW ERA 569217-14, REV ORIGINAL.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 58,215 hrs · 31,801 cycles

CRACK FOUND IN THE VERTICAL STABILIZER SKIN NEAR THE RAM AIR INLET AREA, LT SIDE, ZFS 9. THE SKIN WAS REPAIRED IAW ERA 569140-14, REV ORIGINAL, AND ETI-90-18-027, REV 2.

Part: FORMER — CRACKED (VERTICAL STAB) · airframe 58,215 hrs · 31,801 cycles

A CRACK WAS FOUND ON THE VERTICAL STABILIZER FORMER AT ZFS 26.812. REPLACED THE FORMER IAW SRM 51-30-02, VOL. II, AND 51-30-05.

Part: ATTACH ANGLE — CRACKED (BS 1458-1486) · airframe 58,215 hrs · 31,801 cycles

CRACK IN THE LT & RT INTERNAL VERTICAL STABILIZER ATTACH ANGLES BS 1458 TO 1486. REPLACED THE ATTACH ANGLES IAW SRM 51-30-02, VOL II, AND 51-30-05.

Part: SKIN — DAMAGED (BS 465-522) · airframe 58,215 hrs · 31,801 cycles

DAMAGE FOUND ON THE FUSELAGE SKIN, BETWEEN BS 465 - 522. PERFORMED A PERMANENT REPAIR IAW ERA 569135-14, REV ORIGINAL, AND ETI-90-17-023, REV 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,215 hrs · 31,801 cycles

CRACK ON FUSELAGE SKIN AROUND AFT HINGE OF LT/AFT NLG DOOR. FUSELAGE SKIN AROUND AFT HINGE OF LT NLG DOOR WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-30-01 VOLUME 1 PARAGRAPH 14.

Part: SKIN — DAMAGED (BS 1328-1344) · corrosion level 2 · airframe 58,215 hrs · 31,801 cycles

CORROSION ON PRODUCTION DOUBLER CUT-OUT ON DRAIN BS 1328-1344 BETWEEN LONGERONS 26 - 27R. REPLACED IAW DWG:5936667, REV CD, AND SRM 51-30-02, VOL II.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 57,983 hrs · 31,653 cycles

AFT TAILCONE SLIDE WAS FOUND TO BE UNWRAPPING. REMOVED AND INSTALLED SLIDE IAW 2561-4643.

Part: STRUCTURE — NOT REPORTED (R1 DOOR) · airframe 55,272 hrs · 30,083 cycles

MAJOR REPAIR, R1 DOOR FINAL DRAWING REPAIR. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-20-02.

Part: LIGHT — BROKEN (AFT CABIN) · airframe 55,194 hrs · 30,046 cycles

TAIL COMPARTMENT EMERGENCY LIGHT LENS AND BASE BROKEN. INSTALLED A NEW LIGHT. OPERATION CHECKED GOOD.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 53,397 hrs · 28,965 cycles

ARCING OBSERVED ON CAPTAINS FORWARD WINDSHIELD. CIRCUIT BREAKER X24 PULLED PER QRH. CRACKS NOTED. REMOVED AND REPLACED WINDOW IAW MM. OPS CHECKED OK.

Part: CABLE — MISSING (TAILCONE) · airframe 53,069 hrs · 28,762 cycles

TAILCONE NITROGEN CYLINDER PULL CABLE MISSING. REPLACED CABLE IAW MM. AIRCRAFT OK FOR SERVICE.

Part: FRAME — CRACKED (BS 1520) · airframe 52,993 hrs · 28,718 cycles

SEVERAL CRACKS ON FRAME BS 1520 CANT BETWEEN LONGERON 1-11L, AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-02 AND 51-30-0. CRACK 11" IN LENGTH.

Part: HOUSING — WORN (DOOR HANDLE) · airframe 52,993 hrs · 28,718 cycles

WEAR ON MID CARGO COMPARTMENT DOOR HANDLE HOUSING. REPLACED IAW SRM 51-10-03.

Part: FRAME — CRACKED (BS 1520) · airframe 52,993 hrs · 28,718 cycles

CRACKED UPPER CAP OF FRAME, BS 1520 CANT AT 11 O'CLOCK POSITION ON AFT ACCESSORY COMPARTMENT. REPAIRED IAW ERA 546490-14, REV O AND ETI 90-16-018, REV 4.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 52,993 hrs · 28,718 cycles

CRACK WAS FOUND ON RT HORIZONTAL STABILIZER, REAR SPAR, AFT BARREL NUT HOLE. REPLACED IAW SRM 51-30-02 AND 51-30-05 AND DWG 90550002, REV B.

Part: STIFFENER — CRACKED (BS 1520) · airframe 52,993 hrs · 28,718 cycles

SEVERAL STIFFENERS CRACKED AT FRAME 1520 CANT AFT ACCESSORY COMPARTMENT. REPLACED FRAME IAW SRM 51-30-02 AND DWG 9953015.

Part: FRAME — CRACKED (BS 1520) · airframe 52,993 hrs · 28,718 cycles

CRACKED WEB FRAME, BS 1520 CANT. CANT WAS REPLACED IAW SRM 51-30-02, DWG 9953015 AND 51-30-05.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 52,993 hrs · 28,718 cycles

BORE ON CAP, BS X= 5.93 AND X= 13.21 HORIZONTAL STABILIZER OUT OF TOLERANCE. REPAIRED IAW ERA 546508-14AD, REV O.

Part: FRAME SPLICE — DAMAGED (BS 1520) · airframe 52,993 hrs · 28,718 cycles

DAMAGED SPLICE ON FRAME, BS 1520. FABRICATED AND INSTALLED NEW SPLICE IAW DWG 9953015.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 52,993 hrs · 28,718 cycles

HORIZONTAL STABILIZER HARDWARE ATTACH POINTS CORRODED. REPLACED IAW AMM 55-10-00.

Part: SKIN — DAMAGED (BS 206) · airframe 52,993 hrs · 28,718 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 206 BETWEEN LONGERON 1R AND 2R. REPAIRED IAW SRM 53-31-02, 51-30-03 AND 51-10-05.

Part: SKIN — CRACKED (BS 1542) · airframe 52,993 hrs · 28,718 cycles

CRACK ON FUSELAGE SKIN , BS 1542 CANT BETWEEN LONGERONS 3 TO 5L. REPAIRED IAW SRM 53-00-01.

Part: INTERCOSTAL — WORN (CARGO BAY) · airframe 52,993 hrs · 28,718 cycles

WORN INTERCOSTALS MID CARGO COMPARTMENT, BETWEEN BERM 1 AND 2. REPLACED IAW SRM 51-30-05, 51-10-01, 51-10-02, AND DWG 9957664, REV N.

Part: DOUBLER — WORN · airframe 52,993 hrs · 28,718 cycles

WEAR ON REPAIR DOUBLER OF GUST LOCK CUTOUT AT L1 DOOR. DOUBLER WAS REPLACED IAW ERA 413167-14, REV O.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,993 hrs · 28,718 cycles

EXCESSIVE DENTS ON EXTERNAL SKIN BETWEEN BEAMS 4 AND 5 AT FORWARD CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02.

Part: INTERCOSTAL — CRACKED (MLG DOOR FRAME) · airframe 52,993 hrs · 28,718 cycles

CRACK ON INTERCOSTAL ON FORWARD DOOR JAMB AT LT MLG WHEEL WELL AREA, JUST BELOW HYDRAULIC GROUND SERVICE. REPAIRED IAW SRM 51-30-02 AND 51-30-005 AND DWG 5930584.

Part: HINGE — SCRATCHED (RT ELEVATOR) · airframe 52,993 hrs · 28,718 cycles

SCRATCHES ON RT ELEVATOR ATTACH POINT BUSHING HINGE, NR 2, 3, 4 AND 5. REPLACED IAW MM AND PS 900-1-2-1.

Part: ANGLE — WORN (RT OVERWING) · airframe 52,993 hrs · 28,718 cycles

WEAR ON ANGLE CLIP ON RT FORWARD OVERWING, EMERGENCY EXIT DOOR JAMB, BS 902. R & R IAW SRM 51-30-08.

Part: BRAKE — FIRE (MLG) · airframe 52,538 hrs · 28,455 cycles

AFTER LANDING THE NR 3 MLG BRAKE WAS SHOWING HOT. MLG NR 1, LOW BRAKE 250 DEGREES. NR 2, LT BRAKE 270, NR 3, RT BRAKE 510 DEGREES. NR 4, RO BRAKE 360 DEGREES. UPON WALK AROUND FLAMES WERE OBSERVED FROM MLG NR 3, RT BRAKE. PORTABLE FIRE EXTINGUISHER USED. FIRE DEPARTMENT RESPONDED. RT ENGINE THRUST REVERSER ON MEL SINCE 3/10. REPLACED NR 3, RT AND NR 4, RO MLG TIRE AND WHEEL ASSYS. REPLACED NR 3, RT MLG BRAKE IAW AACU BITE REPLACED IBCV 1 AND RT A/S TRANSDUCER. PERFORMED LOCK WHEEL AND SPIN TEST AND HIGH ENERGY STOP INSPECTION. ALL CHECKS GOOD.

Part: PUMP — ODOR (LAVATORY) · airframe 51,667 hrs · 27,901 cycles

AT ARRIVAL TO GATE, REPORT OF STRONG CHEMICAL BURNING ODOR. MAINTENANCE CONFIRMED ELECTRICAL ODOR IN FORWARD HALF OF CABIN. R & R RELAYS R2-528 AND R2-529 DUE TO SIGNS OF HEAT DAMAGE. CONTINUED TROUBLESHOOTING ODOR TO ROWS 20-22 CDE. FOUND POTABLE WATER AUXILIARY PUMP WITH BURNED ODOR. R & R AUXILIARY PUMP IAW MM. OPS CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,424 hrs · 26,538 cycles

MID CABIN CEILING EMERGENCY EXIT SIGN IS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: RELEASE CABLE — CORRODED (TAILCONE) · airframe 47,602 hrs · 25,381 cycles

TAILCONE RELEASE CABLE TERMINAL CORRODED. R & R TAIL CONE RELEASE CABLE. OPERATION CHECKED IAW AMDS 53-52-7116.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 47,602 hrs · 25,381 cycles

RIGHT FIXED VANE INBD HAS PUNCTURE AND A GOUGE. SANDED, CLEANED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-02 AND 59-20-05.

Part: SKIN — CRACKED (BS 1520) · airframe 47,602 hrs · 25,381 cycles

AFT ACCESSORY COMPARTMENT AT BS 1520 INBD SIDE OF LONGERON 2R SKIN DOUBLER CRACKED. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-03.

Part: WEB — CRACKED (BS 1520) · airframe 47,602 hrs · 25,381 cycles

AFT ACCESSORY COMPARTMENT AT BS 1520 WEB CRACKED. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR IAW ERA 524972-14.

Part: STOP FITTING — WORN (CARGO DOOR) · airframe 47,602 hrs · 25,381 cycles

AFT CARGO DOOR LOWER AFT STOP FITTING IS WORN AND HAS BARE METAL. R & R LOWER STOP FITTING ON AFT CARGO DOOR IAW SRM 51-30-02.

Part: FRAME — DAMAGED (BS 1344) · airframe 47,602 hrs · 25,381 cycles

AFT CARGO FRAME BS 1344, LONGERON 28L IS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-02.

Part: STRUCTURE — CORRODED (BS 1364) · airframe 47,601 hrs · 25,380 cycles

BS 1364, LONERON 29R CORRODED WHERE FRAME ATTACH ANGLES AND SKIN JOINT. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER IAW SRM 51-10-03.

Part: FORMER — CORRODED · airframe 47,601 hrs · 25,380 cycles

FORMER CORRODED FROM LONGERON 29L-29R. REMOVED CORROSION FROM L28L - 29R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER IAW SRM 53-00-01, 51-30-02 AND 51-30-05.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 47,601 hrs · 25,380 cycles

AFT LOWER CARGO DOOR FRAME DOUBLER HAS SURFACE CORROSION, REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R HEADER BEAM IAW DWG 5930483, REV AR.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 47,601 hrs · 25,380 cycles

CORROSION ON LONGERON 28L BETWEEN BS 1344-1364. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW LONGERON IAW DWG 5936667, REV CD.

Part: FINGER DOUBLER — CRACKED (BS 1288) · airframe 47,601 hrs · 25,380 cycles

FINGER DOUBLER LONGERON 26L BS 1288 IN AFT CARGO CRACKED. REMOVED, FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DWG 5936667, REV CD.

Part: LONGERON — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY BAY HAS CORROSION ON LONGERON 28L, BS 1395. FOUND OUT OF LIMITS. INSTALLED NEW LONGERON IAW SRM 53-00-01 AND DWG 5936667, REV CD.

Part: FRAME — CRACKED (BS 1542) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY COMPARTMENT, RIGHT HAND SIDE, AT CANT FRAME 1542 LOWER END CRACKED.

Part: SKIN — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY BAY CORROSION AT BS 1395, LONGERON 29L SKIN. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW DWG# 5936667, REV CD.

Part: STRUCTURE — CORRODED (BS 1344-1364) · airframe 47,601 hrs · 25,380 cycles

BS 1344-1364 S29-30L CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION IAW SRM 51-10-02 AND 53-10-01.

Part: LONGERON — CORRODED (BS 1350-1375) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO BAY LONGERON 26L CORRODED BETWEEN BS 1350-1375. REMOVED AND REPLACED AND INSTALLED NEW LONGERON IAW SRM 53-00-01, 51-30-02, 51-30-05 & DWG 5936667.

Part: FITTING — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO BAY CARGO FITTING CORRODED BS 1395, L26L. R & R CARGO FITTING IAW SRM 51-10-03, 51-30-05, 53-00-01 AND DWG 5936667, REV BW.

Part: SKIN — CORRODED (BS 1136-1155) · airframe 47,601 hrs · 25,380 cycles

EXTERNAL LOWER FUSELAGE AT BS 1136-1155 FROM L28-30L HAS SOME CORRODED SPOTS IN SKIN. REMOVED CORROSION. TWO AREAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-01.

Part: FRAME — CRACKED (BS 1484) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY COMPARTMENT AT FRAME BS 1484, S2R CRACKED. REPAIRED IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 1288) · airframe 47,601 hrs · 25,380 cycles

CORROSION BETWEEN S26-30L AT BS 1288 FRAME. REMOVED CORROSION. FABRICATED NEW FRAME SECTION AND SPLICE IAW SRM 53-10-02 AND 51-10-03.

Part: FRAME — CRACKED (BS 1486) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY BAY AT BS 1486 FRAME, LONGERON 1 CRACKED. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED IAW SRM 51-30-05 AND DWG 9911840, RV CR & DC.

Part: STRAP — CORRODED (BS 1328) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO L23L FRAME BS 1328 STRAP HAS CORROSION. REMOVED, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-30-02 AND DWG 5911423, REV CD.

Part: LONGERON SPLICE — CORRODED (BS 1350) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO LONGERON SPLICE L30 AT BS 1350 IS CORRODED. REMOVED, FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 51-30-02 AND 51-30-05.

Part: FRAME — CRACKED (BS 1520) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY COMPARMENT AT CANT FRAME 1520, L17R DOUBLER STRAP CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-30-01, 51-10-05 AND 51-10-03.

Part: STRUCTURE — GOUGED (DOOR FRAME) · airframe 47,601 hrs · 25,380 cycles

L1 DOOR GUST LOCK LATCH POINT ON BS 133 PANE IS GOUGED OVER PREVIOUS REPAIR. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-30-02 AND ERA 38169-14.

Part: STRUCTURE — CORRODED (SERVICE PANEL) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY COMPARTMENT, LAVATORY SERVICE PANEL INTERIOR AREA CORRODED ALL AROUND. REMOVED CORROSION. FABRICATED AND INSTALLED NEW DOUBLER SUPPORT IAW DWG 5965767, REV I AND ERA 524969-14, REV O.

Part: FITTING — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO BAY, CORROSION AT BS 1395 L27L. REMOVED CORROSION, FABRICATED AND INSTALLED NEW END FITTING IAW DWG 5936667, REV CD.

Part: FLOOR SUPPORT — CORRODED (BS 1193-1276) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO BS 1193-1276, L29R, FLOOR SUPPORT TEE IS CRACKED AND HAS HEAVY CORROSION. REMOVED FLOOR SUPPORT. FABRICATED AND INSTALLED NEW TEE IAW SRM 51-20-05, 51-30-02 AND 51-30-01.

Part: LONGERON — CORRODED (BS 1350-1375) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY BAY LAVATORY SERVICE PANEL INTERIOR HAS CORROSION ON RT LONGERON 25L BETWEEN BS 1350-1375.

Part: SUPPORT — CRACKED (L1 DOOR) · airframe 47,601 hrs · 25,380 cycles

L1 DOOR INTERNAL STRUCTURE, CRACKED IN CORNER OF HORIZONTAL SUPPORT. REMOVED CRACKED SUPPORTAND INSTALLED NEW IAW 9955752, REV K, SRM 51-30-02 AND 51-30-05.

Part: FRAME — CORRODED (BS 522) · airframe 47,601 hrs · 25,380 cycles

CENTER CARGO BAY AT BS 522, L28L-28R LOWER SIDE OF FRAME CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-02.

Part: FITTING — GOUGED (RT MLG UPLOCK) · airframe 47,601 hrs · 25,380 cycles

RIGHT MLG UPLOCK LATCH CRANK FITTING IS GOUGED. BLENDED OUT GOUGES IAW ERA 524960-14, REV O.

Part: SLAT TRACK — DENTED (NR 5 SLAT) · airframe 47,601 hrs · 25,380 cycles

LEFT HAND OUTER WING FRONT SPAR, AFT FACE, NR 5 SLAT INBOARD SLAT TRACK HAS A DENT. TREATED AND PRIMED AND PERFORMED SLAT OPERATION CHECK IAW ERA 524971-14, REV - 0. (LP# 1430203_

Part: ARM — GOUGED (UPLOCK SENSOR) · airframe 47,601 hrs · 25,380 cycles

LEFT WHEEL WELL ARM FOR UPLOCK SENSOR SUPPORT IS GOUGED 85-03. BLEND OUT GOUGES IAW ERA 524960-14, REV O.

Part: FITTING — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO BAY CORROSION AT BS 1395, LONGERON 25L. R & R AFT CARGO END FITTING IAW SRM 51-10-03.

Part: WEB — CORRODED (BS 160) · airframe 47,601 hrs · 25,380 cycles

BS 160, RBL 24-44 FLOOR WEB CORRODED. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-00-01.

Part: WEB — CORRODED (BS 160-200) · airframe 47,601 hrs · 25,380 cycles

MAIN CABIN FWD WET AREA WEB BS 160-200, BL 0-LBL 6 HAS CORROSION. CUTOUT DAMAGED SECTION. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-00-01.

Part: DOOR FRAME — CORRODED (BS 698-740) · airframe 47,601 hrs · 25,380 cycles

CENTER LOWER CARGO COMPARTMENT DOOR JAMB, REPAIR DOUBLER HAS SURFACE CORROSION FROM STA 698-740. TASK 53-122-02. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER ON CENTER LOWER CARGO COMPARTMENT DOOR JAMB IAW SRM 53-60-02.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 47,601 hrs · 25,380 cycles

BS 731-750 RT CUSP WEB CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 864-963) · airframe 47,601 hrs · 25,380 cycles

CUSP WEB RT SIDE, BS 864-963 HAS CORROSION ON BOTTOM SIDE. CUTOUT DAMAGE SECTION OF CUSP WEB. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 47,601 hrs · 25,380 cycles

BS 200, BL 0 - RBL 44 FLOORBEAM CORRODED. FABRICATED AND INSTALLED NEW FLOORBEAM ANGLE IAW DWG 9936534 AND SRM 51-10-03.

Part: FRAME — CORRODED (BS 1520) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY COMPARTMENT AT CANT FRAME BS 1520, LOWER END CORRODED LT SIDE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW LOWER CAP SECTION AND DOUBLER IAW SRM 53-10-02 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 280) · airframe 47,601 hrs · 25,380 cycles

BS 280, LT CUSP WEB HAS A HOLE. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-20-02, FIG 22, 51-10-03, PARA 14 AND 32, AND 51-10-00-370-801.

Part: SEAT TRACK — GOUGED (BS 1079) · airframe 47,601 hrs · 25,380 cycles

CABIN SEAT TRACK, BS 1079, RBL 24 HAS GOUGES. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-20-01, 51-10-05, 51-30-01, 51-30-05 AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 47,601 hrs · 25,380 cycles

MAIN CABIN FORWARD WET AREA FLOOR SUPPORT AT BS 160 - 200, RBL 6 IS HEAVILY CORRODED. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-03 AND DWG 53932140.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 47,601 hrs · 25,380 cycles

FLOORBEAM AT BS 180, CORRODED, LBL 20-44. REMOVED DAMAGED FLOORBEAM. FABRICATED AND INSTALLED NEW FLOORBEAM IAW DWG 9936534.

Part: CUSP WEB — CORRODED (BS 945) · airframe 47,601 hrs · 25,380 cycles

RT CUSP WEB, HAS CORROSION ON TOP AT BS 945. FOUND TO BE OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-10-05.

Part: FRAME — CRACKED (BS 1486) · airframe 47,601 hrs · 25,380 cycles

AFT ACCESSORY BAY BS 1486, LOWER END OF FRAME CRACKED RT SIDE. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02.

Part: DOUBLER — CORRODED (BS 1395) · airframe 47,601 hrs · 25,380 cycles

AFT CARGO JACK POINT DOUBLER AT BS 1395, LBL 2 IS HEAVILY CORRODED. REMOVED JACK POINT FITTING SUPPORT. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-10-03 AND DWG 9915561, REV CC.

Part: CUSP WEB — CORRODED (BS 845-864) · airframe 47,601 hrs · 25,380 cycles

BS 845-864, LT CUSP WEB HAS CORROSION. REMOVED, FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-05 AND 51-00-02.

Part: BULKHEAD — CORRODED · airframe 47,601 hrs · 25,380 cycles

AFT PRESSURE BULKHEAD, FORWARD FACE, BOTTOM SIDE CORRODED SKIN, TEE ANGLE LOWER END TRIANGLAR PLATE AT BL0, BETWEEN L29L-29R. REMOVED AFT BULKHEAD FORWARD FACE. FABRICATED AND INSTALLED DOUBLER AND TEE ANGLE IAW DWG 5910130, REV EG.

Part: SEAT TRACK — GOUGED (BS 1360) · airframe 47,601 hrs · 25,380 cycles

CABIN SEAT TRACK, BS 1360, LBL 24 GOUGED. REMOVED DAMAGE. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-01, 53-20-01, AND 51-10-05.

Part: WEB — CORRODED (BS 180) · airframe 47,601 hrs · 25,380 cycles

BS 180, WEB BL 0 - LBL 44 CORRODED. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01 AND 51-10-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,367 hrs · 24,039 cycles

FUSELAGE SKIN SPLICE AND DORSAL FIN INNER ATTACH ANGLE FOUND CRACKED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,010 hrs · 23,848 cycles

DURING CHECK, TAILCONE EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,690 hrs · 23,680 cycles

CORROSION FOUND UNDER LOWER AFT VHF ANTENNA. REMOVED NR 3 LOWER ANNTENNA, BONDING CHECK COMPLETED IAW SWPM. ERA 511497-14, REV O.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 43,082 hrs · 22,789 cycles

RIGHT FORWARD GEAR DOOR FRAME HAS 2.5 INCH CRACK LOCATED JUST BELOW DOOR CLOSED PROXIMITY SENSOR. REMOVED AND REPLACED FRAME PER SRM 53-60-02 AND 51-00-00.

Part: SKIN — CRACKED (BS 1486) · airframe 45,338 hrs · 24,023 cycles

FUSELAGE SKIN SPLICE AND DORSAL FIN INNER ATTACH ANGLE, BS 1486 L2R FOUND CRACKED. MAJOR REPAIR.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,721 hrs · 22,599 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND ONLY HALF OF THE EMERGENCY LIGHTS OPERATING. REMOVED AND REPLACED SWITCH S1-177. OPERATION CHECKS NORMAL.

Part: BOTTLE — DISCHARGED (EVAC SLIDE) · airframe 42,391 hrs · 22,420 cycles

DURING DOOR CLOSING, FLIGHT CREW DISCOVERED MAIN ENTRY DOOR SLIDE NITROGEN BOTTLE LOST PRESSURE SLIDE DID NOT DEPLOY. MAINTENANCE REMOVED AND REPLACED LEFT MAIN DOOR SLIDE PER OPN 7008 AND AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,633 hrs · 22,073 cycles

DURING CHECK, MAINTENANCE FOUND RIGHT TAIL CONE EMERGENCY LIGHT, ABOVE THE SLIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY B5-239. OPERATION CHECKS OKAY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,691 hrs · 21,157 cycles

FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT STA 731 BETWEEN L1 AND L2R, ACCOMPLISHED ER/A 491834-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,691 hrs · 21,157 cycles

LIGHTNING STRIKE DAMAGE AT STA 448 L1 AND L2R, ACCOMPLISHED ER/A 491856-14 REVISION 0.

Part: TAIL CONE — DAMAGED · airframe 39,687 hrs · 21,156 cycles

TAIL CONE T/E LWR END CAP LIGHTNING DAMAGE.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,368 hrs · 20,119 cycles

ON FLIGHT CHECK MX FOUND EMERGENCY TRACK LIGHT INOPERATIVE, ROW 22. RE-LAMPED AND NO HELP ON 5-16-10 DCA MX REPLACED WIRING HARNESS. OPS CHECK OF LIGHT NOW CHECKS OK.

Part: CONTROL UNIT — FAILED (E/E) · airframe 34,886 hrs · 18,671 cycles

ELEVATOR SPLIT MESSAGE ON EOAP FOR LOSS OF LEFT ENG GENERATOR. TROUBLESHOT PER MD-90 TSM 27-30 PAGE 5. DUE TO LEFT GENERATOR POWER FAULT SUSPECT ACS SYSTEM LOST LEFT ELEVATOR POSITION INDICATION CAUSING FAULT. CLEARED ELEVATOR SPLIT MESSAGE THROUGH MCDU. MESSAGE DID NOT COME BACK. REPLACED ACU PER AMM. ACS R-T-S PASSED. ELEVATORS FAIRED NORMALLY AND THERE IS NO ELEVATOR POSITION SENSOR SPLIT INDICATION THROUGH MCD SENSOR VALUES.

Part: DOOR FRAME — CORRODED (AIRSTAIR) · airframe 32,522 hrs · 17,288 cycles

AFTER REMOVAL OF WEATHER SEAL, FOUND VENTRAL STAIRWAY DOOR JAMB CORRODED OUT OF LIMITS, LOWER SECTION AT FLOOR LEVEL. REPAIRED STAIRWAY DOOR JAMB, IAW DELTA ER/A 468148-14 REV ORIG.

Part: INTERCOSTAL — BROKEN (BS 1360) · airframe 32,522 hrs · 17,288 cycles

INTERCOSTAL AT FS 1360 BLO TO HAVE A SECTION OF UPPER FLANGE BROKEN OFF. REPAIRED INTERCOSTAL, IAW DELTA ER/A 12670 DATE 5/19/08 REV I/R.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 32,522 hrs · 17,288 cycles

MIDPIT DOOR JAMB LWR SURFACE HAS CORROSION ON LWR SURFACE AT FASTENER HOLES. REPAIRED MIDPIT DOOR JAMB, IAW DELTA ER/A 468150-14, REV ORIG DATE ISSUED 05MAY08 VIA AAR EA 12661 REV I/R DATE ISSUED 05/05/08.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 32,522 hrs · 17,288 cycles

AFT CARGO BAY LOWER DOOR JAMB BEAM CORRODED BETWEEN STA 1212 AND 1269 LONGERON 28R. REPAIRED AFT CARGO LOWER JAMB BEAM, IAW DELTA ER/A 468149-14, REV ORIG DATED 05MAY08.

Part: SKIN — CRACKED (FLAP VANE) · airframe 32,522 hrs · 17,288 cycles

LEFT WING O/B FLAP CENTER FIXED VANE UPPER SURFACE IS CRACKED. REMOVED & REPLACED LT O/B CENTER FIXED VANE, IAW MD90 AMM 27-50-02.

Part: SKIN — DENTED (FLAP VANE) · airframe 32,522 hrs · 17,288 cycles

LEFT WING I/B FIXED VANE LOWER SURFACE HAS SEVERAL SMALL DINGS. REPAIRED DENT DAMAGE TO LOWER SURFACE OF LT WING I/B FIXED VANE, IAW MD90 SRM 57-20-05D, PARA 14, FIG 21.

Part: FRAME — CORRODED (AFT CARGO) · airframe 32,522 hrs · 17,288 cycles

AFT CARGO BAY FRAME CORRODED AFT SIDE STA 1364 BETWEEN LONG 27L AND 28R. REPAIRED FRAME, IAW MD90 53-10-02.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

AFT CARGO BAY LONG 27L CORRODED AROUND FASTENERS AND DRAIN HOLES STA 1344-1364. REPAIRED LONG, IAW MD90 SRM 53-10-01, FIG 7 VOL 1.

Part: SKIN — DENTED (BS 237) · airframe 32,522 hrs · 17,288 cycles

PRIOR TO FIRST FLT OF THE DAY, FOUND FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERON 18L AND 19L AND REPAIR ID TAG MISSING. REPAIRED DAMAGED AREA, IAW MD80 SRM 53-04D, FIG 12 B AND MD90 SRM VOL 1, 51-00-01.

Part: SEAT TRACK — CORRODED (BS 1204) · airframe 32,522 hrs · 17,288 cycles

SEAT TRACK EXFOLIATED AT FS 1204 LBL 22. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6.

Part: CUSP WEB — CORRODED (BS 674-769) · airframe 32,522 hrs · 17,288 cycles

RIGHT CUSP WEB CORRODED ON DOUBLER FROM STA 674-769. REPLACED CUSP WEB, IAW MD90 SRM 51-10-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

RIGHT CUSP WEB CORRODED AT FIRST LIGHTNING HOLE AFT OF STA 465 ON UPPER AND LWR SURFACE. WEB WAS FOUND TO BE OUT OF LIMITS, IAW MD90 SRM 53-00-01, FIG 3. WORK TO BE ACCOMPLISHED ON N/R 1003732 2400/0215 S/N 109915.

Part: SEAT TRACK — GOUGED (BS 674-760) · airframe 32,522 hrs · 17,288 cycles

CABIN SEAT TRACK FS 674-760 RBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL 1.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 32,522 hrs · 17,288 cycles

RIGHT CUSP WEB CORRODED ON UPPER AND LWR SURFACE FROM STA 446-465 RT. REMOVED AND REPLACED CUSP WEB, IAW MD90 SRM 51-30-01, 51-30-02, 51-30-05 AND DELTA ER/A 398181-14MA DATED 9-18-02 REV 1, STEP NR 9 FIG NR 5.

Part: WEB — CORRODED (BS 200) · airframe 32,522 hrs · 17,288 cycles

FLOOR MEMBRANE CORRODED FS 200 RBL 48-54. REPAIRED FLOOR MEMBRANE, IAW MD90 SRM 51-30-02, VOL 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

RIGHT CUSP WEB CORRODED ON LWR SURFACE BETWEEN STA 484-503 AT CENTER LIGHTENING HOLE. WEB FOUND TO BE OUT OF LIMITS, IAW MD90 SRM 53-00-01, FIG 3. WORK TO BE ACCOMPLISHED ON N/R 1003732 2400/0215.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

FOUND CRACK AFT OF STA 1494 BETWEEN LONGERONS L-1 AND L-2. REMOVED AND REPLACED BRACKET, IAW MD90 SRM 51-30-05.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

CABIN SEAT TRACK FS 1136-1174 RBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL I.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

LT STA 1360 CUSP WEB CRACKED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01, FIG 2.

Part: CUSP WEB — CORRODED (BS 579-598) · airframe 32,522 hrs · 17,288 cycles

RIGHT CUSP WEB CORRODED ON LOWER SURFACE BETWEEN STA 579-598 AT LIGHTNING HOLES. REPAIRED RT CUSP WEB STA 579-598, IAW DELTA ER/A 398191-14MA REV ORIG 09-18-02.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

CABIN SEAT TRACK FS 845-879 LBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL I.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 32,522 hrs · 17,288 cycles

AFT CARGO BAY RT CARGO TRACK CORRODED AROUND FASTENER STA 1269 TO 1307. REMOVED AND REPLACED TRACK, IAW MD90 SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

LT CUSP WEB HAS CORROSION AT LIGHT WING HOLE AFT OF STA 560 ON UPPER AND LOWER SURFACE. REPAIRED CUSP WEB, IAW MD80 SRM 53-05D, FIG 827D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

LT CUSP WEB HAS CORROSION ON UPPER SURFACE AT STA 541-560. REPAIRED CUSP WEB, IAW MD80 SRM 53-05D, FIG 827D.

Part: CUSP WEB — CORRODED (BS 1117-1136) · airframe 32,522 hrs · 17,288 cycles

LEFT CUSP WEB HAS CORROSION ON FWD END BETWEEN STA 1117 TO 1136. BLENDED CORROSION ON LEFT CUSP WEB STA 1117 TO 1136, FOUND TO BE OUT OF LIMITS, IAW MD90 SRM 53-00-01, FIG3. WORK WILL BE ACCOMPLISHED ON W/O S/N 109897 1003732 2400/0205.

Part: SEAT TRACK — GOUGED (BS 1136-1174) · airframe 32,522 hrs · 17,288 cycles

CABIN SEAT TRACK FS 1136-1174 RBL 54 OUT OF LIMITS. REPAIRED SEAT, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — GOUGED (BS 1326) · airframe 32,522 hrs · 17,288 cycles

CABIN SEAT TRACK FS 1326-LBL 22 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6 VOL I.

Part: CUSP WEB — DAMAGED (BS 560) · airframe 32,522 hrs · 17,288 cycles

LT CUSP WEB AT STA 560 O/B SEAT TRACK HAS A HOLE IN WEB ON O/B SIDE OF TRACK BELOW CLIP NUT. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01, FIG 6.

Part: SHEAR TIE — CRACKED (BS 1458 L14-15) · airframe 32,522 hrs · 17,288 cycles

FOUND CRACKED BRACKET AT STA. 1458 BETWEEN LONGERONS L14 AND L15. REMOVED, FABRICATED AND INSTALLED BRACKET, IAW MD90 SRM 51-10-05, VOL.II.

Part: CUSP WEB — CORRODED (BS 1079-1098) · airframe 32,522 hrs · 17,288 cycles

LT CUSP WEB HAS CORROSION ON O/B AFGT SURFACE BETWEEN STA 1079-1098. REMOVED AND REPLACED LT CUSP WEB STA 1079-1136 LBL 44.5.TO 58, IAW MD9 SRM 51-30-02, SRM 51-30-01.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 32,522 hrs · 17,288 cycles

FOUND CABIN SEAT TRACK FS 221 LBL 44 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6 VOL I.

Part: CUSP WEB — CORRODED (BS 465) · airframe 32,522 hrs · 17,288 cycles

LEFT CUSP WEB HAS CORROSION ON UPPER SURFACE AT FIRST LIGHTNING HOLE FWD OF STA. 465. REPAIRED CUSP WEB ON AAR N/R 1003732-2600-0194 S/N 109886.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

FOUND RIGHT CUSP WEB CORRODED ON SURFACE BETWEEN STA 636-655. REMOVED AND REPLACED RIGHT CUSP WEB BETWEEN STA 636-655, IAW MD90 SRM 51-10-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

UPON REMOVAL OF SEAT TRACK, FOUND CUSP WEB CRACKED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

AFT CARGO BAY FRAME AFT SIDE CORRODED STA 1328 FROM LONGERON 29L TO 28R. REPAIRED FRAME AT STA 1328, IAW MD90 SRM 53-10-02 FIG 2.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 32,522 hrs · 17,288 cycles

FWD CARGO DOOR CUTOUT LOWER JAMB CORRODED FS 370 TO 427. REPAIRED FWD CARGO DOOR JAMB, IAW MD80 SRM.

Part: LANYARD — OUT OF ADJUST (AFT STAIR SLIDE) · airframe 29,997 hrs · 15,899 cycles

WHEN TAILCONE INADVERTENTLY DEPLOYED SLIDE DID NOT DEPLOY. FOUND THAT ONE OF THE FLOOR MOUNTED ATTACH POINTS FOR THE LANYARD WAS INCORRECTLY ADJUSTED. ADJUSTED ATTACH POINT AS REQUIRED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 27,851 hrs · 14,689 cycles

CEILING EMERGENCY EXIT LIGHTS WILL NOT TURN ON WHEN SELECTED STARTING AT ROW 38 TO AFT LAVS. FOUND POWER SUPPLY B5-237 INOP STA 1393 R&R B5-237 OPS NORMAL.

Part: STARTER — BURNED (APU) · airframe 27,415 hrs · 14,422 cycles

FOUND APU STARTER AND HARNESS BURNED DURING START. REPLACED APU STARTER AND HARNESS ASSEMBLY AND R2-63 START RELAY PER M/M. NOW CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 27,415 hrs · 14,422 cycles

ON APPROACH INTO PHX, LOST OIL PRESSURE ZERO INDICATION WITH LOW OIL PRESSURE MESSAGE ON EOAP WITH BOTH OIL PRESSURE CAUTION AND WARNING LTS ILLUMINATED. ENGINE SHUTDOWN ACCOMPLISHED PER QRH. OIL TEMP AND ALL OTHER PARAMETERS WERE NORMAL PRIOR TO SHUTDOWN. NO OIL PRESSURE INDICATED DURING WINDMILL PERIOD. CKD OIL LEVEL AT TANK FOUND FULL PER WINDMILL INSP MM. REMOVED OIL ENG OIL SYS CHIP DETECTORS AND MAIN AND SCAVENGE OIL FILTER ELEMENTS FOR INSP NO METALS FOUND, ALL MCD AND BOTH FILTERS REINSTALLED BUT REQ PACKING. REPLACEMENT AND LEAK CK REPLACED ENG INSTEAD.

Part: GUIDE ARM — OUT OF ALIGNMENT (PAX DOOR) · airframe 26,075 hrs · 13,676 cycles

FLOW LIGHT ILLUMINATED ON CLIMBOUT. GOOD FLOW ON BOTH PACKS FLT ATTENDANT REPORTED LOUD NOISE AT 2 LEFT DOOR. MAX CABIN ALT 9000. CABIN PRESSURE 2 PSID. FOUND DOOR GUIDE ARM ON WRONG SIDE OF ROLLER MECHANISM AND GUIDE ROLLERS NOT SEATED IN GUIDES. LUBRICATED DOOR GUIDE MECHANISM AS PRECAUTIONARY, EXERCISED DOOR SEVERAL TIMES. CHECKS GOOD. PRESSURIZES A/C TO 4.0 PSI. NO LEAKS NOTED.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 22,452 hrs · 11,802 cycles

RADAR RT FAIL. REPLACED WXR RADAR RT PER M/M.

Part: GENERATOR — BROKEN (NR 1 ENGINE) · airframe 21,822 hrs · 11,494 cycles

LT GEN FAILED IN CLIMB WITH GEN OFF, LIGHT ILLUMINATED. RESET ONCE UNSUCCESSFUL. VERBAL FROM CREW VIBRATION FELT IN A/C AND YOKE. FOUND GENERATOR BROKEN IN 2 PIECES WITH GEARBOX CONTAMINATED WITH METAL MATERIAL. WILL REQUIRE ENGINE REPLACEMENT.

Part: CONTROL UNIT — FAILED (NR 1 ENGINE) · airframe 20,336 hrs · 10,786 cycles

LT ENG GEN INOPERATIVE REPLACED EPCU AND LT SYS GEN RELAY ELECTRICAL SYS OPS NML.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 19,875 hrs · 10,546 cycles

UPON SHUTDOWN AT GATE LEFT ENG HAD SMOKE AND SOME FLAME AROUND CORE ENGINE IN THE REAR. PERFORMED TS PER AMM 71-09 PG 9, RAN ENG NO FURTHER SMOKE OR FLAME OBSERVED. ALL INSP GOOD PER M/M. MTC STILL IN WORK DUE HISTORY R&I OIL SCAVENGE PUMP. REPLACED ENGINE OIL SCAVANGE PUMP PER AMM CHAPT 79. PERFORMED DRY MOTOR LEAK CHECK AND ENG RUN PER PREFLIGHT HANDBOOK TESTS 1 AND 3, NO SMOKE ON SHUTDOWN. A/C OK FOR SERVICE.

Part: TIRE — FAILED (LT MLG) · airframe 19,066 hrs · 10,150 cycles

ON LANDING BOTH LT MAIN TIRES BLEW. EMERGENCY VEHICLES CONFIRMED BLOWN TIRES AND SOME DAMAGE TO THE STRUT AND WING OCCURRED. TOUCHDOWN WAS VERY SMOOTH WITH CONTAMINATED RUNWAY AND MAX AUTOBRAKES SELECTED. BRAKES, DACMS, AND CONTROLLER CHANGED.

Part: SOCKET — DAMAGED (CABIN) · airframe 16,900 hrs · 9,068 cycles

ON PREFLIGHT FOUND EMERGENCY LIGHT TRACK SECTION INOP FROM ROW 12 THROUGH ROW 22. FOUND EMERGENCY LIGHT ASSY BAD AT ROWS 14 & 16. REPLACED SAME. NOW CKS NORMAL.

Part: OVEN — FAULTY (GALLEY) · airframe 14,146 hrs · 7,658 cycles

FLT ATT SMELLED SMOKE IN FIRST CLASS AREA RIGHT AFTER T/O TURNED OVENS OFF AND GALLEY POWER OFF. SMOKE AND SMELL PERSISTED. FOUND F/C OVEN WITH STRONG BURNING SMELL. REPLACED SAME. NO ODOR PRESENT.

Part: CABLES — LOCKED UP (ELEVATOR CONTROL)

ON FINAL IN LANDING CONFIGURATION CONTROL COLUMN LOCKED APPROX 6 INCHES FWD OF NEUTRAL AIRSPEED 145 TO 150 KNOTS COLUMN WAS FORCEFULLY PUSHED FORWARD. RELEASE OCCURRED, BUT LOCKED ON A SECOND TRY COULD NOT DUPLICATE ON THE GROUND. REMARKS- AS OF 2130E/30 ITEM IS STILL IN WORK CABLES BEING RIGGED,T.E COLUMN OVERRIDE MECHANISM HAS BEEN RESET.

Part: ANGLE — CRACKED (BS 940)

LT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT FS 940. THE CRACK MEASURED APPROXIMATELY 1 INCH LENGTH AND EXTENDED FWD/AFT IN THE FLANGE COMMON TO THE FUSELAGE BODY. THE CRACK WAS REPAIRED BY THE INSTALLATION OF A REPAIR DOUBLER PER ER/A 364942-14.