N656SW
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.
315 reports on file, 1997-10-20 – 2019-11-06.
Part: RIVET — WRONG PART (BS 360)
A BRIEF DESCRIPTION OF APPARENT VIOLATION: THE MANUFACTURER (PRECISION FORM INC) HAS INCORRECTLY MARKED DIFFERENT RIVETS WHICH ARE VERY SIMILAR IN PHYSICAL APPEARANCE AND SOLD THEM TO KLX INC'S WHO THEN SOLD THEM TO STAECO. AND UNFORTUNATELY, SOME OF THESE RIVETS HAVE BEEN INSTALLED TO THE DEPARTED AIRCRAFT N656SW. WHILE STAECO PERFORM CARGO CONVERSION TO N656SW (CUSTOMER :ROSTRUM LEASING,), ACCORDING TO PEMCO (STC HOLDER)DRAWING 007-00200 SHEET 13, RIVET # BACR15CE6D7 SHOULD BE INSTALLED COMMON TO FWD JAMB AT BS 360, BETWEEN S-24L AND S-27L. FOR DETAIL LOCATION, PLEASE SEE REF/A/. DUE TO SHORTAGE OF RIVET #BACR15CE6D7, STAECO PURCHASED FROM SUPPLIER KLX INC (NOW, BOEING DISTRIBUTION SERVICES) AND USED NAS1097D6-7 INSTEAD PER SRM 51-40-03. THE RIVETS WERE PURCHASED FROM SUPPLIER KLX INC AND RECEIVED IN NOVEMBER, 2018 AND KEPT IN STORES. ON 6 NOV 2019, A MECHANIC PICKED UP A NUMBER OF THE RIVETS TO PERFORM A MODIFICATION ON AN B-REGISTERED AIRCRAFT, DURING RIVET INSTALLATION, ACCORDING TO HIS EXPERIENCE, HE FELT THE RIVETS ARE SOFTER TO FORM, AND SUSPECTED THEY MAY NOT BE THE REQUESTED TYPE OF RIVETS. AFTER A DETAILED LOOK AT THE RIVETS, HE FOUND THE PRODUCTION HEAD OF THE RIVETS HAS DIMPLE MARK ON THEM WHICH MEANS THEY ARE ACTUALLY #NAS1097AD6-7 RIVET(SEE REF/B/ FOR DETAIL). ACCORDING TO INTERNAL REPORTING PROCEDURES, HE REPORTED THE ISSUE TO QUALITY DEPARTMENT. IN RECEIPT OF THE REPORT, QUALITY ENGINEER INVESTIGATED THE ISSUE AND VERIFIED TOTALLY 6 AIRCRAFT (4 ARE B-REGISTERED, 2 ARE N-REGISTERED) MAY BE AFFECTED. AMONG THEM, ONLY ONE N-REGISTERED AIRCRAFT N656SW HAS DEPARTED FROM STAECO ON 14 SEP 2019. THE OTHER AIRCRAFT N653SW IS UNDERGOING MAINTENANCE IN STAECO AND THE INCORRECT RIVETS IS BEING REPLACED. VERIFICATION OF CEASE OF NONCOMPLIANCE: 1. ALL THE RIVETS FROM KLX INC HAVE BEEN REVIEWED AND QUARANTINED TO PREVENT FURTHER USE (TOTALLY 4 BATCHS, 1920EA, 864EA ISSUED). AND THE ISSUED RIVETS HAVE BEEN PREVENTED FOR FURTHER USE. 2. AND WE ALREADY INFORMED KLX INC THE INCIDENT AND GOT RESPONSE THAT STAECO WAS THE ONLY CUSTOMER SUPPLIED UNDER THIS BATCH OF PRODUCT IN CHINA. IMMEDIATE ACTIONS TAKEN: 3. THE AIRCRAFT N656SW IS NOT BEING OPERATED BUT FERRIED TO INDONESIA FOR MAINTENANCE. AND STAECO HAS INFORMED THE CUSTOMER TO PERFORM INSPECTION OF AFFECTED AREAS AND IDENTIFIED THE INCORRECT RIVETS USED WHICH SHALL BE REPLACED BEFORE REDELIVERY. THE CUSTOMER HAS ISSUED EO TO ADDRESS THIS ISSUE. 4. AIRCRAFT N653SW IS UNDERGOING MAINTENANCE IN STAECO AND THE INCORRECT RIVETS IS BEING REPLACED. 5. FOR THE 4 B-REGISTERED AIRCRAFT, STAECO HAS ALSO REPORTED TO CHINA CAAC AND AIRCRAFT OPERATORS FOR FURTHER ACTIONS. VERIFICATION OF EVALUATION: THE MANUFACTURER (PRECISION FORM INC) HAS INCORRECTLY MARKED DIFFERENT RIVETS WHICH ARE VERY SIMILAR IN PHYSICAL APPEARANCE. THE ERROR SHOWS THAT THE MANUFACTURER SHALL IMPROVE ITS PRODUCTION QUALITY SYSTEM. AND THE ERROR RESULTED IN THE DISAGREEMENT OF RIVETS AND THE ACCOMPANYING DOCUMENTS AND IT IS VERY HARD FOR THE DISTRIBUTOR (KLX INC) AND END USER (STAECO TX92) TO IDENTIFY THE PROBLEM. IDENTIFICATION OF RESPONSIBLE PERSON: THE ULTIMATE RESPONSIBLE PERSON IS PRECISION FORM INC AND DIRECT RESPONSIBLE PERSON IS KLX INC. ALL THE REF/A/ & REF/B/ MENTIONED SHALL BE SENT TO [email protected].
Earlier reports · 1997–2017 · 314 reports
2017
Part: LENS — UNSECURE (EXIT SIGN) · airframe 61,540 hrs · 47,706 cycles
R1 DOOR EMERGENCY EXIT SIGN FELL OFF. R&R LENS ASSEMBLY PER AMM.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 61,296 hrs · 47,534 cycles
REAR SERVICE DOOR EMERGENCY EXIT SIGN MISSING COVER PLATE. R & R THE SIGN IAW SIP.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 61,206 hrs · 47,467 cycles
FORWARD EMERGENCY LOCATOR SIGN L1086 INOP. RESEATED CONNECTOR PER WDM & MM.
Part: SKIN — CRACKED · airframe 61,206 hrs · 47,467 cycles
FORWARD RIGHT CORNER CONDITIONED AIR ACCESS PANEL CUTOUT CRACKED. REPAIRED STRUCTURE IAW SRM.
Part: LIGHT — BROKEN (ROW 1) · airframe 60,828 hrs · 47,213 cycles
RIGHT EMERGENCY LIGHT BROKEN AT ROW 1. R & R THE LIGHT IAW DWG.
Part: FLAP — WARPED (RT WING) · airframe 60,820 hrs · 47,208 cycles
RT WING OUTBOARD AFT FLAP WARPED. R&R AFT FLAP PER AMM.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,033 hrs · 46,640 cycles
RT EMERGENCY EXIT DOOR LIGHT INOP. R&R LIGHT ASSEMBLY PER AMM.
Part: SKIN — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING REAR SPAR FASTENER HOLE CRACKED, COMMON TO UPPER SKIN & CHORD AT RSS 293. REPAIRED SKIN IAW EA & DWG.
Part: SKIN — CRACKED (LT WING) · airframe 58,364 hrs · 45,540 cycles
LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AFT OF RSS 239. REPAIRED SKIN IAW ER & EA.
Part: SPAR — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING REAR SPAR UPPER CHORD, VERTICAL FLANGE CRACKED, AT FASTENER HOLE ROW RSS 251. REPAIRED FLANGE IAW EA & DWG.
Part: SPAR — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING SPAR, WEB CRACKED IN FASTENER HOLE, COMMON TO STIFFENER 8, RSS 216.5, THIRD HOLE FROM BOTTOM. REPAIRED WEB IAW EA & DWG.
Part: SKIN — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING UPPER SKIN COMMON TO SPLICE PLATE ON TE CRACKED AT RSS 239.5. REPAIRED SKIN IAW ER & EA.
Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 58,364 hrs · 45,540 cycles
LEFT ELEVATOR TAB INBD SIDE OF NR 1 HINGE CUT OUT DELAMINATED BULLNOSE SKIN. R & R TAB IAW MM & EA.
Part: SPAR — CRACKED (LT WING) · airframe 58,364 hrs · 45,540 cycles
LEFT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.
Part: SPAR — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW ER & EA.
Part: LINK — CORRODED (LT MLG) · airframe 58,364 hrs · 45,540 cycles
LEFT MLG SWING LINK CORRODED. R & R SWING LINK IAW EA.
Part: SPAR — CRACKED (RT WING) · airframe 58,364 hrs · 45,540 cycles
RIGHT WING UPPER SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW ER & EA.
Part: SPAR — CRACKED (LT WING) · airframe 58,364 hrs · 45,540 cycles
LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW EA.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 58,364 hrs · 45,540 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT APPROX STAB STATION 114. REPAIRED SKIN IAW ER & EA.
Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,360 hrs · 45,538 cycles
RIGHT WING NR 5 SLAT WEDGE DELAMINATED AT OTBD END. REPAIRED NR 5 SLAT IAW AMM.
Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,360 hrs · 45,538 cycles
RIGHT WING NR 6 SLAT TE WEDGE DELAMINATED. R & R NR 6 SLAT IAW AMM.
2015
Part: LENS — CRACKED (CABIN) · airframe 57,981 hrs · 45,301 cycles
RIGHT MID CABIN EXIT LIGHT LENS CRACKED. R & R LENS IAW MM.
Part: LENS — UNSECURE (CABIN) · airframe 57,805 hrs · 45,178 cycles
RIGHT OVERWING EMER EXIT LENS FELL OFF. REINSTALLED LENS IAW MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,935 hrs · 44,600 cycles
L1 DOOR EMER LIGHT BULB AFT INOPERATIVE. RELAMPED LIGHT IAW AMM.
Part: CASTING — CRACKED (FUSELAGE) · airframe 56,935 hrs · 44,600 cycles
L1 DOOR UPPER HINGE CASTING CRACKED AT THE LOWER CORNER. REMOVED CASTING IAW SRM & DWG.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,935 hrs · 44,600 cycles
LEFT WING INBD FLAP, FORE FLAP TOP SURFACE DELAMINATED APPROX 36" INBD OF OTBD EDGE. REPAIRED FORE FLAP IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,935 hrs · 44,600 cycles
FORWARD ENTRY DOOR, UPPER HINGE CUT OUT CRACKED AT BS 304, STRINGER 10L. REPAIRED CUT OUT IAW EA.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,935 hrs · 44,600 cycles
AFT CARGO PIT VERTICAL ANGLE CORRODED AT BS 794, RBL 7. R & R ANGLE IAW SRM.
Part: PANEL — CRACKED (NLG WW) · airframe 56,935 hrs · 44,600 cycles
RIGHT NOSE WHEEL WELL PANEL AT BS 239, JUST BELOW PANEL 3103R CRACKED. REPAIRED WEB IAW SRM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,296 hrs · 44,149 cycles
L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.
Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 56,189 hrs · 44,075 cycles
RIGHT WING TO BODY FAIRING FWD OF WW DELAMINATED. R & R FAIRING IAW SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 55,733 hrs · 43,772 cycles
R1 DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.
Part: LENS — LOOSE (CABIN) · airframe 55,332 hrs · 43,505 cycles
R2 DOOR EMER LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.
2014
Part: LENS — MISSING (CABIN) · airframe 54,687 hrs · 43,064 cycles
LEFT OVERHEAD BIN EMER EXIT LIGHT LENS COVER MISSING AT ROW 18. INSTALLED LENS COVER IAW SIP.
Part: PANEL — LOOSE (CABIN) · airframe 54,631 hrs · 43,026 cycles
LEFT EMER LIGHTING PANEL LOOSE AT ROW 17. SECURED PANEL IAW SIP.
Part: GAUGE — INOPERATIVE (EVAC SLIDE) · airframe 54,437 hrs · 42,893 cycles
L1 DOOR EMER EVAC SLIDE PRESS GAUGE INOPERATIVE. R & R SLIDE IAW MT.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,326 hrs · 42,811 cycles
L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 54,226 hrs · 42,739 cycles
PRESSURE BULKHEAD OUTER WEB OIL CANNING AT BS 1016 BETWEEN STRINGER 6R TO 7R. REPAIRED WEB IAW SRM & EA.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,226 hrs · 42,739 cycles
BULKHEAD WEB CRACKED AT BS 1016 STRINGER 2R. REPAIRED WEB IAW EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
STRINGER CLIP AT CRACKED AT BS 727A STRINGER 5R. R & R CLIP IAW SRM & DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
STRINGER CLIP CRACKED AT BS 450 STRINGER 14L. R & R CLIP IAW DWG & SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
STRINGER CLIP CRACKED AT BS 887 STRINGER 13L. R & R CLIP IAW DWG & SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
SKIN CRACKED AT BS 847 STRINGER 14L. REPAIRED SKIN IAW EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
STRINGER CLIP CRACKED AT BS 747 STRINGER 13L. R & R CLIP IAW DWG.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 400+10 WINDOW FRAME CRACKED AT HOLES 5 & 6. R & R FRAME IAW DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 887+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 767+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 807+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 787+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 727+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.
Part: STRAP — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
STRAP CRACKED BETWEEN BS 343 TO 348 STRINGER 16L. R & R STRAP IAW SRM & DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 727E+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB & TC.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 500A+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 500C+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 440+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 847+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 500C+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 400+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 400+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 500A+10 UPPER FWD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 420+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 400+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 440+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 380+10 UPPER FWD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 500B+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 520+10 LOWER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 420+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 500B+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUT OUT. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
RIGHT BS 480+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,075 hrs · 42,633 cycles
LEFT BS 500A+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,053 hrs · 42,617 cycles
L1 DOOR SLIDE OUT OF POSITION. ADJUSTED SLIDE IAW MM.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,294 hrs · 42,088 cycles
LEFT WING OTBD AFT FLAP LOWER SURFACE DELAMINATED AT INBD SIDE. R & R AFT FLAP IAW MM.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 53,117 hrs · 41,978 cycles
FORWARD FLASHLIGHT STRAP BROKEN. R & R STRAP IAW SIP.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,659 hrs · 41,656 cycles
SKIN CRACKED AT BS 727B+12 STRINGER 10R. REPAIRED SKIN IAW EA.
2013
Part: INDICATOR — FAULTY (COCKPIT) · airframe 5,241 hrs · 41,484 cycles
DECLARED EMERGENCY WHEN FLAPS PLACED TO "25" POSITION, INDICATOR SHOWED APPROXIMATELY 15 & 20 & NO ROLL NOTED. R & R FLAP POSITION INDICATOR IAW MM.
Part: ACTUATOR — FAULTY (RT MLG) · airframe 51,622 hrs · 40,944 cycles
AIR TURN BACK DECLARED EMERGENCY. RT MAIN GEAR LIGHT REMAINED ON AFTER GEAR LEVER IN OFF POSITION LIGHT WAS RED INDICATION DISAGREEMENT LIGHT. WENT OFF IAW QRH WHEN POSITIONED IN THE UP POSITION. R&R RT NLG UPLOCK ACTUATOR IAW MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,492 hrs · 40,843 cycles
LT EMERGENCY EXIT LIGHT JUST AFT OF WING TO BODY FAIRING INOPERATIVE. R&R LIGHT IAW AMM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM CRACKED AT BS 616, RBL 45.5. REPAIRED FLOOR BEAM IAW SWA EA.
Part: BEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STUB BEAM CRACKED AT BS 616, STRINGER 17R. REPAIRED BEAM IAW SWA EA.
Part: FITTING — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
ELECTRONIC ACCESS DOOR ELECTRONICS EQUIPMENT COMPARTMENT TRACK AFT FITTING CRACKED. R&R FITTING IAW DRAWING & SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
E/E COMPARTMENT ACCESS DOOR FWD FITTING CRACKED. R&R FITTING IAW SRM & DRAWING.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
RT CHORD CRACKED AT BS 178, BELOW WL 207. REPAIRED CHORD IAW EA.
Part: TRACK — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
ELECTRONIC COMPARTMENT ACCESS DOOR AFT POSITION TRACK CRACKED. R&R TRACK IAW SRM & DRAWING.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
LT CHORD CRACKED AT BS 178, AT WL 184. REPAIRED CHORD IAW EA.
Part: BEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STUB BEAM CRACKED AT BS 706, RBL 57.5. R&R STUB BEAM IAW SRM & DRAWING.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STUB FRAME CRACKED AT BS 616, STRINGER 17R. REPAIRED FRAME IAW SWA EA.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 400, STRINGER 25L. R&R TIE CLIP IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 380, STRINGER 21L. R&R TIE CLIP IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 380, STRINGER 22L. R&R TIE CLIP IAW SRM & DRAWING.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
RT FS FRAME CRACKED AT BS 188, WL 207.5. REPAIRED FRAME IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
LT FRAME CRACKED AT BS 188, WL 207.5. REPAIRED FRAME IAW SRM & DRAWING.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 360, BETWEEN STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW SRM.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SUPPORT BRACKET CRACKED AT BS 927, STRINGER 12L. R&R BRACKET IAW SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
CLIP CRACKED AT BS 294.5, STRINGER 23L. R&R CLIP IAW SRM & DRAWING.
Part: REVEAL — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FWD ENTRY CUT OUT AFT LOWER CORNER REVEAL CRACKED. R&R REVEAL IAW SRM & DRAWING.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRINGER SPLICE CRACKED AT BS 360, STRINGER 4R. R&R SPLICE IAW SRM & DRAWING.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED BETWEEN BS 312 & BS 328, RBL 32. REPAIRED WEB IAW SRM & DRAWING.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
UNDER FLOOR STRUCTURE FWD LAVATORY AREA STRAP CRACKED AT BS 328+2, LBL 48. R&R STRAP IAW SRM & DRAWING.
Part: FITTING — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
CLIP CRACKED AT BS 559, STRINGER 11L. R&R CLIP IAW SRM & DRAWING.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED BETWEEN BS 344 & BS 360, BL 0. R&R WEB IAW DRAWING.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB ANGLE CRACKED BETWEEN BS 344 & BS 360, LBL 12. R&R ANGLE IAW SRM & DRAWING.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
UNDER FLOOR STRUCTURE FWD GALLEY AREA STRAP CRACKED AT BS 312+14, RBL 32. R&R STRAP IAW SRM & DRAWING.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
UNDER FLOOR STRUCTURE STRAP CRACKED AT BS 312+3, BL 0. R&R STRAP IAW SRM & DRAWING.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM CRACKED AT BS 328, BETWEEN LBL 22 & LBL 37. REPAIRED BEAM IAW SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM UPPER FLANGE CRACKED AT BS 312, RBL 24. REPAIRED FLANGE IAW SRM.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
UNDER FLOOR STRUCTURE FWD GALLEY AREA STRAP CRACKED AT BS 312+1, RBL 46. R&R STRAP IAW SRM & DRAWING.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SPLICE CRACKED AT BS 907, STRINGER 4R. R&R SPLICE IAW SRM & DRAWING.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
UNDER FLOOR STRUCTURE FWD LAVATORY STRAP CRACKED AT BS 312+2, LBL 12. R&R STRAP IAW SRM & DRAWING.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SUPPORT ANGLE CRACKED BETWEEN BS 887-BS 907, RBL 45.5. R&R ANGLE IAW SRM & DRAWING.
Part: BEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STUB BEAM CRACKED AT BS 706, RBL 46. R&R STUB BEAM IAW SRM & DRAWING.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRINGER SPLICE CRACKED AT BS 907, STRINGER 4L. R&R CHANNEL IAW SRM & DRAWING.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 294.5+2, RBL 63. R&R WEB IAW SRM.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 695, RBL 62. R&R WEB IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 578, STRINGER 11R. R&R CLIP IAW SRM & DRAWING.
Part: SKIN — CRACKED (SERVICE DOOR) · airframe 51,342 hrs · 40,730 cycles
FWD SERVICE DOOR AFT LOWER CORNER CRACKED AT FASTENER HOLE. REPAIRED SKIN IAW SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW EA & ACO.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRINGER SPLICE CORRODED BETWEEN BS 847 - BS 867, STRINGER 23R. REPAIRED SPLICE IAW SRM.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FWD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 380, STRINGER 26L. R&R ANGLE IAW SRM & DRAWING.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM SPLICE ANGLE CORRODED AT BS 328, RBL 58. R&R ANGLE IAW SRM & DRAWING.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA.
Part: WEB — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CORRODED BETWEEN BS 747 TO BS 767, STRINGER 17R. R&R WEB IAW SRM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 663.75, STRINGER 10L. R&R TIE CLIP IAW SRM & DRAWING.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SUPPORT PLATE CRACKED AT BULKHEAD BS 1016, LBL 9. R&R INTERCOSTAL IAW SRM & DRAWING.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM CRACKED AT BS 947.5, LBL 53. REPAIRED FLOOR BEAM IAW SWA EA.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 663.75, STRINGER 10R. R&R TIE CLIP IAW SRM & DRAWING.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
ANGLE CRACKED BETWEEN BS 291.5-BS 277, BETWEEN STRINGER 10R-STRINGER 11R.. R&R ANGLE IAW SRM & DRAWING.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STUB FRAME CRACKED AT BS 294.5, STRINGER 7R. REPAIRED FRAME IAW SWA EA.
Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING TE SUPPORT ANGLE CRACKED AT WS 537.872. R&R ANGLE IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 706, STRINGER 11R. R&R TIE CLIP IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 360, STRINGER 7L. R&R TIE CLIP IAW SRM & DRAWING.
Part: ANGLE — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING TE ANGLE CRACKED AT WS 537.872. R&R ANGLE IAW SRM & DRAWING.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FLOOR BEAM CORRODED AT BS 986.5, LBL 5. REPAIRED BEAM IAW SRM.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRAP CRACKED AT BS 351.2, STRINGER 16L. R&R STRAP IAW SRM & DRAWING.
Part: BRACKET — CRACKED (L1 DOOR) · airframe 51,342 hrs · 40,730 cycles
L1 DOOR FWD LOWER EDGE BRACKET CRACKED. R&R ANGLE IAW SRM & DRAWING.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 706, STRINGER 11L. R&R TIE CLIP IAW SRM & DRAWING.
Part: RIB — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING RIB CRACKED AT WBL 135.5, BETWEEN STRINGER 2 & STRINGER 3. REPAIRED RIB IAW SWA EA.
Part: PLATE — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING TE PLATE CRACKED AT WBL 179. R&R PLATE IAW SRM & DRAWING.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 520+ 7, BETWEEN STRINGER 22R-STRINGER 24R. R&R WEB IAW SRM & DRAWING.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
LT FWD WING TO BODY FAIRING STRUCTURE ANGLE CRACKED AT BS 540, BETWEEN STRINGER 21L & STRINGER 22L. REPAIRED ANGLE IAW SRM & DRAWING.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 787, BETWEEN STRINGER 27R-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: ANGLE — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING TE ANGLE CRACKED AT WBL 204.40. R&R ANGLE IAW SRM & DRAWING.
Part: SKIN — CRACKED (RT WING) · airframe 51,342 hrs · 40,730 cycles
RT WING LE SKIN CUTOUT CRACKED AT WBL 157. REPAIRED SKIN IAW EA.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 727D, BETWEEN STRINGER 27L-STRINGER 27R. REPAIRED FRAME IAW SRM.
Part: WEB — CRACKED (FAIRING) · airframe 51,342 hrs · 40,730 cycles
LT FORWARD WING TO BODY FAIRING STRUCTURE WEB CRACKED AT BS 520+6, BETWEEN STRINGER 22L- STRINGER 24L. R&R WEB IAW SRM & DRAWING.
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,342 hrs · 40,730 cycles
LT WING TE SUPPORT ANGLE CRACKED AT RSS 537.806. R&R ANGLE IAW SRM & DRAWING.
Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
MAIN WW PRESSURE DECK CRACKED AT BS 672.5, LBL 42.5. REPAIRED WEB IAW EA.
Part: STRAP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRAP CRACKED AT BS 663, LBL 41. R&R STRAP IAW DRAWING & SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28R-STRINGER 27R. R&R SHEAR TIE IAW SRM & DRAWING.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
ATTACH ANGLE CRACKED AT BS 500C, STRINGER 26L. R&R ANGLE IAW SRM & DRAWING.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
STRINGER CLIP CRACKED AT BS 500B, S22L. R & R STRINGER CLIP IAW SRM AND DWG.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FWD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 500A - BS 500B, STRINGER 26R. R&R WEB IAW SRM & DRAWING.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28L-STRINGER 27L. R&R SHEAR TIE IAW SRM & DRAWING.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28R-STRINGER 28L. R&R SHEAR TIE IAW SRM & DRAWING.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SUPPORT ANGLE CRACKED BETWEEN BS 380 - BS 400, BL 0. R&R ANGLE IAW SRM & DRAWING.
Part: PLATE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FWD CARGO DOOR PLATE CRACKED AT BS 492.4, BETWEEN STRINGER 25R-STRINGER 26R. R&R PLATE IAW SRM & DRAWING.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 767+5, STRINGER 25R. R&R ANGLE CLIP IAW SRM & DRAWING.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SUPPORT ANGLE CRACKED AT BS 807, STRINGER 25R. R&R ANGLE IAW SRM & DRAWING.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 727E, BETWEEN STRINGER 26L-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 787, STRINGER 20R. R&R TIE CLIP IAW SRM & DRAWING.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FS FRAME CRACKED AT BS 400, BETWEEN STRINGER 26L & STRINGER 27L. REPAIRED FRAME IAW SWA EA.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, LBL 6.5. REPAIRED STIFFENER IAW SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, RBL 6.5. R&R STIFFENER IAW SRM & DRAWING.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FS FRAME CRACKED AT BS 400, BETWEEN STRINGER 24L & STRINGER 28L. REPAIRED FRAME IAW SWA EA.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 767, BETWEEN STRINGER 27R-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
CENTER WING BOX LONGITUDINAL FLOOR BEAM LOWER CHORD STIFFENER CRACKED AT BS 663, RBL 24.8. REMOVED STIFFENER IAW SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 867, BETWEEN STRINGER 27R-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FS FRAME CORRODED AT BS 807, BETWEEN STRINGER 25L & STRINGER 26L. REPAIRED FRAME IAW SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 787, BETWEEN STRINGER 27L-STR 26L. REPAIRED FRAME IAW SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 747, BETWEEN STRINGER 26L-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 28L- STRINGER 28R. R&R SHEAR TIE IAW SRM & DRAWING.
Part: FRAME — CORRODED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME CORRODED AT BS 807, BETWEEN STRINGER 27R-STRINGER 27L. REPAIRED FRAME IAW SRM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
TIE CLIP CRACKED AT BS 727A, STR 25L. R&R TIE CLIP IAW SRM AND DWG.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
LONGITUDINAL FLOOR BEAM LOWER CHORD CRACKED AT BS 662, LBL 24.8. R&R CHORD IAW SRM & DRAWING.
Part: LENS — CRACKED (EXIT SIGN) · airframe 51,342 hrs · 40,730 cycles
FWD LAVATORY EMERGENCY EXIT SIGN LENS ON LOWER SIDE CRACKED. R&R LENS IAW AMM.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 707, BBL 0.07. REPAIRED WEB IAW EO.
Part: LENS — CRACKED (EXIT SIGN) · airframe 51,342 hrs · 40,730 cycles
FWD GALLEY EMERGENCY EXIT SIGN LENS CRACKED. R&R LENS IAW AMM.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 708, BBL 0.07. REPAIRED WEB IAW EO & EA.
Part: STRAP — CRACKED (LT MLG WW) · airframe 51,342 hrs · 40,730 cycles
LT WW AFT POSITION MLG SUPPORT STRAP CRACKED. R&R STRAP IAW SRM & DRAWING.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT STATION 666, LBL 24.8 CENTER WING BOX. REPAIRED CHORD IAW EA.
Part: WEB — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
WEB CRACKED AT BS 710.5, BBL 0.07. REPAIRED WEB IAW EO & EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FS FRAME CRACKED AT BS 947, STRINGER 25R. REPAIRED FRAME IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FRAME OTBD CHORD CRACKED AT BS 727, BETWEEN STRINGER 17L TO STRINGER 27. R&R CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 51,342 hrs · 40,730 cycles
FS FRAME CRACKED AT BS 727, STRINGER 18A RT. REPAIRED FRAME IAW SRM & SWA EA.
Part: LENS — MISSING (EXIT SIGN) · airframe 50,670 hrs · 40,242 cycles
FWD ENTRY FLOOR LEVEL EXIT SIGN LENS MISSING. INSTALLED LENS PER AMM.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 50,625 hrs · 40,215 cycles
PHOTO LUMINSCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHT LOOSE. SECURED EEPLS PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,411 hrs · 40,065 cycles
FORWARD SERVICE DOOR SLIDE FELL OUT WHEN SERVICE DOOR OPENED. RE-INSTALLED SLIDE PER MT.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 49,912 hrs · 39,703 cycles
RIGHT OVERWING EMERGENCY EXIT LIGHT AND SEVERAL CABIN BULL NOSE EMERGENCY EXIT LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK IAW M/M.
2012
Part: HINGE — BROKEN (RT SPOILER) · airframe 49,266 hrs · 39,242 cycles
RIGHT WING I/B GROUND SPOILER O/B CENTER HINGE BROKEN. REMOVED AND REPLACED SPOILER PER AMM.
Part: LENS — MISSING (CABIN) · airframe 48,988 hrs · 39,032 cycles
LEFT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER M/M.
Part: SPINDLE — CORRODED (TE FLAP) · airframe 48,855 hrs · 38,933 cycles
LEFT WING NR 1 SPINDLE CORRODED. REMOVED & REPLACED NR 1 SPINDLE ASSY PER MT.
Part: LENS — LOOSE (CABIN) · airframe 48,539 hrs · 38,698 cycles
FWD EEPLS LENSES LOOSE. SECURED LENS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,390 hrs · 37,804 cycles
LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY HOUSING PACK PER M/M.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,390 hrs · 37,804 cycles
LT OVERWING EXERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY HOUSING PACK PER M/M.
Part: SKIN — PUNCTURED (TE FLAP) · airframe 47,243 hrs · 37,690 cycles
LT WING I/B FOREFLAP PUNCTURED ON LOWER SURFACE. REMOVED AND REPLACED FORE FLAP PER M/M.
Part: COVER — MISSING (EXIT SIGN) · airframe 46,931 hrs · 37,472 cycles
OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED SIGN PER MM.
2011
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles
DURING SCHEDULED 14Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles
DURING SCHEDULED 14Y CHECK FOUND, LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB IAW EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 11. REPAIRED SHEAR TIE PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles
DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD PER EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles
DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER EA.
Part: LENS — MISSING (CABIN) · airframe 45,190 hrs · 36,107 cycles
DURING SCHEDULED MV1 CHECK FOUND, RT EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,527 hrs · 35,609 cycles
DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
Part: SKIN — PUNCTURED (FOREFLAP) · airframe 44,128 hrs · 35,307 cycles
DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED AT LOWER SURFACE I/B END. REPAIRED FORE FLAP PER SRM.
Part: LENS — LOOSE (CABIN) · airframe 44,154 hrs · 35,326 cycles
RT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 19. SECURED LENS PER MM.
2010
Part: WEDGE — DELAMINATED (LE SLAT) · airframe 43,757 hrs · 35,039 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT I/B END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,422 hrs · 34,782 cycles
LT FWD EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,994 hrs · 34,445 cycles
DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,923 hrs · 33,616 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED PER MM.
2009
Part: ATTACH FITTING — BROKEN (SPOILER) · airframe 40,582 hrs · 32,566 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND NR 5 GRND SPOILER OUTBOARD ATTACH FITTING BROKEN. REMOVED AND REPLACED NR 5 SPOILER ASSY PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,582 hrs · 32,566 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING SNUBBER CUTOUT SKIN WEB CRACKED AT LBL 7.75. REPAIRED WEB PER ACO.
Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING SNUBBER CUTOUT SKIN WEB CRACKED AT RBL 7.75. REPAIRED WEB PER ACO.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,318 hrs · 32,369 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,457 hrs · 31,731 cycles
DURING SCHEDULED SPV CHECK, FOUND LT CENTER EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLAT — CRACKED (LT WING) · airframe 39,457 hrs · 31,731 cycles
DURING SCHEDULED SPV CHECK, FOUND LT WING L/E NR 3 SLAT O/B END CRACKED. REPAIRED SLAT PER SRM.
Part: SLAT — CRACKED (RT WING) · airframe 39,457 hrs · 31,731 cycles
DURING SCHEDULED SPV CHECK, FOUND RT WING L/E NR 6 SLAT O/B END CRACKED. REPAIRED SLAT PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,625 hrs · 31,138 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
2008
Part: FLAP — DELAMINATED (RT WING) · airframe 37,467 hrs · 30,330 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 37,261 hrs · 30,176 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27L. REPAIRED FRAME PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 37,261 hrs · 30,176 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27L. REPAIRED FRAME PER SRM.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 36,489 hrs · 29,614 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,236 hrs · 29,428 cycles
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,039 hrs · 29,276 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 36,030 hrs · 29,267 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LENS — OUT OF POSITION (CABIN) · airframe 35,547 hrs · 28,916 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.
2007
Part: STRAP — CORRODED (SPAR) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER AFT SPAR UPPER STRAP CORRODED. REPAIRED STRAP PER SRM.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STABILIZER FWD ATTACH FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.
Part: BEARING — WORN (LT ELEVATOR) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED HORN BEARING PER MM.
Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER BOEING SB.
Part: TORQUE TUBE — FAILED (RT ELEVATOR) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 STR 8L. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 787 S8L) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 727D S8L) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 480 S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 747 S8L) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 500A S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 440) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (BS 500C S8R) · airframe 33,969 hrs · 27,716 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.
Part: GLOWSTRIP — WORN (CABIN) · airframe 33,146 hrs · 27,041 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 ABC. REMOVED AND REPLACED STRIP PER MM.
2006
Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 31,363 hrs · 25,637 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,240 hrs · 25,543 cycles
DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 31,240 hrs · 25,543 cycles
DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER MM.
Part: HOOK — LOOSE (R1 DOOR) · airframe 30,691 hrs · 25,100 cycles
R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.
Part: HOOK — LOOSE (R1 DOOR) · airframe 30,682 hrs · 25,092 cycles
FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER MM.
Part: SKIN — DELAMINATED (LT WING TE FLAPS) · airframe 30,423 hrs · 24,879 cycles
DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.
Part: LENS — DISLODGED (EMERGENCY EXIT) · airframe 29,344 hrs · 24,033 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER MM.
2005
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,016 hrs · 23,011 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 25,996 hrs · 21,410 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 25,973 hrs · 21,391 cycles
DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,973 hrs · 21,391 cycles
DURING SCHEDULED C1 CHECK, FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 25,724 hrs · 21,187 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 787, LBL 51.5. REPAIRED FRAME PER SWA EA.
Part: WINDOW — ARCED (COCKPIT) · airframe 25,716 hrs · 21,175 cycles
DURING SCHEDULED RON CHECK, FOUND R2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,194 hrs · 20,733 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,068 hrs · 20,653 cycles
DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
2004
Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 24,824 hrs · 20,475 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E AFT FLAP PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,079 hrs · 19,885 cycles
DURING SPV, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 13 ABC, 17 ABC, INOP. RELAMPED LIGHTS PER MM.
Part: GLOWSTRIP — WORN (CABIN) · airframe 24,095 hrs · 19,885 cycles
DURING SPV, FOUND PHOTOLUMINESCENT STRIPS AT ROW 20 ABC, 20 DEF, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.
Part: SLIDE — DISLODGED (R1 DOOR) · airframe 23,718 hrs · 19,597 cycles
R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.
Part: LENS — MISSING (R1 DOOR SLIDE) · airframe 23,421 hrs · 19,343 cycles
R1 DOOR EVAC SLIDE CONTAINER MISSING GAUGE LENS. REPLACED LENS PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,206 hrs · 19,187 cycles
DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,179 hrs · 19,166 cycles
DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,152 hrs · 19,143 cycles
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,920 hrs · 18,957 cycles
DURING SCHEDULED PM CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,907 hrs · 18,950 cycles
R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 22,875 hrs · 19,834 cycles
DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,702 hrs · 18,973 cycles
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,519 hrs · 18,653 cycles
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,500 hrs · 18,636 cycles
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,271 hrs · 18,445 cycles
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
2003
Part: LIGHT — WORN (CABIN) · airframe 21,366 hrs · 17,726 cycles
DURING SCHEDULED C4 CHECK, FOUND EELPS TRACK STRIPS WORN. REMOVED AND REPLACED EELPS TRACK STRIPS PER MM.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 21,166 hrs · 17,581 cycles
R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 20,947 hrs · 17,408 cycles
FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 20,441 hrs · 16,987 cycles
DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 20,434 hrs · 16,981 cycles
DURING SCHEDULED C3 CHECK, FOUND RT INBD T/E FOREFLAP DELAMINATED AT LOWER OUTBD CORNER. REMOVED AND REPLACED RT INBD T/E FOREFLAP PER MM.
Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 19,524 hrs · 16,248 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 18,598 hrs · 15,529 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: LENS — LOOSE (MID CABIN) · airframe 18,592 hrs · 15,524 cycles
DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
2002
Part: PIN — CORRODED (LT/RT MLG) · airframe 18,080 hrs · 15,127 cycles
DURING SCHEDULED PM CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.
Part: TRACK — LOOSE (CABIN) · airframe 17,796 hrs · 14,907 cycles
EEPLS PULLED UP AT CABIN FLOOR. REINSTALLED EEPLS PER MM.
Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 17,681 hrs · 14,822 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: COVER — DAMAGED (CABIN) · airframe 17,630 hrs · 14,783 cycles
EEPLS TRACK COVER PEELED OFF AT ROWS 21 AND 22.
Part: PUMP — INTERMITTENT (NR 1 FUEL TANK) · airframe 17,554 hrs · 14,721 cycles
DIVERSION, DURING CLIMB NR 1 FUEL TANK FWD BOOST PUMP LOW PRESS LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED NR 1 FUEL TANK FWD BOOST PUMP AND P-5 PANEL PER MM.
Part: TRACK — DISLODGED (CABIN) · airframe 17,554 hrs · 14,721 cycles
PHOTO LUMINESCENT STRIP DISLODGED IN CABIN. REATTACHED STRIP PER MM.
Part: CONNECTOR — DAMAGED (NR 1 ENGINE) · airframe 16,719 hrs · 14,024 cycles
AIRTURN BACK, INFLIGHT SHUTDOWN, OVERTEMP ON NR 1 ENG EGT WENT TO 1200 DEGREES DURING CLIMB AT 33,000 FT. RETARDED THROTTLE TO IDLE, EGT IND WENT BLANK BUT RED LIGHT REMAINED ILLUMINATED UNTIL ENG WAS SHUT DOWN. FOUND EGT CONNECTOR D1208P DAMAGED. REMOVED AND REPLACED EGT CONNECTOR D1208P PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 16,702 hrs · 14,008 cycles
EEPLS LOOSE AT ROW NR 13. SECURED EEPLS PER MM.
Part: COVER — CRACKED (CABIN) · airframe 16,667 hrs · 13,957 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S NR 4, 10, 14, 16, 17, 22 AND 23. REMOVED AND REPLACED COVERS PER MM.
2001
Part: BUSHING — LOOSE (ELEVATOR) · airframe 13,819 hrs · 11,750 cycles
DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR NR 6 HINGE BEARING PLATE BUSHINGS MIGRATED. REMOVED AND REPLACED BEARING PLATE PER MM.
Part: FLAP — DELAMINATED (RH WING) · airframe 13,819 hrs · 11,750 cycles
DURING SCHEDULED C4 CHECK, FOUND OTBD T/E FLAP DELAMINATED AT INBD CORNER. R&R FLAP PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 13,591 hrs · 11,556 cycles
EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM.
Part: TRACK — LOOSE (CABIN) · airframe 13,266 hrs · 11,272 cycles
EEPLS TRACK LOOSE. SECURED EEPLS PER MM.
Part: WIRE — EXPOSED (CABIN) · airframe 11,741 hrs · 9,999 cycles
EEPLS WIRING EXPOSED AT ROW 2. SECURED TRACK COVER PER MM.
2000
Part: COVER — LOOSE (CABIN) · airframe 10,865 hrs · 9,307 cycles
EEPLS COVER LOOSE AT ROW 14. SECURED EEPLS PER MM.
Part: WINDOW — UNSECURED (COCKPIT)
ABORTED TAKEOFF, F/O'S SLIDING WINDOW OPENED DURING TAKEOFF. DISCOVERED WINDOW NOT LATCHED PROPERLY. CLOSED AND LATCHED WINDOW PER MM. OPS CK GOOD.
1999
Part: SLIDE — OUT OF POSITION (SERVICE DOORWAY)
AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
1997
Part: ENGINE — FAILED (NR 1)
AFTER LEVELING OFF AT FL 330, CREW NOTED NR 1 ENGINE OIL PRESSURE FLUCTUATING SLIGHTLY AS THRUST REDUCED. IN ADDITION, AVM INDICATION SPIKED UP 2 UNITS, THEN RETURNED TO LESS THAN 1 UNIT. A FEW MINUTES LATER, A LOUD BOOM WAS HEARD FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. CREW DECLARED AN EMERGENCY, AND MADE AN UNEVENTFUL LANDING AT BNA. INSPECTED AND FOUND METAL PIECES INSIDE FAN COWL. FURTHER INSPECTION FOUND A HOLE IN ENGINE ACCESSORY GEARBOX JUST AFT OF STARTER PAD. ENGINE CHANGE IN PROGRESS.