N379DA

Part: ACTUATOR — INOPERATIVE (ZONE 300) · airframe 78,780 hrs · 31,792 cycles

SHIP 3709 -MISC/DE- DECLARED EMERGENCY INTO SLC DUE TO STAB OUT OF TRIM LIGHT AND STAB TRIM ELECTRICALLY INOPERABLE. CORRECTIVE ACTION: REPLACED STABILIZER TRIM MOTOR. OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 78,676 hrs · 31,745 cycles

(LOG 7511337) ON SVC CHECK FOUND EMERGENCY LIGHTS ON LH SIDE NEAR EMERGENCY OVER WING EXIT OUT. REMOVED AND REPLACED BATTERY PACK OVER WING LH EXIT IN POSITION M1694. OPS CHECK GOOD EMERGENCY LIGHTS OPERATE NORMAL. DONE IAW B737 AMM 33-51.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 76,757 hrs · 30,897 cycles

(LOG 6350880) EMERGENCY OVERHEAD AREA LIGHT ROW 13 F.E.D INOP. R/R EMERGENCY OVERHEAD LIGHT ASSY. PER B737 AMM 33-51. OPS CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 74,559 hrs · 29,953 cycles

(LOG 5304716) ON SVC FOUND MID AFT CEILING EXIT SIGN BROKEN. R/R MID AFT EXIT SIGN IAW B737 AMM 33-51. OPS CHK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,009 hrs · 29,698 cycles

(LOG 4310456) RIGHT REAR SLIDE/ OVERWING LIGHT INOP. R/R RIGHT REAR SLIDE/ OVERWING LAMP IAW B37 AMM 33-51. OPS CHK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,687 hrs · 29,560 cycles

(LOG 4587612) DURING SERVICE CHECK FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. AT 28D. R/R EMERGENCY LIGHTING WIRING HARNESS PER B737 AMM 33-51. OPS CKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,519 hrs · 28,987 cycles

(LOG 2768240) DURING MAINTENANCE OF THE A/C B737-800 SHIP NUMBER 3709 ON MXA MRO AT MEX, WHILE PERFORMING WORK CARD 2020-9002  CHECK - AIRCRAFT EXTERNAL DAMAGE IDENTIFICATION (ADF FILE) AND DENT RE-EVALUATION A CREASE WAS FOUND ON FUSELAGE SKIN AT BS 380 AND BETWEEN STR 16 / 17 LH. MAINTENANCE REPAIRED DAMAGE PER ERA 608674-14.

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 72,519 hrs · 28,987 cycles

(LOG 2758049) DURING INSPECTION FOUND PASSENGER COMPARTMENT FLOOR STRUCTURE, STA 947.5 IN THE MIDDLE OF THE BEAM UPPER SURFACE WITH CORROSION. PASSENGER COMPARTMENT FLOOR SRTUCTURE, STA. 947.5 IN THE MIDDLE OF THE BEAM UPPER SURFACE WAS REPAIRED I.A.W B737-800 SRM 53-70-51-2R-5.

Part: ACTUATOR — LEAKING (X) · airframe 71,662 hrs · 28,597 cycles

SHIP 3709 -DIV/GEAR- DIVERTED TO ATL DUE TO NOSE LANDING GEAR INDICATION AFTER TAKE OFF. CORRECTIVE ACTION: NLG RETRACT ACTUATOR LEAKING FROM FORWARD SEAL. REPLACED SAME. FOUND NLG DOWN SENSOR SS853 INTERMITTENT. REPLACED SAME. OPS CHECKS GOOD.

Part: CONNECTOR — DAMAGED (HYD PUMP) · airframe 71,550 hrs · 28,534 cycles

ON DESCENT LT ELEC HYD PUMP OVERHEAT. THERE WAS AN ACCOMPANYING BURNT ODOR BRIEFLY JUST BEFORE ELEC PUMP WAS TURNED OFF PER QRH. FOUND CONNECTOR AT PUMP CONTAMINATED. R/R CONNECTOR D2664 FOR SYS A ELEC HYD PUMP PER B737 WDM 29-11-12 (503183) R/R BOTH RECIRCULATION FILTERS IAW B-737 AMM 21-25 AND INSTALLED NEW EMDP PER B737 AMM 29-11-21.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,530 hrs · 28,523 cycles

(LOG 9346428) DURING INSPECTION FOUND FWD GALLEY, F/C & AFT CABIN EMERGENCY LIGHT DID NOT PASS TEST. T/S PER B737 AMM 33-51. R/R FWD GALLEY BATTERY PACK AND RIGHT AFT EMERGENCY BATTERY PACK PER B737 AMM 33-51. OPS CKS NML.

Part: LINE — LEAKING · airframe 70,358 hrs · 27,934 cycles

SHIP 3709 -HYD/DE- DUE TO A SYSTEM HYDRAULIC LEAK. CORRECTIVE ACTION: FOUND LEFT MLG RETRACT ACTUATOR SUPPLY LINE LEAKING. INSTALLED TEMPORARY FLEX LINE PER AMM. OPS & LEAK CHECK OK.

Part: FUSE — INOPERATIVE · airframe 69,816 hrs · 27,629 cycles

SHIP 3709 - MISC/DE- DUE TO LEADING EDGE IN TRANSIT LIGHT ILLUMINATED ON APPROACH. CORRECTIVE ACTION: REPLACED LE 'B' SYSTEM RETRACT HYDRAULIC FUSE. OPS CHECKS GOOD.

Part: NONE — NONE · corrosion level 2 · airframe 68,628 hrs · 27,151 cycles

(LOG 1975286) DURING INSPECTION FOUND CORROSION AT LAV VENT NOZZLE ASSY. GAINED ACCESS AND REMOVED AND REPAIRED DAMAGE PER B737 SRM 53-70-01-02R PROCEDURE 3, REP 3, 4 A-D. (889397) C/W B737-800 SRM 53-70-01-2R PROCEDURE 3, REPAIR 3.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 67,181 hrs · 26,556 cycles

(LOG 1767957) DURING INSPECTION FOUND EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. INSTALLED EXIT LIGHT COVER. OK FOR SVC. REF B737 AMM 33-51.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 67,071 hrs · 26,511 cycles

(LOG 7515565) DURING INSPECTION FOUND SEAT 4DC EMERGENCY AISLE ILLUMINATION INOP. RECONNECTED AISLE LIGHTING UNDERNEATH SEAT IAW B737 AMM 33-51. OPS CHECK GOOD.

Part: LANDING — CRACKED (GRND PWR DOOR) · airframe 66,554 hrs · 26,290 cycles

DURING CCK AT QRO, WHILE PERFORMING BASE ZONAL INSPECTIONS PER WC 5330-2517, A CRACK WAS REPORTED AFFECTING THE GROUND POWER ACCESS LAND EGPR DOUBLER, BETWEEN STA 219.80 TO 235.80 & S-21R TO S-24R. MAINTENANCE REPAIRED DAMAGE, PER ERA 589204-14.

Part: BULKHEAD WEB — CRACKED · airframe 66,554 hrs · 26,290 cycles

DURING INSPECTION FOUND CRACKS (2 EA) ON VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LT WHEEL WELL. VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LT WHEEL WELL WAS REPAIRED, PER 737-800 SRM 57-10-10-2R-2 PROCEDURE 2.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,404 hrs · 26,224 cycles

(LOG 6960526) WITH SWITCH IN ARMED POSITION, EMER LIGHTS FROM ROW 13 FWD REMAIN ON. REPLACED BATTERY AT PWR SUPPLY M1674 PER B737 AMM 33-51. EMERGENCY LIGHTS CK OK.

Part: LENS — UNKNOWN (CABIN) · airframe 65,355 hrs · 25,789 cycles

(LOG 1344970) DURING INSPECTION FOUND EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REINSTALLED LIGHT LENSE CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,813 hrs · 25,118 cycles

(LOG 5004387) DURING INSPECTION FOUND F/C SEAT EMERG LIGHTS INOPERATIVE. R/R BATTERY PACK F/C PER AMM 33-50.

Part: NONE — NONE · corrosion level 2 · airframe 72,141 hrs · 28,808 cycles

(LOG 0032235) DURING INSPECTION FOUND CORROSION ON FRAME WEB AT STATION 767 RBL 10. MAINTENANCE REPAIRED DAMAGE PER ERA 558404-14.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE RIGHT HORIZONTAL STAB AT HSS 92.70 RIB, THE FOURTH RIB STIFFENER FROM THE FRONT SPAR IS CRACKED. MAINTENANCE ACCOMPLISHED A RIB STIFFENER REPAIR IAW SRM 55-10-09, REPAIR 4.

Part: FRAME — DENTED (BS 727F) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND A DENT COMMON TO THE FRAME BS 727F, STRINGER 22L, 19R & 24R. MAINTENANCE REPAIRED THE FRAME IAW ERA 557935-14.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FLOOR PANEL 140CF HAS CORROSION UPPER AND LOWER SURFACES AROUND EDGES. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610, REV. K.

Part: FLOOR SUPPORT — CORRODED (BS 727-727F) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT, LBL 20, BS 727-727F+12 CORRODED AT SEVERAL SPOTS. MAINTENANCE REPLACED THE FLOOR SUPPORT SRM 53-00-53, REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (BS 727J-847) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT BS 727J+12 - 847, LBL 20 IS CORRODED. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 5.

Part: STRINGER — CORRODED (BS 360-351) · airframe 57,338 hrs · 22,690 cycles

DURING ROUTINE MAINTENANCE VISIT, CORROSION WAS FOUND COMMON TO STRINGER 27L BETWEEN BS 360 AND 351.2. MAINTENANCE REPAIRED THE STRINGER IAW ERA 558403-14.

Part: SHIELD — CORRODED (BS 767-794) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY DOOR SURROUND, FORWARD SHEILD BS 767 - 794, RBL 21 HAS CORROSION ON THE UPPER AND LOWER SURFACES. MAINTENANCE REPLACED THE SHIELD IAW DWG 146A8127, SRM 51-10-02,.AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 727F-727J) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT BS 727F+12 - 727J+12 CORRODED. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 5.

Part: STRINGER — CORRODED (BS 344-369) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE E & E BAY STRINGER 27L, BS 344 - 369 HAS CORROSION. MAINTENANCE REPAIRED THE STR IAW ER/A 558403-14, REV O, AND PRI 558403-14, REV 1.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE FWD CARGO BAY FLOOR PANEL 120CF CORRODED. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW SRM 53-30-53, & DWG 453A1610, REV T.

Part: SKIN — CORRODED (BS 540) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE LEFT EXTERNAL FUSELAGE SKIN AT BS 540 HAS EVIDENCE OF CORROSION UNDER DRAG ANGLE. MAINTENANCE REPAIRED IAW PRI 558394-14, REV, 2, & ERA 558394-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 727H) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY BS 727H, FRAME INNER FLANGE DENTED BETWEEN STRINGERS 22 AND 23L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557934-14, REV 2, AND ERA 557934-14, REV ORIGINAL.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR PANEL 140BF CORRODED ON THE UPPER AND LOWER SURFACES AROUND EDGES. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW SRM-53-60-53, & DWG 453A2610, REV K.

Part: FRAME — DENTED (BS 727H) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY BS 727H FRAME INNER FLANGE DENTED JUST BELOW STRINGER 23R. MAINTENANCE REPAIRED THE FRAME IAW PRI 557934-14, REV 2, & ERA 557934-14, REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 727G-767) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT, BS 727G+10 - 767, RBL 20 CORRODED. MAINTENANCE REPAIRED THE FRAME.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE RIGHT HORIZONTAL STABILIZER, HSS 92.70, RIB CRACKED. MAINTENANCE ACCOMPLISHED A RIB REPAIR IAW ER/A 558406-14.

Part: SKIN — CORRODED (BS 727D-727E) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE LOWER FUSELAGE SKIN BS 727D - 727E SKIN CORRODED. MAINTENANCE REPAIRED THE SKIN IAW PRI 558408-14, REV O.

Part: FRAME — DENTED (BS 440) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FRAME BS 440, STRINGER 8R HAS EVIDENCE OF A CRACK. MAINTENANCE REPAIRED THE FRAME IAW PRI 557923-14AD, REV ORIGINAL, AND ER/A 557923-14AD, REV ORIGINAL.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE RIGHT HORIZONTAL STAB HSS 92.70 RIB CRACKED. MAINTENANCE ACCOMPLISHED A RIB REPAIR IAW ER/A 558406-14.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR PANEL 140AF CORRODED ON UPPER AND LOWER SURFACES AROUND EDGES. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610, REV K.

Part: SHIELD — CORRODED (BS 495-500A) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE FWD CARGO BAY, AFT OF DOOR CUTOUT RT SIDE SHIELD FROM BS 495 - 500A, STRINGER 26R HAS MULTIPLE AREAS OF CORROSION AND BROKEN NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE SHIELD IAW DWG 143A8126, REV A, AND SRM 51-40-02.

Part: DOUBLER — CORRODED (BS 747-767) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY BILGE BETWEEN BS 747 AND 767, STRINGER 27L TO 27R EXISTING INTERNAL ANTENNA DOUBLER HAS CORROSION. MAINTENANCE INSTALLED A NEW DOUBLER AND COVER PLATE IAW SRM 51-10-02, SRM 51-40-02, AND AMM 51-21.

Part: FRAME — DENTED (BS 727H) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 727H, STRINGER 24L, FRAME INNER FREE FLANGE IS DENTED. MAINTENANCE REPAIRED THE FRAME IAW PRI 557934-14, REV 2, & ERA 557934-14, REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 294.5-312) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FLOOR SUPPORT BS 294.5 - 312, LBL 10, CORRODED. MAINTENANCE REMOVED & REPLACED THE FLOOR SUPPORT IAW ERA 558402-14, REV 1.

Part: ANGLE — CORRODED (BS 500B-500D) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE FWD CARGO BAY, LT SIDE ZEE ANGLE FROM BS 500B - 500D, STRINGER 26L HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPLACED THE ANGLE.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE FWD CARGO BAY FLOOR PANEL 120AF HAS EVIDENCE OF CORROSION. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW 453A1610, REV C.

Part: FRAME — DENTED (BS 500C) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FORWARD CARGO BAY FRAME BS 500C, STRINGER 25L FREE FLANGE DENTED. MAINTENANCE REPAIRED THE FRAME IAW PRI/ERA 557939-14, REV 0, & SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND FWD CARGO BAY FLOOR PANEL 120DF CORRODED. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610, REV B.

Part: ANGLE — CORRODED (BS 500D-500F) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND FORWARD CARGO BAY BS 500D - 500F, LBL 23 ZEE ANGLE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW SRM 53-00-53, REPAIR 6.

Part: FLOOR SUPPORT — CORRODED (BS 727-727G) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT IS CORRODED, BS 727 - 727G+10, RBL 20. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW DWG 146A7500, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FLOOR SUPPORT BS 727I+6, RBL 13 CORRODED. MAINTENANCE REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 3, AND ER/A 492962-14MA.

Part: FRAME — DENTED (BS 827) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FRAME BS 827, STRINGER 25L FLANGE DENTED. MAINTENANCE REPAIRED THE FRAME IAW ER/A 557929-14, REV O, & PRI 557929-14, REV O.

Part: STRINGER — CORRODED (BS 363-366) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE LOBE, E & E BAY, JUST AFT OF ACCESS DOOR, BS 363 - 366, STRINGER 28R HAS CORROSION ON OTBD SIDE AT STRINGER SPLICE. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-00-03, REP 1, & DWG 143A3241, REV D.

Part: FRAME — DENTED (BS 727G) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 727G, FRAME INNER FLANGE IS DENTED BETWEEN STRINGERS 24 AND 25L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557928-14, REV 3, AND ERA 557928-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 727G) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 727G FRAME INNER FLANGE IS DENTED AT STRINGER 24R. MAINTENANCE REPAIRED THE FRAME IAW PRI 557928-14, REV 3, AND ERA 557928-14.

Part: FRAME — DENTED (BS 727G) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY BS 727G FRAME INNER FLANGE IS DENTED BETWEEN STRINGERS 20 AND 21L. MAINTENANCE REPAIRED THE FRAME IAW PRI 5579285-14, REV 3, AND ERA 557928-14.

Part: FRAME — DENTED (BS 827) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FRAME BS 827, STRINGER 22L DENTED. MAINTENANCE REPAIRED THE FRAME IAW ERA 557929-14, REV 0, AND PRI 557929-14, REV 0.

Part: FRAME — DENTED (BS 747) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY LT SIDE FRAME, BS 747 INNER FLANGE IS DENTED IN 2 PLACES BETWEEN STRINGERS 23, AND 24L. MAINTENANCE REPAIRED THE FRAME IAW PRI ER/A 557925-14, REV 1, AND ERA 557925-14, REV ORIGINAL.

Part: BRACKET — CORRODED (BS 380) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE E&E BAY GROUND BRACKET, BS 380, STRINGER 23L CORRODED. MAINTENANCE INSTALLED A NEW GROUND BRACKET.

Part: FRAME — DENTED (BS 727E) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO CAY FUSELAGE FRAME BS 727E, STRINGER 25L, FRAME INNER FLANGE HAS A DENT. MAINTENANCE REPAIRED THE FRAME IAW ERA 557933-14, REV ORIGINAL, AND PRI 557933-14, REV 1.

Part: STRINGER — CORRODED (BS 380) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE E&E BAY BS 380, STRINGER 23L IS CORRODED. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-00-03, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 888) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT, BS 888, RBL 12 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53.

Part: STRINGER — CORRODED (BS 351-380) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE E & E BAY BILGE AREA AFT OF ACCESS DOOR, STRINGER 28L AND SPLICE FROM BS 351 - 380 HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-00-03, REP 1.

Part: FRAME — CRACKED (BS 295.5) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND FORWARD CABIN AT R1 DOOR CUTOUT FWD FRAME BS 295.5 LOWER FASTENER HOLE COMMON TO INNER CREASE BEAM IS CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 558398-14, REV 0, AND ERA 558398-14, REV ORIGINAL.

Part: STRINGER CLIP — CORRODED (BS 360) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE LOBE, E&E BAY STRINGER CLIP AT 27L, BS 360 IS CORRODED. MAINTENANCE FABRICATED A NEW STRINGER CLIP IAW DWG 143A1010, REV A, AND INSTALLED ON W/C 5453665 CONTINUATION 5403049 ITEM 4.

Part: FRAME — DENTED (BS 727J) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY, BS 727J FUSELAGE FRAME IS DENTED ON INNER FLANGE ABOVE STRINGER 22R. MAINTENANCE REPAIRED FRAME IAW PRI 557930-14 REV 1, AND ERA 557930-14.

Part: FRAME — DENTED (BS 727B) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY LT SIDE FUSELAGE FRAME INNER FLANGE IS DENTED AT BS 727B, BETWEEN STRINGERS 24L AND 25L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557938-14, REV 1, AND ERA 557938-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 727E) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FRAME, BS 727E, STRINGER 22L INNER FLANGE HAS A DENT. MAINTENANCE REPAIRED THE FRAME IAW PRI 557933-14, REV 1, AND ER/A 557933-14.

Part: FRAME — DENTED (BS 727C) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY, FRAME INNER FLANGE IS DENTED IN TWO PLACES, BS 727C BETWEEN STRINGER 24 AND 25L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557936-14 REV O, SRM 51-40-02, AND ERA 557936-14.

Part: INTERCOSTAL — CORRODED (BS 351-360) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE LOBE, E & E BAY BILGE AREA AFT OF THE ACCESS DOOR, INTERCOSTAL AT STRINGER 28L FROM BS 351 - 360 IS CORRODED. MAINTENANCE INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02, AND DWG 141A8511, REV C.

Part: CARGO TRACK — CORRODED (BS 727-727A) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY CARGO TRACK, BS 727 - 727A, RBL 13 CORRODED. MAINTENANCE REMOVED AND REPLACED AFT CARGO TRACK IAW SRM 53-00-53, REPAIR 4.

Part: INTERCOSTAL — CORRODED (BS 360-380) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND INTERCOSTAL BETWEEN BS 360 - 380, JUST ABOVE STRINGER 27L IS CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02, DWGS 143A9173, REV E, AND 143A7902, REV A.

Part: STRINGER — CORRODED (BS 368-372) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE LOWER FUSELAGE E & E BAY STRINGER 27L FROM BS 368 - 372 IS CORRODED. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-00-03, REPAIR 1, DWGS 143A3241, REV E, AND 1411A3341, REV A.

Part: FRAME — DENTED (BS 827) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY FRAME, BS 827, STRINGER 23L DENTED. MAINTENANCE REPAIRED THE FRAME IAW SRM 51-40-02-0G, ER/A 557929-14, REV O, AND PRI 557929-14, REV O.

Part: FRAME — DENTED (BS 727J) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY, LT SIDE BS 727J, FRAME DENTED AT STRINGERS 22L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557930-14, REV 1, AND ERA 557930-14.

Part: FRAME — DENTED (BS 747) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY LT SIDE FRAME BS 747 INNER FLANGE IS DENTED ABOVE STRINGER 22L. MAINTENANCE REPAIRED THE FRAME IAW PRI ERA 557925-14, REV 1, AND ERA 557925-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 400) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FRAME AT BS 400, STRINGER 8L HAS EVIDENCE OF A CRACK. MAINTENANCE REPAIRED THE FRAME IAW PRI 557923-14AD, REV ORIGINAL, AND ERA 557923-14AD.

Part: FRAME — CRACKED (BS 727B) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND CABIN FRAME AT BS 727B CRACKED NEAR STRINGER 8R AT FIRST FASTENER HOLDING PSU RAIL SUPPORT. MAINTENANCE REPAIRED THE FRAME IAW PPRI 557923-14AD, REV ORIGINAL, AND ERA 557923-14AD.

Part: FRAME — CRACKED (BS 500A) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FRAME AT BS 500A, STRINGER 8 HAS EVIDENCE OF A CRACK. MAINTENANCE REPAIRED IAW 14AD REV ORIGINAL AND ERA 557923-14AD.

Part: FRAME — CRACKED (BS 380) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FRAME AT BS 380, STRINGER 8L CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 557923-14AD, REV ORIGINAL, AND ER/A 557923-14AD.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE RIGHT HORIZONTAL STABILIZER AT HSS 92.70 RIB, THE FIRST RIB STIFFENER FROM THE FRONT SPAR, CRACKED. MAINTENANCE ACCOMPLISHED A RIB STIFFENER REPAIR IAW ERA 558406-14.

Part: FRAME — CRACKED (BS 727B) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND CABIN FRAME AT BS 727B CRACKED NEAR STRINGER 8L. MAINTENANCE REPAIRED THE FRAME IAW PRI 557923-14AD.

Part: CREASE BEAM — CORRODED (BS 328) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN AT R1 DOOR, FORWARD OF BS 328, CREASE BEAM CORRODED AROUND FASTENER HOLES. MAINTENANCE REPLACED THE CREASE BEAM IAW SRM 51-40-02, AND DWG 141A8310 REV 0.

Part: FRAME — CRACKED (BS 400) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE PASSENGER CABIN FRAME BS 400, STRINGER 8R CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 557923-14AD.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE AFT CARGO BS BS 747 - 767, RBL 21 FLOOR SUPPORT UNDER ZEE ANGLE HAS CORROSION ON LOWER SURFACE. MAINTENANCE REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G, PAGE 2, PARA 4. & DWG 146A7505, REV B.

Part: FRAME — DENTED (BS 807) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FRAME BS 807 INNER FLANGE DENTED TWO INCHES ABOVE STRINGER 22L. MAINTENANCE REPAIRED THE FRAME IAW PRI/ERA 557924-14, REV O.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE LT HORIZONTAL STABILIZER HSS 92.7 RIB IS CRACKED AT SECOND FROM AFT VERTICAL STIFFENER. MAINTENANCE REPAIRED THE RIB IAW SRM 55-10-09, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 500F-520) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN LEFT OTBD SEAT TRACK CROWN FROM BS 500F - 520 HAS MULTIPLE GOUGES. MAINTENANCE REPAIRED THE SEAT TRACK IAW IAW SRM 53-00-52, REPAIR 4.

Part: RETAINER — CRACKED (RT WING SEAL) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE RIGHT WING MIDSPAN FIXED TRAILING EDGE MIDSPAN BULKHEAD AFT CURVED SEAL RETAINER CRACKED. MAINTENANCE REPLACED THE SEAL RETAINER IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND LT HORIZONTAL STABILIZER HSS 92.7 RIB IS CRACKED AT FOURTH FROM AFT VERTICAL STIFFENER. MAINTENANCE REPAIRED THE RIB STIFFENER IAW SRM 55-10-09, REPAIR 4.

Part: FRAME — CRACKED (BS 480) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND CABIN FRAME AT BS 480 CRACKED NEAR STRINGER 8L AT FASTENER HOLE. MAINTENANCE REPAIRED IAW ER/A 557923-14AD.

Part: FRAME — CRACKED (BS 440) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FRAM AT BS 440, STRINGER 8L HAS EVIDENCE OF A CRACK. MAINTENANCE REPAIRED IAW ERA 14-557922.

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND THE CREASE BEAM BS 947 - 986.5 CORRODED. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR CREASE BEAM DWG 147A5700, REV -, 147A0004 REV- , AND 147A8501.

Part: CREASE BEAM — CORRODED (BS 967-993) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, CREASE BEAM AT THE R2 DOOR, BS 967 - 993 HAS CORROSION. REMOVED AND REPLACED THE CREASE BEAM IAW SRM 51-40-02, AND DWG 147A8501.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION FOUND AFT CARGO BAY FLOOR SUPPORT BS 727I+6, RBL3 CORRODED. REPAIRED IAW SRM 53-00-53 FIG 201.

Part: WEB — CRACKED (BS 663) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND CABIN VERTICAL WEB CRACKED AT BS 663, LBL 42. MAINTENANCE REPAIRED THE VERTICAL WEB IAW SRM 57-10-10, REPAIR 3.

Part: SHIELD — CORRODED (CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND FWD CARGO BAY FWD OF CARGO DOOR CUT-OUT RT SIDE SHIELD AT BS 440, STRINGER 26R HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE SHIELD BS 420 - 440 IAW SRM 51-10-02, 53,-30-15, 51-40-02, AND 51-40-05.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT BS 727I+6, RBL 8, CORRODED AT NUTPLATES. MAINTENANCE INSTALLED A NEW REPAIR IAW SRM 53-00-53, REPAIR 2 AND ERA 492969-14MA REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION FOUND AFT CABIN FLOOR WET AREA, FLOORBEAM UPPER TEE HAS CORROSION AT PREVIOUS REPAIR, BS 986.5, LBL 43. CUT OUT CORROSION ON FWD TEE IAW ERA 464736-14MA.

Part: SEAT TRACK — GOUGED (BS 727A-727C) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, LT INBD SEAT TRACK, CENTER OF TRACK GOUGED BS 727A - 727C. MAINTENANCE REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN FLOOR SUPPORT BS 328 - 344, LBL 12, CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 141A5400.

Part: SEAT TRACK — GOUGED (BS 727-727A) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, BS 727+18-727A+9, RBL 45, BOTTOM SURFACE OF SEAT TRACK HAVE MULTIPLE GOUGES. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-R3.

Part: SHEAR WEB — CORRODED (BS 987) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR WET AREA, BS 987, RBL 43, SHEAR WEB UPPER SURFACE HAS CORROSION. MAINTENANCE REMOVED & REPLACED THE SHEAR WEB IAW SRM 51-40-02 AND DWG 147A5700.

Part: STRAP — CORRODED (FUSELAGE) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION FOUND PASSENGER CABIN FLOOR STRUCTURE AT STATION 1022, LBL 18, TOP STRAP HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED STRAP IAW SRM 51-40-02 & DWG 147A5700.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION FOUND AFT CARGO PIT FLOOR PANEL 140DF HAS CORROSION UPPER SURFACE AROUND EDGES. MAINTENANCE FABRICATED NEW AFT CARGO PIT FLOOR PANEL 140DF IAW DWG 453A2610 REV K & REV A.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION FOUND PASSENGER CABIN FLOOR STRUCTURE STATION 277 LBL 45 FWD LAV DUMP TUBE BRACKET IS CORRODED. MAINTENANCE REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT BRACKET AT LBL 45 AT FWD LAV DUMP TUBE AT FS 277 IAW DRAWING 417A8761 REV M AND SRM 51-40-02.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN AREA ABOVE MLG WHEEL WILL BS 663 VERTICAL WEB IS CRACKED RBL 35 WL 199. MAINTENANCE PERFORMED A REPAIR IAW SRM 57-10-10, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 57,338 hrs · 22,690 cycles

DURING INSPECTION, FOUND PASSENGER CABIN AREA ABOVE MLG WHEEL WILL BS 663 VERTICAL WEB IS CRACKED RBL 35 WL 199. MAINTENANCE PERFORMED REPAIR IAW SRM 57-10-10, REPAIR 3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,343 hrs · 21,669 cycles

DURING INSPECTION FOUND EXIT SIGN LIGHT, SLIDE LIGHT, OVERDOOR EXIT SIGN LIGHT AT L2 DOOR INOPERATIVE. MAINTENANCE FOUND BATTERY PACK, M1673, DRAINED. R & R IAW AMM 33-51-06-960-805. OPS TEST SATISFACTORY. ALSO FOUND BATTERY CHARGER NOT WORKING DURING TEST. R & R IAW AMM 33-51-06-960-806. OPS TEST OK.

Part: LIGHT — INOPERATIVE (NOT REPORTED) · airframe 53,298 hrs · 21,323 cycles

DURING INSPECTION FOUND FORWARD MID EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT ASSY IAW AMM 33-51. OPS CK NML.

Part: OVEN — ODOR (GALLEY) · airframe 53,228 hrs · 21,296 cycles

CREW NOTICED A BURNING ODOR IN THE FORWARD CABIN. F/A ALSO REPORTED AN ELECTRICAL BURNING ODOR AND FOOD ON THE FIRST CLASS OVEN ELEMENT. F/A TURNED THE OVEN OFF AND PULLED THE CIRCUIT BREAKER. MAINTENANCE FOUND EVIDENCE OF BURNED FOOD INSIDE OVEN. INSPECTED WIRING AND CONNECTOR PLUG WITH NO DEFECTS NOTED. INSTALLED NEW OVEN OPS CHECKS NORMAL IAW AMM 25-31-88. ACFT RETURNED TO SERVICE.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 50,498 hrs · 20,412 cycles

DURING INSPECTION FOUND PASSENGER CABIN FLOOR RT SIDE BS 520, RBL 24 INBD SEAT TRACK GOUGED ON CROWN UPPER SURFACE. MAINTENANCE BLENDED AREA FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS OF SRM 53-00-52, PG 111. ACCOMPLISHED SEAT TRACK REPAIR IAW SRM 53-00-52, REPAIR 4.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 50,180 hrs · 20,301 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 29 FED. MAINTENANCE REPAIRED 29 FED EMERGENCY LT WIRING IAW SPWM 20-30-12. EMERGENCY LIGHTS CK GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,052 hrs · 20,257 cycles

DURING INSPECTION FOUND L2 DOOR EXT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE R & R L2 DOOR EXT EMERGENCY LIGHT IAW AMM 33-10. OPS CK NORMAL.

Part: GROUNDING STRAP — DAMAGED (EMERGENCY LIGHTS) · airframe 46,394 hrs · 19,004 cycles

DURING INSPECTION, FOUND EXTERIOR EMERGENCY LIGHTING SYS AT R2 SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED GD3810DC GROUND BLOCK. ALL EMERGENCY LIGHTS, OPS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,180 hrs · 18,933 cycles

DURING TEST, FOUND SEVERAL SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE LAMPS, OPS TESTED OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,665 hrs · 18,736 cycles

DURING INSPECTION, FOUND MID EXIT CENTER EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND FAULTY BATTERY PACK & CHARGER ASSY. REPLACED IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 43,750 hrs · 18,029 cycles

NDT INSPECTION DETECTED A CRACK INDICATIONS IN FLOORBEAM FASTENERS HOLES COMMON TO THE SPLICE STRAPS BS 727B LBL 24.75 LBL 45.5 RBL 24.75 AND RBL 45.5 AREA REPAIRED IAW ERA 515108-14, REV ORG ERA 515108-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,633 hrs · 17,616 cycles

DURING INSPECTION, FOUND FORWARD CABIN AND R1 DOOR EMERGENCY EXIT LIGHTS NOT ILLUMINATING. MX R & R BATTERY PACK IN FWD GALLEY CEILING IAW AMM 33-51. LIGHTS OPS CHECK OK.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 37,288 hrs · 15,631 cycles

CABIN BS 480, STR 8R FRAME CRACKED. REPAIRED IAW ERA492961-14 AND INSTALLED DOUBLERS.

Part: LINE — RUPTURED (NR 2 FUEL) · airframe 27,049 hrs · 11,421 cycles

CREW FOUND FUEL IMBALANCE DETERMINED TO BE COMING FROM NR 2 ENG, FOLLOWED QRH PROCEDURE FOR ENGINE FUEL LEAK AND SHUT ENGINE DOWN. FUEL LEAK FOUND TO BE CAUSED BY RUPTURED FLEX LINE COMING FROM IDG OIL COOLER, P/N 340-016-251-0 REF IPC 73-11-00-02 ITEM 245J.

Part: FUEL CONTROL — UNSERVICEABLE (NR 2 ENGINE) · airframe 22,158 hrs · 9,657 cycles

NR 2 ENGINE WILL NOT REACH T/O POWER RTO. INSPECTED NOSE WHEEL AREA FOR DAMAGE, NO DAMAGE/TROUBLE FOUND. REMOVED AND REPLACED FUEL PUMP AND HMU PER AMM. NEEDS LEAK CHECK. RAN TEST PER AMM 73-21-10 AND ACCEL CHECK PER 71-00-, ALL TESTS PASS.

Part: HEAT EXCHANGER — LEAKING (NR 2 ENGINE) · airframe 16,286 hrs · 7,423 cycles

AFTER TAKEOFF RAMP REPORTED TO TMC THAT NR 2 ENG WAS LEAKING FUEL ON TAXI OUT OF SMF. AIRCRAFT DIVERTED INTO SFO FOR MTC. MTC IN PROGRESS. FOUND FUEL/OIL HEAT EXCHANGER LEAKING. REPLACED SAME.

Part: ARM — CRACKED (WINDSHIELD) · airframe 15,966 hrs · 7,311 cycles

CAPTAINS WINDSHIELD WIPER ARM BROKE OFF .25 INCH ABOVE TENSIONING MECHANISM.

Part: FAIRING — MISSING (FUSELAGE) · airframe 14,088 hrs · 6,557 cycles

WING TO BODY FAIRING PANEL 192JL FOUND MISSING ON ARRIVAL. REPLACED PANEL 192JL.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 8,517 hrs · 4,022 cycles

POWER SUPPLY AT STATION 952 LBL 14 HAS BAD OUTPUT FOR THE EMERGENCY AISLES LIGHTS. REPLACED PWR SUPPLY.

Part: SMOKE — DETECTED (COCKPIT) · airframe 6,982 hrs · 3,339 cycles

SMOKE ENTERED COCKPIT WHEN PACKS SELECTED. NO SMOKE NOTED IN CABIN. APU PRESS WEAK IN SLC, JUST ENOUGH TO START ENGINES. SMOKE HAD ODD ODOR (SWEET). DE-ICED IN SLC. OPERATED RT/LT PACKS WITH APU. NO SMOKE OR ODOR NOTED. ALL PACK INDICATIONS CHECK OK.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 6,303 hrs · 3,016 cycles

LOST COMMUNICATIONS. FD OBS MIC SELECT PANEL PTT SW BAD. REPLACED PANEL PER MM.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 3,060 hrs · 1,479 cycles

EMERGENCY FLASHLIGHT AT AFT LT JUMPSEAT RED LED DOES NOT FLASH. REPLACED SAME.