N955DL

Part: SKIN — CORRODED (BS 464) · corrosion level 2 · airframe 75,248 hrs · 55,802 cycles

FUSELAGE/SKIN/STA 464 / BETWEEN L-29L AND L-30 / CORROSION. ER/A 561921-14 REV B - PERMANENT REPAIR RESTRICTION = REPAIR MUST BE REACCOMPLISHED PER SECTION II. INSTRUCTIONS NOT MORE THAN 24 MONTHS OF SERVICE AFTER SECTION I REPAIR. APPROVAL IS LIMITED TO 24 MONTHS OF SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (REPAIR REACCOMPLISHMENT) IS REQUIRED FOR CONTINUED SERVICE LONGER AFTER 20SEP19. (LP0807279)

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 74,784 hrs · 55,400 cycles

FOUND L2 DOOR SLIDE PRESSURE WAS BELOW LIMITS. REMOVED AND REPLACED THE SLIDE IAW WORK CARD 2561-4002, AND AMDS 2561-4002 440684.

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 73,720 hrs · 54,515 cycles

RT FWD MLG WELL CHANNEL CRACKED FOUND ON SVC CHECK. FND CRACKS IN RT WHEEL WELL 1", 3.5" &3" CORNER CHANNEL BY SERVICING DOOR. REF TOP PARA XB2- ENGINEERING HAS EVALUATED & FINDS ACCEPTABLE FOR FERRY FLIGHT, PER ENGINEERING STOPPED DRILLED CRACKED. A/C TO FERRY TO DTW FOR REPAIR. REPAIRED RT WHEEL WELL FWD CHANNEL P/N 5930584U124 PER SRM 53-05. LDG PROX SENSOR OPS CHECKS GOOD PER AMM 32-60. ALL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,524 hrs · 54,361 cycles

CEILING EMERGENCY LIGHTS ROWS 22 TO 26 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK B5104 IAW AMM 33-53.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,605 hrs · 53,638 cycles

PER MAINTENANCE REQUEST FOUND SKIN DAMAGE AT LONGERON 30 AND STATION 465 IN FRONT OF THE VHF ANTENNA. SEVERAL RIVET HEADS ARE MISSING. AREA LOOKS LIKE LIGHTNING STRIKE. C/W PRI 561921-14 REV O MATCHES ERA 561921-14.

Part: SKIN — NOT REPORTED (BS 464) · airframe 75,248 hrs · 55,802 cycles

PER ERA 561921-14 DTE IS REQUIRED ON THE FUSELAGE SKIN AT FS 464 BETWEEN L-30 AND L29L DUE TO A SKIN REPAIR. REF LOG PAGE 0807279 FOR ERA561921-14 REV B TRACKING. LOGPAGE TERMINATED, PERMANENT REPAIR REQUIRED ON DIFFERENT LOGPAGE PER ER/A 561921-14 REV B. (LP0221707)

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 71,136 hrs · 52,536 cycles

NR 2 COFFEEMAKER SMOKING WHEN ON, BUT NOT BREWING; TURNED OFF, SMOKE STOPPED. REPLACED THE COFFEEMAKER.

Part: ACTUATOR — FAILED (NLG) · airframe 71,051 hrs · 52,470 cycles

ON APPROACH INTO BHM WHEN GEAR SELECTED DOWN, THE NLG FAILED TO EXTEND. CREW ACCOMPLISHED QRH PROCEDURE AND PERFORMED AN ALTERNATE GEAR EXTENSION. NLG EXTENDED NORMALLY WITH GREEN DOWN/LOCKED INDICATION, CREW STOWED ALTERNATE EXTENSION LEVEL AND LANDED NORMALLY. AIRCRAFT WAS MAINTENANCE FERRIED BACK TO ATL WITH GEAR EXTENDED FOR REPAIR. MAINTENANCE JACKED AIRCRAFT AND WAS ABLE TO DUPLICATE THE FAULT. REMOVED AND REPLACED NLG BUNGEE ACTUATOR PER AMM 32-32.

Part: INTERCOSTAL — CRACKED · airframe 69,709 hrs · 51,517 cycles

INTERCOSTAL FOUND CRACKED 2 OCLOCK POSITION. REMOVED INTERCOSTAL AND ATTATCHING PARTS. DRILLED UP NEW INTERCOSTAL IAW DWG 9911875. INSTALLED IAW DWG 9911875.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,839 hrs · 50,215 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 19D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: STRUCTURE — CRACKED (EMPANNAGE) · airframe 67,492 hrs · 49,954 cycles

AFT LT EMPENNAGE, JUST ABOVE NR 1 PYLON. PACK EXIT FLANGE IS CRACKED. REPAIRED IAW ERA 539229-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 241) · airframe 67,492 hrs · 49,954 cycles

ACFT HAS SKIN PROTRUDING AND CRACKED AT BS 241, STRINGER 29L. REPAIRED IAW PRI 539193-14, REV 7.

Part: SKIN — CORRODED (BS 578) · corrosion level 2 · airframe 67,488 hrs · 49,951 cycles

SKIN HAS AN AREA OF CORROSION, BS 578, STRINGER 29L. REPAIRED IAW SRM 53-04, FIG 12C, VIEW H.

Part: SKIN — CORRODED (BS 555) · airframe 67,488 hrs · 49,951 cycles

BELLY SKIN BULGED, FASTENERS PULLED THROUGH BS 555 STRINGER 29R. REPAIRED IAW SRM 53-04, FIG 12C.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 70,614 hrs · 52,207 cycles

MTC REPORTED CORROSION, CRACKED SKIN, AND THREE PLUGS UNDER THE TCAS ANTENNA DOUBLER LOCATED BETWEEN FS 229-255 AND L-28L TO L-29R. ER/A 539193-14 WAS ISSUED TO REPAIR THE DAMAGE.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON FWD & AFT CARGO BAY DOOR FRAME BEAM. CORROSION REMOVED IAW SRM 51-10-3, PAR 26A. FOUND OUT OF LIMITS IAW SRM 53-05, FIG 123A. REPAIRED IAW ER/A 519124-14, REV ORIGINAL. REPAIR INSPECTED IAW ER/A 5109124-14 RE, ORIG AND SRM 53-05, FIG 123A.

Part: TEE FITTING — DAMAGED (PRESSURE BLKHD) · airframe 62,782 hrs · 46,703 cycles

SCRATCHES ON TEE ANGLE OF PRESSURE DOME LOWER AREA Y=1338 X=25 TO 23, X=6 TO 4, X=-35 TO 33. DAMAGED TEE SECTION AND STRUCTURE PARTS WERE REMOVED IAW SRM 53-03, FIG 37. NEW TEE SECTION FABRICATED AND INSTALLED IAW SRM 53-03, FIG 37, 51-30-2 AND 51-30-5.

Part: FINGER DOUBLER — DAMAGED (BS 617) · airframe 62,782 hrs · 46,703 cycles

DAMAGE ON FINGER DOUBLER FASTENER PROTUDING LOWER AFT CORNER, BS 617, S20-21R. DOUBLER WAS REPLACED IAW ER/A 239715-14, REV D.

Part: SKIN — DAMAGED (BS 807) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON FUSELAGE SKIN BELOW FILLET PANEL RUBSTRIP AREA ON BS 807 BETWEEN LONGERONS 28-29R. SKIN REPAIRED IAW SRM 53-04, FIG 57, 51-30-5, 51-30-1.

Part: TAB — DAMAGED · airframe 62,782 hrs · 46,703 cycles

LIGHTING STRIKE ON T/E CONTROL TAB. REPAIRED IAW SRM 55-04 PH3.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 62,782 hrs · 46,703 cycles

CORROSION ON LONGERON 26L BETWEEN, BS 1287 AND 1309, AFT CARGO BAY. CORROSION REMOVED, OUT OF LIMITS. LONGERON REMOVED AND NEW LONGERON SECTION INSTALLED IAW SRM 51-10-3 PAR. 26-21-14 53-02 FIG. 18.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,782 hrs · 46,703 cycles

DAMAGED METALLIZED SURFACE ON RUDDER. REPAIRED IAW SRM 51-70-IA.

Part: STRUCTURE — CORRODED (BS 731-750) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

DURING SCHEDULED CHECK, CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLERS BETWEEN BS 731 & 750 IN THE CABIN FLOOR STRUCTURE. DOUBLERS WERE REMOVED AND NEW REPAIR DOUBLERS INSTALLED IAW SRM 53-05, FIGURE 131A.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

DURING SCHEDULED HEAVY CHECK, CORROSION WAS NOTED AT ALL 4 RADIO ALTIMETER TO SKIN FAYING SURFACES. CORROSION WAS REMOVED AND NEW DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Part: SEAT TRACK — CORRODED (BS 480-482) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON RT SEAT TRACK, X=-54, STA Y=480-482 AT CABIN FLOOR STRUCTURE. REPAIRED PLUG, INSTALLED PLUG IAW SRM 53-05, FIG 4A.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 62,782 hrs · 46,703 cycles

CORROSION ON ACCESS PLATE NR 1464C AND SCREW HOLES OF RT MAIN FUEL TANK. REPLACED PLATE 1464C IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,782 hrs · 46,703 cycles

CRACKED LONGERON 12L AT BS 1437. REPAIRED IAW SRM 53-02, FIG 18.

Part: SEAT TRACK — CORRODED (BS 423-425) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON LT SEAT TRACK X=54 BETWEEN STA Y=423-425 AT CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED AND REPAIR PLUG WAS INSTALLED IAW SRM 53-05, FIG 4A.

Part: FRAME — CORRODED (BS 127) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON FRAME AT STA Y=127 AND BETWEEN LONGERONS 17 AND 18R COCKPIT STRUCTURE. FRAME WAS REPLACED IAW SRM 51-30-5 , 51-30-2 AND DWG 9911511, REV "B".

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON ACCESS PLATE NR 1462C AND SCREW HOLES OF RT MAIN FUEL TANK. ACCESS PLATE NR 1462C. REPLACED IAW SRM 51-22-2A.

Part: SKIN — CORRODED (BS 769-771) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON FUSELAGE SKIN BENEATH RUBSTRIP FROM BS 769 TO 771 AND BETWEEN LONGERONS 27-28R . REPAIR DOUBLER WAS FABRICATED AND REPAIR WASHERS, AND REPAIR DOUBLER WERE INSTALLED IAW SRM 53-0 4 FIG. 57.

Part: DOOR FRAME — CRACKED (BS 423.5) · airframe 62,782 hrs · 46,703 cycles

CRACK ON INTERNAL DOUBLER AT THE LOWER AFT DOOR FRAME CORNER, BS 423.5 BETWEEN LONGERONS 27-28R AT THE FWD CARGO BAY. FASTENERS WERE REMOVED AND DAMAGE REMOVED IAW SRM 51-30-2 AND 51-30-5 AND 53-05, FIG 105. DOUBLERS AND FILLERS WERE FABRICATED IAW SRM 53-05, FIG 105. DOUBLER AND FILLERS INSTALLED IAW SRM 53-05, FIG 105.

Part: BUSHING — DAMAGED (RT WING) · airframe 62,782 hrs · 46,703 cycles

ELONGATED BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING. BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING WERE R & R IAW EA 09-070683-03, AD REV L AND SRM 51-30-10; RII COMPLETED.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON FRAME BS 1380 FROM X=-25 TO X=25. FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5, DWG 9912246, REV CE.

Part: LONGERON — CRACKED (BS 1431) · airframe 62,782 hrs · 46,703 cycles

CRACK LONGERON 10R, BS 1431, SECTION OF LONGERON DAMAGE WAS REMOVED. NEW SECTION AND SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-20-0.

Part: SKIN — WORN (RT WING) · airframe 62,782 hrs · 46,703 cycles

WORN PREVIOUS REPAIR DOUBLER ON L/E STA XFS=110 RT WING. PREVIOUS REPAIR REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, INSTALLED AND IDENTIFIED IAW ER/A N 378819-14, REV A.

Part: CUSP WEB — CORRODED (BS 1022-1041) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1022 TO 1041 AND BETWEEN X=54 TO X=60 AT PAX CABIN REF NRC (T0 294284) OR NC 193 ZONE 58, REF (T0 295304). DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131A. REPAIR WAS IDENTIFIED IAW PS 900-5-1 N.-04 ASSOCIATED ER/A 51-116514 ADDED FOR AC 0955.

Part: CUSP WEB — CORRODED (BS 1003-1022) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1003 TO Y=1022 AND BETWEEN X=54 TO X=60 AT PAX CABIN. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, INSTALLED, IDENTIFIED, AND CIC WAS APLICATED IAW SRM 53-05 FIG 131A, 51-10-3 PAR 14 AND 21 AND PS 900-2-N-9.

Part: LONGERON — CRACKED (BS 160) · airframe 62,782 hrs · 46,703 cycles

CRACK ON LONGERON 2LT AT BS 160. SECTION OF LONGERON WAS REMOVED AND NEW SECTION LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1271-1322) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON LONGERON 23LT FROM BS 1271 - 1322 IN AFT CARGO BAY LT TUNNEL. CORROSION REMOVED. REWORKED AREA FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1., DAMAGE LONGERON SECTION REMOVED, AND A NEW SECTION LONGERON INSTALLED.

Part: LONGERON — WORN (BS 1375) · airframe 62,782 hrs · 46,703 cycles

WORN LONGERON 19 LEFT BS 1375 . DAMAGE BLENDED AND LONGERON SECTION REMOVED. NEW SECTION INSTALLED IAW SRM 53-01, FIG 1, 51-30-2, 51-30-5,53-02, FIG 18, 51-10-3 PAR 21 AND 14, AND PS 900-5-1.

Part: BEAM — CORRODED (BS 636-693) · corrosion level 2 · airframe 62,782 hrs · 46,703 cycles

CORROSION ON MID CARGO BAY DOOR FRAME BEAM FROM BS 636 TO 670. REPAIRED IAW ER/A 519117-14.

Part: SKIN — CRACKED (BS 1418) · airframe 62,782 hrs · 46,703 cycles

CRACKS FOUND ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 519129-14AD REV. ORIG.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 61,241 hrs · 45,621 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX FOUND A BROKEN WIRE AT THE CONNECTOR AND REPLACED THE PIG-TAIL. THE SYS RETURNED TO NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,241 hrs · 45,621 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT 15, 18, 22, 25, 29, 32, AND 36 WERE INOPERATIVE. MX CYCLED THE POWER SWITCH AND ALSO REPLACED 3 OF THE LIGHT LAMPS. THE SYSTEM HAS RETURNED TO NORMAL OPERATION.

Part: CAM — WORN (TAILCONE) · airframe 60,802 hrs · 45,322 cycles

TAILCONE RELEASE CAM LUG - WORN, KEVLAR CABLE RELEASE CAM MAX MATERIAL LOSS IS .025", BLENDED WEAR MARKS, HFEC INSPECTED WORN AREA IAW NTM 06-01-01.001. NO DEFECT NOTED QC1971 INSTALLED TAILCONE RELEASE CAM IAW AMM 53-53-02. AWAITING FINAL ER/A. 255074. COMPLETED FINAL ER/A 509765-14, REV O.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 60,796 hrs · 45,318 cycles

LEFT VERTICAL STABILIZER REPAIR DOUBLER-SKATE ANGLE-CRACKED AT STABILIZER T/E. REF NR 142, REMOVED PREVIOUS REPAIR ANGLE THAT WAS CRACKED AND REPAIRED BY FABRICATING NEW REPAIR ANGLE SAME AS PREVIOUSLY INSTALLED. REPAIRED IAW SRM 53-05, FIG 23.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,617 hrs · 45,180 cycles

ONE LIGHTNING STRIKE AT FS 42, 16" BELOW LONG 18R FOUND TO BE OUT OF LIMITS IAW SRM 53-04-1, PAR 6. REMOVED DAMAGE AND INSTALLED REPAIR. HFEC INSP OF REPAIR FASTENER HOLE, OK. REPAIRED IAW ER/A 508740-14, REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,617 hrs · 45,180 cycles

LIGHTNING STRIKE AT FS 42, 15.5" BELOW LONG 18R. FOUND TO BE OUT OF LIMITS IAW SRM 53-04-1 PAR 6. REMOVED DAMAGE AND INSTALLED REPAIR. HFEC INSP OF REPAIR FASTENER HOLE, OK (QC 1707).

Part: SKIN — DAMAGED (BS 168) · airframe 60,680 hrs · 45,231 cycles

LIGHTNING STIRKE AT FS 168, 3 INCHES BELOW LONGERON 23R. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW SRM. I

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,577 hrs · 45,143 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12 & 13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES AND THE BATTERY PACK. OPS CHECKED GOOD.

Part: HANDSET — OVERHEATED (FWD CABIN) · airframe 59,831 hrs · 44,637 cycles

ON APPROACH, CABIN CREW NOTED A BURNING ODOR AND UNUSUAL HEAT COMING FROM THE FORWARD FLIGHT ATTENDANT HANDSET. ON INSPECTION, MAINTENANCE NOTED THE HANDSET BEGAN TO OVERHEAT WHEN THE FUEL LEVER WAS TURNED ON. MAINTENANCE REPLACED THE HANDSET AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,679 hrs · 44,522 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHT AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LANYARD — BROKEN (R1 DOOR SLIDE) · airframe 59,438 hrs · 44,349 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1R HAD A BROKEN LANYARD. LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND SLIDE RELEASE. THE DOOR SLIDE LANYARD WAS REPLACED.

Part: APU — LEAKING (APU BAY) · airframe 58,902 hrs · 43,974 cycles

THE FLIGHT RETURNED TO BWI WITH AN UNEVENTFUL LANDING AFTER THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN ON CLIMBOUT. MAINTENANCE FOUND THAT THE APU WAS LEAKING OIL INTO THE INLET. PERFORMED DUCT BURNOUT OPN 5089 AND REPLACED BOTH COALESCER BAGS. LEAK CHECKS GOOD.

Part: WIRE — CUT (CABIN) · airframe 57,928 hrs · 43,327 cycles

EMERGENCY EXIT SIGN INOPERATIVE AT AFT GALLEY DOOR. FOUND WIRES FOR EXIT SIGN AND GALLEY DOOR WARNING CUT IN CEILING ABOVE THE HINGED PANEL ABOVE THE AFT GALLEY DOOR. REPAIRED WIRES PER MD88 SWPM CHAPTER 20. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,926 hrs · 43,326 cycles

SDR - CORROSION ON FLOORBEAM RBL 7 FS 160-200 MCF 04. SAA102 CORROSION. FABRICATED FLOORBEAM TRACK FROM MATERIAL S3932140 BATCH # 0002110433 PER SRM DC9/MD88 SRM 53-14-1 FIG 11 SHT 2 ITEM 64. INSTALLED FLOORBEAM AT MAIN CABIN STA 160-200 RBL 7 PER SRM 51-30-3. AT SAA/SAT DURING PAX MOD DOCUMENTEDON W/O 89208290001.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,926 hrs · 43,326 cycles

CORROSION ON FLOOR Z-ANGLE LBL 56 FS 160-200. REMOVED FLOOR Z-ANGLE AND REPLACED IAW DC9/MD80 SRM 51-30-5 PG 1, 3, 9, 10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,926 hrs · 43,326 cycles

FLOOR SUPPORT LBL 56 FS 180-200 HAS CORROSION AND IS EXFOLIATING. REMOVED FLOOR SUPPORT IAW DC9/MD80 SRM 51-30-5 PG 29, FABRICATED NEW SUPPORT AND INSTALLED AT ST AEROSPACE SAN ANTONIO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,926 hrs · 43,326 cycles

CORROSION ON FLOORBEAM FS 200 RBL 40 MCF 05. SAA102- CORROSION FWD GALLEY. FABRICATED FLOOR SUPPORT ANGLE AT STA 200 RBL 7 TO RBL 40 IAW DC9/MD80 SRM 53-14-1 FIG 11 SHEET 1-22 PG 27-29. INSTALLED FLOOR SUPPORT ANGLE STA 200 RBL 7 TO 40 IAW DC9/MD80 SRM 51-30-05 PG 12. AT SAA/SAT ON NR 42 W/O 89208300001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,926 hrs · 43,326 cycles

CORROSION ON SEAT TRACK LBL 22 FS 200-220. REMOVED AND REPLACED SECTION OF SEAT TRACK BETWEEN FS 200-229 LBL 22 PER DC9/MD80 SRM 53-05 FIG 4F.

Part: CONNECTOR — DIRTY (ANTI-SKID SYS) · airframe 57,827 hrs · 43,250 cycles

DURING LANDING BRAKES WERE INACTIVE AT HIGH SPEEDS. WOULD NOT RESPOND TO BRAKE PEDAL DEFLECTION. MAINTENANCE CHECKED BRAKE PRESSURE AT EACH BRAKE PER AMM 32-42. PRESSURE CHECKS GOOD. ALL FOUR ANTI-SKID TRANSDUCERS CONNECTOR WERE REMOVED AND CLEANED PER AMM 32-43. ALL CHECKS WERE NORMAL. AIRCRAFT OK FOR SERVICE.

Part: TRANSMITTER — LEAKING (HYDRAULIC SYS) · airframe 57,441 hrs · 43,001 cycles

CLIMBING THROUGH 10000 FEET, A HAZE AND BURNING SMELL WAS NOTED IN THE AFT CABIN. COCKPIT CREW COMPLIED WITH QRH PROCEDURES AND DIVERTED THE FLIGHT TO JAX. MAINTENANCE FOUND THE RIGHT HYDRAULIC SYSTEM PRESSURE TRANSMITTER LEAKING AND REPLACED IT. PERFORMED ALTERNATE DUCT BURNOUT PER OPN 5090 REPLACED THE COALESCER BAGS.

Part: SKIN — DAMAGED (BS 693) · airframe 57,303 hrs · 42,894 cycles

THE FUSELAGE SKIN WAS FOUND WITH A POPPED RIVET HEAD AND SKIN PILLOWING AT BS 693 BETWEEN L29-30L. REPAIR IAW ERA 494249-14

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,303 hrs · 42,894 cycles

FUSELAGE LWR BELLY SKIN HAS BULGED AND PILLOWED AREA AT BUTT JOINT STA 588 LONG 28 RT TO 29 RT.

Part: SPLICE — DAMAGED (VERTICAL STAB) · airframe 57,303 hrs · 42,894 cycles

2ND FASTENER HOLE DOWN FROM LOWER END OF VERT STAB L/E BUTT SPLICE HAS DAMAGE AT COUNTER SINK. CORRECTED PER PRI 494239-14 REV 1 AS NOTED ON ENR 88.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 57,279 hrs · 42,879 cycles

CREW FOUND L1 DOOR SLIDE LANYARD BROKEN. MAINTENANCE REPLACED L1 DOOR SLIDE LANYARD PER AMM 25-62-00-201.

Part: O-RING — LEAKING (APU OIL CAP) · airframe 56,319 hrs · 42,235 cycles

STRONG ODOR IN ACFT AFTER TAKEOFF. AFT LAVATORY SMOKE DETECTOR SOUNDED AND F/A REPORTED SMOKE AND HAZE IN THE CABIN. FLIGHT CREW RETURNED ACFT TO DEPARTURE. MX FOUND OIL LEAK FROM APU OIL CAP. REPLACED OIL CAP AND CLEANED RESIDUAL OIL. RAN APU AND NO OIL LEAK NOTED. C/W FULL DUCT BURNOUT. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 55,017 hrs · 41,333 cycles

MX FOUND ONE RED EMERGENCY ESCAPE PATH LIGHT OUT AT RT AFT OVER WING DOOR SEAT ROW. MX FOUND THE CONNECTOR AT LIGHT 25D CUT OFF. MX REPAIRED THE WIRES. MX FOUND THE FUSE IN THE AFT BATTERY PACK TO BE BLOWN. MX REPLACED THE FUSE. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — FRAYED (CABIN) · airframe 54,918 hrs · 41,271 cycles

MAINTENANCE FOUND THE RED EMERGENCY FLOOD LIGHT AT GALLEY NR 2 NOT ILLUMINATED. MAINTENANCE REPAIRED A FRAYED WIRE. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0929) ATL 254259 (DLM88101997).

Part: CLAMP — LOOSE (AC BAY) · airframe 54,838 hrs · 41,203 cycles

THE PILOTS GOT AN INTERMITTENT TAIL COMPARTMENT TEMP HIGH WARNING LIGHT ON CLIMBOUT. THE PILOTS DIVERTED TO BUF DUE TO BOTH FIRE EXTINGUISHER AGENT LOW LIGHTS BEING ILLUMINATED. MAINTENANCE REPLACED BOTH FIRE EXTINGUISHING AGENT BOTTLES, BOTTLES WERE EMPTY. MAINTENANCE FOUND A CLAMP LOOSE AT THE LEFT FLOW CONTROL VALVE BLOWING HOT AIR ONTO THE EXTINGUISHER BOTTLES. MAINTENANCE TIGHTENED THE CLAMP AND REPLACED BOTTLES. A CHECKOUT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0842)(DLM88101920).

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHT) · airframe 53,913 hrs · 40,595 cycles

MX FOUND THE CEILING EMERGENCY LIGHT ABOVE L1 WOULD NOT TEST. MX SECURED THE GROUND WIRE BEHIND THE LIGHT ASSY. THE OPS CHECK WAS GOOD AND THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 637) · airframe 48,315 hrs · 36,993 cycles

FUSELAGE SKIN AND DOUBLER AT THE FORWARD EDGE OF THE C2 CARGO DOOR CUTOUT WAS DAMAGED BY GROUND EQUIPMENT. CUTOUT DAMAGE AND INSTALLED A REPAIR DOUBLER/TRIPLER.

Part: TAIL CONE — DEPLOYED (TAIL) · airframe 44,370 hrs · 34,473 cycles

TAIL CONE INADVERTENTLY DEPLOYED. ADJ SPRING CAM RELEASE CABLE. REINSTALLED TAIL CONE PER MM 53-53-00. ADJ OF TAIL CONE RELEASE MECHANISM CAM OK PER MM.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,393 hrs · 31,655 cycles

THE FUSELAGE SKIN WAS BADLY CREASED BY CONTACT WITH GROUND EQUIPMENT BETWEEN FS 461 & 522 BELOW STRINGER 20R. THE DAMAGE WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND INTERNAL ALUMINUM FINGER DOUBLERS PER MD-88 SRM AND ER/A 095369-14, REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,939 hrs · 31,325 cycles

THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED IN THE BELLY AT STRINGER 30 NEAR AN ANTENNA CUTOUT AT FS 725. THE DAMAGED AREA OF SKIN AND DOUBLER WERE CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 093801-14, REV A.

Part: SWITCH — OUT OF ADJUST (THROTTLE) · airframe 38,394 hrs · 30,253 cycles

GEAR UNSAFE LIGHTS (3) WITH GEAR HANDLE UP AFTER TAKEOFF. AURAL WARNING TOO. AFTER LEVEL OFF AT 5000 FT WARNINGS INTERMITTANT. FOLLOWED POM GEAR UNSAFE LIGHT GEAR HANDLE UP CHECKLIST. GEAR LIGHTS 3 GREEN AFTER GEAR HANDLE RETURNED TO DOWN POSITION. FOUND RT THROTTLE SWITCH PACK OUT OF ADJUST. ADJUSTED PER AMM. SWUNG GEAR, CHECKS NORMAL.

Part: AUGMENT VALVE — FAILED (TAIL AREA) · airframe 38,170 hrs · 30,081 cycles

LOST PRESSURIZATION AT FL LVL 330 EMERGENCY DESCENT. REPLACED RT AUG VALVE.

Part: SENSOR — UNSERVICEABLE (NLG) · airframe 36,561 hrs · 29,003 cycles

AFTER TAKEOFF, NOSE GEAR LIGHT REMAINED RED WITH GEAR HANDLE UP. GEAR LOWERED NORMALLY PER POM PROCEDURES. ADJUSTED NOSE GEAR UP POSITION SENSOR.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 36,280 hrs · 28,811 cycles

ON PUSHBACK FROM CVG GOT OAP..CARGO FIRE..LIGHT WITH NO OTHER FIRE INDICATIONS. REPLACED OAP PANEL PER M/M. OP CHECKS OK

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,103 hrs · 28,706 cycles

EMERGENCY TRACK LIGHTS INOP FROM SEAT 31 THRU AFT SECTION. REPLACED BLOWN FUSE F1 ON AFT POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,024 hrs · 28,667 cycles

FOUND ON LAYOVER, AFT CABIN EMERGENCY AISLE LIGHTS AND SIGNS INCLUDING TAIL COMPARTMENT INOP. REPLACED POWER SUPPLY AND BATTERY R5-212. CHECKS GOOD.

Part: APU — CONTAMINATED · airframe 35,701 hrs · 28,444 cycles

DURING TAXI OUT WITH ONE ENGINE OPERATING AND APU OPERATING, SMOKE BEGAN TO FILL THE CABIN. AFTER BOTH PACKS TURNED OFF, SMOKE BEGAN TO CLEAR. RETURNED TO GATE. FOUND OIL LEAKING FROM APU COMPARTMENT AND DRIPPING IN VICINITY OF APU AIR INTAKE. APU AIR INLET SATURATED WITH OIL. CLEANED INLET, PERFORMED DUCT BURNOUT.

Part: POWER SUPPLY — INOPERATIVE (AFT CABIN) · airframe 35,152 hrs · 28,068 cycles

FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROWS 31 TO 38. REPLACED POWER SUPPLY. CHECKS GOOD.

Part: ENGINE — MAKING METAL (NR 1) · airframe 32,393 hrs · 26,034 cycles

LEFT OIL STRAINER CLOGGED MESSAGE CAME ON 1 HR INTO FLT. ENGINE SHUTDOWN. FOUND METAL ON CHIP DETECTOR AND MAIN OIL FILTER. REPLACED ENGINE.

Part: SEAL — LEAKING (PAX DOOR) · airframe 31,443 hrs · 25,348 cycles

AIRPLANE WOULD NOT PRESSURIZE AFTER T/O RETURNED TO LAND CVG EXCESSIVE WIND NOISE AT 2L DOOR - SECURED SEAL AND REPLACED FILLER

Part: ENGINE — MAKING METAL (NR 2) · airframe 30,385 hrs · 24,581 cycles

NBR 2 ENG SHUTDOWN IN FLIGHT DUE TO OIL STRAINER CLOG MSG- STAYED ON AFTER THROTTLES RETARDED. - FOUND CARBON IN FILTER - REPLACED SAME - RAN ENGINE - OK FOR SERVICE

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,133 hrs · 23,659 cycles

THE RT SIDE FUSELAGE TO VERT STAB ATTACH ANGLE WAS FOUND CRACKED AT APPROX FS 1474 (CANTED). THE CRACK IS APPROX 0.75 INCHES IN LENGTH AND EXTENDS FWD/AFT IN THE HORIZ FLANGE.

Part: GENERATOR — FAILED (NR 2)

AFTER T/O, 400 FT AGL HAD BOTH BUSSES FAIL IN SUCCESSION AND HAD STBY PWR IN USE. REPLACED RIGHT GENERATOR AND CSD.

Part: BRAKE — LOCKED UP (NR 2)

LEFT INBOARD BRAKE OVERHEATED ON TAKEOFF, RETURNED TO ATL. REPLACED NR 2 BRAKE DUE TO BEING LOCKED UP. ALSO, REPLACED BOTH LT MLG WHEEL ASSYS.

Part: STRUT — FAILED (NLG)

AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT AND DOORS OPEN. CYCLED GEAR NO HELP. PUT GEAR BACK DOWN WITH THREE GREEN LIGHTS. CORRECTIVE ACTION: REPLACED NLG PISTON ASSY.

Part: STRUT — WATER CONTAM (NLG)

ON T/O ROLL, LOUD NOISE FROM NOSE GEAR AREA, MULTIPLE FLAGS NOTED ON FMA, A/S INDICATOR ETC, CAPTS INSTRUMENTS FAILED. FOUND STRUT FLAT. SERVICED STRUT PER OPN 4703 AND PERFORMED BITE CHECK ON INSTRUMENTS, ALL OK. A/C DEPARTED A SECOND TIME, AFTER GEAR RETRACTION NOSE GEAR RED LIGHT REMAINED ILLUMINATED. RETURNED JFK, FERRIED ATL. REPACKED STRUT, FOUND FLUID CONTAMINATED WITH WATER. SERVICED STRUT AND OPERATION NORMAL.

Part: PACKING — LEAKING (LT HYD SYST)

LEFT HYD SYS FAILURE, QTY DECREASED TO 4 QTS. COMPLIED WITH PROCEDURES, LEFT ENG HYD PUMP OFF, QTY TO 17 QTS BUT NO LEFT HYD PRESS. FOUND LEFT SYSTEM HYD FWD FILTER UNION OF ENG HIGH PRESS MOD LEAKING. REPLACED UNION PACKING, LEAK CHECK OK.

Part: ENGINE — SMOKE (NR 1 ENGINE)

DURING TAKEOFF, CABIN FILLED WITH SMOKE, RETURNED TO ATL. ENGINE RUN UP DISCOVERED NR 1 ENGINE PRODUCING SMOKE AT HIGH POWER SETTINGS. ENGINE WAS REPLACED AND ROUTED TO SHOP.