N16804
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.
96 reports on file, 1995-01-28 – 2000-04-25.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,344 hrs · 23,585 cycles
VERTICAL AND HORIZONTAL SUPPORT ANGLES AT CFS 1485 VENT BOX ARE CRACKED (2). REMOVED AND REPLACED SUPPORT ANGLES PER SRM 51-30-5.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,344 hrs · 23,585 cycles
LEFT SIDE HEAT EXCHANGER SUPPORT BRACKET CRACKEDAT FS 1429 LONG. 4L (8). REMOVED AND REPLACED BRACKET PER SRM 51-30-1.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR LOWER DOOR JAMB CORRODED BETWEEN STA 1156 AND 1212. A DOUBLER AND SPACER WERE INSTALLED IAW ECRA 5310-03027.
Part: FRAME — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO PIT MAIN FRAME CENTER FLOOR STA 1300 CORRODED. REMOVED AND REPLACED SPLICES IAW SRM 51-30-2 AND 51-30-5.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND THE AFT CARGO PIT RT FLOOR TIE DOWN TRACK CORRODED AT STA 1211. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND MID CARGO COMPARTMENT FLOORBOARD SUPPORT CORRODED AT FS 598 - 636, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: WEB — CORRODED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR AFT JAMB TORQUE BOX UPPER WEB CORRODED AT LONGERON 28R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD CARGO DOOR JAMB AT O/B END OF TORQUE BOX CORRODED FROM STA 370 - 427. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LONGERON 29L TO 29R HAD SEVERAL CORRODED FASTENERS IN LONGERONS AND SPLICES IN MID CARGO COMPARTMENT AT FS 579 - 598. THE LONGERON SPLICES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
Part: SKIN — DENTED (NR 1 SLAT) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LT WING NR 1 SLAT DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 427 - 463. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: SKIN — DENTED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1380 BETWEEN LONGERON 4L AND 6L. THE DENTED SECTION OF SKIN WAS CUTOUT IAW SRM 53-01, FIGURE 2. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-02, AND 51-30-08.
Part: FITTING — CORRODED (E/E BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND SUPPORT FITTING CORRODED AT E & E COMPARTMENT INSIDE OF DOOR TORQUE BOX FS 148, LONGERON 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5.
Part: PAN — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR PAN STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1117 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LT HORIZONTAL STABILIZER O/B LEADING EDGE SKIN DENTED. DOUBLERS WERE INSTALLED IAW SRM 55-03, FIGURE 3.
Part: BRACKET — CRACKED (RT LAVATORY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 4 INCH CRACK IN TWO RT AFT LAV WALL ATTACH ANGLE BRACKETS. THE WALL ATTACH ANGLE BRACKETS WERE REMOVED AND REPLACED IAW MM 51-10-2.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD CARGO RT TIEDOWN TRACK CORRODED AT FS 229 - 370. THE TIEDOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: SKIN — PUNCTURED (RT MLG DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND THREE HOLES PUNCTURED INTO RT I/B MLG DOOR OUTER SKIN UPPER BLOCK. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: SKIN — DAMAGED (LT WING TIP) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LT WING TIP UPPER T/E SCREW HOLES ELONGATED. THE ELONGATED HOLES WERE CUTOUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 5 AND 51-30-2.
Part: PAN — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD CARGO DOOR PAN WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND RT TIEDOWN TRACK ATTACH FITTING CORRODED IN AFT CARGO PIT AT FS 1007. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND R-1 DOOR FLOORBEAM CORRODED AT FS 160 - 200, RBL 48. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2, 51-10-3 AND 51-30-1.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1155 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: SKIN — CHAFED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND EXTERNAL FUSELAGE SKIN CHAFED AT AREA OF HOLD OPEN HOOK RECEPTACLE FOR FORWARD ENTRY DOOR. THE CHAFED AREA WAS BLENDED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 24.
Part: BRACKET — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND TWO FORWARD AND TWO AFT SUPPORT BRACKETS HAD WORN AND ELONGATED HOLES AT AFT CARGO DOOR HINGE. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 16A.
Part: SKIN — DENTED (RUDDER) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND EXTERNAL SKIN OF LT SIDE OF RUDDER DENTED BETWEEN CENTER AND LOWER HINGE POINT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 10A, 51-10-4, 51-10-3, AND 51-30-6.
Part: DOUBLER — CRACKED (LT MLG DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 6 INCH CRACK IN LT MLG DOOR I/B LOWER AFT CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28 AND 51-30-5.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND WEB AND ATTACH ANGLE CORRODED AT PAX DOOR JAMB AFT SIDE, FS 200, LBL 58. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-3, 51-10-4, AND 51-30-5.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LT CARGO TIEDOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360, LONGERON 27L. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-3.
Part: FITTING — CORRODED (E/E BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND DOOR LATCH SUPPORT FITTING INSIDE OF E&E COMPARTMENT DOOR CORRODED AT FS 48, LONGERON 28 RT. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: STOP — CHAFED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR PAN STOP CHAFED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-1, 51-30-2, AND ECRA 5330-02189.
Part: SKIN — GOUGED (MLG DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND RT MLG DOOR LOWER SKIN, GOUGED ON O/B SIDE. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.
Part: SKIN — CHAFED (CRAGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND MID CARGO DOOR OUTER SKIN CHAFED AT LOWER AFT CORNER. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR CUSP WEB AT AFT END AND BULGING AT RIVETS, FS 198. FILLERS AND DOUBLERS WERE INSTALLED IAW ECRA 5320-01638 AND SRM 51-10-3.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR FLOOR SUPPORT AT FS 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-5.
Part: SKIN — GOUGED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AT FS 487 BETWEEN LONGERON 23 RT AND 24 RT. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND MID CARGO BAY FLOORBOARD SUPPORT CORRODED ON LOWER SIDE AT FS 636, LBL 15 TO RBL 15. THE FLOOR SUPPORT WAS REMOVEDAND REPLACED IAW SRM 51-30-2.
Part: WEB — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 218, LBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-3, 53-01, FIGURE 4, 51-01, 51-30-2, 51-30-5, AND 51-30-6.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 6 CRACK IN CABIN RT SUPPORT ANGLE AT FS 1308, STRINGER 13 RT - 14 RT. THE FASTENER WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED JUST INSIDE AFT CARGO BAY DOORWAY. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: WEB — WORN (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A HOLE WORN INTO CUSP WEB AT FS 220, RBL 54. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 18, 53-11-3, PAGE 49, 51-30-08, AND 53-01, FIGURE 4.
Part: PAN — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR PAN STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND ECRA 5330-02819.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND MID CARGO BAY FLOOR, LT CARGO TRACK CORRODED AROUND CLIPNUT HOLES ON LOWER SURFACE, FS 579 - 676. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT RT FS 1007 IN AFT CARGO BAY. THE SUPPORT WAS REMOVED AND A NEW SUPPORT AND REPAIR DOUBLER WERE INSTALLED IAW SRM 51-30-2, 53-01, FIGURE 2, 51-10-3, AND 51-60, FIGURE 1.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND SUB FLOOR BRACKET CRACKED AT FS 200, LBL 58. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND TOP T-CHORD OF FLOORBEAM CORRODED THE ENTIRE LENGTH AT STA 1322 LT, RT AND CENTER AISLE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 20A.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT AT RT AFT LAV CENTER AISLE, FS 1307 - 1338 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-01.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 1 INCH CRACK IN CABIN LT FLOOR SKIN AT FS 218, LBL 54. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160-200, RBL 53. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A .25 INCH CRACK IN WINDOW FRAME AT UPPER FORWARD CORNER, FS 946. AN ANGLE DOUBLER WAS INSTALLED IAW ECRA 5330-02564, SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.
Part: SKIN — CRACKED (PAX DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD ENTRY DOOR SKIN CRACKED AT LOWER EDGE. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32, 51-10-3, AND 52-05-00.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR STIFFENER IN AFT PIT CORRODED AT STA 1165, LONGERON 18L. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: FITTING — CORRODED (PAX DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND TWO R-1 DOOR GIRT BAR FITTINGS CORRODED. THE GIRT BAR FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-10-4.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LT AFT FLOORBEAM CORRODED AT STA 1338. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIGURE 20A.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A .375 INCH CRACK IN FORWARD CARGO DOOR OUTER SKIN AT EDGE OF SKIN ABOUT 3 INCHES BELOW GRAY PAINT. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHIMS WERE INSTALLED IAW SRM 52-05, FIGURE 4.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO PIT LT CABIN FLOOR SUPPORT AT TRANSITION FRAME STA 1194 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1200 - 1075. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-1, 51-10-4, 51-10-1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, RBL 44 - 54. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: PAN — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR PAN WORN AT FOUR STOPS. DOUBLER REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5330-02819, SRM 51-30-1 AND 51-30-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT L-2 DOOR, FS 1140, LBL 53. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND MID CARGO PIT FLOORBOARD SUPPORT STRUCTURE AT DOOR OPENING CORRODED WITH SURFACE CORROSION AROUND ALL CLIP NUT HOLES AT FS 636 - 693, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: SKIN — CHAFED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT CARGO DOOR OUTER SKIN LOWER FORWARD CORNER CHAFED. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-2.
Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LOWER SURFACE OF CABIN FLOORBEAM CHAFED IN AFT CARGO PIT OVERHEAD AT STA 1174. THE CHAFED AREA WAS BLENDED IAW SRM 53-05, FIGURE 86. DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-4 AND 51-10-3.
Part: ANGLE — CRACKED (WING TO BODY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 4 INCH CRACK IN WING TO FUSELAGE SUPPORT ANGLE AT STA 870. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1130, LBL 48. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LOWER SIDE OF FLOORBEAM ANGLE CHAFED IN FORWARD CARGO COMPARTMENT AT STA 370, BL 0. A NEW ANGLE AND REPAIR DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 86.
Part: GUARD — GOUGED (VENTRAL DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND LEFT SIDE OF AFT VENTRAL DOOR JAMBGOUGED AT LOWER AND UPPER LATCH. THE DOOR JAMB GUARDS WERE REMOVED AND REPLACED IAW SRM 51-30-1.
Part: PAN — WORN (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FORWARD CARGO DOOR PAN STOP WORN IN THREE PLACES. THE WORN AREAS WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5330-02819.
Part: SPAR — CRACKED (VERTICAL STAB) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A .5 INCH CRACK IN REAR SPAR VERTICAL STABILIZER RT LOWER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-3, AND 51-30-2.
Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND CORROSION UNDER PRESSURE SEAL OF LT FORWARD EMERGENCY EXIT DOOR. THE DOOR WAS REMOVED AND REPLACED IAW MM 52-21-00.
Part: SKIN — GOUGED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AT FS 487 BETWEEN LONGERON 23R & 24R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 180 - 200, RBL 44 TO RBL 8 AND AT STA 200, LBL 12. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN I/B AND CENTER TRACK AT FS 1150. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: PAN — CHAFED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND AFT OUTER EDGE OF MID CARGO DOOR PAN CHAFED AT FOUR STOPS. THREE STOPS WERE BLENDED IAW SRM 52-01. THE AFT CENTER DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND CENTER LT SEAT TRACK CORRODED AT FS 1075 - 1212. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-3.
Part: ANGLE — CRACKED (WING TO BODY) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND ANGLE CRACKED AT WING TO FILLET SUPPORT STRUCTURE AT STA 864. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: THRESHOLD — CRACKED (CARGO DOOR) · airframe 51,345 hrs · 23,585 cycles
INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FORWARD CARGO DOOR SILL AT AFT DOOR CAM SIDE. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A.
Part: BATTERY PACK — INOPERATIVE (CABIN)
THE EMERGENCY CEILING LIGHTS WOULD NOT ILLUMINATE AT STA 503 AND 900. THE BATTERY PACKS AT EACH STA WERE REMOVED AND REPLACED IAW MM 33-53-00, PAGE 407.
Earlier reports · 1995–1999 · 15 reports
1999
Part: CYLINDER — LEAKING (RT MLG)
THE RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO APPROXIMATELY 10 MINUTES FROM LANDING AT EWR. ABNORMAL PROCEDURES WERE FOLLOWED AND ALTERNATE GEAR EXTENSION WAS USED. THE LT MLG DOOR SUSTAINED DAMAGE ON LANDING. MAINTENANCE FOUND THE RT MLG BUNGEE CYLINDER LEAKING. THE RT MLG BUNGEE CYLINDER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 32-32-03. THE LT MLG DOOR WAS REMOVED AND REPLACED IAW MM 32-12-01. A GEAR RETRACTION WAS PERFORMED AND OPERATION CHECKED GOOD. IN ADDITION, THE RT ENGINE DRIVEN HYDRAULIC PUMP AND RT AUX ELECTRIC HYDRAULIC PUMP WERE REMOVED AND REPLACED.
1998
Part: SLIDE — FAILED (AFT SERV DOOR)
THE AFT GALLEY SERVICE DOOR SLIDE WAS INADVERTENTLY PULLED, BUT DID NOT DEPLOY. INSPECTION BY MAINTENANCE FOUND THE AFT GALLEY SERVICE DOOR SLIDE LANYARD PULLED AND PRESSURE AT ZERO. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-0.
Part: CABLES — OUT OF ADJUST (TAIL CONE)
TAIL CONE PULL FROM INTERIOR RELEASE HANDLE WAS LOW AT SIX POUNDS. AN ADJUSTMENT/TEST WAS PERFORMED IAW WORK CARD 08-5350-1-0008 AND PULL TEST WAS WITHIN SPECIFICATIONS AT 20 POUNDS.
Part: BRACKET — CORRODED (BS 1174)
INSPECTION FOUND ANGLE BRACKET CORRODED AT STA 1174, LONGERON 29R. A NEW ANGLE BRACKET WAS INSTALLED IAW SRM 51-10-03.
Part: BELLFRAME — CRACKED (BS 1418)
INSPECTION FOUND A 2 INCH CRACK IN BELLFRAME AT LONGERON 2R, STA 1418. THE AREA WAS REPAIRED IAW ECRA 5310-03700 AND SRM 53-03, FIGURE 32.
Part: SUPPORT COVER — BROKEN (NR 2 ENGINE)
THE FLIGHT ATTENDANT REPORTED, LIGHT SMOKE IN THE CABIN WHILE EN ROUTE. WHILE ACCOMPLISHING ABNORMAL PROCEDURES THE RT ENGINE OIL QUANTITY BEGAN TO DECREASE. THE AIRCRAFT WAS DIVERTED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE SUPPORT CASE COVER BROKEN. THE SUPPORT COVER WAS REPLACED. IN ADDITION, THE COALESCER BAGS WERE REPLACED AND A BURNOUT OF THE HIGH PRESSURE PNEUMATIC SYSTEM WAS PERFORMED IAW MM 21-20-02, PAGE 209-216.
1996
Part: BREAKER — TRIPPED (E/E COMPT)
THE A AND B CIRCUIT BREAKER FOR CENTER AFT FUEL BOOST PUMP, FORWARD LEFT FUEL PUMP, AND RECIRCULATING FAN ALL TRIPPED SHORTLY AFTER TAKEOFF. THE CIRCUIT BREAKERS WERE RESET, BUT TRIPPED AGAIN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE CIRCUIT BREAKERS WERE RESET. THE ENGINES WERE RUN AND OPERATION OF BOOST PUMP AND RECIRCULATING FAN CHECKED GOOD. THE RIGHT ENGINE GENERATOR CONNECTOR WAS REMOVED FROM FIREWALL AND THE PINS AND RECEPTACLE WERE INSPECTED WITH NO DEFECTS NOTED. MAINTENANCE FOUND NO DISCREPANCIES AND COULD NOT DUPLICATE THE FAILURE. THE B1-740 CIRCUIT BREAKER IN ELECTRICAL EQUIPMENT COMPARTMENT WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE.
Part: SKIN — DAMAGED (CARGO DR JAMB)
THE FUSELAGE SKIN AT MID-CARGO DOOR THRESHOLD AREA WAS DAMAGED BY A BELT LOADER. THE DAMAGED AREA WAS REPAIRED IAW ECRA 5330-02404.
Part: SKIN — CREASED (BS 332)
MIA - INSPECTION FOUND A 3.5 INCH LONG CREASE IN RT FUSELAGE SKIN AT STA 332. THE DAMAGED SECTION WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B. (X)
Part: FRAME — CORRODED (BS 1155)
MIA - INSPECTION FOUND FLOOR FRAME CORRODED AROUND NUTPLATES AT STA 1155. A NEW FLOOR FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-00 AND SRM 51-30-2. (X)
Part: FLOOR WEB — CORRODED (BS 180-218)
MIA - INSPECTION FOUND FLOOR WEB CORRODED BELOW FORWARD ENTRY FLOOR SUPPORT AT STA 180-STA 218. THE CORRODED AREA WAS CUT OUT AND REPAIRED IAW SRM 53-01. (X)
Part: SUPPORT ANGLE — CORRODED (BS 180-218)
MIA - INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT ANGLE CORRODED AFT OF DOOR CUTOUT, STA 180-STA 218. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SRM 51-30-2. (X)
Part: LIGHT — INOPERATIVE (FORWARD ENTRY)
FLT NR 0697 - EWR - THE PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY WOULD NOT ILLUMINATE. THE PORTABLE EMERGENCY LIGHT WAS REPLACED AND OPERATION CHECKED GOOD. (M)
1995
Part: TORQUE LINK — FAILED (LT MLG)
EWR - FLT 0364 - THE LT MLG SHUDDERED UPON TOUCH DOWN AT IAH. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MLG UPPER TORQUE LINK HAD BROKEN AND RESULTED IN ADDITIONAL DAMAGE TO THE LT MLG, P/N 59305935511. THE LT MLG WAS REMOVED AND REPLACED IAW MM 32-11-01, PAGES 405-407, AND OPERATION CHECKED GOOD. THE SDR WILL REMAIN OPEN PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED VIBRATION AS THE CAUSE OF FAILURE. AN E.A. HAS BEEN ISSUED TO MODIFY THE HYDRAULIC SHIMMY DAMPER TO CONTROL VIBRATION. AN ADDITIONAL MODIFICATION WILL BE DONE TO INSTALL RESTRICTORS ON HYDRAULIC BRAKE LINES TO CONTROL FLOW TO BRAKES AND ANTI-SKID TO PREVENT VIBRATION. (X)
Part: O-RING — LEAKING (NR 1 ENGINE)
IAH - FLT 464 - THE NR 1 ENGINE LOST OIL QUANTITY IN FLIGHT. THE OIL PRESSURE GRADUALLY DROPPED TO 20 PSI. THE ACFT WAS DIVERTED TO BNA AS A PRECAUTIONARY MEASURE. MAINTNANCE FOUND O-RING ON HIGH PRESSURE SHAFT OF NR 1 ENGINE LEAKING. THE O-RING WAS REPLACED. THE NR 1 ENGINE WAS RUN AND OPERATION CHECKED GOOD WITH NO LEAKS NOTED. (W)