N16642

Part: CONTROL SYSTEM — OUT OF ADJUST (LANDING GEAR) · airframe 33,993 hrs · 17,557 cycles

ON FINAL, AFTER SELECTING LAND GEAR DOWN ALL GREEN LIGHT LIGHTS ILLUMINATED AND ALL RED GEAR LIGHT REMAINED ILLUMINATED. RAN QRH CHECK LIST AND RED GEAR LIGHTS EXTINGUISHED. LANDING WAS NORMAL. GA WAS ACCOMPLISHED TO RUN CHECKLIST. ADJ THE LANDING GEAR CONTROL SYS PER AMM 32-31-00-735-001, OPS CHECK NORMAL. GEAR SWING NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,837 hrs · 17,482 cycles

STA 303 LOWER HINGE CUTOUT BOTTOM FASTENER HOLE HAS CRACK INDICATION ON HFEC PROBE INSP REF EA 5330-03736 STEP 20. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER AT STA 303 L1 DOOR HINGE CUTOUT, REPAIR WAS COMPLIED WITH PER ECRA 5330- 04019, ISSUED DIP FOR FURTHER INSPECTION PER PART 2 OF ECRA 5330-04016. DIP CNTRL NUMBER 05029. BEFORE THE ACCUMULATION OF 72,482 TOTAL A/C FLT CYC, PERFORM AN INSP PER PART 2 OF ECRA. PLANNING TO CONTACT ENGR AFTER THE ACCUMULATION OF 66,000 TOTAL FLT CYC BUT BEFORE 67,000 TOTAL FLT CYC FOR INSP DETAILS.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 33,837 hrs · 17,482 cycles

SUPPORT TASK: (L-1 DOOR REPAIR) CRACK INDICATIONS AT ALL 9 FASTENERS THAT ARE .25 INCH (PRIOR TO STEPPING UP) REF EA.5330-03736. CLEANED AND RE-INSPECTED ALL 9 HOLES NO CRACKS NOTED EXCEPT A CRACKED BRACKET WHICH WAS FABRICATED AND INSTALLED REF GMM 10-900-01, SRM 51-40-02 AND BOEING DRAWING 69-78510 AND 65C34778.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 29,355 hrs · 15,161 cycles

Z-ANGLE AT R2 DOOR HAS CORROSION. REMOVED AND REPLACED R2 Z-ANGLE REF SRM 51-40-02.

Part: FRAME — CRACKED (BS 360 S8-9) · airframe 29,355 hrs · 15,161 cycles

FOUND FRAME CRACK AT THE AIR CONDITION (A/C) BRACKET AT BODY STATION 360 BETWEEN S-8 AND S-9. REPAIRED PER ECRA 5310-04787.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 869 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 869 A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04198.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 727B RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. FABRICATED REPAIR PARTS FOR BODY STATION 727B RIGHT-HAND SIDE FRAME AT A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

INTERCOSTAL CRACKED AT NUT PLATE HOLES FROM BS 328-344 LBL 44. REMOVED AND REPLACED CRACKED INTERCOSTAL FROM BS 328-344 LBL 44 PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,335 hrs · 15,161 cycles

THE Z-ANGLE AT L2 DOOR HAS CORROSION. REMOVED CORRODED Z-ANGLE AT L-2 DOOR, LOCATED AND DRILLED NEW ANGLE PER 51-60-02 AND INSTALLED NEW Z-ANGLE AT L-2 DOOR PER B737 SRM 51-60-02.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

MAIN CABIN FLOORBEAM GOUGED AT STATION 927 AT B-0. REPAIRED DAMAGED FLOORBEAM FORWARD FLANGE AT BODY STATION 927 AT BL 0 PER B737-500 SRM 53-60-51, REPAIR 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 867 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT BODY STATION 867 LEFT-HAND SIDE A/C BRACKET BETWEEN S-8 & S-9 PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 747 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT CRACKED AREA OF BODY STATION 747 LEFT SIDE FRAME BETWEEN S8 AND S9 AND INSTALLED REPAIR PARTS PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 827 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 827 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 440 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 440 AT A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 400 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 400 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 907 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT CRACKED AREA OF BODY STATION 907 LEFT SIDE FRAME BETWEEN S8 AND S9 AND INSTALLED REPAIR PARTS PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 380 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 380 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 907 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 907 A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 787 LEFT-HAND FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 787 LEFT-HAND AT A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,335 hrs · 15,161 cycles

BODY STATION 747 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING A/C BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 747 RIGHT-HAND STRINGER S-8 AND S9 A/C BRACKET PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,335 hrs · 15,161 cycles

BODY STATION 787 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 787 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 400 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8L AND S-9L. REPAIRED CRACKED FRAME AT STATION 400 AT A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,335 hrs · 15,161 cycles

BODY STATION 827 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 827 A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

BODY STATION 440 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 440 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498.

Part: FRAME — GOUGED (FUSELAGE) · airframe 29,335 hrs · 15,161 cycles

E&E ACCESS BAY LEFT-HAND FRAME IS GOUGED. TRIMMED OUT DAMAGE AT E&E ACCESS BAY LEFT-HAND FRAME AND REPAIRED SAME PER SRM 51-70-13 FIG 1.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

VERTICAL STABILIZER PANELS 9504R, 9506R 9508R ARE FRETTING FUSELAGE ATTACH ANGLE, WEAR ON ANGLE AND PANELS. REMOVED DAMAGED ANGLES BEHIND VERTICAL STABILIZER PANELS 9504R, 9506R, 9508R. FABRICATED REPAIR ANGLES AND INSTALLED IAW TYPICAL REPAIR 5380-10113. RESTORED PROTECTIVE FINISH ON PANELS IAW SRM 51-20-01.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

VERTICAL STABILIZER PANELS 9501L, 9505L 9503L ARE FRETTING FUSELAGE ATTACH ANGLE, WEAR ON ANGLE AND PANELS. REMOVED DAMAGED ANGLES BEHIND VERTICAL STABILIZER PANELS 9501L, 9505L, 9503L. FABRICATED REPAIR ANGLES AND INSTALLED ANGLES IAW TYPICAL REPAIR 5380-10113. RESTORED PROTECTIVE FINISH ON PANELS IAW SRM 51-20-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,355 hrs · 15,161 cycles

INTERCOSTAL IS CRACKED AT BL48 LEFT BETWEEN BODY STATION 312-328. REMOVED & REPLACED INTERCOSTAL AT BODY STATION 312 TO 328 BL48 PER 737-500 SRM 51-40-02.

Part: RUDDER — DAMAGED · airframe 29,355 hrs · 15,161 cycles

RUDDER TRAILING EDGE DAMAGED ON RIGHT-HAND SIDE 30 INCHES BELOW LOWER STATIC DISCHARGE WICK. REPAIRED RUDDER TRAILING EDGE AT STATION 220 PER CONTINENTAL EC/RA 5540-01251 INIT FIRST CALCULATED REBALANCE PER CONTINENTAL EC/RA 5100-02041 COMPLIED WITH, NEW MOMENT IS + 367.94, NO ADDITIONAL WEIGHTS REQUIRED.

Part: BRACKET — CRACKED (RT WING) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND A 6 INCH CRACK IN RT WING BRACKET UNDER PANEL 5849, WBL 198.6. THE BRACKET WAS REPLACED IAW SRM 51-40-02.

Part: BRACKET — CRACKED (NR 8 FLAP TRACK) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND A .75 INCH CRACK IN RT WING NR 8 FLAP TRACK FORWARD FAIRING ATTACH BRACKET. REPAIRED IAW ECRA 5740-02040.

Part: SKIN — GOUGED (LT WING LE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND A GOUGE IN LT WING FIXED L/E UPPER SKIN PANEL AT O/B END OF NR 2 SLAT. THE SKIN WAS REPAIRED IAW SRM 51-70-16 AND ECRA 5721-01048.

Part: SKIN — DENTED (CARGO DOOR) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND IN AFT CARGO DOOR SKIN APPROXIMATELY 23 INCHES FROM FORWARD EDGE AND 23 INCHES FROM TOP EDGE.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED APPROXIMATELY 37 INCHES FROM FORWARD EDGE AND 31 INCHES FROM TOP EDGE. A REPAIR WAS INSTALLED IAW SRM 52-00-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND FUSELAGE SKIN GOUGED JUST LEFT OF RUDDER SEAL AT STA 1116. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-80-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND L-ANGLE CORRODED AT STA 951-995, RBL 55. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHING CORRODED AT LT O/B AFT LOCATION. THE BUSHING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-52274.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT RT I/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED IAW SOPM 20-50-03.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT O/B FORWARD AND AFT AND RT O/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE PER DRAWING 65-46872.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT AT STA 328-344, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65C33973.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND FLOOR SUPPORTS AT STA 344-360 BL 0 AND LBL 10 CRACKED. THE CRACKS WERE .5 INCH AND 4 INCH. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND DRAWING 65C33970-53.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND L-1 DOOR GIRT BAR AFT LATCH ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 16,933 hrs · 8,719 cycles

INSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT I/B FORWARD AND AFT AND RT I/B AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE IAW DRAWING NR 65-46872.

Part: SOLENOID — INOPERATIVE (MLG LEVER) · airframe 16,899 hrs · 8,695 cycles

THE LANDING GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION AFTER TAKEOFF FROM EWR. QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE LANDING GEAR LEVER LOCK CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. THE GEAR WAS SWUNG SEVERAL TIMES, BUT THE FAILURE COULD NOT BE DUPLICATED. THE LANDING GEAR LEVER LOCK SOLENOID WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE GEAR WAS SWUNG SEVERAL TIMES AGAIN AND ALL OPERATION CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 16,366 hrs · 8,399 cycles

THE AIRCARFT FUSELAGE SKIN SUSTAINED LIGHTNING STRIKE DAMAGE AT STA 747 S1R AND STA 727 S1R. THE DAMAGE WAS IN THE FORM OF A .5 INCH CRACK AND A .1562 INCH HOLE. THE SKIN WAS REPAIRED IAW SRM 53-00-01.

Part: ENGINE — FAILED (NR 1)

THE NR 1 ENGINE FLAMED OUT WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO ELP WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE IS IN THE PROCESS OF BEING CHANGED.