N35888
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.
119 reports on file, 1995-02-03 – 2000-10-23.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED UNDER CLIP NUTS AT FS 1230 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-05, FIGURE 3.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO RT SIDE TIE DOWN TRACK CORRODED BETWEEN FS 1212 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4 AND 51-10-3.
Part: DOUBLER — CRACKED (RT MLG WW) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 2 INCH CRACK IN DOUBLER AT RT WHEEL WELL FORWARD LOWER CORNER. REMOVED INTERCOSTAL AND DOUBLER AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-04 AND 53-30-5.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FORWARD CARGO AFT RT TIE DOWN TRACK HAD CORRODED SCREW HOLES ON TOP AND BOTTOM. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-3, AND 51-30-4.
Part: SKIN — GOUGED (DOOR CUTOUT) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RT AFT EMERGENCY EXIT DOOR CUTOUT SKIN GOUGED AT UPPER DOOR LATCH. THE RIVETS WERE REMOVED IAW SRM 51-30-2. THE SEAL DEPRESSOR WAS CUT IAW SRM 53-05, FIGURE 32. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4 AND 53-05, FIGURE 32.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO AREA CORRODED BETWEEN FS 1007 AND 1320. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4G.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT RT END OF TRACK TO AFT BULKHEAD FRAME IN FWD CARGO PIT CORRODED AT STA 522. THE TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.
Part: ANGLE — CRACKED (TAIL) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 6 INCH CRACK IN ANGLE JUST FORWARD OF RUDDER TRIM ACTUATOR IN TAIL COMPARTMENT AREA AT STA 1485, RT SIDE. THE VENT BOX WAS REMOVED IAW SRM 51-30-1. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. THE VENT BOX WAS REINSTALLED IAW SRM 51-30-1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 200, RBL 39. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-03, 51-30-2, AND 51-10-04.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 6 INCH CRACK IN CENTER KEEL SUPPORT AT STA 948. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-01 AND 53-01.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND INTERCOSTAL AND ATTACHING BRACKETS CORRODED IN AFT CARGO AREA BETWEEN FS 1148 - 1155, LONGERONS 29R AND 30. THE INTERCOSTAL AND BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-2.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 1 INCH CRACK AT AFT END LOWER SIDE OF AFT ACCESSORY COMPARTMENT INTERCOSTAL BETWEEN FS 1497 AND 1510. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND CABIN FORWARD ENTRY FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 190, LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5, PAGE 1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 180, LBL 12 - 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.
Part: FLOORBEAM — CRACKED (CABIN) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT FS 218, LBL 44. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW 53-05, FIGURE A AND 51-30-2.
Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A GOUGE IN RADIUS OF INTERCOSTAL AND CORROSION WAS NOTED BETWEEN FASTENERS ON LOWER ANGLE MATING SKIN AT FS 430 - 446, L28R. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-5.
Part: INTERCOSTAL — CORRODED (DOOR FRAME) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO CHANNEL INTERCOSTAL CORRODED ON DOOR JAMB. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2 AND 51-30-05.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND LOWER BULKHEAD SUPPORT CORRODED IN AFT CARGO AREA AT FS 1322. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.
Part: PAN — CORRODED (CARGO DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED BETWEEN FS 370 AND 427. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2. THE OUTSIDE LOWER SCUFF PLATE WAS REPLACED IAW SRM 51-30-3.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RT CARGO TIEDOWN TRACK CORRODED IN AFT CARGO AREA AT FS 1007 - 1155. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-04, FIGURE 4.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1117 - 1155 BETWEEN L28L AND L28R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-2 AND 51-30-5.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180, RBL 9 TO RBL 38. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, RBL 4 TO LBL 4, LBL 8, AND RBL 10 TO 40. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.
Part: PLATE — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO CENTER THRESHOLD PLATE CORRODED AT STA 1231. THE THRESHOLD PLATE REMOVED AND REPLACED IAW SRM 51-10-3.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL AT SUB FLOOR INSIDE L-1 DOOR, FS 190, LBL 56. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT Z-ANGLE CORRODED AT FS 586 - 636. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-01, FIGURE 1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND R-1 DOOR ENTRY FLOOR SUPPORT CORRODED AT FS 155 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND MID PIT LT TIE DOWN TRACK CORRODED AT FASTENER HOLES FROM FS 541 - 790. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW 51-30-2, 51-10-3, AND 51-30-5.
Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND SKIN FINGER DOUBLER CORRODED AT FS 256, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND A NEW FINGER DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND EA 9-5332-2-A0790.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RIGHT I/B CABIN SEAT TRACK CORRODED AT FS 200 - 265. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1.
Part: WEB — CRACKED (CABIN) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 19 INCH CRACK IN CABIN RT CUSP WEB AT FS 218 - 237, RBL 44 - 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
Part: RIB — CORRODED (FAIRING) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FUSELAGE FAIRING MOUNTING RIB 5L CORRODED AT BOTTOM LOCATION FS 826, LONGERON 29L. DOUBLERS AND SHIM WERE INSTALLED IAW SRM 53-01, FIGURE 2.
Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND G-2 GALLEY SUPPORT CORRODED AT FS 218, RBL 11. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO BULKHEAD CENTER VERTICAL SUPPORT CORRODED AT FS 1322. THE VERTICAL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN FS 1271 AND 1289 AT LONGERON 27L. THE DENT WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND TWO CRACKS IN DOUBLER AROUND DOOR HANDLE OF FWD CARGO DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.
Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 2 INCH CRACK IN FIRST OFFICER''S SEAT LOWER FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-4.
Part: FITTING — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO SUPPORT FITTING CORRODED AT FS 1007, LONGERON 28R. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: HINGE — CORRODED (ACCESS DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT LAV SERVICE PANEL ACCESS DOOR HINGE AND BRACKET CORRODED. THE DOOR HINGE AND BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-1, AND 51-10-4.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 160, RBL 7 TO LBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1.
Part: BEAM — CORRODED (DOOR FRAME) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND LOWER HALF OF AFT CARGO DOOR JAMB BEAM CORRODED ON BOTH SIDES AT FS 1155 - 1212. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.
Part: WEB — CORRODED (TORQUE BOX) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND CORROSION UNDER AND ON FORWARD TORQUE BOX STRAP AND WEB AT FS 1155 - 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3. CORROSION REMOVAL FROM THE STRAP WAS WITHIN LIMITS IAW SRM 53-01, FIGURE 1 AND 51-10-3.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND G-2 GALLEY SUPPORT CUSP WEB CORRODED AT FS 218, RBL 11. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 200 - 237. THE SEAT TRACK WAS REMOVED AND REPLACED IAW 53-05, FIGURE 4A.
Part: WEB — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND WEB CORRODED AT FS 200, RBL 13, AFT OF FLOORBEAM. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED USING A SPLICE IAW SRM 51-10-2 AND 51-30-2.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1030 - 1309. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 47. THE FLOOR PANELS WERE REINSTALLED AND SEALED IAW ECRA 5100-01844.
Part: CHANNEL — CORRODED (DOOR FRAME) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND ON O/B END OF INSIDE CHANNEL OF THE L-1 DOOR JAMB STRIP. THE CHANNEL WAS REPLACED IAW SRM 51-30-2 AND 51-10-3.
Part: STRAP — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND STRAP CORRODED IN AFT PIT AT STA 1184 BETWEEN LONGERONS 29R AND 30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-34-0, 51-10-4, 51-10-3, 51-30-2, 51-30-5.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND CUSP WEB AT L-1 DOOR LOWER JAMB AREAS CORRODED BETWEEN FS 136 AND 202. REPAIRED IAW SRM 51-30-5 AND ECRA 5310-04053.
Part: PANEL — CORRODED (LT ELEVATOR TAB) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND LT ELEVATOR O/B GEAR TAB MECHANISM PANEL CORRODED AROUND DIMPLED FASTENER HOLES AND ONE FASTENER HOLE WAS CRACKED. THE PANEL WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW 51-30-2.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND ATTACH ANGLE CORRODED IN AFT CARGO AREA AT FS 1041 BETWEEN LONGERONS 29L AND 29R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.
Part: BRACKET — CORRODED (DOOR FRAME) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO TORQUE BOX CHANNEL BRACKET CORRODED IN DOOR JAMB AREA. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND CENTER LOWER FLOOR SUPPORT CORRODED IN AFT CARGO AREA AT FS 1007. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-4, 51-10-3, AND 51-30-2.
Part: DOUBLER — CRACKED (NLG DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 1 INCH CRACK IN LEFT NLG DOOR AFT HINGE DOUBLER. REPAIRED IAW SRM 53-05, FIGURE 62.
Part: INTERCOSTAL — CORRODED (DOOR FRAME) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO T-INTERCOSTAL CORRODED AROUND CLIPNUT HOLES IN DOOR JAMB AREA. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
Part: SKIN — DENTED (CARGO DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 52-05. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 & 2 AND 51-30-1.
Part: DOUBLER — CRACKED (NLG DOOR) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 1 INCH CRACK IN RIGHT NLG DOOR AFT HINGE DOUBLER. REPAIRED IAW SRM 53-05, FIGURE 62.
Part: SKIN — GOUGED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RT FORWARD EMERGENCY EXIT DOOR CUTOUT SKIN GOUGED AT UPPER DOOR LATCH. THE RIVETS WERE REMOVED, CUT OUT SEAL DEPRESSOR, AND INSTALLED REPAIR ANGLE AND SEAL DEPRESSOR IAW SRM 51-30-2, 53-05, FIGURE 32, 51-10-4, AND 51-10-3.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND INTERCOSTAL CORRODED AROUND AND UNDER NUT PLATES AT FS 1309 - 1322, LONGERON 27L AND 28L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5 AND 51-10-3.
Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND A 4 INCH CRACK IN LEFT W/W FORWARD INTERCOSTAL AT LOWER I/B CORNER. THE INTERCOSTAL AND EXISTING REPAIR WERE REMOVED. A NEW REPAIR AND INTERCOSTAL WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-10-3.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND RT FORWARD FUSELAGE SKIN DENTED AT STA 37. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-10-3.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
SKIN DENTED BETWEEN STATION 370 AND 389 AT LONGERON 29 AND 30R. COLD WORKED DENT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
RIGH AFT LAV SUPPORT STRUCTURE CORRODED AT STATION 1309 - 1325. REMOVED AND REPLACED SUPPORT PER SRM 51-30-1.
Part: RIB — CRACKED (RT WING TE FLAP) · airframe 52,990 hrs · 29,245 cycles
RIGHT WING FLAP INBOARD TRAILING EDGE WEDGE CENTER RIB HAS A CRACK 5 INCHES ON STIFFENER CORNER. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-01 FIG 3.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CABIN FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 250 AT LBL 12 ON FORWARD AND UPPER SURFACE. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5.
Part: SUPPORT BRACKET — CRACKED (BULKHEAD) · airframe 52,990 hrs · 29,245 cycles
AFT CARGO FORWARD BULKHEAD VERTICAL SUPPORT CRACKED 2 INCHES AT FS 1007 AT LOWER END. FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 53-10 FIG 2.
Part: SKIN — GOUGED (RT WING LE FLAP) · airframe 52,990 hrs · 29,245 cycles
RIGHT WING FLAP NUMBER 8 LEADING EDGE HAS CUT ON SURFACE. FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 57-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
AFT CABIN FLOORBEAM AT FS 1322 CORRODED ON UPPER AND LOWER SURFACES. TRIMMED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 53-05 FIG 2.
Part: DOOR — CRACKED (RT MLG) · airframe 52,990 hrs · 29,245 cycles
RIGHT MLG DOOR FORWARD LOWER LEADING EDGE IS CRACKED 2 INCHES. FABRICATED AND INSTALLED ANGLE REPAIR PER EA 9-5281-2-A0771.
Part: FAIRING — CHAFED (NR 2 TE FLAP) · airframe 52,990 hrs · 29,245 cycles
LEFT NUMBER TWO FLAP HINGE FAIRING IS CHAFED ON INNER PERIMETER. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-01 FIG 1.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
SHEAR TIE CORRODED AT FS 1193 FROM LONG 2 TO 4L. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-5.
Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 52,990 hrs · 29,245 cycles
RIGHT MLG DOOR FORWARD LOWER CORNER IS CRACKED 2 INCHES. FABRICATED AND INSTALLED REPAIR ANGLE PER EA 9-5281-2-A0771.
Part: SKIN — DAMAGED (LE FLAP) · airframe 52,990 hrs · 29,245 cycles
RIGHT WING FLAP LEADING EDGE NUMBER 8 HAS A DAMAGED SCREW HOLE. FABRICATED AND INSTALLED CONICAL WASHER AND REPAIR DOUBLER PER SRM 51-01 FIG 3, 51-10-3, AND 51-01.
Part: STRUCTURE — GOUGED (AFT CARGO DOOR) · airframe 52,990 hrs · 29,245 cycles
AFT CARGO DOOR HINGE ACCESS HOLE HAS A GOUGE IN THREE PLACES IN TOP CENTER OF THE HOLE. TRIMMED OUT GOUGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-05 FIG 35A.
Part: DOUBLER — WORN (CARGO DOOR) · airframe 52,990 hrs · 29,245 cycles
FORWARD CARGO DOOR AFT EDGE CORNER DOUBLER WORN. REMOVED FABRICATED AND INSTALLED NEW DOUBLER PER TRAVELER T10017 AND SRM 51-30-2.
Part: WEB — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
SUBFLOOR CORRODED AT FS 200 LBL 56 CORRODED. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-4-1 AND 51-30-2.
Part: WEB — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CABIN LEFT HAND CUSP WEB IS CRACKED (.5 INCH) ON INBOARD SIDE AT FS 1041. ROUTED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER OVER CUSP PER SRM 53-01 AND 51-30-2.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CORROSION IN FORWARD CABIN FLOOR WEB BETWEEN STATIONS 200 AND 237 AT 18L. REMOVED FLOOR SUPPORT CUSP. FABRICATED AND INSTALLED NEW CUSP PER SRM 53-14-1.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
LEFT INBOARD SEAT TRACK FS 322 - 437 IS CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FIG 4F AND SPLICED PER SRM 53-05.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CABIN FS 148 - 200 LBL 7 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-4 AND 51-30-1.
Part: ANGLE — CORRODED (DOOR JAMB) · airframe 52,990 hrs · 29,245 cycles
L2 DOOR JAMB LOWER AFT ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER SRM 51-10-3 AND 51-30-5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
LEFT OUTBOARD SEAT TRACK CORRODED FROM FS 1079 - 1174. REMOVED DAMAGED SECTION OF SEAT TRACK. FABRICATED AND INSTALLED SPLICE MATERIAL PER SRM 51-30-1, 51-30-2, 53-05 PG109 FIG 4F, AND 51-30-5.
Part: CLIP — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
MID PIT FS 636 L28R T CLIP IS CORRODED. REMOVED AND REPLACED T CLIP PER SRM 51-30-5 AND 51-10-3.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
CABIN FLOOR SUPPORT AT FS 1155 BETWEEN LEFT SEAT TRACKS CORRODED. REMOVED, FABRICATED, AND REINSTALLED FLOOR SUPPORT PER SRM 51-10-03, 51-30-05, AND 51-10-04.
Part: WEB — CRACKED (TORQUE BOX) · airframe 52,990 hrs · 29,245 cycles
L1 DOOR AFT TORQUE BOX LOWER SKIN AFT LUG CRACKED (2 INCHES). TRIMMED CRACKED AREA, INSTALLED REPAIR FILLER AND DOUBLER PER EA 9-5314-2-A0773, SRM 51-10-03, AND 51-30-02.
Part: WEB — CRACKED (TORQUE BOX) · airframe 52,990 hrs · 29,245 cycles
L1 DOOR AFT TORQUE BOX UPPER SKIN AFT AUG CRACKED (2 INCHES). TRIMMED CRACKED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER EA 9-5314-2-A0774, SRM 51-10-03, AND 51-30-02.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CRACK FOUND ON LT AFT CABIN FLOORBEAM WEB 18L BETWEEN STA 1231 TO STA 1250. FABRICATED REPAIR DOUBLER FOR LT CABIN FLOORBEAM WS 18L BETWEEN STA 1231 TO 1250 AS PER SRM 53-01 FIG 1, DRILLED UP NEW DOUBLER AS PER SRM 51-10-4, TREATED AND PRIMED AS PER SRM 51-10-3, AND INSTALLED DOUBLER AS PER SRM 51-30-5.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,990 hrs · 28,245 cycles
MID PIT CEILING-FLOOR SUPPORT AT BL 0, BETWEEN FS 770 & 790 CRACKED. REMOVED INTERCOSTAL, FAB NEW INTERCOSTAL IAW TRAV 10005, TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED IAW SRM 51-30-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,990 hrs · 28,245 cycles
CABIN FWD ENTRY FLOOR SUPPORT BETWEEN FS 160 AND 190 APPROX LBL 54 HAS AREAS OF CORROSION. REMOVED FLOOR SUPPORT IAW SRM 51-30-02, FABBED SUPPORT ON TRAVELER T9999, TREATED AND PRIMED IAW SRM 51-10-03, INSTALLED FLOOR SUPPORT AT L1 ENT FS 160 FS 190 LBL 54.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
EXTERNAL POWER DOOR LOWER LANDING SKIN IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-01, 53-34-0, 51-10-03, AND 51-30-02.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 52,990 hrs · 29,245 cycles
CABIN FLOOR SUPPORT FS 1174 BETWEEN L/R I/B SEAT TRACKS HAS CORROSION. REMOVED FLOOR SUPPORT AS PER SRM 54-30-02 REC NEW SUPPORT FROM FAB SHOP TRAVELER NR T 10010. ALODINED WASHED PRIMED PER SRM 51-10-03, INSTALLED IAW SRM 51-30-05.
Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 52,990 hrs · 29,245 cycles
PILOT SEAT LOWER FLOOR PANEL IS DAMAGED AND CRACKED. REMOVED PANEL, FABRICATED AND INSTALLED NEW PANEL PER SRM 51-30-01, 51-20-00, 53-20-00, AND 51-32-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
SKIN IS DENTED AT APPROXIMATELY STATION 446 BETWEEN LONG 25 AND 26R. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER PER SRM 53-04 FIG 38, 51-30-2, AND 53-03 FIG 3.
Part: SKIN — DENTED (LT NR 2 FLAP) · airframe 52,990 hrs · 9,245 cycles
LEFT FLAP NUMBER TWO TRAILING EDGE PANEL HAS A 1 INCH DENT 24 INCHES OUTBOARD OF INBOARD END. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 57-01 FIG 5. TREATED AND PRIMED PER SRM 51-30-2 AND 57-01-0.
Part: PANEL — TORN (RIGHT WING) · airframe 52,990 hrs · 29,245 cycles
RIGHT WING PANEL 1258 FASTENER HOLE TORN. REPAIRED AREA PER SRM 57-01 FIG 13 AND 57-32-1 PAGE 2.
Part: SKIN — GOUGED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 225, L18L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5330-02485 AND SRM 51-30-02.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 179 BETWEEN LONGERONS 21 & 22R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22 AND 51-10-03.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 503 BETWEEN LONGERONS 27 & 28R AND AT STA 565 BETWEEN LONGERONS 24 & 25L. THE DENTS WERE REFORMED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-3, 51-20-0, AND 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 208 BETWEEN LONGERONS 16 & 17L. THE DENT WAS REFORMED IAW SRM 53-04, FIGURE 38, SHEET 11. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22 AND 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 541 BETWEEN LONGERONS 20 & 21R. THE DENT WAS REFORMED IAW SRM 53-04, FIGURE 38, SHEET 11. DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 11, 51-10-3, 51-20-00, AND 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 391 BETWEEN LONGERONS 22 & 23L AND AT STA 408 BETWEEN LONGERONS 29 & 30R. THE DENTS WERE REFORMED IAW SRM 53-04, FIGURE 38. A DOUBLER REPAIR WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, SHEET 11, 51-10-3, 51-20-0, AND 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,990 hrs · 29,245 cycles
CABIN FS 1338 FLOORBEAM CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR FILLER PER SRM 53-05, 51-10-3, AND 51-30-5.
Earlier reports · 1995–1998 · 17 reports
1998
Part: SENSOR — INOP (NLG)
THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING EWR. THE UNSAFE LIGHT WAS ACCOMPANIED BY AIR NOISE INDICATIVE OF THE NOSE GEAR NOT BEING RETRACTED. THE GEAR WAS RECYCLED AND GEAR SAFE WAS INDICATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SENSOR AT FAULT. THE NOSE GEAR DOWNLOCK SENSOR WAS REPLACED AND ADJUSTED IAW MM 32-60-05. IN ADDITION, A FULL NOSE STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. A NOSE GEAR SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD.
Part: TAIL CONE — WARPED (AFT FUSELAGE)
THE TAILCONE PULL TEST EXCEEDED LIMITS AND THE TAILCONE DID NOT DEPLOY USING EITHER THE INTERIOR OR AFT RELEASE HANDLES. THE TAILCONE WAS REMOVED AND REPLACED IAW MM 53-53-00.
Part: TAB — DELAMINATED (RT ELEVATOR)
INSPECTION FOUND RT ELEVATOR GEAR TAB DELAMINATED. THE RT ELEVATOR GEAR TAB WAS REMOVED AND REPLACED IAW MM 27-30-04.
Part: SKIN — DENTED (BS 218-275)
INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 218 TO 275, LONGERON 17-18L. REPAIRED IAW ECRA 5330-02445.
Part: SKIN — DENTED (BS 370)
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 370 BETWEEN LONGERON 27L AND 28L. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.
Part: SKIN — GOUGED (BS 448-465)
INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT STA 448-465, LONGERON 19L TO 20L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B.
Part: DOUBLER — CORRODED (BS 465-489)
INSPECTION FOUND FORWARD BAGGAGE BIN INTERNAL DOUBLERS CORRODED BETWEEN STA 465 AND 489, LONGERONS 24L TO 26L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B, PAGE 35.
Part: BEAM — CRACKED (PAX DOOR)
INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, SECTION U-U, PAGE 179.
Part: SKIN — CRACKED (PAX DOOR)
INSPECTION FOUND A .5 INCH CRACK IN SKIN AT LOWER FORWARD CORNER OF MAIN ENTRY DOOR. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 32.
1996
Part: SLIDE — TORN (R1 DOOR)
SLIDE ON FORWARD GALLEY TORN AT GIRT BAR. REMOVED AND REPLACED SLIDE PER MAINTENANCE MANUAL.
Part: BELT FRAME — CORRODED (STA 1322)
INSPECTION FOUND BELT FRAME CORRODED ON RT SIDE AT STA 1322. A BELT FRAME WAS INSTALLED IAW SRM 53-03.
Part: FRAME — CRACKED (STA 1446)
INSPECTION FOUND CANTED FRAME STA 1446 CRACKED OUT WHERE LONGERONS 4R AND 5R ATTACH. THE UPPER CANTED CAP FRAME WAS REPLACED IAW SRM 51-30-2.
Part: FRAME — CRACKED (STA 1446)
INSPECTION FOUND CANTED FRAME STA 1446 CRACKED OUT WHERE LONGERONS 3L, 4L AND 5L ATTACH. THE UPPER CANTED CAP FRAME WAS REPLACED IAW SRM 51-30-2.
1995
Part: ANGLE — CRACKED (RT VERTICAL FIN)
IAH - INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF RT VERTICAL FIN ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 19. (X)
Part: LIGHT — INOPERATIVE (L-1 DOOR)
FLT NR 0603 - EWR - WHEN EMERGENCY LIGHTS TEST WAS PERFORMED, THE EMERGENCY PORTABLE LIGHT AT THE L-1 DOOR WOULD NOT ILLUMINATE. THE L-1 DOOR EMERGENCY PORTABLE LIGHT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M)
Part: HYD LINE — LEAKING (RT HYD SYSTEM)
FLT NR 0317 - DCA - THE RIGHT HYDRAULIC QUANTITY DECREASED 4 QUARTS WHILE IN FLIGHT FROM EWR TO DCA. MAINTENANCE FOUND THE HYDRAULIC BRAKE PRESSURE LINE IN THE RT WHEEL WELL LEAKING. THE LINE WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. SYSTEM LEAK CHECKS WERE GOOD. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
FLT NR 0751 - EWR - THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (Z)