N903DA

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 51,117 hrs · 27,445 cycles

LT SIDEWALL AFT EMERGENCY STAIRWELL LIGHT IS INOPERATIVE. FOUND AND REPAIRED BROKEN WIRE IN TAILCONE AREA BEHIND LEFT AFT BULKHEAD. OPS CHECKED GOOD.

Part: SKIN — CRACKED (BS 1475) · airframe 50,803 hrs · 27,244 cycles

FUSELAGE, SKIN BS 1475 L1-2R CRACKED. REPAIRED IAW ERA 524612-14

Part: FINGER DOUBLER — CRACKED (BS 1520) · airframe 50,943 hrs · 27,331 cycles

CRACKED FRAME TO SKIN FINGER DOUBLER AT L2R FORWARD SIDE OF STA 1520 FRAME. NR 62. REPAIRED CRACKED DOUBLER IAW SRM 53-10-03, FIG 20 AND ERA 524742-14, REV O.

Part: WEB — CRACKED (BS 1542) · airframe 50,780 hrs · 27,232 cycles

WEB CRACKED AT FASTENER BS 1542, AT 11:00 O`CLOCK POSTION. REPAIR ACCOMPLISHED IAW SRM 53-10-03, FIG 16.

Part: SKIN — CRACKED (BS 1475) · airframe 50,780 hrs · 27,232 cycles

CROWN SKIN CRACKED BETWEEN FASTENERS OF PREVIOUS REPAIR, BS 1475, RBL 5. REPAIRED CRACK IAW ERA 524612-14, REV O, SECTION I, SECTION II PERFORMS REPETATIVE INSPECTION EVERY 3000 CYCLES.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 50,780 hrs · 27,232 cycles

CRACK FOUND VERTICAL STAB SKIN AT BS 1475, L2R. ERA 524612-14, SECTION I WAS ACCOMPLISHED IN MSP.

Part: SEAL DEPRESSOR — CRACKED (E/E BAY DOORWAY) · airframe 50,780 hrs · 27,232 cycles

NOSE WHEEL WELL UPPER E & E COMPARTMENT DOOR SEAL DEPRESSOR IS CRACKED IN RADIUS, AFT CENTER LINE. REPAIR IAW ERA 524592-14, REV O.

Part: DOOR FRAME — CORRODED (BS 1212-1226) · airframe 50,780 hrs · 27,232 cycles

AFT CARGO LOWER FRAME CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER REPAIR BS 1212 - 1226 IAW SRM 53-60-02.

Part: CHANNEL — CRACKED (BS 984) · airframe 50,780 hrs · 27,232 cycles

FRAME BS 984, RT SIDE, FORWARD CROSSTIE, CRACKED AT FRAME TO FLOORBEAM. REMOVED, FABRICATED AND INSTALLED NEW CROSSTIE CHANNEL IAW SRM 51-00-01.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 50,238 hrs · 26,915 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS ON AFT CATWALK FOUND INOPERATIVE. R & R QUICK DISCONNECTORS IAW SWPM. OPS CHECKED GOOD.

Part: CABLE — FRAYED (GIRT BAR) · airframe 49,850 hrs · 26,655 cycles

L2 GIRT BAR CABLE FRAYED. MAINTENANCE REMOVED AND REPLACED GIRT BAR LANYARD PER AMM.

Part: SWITCH — INOPERATIVE (TAILCONE RELEASE) · airframe 49,109 hrs · 26,200 cycles

DURING TAILCONE RELEASE OPS CHECK, FOUND EXTERNAL TAILCONE RELEASE SWITCH INOPERATIVE, TAILCONE UNSAFE SWITCH. R & R SWITCH FOR EXTERNAL HANDLE RELEASE. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,769 hrs · 25,458 cycles

RT EXIT DOOR, AFT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 45,965 hrs · 24,373 cycles

DUE PERMANENT REPAIR PER ERA 490525-14AD REV A CODE 55-11. ACTL 2102-2100. STAB HORIZ RT UPPER AFT SKIN CRACK. ACCOMP SEC III PERM REP INSTR PRIOR TO 6000 CYC. ACCOMPLISHED PERM REPAIR PER ERA 490525-14AD REV B. DURING HMV AT SAA ON N/R CARD 192663.

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 45,964 hrs · 24,372 cycles

WHILE ACCOMPLISHING ERA 490525-14AD REV A SECT 1, REPLACEMENT OF UPPER SKIN PANEL ON RT HORIZONTAL STAB WAS TRIMMED TO SHORT CAUSING SHORTED ON EDGE FASTENERS AND TRIM LINE GAP TO BE WIDER THAN REQUIRED. ACCOMPLISHED PRI 490525-14AD REV 0, 1, 2.

Part: FLOOR PANEL — CORRODED (BS 180-185) · airframe 45,964 hrs · 24,372 cycles

RT CABIN FLOOR PANEL STA 180-185 HAS CORROSION OUT OF LIMITS PER VOL 1 SRM 53-00-01 P9 FIG 3. FABRICATED NEW FLOOR PANEL, TREATED PAINTED PER VOL 2 SRM 51-10-03 P83. INSTALLED FLOOR PANEL IAW SRM VOL 2 51-30-05 PG 10A PAR 7.

Part: INTERCOSTAL — CRACKED (BS 169 LBL 55) · airframe 45,964 hrs · 24,372 cycles

AFTER REMOVAL MAIN CABIN FLOOR PANEL WEB, FOUND INTERCOSTAL CORRODED AND BROKEN THRU AT STA 169 LBL 55. REMOVED INTERCOSTAL AT MAIN CABIN STA 169 LBL 55 IAW MD90 SRM 51-30-02 PG1 VOL 2. FABBED INTERCOSTAL. INSTALLED INTERCOSTAL IAW MD90 SRM 51-10-05 PG 1 AND MD90 SRM 51-30-02 PG 1. AT SAA/SAT DURING HMV.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

LT EXTERIOR FUSELAGE INCOMING DOUBLER REPAIR BETWEEN STA 229-237 AND L17L-L18L NOT PER ERA#476094-14 REV B AND SOME RIVETS BUCK TAIL ARE DEFORMED. C/W ERA 476094-14 REV D.

Part: BUSHING — CORRODED (RT MLG) · airframe 45,964 hrs · 24,372 cycles

CORROSION ON RT MLG RETRACT ACT SUPPORT FITTING BUSHING BORE. FOUND UPON REMOVAL OF FITTING BUSHING PER EA 02-093855-03 AD REV A OPN 0201. C/W IAW EA 02-093855-03 AD REV A OPN 0201 AND SAA NR 225670. DURING HMV AT SAA/SAT.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

LT EXTERIOR FUSELAGE INCOMING DOUBLER REPAIR BETWEEN STA 229 TO 237 AND LONGERONS 17L TO 18L NOT PER ERA 476094-14 REV B AND SOME RIVETS BUCKTAILS ARE DEFORMED. REPAIR TO BE REPLACED DURING HMV.

Part: BUSHING — CORRODED (LT MLG) · airframe 45,964 hrs · 24,372 cycles

CORROSION ON LT MLG RETRACT ACT SUPPORT FITTING BUSHING BORE. FOUND UPON REMOVAL OF FITTING BUSHING PER EA 02-093855-03 AD REV A OPN 0101. C/W IAW EA 02-093855-03 AD REV A OPN 0101 AND SAA NR 225669. DURING HMV AT SAA/SAT.

Part: SEAT TRACK — CORRODED (BS 1260-1364) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 44 HAS CORROSION & GOUGES FROM BS 1260 TO 1364. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM SRM 53-40-01.

Part: CUSP WEB — CORRODED (BS 664-693) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION FROM BS 664 TO 693. CUSP WEB CORROSION REPAIRED PER ERA398191-14MA.

Part: CUSP WEB — CORRODED (BS 693-731) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION BETWEEN BS 693 TO 731. REMOVED CORROSION, FOUND AREAS OUT OF LIMITS, REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED, COMPLIED WITH ERA 501651-14 REV A.

Part: SEAT TRACK — CORRODED (BS 1290-1364) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 55 HAS CORROSION & GOUGES FROM STA 1290 TO 1364. BLENDED CORROSION AND GOUGES, FOUND AREAS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SEAT TRACK, FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-30-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT RBL 22 HAS CORROSION/GOUGES FROM STA 972 TO STA 1069. BLENDED SEAT TRACKS IAW MD90 SRM 53-40-01 PG 22 AND 23. STA 1059 RBL 22 CROWN AREA OUT OF LIMITS IAW 53-40-01 PG 20 THRU 23. REMOVED SEAT TRACK FROM STA 972 THRU 1069 RBL 22 IAW MD90 SRM 51-30-05 PG 15. INSTALLED SEAT TRACK AT SAME LOCATIONS IAW MD90 SRM 51-30-05 PG 15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT RBL 55 HAS CORROSION FROM STA 588-854. CUT OUT DAMAGE CROWN ON SEAT TRACK AT MAIN CABIN STA 641 RBL 55 PER MD90 SRM 52-40-01 PG 5. INSTALLED NEW PLUG AND NUT PLATE CHANNEL ON STA 641 RBL 55 REF MD90 51-30-01 AND 53-40-01 FIG 6. AT SAA SAT IN HMV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 22 HAS CORROSION/GOUGES FROM 854 TO STA 1069 AND A DRILL START AT STA 991.5 / REMOVED CORROSION ON SEAT TRACKS AT STA 854 TO 1069 IAW MD90 SRM 51-10-3 PG 46-48 PARA 26 AND MD90 SRM 53-40-01 PG 22. FOUND TO BE OUT OF LIMITS PER MD90 SRM 53-40-01 PG 22-22B. INSTALLED 2EA SEAT TRACK, 2EA SPLICE, 2EA PLATE AT MAIN CABIN LBL 22 FROM STA 854 TO STA 1069 PER MD90 SRM 51-30-05 VOL 2 PG 10A AND MD90 SRM 53-40-01 FIG 6 AND INSTALLED ID IAW PS 900-5-1 NO 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 22 HAS CORROSION AND GOUGES FROM STA 588-854. OUT OF LIMITS CUT AND REMOVED DAMAGED SECTION STA668-797. INSTALLED NEW SET TRACK AND SPLICES STA674-797 LBL22 IN REF MD90 SRM 53-40-01 PG 30-36. AT SAA SAT IN HMV.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION FROM BS 731-750. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW ERA 501651-14 REV O. REPAIRS MADE PER PRI 501651-14 REV O, ERA 501651-14 REV A.

Part: SEAT TRACK — CORRODED (BS 1145-1203) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL HAS CORROSION/GOUGES FROM STA 1145-1203. DAMAGE IS OUT OF LIMITS. REPLACED SEAT TRACK SECTION STA 1069 - 1180 LBL 22. PER SRM 53-40-01 VOL 1.

Part: SEAT TRACK — CORRODED (BS 854-972) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT RBL 53 HAS CORROSION/GOUGES FROM BS 854-972. FOUND OUT OF LIMITS PER MD90 SRM 53-40-01 PG 20-23. REPLACED SEAT TRACK PER SRM 53-40-01 PG 6 VOL 1 AND 51-30-01 PG 1 PAR 2.

Part: SEAT TRACK — CORRODED (BS 608-854) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 55 HAS CORROSION/GOUGES FROM BS 608 TO 854. REMOVED CORROSION, FOUND TO BE OUT OF LIMTS. REPLACED SEAT TRACK IAW SRM SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 284-588) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK IS GOUGED AND CORRODED BS 284-588 RBL 55. REMOVED DAMAGE ON SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 854-1088) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT LBL 55 HAS CORROSION & GOUGES FROM BS 854 TO 1088. BLENDED DAMAGED AREAS ON SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTON IAW SRM 53-20-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

CORROSION ON DOUBLER AT AFT PRESSURE BULKHEAD BOTTOM SDGE AREA LBL 4-RBL 4. FABRICATED DOUBLER AND INSTALLED PER MD90 51-30-05 P10A. AT SAA SAT HMV.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

CORROSION ON AFT PRESSURE BULKHEAD T-ANGLE SUPPORT BL 0 LOWER END. FABRICATED NEW T-ANGLE AND INSTALLED PER MD90 53-10-03 PG 21 FIG 21 SHEET 2.

Part: SEAT TRACK — DAMAGED (BS 588-854) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT RBL 22 HAS CORROSION & GOUGES FROM BS 588 TO 854. REMOVED CORROSION FROM SEVERAL AREAS, FOUND SCALLOPED AREAS TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BS 665 TO 778 IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 400-588) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK BS 231-588 LBL 55 HAS GOUGES AND CORROSION. CORROSION OUT OF LIMITS PER SRM 53-40-01 PG 22-23. FABRICATED NEW SEAT TRACK PER SRM 53-40-01 FIG 6 VOL 1. INSTALLED TRACK AND STRAPS AND FITTINGS PER SRM 53-40-01 FIG 6 VOL 1.

Part: SEAT TRACK — GOUGED (BS 313-588) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK HAS GOUGES BS 588 -313 LBL 22. REMOVED DAMAGE ON SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK AND REPLACED IAW SRM 51-30-01.

Part: SHEAR TIE — CORRODED · airframe 45,964 hrs · 24,372 cycles

VENTRAL STAIR NR 9 STEP, FWD FRAME SHEAR TIE, AFT FRAME, LOWER ANGLE, LEFT AND RIGHT BULKHEAD LOWER ANGLES AND CORNERS ABOVE PANEL LANDS AND LEFT, RIGHT AND AFT STEP LANDS HAVE CORROSION. REMOVED CORROSION FROM AREAS, REPLACED SHEAR TIE AND ANGLE FOUND TO BE OUT OF LIMITS. SHEAR TIE FOUND DAMAGED BEYOND LIMITS, FABRICATED AND INSTALLED SHEAR TIE PER SRM 51-30-02.

Part: SEAT TRACK — DAMAGED (BS 1145-1303) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN SEAT TRACK AT RBL 55 HAS CORROSION & GOUGES FROM BS 1145 TO 1303. BLENDED CORROSION, FOUND SOME AREAS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 1145-1212) · airframe 45,964 hrs · 24,372 cycles

A/C LEFT GALLEY 3, THE MIDDLE SEAT TRACK HAS CORROSION AROUND 3 EA FASTENER HOLES STA 1212-1145 INBD OF L-2. REMOVED CORROSION AT G3 MID SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-01.

Part: CUSP WEB — CORRODED (BS 962-984) · airframe 45,964 hrs · 24,372 cycles

RIGHT CUSP WEB IS CORRODED STA 962-984 RBL 56-60. REMOVED CORROSION, ACCOMPLISHED ERA 39819-14MA REV B.

Part: CUSP WEB — CORRODED (BS 984-1003) · airframe 45,964 hrs · 24,372 cycles

RIGHT CUSP WEB IS CORRODED STA 984-1003 RBL 58 IN MAIN CABIN. CORROSION ON CUSP WEB REPAIRED PER SRM 53-10-01.

Part: CUSP WEB — CORRODED (BS 1211-1288) · airframe 45,964 hrs · 24,372 cycles

RIGHT CUSP WEB IS CORRODED IN MAIN CABIN BS 1211-1288 RBL 56-60. REMOVED CORROSION, REMOVED DAMAGED AREAS OF CUSP WEB FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-10-03.

Part: CUSP WEB — DAMAGED (BS 1041-1062) · airframe 45,964 hrs · 24,372 cycles

RIGHT CUSP WEB LIGHTING HOLES ARE DAMAGED BS 1041-1062 RBL 56-60 IN MAIN CABIN. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED FILLERS, DOUBLER AND TRIPLERS, COMPLIED WITH ERA 501651 REV A.

Part: CUSP WEB — CORRODED (BS 1136-1211) · airframe 45,964 hrs · 24,372 cycles

RIGHT CUSP WEB IS CORRODED STA 1136-1211 RBL 56-60. REMOVED CORROSION, FOUND WEB CRACKED. CUT OUT DAMAGED AREA , FABRICATED REPAIR AND INSTALLED IAW ERA 398191-14MA.

Part: WEB — CRACKED (BS 1211-1288) · airframe 45,964 hrs · 24,372 cycles

RT CUSP WEB IS CORRODED IN MAIN CABIN BS 1211-1288 RBL 56-60. REMOVED CORROSION REF MD90 SRM VOL 2 51-10-03 PG 46. CRACK FOUND AT STA 1236. REMOVED DAMAGE AREAS PER MD90 SRM 53-20-21 VOL 1 PG 157 FIG 18. CW PRI 501651-14 ERA 501651-14 REV A, AT SAA/SAT DURING HMV.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

L1 DOOR JAMB I/B THRESHOLD ATTACH ANGLE HAS CORROSION AT FASTENER HOLES. REMOVED CORROSION FROM L1 DOOR JAMB I/B THRESHOLD ATTACH ANGLE IAW MD90 SRM 51-10-03 VOL 2 PG 46. FOUND TO BE OUT OF LIMITS IAW MD90 SRM 53-00-01 VOL 2 PG 6. REMOVED AND INSTALLED NEW ATTACH ANGLE IAW MD90 SRM 51-30-02 VOL 2 PG 1. AT SAA/SAT DURING HMV.

Part: RUB STRIP — MISSING (FAIRING) · airframe 45,964 hrs · 24,372 cycles

LT WING TO BODY FAIRING LOWER RUB STRIP IS MISSING AT STA 864-885 AND AT RT LOWER SIDE STA 865. ACCOMPLISHED ERA 501656-14 REV ORIG DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: SHEAR TIE — CRACKED (BS 1231 L7L) · airframe 45,964 hrs · 24,372 cycles

MAIN CABIN FRAME SHEAR TIE STRUCTURE IS CRACKED AT STA 1231 AND LONGERON 7L. CUT OUT DAMAGE PER MD90 SRM 53-10-02 PG 36 FIG 4 AND FABRICATED REPAIR. INSTALLED REPAIR PER MD90 SRM 51-30-02 PG 1 VOL 2, 51-30-05 PG 10A AND 53-10-02 PG 36 FIG 4. REPAIR IS A CAT B REPAIR WITH THRESHOLD INSPECTION TO START OR BEFORE 44372 FLT CYCLES AND REPEAT INSPECTION EVERY 6000 FLT CYCLES THEREAFTER AC IS CURRENTLY AT 24372 FLT CYCLES.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

CABIN FLOOR RT CUSP WEB BETWEEN STA 489-503 FWD AND MID LIGHTENING HOLES ARE CORRODED. REMOVED CORROSION ON CUSP WEB FROM STA 489-503.100% MATERIAL LOSS. REF MD90 VOL2 51-10-03 PG 46.CW ERA 398191-14MA ERVB . AT SAA SAT IN HMV.

Part: CUSP WEB — CORRODED (BS 210) · airframe 45,964 hrs · 24,372 cycles

A/C CABIN LT CUSP WEB BS 210 HAS CHAFING MARKS. REMOVED CORROSION, FOUND CRACK ON WEB, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 45,964 hrs · 24,372 cycles

ACCOMPLISH ACTIONS PER OMI LOG W/CN C03171305 DUE PERM REPAIR ERA 490525-14AD REV A CODE 55-11 ACTL 2102/2100 STAB HORIZ RT UPPER AFT SKIN CRACK ACCOMP SEC III PERM REPAIR IN STR PRIOR TO 600 CYC. REQ 1EA P/N SA90550012-5 PANEL SPLICE INSTALL KIT UPPER RIGHT. TO BE COMPLETED ON (NR 192663).

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

LOWER FUSELAGE PREVIOUS REPAIR HAS AN OUTWARD DENT AT STA 262 BETWEEN L23R/L24R. C/W ER/A 384598-14 REV D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,964 hrs · 24,372 cycles

ACCOMPLISH PERM REPAIR AT FUSELAGE SKIN FS 1475 L1-R AND 2-R CRACK. THIS REQUIRES CONTACTING LIASON ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS. PERMANENT REPAIR PER ERA 477091-14 AD REV C CODE 2-53-31-40.

Part: FLOORBEAM — CORRODED (BS 160 RBL 29) · airframe 45,964 hrs · 24,372 cycles

E&E BAY BS 160 RBL 29 AFT SIDE OF CABIN FLOORBEAM IS CORRODED AT DOME NUT 77-65RE. CORROSION OUT OF LIMITS PER SRM 53-00-01 PG 9. ACCOMPLISHED PRI 501030-14 REV 0, 1 AND 2, ERA 501030-14 REV ORIG.

Part: OVEN — OVERHEATED (GALLEY) · airframe 45,421 hrs · 24,129 cycles

FLIGHT CREW REPORTED THE FORWARD GALLEY OVEN GOT HOT AND HAD A STRONG ODOR. CREW PULLED CIRCUIT BREAKER ABOVE OVEN. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY OVEN PER AMM 25-35. OPERATION CHECKS GOOD. REMOVED (LP C12061126).

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,333 hrs · 23,137 cycles

RT HORIZONTAL STABILIZER UPPER SKIN CRACK ERA 490525-14REV ORIG TIME LIMITED REPAIR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,255 hrs · 21,627 cycles

EMERGENCY ESCAPE PATH LIGHT. ONE BULB INOP. REPAIRED WIRE AND RELAMPED - OPS OK - MCO/PLAC RMVD.

Part: SEAL — DAMAGED (NLG STRUT) · airframe 40,089 hrs · 21,527 cycles

ON T/O ROLL AUTOSPOILER FAIL MESSAGE ILLUMINATED. WHEN GEAR WAS RETRACTED THE GEAR HANDLE ONLY CAME HALFWAY UP AND ALL 3 GEAR LIGHTS WENT RED. THE GEAR HANDLE WAS RETURNED TO THE DOWN POSITION AND ALL 3 GEAR LIGHTS TURNED GREEN. THE OAP SHOWED LT & RT EEC FAULTS WITH PERF PENALTY 5 ON THE STATUS PAGE. THE PRESSURIZATION DEPRESSURIZED AND THE ACARS DID NOT HAVE AN OUTTIME INDICATING THE ACFT THOUGHT IT WAS ON THE GROUND. REPLACED SEALS ON METERING TUBE ASSY. REPACKED NOSE STRUT 32-21-09.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,557 hrs · 21,242 cycles

FUSELAGE SKIN CRACKED AT FS 1475 BETWEEN LONGERON 1R AND 2R.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,260 hrs · 21,079 cycles

DURING LO WALK AROUND FOUND A DENT ON TOP A ERA 462536-14 REPAIR DOUBLER. INFORMED MCC AND ENGINEERING. C/W VISUAL INSP PER ERA 476064-14. NO CRACKS OR PULLED FASTENERS NOTED. C/W S/M REPAIR PER PRI 476094-14 REV 0, 1, 2, 3, 4. ALSO ERA 476094-14 REV A FAA APPROVED DATA RETRIEVAL SUBMITTED TO DEPT 572 ATL RII INSP C/W 5009.

Part: HOUSING — FAILED (CYLINDER) · airframe 38,462 hrs · 20,634 cycles

AIRCRAFT LOST BOTH HYDRAULIC SYSTEM AFTER LANDING. FOUND LT MANUAL REVERSION CYLINDER HOUSING HAD FAILED. FOUR EACH BOLTS THAT SECURE THE TOP OF THE CYLINDER TO THE HOUSING HAD SHEARED CAUSING CYLINDER TO SEPARATE. FOUND LEFT ELEVATOR MANUAL REVERSION CYLINDER FAILED. REMOVED M/M. OK TO INSTALL. INSTALLED AND TESTED LEFT MANUAL REVERSION C PER M/M 27-33-09-420-801 AND 27-30-00-720-801. CKS GOOD LK GOOD. ALL PANELS REINSTALLED. RIG AND OPS CK GOOD PER 27-33-09-420-801, CKS GOOD RII COMPLETE.

Part: WIRE — BURNED (FWD RELAY PANEL) · airframe 34,589 hrs · 18,417 cycles

A/C RETURNED TO GATE, FLT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR IN F/C AREA. FOUND APU RELAY B9-607 WITH HEAT DAMAGE. SPLICED 12 INCHES NEW WIRE-RETERMINATED TERMINALS A2-B2-C2. REPLACED APU RELAY, BASE AND ELECTRICAL BUS TIE. ALL OPS NORMAL.

Part: ENGINE — VIBRATION (NR 1) · airframe 34,293 hrs · 18,245 cycles

AT FL300 THE LT STATOR VANE MSG ILLUMINATED, THE CREW DISCONNECTED THE AUTOTHROTTLES AND KEPT THE LT ENG ABOVE IDLE AS PER THE QRH. WITH INCREASING VIBS AND EGT CLIMBING THE CREW REDUCED THE THROTTLE TO IDLE AND SHUT DOWN THE ENGINE. LT ENG WINDMILLED FOR LESS THAN 30 MIN WITH AN UNKNOWN BUT POSITIVE OIL PRESSURE. REMOVED AND REPLACED NR 1 ENG PER TRANS 2T102.

Part: SKIN — DENTED (BS 245 L17-18L) · airframe 33,900 hrs · 18,022 cycles

DENT NEAR STA 245 BETWEEN L-17L AND L-18L. CUT OUT DENT AND INSTALL REPAIR DOUBLER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,510 hrs · 16,081 cycles

CORROSION ON LOWER FUSELAGE SKIN AT STA 864 BETWEEN L-30 AND L-29R. REMOVED CORROSION AND INSTALLED REPAIR DOULBER.

Part: CONTROL UNIT — FAILED (PYLON FLAPS) · airframe 29,628 hrs · 15,595 cycles

ELEVATOR SPLIT MSG AND PYLON FLAP FAULT MSG ILLUM IN FLT. REPLACED ACU, ALL DIAGNOSTIC TESTS PASSED.

Part: RELAY — FAILED (APU STARTER) · airframe 27,985 hrs · 14,735 cycles

APU SMOKED THE CABIN CAUSING AN EMERGENCY EVACUATION. REPLACED BAD APU STARTER AND START RELAY.

Part: MONITOR — ODOR (CABIN ROW 13AB) · airframe 27,615 hrs · 14,544 cycles

VISIBLE SMOKE COMING OUT OF OVHD PNL 13AB WITH ACRID SMELL. SUSPECT VIDEO MONITOR OR SEAT BELT NO SMOKING LIGHT. REPLACED INOP, ACRID SMELLING VIDEO MONITOR AT 13 AB PER MM. PERFORMED OPS TEST OF ENTERTAINMENT SYS, OPS CHECK NORMAL. SEAT BELT NO SMOKING LIGHTS CHECK NORMAL.

Part: BEARING — COKED (NR 1 ENGINE) · airframe 24,781 hrs · 13,152 cycles

NUMBER ONE ENGINE HAD TAIL PIPE FIRE ON SHUT DOWN. NUMBER 1 ENGINE BEING CHANGED DUE TO EXCESSIVE COKING IN NUMBER 5 BEARING COMPARTMENT PER IAE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,944 hrs · 12,714 cycles

F/C EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: TIRE — FAILED (NR 1 MLG) · airframe 23,358 hrs · 12,420 cycles

UPON ARRIVAL INTO SLC TOWER INFORMED CAPTAIN THERE WAS SMOKE FROM NR 1 GEAR. FOUND NR 2 AND NR 3 TIRES BLOWN. LEFT AFT INBOARD FLAP DAMAGED. REPLACED NR 2 AND NR 3 MAIN WHEEL ASSEMBLIES. AFT FLAP REPAIRED. NO DAMAGE FOUND IN NR 1 ENGINE.

Part: CONTROLLER — FAILED (BRAKE SYSTEM) · airframe 20,263 hrs · 10,893 cycles

FLT DIV- AFTER GEAR EXTENSION UNABLE TO ARM AUTO-BRAKES. AUTO-BRAKE FAIL MSG ON OAP. ANTI-SKID FAULT DISPLAYED ON OAP. REPLACED ASAB CONTROLLER.

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 20,239 hrs · 10,883 cycles

WORKING INBOUND MCO APU NO START WITH MESSAGE ON OAP. FOUND BRACKET WITH BURNT AREA WHERE GROUND STUD SHOULD HAVE MOUNTED. BRACKET P/N 7961078-653, STUD P/N AN 6-6. TERMINAL 5D0084-53 NOT DAMAGED. REF MD90 SB MD90-49A010 PAGE 12 OF 13 VIEW A-A FIG 2 (SH 2 OF 2). REMOVED BRACKET FOR REPLACEMENT. LIAISON ENGINEERING CONTACTED FOR REPAIR INSTRUCTIONS. BRACKET LOCATION IS UPPER BRACKET AT STA 1395 AND LONGERON 24-25.

Part: MANIFOLD — DAMAGED (ANTI SKID SYS) · airframe 19,410 hrs · 10,462 cycles

DURING TAXI RIGHT HYD QUANTITY DROPPED TO 3 RAPIDLY. VISIBLE FLUID SEEN ON TAXIWAY. FOUND DUAL ANTI-SKID CONTROL MANIFOLD ASSY TO HAVE A HYD FUSE BLOWN OFF MANIFOLD ASSY. REPLACED ANTI-SKID MANIFOLD PER AMM. LEAK CHECKS GOOD.

Part: LINE — LEAKING (THRUST REVERSER) · airframe 15,636 hrs · 8,465 cycles

RT HYD QUANTITY SLOWLY DECREASED IN FLT. APPROX 1 QT (EVERY 30 MIN) TO 6 QTS AND LOW LEVEL LIGHT ILLUMINATED. FOUND RT THRUST REVERSER RETURN LINE LEAKING. REPLACED SAME.

Part: WIRE — SHORTED (NR 2 ENGINE)

PASSING 28,000 STATUS LT AND RT ENG SYSTEM FAIL MESSAGE CAME ON. ENG WENT INTO N1 DEFAULT MODE. EPR AND EPR LIMIT INDICATIONS WENT AWAY AND AUTO THROTTLES DISENGAGED. FOUND WIRE 4 INCH AFT OF DISCONNECT P1-8066 GOING TO P1-8078 T2 CHANNEL A SHORTED TO ENG CASE. REPAIRED DAMAGED WIRE, RAN ENGINE AND OPN NORMAL.

Part: POWER SUPPLY — INOP (CABIN)

FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED POWER SUPPLY AND BATTERY.

Part: ACM — SEIZED (LEFT)

STRONG UNIDENTIFIED ODOR IN COCKPIT AND CABIN RETURN TO DFW. FOUND LT ACM SEIZED, REPLACED ACM OPN NOW NORMAL.

Part: BATTERY PACK — DISCHARGED (R1 DOORWAY)

R1 DOOR EMERGENCY EXIT LIGHTS VERY DIM. REPLACED BATT PACK, OPS NOW OK.

Part: CONTROL CABLE — FAILED (LANDING GEAR)

GEAR WOULD NOT RETRACT AFTER TAKEOFF. MTC IN PROGRESS REPLACING LDG GEAR HANDLE ANTI-RETRACTION LATCH CABLE.

Part: LIGHT — INOPERATIVE (CABIN)

MID CABIN EMERGENCY FLASHLIGHT INOP. REPLACED FLASHLIGHT.

Part: EEC — FAILED (NR 1 ENGINE)

ON TAKEOFF ROLL AFTER ADVANCING THROTTLES, THE LEFT ENGINE SURGE LIGHT CAME ON WITH THE LEFT ENGINE IGNITION LIGHT. BOTH LIGHTS CAME ON AND OFF, 3 TIMES TOTAL. REPLACED LEFT ENGINE EEC PER MM. PERFORMED ENGINE FAULT, DISPLAY SYSTEM CHECK AND OPERATIONAL/IDLE SYSTEM TEST NORMAL.