N597UA

Part: UNKNOWN — ODOR (AFT LAV LEFT) · airframe 70,767 hrs · 18,572 cycles

AFT LAVATORY LEFT SMOKE ALARM ACTIVATED IN FLIGHT, CREW SMELLED AN ODOR AND A HAZE OBSERVED BY FA. NOTICED HAZE OF SMOKE AT THE CIELING OF THE LEFT AFT LAVATORY WALL. INDICATED THAT THE ODOR WAS STRONGEST WHERE THE FLIGHT ATTENDANT SEATS ATTTACH TO THE LAVATORY WALL AREA.

Part: GUARD — OUT OF ADJUST (LIGHT SWITCH) · airframe 70,636 hrs · 18,546 cycles

WHEN GUARD ON THE EMERGENCY LIGHT SWITCH IS CLOSED, THE SWITCH IS FORCED TO THE OFF POSITION. REPOSITIONED THE HOOK UNDER TH EGUARD. THE SWITCH NOW GOES TO ARMED POSITION WITH GUARD CLOSED.

Part: WARNING SYSTEM — FALSE ACTIVATION · airframe 70,605 hrs · 18,540 cycles

DOOR 2R SLIDE LIGHT REMAINS ILLUMINATED WITH DOOR DISARMED. CYCLED DOOR ARM/DISARM LEVER AT 2R. DOOR ARMED LIGHT OPS CK NORMAL AT THIS TIME. COULD NOT GET FAULT TO DUPLICATE. INSPECTED GIRT BAR AND PROX SENSORS IN DOOR SILL. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 1498-1510) · airframe 70,535 hrs · 18,527 cycles

AFT CARGO FLOOR SUPPORT AT LBL 7.55 HAS CORROSION ON UPPER AND LOWER SURFACES AT NUTPLATES FROM BS 1498 TO 1510. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PARA 4 AND 7.

Part: LIGHT — MALFUNCTIONED (R2 DOOR SLIDE) · airframe 70,535 hrs · 18,527 cycles

R2 DOOR IS DISARMED, BUT SLIDE LIGHT REMAINS ILLUMINATED. CYCLED THE ARMING LEVER, SLIDE LIGHT CHECKED OK.

Part: SKIN — CRACKED (NR 1 SLAT COVE) · airframe 70,535 hrs · 18,527 cycles

LEFT WING LE SLAT 1 COVE SKIN HAS CRACKED FWD OF OTBD MAIN TRACK. REPAIRED THE SKIN IAW SRM 57-43-10, FIG 201, REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 70,531 hrs · 18,526 cycles

AFT CARGO FLOOR SUPPORT AT RBL 2.90 HAS CORROSION BS 1470. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1343-1362) · airframe 70,531 hrs · 18,526 cycles

AFT CARGO FLOOR SUPPORT, RBL 16.1 CORRODED BS 1343.5 TO 1362. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 5 1-40-02, PG 2-7 & DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 70,531 hrs · 18,526 cycles

AFT CARGO FLOOR SUPPORT LBL 2.9 CORRODED BS 1470. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-0 2, & DWG 4 6N5390.

Part: FLOOR SUPPORT — DENTED (BS 1423) · airframe 70,531 hrs · 18,526 cycles

AFT CARGO FLOOR SUPPORT, LBL 10.45 HAS A DENT AT BS 1423. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101, PG 102. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 7 & DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1359-1375) · airframe 70,531 hrs · 18,526 cycles

AFT CARGO FLOOR SUPPORT AT RBL 2.9 CORRODED, BS 1359 - 1375. REMOVED AND REPLACED THE FLOOR SUPPORT IAW AMM 51-40-02, PARA 4, AND 7.

Part: RIB — CRACKED (NR 8 SLAT) · airframe 70,531 hrs · 18,526 cycles

NR 8 SLAT INBD END BELOW ANTI-ICE DUCT END RIB CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02 .

Part: SEAT TRACK — GOUGED (BS 1080-1180) · airframe 70,503 hrs · 18,521 cycles

MAIN CABIN SEAT TRACK BETWEEN BS 1080 AND 1180, LBL 24 GOUGED AT MULTIPLE AREAS. BLENDED OUT THE SEAT TRACK DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-0052, ALLOWABLE DAMAGE 1, REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 3, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 310-324) · airframe 70,503 hrs · 18,521 cycles

MAIN CABIN FWD FLOOR SUPPORT BETWEEN BS 310 AND 324, RBL 40 CORRODED ON UPPER SURFACE AT MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, ALLOWABLE DAMAGE I. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 7, PAR 7D, AND DWG 141N5160.

Part: FITTING — CORRODED (BS 326) · airframe 70,498 hrs · 18,520 cycles

MAIN CABIN FWD FLOOR SUPPORT FWD GALLEY MOUNT FITTING AT BS 326, RBL 40 HAS CORROSION. REMOVED AND REPLACED THE FITTING IAW AMM 20-11-00-912-001.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,435 hrs · 18,508 cycles

R4 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-01-012-002, AND 33-51-01-402-003. OPS CHECKED GOOD.

Part: SKIN — DENTED (BS 600-620) · airframe 70,435 hrs · 18,508 cycles

FUSELAGE SKIN, BETWEEN BS 600 - 620 AND STRINGERS 15L - 16L, HAD TWO DENTS . ACCOMPLISHED EC/RA 5330-06284.

Part: FLOOR SUPPORT — CORRODED (BS 1257-1330) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT RBL 7.55 HAS CORROSION ON UPPER AND LOWER SURFACES BS 1257 TO 1330. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 630-705) · airframe 70,435 hrs · 18,508 cycles

FORWARD CARGO FLOOR SUPPORT LBL 16.1 AT BS 705 TO 630 HAS CORROSION ON THE TOP AND AT THE NUTPLATES ON THE UNDER SIDE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 143N5390, SRM 51-40-02, PG 7, AND PG 3.

Part: SKIN — CRACKED (WING) · airframe 70,435 hrs · 18,508 cycles

NR 9 LE SLAT COVE SKIN PANEL CRACKED AROUND INBD TRACK ATTACH POINT. THE SKIN WAS REPAIRED IAW SRM 57-43-01, REPAIR 4.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 70,435 hrs · 18,508 cycles

LEFT WING OTBD FLAP MOST OTBD BULNOSE HAS A GOUGE. BLENDED OUT THE GOUGED, FOUND OUT OF LIMITS IAW SRM 57-53-0 1, AD1, FIG 101, DETAIL VI. INSTALLED A REPAIR DOUBLER IAW SRM 57-53-01, REPAIR 5, FIG 201.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN FWD FLOORBEAM BS 365, RBL 5 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DAMAGE 1, FIG 101, DETAIL III. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-51-201, REP AIR 8, AND DWG 141N5112.

Part: SKIN — CRACKED (WING) · airframe 70,435 hrs · 18,508 cycles

NR 9 LE SLAT HAS CRACK AT COVE SKIN PANEL AROUND OUTBD TRACK ATTACH POINT. THE SKIN WAS REPAIRED IAW SRM 57-43-01 REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 1330-1343) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT RBL 10.45 HAS CORROSION ON UPPER AND LOWER SURFACES FROM BS 1330 TO 1343.4. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53, AD1, DETAIL V. AND DWG 143N5320. REMOVED AND REPLACED THE FLOOR SUPPORT IAW IAW SRM 51-40-02, PG 2, PG1.

Part: FLOOR SUPPORT — CORRODED (BS 1240-1343) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT RBL 16.10 HAS CORROSION ON UPPER AND LOWER SURFACES FROM BS 1240 TO 1343.5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143N5320, PG 7, AND PG 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

FORWARD CARGO STRINGER LBL 2.90, FROM SPLICE AT STATION 705 TO 630 HAS CORROSION. REMOVED AND REPLACED FWD CARGO STRINGER LBL 2.90 STA 705-630 IAW SRM 51-40-02 PG 4 AND 51-40-05 P/N 143N5346-40. AREA OF CORROSION WAS AT STA 653 LBL 2.90 L=2.4" W=0.9" D=.010" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 AD1 DETAIL V REF DWG INSTL N 143N5320.

Part: BOX BEAM — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

CORROSION AT STATION 735 LEFT SIDE, AT THE BOX BEAM, LBL 62, UNDER THE FLOOR PANEL, STICKER 20-141 REMOVED AND REPLACED BOX BEAM AT STA 735 LBL 62, UNDER THE FLOOR PANEL IAW SRM 51-40-02 PG 2. P/N NR 143N5522-5 REF INSTALLATION DWG 143N5400.

Part: SKIN — GOUGED (BS 700-710) · airframe 70,435 hrs · 18,508 cycles

UPPER FUSELAGE SKIN HAS THREE GOUGES BETWEEN BS 700 AND 710, STRINGER 2L AND 3L. BLENDED THE GOUGES AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 AD1, AND DWG 143N3121, REPAIRED IAW EC/RA 5330-06278.

Part: FITTING — CORRODED (BS 1638) · airframe 70,435 hrs · 18,508 cycles

MAIN AFT CABIN, TWO LAVATORY MOUNT FITTINGS AT BS 1638, LBL 24 AND 45 CORRODED. REMOVED AND REPLACED THE MOUNT FITTINGS IAW SRM 51-40-02, PG 10.

Part: BOX BEAM — CORRODED (BS 1640-1660) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN, AFT FLOOR SUPPORT BOX BEAM BETWEEN BS 1640 AND 1660, RBL 57, UPPER SURFACE HAS CORROSION AT MULTIPLE AREAS. REMOVED AND REPLACED THE BOX BEAM IAW SRM 51-40-02, PARA 7D, AND 11.

Part: BOX BEAM — CORRODED (BS 1640-1660) · airframe 70,435 hrs · 18,508 cycles

MAIN AFT CABIN FLOOR SUPPORT BOX BEAM BETWEEN BS 1640 AND 1660, LBL 57 CORRODED ON UPPER SURFACE AT MULTI PLE AREAS. REMOVED AND REPLACED THE BOX BEAM IAW SRM 51-40-02, PARA 7D, AND 4B.

Part: SUPPORT ANGLE — CRACKED (BS 1520-1540) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO CEILING, BS 1520 - 1540, CENTERLINE OF THE CEILING, THE INTERCOSTAL UPPER SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 140N2505.

Part: SKIN — GOUGED (BS 1100-1120) · airframe 70,435 hrs · 18,508 cycles

UPPER FUSELAGE SKIN HAS A GOUGE FROM BS 1100 TO 1120, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A PERMANENT REPAIR IAW EC/RA 53 30-06270.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT RBL 16.1 HAS CORROSION AT TWO NUTPLATES, BS 1470. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-53, REPAIR 1.

Part: FRAME — DENTED (BS 1480) · airframe 70,435 hrs · 18,508 cycles

FRAME AT BS 1480, STRINGERS 26-27L, FOUND DENTED. REPAIRED IAW SRM 53-00-07, REPAIR 5, P201, FIG 201.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 70,435 hrs · 18,508 cycles

NR 1 LE SLAT, LOWER COVE SKIN HAS A CRACK FWD OF INBD MAIN TRACK. REPAIRED IAW SRM 57-43-01, REPAIR 4.

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 70,435 hrs · 18,508 cycles

NR 10 SLAT COVE SKIN CRACKED AROUND THE INBD TRACK ATTACH POINT. REPAIRED IAW SRM 57-43-01, REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT LBL 7.55 HAS CORROSION ON THE UPPER AND LOWER SURFACES AT TWO NUTPLATES, BS 1470. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-53, FIG 201.

Part: SKIN — GOUGED (BS 1139-1160) · airframe 70,435 hrs · 18,508 cycles

UPPER FUSELAGE SKIN HAS A GOUGE FROM BS 1139.819 TO 1160, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REPAIRED IAW EC/RA 5330-06260.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1660) · airframe 70,435 hrs · 18,508 cycles

MAIN AFT CABIN FLOOR SUPPORT BETWEEN BS 1640 AND 1660, BL 0 HAS CORROSION ON THE UPPER SURFACE AT MULTI PLE AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 2 & 10 & DWG 146N5651.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1343) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT LBL 2.9 HAS CORROSION FROM BS 1343.5 TO 1320. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PARA 4 AND 7, AND DWG 146N53 90.

Part: FLOOR SUPPORT — CORRODED (BS 345-365) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN FWD FLOOR SUPPORT BETWEEN BS 345 AND 365, RBL 51 HAS CORROSION AND GOUGED ON UPPER SURFACE, REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, PAGE 7, PARA D, AND DWG 141N5160, CORROSION REMOVED FOUND OUT OF LIMITS IAW SRM 53-00-51-101, DAMAGE 1.

Part: FLOOR SUPPORT — CORRODED (BS 365-377) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN FWD FLOOR SUPPORT BETWEEN BS 365 AND 377, RBL 55 HAS CORROSION ON UPPER SURFACE. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 -00-51-101, DAMAGE 1. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PARA 7, AND DWG 141N5160.

Part: FLOOR SUPPORT — CORRODED (BS 1330) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR SUPPORT AT LBL 10.45 HAS CORROSION ON UPPER AND LOWER SURFACES AT BS 1330. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-53, REPAIR 1, FIG 201.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 70,435 hrs · 18,508 cycles

CORROSION ON THE R2 DOOR ANGLE IN MULTIPLE PLACES. REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, 1, FIG 101, DET IV. REPLACED THE ANGLE IAW SRM 51-40-02, PAR 7, AND DWG 143N8222.

Part: FLOORBEAM — CORRODED (BS 1018) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN MID FLOORBEAM INBD AND RBL 64, BS 1018 HAS CORROSION ON UPPER SURFACE. REMOVED THE CORROSION AND FOUND FOUND OUT OF LIMITS IAW SRM 53-40-13, ALLOWABLE DAMAGE 1, FIG 101. FABRICATED AND INSTALLED A REPLACEMENT FLOORBEAM IAW SRM 51-40-02, AND DWG 144N5140.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 70,435 hrs · 18,508 cycles

FWD CARGO DOOR UPPER AFT CORNER BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET AT FWD CARGO DOOR UPPER AFT CORNER IAW SRM 51-40-02 AND SRM 51-40-04 TR I/D 16-36 6 DUE DATE 09MAR18.

Part: FRAME — DENTED (BS 1560) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FRAME AT BS 1560 HAD TWO DENTS, JUST ABOVE STRINGER 26R. ACCOMPLISHED AFT CARGO FRAME REPAIR IAW SRM 53-00-07, FIG 201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

MAIN FWD CABIN FLOOR SUPPORT STRUCTURE STABILIZATION STRAP CRACKED AT STA 371, LBL 24, 209-006 ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN FLOOR SUPPORT STRUCTURE STABILIZATION STRAP STA 365-377 LBL 24 IAW SRM 53-0 0-51, FIG 201, REPAIR 12 AND 13, PG 201-207.

Part: PANEL — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO LT SIDE PANEL HAS MULTIPLE AREAS OF CORROSION ON TOP AND UNDERNEATH FROM STA 1310 TO 1372 AS MARKED. REMOVED CORROSION AFT CARGO LT SIDE PANEL 12"L X 2"W X .012 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1 FIG 101 REPLACED WITH NEW SIDE PANEL P/N 146N5391Y179 PO S AG 1743627 LOCATED AND DRILLED INSTALLED IAW SRM 51-40- 08 PG 1-3 AND SRM 51-40-02 PG 1-4 DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STR RBL 10.45 HAS CORROSION ON UPPER AND LWR SURFACE AT NUTPLATES AT STA 1470. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR, AT STA 1470 RBL 10.45" IAW SRM 53-00-53 REPAIR 1, FIG 201. REMOVED CORROSION DETAILS BLENDED DAMAGED L=2.4 W=.9" D=.020" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 AD1 DETAIL V.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STGR AT LBL 16.10 HAS CORROSION ON UPPER AND LWR SURFACE AT STA 1470. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR AT LBL 16.10 STA 1470 IAW SRM 53-00-53 REPAIR 1 FIG 201. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR AT LBL 16.10 STA 1470 IAW SRM 53-00-53 REPAIR 1 FIG 201 CORROSION THAT WAS REMOVED (DIMENSIONS: L=1" X W=.9" X D=.011) FOUND TO EXCEED LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1, FIG 101, DETAIL V.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STR AT LBL 10.45 HAS CORROSION AT 2EA NUTPLATES ON UPPER AND LWR SURFACE, AT STA 1470. ACCOMPLISHED PERMANENT REPAIR AT AFT CARGO FLOOR STR AT STA 1470, LBL 10.45 IAW SRM 53-00-53 REPAIR 1, FIG 201. L=3"W =.5" D=.008" DRAWING NR 146N5390. CORROSION THAT WAS REMOVED DIMENSIONS STATED ABOVE WAS FOUND TO EXCEED LIMITS REF SRM 53-00-53 ALLOWABLE DAMAGE 1, FIG 101, DETAIL V.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STR AT RBL 10.45 HAS CORROSION FROM SPLICE TO STA 1348 UPPER AND LWR SURFACE AT NUTPLATE AT STA 1348 (96-56). REMOVED AND REPLACED AFT CARGO FLOOR STR PN 146N5417U11 PO NR SAG1743627 AT STA 1340-1440 RBL 10.45 IAW SRM 51-40-02 PG 2-7 AND DWG NR 146N5390, CORROSION REMOVAL DETAILS STA 134 8 L=1.7" W=1.0" D=.010" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-83 DETAIL V.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN FWD FLOOR SUPPORT BEAM APPROX STA 345 RBL 1 TO LBL 20, HAS CORROSION ON UPPER SURFACE AT MULTIPLE AREAS 209-075 ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOORBEAM AT STA 34 5 RBL1-RBL12 IAW SRM 53-00-51 REPAIR 5 FIG 201-204. BLENDED OUT CORROSION ON FLOORBEAM UPPER SURFACE AT STA 345, RBL1 - LBL-20, L=20, W=2, D=0.08. FOUND WITHIN LIMITS, HFEC INSPECTION C/W IAW SRM 53-00-51 AD 1 DET III. A2/A1=0.0072/0.1 875=0.0384 X 100=3.84% FOUND IN LIMITS IAW SRM 53-00-51 AD 1 DET IV.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 70,435 hrs · 18,508 cycles

(B757-53-3-6338) AFT CARGO FLOOR STGR AT RBL 7.55 HAS CORROSION AT 2EA NUTPLATES ON UPPER AND LWR SURFACE AT STA 1470. (96-43) ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STGR AT STA 1470 RBL 7.55 IAW B757-200 SRM 53-00-53 REPAIR 1 FIG 201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

MAIN CABIN FLOOR STRUCTURE STABILIZATION STRAP AT STA 560, LBL 45 CRACKED. ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN FLOOR STRUCTURE STABILIZATION STRAP AT STA 560, LBL 45 IAW SRM 53-00-51, FIG 201, REPAIR 13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STR AT RBL 7.55 HAS CORROSION ON UPPER AND LWR SURFACE AT NUTPLATES FROM STA 1498-1520. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR. AT STA 15 10 RBL 7.55. REMOVED CORROSION ON AFT CARGO FLOOR STR AT RBL 7. 55 STA 1504 AREA (A)L=2.4 W=0.80 D=.003 AND STA 1514 AREA (C) L= 2.4 W=.8 D=.003, ALL FOUND WITHIN LIMITS IAW B757-200 SRM 53-00- 53 REPAIR 1 FIG 201 AND SRM 53-00-53 A.D.1 HFEC C/W. SEE ATTACHMENT 73411.

Part: FLOOR SUPPORT — CORRODED (BS 720-740) · airframe 70,435 hrs · 18,508 cycles

(B757-53-3-6498) CORROSION AT 2R DOOR BOX BEAM, STATION 720-740 RBL 62 MULTIPLE PLACES, STICKER 20-147 REMOVED AND REPLACEMENT WILL BE INSTALLED ON NR 0006870 BOX BEAM STA 720-740 RBL 62.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO FLOOR STGR AT RBL 10.45 HAS CORROSION ON UPPER AND LWR SURFACE AT STA 1510. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STGR. AT STA 1510 RBL 10.45 IAW B757-200 SRM 53-00-53 REPAIR 1 FIG. 201.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · airframe 70,435 hrs · 18,508 cycles

(B757-53-3-6129) MAIN CABIN AFT FLOOR SUPPORT BOX BEAM BETWEEN STA 1660 AND STA 1680, RBL 57 UPPER SURFACE HAS CORROSION AT MULT IPLE AREAS. 209-059 REMOVED & REPLACED MAIN CABIN AFT FLOOR SUPPORT BOX BEAM BETWEEN STA 1660 TO 1680 RBL 57 IAW B757-200 SRM 51-40-02 PG 6 & 7.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · airframe 70,435 hrs · 18,508 cycles

(B757-53-3-6129) MAIN AFT CABIN FLOOR HAT CHANNEL BETWEEN STA 16 60 AND STA 1680 BL0 HAS CORROSION ON UPPER SURFACE AT MULTIPLE AREAS. 209-52 REMOVED AND REPLACED FLOOR HAT CHANNEL AT MAIN CABIN STA 1660 AN D STA 1680, BL0 IN ACCORDANCE WITH B757-200 SRM 51-40-02 PG 2 D UE TO UPON FURTHER EVALUATION FOUND HAT CHANNEL AT 15% EXFOLIATE D AND OUT OF LIMITS IAW 757-200 SRM 53-00-51.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

AFT CARGO COMPARTMENT, CEILING UPPER SUPPORT ANGLE ON INTERCOSTAL IS CRACKED, STATION 1440 CENTER LINE. REPLACED UPPER SUPPORT ANGLE ON INTERCOSTAL AT STA 1 440-1460 BLO IAW SRM 51-40-02.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 70,435 hrs · 18,508 cycles

MAIN AFT CABIN FLOOR SUPPORT AFT GALLEY MOUNT FITTINGS 2EA AT STA 1682 AND STA 1718, RBL 57 HAVE CORROSION. REMOVED AND REPLACED 2EA GALLEY MOUNT FITTINGS, AT MAIN CABIN STA 1682 AND 1718, RBL 57 IAW SRM 51-40-02 PG 10, ACCOMPLISHED TORQUE TO 85 IN-LB IAW AMM 20-11-00-912-001.

Part: FLOOR SUPPORT — CORRODED (BS 1680) · airframe 70,435 hrs · 18,508 cycles

(B757-53-3-6129) MAIN CABIN AFT FLOOR SUPPORT DECK PLATE GUSSET 2EA AT STA 1680, RBL 31 AND RBL 38 HAVE CORROSION ON UPPER SURFACE, 209-063. REMOVED AND REPLACED 2 EACH GUSSETS IN MAIN CABIN AT AFT FLOOR S UPPORT DECK PLATE STA 1680 RBL 31 AND 38

Part: LIGHT — INOPERATIVE (MLG INDICATOR) · airframe 70,406 hrs · 18,502 cycles

NO LEFT MAIN GEAR LIGHT WHEN GEAR SELECTED DOWN. LIGHT TESTED GOOD ALT PROCEEDURE, STILL NO LIGHT. EMERGENCY DECLARED. REPLACED THE LT MAIN GEAR LED LENS AND BASE ASSY. P3 PANEL, LIGHT CHECKED OK.

Part: SLIDE — DETACHED (L4 DOOR) · airframe 70,106 hrs · 18,444 cycles

L4 DOOR SLIDE, OFF THE MOUNT. INSTALLED THE DOOR SLIDE IAW AMM 25-66-01-404-044.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 70,022 hrs · 18,428 cycles

IAW WDM 33-51-21, FOUND EMERGENCY EXIT INDICATOR L777 SHORTED BEHING L2 DOOR SIDEWALL. WIRES PINCHED. REPLACED EMERGENCY LIGHT INDICATOR L777. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,022 hrs · 18,428 cycles

EMERGENCY LIGHTS INOPERATIVE AT THE L2 DOOR, RIGHT AND LEFT. REPLACED THE INVERTER MODULE M10949 AND TESTED EMERGENCY LIGHTS. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: MODULE — LEAKING (EDP CASE DRAIN) · airframe 69,692 hrs · 18,364 cycles

LEFT HYD QTY EICAS MESSAGE, .21 INDICATED QTY. EMERGENCY DECLARED. FOUND AFT DPI LEAKING ON EDP PRESSURE CASE DRAIN FILTER MODULE. REPLACED THE AFT DPI IAW AMM 29-11-17-004-001, AND 29-11-17-404-027. MOTORED THE NR 1 ENG FOR 2 MINUTES, LEAK CHECKED GOOD, APPLIED HYD PRESSURE FROM ALL HYD SYSTEMS, LEAK CHECKED GOOD. NEW O-RINGS INSTALLED WITH NEW DPI.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,251 hrs · 18,086 cycles

L2 AND R2 DOOR SIDEWALL EXIT SIGNS INOPERATIVE. REPLACED THE POWER SUPPLY M733 AND LAMP 776. OPS CHECKED NORMAL.

Part: FLOOR SUPPORT — CRACKED (BS 1200-1220) · airframe 66,977 hrs · 17,839 cycles

AFT CARGO BAY BS 1200 - 1220, BL 0 FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-00-02 PARA 4 .

Part: INTERCOSTAL — CRACKED (BS 1200-1220) · airframe 66,977 hrs · 17,839 cycles

MAIN CABIN AT BS 1200 - 1220 HAS A CRACKED INTERCOSTAL. REPLACED MAIN CABIN INTERCOSTAL IAW SRM 51-04-02 PARA 4.

Part: IDLER LINK — WORN (LT ELEVATOR) · airframe 58,679 hrs · 16,231 cycles

DURING INSPECTION, LT ELEVATOR PCA'S FOUND ALL THREE IDLER LINKS WITH EXCESSIVE WEAR. WEAR LIMIT IAW 27-31-05-6 01 IS REFERRED TO BY AMM 27-31-05 PG 424 SUB PARAGRAPH F 1. LARGEST LIMIT FOR ANY BEARING IN THIS REFERENCE .003 INCHES. MOVEMENT NOTED APPROXIMATELY .150 INCHES, ALL THREE IDLER LINKS.

Part: MODULE — FAULTY · airframe 57,862 hrs · 16,076 cycles

MACH SPEED TRIM EICAS ON. REPLACED RT SAM MODULE IAW AMM 27-09-00, PG 201, CHECKED OK.

Part: STRAP — UNSECURE (R1 DOOR) · airframe 57,404 hrs · 15,987 cycles

DOOR 1R WILL NOT ARM FOUND STRAP LOOSE FROM SLIDE PACK JAMMING IT. STOWED LOOSE STRAP PROPERLY, PUT SLIDE COVER ON SECURELY, DOOR 1R ARMED NORMAL.

Part: BOTTLE — FAILED (EVAC SLIDE) · airframe 57,172 hrs · 15,943 cycles

TEST 2 LT EMERGENCY ESCAPE SLIDE SQUIB FAILED TO TEST. REPLACED K10486, NO HELP. REPLACED OVERWING BOTTLE IAW MM.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 57,038 hrs · 15,918 cycles

SPOKING PRESENT ON WXR DISPLAY. REPLACED WXR TRANSCEIVER IAW MM.

Part: FCU — LEAKING (NR 1 ENGINE) · airframe 56,738 hrs · 15,861 cycles

LEAK FOUND AROUND FUEL CONTROL UNIT ON NR 1 ENG. REPLACED FUEL CONTROL UNIT IAW MM.

Part: ENGINE — FAULTY (NR 2) · airframe 56,738 hrs · 15,861 cycles

BAD OIL SMELL FROM PACKS. LAX & MAINT REPORTED BAD ODOR COMING FROM FWD GALLEY, TO ISOLATE ENGS AS A CAUSE OF OIL SMELL IAW LM7484 NR 1 ENG, LM7485 NR 2 ENG & AMM 71-05-00 FIG 109B PAGE 119, DEBRIEFED FLIGHT CREW & ATTENDANTS. CAPT SAID SMELL WAS NOTICED ON THE GROUND DURING TAXI & ALL PHASES OF FLIGHT & SMELLED LIKE OIL OR DE-ICING FLUID. REPLACED ENG.

Part: OIL FILTER — DEFECTIVE (RT ENGINE) · airframe 56,514 hrs · 15,818 cycles

EICAS STATUS RT ENG OIL SEAL. ACCOMPLISHED FIM 79-21-00 PG 112. REPLACED MAIN OIL FILTER. RAN ENG IAW AMM 71-00-59 PG 201. ALL PARAMETERS NORMAL.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 56,177 hrs · 15,750 cycles

NR TWO CENTER HYDRAULIC PUMP NOT PRESSURIZING.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,175 hrs · 15,748 cycles

EMERGENCY EXIT LIGHT ABOVE DOOR 1 RIGHT AND FLIGHT DECK AISLE ON BULKHEAD INOPERATIVE. REPLACED POWER SUPPLY M730 PER AMM, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,175 hrs · 15,748 cycles

EMERGENCY LIGHT BELOW STOW BIN 4ABC AND 26ABC INOPERATIVE. APPLIED MEL 3351A.

Part: ACTUATOR — INOPERATIVE (AILERON TRIM) · airframe 56,145 hrs · 15,742 cycles

AILERON TRIM INOPERATIVE. AILERON CENTERED AND PULLED BREAKER. GROUNDS WERE GOOD & FOUND 28V BETWEEN PIN 1 AND 5. NEED TO REPLACE M488 TRIM ACTUATOR 585-9091. R & R LATERAL TRIM ACTUATOR IAW MM.

Part: GIRT BAR — LACK OF LUBE (R1 DOOR) · airframe 56,086 hrs · 15,731 cycles

UNABLE TO ARM DOOR 1R. LUBRICATED GIRT BAR AND TRACK, CHECKED OK.

Part: CONTROLLER — MALFUNCTIONED (NR 2 BLEED SYS) · airframe 56,050 hrs · 15,724 cycles

ON TAXI FOUND NR 2 ENGINE BLEED AT 4 PSI. REPLACED HIGH STAGE PILOT CONTROLLER IAW MM.

Part: STATIC LINE — OUT OF POSITION · airframe 56,027 hrs · 15,718 cycles

R1 DOOR WOULD NOT ARM. FOUND STATIC LINE OUT OF POUCH. REINSTALLED STATIC LINE IAW MT 25-66-00, OPS NORMAL.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 55,894 hrs · 15,692 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE WITH DOOR ARMED. ADJUSTED GIRT BAR CRANK PUSHROD ONE TURN OUT IAW AMM, CHECKED OK.

Part: FILTER — ODOR (RECIRCULATION FA) · airframe 55,746 hrs · 15,663 cycles

BURNING ODOR IN CABIN AND COCKPIT DURING CRUISE AT FL370. TURNED RT RECIRCULATION FAN OFF, ODOR GONE. REPLACED RT AND LT RECIRCULATION FAN FILTERS IAW MM-21-25-02 AND ACCOMPLISHED CHECK, IAW MM-21-00-01 OPS CHECKED NORMAL. NO ELECTRICAL ODOR NOTED.

Part: LENS — UNSECURE (R1 DOOR) · airframe 55,679 hrs · 15,650 cycles

R1 DOOR ARM LIGHT INOPERATIVE. SECURED LAMP LENS.

Part: CONTROL UNIT — MALFUNCTIONED (HYD SYSTEM) · airframe 55,664 hrs · 15,647 cycles

C HYD ELEC 2 EICAS AND SWITCH PRESSURE LIGHT ILLUMINATED. SHUT OFF PUMP IAW QRH. REPLACED C2 ELCU IAW MM 29 -11-67. SWITCH AND PUMP PRESSURE OK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 55,621 hrs · 15,636 cycles

EMERGENCY LIGHTS IN MID CABIN BUSINESS SEATS, OVERWING EXIT LIGHTS AND OUTSIDE OVERWING WON'T COME ON WITH COCKPIT SWITCH ON. REPLACED POWER SUPPLY AND BATTERY, RELAMPED RT AND LT OUTSIDE OVERWING EXIT EXTERIOR LIGHTS, OPS CHECKED NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 55,621 hrs · 15,636 cycles

ACFT FAILED, ITEM 11 OF 2 SERVICE, INTERIOR AND EXTERIOR EMERGENCY LIGHTS OP CHECK. REPLACED POWER SUPPLY AND BATTERY.

Part: SKIN — DAMAGED (BS 1433 S28L-29R) · airframe 55,619 hrs · 15,635 cycles

SKIN DOUBLER REPAIR INSTALLED SRA 1433, STR 28L- 29R. IAW SRM 53-00-01, REPAIR 3, THIS IS A CLASS B REPAIR.

Part: SHUTOFF VALVE — NO TEST (NR 2 ENGINE) · airframe 55,619 hrs · 15,635 cycles

NR 2 ENGINE HPSOV FAILED HEALTH CHECK. R & R HPSOV IAW AMM 36-11-07. PERFORMED LEAK CHECK IAW AMM 36-11-07, NO LEAKS NOTED.

Part: WIRE — BROKEN (FUEL DOOR) · airframe 55,619 hrs · 15,635 cycles

RIGHT WING L/E, FUELING DOOR 621GB, LIGHT WIRES BROKEN. REPAIRED BROKEN WIRES, W3 426-A-AE, W3426-A-AG IAW BSWPM 20-10-13, PAR 4A, WDM 28-21-11 PAGE 4. PERFORMED GOOD OP'S CHECK IAW AMM 12-11-01 STEP 3E9.

Part: HANDLE — MISSING (T/R ACTUATOR) · airframe 55,518 hrs · 15,610 cycles

NR 1 ENGINE THRUST REVERSER LOCKING ACTUATOR ASSY FOUND MISSING HANDLE ASSY. ACCOMPLISHED INSTALLATION OF MISSING PARTS ON NR 1 ENGINE O/B TR SYNC ACTUATOR AS PER MM. SYSTEM OPS CHECKED OKAY.

Part: CONTROL UNIT — FAULTY (HYDRAULIC SYS) · airframe 55,498 hrs · 15,604 cycles

EICAS MSG - RT HYD ELEC PUMP DISPLAYED. CREW COMMENTS: 15 MIN INTO FLT PASSING FL260 R HYD ELEC PUMP REPEAT WRITEUP PUMP TURNED OFF QRH. CHECKED RIGHT ACMP CONNECTOR, CHECKS NORMAL. CHECKED WIRING AROUND M10005 ELEC HYD PUMP RT ELCU. ALL APPEARS NORMAL. REPLACED M10005 ELCU FOR RT ELEC HYD PUMP PER MM. RAN PUMP, CYCLED FLIGHT CONTROLS, NO FAULTS.

Part: PUMP — FAILED (RT HYD SYSTEM) · airframe 55,493 hrs · 15,603 cycles

RECEIVED A RT HYD ELEC PUMP EICAS. RIGHT BEFORE TOP OF CLIMB. RAN QRH. SYSTEM PRESS AND QTY NORMAL. PER FIM REPLACED RIGHT ELEC HYD PUMP AND PRESSURE SWITCH S-30 REF AMM 29-11-18. RIGHT HYD SYSTEM, OPS CHECKED OK AND NO LEAKS NOTED.

Part: ANTI-ICE VALVE — STUCK (NR 1 ENGINE) · airframe 55,493 hrs · 15,603 cycles

LEFT ENGINE ANTI ICE VALVE STUCK IN CLOSED POSITION. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE IAW AMM.

Part: BLOCK — WORN (RT NACELLE) · airframe 55,442 hrs · 15,588 cycles

DURING RIGHT ENGINE PLUMBING INSPECTION EQ7592, SEVERAL BLOCKS FOUND WORN. REPLACED RUBBER BLOCKS ON HYD LINE BETWEEN NAC STA 180.8 AND 149.5.

Part: BONDING WIRE — BROKEN (PC AIR DOOR) · airframe 55,307 hrs · 15,555 cycles

BONDING WIRE ON PC AIR DOOR BROKEN. REPLACED BONDING WIRE ON AC AIR DOOR.

Part: CONTROL UNIT — MALFUNCTIONED (HYD SYSTEM) · airframe 55,237 hrs · 15,536 cycles

RIGHT HYDRAULIC PUMP CIRCUIT BREAKER TRIPS WHEN PUMP SELECTED ON. REPLACED ELCU M10005 IAW MM 29-11-67. SYSTEM GROUND CHECKED NORMAL.

Part: SEAT BELT — MALFUNCTIONED (COCKPIT) · airframe 54,955 hrs · 15,449 cycles

CHECKED CROTCH STRAP DOES NOT OPERATE NORMAL.

Part: COUPLER — FAILED (HF ANTENNA) · airframe 54,636 hrs · 15,364 cycles

FEEDBACK IN BOTH HF RADIOS. FOUND LEFT AND RIGHT HF TRANSMIT NORMAL, BUT BOTH RECEIVE UNREADABLE AND GARBLED. REPLACED LEFT AND RIGHT ANTENNA COUPLERS M241 AND M242 REF MM. PERFORMED HF COMMUNICATION SYSTEM TEST REF MM. HF SYSTEM OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,361 hrs · 15,300 cycles

EMERGENCY LIGHT AT L60 AT DOOR 3R IS INOP, NEED SLIGHT ASSY 564-0419. EMERGENCY LIGHT ASSY AT DOOR 3R PER IPC, OPS CHECK GOOD.

Part: SOCKET — FAULTY (CABIN) · airframe 54,361 hrs · 15,300 cycles

EMERGENCY EGRESS LIGHT L563 INOP LOCATED AT AFT RIGHT OVERWING. NEED LIGHT ASSY 564-0044. REPLACED SOCKET ASSY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,361 hrs · 15,300 cycles

STAR DEPARTURE CHECK REVEALS OVERWING SLIDE LIGHTS AT 2R, 3R, AND OVERWING AFT ARE INOP ON LIGHT TEST. RELAMPED DOOR 2R EXT EMERGENCY LIGHT, CHECK OK. DOOR 3R HAS POWER & GRD. RELAMPED, NO HELP. NEEDS REFLECTOR SOCKET, OVERWING RT AFT EMERGENCY LIGHT HAS 6.8VDC AND GROUND, RELAMPED NO HELP. LIGHTS LOCATED 5 WINDOWS AFT OF RT AFT OVERWING EXIT DOOR. DOOR 3RT OUTSIDE EMER LIGHT L60 NEEDS LAMP ASSY (LT INTERMITTANT) P-N 30-1672-2 OVERWING AFT OUTSIDE EMER LIGHT NEEDS LIGHT ASSY P-N 30-2537-2.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 53,929 hrs · 15,193 cycles

RIGHT OVERWING EMERGENCY EXIT, SECOND INCANDESCENT LIGHT FROM FWD INOP. RELAMPED AND CHECKED OKAY.

Part: IGNITION LEAD — FAULTY (NR 2 ENGINE) · airframe 53,746 hrs · 15,149 cycles

NR 1 ENGINE NO LIGHT OFF IN IGNITION 2. START NORMAL IN BOTH. FUEL FLOW NORMAL, VALVE LIGHTS OK. REPLACED NR 2 ENGINE IGNITER LEAD. ENGINE LIGHT OFF NORMAL PER JRH WHEN SELECTED TO NR 2 ONLY.

Part: FUEL CONTROL — FAULTY (ENGINE) · airframe 53,644 hrs · 15,125 cycles

INTERMITTENT SEC CONT STATUS MESSAGE. REPLACED FUEL CONTROL.

Part: FASTENER — MISSING (NACELLE) · airframe 53,621 hrs · 15,119 cycles

AFT STARBOARD (NR 2) SAILPLANE HAS A RIVET MISSING ON OUTWARD SIDE. NON LEADING EDGE FASTENER. 3RD FROM L/E. RIVET NOT LOOSE. STEM MISSING. OTHER FASTENERS NOT LOOSE. MAX 5 FLT CYCLES FOR REPLACEMENT PER AMM. SECURED FASTENER ON NR 2 SAILTAIL.

Part: FAIRING — LOOSE (TE FLAP) · airframe 53,626 hrs · 15,120 cycles

RIGHT INBOARD TRAILING EDGE BOTTOM FIXED FAIRING ATTACH SCREWS FOUND LOOSE ON WALKAROUND. TIGHTENED FAIRING PER AMM. RAN FLAPS, CHECKS NORMAL.

Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 53,515 hrs · 15,086 cycles

RIGHT PRECOOLER OUT TEMP INDICATION ON ECS PAGE IS BLANK. REPLACED PRECOOLER DISCHARGE TEMP SENSOR PER AMM, SYSTEM INDICATION NORMAL.

Part: SCANNER — FAULTY (WEATHER RADAR) · airframe 53,465 hrs · 15,071 cycles

WXR FAIL DISPLAYED ON HSI. WXR FAIL ANT DISPLAYED ON HSI IN WXR TEST POS. TROUBLESHOT PER TSM 34-43-00. NEW T-R NO HELP, REINSTALLED ORIGINAL T-R. REPLACED WX RADAR DRIVE AND SCANNER PLATE PER AMM, RADAR SYSTEM TESTS OK PER AMM. NO FAILURE MSG'S AFTER TEST. AUTO AND MANUAL TILT FUNCTIONS NORMAL.

Part: ACTUATOR — FAULTY (SPEED BRAKE) · airframe 53,399 hrs · 15,056 cycles

AIR DATA COMPUTER TEST RIGHT HAS STRANGE GRINDING SOUND. TROUBLESHOT SYSTEM FOUND SPEED BRAKE AUTO STOW ACTUATOR (MOTOR) AT FAULT. PLACED AUTO SPEED BRAKE SYSTEM ON MEL. COMPLIED WITH DDPG. RDF-P :REPLACED ACTUATOR 563-920 1, STILL HAVE GRINDING NOISE. FOUND SPEED BRAKE ACTUATOR 560-9613 MAKING NOISE. AUTO SPEED BRAKE ACTUATOR WAS REPLACED. REPLACED AUTOSTOW ACTUATOR, TEST OKAY.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 53,344 hrs · 15,040 cycles

UPON ARRIVAL FOUND DENT, AND SCRATCH ON LEFT SIDE OF FUSELAGE SECTION 41. DAMAGED AREA IS LOCATED AT STATION 402 TO 409 BETWEEN STRINGER 15, AND 16. DENT IS 5 INCHES LONG 3-4 INCHES WIDE, AND 5-32 DEEP. SCRATCH IS .031 DEEP 4 INCHES LONG. BLENDED OUT DAMAGE PER SRM. DENT NOW AT DEEPEST POINT.100. ACCOMPLISHED REPAIR AT STA 418 STR 15L & 16L. NO DAMAGE FOUND AT STATION 402 TO 409.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 53,499 hrs · 15,081 cycles

NR 2 ENGINE BIRD STRIKE, RTFL ENGINE PARAMETERS WERE NORMAL. TWO LARGE BIRDS ONE MAY HAVE HIT TAIL. BIRD DAMAGE CONFINED TO NR 2 ENGINE, NR 2 ENGINE NOSE COWL APPEARS TO HAVE NO DAMAGE. CHANGE NR 2 ENGINE DUE TO MULTIPLE DEFECTS FROM BIRD STRIKE.

Part: PANEL — FAULTY (VHF COMM) · airframe 53,223 hrs · 15,007 cycles

LEFT VHF LIGHT BURNED OUT RIGHT DISPLAY. REPLACED VHF PANEL PER MM, RADIO CHECKED GOOD.

Part: COUPLER — FAULTY (NR 2 HF SYS) · airframe 53,056 hrs · 14,965 cycles

NR 2 HF WILL NOT TUNE. REPLACED NR 2 COUPLER PER AMM, OPS CHECKED GOOD.

Part: FLOOR PANEL — PUNCTURED (BS 1402) · airframe 52,863 hrs · 14,911 cycles

TWO PUNCTURES IN AFT CARGO BAY FLOOR PANEL AT STA 1402. FIRST HOLE 4X5 AND SECOND HOLE 2.5 X .5. REPAIRED DAMAGED FLOOR PANEL PER MM 53-30-98 REPAIR 4.D

Part: SWITCH — OUT OF POSITION (LAVATORY) · airframe 52,323 hrs · 14,754 cycles

DOOR 2L LAV OCCUPIED LIGHT DOESN'T GO OUT. RETURNED LAV 2L DOOR SWITCH TO NORMAL CONFIGURATION. CHECK OK.

Part: INSULATION — DAMAGED (RT COWLING) · airframe 51,557 hrs · 14,530 cycles

INSULATION DAMAGE FOUND UNDER RT FAN COWL FWD SIDE OF THRUST REVERSER BULKHEAD. LOCATION RED TAGGED FOR IDENTIFICATION. INSPECTED WIRES IN EFFECTED AREA. NO DAMAGE TO WIRES FOUND WHILE AT THE GATE. SECURED WIRES WITH TAPE.

Part: VALVE — FAULTY (POSIT 2) · airframe 51,140 hrs · 14,415 cycles

AFT TRIM AIR VALVE HAS NO POSITION INDICATION. REPLACED TRIM AIR VALVE. OPS CHECKED GOOD PER MM.

Part: CONTROLLER — FAULTY (ZONE TEMP) · airframe 51,132 hrs · 14,412 cycles

OFF THE GATE RECEIVED FLT DECK FWD CABIN AND AFT CABIN ZONE TRIM VALVES INOPERATIVE LIGHT. CYCLING AUTO AND OFF NO CHANGE PER CREW. REPLACED ZONE TEMPERATURE CONTROLLER PER MM.

Part: CONTROL UNIT — FAULTY (SPOILER SYS) · airframe 50,924 hrs · 14,350 cycles

DURING CLIMB SPEED BRAKE "AUTO STOW" MOTOR RAN TWICE WITH GEAR UP, FLPS UP, SPEED BRK LEVER STOWED BEFORE CLEARING THIS ITEM NEED TO ENSURE ALL THE STEPS OF MEL 2762C HAVE BEEN REVERSED INCLUDING THE CB, ANN LT, AND SPEEDBRAKE AUTOSTOW HARNESS CONNECTOR. FOUND FAULT BALL ON RT NR 3 SC MODULE. REPLACED NR 3 SC MODULE PER MM. PERFORMED SPEEDBRAKE AUTOSTOW TEST PER MM TASK 27-62-01-000-501, TASK 27-62-0 1-000-502, AND OP CHECK PER MM TASK.

Part: PCA — FAULTY (SPOILER) · airframe 50,766 hrs · 14,310 cycles

AUTOSPEED BRK SYS FAILUIRE, RTFL. SPOILER AUTO STOW MOTOR ACTIVATED DURING CLIMB WITH SPOILER LEVER STOWED. REPLACED NR 9 SPOILER PCA PER MM.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 50,720 hrs · 14,300 cycles

FOUND SMALL AMOUNT OF STRAW COLORED FLUID UNDER RT AILERON ON WALKAROUND. SECURED FOUR B-NUTS. RAN AILERONS THRU SEVERAL CYCLES, NO LEAKS NOTED.

Part: THERMOCOUPLE — FAULTY (APU) · airframe 50,707 hrs · 14,297 cycles

APU ALTITUDE NO START - COLD SOAKED. APU SHUTDOWN AFTER REACHING 95 PERCENT SPEED AFTER 10 SECONDS. APU RAN STABILIZED AT 100 PERCENT FOR 1 MIN THEN APU FAULT AND APU GEN EICAS MESSAGE DISPLAYED. ACCOMPLISHED SUCCESSFUL APU ALT COLD SOAK START. REPLACED NR 2 THERMOCOUPLES PER MM. APUC FAULTED NR 2 TC RAKE SNAPSHOT READS EGT 278 RPM 78 PERCENT.

Part: BATTERY — FAULTY (APU) · airframe 50,690 hrs · 14,293 cycles

APU FAULT DURING TAXI IN. APU START ATTEMPT SHOWS 5 VOLTS AT CRANK. APU BATTERY WARM TO TOUCH. REPLACED APU BATTERY IAW AMM.

Part: CHARGER — FAILED (APU BATTERY) · airframe 50,690 hrs · 14,293 cycles

APU BATTERY TEST FAILS. REPLACED APU BATTERY CHARGER IAW AMM, OPS CHECKED OK.

Part: RVDT — OUT OF ADJUST (CONTROL WHEEL) · airframe 50,196 hrs · 14,142 cycles

SPOILER EICAS MSG. DUE TO THE HISTORY OF THE SPOILER EICAS MSG AND ASC LIGHT, ADJ THE CONTROL WHEEL RVDTS PER MM 27-61-00 P515. POSSIBLE PARTS REQ RVDT TS5082 PCN 480-9277. VERIFY EFFECTIVITY WITH ONLINE IPC. FOUND LT CONTROL WHEEL RVDT AT-.50 VOLTS. FOUND RT CONTROL WHEEL RVDT AT-.69 VOLTS. ADJUSTED TO -.48 VOLTS. PERFORMED OPERATIONAL PER MM. NO FAULTS NO MSGS. CHECKS OKAY.

Part: ACTUATOR — OUT OF ADJUST (SPOILER) · airframe 50,191 hrs · 14,140 cycles

SPOILER EICAS MSG CAME ON IN CRUISE. CHECK RVDT ADJUSTMENT AND RIG ADJUSTMENT ON NR 4 SPOILER. CHECKED RVDT ADJUSTMENT AND ADJUSTED. CHECKED RIG ON SPOILER AND ADJUSTED NR 4 SPOILER. OP CHECKED GOOD.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 50,170 hrs · 14,133 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED. SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE LEVER SELECTED TO DOWN. DEFERRED REF MEL 2761A LOCKED OUT SPOILERS 4 AND 9. FOUND NR 4 PCA RVDT OUT OF RANGE, WITH NO RESPONSE WHEN TRYING TO MAKE AN ADJUSTMENT. NEED TO REPLACE NR 4 PCA. FOUND NR 4 ACTUATOR CHECKS BAD. REPLACED ACTUATOR, OPS CHECK OK. NO MESSAGE.

Part: B-NUT — STRIPPED (FUEL/OIL COOLER) · airframe 50,157 hrs · 14,127 cycles

B-NUT TO FUEL BYPASS ELBOW STRIPPED. OIL LINE GOES TO SCAVENGE PUMP (NR 2 ENG). INSTALLED NEW OIL LINE FROM SCAVENGE OIL PUMP TO FUEL OIL HEAT EXCHANGER, NR 2 ENG.

Part: IDG — LACK OF LUBE (NR 2 ENGINE) · airframe 50,133 hrs · 14,119 cycles

RIGHT GEN TRIPPED OFF ON T/O ROLL ABORTED T/O BELOW 60 KNOTS. REPLACED NR 2 ENG IDG PER MM. RAN 5 MINS, NO LEAKS. OPERATED OK UNDER LOAD. FOUND IDG LOW ON OIL ON REMOVAL. BPPC BITE CHECK SHOWS LOW IDG OIL. IDG TRIP. LOW FREQS. CALLED LM TO HAVE IDG OIL RECHECKED.

Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 50,133 hrs · 14,119 cycles

OIL DRIPPING FROM BOTH ENGINES. INSP'D BOTH ENG. FOUND OIL DRIPS FROM ACCUMULATED OIL ON BOTTOM OF COWL AROUND BREATHER HOLE. NO ACTIVE OIL LEAKS FROM DRAINS.

Part: ANTI-ICE VALVE — DEFECTIVE (LT ENGINE) · airframe 50,101 hrs · 14,112 cycles

LEFT ENG EPR FLUCTUATES ABRUPTLY WHEN TURNING ANTI-ICE ON AND OFF. REPLACED NR 1 ENGINE COWL ANTI-ICE VALVE AS PER MM. RAN ENG, OPS CHECK NORMAL.

Part: COMPUTER — FAULTY (AUTOPIOT SYS) · airframe 50,064 hrs · 14,101 cycles

F/O ADI FLT DIRECTOR NO LATERAL GUIDANCE BAR. REPLACED RT FCC AND OP CHECK SATS PER MM. ACP CAT III TEST SATS PER MM.

Part: LANYARD — OUT OF POSITION (L4 DOOR) · airframe 50,068 hrs · 14,103 cycles

DOOR 4L WON'T ARM. FOUND SURVIVAL KIT LANYARD CAUGHT IN GIRT BAR FITTING, SECURED LANYARD AND DOOR ARMING OPS CHECK GOOD.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 50,052 hrs · 14,097 cycles

INST-PANEL (STATE LOCATION) LGT EXTIN. CREW COMMENTS: CAPTS AUTOLND STATUS IND INTEGRAL LTNG 90 PERCENT INOP DOWN TO ONE BULB. NEED MORE TIME TO TROUBLESHOOT. -INF- :NEED AUTOLAND STATUS IND PCN (481-9058). -INF- :IND PCN 481-9058 HAVE BEEN PUT IN LOB. RPL ASA PER MM. THEN ACP AUTOPILOT SYSTEM TEST PER MM, ALL CHECKS SAT. AUTOLAND UPDATED.

Part: RECEIVER — FAULTY (ADF) · airframe 50,041 hrs · 14,093 cycles

ADF AUDIO AT ALL CREW STAT'N IS WEAK, INOP, INTERMIT, ETC WITH ANT MODE SET ON ADF CNTRL PNL. RDMI BEARING POINTER OPERATION OK. CREW COMMENTS: RIGHT ADF DOES NOT PICKUP AURAL NDB SIGNAL. NO AURAL OR SENSE ON NDB FREQS. L ADF OK-NEED MORE TIME. INSTALLED NEW ADF R(M216) PASSED GROUND TESTS PER AMM. ADF CHANGED FOR T.S.

Part: AUDIO PANEL — INOPERATIVE (COCKPIT) · airframe 50,040 hrs · 14,092 cycles

CAPTS AUDIO PNL NEEDS TWO SATCOM INOP STIKERS. REPLACED AUDIO SELECTOR PANEL. RADIO CHECKED WITH 130.22, RADIO CHECKED NORMAL ON GROUND.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 49,979 hrs · 14,077 cycles

CREW REPORTS TRIM INOP IN COCKPIT AND BOTH CABIN ZONES. REPLACED CABIN TEMP CONTROLLER, CHECKS OKAY, NO MSGS.

Part: CABLE — DAMAGED (SLAT SYSTEM) · airframe 49,978 hrs · 14,076 cycles

L/E SLAT ASYM DISPLAY, AIR TURNBACK. ACCOMPLISHED TROUBLESHOOTING PER MM. FSEU NR 1 SHOWS SLAT LOSS 317 ON FLIGHT LEG "0". FSEU NR 2 BITE SHOWS SLAT LOSS 337 ON EXISTING FAULTS. FOUND LT INBD SLAT LOSS SWITCH CABLE DAMAGED WITH TEFLON COATING JAMMED UP INSIDE TUBE. REPLACED CABLE. LT WING OTBD SW CABLE SPRING MECHANISM WRAPPED INCORRECTLY. LEFT INBD SLAT LOSS WHITE HOOK SPRING IS WRONG PART (TOO LONG) PER IPC. REPLACED HOOK SPRING. AFTER OPEN LT WING OTBD PANEL FOR OTBD SLAT LOSS SWITCH FOUND TRIGGERED ALSO. FOUND HOOK SPRING CATCHING ON COIL SPRING AND COIL SPRING ORIENTATED INCORRECTLY, REPLACED COIL SPRING & HOOK SPRING. REPLACED SPRING & HOOK FOR RT INBD LE SLAT LOSS SWITCH WITH CORRECT CONFIG PARTS, OP CHECKED GOOD. NO BINDING, NO FAULTS.

Part: PANEL — HOT (SIDEWALL) · airframe 49,765 hrs · 14,011 cycles

FLT CREW REPORTING SIDEWALL PANEL VERY WARM-HOT TO TOUCH AT ROW 20 RT SIDE. OPS CHECKED OVERWING EXIT HEATER SYSTEM IAW MM. CHECKED GOOD. HEATER CYCLES ON AND OFF, AND IS NO WARMER THAN LEFT SIDE HEATERS.

Part: CONTROL VALVE — FAULTY (STARTER) · airframe 49,759 hrs · 14,009 cycles

LEFT ENGINE START VALVE WOULD NOT OPEN. TWO ATTEMPTS, START VALVE WON'T OPEN NORMALLY. REPLACED STARTER CONTROL VALVE, OP CHECKED NORMAL.

Part: ACTUATOR — FAILED (SPAR VALVE) · airframe 49,744 hrs · 14,004 cycles

RIGHT FUEL SPAR VALVE EICAS MESSAGE DURING ENGINE START ATTEMPT. CREW TRIED TO CYCLE CIRCUIT BREAKER E02, FUEL VALVES RIGHT SPAR. BREAKER WOULD NOT STAY CLOSED. REPLACED RT SPAR VALVE ACTUATOR, OPS CHECKED OKAY.

Part: LINE — UNSECURE (OXYGEN SYSTEM) · airframe 49,629 hrs · 13,965 cycles

CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: OXY PRESS 710. REPEAT WRITE-UP. SECURED LINE ON REGULATOR AT BOTTLE. PRESS AT 1750. SECURED CONE SHAPED DIAPHRAM HOUSING, RESAFETIED. LEAK CHECK OKAY.

Part: MODULE — FAULTY (STALL WARNING) · airframe 49,536 hrs · 13,939 cycles

EICAS MSG "WARN ELEX" DISPLAYED. CREW COMMENTS: STATUS MSG WARN ELEX DISPLAYED DURING FLIGHT. SAMC TEXT: DUE TO THE REPETITIVE GRIPES, MUST HAVE A POSITIVE FIX. TROUBLESHOT PER MM & REPLACED LEFT STALL WARNING MODULE PER MM. CHECKED OKAY PER MM.

Part: MODULE — FAULTY (WARNING SYSTEM) · airframe 49,535 hrs · 13,938 cycles

WARN ELEX STATUS MSG. DUE TO REPORTS OF WARN ELEX STATUS MSG AND NO FAULTS FOUND AFTER FIM 31-51-00 ACCOMPLISHMENT AND POWER SUPPLY 'A' M616 HAS BEEN REPLACED (SEQ5252004, PLZ REPLACE POWER SUPPLY 'B' M621 PER MM, (PCN 481-9027), PLZ CHECK WITH ON LINE IPC FOR PROPER EFFECTIVITIES. REPLACED M621 MODULE,CHECK OK PER MM.

Part: MODULE — FAULTY (WARNING SYSTEM) · airframe 49,525 hrs · 13,936 cycles

EICAS MSG "WARN ELEX" DISPLAYED. CREW COMMENTS: WARN ELEX STATUS MSG DSPL IN FLT. THIS IS THE 4TH OCC. SYS TESTS & CB RESETS ARE NOT A FIX. UNABLE TO DUPLICATE WRITE-UP, ACCOMPLISHED FIM 31-51-00, NO FAULTS. REPLACED M616 POWER SUPPLY MODULE A PER LM1617.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 49,519 hrs · 13,934 cycles

F/O FD FAILED ROLL MODE IN CRUISE. REPLACED RT FCC PER MM. PASSED FCC RT GROUND MCDP TEST. THE FCC GENERATES F-D COMMANDS. PER MM ACCOMPLISHED CAT 3 FOR FCC REPLACED PER MM. F-D BARS COME ON WITH F/O FD SWITCH ON, MCP OK NOW.

Part: CIRCUIT CARD — FAULTY (WEU) · airframe 49,514 hrs · 13,932 cycles

LEFT AIR DATA COMPUTER DOES NOT TEST. REPLACED M999 WEU CARD MODULE PER MM, OPS CHECKED OKAY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,505 hrs · 13,929 cycles

CORROSION ON FLOORBEAM AT STATION 1640 LBL 22 - RBL 58. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM AT BS 1640 BETWEEN LBL 9.5 TO THE RT SIDE FRAME JOINT IAW PD 57-53-168 AND EVA 81201 WITHOUT DEVIATION.

Part: FRAME — DAMAGED (NR 1 PYLON) · airframe 49,505 hrs · 13,929 cycles

AFT FRAME WEB IS BENT AND CRACKED ON THE OUTBOARD TOP CORNER OF THE NR 1 PYLON AT NACELLE STATION 206.0. MAJOR REPAIR ACCOMPLISHED. AFT BULKHEAD DAMAGE AT NAC STATION 201.3 BELOW LEFT MOUNT ATTACH FLANGE WAS REPAIRED PER THE INSTRUCTIONS ON PD 57-54-018 AND EVA 81227 WITHOUT DEVIATION. CF ITEM CREATED FOR RECHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,505 hrs · 13,929 cycles

ROW 28 OVERHEAD STORAGE BIN EEL LIGHT INOPERATIVE. RELAMP AND OPS CHECKED LIGHT BULB ABOVE SEAT 28D.

Part: SKIN — CRACKED (R1 DOOR) · airframe 49,505 hrs · 13,929 cycles

R-1 FWD GALLEY DOOR HAS CRACK ON INTERIOR SKIN INBOARD OF LOWER LATCH TORQUE TUBE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, ACCOMPL'D HFEC NO CRACKS NOTED, FABRICATED AND INSTALLED DOUBLER AND STRAPS PER EA PD 57-52-026 ON NR 3025N00423.

Part: LIGHT — MISSING (CABIN) · airframe 49,505 hrs · 13,929 cycles

ROW 22 EEL PATH LIGHT MISSING UPON ARRIVAL. REPLACED AND OPS CHECKED THE FLEX LAMP AT SEAT ROW 22 PER MM AND INSPECTED BY QC. OPS CHECKED GOOD.

Part: LEAD — DAMAGED (CABIN) · airframe 49,505 hrs · 13,929 cycles

ROW 39 EEL PATH LIGHT DAMAGED. REPLACED & OPS CHECKED THE EEL LEAD IN CABLE AT STA 1542 PER MM. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,505 hrs · 13,929 cycles

ROW 12 EEL PATH LIGHT INOPERATIVE. REPLACED & OPS CHECKED THE LEAD IN CABLE AT STA 980 PER MM AND INSPECTED BY QC. OPS CHECKED GOOD.

Part: CABLE — DAMAGED (CABIN) · airframe 49,505 hrs · 13,929 cycles

ROW 35 EEL PATH LIGHT DAMAGED UPON ARRIVAL. REPLACED & OPS CHECKED THE LEAD IN CABLE AT STA 1542 PER MM AND INSPECTED BY QC. OPS CHECKED GOOD.

Part: SKIN — CRACKED (L4 DOOR) · airframe 49,505 hrs · 13,929 cycles

THE 4L DOOR CRACKED ON INTERIOR SKIN INBOARD OF LOWER LATCH. MAJOR REPAIR ACCOMPLISHED. CRACKS FOUND ON THE LIGHTNING HOLE FLANGE OF THE P/N 146N6100-671 INNER SKIN AT BS 1671. TRIMMED OUT DAMAGE & PROVIDED AN INSURANCE CUT. ACP NDT OF CUT- OUT & OPEN HOLES. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR REF EA PD57-52-027.

Part: SKIN — DENTED (BS 1706 S13-14R) · airframe 49,505 hrs · 13,929 cycles

DENT ON EXTERIOR FUSELAGE SKIN AT BS 1706 BETWEEN S13-14R. MAJOR REPAIR ACCOMPLISHED. EVALUATED DENT & FOUND OUT OF LIMITS OF SRM 53-60-01. ACCOMPLISHED NDT & TRIMMED OUT EDGES AND FASTENER HOLES. NO CRACKS FOUND. FABRICATED & INSTALLED EXTERNAL FILLER, DOUBLER & TRIPLER REPAIR REF EA PD57-53-169 & EVA 81215.

Part: FRAME — DENTED (BS 1520 S25-26L) · airframe 49,505 hrs · 13,929 cycles

DENT IN FRAME AT STATION 1520 BETWEEN STR 25 AND 26L. ACCOMPLISHED ON TASK CARD 3025N00411 DENT IN FRAME AT STATION 1520 BETWEEN STR 25 & 26 L.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 49,505 hrs · 13,929 cycles

CORROSION ON FLOORBEAM AROUND FASTENERS STATION 345 RBL 0 - RBL 21. REPAIRED PER SRM 53-00-51, PG 203, FIG 201.

Part: CONTROL UNIT — FAULTED (GALLEY) · airframe 49,473 hrs · 13,920 cycles

G4A GALLEY CB FOUND POPPED. REPLACED GALLEY ELECTRIC CONTROL UNIT FOR GALLEY G4A (M225) PERMM, CHECKED OKAY.

Part: BATTERY — FAULTY (APU) · airframe 49,324 hrs · 13,876 cycles

TWO START ATTEMPTS - FAULT BOTH TIMES. REPLACED BATT WAS HOT WITH SLOW START FAULT MSG. REPLACED APU BATT AND APU BATT CHARGER. APU START WAS NORMAL. ALL MSGS WERE ALL ERASED.

Part: CONTROLLER — FAULTY (CABIN) · airframe 48,981 hrs · 13,774 cycles

RIGHT PACK WENT FULL COLD PLACED SELECTOR IN STBY NORMAL. BITE SHOWS CONTROLLER FAULT. REPLACED RT CONTROLLER. OPS CHECK OKAY.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 48,981 hrs · 13,774 cycles

RT PACK TRIPPED OFF ON FINAL. REPLACED FCV, OPS CHECKS OK.

Part: LIGHT — BUCKLED (CABIN) · airframe 48,863 hrs · 13,743 cycles

EMERGENCY FLOOR EXIT LIGHTS AT ROW 12-13 BUCKLED UP. TRACK NOT ADHERING TO FLOOR. INSTALLED NEW ADHESIVE STRIP BETWEEN EEL TRACK AND FLOOR, CHKS OK.

Part: INDICATOR — INOPERATIVE (FUEL) · airframe 48,673 hrs · 13,690 cycles

FUELER REPORTS LT MAIN TANK INDICATION INOP AT FUELING PANEL. NEEDS NEW INDICATOR, PCN 481-9228. PART NOT STOCKED IN SEA. FUELING AND OPS ADVISED. REPLACED LT MAIN TANK UNDER WING FUEL INDICATOR PER MM. OPS CHECKS NORMAL.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 48,671 hrs · 13,689 cycles

NR 1 ENG START VALVE LIGHT CAME ON OTHER THAN DURING START. EICAS MSG STARTER CUTOUT DISPLAYED. CREW COMMENTS: INTERMITTENT LIGHT. NO DUCT PRESSURE CHANGE. SUSPECT FAULTY CAUTION LIGHT. VERY DISTRACTING. RPL START VALVE, RAN ENG OPS NORMAL.

Part: CONTROL SWITCH — FAULTY (COCKPIT) · airframe 48,679 hrs · 13,691 cycles

LEFT WINDSHIELD WIPER CAME ON DURING DESCENT WITH THE SWITCH OFF. STAYED ON FOR 2 MINUTES. REPLACED WIPER CONTROL SW, RAN SEVERAL TIMES. ALL WORKED OKAY.

Part: STARTER — DAMAGED (NR 1 ENGINE) · airframe 48,666 hrs · 13,687 cycles

NR 1 ENG STARTER OIL DRAIN HOLE HELICOIL STICKS OUT AND PLUG IS PARTIALLY STRIPPED. REPLACED NR 1 ENG STARTER.

Part: CONDENSER — FAULTY (AC BAY) · airframe 48,638 hrs · 13,677 cycles

LEFT PACK STILL COOLS POORLY ON GROUND. OK IN FLIGHT REPEAT GRIPE. OK WITH DISPATCH. REPLACED PACK TEMP CONT, NO HELP. TRIM VALVE SHOWS NO MOVEMENT FOR FLT DECK AND PACK OUT TEMP 40-50 DEGREES HOTTER THAN RT PACK. RAN LT PACK, FOUND TRIM VALVE OPERATING NORMALLY. CONDENSER NOT ALLOWING COLD AIR TO FLOW THROUGH, SUSPECT INTERNAL DAMAGE. CONDENSER PART #631-0505 ON AOG U0610. REPLACED LEFT PACK CONDENSER PER MM. LEAK CK AND PACKOUT TEMP NORMALIZED.

Part: EEC — FAULTY (LT ENGINE) · airframe 48,646 hrs · 13,680 cycles

THE FOLLOWING EPCS MESSAGES PRESENT FOR NR 1 ENG. (P) PMA-EEC, (P) EEC, (S) EEC, (S) 275-25, (S) 275-24. REPLACED LEFT ENG EEC. CHKS NORMAL.

Part: STATIC WICK — MISSING (ELEVATOR) · airframe 48,646 hrs · 13,680 cycles

FOUND RT ELEVATOR STATIC DISCHARGER MISSING, SECOND FROM OUTBOARD EDGE. REQUIRED PART PCN 170-1067 IS NOT STOCK AT MCO. DEFERRED PER CDL 23B. REPLACED STATIC DISCHARGER.

Part: LIGHT — LOOSE (CABIN) · airframe 48,638 hrs · 13,677 cycles

EMERGENCY LIGHT STRIP AT 13C IS LOOSE. SECURED STRIP.

Part: ACM — FAULTY (AC BAY) · airframe 48,627 hrs · 13,672 cycles

CREW REPORT: LEFT PACK RUNS APPROX 30 DEGREES WARMER ON GROUND THAN RIGHT PACK. IN FLT, LEFT PACK OK. CKED INLET FOR FOD, NON PRESENT REPLACED ACM PER AMM, OPS CK'D GOOD

Part: SENSOR — FAULTY (AC PACK) · airframe 48,614 hrs · 13,669 cycles

LEFT PACK OUTLET TEMP WON'T GO BELOW 90 DEGREES. PERFORMED PACK BITE PER MM, NO FAULTS FOUND. REPLACED NR 1 SYS PACK TEMP SENSOR PER MM. CHECKED AIR CYCLE MACHINE PER MM. RAN PACK, OPS GOOD.

Part: FITTING — CRACKED (AC PACK) · airframe 48,614 hrs · 13,669 cycles

LEFT PACK LOW LIMIT CONTROL VALVE HAS A CRACKED MS FITTING ON THE CONDENSER OUTLET SENSE LINE. REPLACED FITTING ON LOW LIMIT CONTROLLER. CHECKED SENSE LINES ON LOW LIMIT VALVE. LEAK AND OPS CHECK GOOD.

Part: IDG — FAULTY (LEFT) · airframe 48,124 hrs · 13,515 cycles

LEFT ENGINE GEN DROPPED OFF LINE ON FINAL. RESET ON 1ST ATTEMPT. REPLACED NR 1 IDG PER MM. LEFT ENGINE IDG WAS DISCONNECTED FOR DEF. THEN DF NOT FINISHED. STILL DISCONNECTED. CONFIRMED IDG CONNECTED DURING ENG RUN. LEFT ENGINE GEN DRIVE LIGHT NOT ILLUMINATED. CREW RAN ENGINE, DRIVE LIGHT CAME ON AFTER SHUT DOWN. DUE TO CHRONIC HISTORY OF LEFT ENG IDG ISSUES, RESTRICT ACFT TO DOMESTIC ONLY OPERATIONS FOR 5 CYCLES WITH LEFT ENG IDG OPERATING NORMAL. NR 1 ENGINE IDG INOP. ELECTRIC PAGE SHOWS NO VOLTS OR FREQ. RESET GEN CONTROL SWITCH NO HELP. REPLACED NR 1 ENGINE IDG IAW AMM. COMPLETED NR 1 ENGINE IDG INSTALLATION PER MM, LEAK CHECK AND TEST GOOD. DUE TO CHRONIC IDG REPLACEMENT WITH NO APPARENT LEAKS AND IDG'S FOUND WITH LOW OIL REPLACE NR 1 ENG IDG FOC AND BYPASS VALVE. REPLACED FUEL OIL EXCHANGER PER AMM AND FUEL OIL BYPASS VALVE PER AMM. ACP IDLE TEST NR 3 AND LEAK CHK OKAY.

Part: O-RING — LEAKING (HYD LINE) · airframe 48,124 hrs · 13,515 cycles

RT WHEEL WELL INTERLOCK ACTUATOR (M10279) LEAKING AT UNION FITTING OUTBD LINE (MKD W-TAPE). REPLACED O-RING AND SECURED LINE. LEAK CHECKED. NO LEAKS NOTED.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 48,060 hrs · 13,492 cycles

WXR FAIL RT DSPLYD ON HSI WHEN IN WX TEST. REPLACED WEATHER RADAR TRANSCEIVER UNIT, OPS CHECK OKAY.

Part: INDICATOR — DEFECTIVE (FUEL SYSTEM) · airframe 48,011 hrs · 13,478 cycles

FUELER REPORTED UNABLE TO READ ALL NUMBERS OF CENTER FUEL TANK GAUGE AT SERVICE PANEL. ONLY AFTER THE DECIMAL POINT IS ILLEGIBLE. REPLACED FUEL IND, CHECKS OKAY.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 48,011 hrs · 13,478 cycles

UNWANTED FUEL TRANSFER FROM LEFT WING TO CENTER TANK WHILE ON GROUND. FOUND LEFT DEFUEL VALVE STUCK IN OPEN POSITION. REPLACED LEFT DEFUEL VALVE ACTUATOR PER AMM. NO UNWANTED FUEL TRANSFER OBSERVED AFTER REPLACEMENT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 47,809 hrs · 13,418 cycles

EMERGENCY FLOOR LIGHTING INOP AT OVERWING EXITS. REPLACED BATTERY PACK, LOCATED ABOVE LT STOW BIN AT OVERWING EXIT.

Part: IDG — FAULTY (LT GENERATOR) · airframe 47,710 hrs · 13,385 cycles

LEFT GENERATOR DRIVE LIGHT INOP. NO EICAS MESSAGE WHEN GENERATOR DISCONNECTED. REPLACED LT IDG IAW MM. GROUND RUN NORMAL.

Part: FAN — FAULTY (POSITION 1) · airframe 47,430 hrs · 13,294 cycles

OVERHEAT ON EQUIP COOLING OK IN ALT ON GROUND. ALT OK. DUE ETOPS SENSITIVE, IF UNABLE TO DUPLICATE, REPLACED NR 1 POSITION EQUIP COOLING FAN PER MM.

Part: TRANSCEIVER — FAULTY (WX RADAR SYS) · airframe 46,873 hrs · 13,125 cycles

WITH WEATHER TURB SELECTED WEATHER FAIL LIGHT APPEARS ON HSI NO GROUND RETURNS INDICATED. RESET CB, NO HELP. REPLACED WX RADAR TRANSCEIVER, ACCOMPLISHED TEST NO FAULTS.

Part: FUEL CONTROL — LEAKING (NR 2 ENGINE) · airframe 46,755 hrs · 13,091 cycles

FUEL DRIPPING FROM NR 2 ENGINE ONE DROP EVERY 4 SECONDS. NR 2 ENGINE FUEL CONTROL LEAKING AT REAR MATING SURFACE, REPLACED PER MM. PERFORMED ACCELERATION TEST. ENGINE MEETS ACCELERATION PERFORMANCE REQUIREMENTS, NO LEAKS.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 46,537 hrs · 13,023 cycles

ON WALK AROUND FOUND RT WELL LEAKING HYDRAULIC FLUID. FOUND RT SYS RELIEF VALVE LEAKING FROM LOWER UNION. REPLACED PACKING AND SERVICED HYDRAULICS, OPS CHECKS GOOD.

Part: WINDOW — CRACKED (SEAT 32F) · airframe 46,312 hrs · 12,955 cycles

WINDOW AT SEAT 32F HAS EXTERIOR CRACK. LOUD CRACK HEARD BY FA'S ON CLIMBOUT. SAMC TEXT: CRACK REPORTED BY CREW IN OUTER PANE. REPLACED PASSENGER WINDOW ASSY AT 32F.

Part: EXTINGUISHER — LEAKING (AFT GALLEY AREA) · airframe 46,024 hrs · 12,858 cycles

AFT WATER FIRE EXT LEAKING. REPLACED FIRE EXTINGUISHER AFT GALLEY AREA.

Part: LINK — DISPLACED (PAX DOOR) · airframe 46,024 hrs · 12,858 cycles

MAIN ENTRY DOOR 4 LT LOWER BODY TORQUE TUBE BEARING, LOWER LINK OUT OF SERPENTINE PLATE, IN 2 PIECES. R & R LOWER CAM PLATE REINSTALLED BOTH PLATES AND LWR LINK. REMAINING WORK COVERED BY ADDITIONAL SMC ITEMS.

Part: FITTING — FAILED (LT TE FLAP) · airframe 46,024 hrs · 12,858 cycles

LT INBD AFT AFT FLAP DRIVE TORQUE TUBE ATTACH FITTING ON LWR SURFACE BEARING RETENTION FAILED, BEARING MIGRATED BUT TRAPPED INSIDE TUBE LUGS AND FITTING. R & R FITTING ASSY.

Part: BEARING — MIGRATED (L2 DOOR) · airframe 46,024 hrs · 12,858 cycles

2 LT ENTRY DOOR BODY TORQUE TUBE LOWER SERPENTINE PLATE BEARING MIGRATED UP OUT OF PLATE. RESEATED BEARING ASSY.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,791 hrs · 12,787 cycles

FLIGHT DECK REPORTS FUEL ODOR IN FLIGHT DECK AT GATE AFTER SHUTDOWN. RAN LT ENG. CHECKED FOR FUEL LEAKAGE AFTER SHUTDOWN AT DIFFUSER AND COMBUSTION SECTION. NO LEAKAGE NOTED AND NO SMOKE EVIDENT. REMAINING ODOR IS RESIDUAL. DEEMED OKAY FOR SERVICE.

Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 45,474 hrs · 12,701 cycles

FOUND EQUIPMENT COOLING SUPPLY FAN 1 CIRCUIT BREAKER TRIPPED ON P6 AT F17. FWD EQ COOLING FAN INOP. CB PULLED AND COLLARED. AC ROUTED NON-ETOPS TO HNL FOR FIX. REPLACED NR 1 COOLING FAN PER MM. OPS CHECK NORMAL.

Part: CONTROL PANEL — FAULTY (AUTOPILOT) · airframe 45,430 hrs · 12,690 cycles

VERTICAL SPEED WINDOW DOES NOT DISPLAY THE PLUS OR MINUS SIGN. REPLACED AUTOPILOT MODE CONTROL PANEL IAW MM, GROUND CHECKS NORMAL. ACP'D CAT III TEST IAW MM. ACFT RETURNED TO CAT III STATUS.

Part: EEC — FAULTY (RT ENGINE) · airframe 46,253 hrs · 12,641 cycles

RT ENG SEC CONT STATUS MSG. CREW SHUTDOWN ENG PER SAM & CLEARED FAULT. MSG RETURNED AFTER ENG RESTART. EPCS MSGS 275-16. NOTES EEC, S275-25 AND S275-16 MESSAGES RECORDED ON EPCS PAGE. REPLACED R ENG EEC PER MM, OPS CHECK OK PER MM, RAN ENG PER JRH. REPLACED R ENG EEC PER MM. OPS CHECK OKAY. RAN ENG PER JRH.

Part: BULB — OUT OF ADJUST (EMERGENCY LIGHT) · airframe 45,093 hrs · 12,597 cycles

L1 DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. OP CKS GOOD, ADJUSTED BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,093 hrs · 12,597 cycles

EMERGENCY LIGHT STRIP JUST AFT OF 2L ENTRY DOOR IS INOP. REPLACED DAMAGED EMERGENCY LIGHT STRIP. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,093 hrs · 12,597 cycles

EMERGENCY LIGHT STRIP NEXT TO AFT FWD LAV IS INOP. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (WX RADAR) · airframe 44,810 hrs · 12,516 cycles

AUTO TILT ON WX RADAR NOT PAINTING GROUND RETURN POINTING TOO HIGH. MANUAL TILT ALSO SEEMS OFF. REPLACED THE WX RADAR CONTROL PANEL. ACCMP'D FLIGHT DECK SELF TEST, TESTED OK.

Part: IDG — FAULTY (NR 2) · airframe 44,677 hrs · 12,474 cycles

NR 2 ENG IDG OIL HAS FOUL ODOR & IS BURNED. REPLACED IDG AND FLUSHED SYS REF AMM.

Part: CONTROL VALVE — NOISY (RT RECIRCULATION) · airframe 44,100 hrs · 12,314 cycles

RT RECIRC FAN NOISY. COMMUNICATION & BRIEFING EXTREMELY DIFFICULT. CHRONIC HISTORY OF NOISE. POSSIBILITY DUCT BLOCKAGE AND RECORD CFM AND NOISE FINDINGS. WILL NEED UP TO 6SH SLOT TO ACP. REPLACED 2 EA RECIR FILTERS, FLOW AND DECIBEL CHECK WITHIN LIMITS BUT VELOCITY STILL NOT WITHIN, NEED TO REPLACED LT PACK FLOW CONTROL VALVE UNDER OSTF H1415. DUCT LEAK CHECKED OK. REPLACED LT FLOW CONTROL VALVE. LEAK & OP CHECKED. OPS TEST GOOD REF SERVICE TIP21-22-00 FLOW OF 371FPM & 72 DB NOISE.

Part: STARTER — FAILED (APU) · airframe 43,639 hrs · 12,178 cycles

APU FAILED TO START. FAULT LIGHT ILLUMINATED & EICAS MSG. APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. REPLACED APU STARTER & APU CRANK CONTACTOR. FOUND A 2" DIAMETER HOLE IN STARTER MOTOR CASING. REPLACED APU STARTER, AUTO SHUTDOWN WITH "LOP" FAULT. APU AUTO SHUTDOWN AT 90 PERCENT RPM. ECU FAULT DISPLAY "LOP", FAULT UNIT "STARTER CIRCUIT". STARTED T-S REF FIM 49-11-00 FIG 109. REPLACED LOP, NO HELP. REPLACED OIL FILTERS IAW FIM. START OK. HEAVY SMOKE FROM STARTER AT SHUTDOWN. SUSPECT STARTER NO CUTOUT. REPLACED STARTER & CRANK CONTACTOR, NO HELP. TRIED NEW ECU & START RELAY K197, NO HELP. 1ST START ATTEMPT OK. 2ND ATTEMPT BURNED OUT STARTER. REPLACED STARTER AGAIN. OPS NORMAL.

Part: MOTOR — FAULTY (APU STARTER) · airframe 43,308 hrs · 12,093 cycles

APU WILL NOT START. ECU BITE SHOWED SLOW START WITH STARTER CIRCUIT. T/S IAW MM AND FOUND STARTER MOTOR WITH EVIDENCE OF INTERNAL SHORTING. STARTER MOTOR BURNED. REPLACED STARTER. REPLACED APU CRANK CONTACTOR. APU WORKS NORMAL.

Part: IDG — LEAKING (NR 1 GCU) · airframe 43,206 hrs · 12,070 cycles

OIL ACTIVELY DRIPPING OUT OF LT ENG. R & R NR1 ENG IDG. BITE CHECKED BPCU "HIGH IDG TEMP RISE" CHECKED IDG LEVEL LOW. SERVICED IDG, RAN L ENG. LOADED ELEC SYS OPS GOOD FOR LT IDG. VERIFICATION FLIGHT CONFIRMS NORMAL OPERATION.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN AIR) · airframe 42,907 hrs · 11,988 cycles

EXCESSIVE AIR NOISE IN COCKPIT. CABIN CEILING PANELS ARE REMOVED. CLEANED DISTRIBUTION DUCT FOR EACH OUTLET FROM FIRST TO SEAT ROW 18A-F. CONTINUED ON THROUGH ROW 18. WILL REPLACE FLOW CONTROL VALVE. THEN OPS CHKS AND CABIN RESTORE TO FOLLOW. CLEANING ACCOMPLISHED. OKAY FOR SERVICE.

Part: PACKING — LEAKING (NR 2 ENGINE FUEL) · airframe 42,907 hrs · 11,988 cycles

NR2 ENG IS LEAKING FUEL FROM PLUG ON FUEL CONTROL, INBD SIDE. REPLACED PACKING AS3208-04. LEAK CHKS OK.

Part: GEARBOX — WORN (TE FLAP) · airframe 42,395 hrs · 11,831 cycles

RIGHT T/E FLAP ANGLE TEE GEARBOX RATTLES AND CHATTERS THROUGHOUT RIGHT SIDE, UNABLE TO LOCATE SOURCE OF PROBLEM, LEFT SIDE IS SMOOTH AND QUIET, HYD POWER OR ELECTRIC MAKES NO DIFFERENCE, BUT SOUND IS MUCH LOUDER WITH ELECTRIC MOTOR. SUSPECT WORN OUTPUT GEAR ON ANGLE TEE BOX IS CAUSING THE PROBLEM. RT T/E FLAP ANGLE TEE GEARBOX RATTLES AND CHATTERS THROUGHOUT RT SIDE, UNABLE TO LOCATE SOURCE OF PROBLEM, LT SIDE IS SMOOTH & QUIET, HYD POWER OR ELECTRIC MAKES NO DIFFERENCE, BUT SOUND IS MUCH LOUDER WITH ELECTRIC MOTOR. SUSPECT WORN OUTPUT GEAR ON ANGLE TEE BOX IS CAUSING PROBLEM.

Part: LEAD — DAMAGED (EMERGENCY LIGHT) · airframe 42,210 hrs · 11,772 cycles

K-LAV EMERGENCY LIGHT BAR INOP. SPLICED NEW LEAD-IN. OPS CHECKS GOOD.

Part: GCU — MALFUNCTIONED (LEFT) · airframe 42,210 hrs · 11,772 cycles

EICAS MSG L GEN OFF DISPLAYED AT FL 240. OPERATED NORMAL AFTER RESET. REMOVED AND REPLACED LEFT GENERATOR CONTROL UNIT AND TEST PERFORMED. FOUND GOOD.

Part: GEARBOX — FAILED (TE FLAP) · airframe 42,210 hrs · 11,772 cycles

TRAILING EDGE FLAP NR 6 ANGLE GEARBOX FAILED INSP AXIAL MOVEMENT. REMOVED AND REPLACED NR 6 ANGLE GEARBOX. GEARBOX OPS CHECK GOOD.

Part: GEARBOX — FAILED (TE FLAP) · airframe 42,210 hrs · 11,772 cycles

TRAILING EDGE FLAP NR 3 ANGLE GEARBOX FAILED INSP AXIAL MOVEMENT. REPLACED NR 3 ANGLE GEARBOX, OPS CHECK GOOD.

Part: FSEU — FAULTY (NR 3) · airframe 42,210 hrs · 11,772 cycles

EICAS MSG - FLAP SLAT ELEC BITE WILL NOT CLEAR. REPLACED FSEU 3. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,210 hrs · 11,772 cycles

EXT EMERGENCY LIGHTS DOOR 2L AND 2R ARE INOP. RELAMPED EXT EMERGENCY LIGHTS AND OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,210 hrs · 11,772 cycles

EXT EMERGENCY LIGHT RT MID OVERWING INOP. RELAMPED EXT EMERGENCY LIGHT AND OPS CHECKS GOOD.

Part: STARTER — FAULTY (APU) · airframe 42,148 hrs · 11,749 cycles

TWO ATTEMPTS APU FAULTS. REPLACED APU STARTER & APU BATTERY. OPERATIONAL CHECKS ARE NORMAL.

Part: CIRCUIT CARD — DEFECTIVE (RT ENGINE) · airframe 41,968 hrs · 11,690 cycles

NUMEROUS EICAS MSGS, RTFL. RIGHT ENGINE SPEED CARD, RIGHT ENGINE ANALOG N2, RIGHT PACK OFF, RIGHT ENG BLEED OFF, RIGHT AFT FUEL BOOST PUMP OFF EICAS MESSAGES DISPLAYED, PER CREW. SUSPECT BAD SPEED CARD FROM STOCK. REPLACED RT ENGINE SPEED CARD, RAN ENG, ALL INDICATIONS NORMAL.

Part: BPCU — MALFUNCTIONED (ELECTRICAL SYS) · airframe 41,831 hrs · 11,646 cycles

EICAS MSG L GEN OFF DISPLAYED. GEN OFF LIGHT ILLUM. OPERATED NORM AFTER RESET. CREW COMMENTS: RESET OKAY. REPLACED BPCU. SWAPPED NR 2 AND APU GCU'S PRECAUTIONARY. RAN BOTH ENGINES, BOTH ENGINES AUTO R TRANSFER FROM APU AND BACK TO APU ON ENGINE SHUT DOWN. SYSTEMS BITE CHECK OK.

Part: GCU — FAULTY (LT ENGINE) · airframe 41,765 hrs · 11,629 cycles

EICAS MSG L GEN OFF DISPLAYED. GEN OFF LIGHT ILLUMINATED. OPERATED NORMAL AFTER RESET. CREW COMMENTS: REPEAT GRIPE. LEFT GEN CONTROL OFF LT ILLUMINATED ON CLIMB-OUT. RESET NORMAL. LEFT GEN TRIPPED SECOND TIME. APU STARTED FL370. BPCU SHOWED "OPEN PHASE TRIP" AND "GEN-FDR" MSGS. REPLACED LEFT ENG GCU. BPCU BITE TEST IS OKAY. REPLACED LT IDG. OPS CKS OKAY. REPLACED NR 1 GENERATOR CONTROL BREAKER. ALL CONNECTIONS SECURE WITH NO EVIDENCE OF ANY ARCING OR DISCOLORED LUGS AT CONNECTION POINTS.

Part: CONTROLLER — FAULTY (AC BAY) · airframe 41,532 hrs · 11,563 cycles

MASTER TRIM AIR VALVE APPEARS INOP, ALL 3 ZONES FLT DECK, FWD CABIN, AFT CABIN TRIM AIR INDICATOR INOP WITH TRIM AIR SWITCH SELECTED ON. PACK MAINTAINING 75 DEGREES. REPLACED CONTROLLER AND OPS CHECK OKAY.

Part: INDICATOR — OBSTRUCTED (RT FUEL QTY) · airframe 41,358 hrs · 11,509 cycles

RIGHT FUEL QUANTITY INDICATOR HAS AIR BUBBLES THAT OBSCURE THE MAIN TANK AND TOTALIZER VALUE. REPLACED FUEL QUANTITY INDICATOR, INDICATION TEST GOOD NO MESSAGES NOTED.

Part: TRANSCEIVER — FAILED (HF COMM) · airframe 40,998 hrs · 11,397 cycles

RIGHT HF RADIO UNABLE TO XMIT. RECEPTION GOOD BOTH VOICE & SELCAL. REPLACED RIGHT HF XCVR.

Part: CHARGER — FAILED (APU) · airframe 40,957 hrs · 11,383 cycles

APU AUTOSHUT DOWN. REPLACED APU BATTERY CHARGER. APU OPS CHECKED OKAY.

Part: OXYGEN SYSTEM — LOW PRESSURE (CREW) · airframe 40,808 hrs · 11,338 cycles

CREW O2 PRESSURE LOW. NEEDS SERVICE. SERVICED CREW 02.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,179 hrs · 10,883 cycles

NR 1 RT FWD DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,179 hrs · 10,883 cycles

NR 3 RT MED EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. OPS CHECKED OK

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 39,055 hrs · 10,850 cycles

SECOND TIME RECEIVE INOP HF RIGHT RADIO FREQ 5574. RETUNE, NO HELP. REPLACED RT HF TRANSCEIVER AND F/O'S AUDIO SELECT PANEL. OPS CHECK FOR RT HF NOW TESTS OK.

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 38,892 hrs · 10,804 cycles

EICAS MSG WING ANTI-ICE DISPLAYED. REPLACED ANTI-ICE VALVE RIGHT WING. ANTI-ICE VALVE SENSE LINE FITTING AND B-NUT STRIPPED AT LINE TO VALVE. NEEDS NEW LINE AND FITTING. BOTH ENDS OF SENSE LINE STRIPPED NEED NEW LINE AND BOTH UNIONS REPLACED. REPLACED LINE AND FITTINGS.

Part: COMPUTER — FAULTY · airframe 38,854 hrs · 10,794 cycles

ACMS SYSTEM FAULTY. ACCMP FLIGHT DATA ACQUISITION MGMT UNIT SOFTWARE UPLOAD.

Part: CONTROL VALVE — MALFUNCTIONED (L/E SLAT) · airframe 38,232 hrs · 10,626 cycles

AUTO SLAT STALL WARN EXTENSION AND RETRACTION INOP. REPLACED FSEU 3. CHECKS OK. AUTO SLAT CONTROL VALVE REPLACED. OP CHECKED NORMAL.

Part: LINE — CRACKED (FUEL SYSTEM) · airframe 37,354 hrs · 10,391 cycles

SVA - OPEN LINE FROM FUEL CONTROL TO BIFURCATION PLATE IS LEAKING FUEL FROM B-NUT AT FUEL CONTROL. SUSPECT LINE CRACKED AT FLAIR. FATIGUE CRACK IN FUEL LINE. REPLACED FUEL LINE, LEAK CHECKS GOOD.

Part: IDG — LACK OF LUBE · airframe 37,340 hrs · 10,386 cycles

FAILED ENGINE GENERATOR. RTFL. IDG SHUTDOWN DUE TO LOW OIL. SERVICED IDG, NO REPEATS ON SUBSEQUENT FLIGHTS.

Part: OXYGEN MASK — NO TEST (CAPTAIN'S) · airframe 37,314 hrs · 10,379 cycles

CAPTAIN'S O2 MASK COMM WILL NOT TEST. *S/D* SHORT IN O2 MASK ASSY. REPLACED CAPT O2 MASK ASSY. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (APU ECU) · airframe 37,329 hrs · 10,382 cycles

APU AUTO SHUTDOWN TWO STARTS. *S/D* APU ECU FAILED. REPLACED ECU, STARTS SUCCESSFULLY.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 37,152 hrs · 10,334 cycles

THE L GEN DRIVE LT ILLUMINATED AT APPLICATION OF TAKEOFF THRUST. PROBLEM IDG (CHRONIC) UNIT WAS INSTALLED ON A/C ON 6/17/08, FAILED AGAIN ON 6/25. LAST SHOP VISIT WAS NFF, BUT REPLACED LOG, C/P SWITCH, AND INPUT SEAL AND FILTER. IDG REMOVED AND TAGGED AND SENT TO SHOP FOR T/S AND REBUILD. NEW IDG INSTALLED.

Part: HEAT EXCHANGER — DAMAGED (ENGINE) · airframe 37,057 hrs · 10,307 cycles

SERVICED IDG WITH 46 PUMPS OF OIL CONSUMPTION IN 9 HOURS. FUEL/OIL HEAT EXCHANGER BREAKING DOWN CAUSING AN OIL STARVE IN THE IDG. REPLACED IDG.

Part: TRANSMITTER — OUT OF ADJUST (L/E SLAT) · airframe 37,020 hrs · 10,297 cycles

FLAP SLAT ELEC MESSAGE ON TAXI OUT. OUT OF ADJUSTMENT (TRANSMITTER). ADJUSTED RIGHT L/E SLAT POSITION TRANSMITTER - REPLACED LEFT L/E SLAT POSITION TRANSMITTER PER MM 27-88-01-401. ADJUSTED RIGHT L/E SLAT POSITION TRANSMITTER - ELECTRICAL ANGLE FOR FLAP LEVER UP ADJUSTED TO 8.71 BOTH L AND R TRANSMITTERS.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 36,848 hrs · 10,247 cycles

DOOR 1R WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, STOWED LANYARD AND DOOR ARMS/DISARMS NORMALLY.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL SYS) · airframe 36,839 hrs · 10,244 cycles

LOST GALLEY LOAD SHED ON CLIMBOUT. RELATED TO SDR 2008UALA02620. THIS ISSUE WAS VERY DIFFICULT TO DIAGNOSE AND REQUIRED THREE WEEKS OF CONSTANT TROUBLESHOOTING. AFTER ALL WIRES WERE HAND OVER HAND CHECKED AND FOUND NORMAL, K1 AND K2 RELAYS WERE CHANGED, BUSS TIE BREAKERS WERE ALSO CHANGED - IT WAS FOUND THAT CHANGING THE ELCU WAS THE FINAL FIX.

Part: CONTROL UNIT — FAILED (GALLEY POWER) · airframe 36,796 hrs · 10,232 cycles

LOST AFT GALLEY POWER ON CLIMB-OUT. THIS ISSUE WAS VERY DIFFICULT TO DIAGNOSE AND REQUIRED THREE WEEKS OF CONSTANT TROUBLESHOOTING. AFTER ALL WIRES WERE HAND OVER HAND CHECKED AND FOUND NORMAL, K1 AND K2 RELAYS WERE CHANGED, BUSS TIE BREAKERS WERE ALSO CHANGED- IT WAS FOUND THAT CHANGING THE ELCU WAS THE FINAL FIX.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 36,646 hrs · 10,192 cycles

OXYGEN PRESSURE DECREASING. EICAS STATUS PARAMETERS DISPLAYED, OXY PRESS. CREW COMMENTS, AT TAKEOFF PRESS 1690, AT LDG 1530. RECONNECTED BOTH CREW OXYG EN MASKS AND LEAKED CHECKED GOOD.RESERVICED CREW OXYGEN PER AMM LEAKED CHECKED ALL FITTINGS AT CREW OXYGEN BOTTLE AND R EGULATOR AREA AND NO LEAKS FOUND.EICAS READING AND BOTTLE PRESSU RE ONLY 40 PSI DIFFERENCE.GOOD FOR SERVICE.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 36,576 hrs · 10,174 cycles

CREW OXYGEN LOW. SERVICED CREW OXYGEN TO 1500PSI, NO LEAKS WERE NOTED AT TIME OF SERVICE.

Part: BOTTLE — LOW (CREW OXYGEN) · airframe 36,538 hrs · 10,163 cycles

CREW OXYGEN LOW, INDICATES 1100. SERVICED CREW O2, NO LEAKS WERE NOTED AT TIME OF SERVICE.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 36,532 hrs · 10,161 cycles

1R WILL NOT ARM. FOUND SLIDE LANYARD INTERFERENCE. SECURED LOOSE RAFT LANYARD, DOOR ARMS/DISARMS NORMALLY.

Part: OXYGEN MASK — SHORTED (COCKPIT) · airframe 36,443 hrs · 10,134 cycles

CAPT O2 MASK MIC INOP. FOUND SHORT INSIDE MIC. REPLACED MASK AND STOWAGE BOX ASSY.

Part: FILTER — CLOGGED (EQUIPMENT COOL) · airframe 36,412 hrs · 10,127 cycles

EQUIPMENT COOLING HORN AT DEPARTURE. FOUND EQ COOLING FAN FILTER CLOGGED. REPLACED FILTER, OPS CHECKED GOOD.

Part: SWITCH — DIRTY (APU) · airframe 36,314 hrs · 10,101 cycles

APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. CLEANED LOW PRESSURE SWITCH, CHECKED OIL LEVEL, OK, APU STARTED 1ST ATTEMPT, NO REPEAT ISSUES.

Part: LANYARD — OUT OF POSITION (LIFE RAFT) · airframe 36,305 hrs · 10,098 cycles

DOOR 1R WILL NOT ARM. INTERFERENCE FROM RAFT LANYARD. CLEARED AND STOWED PROPERLY, DOOR ARMS/DISARMS PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,275 hrs · 10,091 cycles

AFT RIGHT HAND OVERWING EMERGENCY EXIT INSIDE AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,275 hrs · 10,091 cycles

NR 2 LEFT MAIN ENTRY DOOR OUTSIDE EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: ASPIRATOR — DAMAGED (ESCAPE SLIDE)

FLAPPER VALVES ON ASPIRATOR LEAKING. FOUND SLIDE WAS DEPLOYED AND COULD BE THE CAUSE OF DAMAGED ASPIRATOR. REPLACED ASPIRATOR, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,895 hrs · 9,982 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOP AND LENS CRACKED RIGHT AFT OVERWING EMERGENCY LIGHT INOP ALSO. REPLACED BOTH BULBS AND REPLACED LIGHT ASSY.

Part: TRANSMITTER — OUT OF LIMITS (TE FLAP) · airframe 34,505 hrs · 9,589 cycles

RIGHT FLAP POSITION TRANSMITTER ACCURACY OUT OF RANGE CAUSING FLAP-SLAT ELEC STATUS.

Part: SLIDE — SEPARATED (L1 DOOR) · airframe 33,838 hrs · 9,405 cycles

FOUND DOOR 1L SLIDE APRON SEPARATED FROM SLIDE LOWER ATTACH POINT. PINNED SLIDE AND DOOR ASSIST BOTTLE. REMOVED SLIDE ASSEMBLY IN TO GALLEY AREA FOR REPLACEMENT. REPLACED DOOR 1L SLIDE AND SLIDE ATTACHMENT HARNESS.

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 33,804 hrs · 9,398 cycles

DOOR 1R WILL NOT ARM. CYCLED DOOR. REMOVED FOREIGN MATERIAL FROM DOORWAY.

Part: ENGINE — DAMAGED (NR 2) · airframe 32,824 hrs · 9,114 cycles

RTFL DUE TO BIRDSTRIKE TO NR 2 ENGINE. NR 2 ENG, WHILE PERFORMING FIM MULTIPLE METAL PIECES FOUND IN THE 10TH STAGE BLEED DUCT AND IN THE PRE COOLER.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 31,871 hrs · 8,826 cycles

LOSS OF NR 2 ENGINE INDICATION, ENGINE SHUT DOWN. NR 2 ENG FLAMED OUT,30 MINUTES OUT OF HNL. ALL INDICATIONS WENT TO ZERO. NO N2 INDICATION. ENGINE WIND MILLED FOR 30 MINUTES WITH NO OIL PRESSURE INDICATED. FOUND EEC ROTOR DISINTEGRATED. REPLACED EEC ROTOR AND STATOR.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 29,520 hrs · 8,157 cycles

LEFT MAIN FUEL TANK TRANSFERRED INTO CENTER TANK. SUPPLEMENTAL DATA UPDATE WITH 10,000 LBS IN THE WING TANKS W-CTR TANK PUMPS OFF, ABOUT 600 LBS TRANSFERED L WING TO CNTR TANK, PUMPS WERE OFF FOR AT LEAST AN HOUR. WING TANKS ABOUT 10K WHEN TRANSFER OCCURRED. DURING PRESSURE CK FOUND THREE WAY COUPLING ASSY LEAKING AT THE RATE OF 200 LB PER HR. LOCATED NEXT TO LT DEFUEL VLV HOUSING BODY FEED LINE. REPLACED FUEL FEED PUMP. REPLACED 3 O-RING PACKING OF FUEL LINE COUPLING AND CHECKED FOR UNWANTED FUEL TRANSFER; OPS CHECK GOOD.

Part: O-RING — LEAKING (DOOR SLIDE) · airframe 28,114 hrs · 7,770 cycles

LOW BOTTLE PRESSURE FILLER VALVE O-RING WAS LEAKING. REPLACED O-RING.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,191 hrs · 6,341 cycles

AFT PIT AT STA 1540 FRAME INBOARD FLANGE IS DENTED AT STR 25R. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,191 hrs · 6,341 cycles

AFT PIT FUSELAGE FRAME INNER FLANGE IS DENTED AT BS 1400, STR 25L. *S/D* DAMAGE DUE TO TYPICAL CARGO LOADING IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,191 hrs · 6,341 cycles

AFT PIT FUSELAGE FRAME INNER FLANGE IS DENTED AT BS 1440, STR 25L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH A NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (AFT PIT STA) · airframe 23,191 hrs · 6,341 cycles

AFT PIT STA 1580 FRAME IS DENTED ON INBOARD FLANGE AT STR 25. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,637 hrs · 5,368 cycles

DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECK OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,191 hrs · 6,341 cycles

LT EXT FUSELAGE SKIN AT BS 620 AND STR 16L IS DENTED. INSTALLED PARTIAL SKIN REPLACEMENT USING DOUBLERS AND TRIPLERS.

Part: LIGHT — DETERIORATED (CABIN) · airframe 23,191 hrs · 6,341 cycles

EMERGENCY EQUIPMENT LIGHT (EEL) STRIPS DETERIORATED THROUGHOUT THE CABIN. REPLACED EEL LIGHT STRIPS.

Part: INDICATOR — FAULTY (COCKPIT)

ABORTED TAKEOFF AT 100KTS DUE TO A CAPT AIRSPEED INDICATOR PROBLEM. THE CAPTAIN'S AIRSPEED INDICATOR WAS REPLACED.

Part: IDG — INOPERATIVE (LT GENERATOR) · airframe 19,216 hrs · 5,256 cycles

ABORTED TAKEOFF DUE TO LT IDG LIGHT. LEFT INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED THE LEFT IDG. NORMAL WEAR, REPLACED THE PUMP AND MOTOR ASSEMBLY.

Part: SENSOR — CONTAMINATED (APU) · airframe 5,182 hrs · 1,506 cycles

AIRCRAFT DIVERTED TO LAX DUE TO THE INABILITY TO START THE APU. *S/D* DUE TO THE CHRONIC NATURE OF REPEATED NO ALTITUDE STARTS, THE APU WAS REPLACED MAY 14, 2000. APU SHOP ACCOMPLISHED A PRELIMINARY BASE CHECK. THE ORIFICE FOR THE COMPRESSOR INLET PRESSURE SENSOR (P2) HAD SOME DEBRIS AND WAS CLEANED AND THE P2 SENSOR WAS REPLACED. APU HAD A DIAGNOSTIC TEST IN THE TEST CELL AND PASSED ALL TESTS WITH GOOD PERFORMANCE. NO OTHER CAUSE WAS FOUND, THE APU WAS RELEASED AND IS BACK IN SERVICE AND INSTALLED ON ACFT 5461 WITH NO FURTHER INCIDENTS.