N948DL

Part: PAINT — MISSING (RUDDER TAB) · airframe 75,335 hrs · 56,759 cycles

RUDDER TAB MISSING PAINT. REMOVED RUDDER TAB REF MD88 AMM 27-20-02. INSPECTED AREA & ATTACHMENTS, OK TO INSTALL TRIM TAB. INSTALLED NEW RUDDER TAB REF AMM 27-20-02. INSPECTED INSTALLATION/SAFETY & ADJUSTMENT PER AMM 27-20-02. (LP5243521)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,888 hrs · 56,355 cycles

DURING SERVICE CHECK MAINTENANCE FOUND ROW 24-30 LOWER EMERGENCY LIGHTS TO BE INOPERATIVE. THEY REPLACED THE POWER SUPPLY PER AMM 33-53. AND THE OPERATIONAL CHECK IS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 74,691 hrs · 56,184 cycles

EMERGENCY CEILING LIGHTS AT 11A,13A/B,14A,22A,24 A/D, & 25A INOPERATIVE. REMOVED & REPLACED THE BATTERY PACKS ROW 12 & 24 IAW AMM 33-55. OPS CHECKED GOOD.

Part: CABLE — OUT OF POSITION (TAILCONE RELEASE) · airframe 74,140 hrs · 55,730 cycles

TAILCONE UNSAFE MESSAGE. FOUND INTERIOR CABLE DISCONNECTED, OUT OF RETAINING MECHANISM. SECURED THE CABLE AND PERFORMED ODI TEST IAW AMM 53-53-00. OPS NORMAL ACFT OK FOR SERVICE. THE TAILCONE SLIDE REARMED. INSPECTION AND RIGGING OK IAW AMM 53-53.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,128 hrs · 55,721 cycles

SEAT 19 EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT ON SEAT 19 REF AMM 33-53 OPS CHECK GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 74,055 hrs · 55,658 cycles

AT 27,000 FT LEFT ENGINE PRODUCED A LOUD BANG AND IMMEDIATELY FOLLOWING THE EPR, N1, N2 ROLLED BACK TO IDLE. WE CONDUCTED THE ENGINE SEVERE DAMAGE QRH AND LANDED WITH THE LEFT ENGINE AT IDLE. THE RIGHT ENGINE NEVER EXCEEDED ANY LIMITS DURING THE FAILURE. REF LOG PAGE 565653 FOR REMOVED AND REPLACED LEFT ENG PER WORKCARD 88-7110-9-0010. OPS CHK GOOD. A/C OK FOR SVC.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,681 hrs · 55,343 cycles

TOP AFT LEFT AND RIGHT OVER WING EMERGENCY DOOR EMERGENCY LIGHT INOP. T/S TOP AFT LT/RT OVER WING EXIT DOOR EMERGENCY LIGHT PER AMM 33-50. R&R EMERGENCY BATTERY PACK. OPS CK GOOD. OK FOR SVC.

Part: WIRE — BROKEN (CABIN) · airframe 73,634 hrs · 55,303 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 28DE INOP, TERMINAL PLUG WIRE BROKEN. RETERMINATED TERMINAL PLUG AT SEAT 28DE PER SPWM CHAPTER 20 AND EWIS OPS CKS GOOD.

Part: CLAMP — FAILED (COALESCER BAG) · airframe 73,282 hrs · 55,031 cycles

RETURNED TO DEPARTURE DUE TO A TAIL COMPARTMENT TEMP HIGH MESSAGE. PERFORMED QRH AND MESSAGE EXTINGUISHED WITH LEFT ENGINE AT IDLE. DURING THE RETURN, THE CABIN PRESSURE WAS LOST AND PASSENGER OXYGEN MASKS DEPLOYED. AN EMERGENCY WAS DECLARED. DURING AN EMERGENCY DESCENT, FLIGHT ATTENDANTS REPORTED SMOKE & HAZE IN THE CABIN WITH A BURNING ODOR. FOUND THE RT COALESCER BAG CLAMP DISLODGED AND BAGGAGE MELTED. REPLACED THE RT TEMP CONTROL VALVE, LT & RT COALESCER BAGS AND CLAMP. PERFORMED ALL PNEUMATIC HEALTH CHECKS AND FUNCTIONAL CHECKS AS REQUIRED WITH NORMAL FUNCTION VALIDATED.

Part: BRACKET — CRACKED (TAIL COMPT) · airframe 73,288 hrs · 55,037 cycles

ON ''A'' CHECK FOUND ATTACH BRACKET FOR HANDRAIL IN TAIL COMP CRACKED. ROBBED HAND RAIL ATTACH BRACKET P/N 5930556-15. INSTALLED BRACKET PER MD88-AMM53-40.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,473 hrs · 54,400 cycles

OVERWING EXIT SIGN LIGHTS OVER FWD DOORS INOP. R&R BATTERIES IAW AMM 33-53-00.

Part: WIRE — DEFECTIVE (CABIN) · airframe 71,898 hrs · 53,943 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT 14D AND 28D INOP. REPLACED PIG TAIL AT 14D AND RETERMINATED CONNECTOR AT 28D PER AMM 33-52 AND EWIS. OPS CKS GOOD.

Part: DOOR — LOOSE (LT OVERWING) · airframe 71,319 hrs · 53,505 cycles

LT FWD OVERWING EXIT DOOR NOT FLUSH WITH FUSELAGE AND LOOSE. ADJUSTED LT FWD OVERWING EXIT DOOR IAW AMM 52-21-00, OK FOR SERVICE.

Part: GUIDE — WORN (RADOME) · airframe 71,188 hrs · 53,403 cycles

BAD VIBRATION AT FRONT OF AIRPLANE CLIMBING OUT ABOVE 300 KNOTS. PERFORMED GVI FOUND EXCESSIVE PLAY ON RADOME GUIDE PIN HOLES R&R RADOME REF AMM 53-51.

Part: DOOR FRAME — CRACKED · airframe 70,504 hrs · 52,896 cycles

CRACKED DOOR FRAME FWD ACCESSORY COMPARTMENT, THE DOOR FRAME WAS REPAIRED IAW ER/A 552876-14 REV. ORIGINAL AND ETI -88-16-484 REV. 2.

Part: SKIN — DENTED (LT ELEVATOR TAB) · airframe 70,504 hrs · 52,895 cycles

DENTS ON UPPER SKIN AT LT ELEVATOR CONTROL TAB. ELEVATOR CONTROL TAB P/N 5910413-511; S/N 49533 (OFF) WAS REMOVED AND INSTALLED SERVICEABLE CONTROL TAB P/N 5910413-507; S/N 49983 (ON).

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 70,504 hrs · 52,895 cycles

NICKS ON LOWER SKIN AT INBOARD LT WING FLAP. THE FLAP WAS REPAIRED IAW SRM 57-01-FIG.5.

Part: LONGERON — CORRODED (BS 1271-1309) · corrosion level 2 · airframe 70,504 hrs · 52,895 cycles

CORROSION ON LONGERON 29L BETWEEN BS 1271 - 1309. REPAIRED IAW SRM. 53-02, FIG 18.

Part: PAN — CRACKED (L1 DOOR) · airframe 70,504 hrs · 52,895 cycles

CRACKED MAIN ENTRANCE DOOR PAN ON FWD UPPER CORNER PAN ON FWD UPPER CORNER OF MAIN L1 DOOR. REPAIRED IAW SRM 52-05 FIG. 18A.

Part: PAN — CRACKED (R1 DOOR) · airframe 70,504 hrs · 52,895 cycles

DOOR, CRACK ON FWD PAN BTW NR 3 AND 4 BEAMS AT R1 DOOR. PAN BTW BEAMS NR 3 AND 4 WAS REPAIRED PER SRM 52-03 D FIG 3.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 70,504 hrs · 52,895 cycles

PAX CABIN, BROKEN WIRES ON L2 SLIDE LANYARD. LANYARD WAS REPLACED PER AMM 25-62-00 PARAGRAPH D-4.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,504 hrs · 52,895 cycles

PAX CABIN CRACKED LONGERON 3 LT ON STA Y=180. FASTENER WAS REMOVED AND INSTALLED PER SRM 51-30-5 AND HFEC INSPECTION WAS ACCOMPLISHED PER NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND.

Part: SUPPORT — CRACKED (LT MLG DOOR) · airframe 70,504 hrs · 52,895 cycles

DOOR, CRACKED SUPPORT ON LT INBD MLG DOOR STA Y=962-970 AND X=30. LANDING GEAR DOOR WAS REPLACED.

Part: ACTUATOR — LEAKING (AIRSTAIR DOOR) · airframe 70,500 hrs · 52,893 cycles

DURING APPROACH, FLIGHT ATTENDANTS REPORTED A BURNING ODOR IN THE FORWARD GALLEY. MAINTENANCE FOUND HYDRAULIC FLUID IN THE APU INLET. DETERMINED THE SOURCE TO BE A LEAKING VENTRAL AIR STAIR ACTUATOR. THE ACTUATOR WAS REPLACED AND DUCT CLEANING AND BURNOUT WAS COMPLETED. (LP# 9137404)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,488 hrs · 52,885 cycles

LT AND RT OVERHEAD, OVERWING EXIT LIGHTS W/N ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53.

Part: STRUCTURE — MISSING (RUDDER) · airframe 70,465 hrs · 52,871 cycles

FLAME SPRAY MISSING ON RUDDER. REMOVED & REPLACED RUDDER. OK FOR SERVICE.

Part: TAB — MISSING (RUDDER) · airframe 70,465 hrs · 52,871 cycles

FLAME SPRAY MISSING ON RUDDER TAB. REMOVED & REPLACED RUDDER TAB. OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 69,707 hrs · 52,281 cycles

SEAT 24E EMERGENCY LIGHT BROKEN. R AND R SEAT 24E LOWER DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50, OPS CKS GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 69,396 hrs · 52,052 cycles

CREW REPORTS LOOSE WIRES AT SEAT 35D & 35E. FOUND EMERGENCY PATH LIGHTING WIRING DISCONNECTED AT SEVERAL SPLICES FROM SEAT 32D AND 32E TO 35D AND 35E. REPAIRED WIRING IAW WDM CHP 20 AND REPOSITIONED WIRING IN CHANNEL. ALL EMERGENCY PATH LIGHTS OPERATING FROM ROW 32 TO 35. OK FOR SERVICE.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 69,249 hrs · 51,951 cycles

DURING SERVICE CHECK FOUND ROW 24-30 EMERGENCY LIGHTS IN THE AISLE INOPERATIVE. R & R POWER SUPPLY 55-107 IAW MM 33-53-00. NO HELP. REPLACED FUSE FOR POWER SUPPLY B5-212. NO HELP. INSPECTED WIRING FOUND DISCONNECTED WIRE THAT WAS NOT SEATED CORRECTLY IN THE QUICK DISCONNECT PLUG. RECONNECTED WIRE AND CHANGED NEW FUSE IAW MM 33-53. OPS CHECK GOOD.

Part: HANDLE — NO TEST (TAILCONE RELEASE) · airframe 69,147 hrs · 51,880 cycles

TAILCONE FUNCTIONAL IAW AMDS 5350-01077-0101, STEP 11D. FAILED INTERIOR HANDLE PULL TEST 37LBS. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/007 00009 REINSTALLED AND TESTED TAIL CONE IAW AMM 53- 53-00, WITHIN LIMITS, 27LBS.

Part: RELEASE MECH — FAILED (TAILCONE) · airframe 69,147 hrs · 51,880 cycles

TAILCONE RELEASE MECHANISM CAM FAILED TORQUE CHECK OF AMDS 5350-01077-0101, STEP NR 12. SEE NR FOR ADDITIONAL INFORMATION 036-0001:5350-01077-0101/005 00007. REPLACED IAW AMM 53-53-02, AJUSTED AND TORQUED.

Part: DOOR — OUT OF ADJUST (L1 DOOR) · airframe 68,570 hrs · 51,482 cycles

F/A REPORTS LOUD HISSING & SQUEAL IN FLIGHT 1L DOOR. FOUND APPROXIMATELY 2" SPLIT IN LOWER FWD CORNER OF 1L DOOR. ACFT PRESSURIZED TO 4PSI. REMOVED L1 DOOR IAW AMM 52-11. INSTALLED AND ADJUSTED DOOR IAW AMM 52-11-00. SLIDE INSTALLED ON CARD 2561-4964.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 67,720 hrs · 50,855 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 28DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE CONNECTOR. THE CONNECTOR WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,399 hrs · 49,927 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT ROW 28 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE OTBD SEAT RAIL. THE CONNECTOR WAS REPLACED AND THE WIRE WAS REPAIRED. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,243 hrs · 48,381 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY PATHWAY LIGHTING SYSTEM WOULD NOT TURN OFF WHEN SELECTED TO. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND OPERATIONAL CHECKED GOOD.

Part: FAN — FAILED (RECIRCULATION) · airframe 63,326 hrs · 47,717 cycles

CREW NOTED STRONG ELECTRICAL FUMES THROUGHOUT CABIN DURING CRUISE FLIGHT. GALLEY POWER, CABIN LIGHTING, AND CIRCUIT BREAKERS FOR AIR RECIRCULATION FAN WERE ALL SECURED. FUMES THEN DIMINISHED AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION WITHOUT FURTHER PROBLEMS. MAINTENANCE REPLACED THE CABIN RECIRCULATION FAN AND CABIN AIR FILTER. OPS CHECKED GOOD AND NO OTHER ODORS NOTICED.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 62,505 hrs · 47,079 cycles

MX FOUND THAT THE TAILCONE RELEASE CABLE INNER SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE INTERIOR TELEFLEX CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 62,505 hrs · 47,079 cycles

MX FOUND THAT THE TAILCONE RELEASE CABLE SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 62,328 hrs · 46,970 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHTS AT ROW 23 IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS AT THE SEAT SIDEWALL UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.

Part: RUB STRIP — DAMAGED (BS 820) · airframe 61,819 hrs · 46,584 cycles

RT FWD LOWER FUSELAGE RUB STRIP STA 820 FOR NR 370, FOUND DEEP PREVIOUS BLENDS. .032" MATERIAL LOSS IS FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. EXISTING REPAIR FOUND AT 6" AND NEEDS TO BE INCORPORATED WITH NEW REPAIR IAW SRM 53-04, PARA 57 C. (4). FABRICATED DOUBLER IAW SRM 51-10-3. INSTALLED DOUBLER IAW SRM 31-30-5.

Part: SKIN — DENTED (BS 256) · airframe 61,819 hrs · 46,584 cycles

FUSELAGE SKIN BS 256 L17L DENTED. REPAIRED IAW SRM 53-04-3, PG 108, ITEM 8A.

Part: DOOR FRAME — CORRODED (BS 674) · airframe 61,819 hrs · 46,584 cycles

CENTER CARGO BAY LOWER DOOR FRAME BS 674 IS CORRODED. FABRICATED AND INSTALLED NEW SPACER AT BS 674 IAW SRM 51-30-05, 53-01, FIG 1-53-05, FIG 123 (OPTION 1), 51-10-3.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · airframe 61,819 hrs · 46,584 cycles

AFT CARGO DOOR FRAME HAS CORROSION AROUND RIVETS & FACE OF DOOR FRAME BS 1155-1212 BETWEEN L28-29. NO DAMAGE NOTED UNDER STRAP, FABRICATED AND INSTALLED STRAP IAW SRM 53-05, FIG 123, OPTION 1, 51-30-05 & 51-10-3.

Part: SKIN — DENTED (BS 237) · airframe 61,819 hrs · 46,584 cycles

FUSELAGE SKIN BS 237, L18L DENTED. FABRICATED DOUBLER, INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-04-5, PARA 4, 53-04-5 FIG 5, 51-10-3 & PSM 900-5-1, NR 4. THIS IS A CLASS 2 REPAIR IAW SRM 53-04-5, FIG 5 INSPECTION REQUIREMENTS IAW 53-04-5, TABLE 2.

Part: FRAME — CORRODED (BS 1380) · airframe 61,819 hrs · 46,584 cycles

AFT ACCESSORY COMPARTMENT FRAME AT BS 1380 LOWER RT SIDE SHOWS EVIDENCE OF CORROSION AROUND FASTENERS. REPLACED FRAME WITH FABRICATED IAW SRM 51-30-02, PARA 1, SRM 53-01, PARA 3, SRM 51-20-0, PARA. 4, DWG 9912246-109 & 9912246-121, SRM 51-10-4, PARA 2, SRM 51-10-3, PARA 21 & 14, SRM 51-10-3B & SRM 51-30-5, PARA 1.

Part: LONGERON — CRACKED (BS 160 L2L) · airframe 61,819 hrs · 46,584 cycles

LONGERON 2 LT IS CRACKED AT AND THROUGH FASTENER HOLE TO EDGE APPROX STA 160 "MARKED" MRB 53-038-05. REMOVED EXISTING LONGERON 2L REPAIR IAW SRM 51-30-02 AND 53-02 FIG 18, TOTAL 19" REMOVED. INSTALLED REPAIR STA 148 TO 120 IAW SRM 51-30-02, 51-30-05, AND 53-02, FIG 18, INSTALLED REPAIR TAB IAW PROCESS STANDARD 900-5-1.

Part: LONGERON — CRACKED (BS 200 L4L) · airframe 61,819 hrs · 46,584 cycles

LONGERON 4L IS CRACKED FROM FASTENER HOLE TO EDGE BS 200. REMOVED, FABRICATED, AND INSTALLED LONGERON REPAIR.

Part: LONGERON — CRACKED (BS 160 L3L) · airframe 61,819 hrs · 46,584 cycles

LONGERON 3L IS CRACK AT AND THROUGH FASTENER HOLE TO EDGE BS 160. CUT OUT LONGERON 3L, AND REMOVED BETWEEN BS 148 TO 170 IAW SRM 51-30-02 AND 53-02, FIG 18. FABRICATED REPAIR SPLICE AND INSTALLED LONGERON REPAIR IAW SRM 51-30-05, 51-30-02, AND 53-02 FIG 18.

Part: SKIN — DENTED (BS 256 L17L) · airframe 61,819 hrs · 46,584 cycles

FUSELAGE EXTERIOR BS 256 L17L DENTED. CUT-OUT DAMAGED AREA, FABRICATED DOUBLER, FABRICATED STRAP DOUBLERS, AND INSTALLED STRAPS DOUBLER, DOUBLER REPAIR AND FILLER & REPAIR IAW SRM 51-30-2, 53-04-3, FIG 4, 51-10-3,

Part: SEAT TRACK — CORRODED (BS 210) · airframe 61,819 hrs · 46,584 cycles

MAIN CABIN SEAT TRACK RBL 24 BS 210 HAS HEAVY CORROSION IN SCALLOPS AND CENTER OF TRACK MRB 53-037-01. REMOVED, FABRICATED, LOCATED, DEBURRED, TREATED PRIMED, TOP COATED, AND INSTALLED SEAT TRACK IAW SRM 53-05 FIG 48, 53-25-0 FIG 4, 51-30-05, 51-30-01, & 51-10-3.

Part: SKIN — CRACKED (BS 1420) · airframe 60,836 hrs · 45,873 cycles

UPPER AFT FUSELAGE SKIN AT BS 1420 BETWEEN L2 AND 3L IS CRACKED AROUND UPPER FASTENER AND FIVE WORKING FASTENERS. WORK WAS ACCOMPLISHED IAW ER/A 509075-14AD, REV ORIG.

Part: SKIN — CRACKED (BS 1420) · airframe 60,836 hrs · 45,873 cycles

AFT UPPER FUSELAGE SKIN AT BS 1420 BETWEEN L2 AND 3R IS CRACKED AT UPPER FASTENER AND HAS FOUR WORKING FASTENERS. WORK WAS ACCOMPLISHED IAW ER/A 509077-14AD, REV ORIG.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 60,126 hrs · 45,349 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE AISLE WAY AT SEAT 24DE WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED. RECONNECTED WIRE, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,239 hrs · 44,072 cycles

CORROSION ON CUSP WEB FROM STA 1174-1193 LBL 54 PREVIOUSLY EXPOSED AREA FOUND ON OK TO CLOSE STEP 10 OF T/C 0401N INSTALL SIDEWALL PNLS SAA102-CORROSION. FABRICATED DOUBLER AND TRIPLE REPAIR FROM 7075-T7 .025 BATCH NO.0002038990 PER ERA 398191-14MA. INSTALLED DOUBLER AND TRIPLER REPAIR AT MAIN CABIN CUSP WEB FS 1174-11*93 LBL 54 PER ERA 398191-14MA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,239 hrs · 44,072 cycles

L1 DOOR AREA FLOOR SECTION CORROSION FS 150 TO 175. CORROSION MAIN CABIN. FOUND AREA OUT OF LIMITS 100 PERCENT AT L1 DOOR AREA FLOOR FS 150-175 IAW DC9/MD80 SRM 53-01 FIG 1 SHEET 3 PG 8 00513 10-21-1110-21-11. REMOVED FLOOR SUPPORT L1 DOOR FS 150-175 IAW MD80 SRM 51-30-5 PG 29 FAB FLOOR SUPPORT WITH P/N 500074-12000 BATCH 500R784463 IAW MD80 SRM 53-14-1 FIG 11 SHEET 1-2 PG 27-29 00513 10/22/11 / 10/22/11.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,239 hrs · 44,072 cycles

L2 DOOR ENTRY WAY CUSP CORROSION ON AREA CA599 CACOSTA2058 -CORROSION AFT MAIN CABIN. HFEC SURFACE INSP IAW MD80 NDTSPM 06-10-01.001 NO CRACKS NOTED IN BLEND AREA. UT THICKNESS INSP IAW MD-80 NDTSPM 04-00-06 MINIMUM MATERIAL THICKNESS IN BLENDED AREA IS .046. AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 PG 68 .017 MATERIAL LOSS MAX ALLOWABLE .012 22OCT11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,239 hrs · 44,072 cycles

SDR - CUSP FLOOR SECTION CRACKED AT RBL 54 FS 218. CRACKED MAIN CABIN. FABRICATE DOUBLER AND TRIPLE REPAIR FROM 7075 T6 .025 BATCH NO.0002038990 PER ERA 398191-14MA. AT SAA/SAT DURING PAX MOD, ON W/O 89240720001.

Part: STOP FITTING — CORRODED (FUSELAGE) · airframe 57,429 hrs · 43,490 cycles

DURING PSV IN MSP CORROSION WAS FOUND ON FWD DOOR STOP FITTING OF THE AFT CARGO DOOR L28R. CORROSION REMOVED AND DOUBLER INSTALLED PER SRM 53-05 FIGURE 123.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 57,071 hrs · 43,233 cycles

DURING LINE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT AT ROW 35D INOPERATIVE. MX FOUND BROKEN WIRE ON LIGHT ASSY HARNESS. R & R LIGHT ASSY HARNESS, OPS CHECKS GOOD.

Part: COALESCER BAG — ODOR (CABIN) · airframe 57,062 hrs · 43,227 cycles

FLIGHT DIVERTED DUE TO STRONG ELECTRICAL ODOR AT 13,000 FT. GALLEY POWER WAS SWITCHED OFF. ODOR DISSIPATED THEN RETURNED. MX PERFORMED, COULD NOT DUPLICATE THE SMELL BUT REPLACED BOTH WATER SEPARATOR BAGS. ACFT IS OK FOR SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 56,512 hrs · 42,879 cycles

CREW WROTE UP BROKEN EXIT SIGN AT L1 DOOR. MAINTENANCE REPLACED EXIT SIGN ASSEMBLY PER M/M. OPERATION OF SIGN NOW CHECKS GOOD. (2011-D0194)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,526 hrs · 42,053 cycles

MX FOUND THE EMERGENCY LIGHT AT SEAT 3C TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — DISCONNECTED (SEAT 3C) · airframe 53,842 hrs · 41,068 cycles

SEAT 3C EMERGENCY LT INOP. RE-CONNECTED ASSY.

Part: PLATE — CORRODED (BS 1680) · airframe 50,360 hrs · 38,838 cycles

MAIN CABIN AFT DECK PLATE STA 1680 LBL 47 TO RBL 51 HAS CORROSION ON UPPER SURFACE, REPAIRED.

Part: SKIN — DAMAGED (EMERGENCY EXIT) · airframe 50,292 hrs · 38,794 cycles

CREASE ON EXTERNAL SKIN OF AFT LT WING EMERGENCY EXIT DOOR REPAIRED.

Part: SEAT TRACK — CORRODED (BS 680-710) · airframe 50,274 hrs · 38,786 cycles

SEAT TRACK HAS EXFOLIATED CORROSION AT STA 680-710 LBL 24.5, REPLACED SECTION.

Part: DOUBLER — CORRODED (STA 1470 S29-30R) · airframe 50,225 hrs · 38,751 cycles

LOWER EXTERNAL FUSELAGE AT FS 1470 VHF ANT MOUNT HAS CORROSION BETWEEN 29R AND 30. REPLACED DOUBLER.

Part: INDICATOR — UNSERVICEABLE (COCKPIT) · airframe 47,667 hrs · 37,064 cycles

ABORTED T/O AGAIN REPEAT CAPT AIRSPEED INDICATOR FLAG IN VIEW. F/O INDICATOR READ 40 KTS. REPLACED CAPT MACH/AIRSPEED INDICATOR PER M/M. SYS CKS GOOD WITH AIR DATA TEST SET. POWER FOR NR 1 ADC C/B CKS GOOD. INFO ON FIRST RTO, FOUND NR 1 ADC FAILING SELF TEST. REPLACED SAME PER M/M. REPLACED MACH/ASPD IND PER M/M SYS CK GOOD WITH AIR DATA TESTER FOR NR 1 CADC. C/B CKS GOOD.

Part: WEB — CRACKED (STA 1463) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACKED WEB AT STA 1463 BETWEEN LONGERON 21-23 LT. REPAIRED PER SRM 53-01 FIG 2 ON N/R T0060676 AT HMV.

Part: CUSP WEB — CORRODED (BS 663) · airframe 47,202 hrs · 36,740 cycles

CORROSION ON RT CUSP WEB AT STA Y=663, TASK 58-53313. REPAIRED PER ERA 398191-14MA ON N/R T0060304 AT HMV.

Part: FRAME — CRACKED (BS 905) · airframe 47,202 hrs · 36,740 cycles

CRACK ON FORMER STA Y=905 X=-58. DOUBLER MANUFACTURED PER SRM 51-70-5 FIG 1 ON N/R T0060286 HMV-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,202 hrs · 36,740 cycles

SKIN DENT BELOW R-1 SERVICE DOOR,FOUND TO BE WITH IN LIMITS PER SRM 53-04D TABLE C. REPAIRED PER SRM 53-04D FIG 38 COND 1B VIEW E ON N/R T0060082 HMV-3.

Part: LONGERON — CRACKED (BS 160 S2L) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACK ON LONGERON 2 LT AT STA 160. REPAIRED PER 53-02 FIG 18 ON NR T0060398.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACK ON STIFFENER AT STA Y=1338 LONGERON 01, TASK 58-53309. REPLACED PER DWG 9915562 ON N/R T0060516 AT HMV.

Part: CUSP WEB — CORRODED (BS 1174-1193) · airframe 47,202 hrs · 36,740 cycles

FOUND CORROSION ON LEFT CUSP WEB BETWEEN STA Y=1174 AND 1193, TASK 58-533313. REPAIRED PER SRM 51-70-4 ON N/R TOO60302 AT HMV.

Part: ANGLE — CORRODED (LT WING) · airframe 47,202 hrs · 36,740 cycles

EXFOLIATION CORROSION ON LT TRAPAZOIDAL PANEL UPPER ANGLE. ANGLE WAS REPLACED PER DWG 5930515 ON N/R TOO60106 HMV-3.

Part: FRAME — CORRODED (BS 1309 L27R-28L) · airframe 47,202 hrs · 36,740 cycles

FOUND CORROSION ON FRAME AT STA. Y=1309 LONGERON 27 RT-28 LT, TASK 57-53300. REPAIRED PER SRM 53-01 FIG 1 ON N/R T0061108 AT HMV.

Part: INTERCOSTAL — CORRODED (BS 1380-1401) · airframe 47,202 hrs · 36,740 cycles

EXFOLIATION CORROSION ON INTERCOSTALS BETWEEN FRAME 1380 AND 1401 IN AFT FUSELAGE LOWER SECTION. REPLACED INTERCOSTAL REF DWG BOEING 9919661 ON NR T0060687 AT HMV GDL.

Part: LONGERON — CRACKED (BS 160 L3L) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACK ON LONGERON 3 LT AT STA 160. REPAIRED PER SRM 53-02 FIG 18 ON N/R T0060396 AT HMV.

Part: LONGERON — CRACKED (BS 160 L4L) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACK ON LONGERON 4 LT AT STA 160. REPAIRED PER SRM 53-02 FIG 18 ON N/R T0060397 AT HMV.

Part: CUSP WEB — CRACKED (BS 840) · airframe 47,202 hrs · 36,740 cycles

FOUND CRACK ON RT CUSP WEB AT STATION Y=840, REPAIRED PER ERA 398191-14MA ON N/R T0060308 AT HMV.

Part: SKIN — DELAMINATED (LT WING) · airframe 47,202 hrs · 36,740 cycles

THE LT INBOARD FLAP OUTBOARD GUIDE VANE WAS FOUND DELAMINATED AT HMV. THE DAMAGE WAS REPAIRED PER ER/A 462557-14 AND APPROVED PER BOEING MESSAGE 1-387586211-3, DATED JUNE 25, 2007.

Part: SKIN — CRACKED (BS 1437) · airframe 47,202 hrs · 36,740 cycles

TWO CRACKS (.500" AND .750") WERE FOUND IN THE FUSELAGE SKIN AT FS 1437 BETWEEN RT L-1 AND L-4. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 462554-14 AND APPROVED BY BOEING MESSAGE 1-385059352-2.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 46,600 hrs · 36,346 cycles

HORIZONTAL STABILIZER/LT/UPPER AFT SKIN AND REAR SPAR : CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE LT HORIZ STAB WAS FOUND WITH A 1.85" LONG CRACK NEAR THE INBD AFT EDGE OF THE PANEL. UPON REMOVAL OF THE CRACKED PANEL, THE UPPER SPAR CAP WAS FOUND WITH A 5/8" CRACK NEAR THE INBD END IN THE VERTICAL FLANGE OF THE CAP. BOTH THE SKIN AND SPAR CAP ARE BEING REPLACED PER OEM DRAWINGS AND DOCUMENTED PER ER/A 460237-14.

Part: FITTING — CORRODED (LT MLG) · airframe 44,985 hrs · 35,247 cycles

CORROSION WAS FOUND ON THE LT MLG RETRACT CYLINDER SUPPORT FITTING BUSHING. THE FITTING BORE WAS OVERSIZED TO REMOVE THE CORROSION REF AD 2004-25-14.

Part: UPLOCK SENSOR — INTERMITTENT (NLG) · airframe 44,789 hrs · 35,119 cycles

NOSE GEAR UNSAFE AFTER GEAR RETRACTION. CYCLED GEAR AND LIGHTS WERE NORMAL. COMPLIED WITH OPN 50006. LANDING GEAR STRUT TROUBLESHOOTING. NO TROUBLE FOUND. TMC SUGGESTS REPLACE NOSE GEAR SENOR. REPLACED UPLOCK SENSOR D1-32. A/C OK FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 44,305 hrs · 34,780 cycles

AFTER T/O LEFT MAIN GEAR UNSAFE RED LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST. RECYCLED GEAR AND LIGHT EXTINGUISHED. JACKED A/C, FOUND LT MLG DOWNLOCK CONDUIT RUBBING UPLATCH, LOCK SENSOR BACKSHELL REPOSITIONED CONDUIT RAN GEAR SEVERAL WITH NO TROUBLE FOUND. DOWN JACKED A/C, REMOVED JACK PADS, ALSO VERIFIED UPLATCH ACTUATOR NOT GETTING HOT. A/C OK FOR SERVICE.

Part: TAIL CONE — DEPLOYED · airframe 42,682 hrs · 33,590 cycles

EMS SERVICES BLEW TAIL CONE AT PHL. REPLACED TAIL CONE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 42,479 hrs · 33,447 cycles

AFTER T/O AND T/O CHECKLIST STEP WHERE HYD AUX AND TRANS PUMPS OFF. ACFT LOST RT HYD SYSTEM PSI AND QTY, DID CHECKLISTS INCLUDING ALTERNATE GEAR EXT CONFIGURED AND LANDED NORMALLY. GEAR DOOR OPEN, LAND WEIGHT 134,000 SINK RATE AT LANDING APPROX 50 FT PER MIN. MX INSTALLED GEAR PINS AND RESTORED DOORS TOWED TO GATE. FOUND FLEX LINE TO SYS PRESS FILTER HOUSING LEAKING. REMOVED AND REPLACED FLEX LINE, RAN ENG. FLEX LINE, LEAK CHECKS GOOD.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 37,361 hrs · 29,829 cycles

AFTER T/O GEAR WOULD NOT RAISE, HANDLE NML 3 RED, AURAL INDICATIONS GEAR DOWN. TOWER CONFIRMED ALL GEAR DOWN. DROP GEAR 3 GREEN, ALL HYD INDICATIONS NML. GROUND SENSE DID NOT SENSE WEIGHT ON WHEELS, SPOILER DEPLOYED MANUALLY. DEPRESSURIZED MANUALLY. ON W/A FOUND DOOR BYPASS HANDLE OPEN SECURED SAME. JACKED A/C OPENED BYPASS HANDLE AND VERIFIED PROBLEM. CLOSED BY PASS HANDLE AND CYCLED GEAR SEVERAL TIMES ALL INDICATIONS NORMAL, OK FOR SERVICE.

Part: SENSOR — FAULTY (A/C BAY) · airframe 37,284 hrs · 29,775 cycles

IR: TAIL COMPARTMENT TEMP HI LIGHT CAME ON AT 400 FT. REPLACED TAIL TEMP HI SENSOR. RAN ENGINES TO TAKEOFF POWER. ALL INDICATIONS NORMAL.

Part: RELAY — FAILED (#2 ENGINE) · airframe 33,317 hrs · 26,985 cycles

INFLIGHT SHUTDOWN OF NBR 2 ENGINE. DIVERSION TO CSG. INCREASING OIL TEMP. TEMP REACHED 142 DEG, ENG SHUTDOWN AFTER 15 MINUTE LIMIT REACHED. MAINTENANCE DISPATCHED FROM DELTA NORTH ATL TO CSG. FOUND RIGHT ENG FUEL HEAT TIMER RELAY NOT SHUTTING OFF, CAUSING FUEL TO OVERHEAT OIL THROUGH FUEL/OIL COOLER. REPLACED RELAY 249201336. EQUIPMENT NBR R2-65, LOC 110 RELAY PANEL IN E&E COMPARTMENT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,317 hrs · 26,985 cycles

RIGHT ENG OIL TEMP CAUTION WAS ILLUM WITH THE TEMP AT 142 DEGS. INCREASED THRUST FOR 15 MINS AND TEMP DID NOT DECREASE. PER POM SHUTDOWN ENG. ENG WINDMILLED FOR 20 MINS ZERO OIL PRESS. PERFORMED ALL REQUIRED CHECKS, NO TROUBLE FOUND.

Part: INDICATOR — SMOKE (COCKPIT) · airframe 30,073 hrs · 24,545 cycles

SMOKE IN COCKPIT DURING FLT, STRONG SMELL IN COCKPIT AND VISIBLE SMOKE BY CO-PILOT LEGS. REPLACED WEATHER RADAR INDICATOR.

Part: LINE — CHAFED (LEFT ENGINE) · airframe 29,087 hrs · 23,804 cycles

AFTER TAKEOFF, LEFT HYD QUANTITY DECREASED TO 0. FOUND LEFT HYDRAULIC PRESSURE FILTER LINE CHAFED. REPLACED SAME.

Part: SENSOR — FAILED (APU)

AT V1, APU FLAMED OUT 122 KNOTS AND ELECTRICAL LOAD WAS PICKED UP BY RIGHT ENGINE ONLY. DID NOT ATTEMPT TO RESTART APU. RETURNED TO DFW. REPLACED PS SENSOR AND SET APU FOR VERIFICATION FLIGHT.

Part: BATTERY — DISCHARGED (CABIN)

ON PREFLIGHT, FOUND EMER FLASHLIGHT AT FWD FLT ATTEND STA NOT TESTING. REPLACED BATT.

Part: LIGHT — INOPERATIVE (CABIN)

ON PREFLIGHT, FOUND EMER FLASHLIGHT AT FWD F/A STATION TEST INOP. REPLACED FLASHLIGHT AND BATT.

Part: LIGHTS — ODOR (CABIN)

STRONG ELECT FUMES AT GATE DETERMINED TO BE FROM UPPER SIDE WALL LIGHTS ROW 3CD AND 4CD. PULLED AND COLLARED C/B FOR UPPER SIDE WALL LIGHTS RT SIDE OF ACFT.

Part: Z-CHANNEL — CRACKED (LT MLG DOOR)

LT MAIN LANDING GEAR DOOR INNER PAN Z-CHANNEL HAS CRACK APPROX 3.25 INCH LONG RUNNING IN THE AFT RADIUS ALONG THE AFT EDGE OF SUBJECT CHANNEL, 19.5 INCHES FROM THE AFT I/B CORNER STRAP. A REPAIR ANGLE WAS USED TO REPAIR THIS CRACK. REV A AND B REVISED THE PERMANENT REPAIR INSTRUCTIONS, PERMANENT REPAIR PER SRM 52-05 FIG 28.

Part: SKIN — SCRATCHED (FUSELAGE)

DURING LETTER CHECK, FOUND FUSELAGE SKIN WITH A DEEP SCRATCH BELOW NR 2 ENGINE PYLON, JUST FWD OF AFT CARGO DOOR. REPAIRED PER SRM 53-04.