N18350
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
99 reports on file, 1996-04-04 – 2008-05-28.
Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 60,256 hrs · 31,049 cycles
RIGHT-HAND MAIN GEAR INDICATION DID NOT INDICATE GREEN WITH LANDING GEAR HANDLE DOWN. COMPLIED WITH MANUAL EXTENSION AND INDICATION WAS NORMAL. RIGHT-HAND MAIN GEAR HANGING UP DURING MAINTENANCE SWING REF NR 4263137 FOR UPLOCK ACTUATOR REMOVE AND REPLACE AND NR 4263138 FOR LEAK AND OPS CHECK.
Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 59,740 hrs · 30,808 cycles
AFT CARGO DOOR FWD SIDE LOWER FRAME CRACKED. REPLACED AFT CARGO DOOR FWD LOWER FRAME REF SRM 51-10-2 & DWG 65-47952.
Part: FITTING — CORRODED (NR 2 PYLON) · airframe 59,740 hrs · 20,808 cycles
NR 2 ENGINE PYLON RIGHT FITTING HAS CORROSION INSIDE BUSHING HOLE. REPAIRED NR 2 ENGINE PYLON RIGHT FITTING IAW EC/RA 5450-01735 AND PACE EA350-54-001.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
CORROSION FOUND ON FLANGE AND RADIUS OF INTERCOSTAL AT BL 0 BETWEEN STA 219 TO STA 227. REMOVED CORRODED STIFFENER, DAMAGE FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-10-08. INSTALLED NEW STIFFENER P/N 69-38740U2 IAW B737 SRM 51-40-02.
Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 59,740 hrs · 30,808 cycles
CO-PILOTS NR 2 SLIDING WINDOW HARD TO CLOSE. ADJUSTED THE CO-PILOTS RT NR 2 WINDOW IAW B737 AMM 56-12-11.
Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 59,740 hrs · 30,808 cycles
PILOTS NR 2 SLIDING WINDOW HARD TO CLOSE. ADJUSTED SHIMS ON THE PILOTS LT NR 2 SLIDING WINDOW IAW B737 AMM 56-12-11.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,740 hrs · 20,808 cycles
R1 DOOR FRAME HAS CRACK AT FS 294.5 AND STRINGER 7R. REMOVED STUB FRAME IAW B737 SRM 51-40-02 FOR REPLACEMENT REF B737 SRM 51-10-02. LOCATED AND DRILLED NEW FRAME P/N 65-45807U6 IAW B737 SRM 51-40-02. INSTALLED NEW STUB FRAME IAW B737 SRM 51-40-02.
Part: DEPRESSOR — CRACKED (R1 DOOR FRAME) · airframe 59,740 hrs · 30,808 cycles
SEAL DEPRESSOR CRACKED AT R1 DOOR FRAME UPPER FWD CORNER. REMOVED CRACKED SEAL DEPRESSOR P/N 65-53595-1 IAW B737 SRM 51-40-02 REF BOEING DWG 65-53595.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
INITIATE A DIP ON RT FUSELAGE BETWEEN STA 340 & 360 AND BETWEEN S-20 RT AND S-21 RT HAS CREASE JUST ABOVE SHEET METAL REPAIR. COMPLETED REPAIR INSTALLATION PER CAL EC/RA 5331-01260.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
INTERCOSTAL CRACKED AT AFT BAG BIN UNLOCK ATTACH POINT. REMOVED AND REPLACED UPLOCK ATTACH CHANNEL ASSEMBLY PER SRM 51-40-02.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 59,745 hrs · 30,811 cycles
BODY STA 303 STRINGER 10L CRACK FOUND AT DOOR HINGE LOWER WEB, SKIN ATTACH CLIP MARKED. REPAIRED STRINGER 10LT LOWER WEB SKIN ATTACH CLIP AT BS 303 PER PACE EA 350-53-003 CAL AND EC/RA 5310-04741.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
STA 70 FLOORBEAM BL 0 TO RBL 12 HAS CORROSION DAMAGE AT BS 270 FLOORBEAM FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-10-51 FIG 101. REMOVED DAMAGE & REPAIRED PER AVO 350-53-007 CAL REV A. WEIGHT OF REPAIR WITH FASTENERS AS INSTALLED IS LESS THAN 5 LBS.
Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 59,740 hrs · 30,808 cycles
UPPER SUPPORT ANGLE FOR NOSE WHEEL WELL VIEWING WINDOW HAS A CRACK AT FWD LT CORNERS. REMOVED AND REPLACED DAMAGED CHANNEL IAW B737-300 SRM 51-40-02.
Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
CORROSION ON L1 ENTRY THRESHOLD SUPPORT CHANNEL AT STA 312 TO 338 LBL 61. REMOVED THRESHOLD DRAIN AND CORRODED CHANNEL, LOCATED AND DRILLED NEW CHANNEL ASSEMBLY. INSTALLED NEW CHANNEL ASSEMBLY AND RE-INSTALLED THRESHOLD DRAIN PER SRM 51-40-02.
Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 59,740 hrs · 30,808 cycles
AFT CARGO DOOR FWD SIDE UPPER FRAME CRACKED. REPLACED AFT CARGO DOOR UPPER FWD FRAME REF SRM 51-10-2 & DWG 65-47952.
Part: SKIN — UNKNOWN (AFTCARGO DOOR) · airframe 59,740 hrs · 30,808 cycles
RE-SKIN AFT CARGO DOOR. WORK ACCOMPLISHED BY SL761. COMPLETED REPLACEMENT OF AFT CARGO DOOR OUTER SKIN IAW SRM 52-3 0-01 (WEIGHT OF OLD SKIN 13.55 LB, WEIGHT OF NEWLY INSTALLED SKIN 17.85 LB, EQUALS TOTAL ADDITIONAL WEIGHT OF 4.35 LB.)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
INTERCOSTAL BETWEEN 967 + 986.5 FLOORBEAMS RBL 18 IS CRACKED 986.5 SIDE. REMOVED AND REPLACED FLOOR SUPPORT LOCATED AT RBL 18 AND BETWEEN BS 967 TO BS 986.5, REF 737-300 SRM 51-40-02.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 59,743 hrs · 30,810 cycles
STRINGER SPLICE CHANNEL IS CRACKED, STA 361 AND STR 15 LT (MARKED). REMOVED & REPLACED STRINGER SPLICE CHANNEL BS 361 & S15L IAW PACE EA 350-53-003 CAL AND EC/RA 5310-04741.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,743 hrs · 30,810 cycles
INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT IAW B737 SRM 51-40-02 AND PACE EA350-53-003 CAL AND EC/RA 53-10-04741.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
STRINGER CRACKED AT STA 297, STR 10LT. REPAIRED CRACKED STRINGER AT STA 297 - STRINGER 10LT PER SRM 51-70-11.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,743 hrs · 30,810 cycles
INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 11 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 11 LT IAW B737 SRM 51-40-02 AND PACE EA 350-53-003 CAL AND EC/RA 5310-04741.
Part: ATTACH ANGLE — CRACKED (BS 294 S11L) · airframe 59,745 hrs · 30,811 cycles
CLIP AND ATTACH ANGLE ARE BOTH CRACKED, THAT ATTACH INTERCOSTAL TO FRAME AT STA 294.5 AND STR 11 LT (MARKED). REMOVED & REPLACED CLIP & ATTACH ANGLE THAT ATTACH INTERCOSTAL TO FRAME AT BS 294.5 & S11L PER PACE EA 350-53-003 CAL AND ECRA 5310-04741.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,743 hrs · 30,810 cycles
INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND 8 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 8 LT IAW B737 SRM 51-40-02 AND PACE EA 350-53-003 CAL AND EC/RA 5310-04741.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,743 hrs · 30,810 cycles
INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT IAW B737 SRM 51-40-02 AND PACE EA350-53-003 CAL AND EC/RA 53-10-04741.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
LEFT SUPPORT ANGLE FOR Z-ANGEL AT L1 DOOR JUST FWD OF FS 324 IS CORRODED. REMOVED AND INSTALLED NEW SUPPORT L-1 DOOR SUPPORT ANGLE IAW SRM 53-10-15.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
INTERCOSTAL AT STA 324 LBL 40 CRACKED AT FORWARD ATTACH POINT. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,745 hrs · 30,811 cycles
INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 294.5 AND STR 12 LT LOCATION IS CRACKED (MARKED). REMOVED & REPLACED ATTACH ANGLE AT BS 294.5 & S12L IAW PACE EA 350-53-003 CAL AND ECRA 5310-04741.
Part: STRAP — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
AFT CARGO STA 847 TO 857 AND RBL 19 THE UPPER AND LOWER STRAP ON THE INTERCOSTAL FLANGE ARE CORRODED. REMOVED LOWER AND UPPER STRAP AT STA 847 TO 857. REMOVED CORROSION FROM LOWER STRAP AND FOUND IT TO BE WITHIN LIMITS AND UPPER STRAP TO BE OUT OF LIMITS. PRIMED LOWER STRAP AND REPLACED UPPER STRAP PER SRM 51-40-02.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 30,808 hrs
FORWARD CARGO DOOR CUTOUT FORWARD FRAME IS CRACKED AT THE STOP PAD FITTING ATTACH POINT AT STRINGER 21R. REMOVED CRACKED FRAME PER SRM 51-40-02.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
AFT CARGO TOP & BOTTOM SURFACES OF FLOOR SUPPORT TRANSITION ANGLE AT STA 767 TO 787, RBL 22 ARE CORRODED. REMOVED AND REPLACED TRANSITION ANGLE P/N 69-43477U2 & INSTALLED NEW NUT PLATES IAW B737 SRM 51-40-02, STA 767-787 RBL 22 IAW B737-300 SRM 51-40-02 SL776.
Part: STRUCTURE — DAMAGED (RUDDER) · airframe 59,740 hrs · 30,808 cycles
RUDDER TRAILING EDGE HAS EXPOSED COMPOSITE APPROXIMATELY 8 INCHES FROM BOTTOM, RT SIDE. REPAIRED DAMAGE TO SUBJECT RUDDER IAW CONTINENTAL EC/RA NO 5540-01246.
Part: SKIN — DENTED (FUSELAGE) · airframe 59,740 hrs · 30,808 cycles
DENT AT STA 887 BETWEEN STR 19L + 20L DENT AREA FWD OF STA 887 IS 3.1 X 2.2 X .065 WITH A/Y RATIO OF 33.8 DENT AFT OF STA 887 IS 7.6 X 2.6 X .057 WITH A/Y RATIO OF 45.6 B737 SRM 53-00-01 FIG 101, SHT 2 NOTE: V DOES NOT PERMIT DENTS IN ADJACENT BAYS. REPAIRED DENTS BS887 BETWEEN STR 19LT & 20LT PER PACE EA350-53-001 CAL REVA EC/RA5330-03789.
Earlier reports · 1996–2007 · 67 reports
2007
Part: ANGLE — CORRODED (BS 986.5) · airframe 58,663 hrs · 30,320 cycles
INSPECTION FOUND TEE ANGLE AT L-2 DOOR GIRT BAR HOLE CORRODED, STA 986.5, WL 208.1, BL 0 TO LBL 40. A REPAIR WAS INSTALLED IAW ECRA 5311-01370.
2006
Part: DOOR FRAME — CRACKED (STA 480-500) · airframe 55,416 hrs · 28,834 cycles
INSPECTION FOUND A .5 INCH CRACK IN FWD CARGO DOOR SURROUNDING (FRAME) AFT DOOR JAMB WEB ABOVE STRINGER 23R, STA 480-500. THE AFT JAMB WEB WAS REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-20723.
Part: FITTING — CORRODED (FUSELAGE) · airframe 55,416 hrs · 28,834 cycles
INSPECTION FOUND STRINGER 27R END FITTING CORRODED AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-46568.
Part: FITTING — CORRODED (FUSELAGE) · airframe 55,416 hrs · 28,834 cycles
INSPECTION FOUND STRINGER 27L END FITTING CORRODED AT STA 1016. THE END FITTING WAS REPLACED IAW BOEING DRAWING 65-45568.
Part: STRINGER — CORRODED (BS 1016 S27R) · airframe 55,416 hrs · 28,834 cycles
INSPECTION FOUND STRINGER 27R CORRODED ON FORWARD SIDE OF CHORD AT STA 1016 APB, LEFT SIDE OF STRINGER END FITTING. REPAIRED IAW SRM 51-40-02 AND BOEING DRAWING 65-46568.
Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 54,101 hrs · 28,250 cycles
THE RIGHT MLG INDICATION WAS UNSAFE WHEN GEAR WAS EXTENDED FOR LANDING AT SAT. NO GREEN LIGHT WAS INDICATED. THE GEAR DID NOT APPEAR TO BE DOWN WHEN VIEWED THROUGH THE GEAR VIEWING PORT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT HAD TO BE TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE RT MLG DOWNLOCK ACTUATOR IAW MM 32-32-51. OPERATIONAL CHECKS WERE GOOD AND NO LEAKS WERE NOTED.
2005
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,613 hrs · 27,542 cycles
INSPECTION FOUND THE FUSELAGE SKIN AT LT NOSE WHEEL WELL CRACKED OUT AND MISSING, STA 259.5, S27L. REPAIRED IAW ECRA 5330-03472
2004
Part: CABLE — OUT OF ADJUST (MLG) · airframe 49,543 hrs · 26,026 cycles
THE GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION WHEN RAISING GEAR AFTER TAKEOFF FROM EWR. THE GEAR WAS CYCLED AND RETRACTION WAS NORMAL. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE TELEFLEX CABLE OUT OF ADJUSTMENT. THE CABLE WAS ADJUSTED IAW MM 27-65-51. AN ADJUSTMENT/TEST OF THE AIR/GROUND SENSORS WAS PERFORMED IAW MM 32-09-01. THE GEAR WAS CYCLED SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD.
Part: ATTACH ANGLE — WORN (LT MLG WW) · airframe 49,463 hrs · 25,990 cycles
DEEP WEAR AROUND FASTENERS ON LEFT AFT WHEEL WELL PANEL ATTACH ANGLE ON KEEL BEAM BETWEEN BS 715 & 272, 12 X 1 INCH. REPAIRED PER ECRA 5311-01195.
Part: PANEL — CRACKED (HORIZ STAB) · airframe 49,463 hrs · 25,990 cycles
GAP PANEL BETWEEN LT HORIZONTAL STAB AND TAIL CONE CRACKED. REPLACED PART PER SRM 51-10-02.
Part: CLIP — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
AFT BAG BIN STA 727E SKIN CLIP CORRODED AT S-26R &S-27R. REPLACED SECTION PER SRM 53-0007, FIG 204.
Part: HEAT SHIELD — CRACKED (LT ENGINE) · airframe 49,463 hrs · 25,990 cycles
LEFT ENGINE HEAT SHIELD CRACKED 2 INCHES. INSTALLED DOUBLER PER ECRA 5450-01073.
Part: CLIP — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
A/B/B ANTENNA U-CHANNEL FORWARD RIGHT ATTACH CLIP CRACKED AT STATION 727D (3 INCHES). REPLACED CRACKED ATTACH CLIP PER SRM 51-40-02.
Part: RIB — GOUGED (RT HORIZ STAB) · airframe 49,463 hrs · 25,990 cycles
RIGHT HORIZONTAL STAB LEADING EDGE RIBS (4 EACH) DAMAGED AT LOWER AFT EDGE. FIRST FOUR RIBS FROM INBOARD SIDE. TRIMMED OUT DAMAGED AREA ON ALL FOUR RIB WEBS. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO ALL FOUR RIBS PER SRM 51-70-13.
Part: SUPPORT — CORRODED (ANTENNA) · airframe 49,463 hrs · 25,990 cycles
ANTENNA SUPPORT CORRODED BETWEEN STA 727D AND 727E. REPLACED U-CHANNEL FOR ANTENNA IAW SRM 51-10-02.
Part: HINGE FITTING — BROKEN (RT WING) · airframe 49,463 hrs · 25,990 cycles
RT WING DOOR LWR HINGE FITTING IS BROKEN AT NR 6 FLAP TRACK. REPLACED DOOR HINGE IAW SRM 51-40-02.
Part: CLIP — CRACKED (LT ELEVATOR) · airframe 49,463 hrs · 25,990 cycles
LEFT ELEVATOR O/B SIDE HINGE PANEL SUPPORT CRACKED. INSTALLED CLIP PER SRM 55-20-02 FIG 1; 51-30-01 FIG 2.
Part: SKIN — CRACKED (R1 DOOR) · airframe 49,463 hrs · 25,990 cycles
R1 DOOR LOWER HINGE CUTOUT UPPER SKIN PULLING AND CRACKED (1 INCH) ALONG RIVETS JUST ABOVE CUTOUT. FABRICATED AND INSTALLED REPAIR PER SRM 52-00-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
DENT IN LEFT SIDE OF FUSELAGE AT BS 380 + 15 BELOW S-16LT. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED, INSTALLED REPAIR PER SRM 53-00-01 FIG 208.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND AFT GALLEY DRAIN MAST HAT CHANNEL CORRODED AFT OF STA 986.5 BETWEEN S25L AND S26L.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND L-1 DOOR Z-ANGLE AT LOWER SILL CORRODED, STA 294-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND STRINGER 25L CORRODED AT STA 967-996. A NEW STRINGER AND SPLICES WERE INSTALLED IAW SRM 53-00-03.
Part: SKIN — GOUGED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND LEFT FUSELAGE SKIN GOUGED AT STA 986 JUST AFT OF DRAIN MAST, S25L. THE GOUGED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 229.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND FORWARD SUPPORT ANGLE THAT ATTACHES TO FRAME CRACKED IN SEVERAL PLACES AT STA 277, S14L TO S16L. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11, FIGURE 1.
Part: SKIN — DENTED (FUSLEAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 380 + 17 BELOW STRINGER 17L. THE DENT WAS REPAIRED USING A DOUBLER IAW SRM 53-00-01, FIGURE 208.
Part: WEB — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 380-400, BL 0. REPAIRED IAW SRM 51-10-02.
Part: WEB — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND LEFT AFT LAV WEB CORRODED AT STA 1006-1016. THE WEB WAS REPLACED IAW SRM 51-10-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND STRINGER 25L CORRODED IN E & E COMPARTMENT AT STA 351, LBL 32. A REPAIR WAS INSTALLED IAW SRM 53-00-03, DETAIL 7.
Part: STRINGER — CORRODED (E/E BAY) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND STRINGER 28L CORRODED AT STA 364, LBL 8 IN THE E&E COMPARTMENT. REPAIRED IAW SRM 51-10-02.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND VERTICAL STABILIZER O/B AFT FUSELAGE FITTING CORRODED AT AFT BOTTOM SIDE OF HOLE CUTOUT, RIGHT AFT CLEVIS, STA 1088. REPAIRED IAW ECRA 5342-01021.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S16L AND S17L. A NEW SHEAR TIE SECTION WAS INSTALLED IAW SRM 53-00-07, FIGURE 207.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S15L AND S16L. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-00-07.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 5 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S15L AND S16L. A DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 207.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND Z-ANGLE SPLICE CORRODED AT BS 1006 LEFT SIDEWALL. A NEW SPLICE WAS INSTALLED IAW SRM 51-10-02.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 4 INCH CRACK IN ZEE ANGLE AT L-2 DOOR JAMB, STA 949. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S14L AND S15L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02, 51-40-02, AND BOEING DRAWING 65-45805.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN STRINGERS 14 AND 15L. THE CRACKED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-07, FIGURE 207.
Part: WEB — CORRODED (STA) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND WEB CORRODED AT FLOOR, STA 947 STRINGER 17L. A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND AFT PRESSURE BULKHEAD RIGHT RADIAL STIFFENER CORRODED AT STA 1016, BL 0. THE CORRODED SECTION OF RADIAL STIFFENER WAS CUT OUT AND A NEW SECTION OF RADIAL STIFFENER WAS INSTALLED IAW BOEING DRAWING 65C28106, REV B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 277 TO 294, RBL 45.6. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-02.
Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND TWO AFT WHEEL WELL PANEL I/B ATTACH BRACKETS CORRODED AT STA 727. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-40-02.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND A 1 INCH CRACK IN STRINGER 8L SUPPORT BRACKET AT STA 578. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: ANGLE — CORRODED (R-1 DOOR) · airframe 49,463 hrs · 25,990 cycles
INSPECTION FOUND R-1 DOOR LOWER CENTER SILL PLATE MOUNT ANGLE CORRODED. THE MOUNT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
2003
Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 47,727 hrs · 25,018 cycles
AN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5510-01682.
Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 47,727 hrs · 25,018 cycles
AN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. THE SPAR CHORDS WERE REPAIRED IAW ECRA 5510-01682.
2000
Part: FRAME — CHAFED (FUSELAGE) · airframe 39,624 hrs · 20,571 cycles
APU PNEUMATIC DUCT CLAMP RUBBING BACK FACE OF1040 FRAME. BURNISHED AREA, VERIFIED DOUBLERS AND FILLER AND INSTALLED PER EC/RA 5310-04008.
Part: FITTING — CRACKED (LT WING SPAR) · airframe 39,624 hrs · 20,571 cycles
LEFT WING MLG BEAM ATTACH BRACKET O/B OF GEAR TO REAR SPAR CRACKED AT EDGE (1) OF OPENING O/B UPPER EDGE. REMOVED AND REPLACED FITTING PER EC/RA 5740-01423.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,625 hrs · 20,571 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 18. AN UPPER CHORD REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.
1998
Part: KEEL BEAM — CORRODED (BS 720 - 727)
RT W/W KEEL BEAM CORROSION FROM BS 720 TO 727. FABRICATED AND INSTALLED STRAP PER EC/RA 5310-03727.
Part: SKIN — DENTED (BS 867)
DENT 64 OF AFT CARGO DOOR. CUT OUT DAMAGED SKIN, PERFORMED HFEC PER SRM 53-00-01. INSTALLED REPAIR PER SRM 53-00-01.
Part: SKIN — CRACKED (NR 1 PYLON)
A .5 INCH CRACK COMING FROM UPPER FWD CORNER OF NR 1 PYLON PANEL 5724. REPAIRED PYLON PER EC/RA 5430-01204.
Part: FLOORBEAM — CORRODED (BS 312)
MAIN CABIN FLOORBEAM CORRODED STA 312 RBL 10 TO LBL 10 UPPER T ON BEAM AROUND NUT PLATES FORWARD AND AFT SIDES OF BEAM. INSTALLED REPAIR PER SRM 53-10-51.
1997
Part: COMBUSTOR UNIT — INOPERATIVE (APU)
THE APU FIRE LIGHT AND BELL ACTIVATED AS APU WAS BEING STARTED ON LANDING. THE APU FIRE CHECKLIST WAS COMPLETED, THE APU FIRE BOTTLE WAS DISCHARGED AND THE APU WAS SHUT DOWN. MAINTENANCE FOUND THE APU HAD TORCHED. THE APU COMBUSTOR UNIT WAS REMOVED AND REPLACED. OPERATION OF THE APU CHECKED GOOD. THE APU FIRE BOTTLE WAS REPLACED.
Part: RETRACT MECH — MALFUNCTIONED (NLG)
THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS JACKED AND THE NOSE GEAR WAS RETRACTED FOUR TIMES WITH NO DEFECTS NOTED. THE AIRCRAFT HAS FLOWN OVER TEN FLIGHTS WITHOUT A REPEAT OF THIS ANOMALY.
1996
Part: CYLINDER — INOPERATIVE (NLG)
THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING MFE. THE GEAR WAS CYCLED, BUT THE LIGHT DID NOT EXTINGUISH. THE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NLG RETRACT ACTUATOR WAS REPLACED BASED ON THE REPORTED FAULT. THE GEAR WAS SWUNG, AND THE PROBLEM WAS DUPLICATED. THE NLG CYLINDER WAS REMOVED AND REPLACED. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD.
Part: BULKHEAD — DAMAGED (BS 178-180)
THE AIRCRAFT EXPERIENCED A BIRD STRIKE RESULTING IN DAMAGE TO FUSELAGE SKIN AND BS 178 BULKHEAD WEB AT APPROXIMATELY RBL 20, WL 190. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03301. THE SKIN AT STA 180 WAS REPAIRED PER SRM 53-00-01, FIGURE 27.
Part: FLOORBEAM — CORRODED (BS 986)
HOU - INSPECTION FOUND FLOORBEAM CORRODED ON TOP AND BOTTOM SURFACE AT STA 986. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-51. (X)
Part: INTERCOSTAL — CORRODED (BS 947)
HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORROSION AT STA 947, LEFT AND RIGHT SIDE. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03252. (X)
Part: STRINGER — CRACKED (BS 500)
HOU - INSPECTION FOUND A .50 INCH CRACK IN STR 16L AT STA 500. A NEW STRINGER SECTION AND SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-00-03. (X)
Part: INTERCOSTAL — CORRODED (BS 947-967)
HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STA 947 TO STA 967, RBL 12. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03252. (X)
Part: INTERCOSTAL — CORRODED (BS 312-328)
HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED BETWEEN STA 312 AND STA 328 AT LBL 10. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03252. (X)
Part: SPAR CAP — DAMAGED (RT HORIZ STAB)
HOU - INSPECTION FOUND IMPACT DAMAGE THREE FEET FROM OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER AND LOWER SPAR CAPS. REPAIRS WERE PERFORMED IAW ECRA 5510-01327. (X)
Part: INTERCOSTAL — CORRODED (BS 328-344)
HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED BETWEEN STA 328 AND STA 344 AT LBL 10. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03252. (X)
Part: INTERCOSTAL — CORRODED (BS 294.5)
HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED JUST AFT OF STA 294.5 AT RBL 15. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 5310-03252. (X)
Part: INTERCOSTAL — CORRODED (BS 344-360)
HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED BETWEEN STA 344 AND STA 360 AT LBL 15. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03252. (X)
Part: INTERCOSTAL — CORRODED (BS 328)
HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED JUST FORWARD OF STA 328 AT RBL 10. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 5310-03252. (X)