N905WN
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.
116 reports on file, 2009-10-28 – 2020-10-29.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 43,114 hrs · 25,940 cycles
EXIT LIGHTS CENTER OVERHEAD, LEFT OVERWING, AND ROW 6 LEFT ARE OUT. ALLOWED MORE TIME FOR BATTERIES TO RECHARGE AND PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST, PER AMM 33-51-00-710-801, CHECKED GOOD.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 43,114 hrs · 25,940 cycles
PANEL 242AF HAS DAMAGE AT AFT EDGE. REPAIRED DAMAGE AT AFT EDGE ON PANEL 242AF, IAW SRM 53-00-50-2R-10.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
RT BS 663 VAPOR BARRIER HAS A VERTICAL CRACK 1' FROM OUTBOARD EDGE, 8' FROM TOP EDGE. RT BS 663 VAPOR BARRIER VERTICAL CRACK 1' FROM OUTBOARD EDGE, 8' FROM TOP EDGE WAS REPAIRED, IAW SRM 51-70-04-2R-10 56144U 10/14/2020.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,114 hrs · 25,940 cycles
FLOOR PANEL 231ZF HAS AREA OF DELAMINATION AT AFT EDGE. REPAIRED DELAMINATION AT AFT EDGE ON FLOOR PANEL 231ZF, IAW SRM 53-00-50-2R-10.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,114 hrs · 25,940 cycles
FLOOR PANEL 241BF HAS 2 AREAS OF DELAMINATION AT FWD AND OUTBOARD EDGES. REPAIRED 2 AREAS OF DELAMINATION AT FWD AND OUTBOARD EDGES ON FLOOR PANEL 241BF, IAW SRM 53-00-50-2R-10.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,114 hrs · 25,940 cycles
FLOOR PANEL 231YF HAS AREA OF DELAMINATION AT AFT EDGE. REPAIRED AREA OF DELAMINATION AT AFT EDGE ON FLOOR PANEL 231YF, IAW SRM 53-00-50-2R-10.
Part: BULKHEAD — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
ANGLE COMMON TO UPPER EDGE OF LT BS 663 VAPOR BARRIER IS CRACKED AT LBL 8.5. REPAIRED ANGLE COMMON TO UPPER EDGE OF LT BS 663 VAPOR BARRIER, PER SRM 57-10-10-2R-5 REP 5.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 43,114 hrs · 25,940 cycles
FLOOR PANEL 232SF HAS AREA OF DELAMINATION AT AFT EDGE. REPAIRED DELAMINATION AT AFT EDGE ON FLOOR PANEL 232SF, IAW SRM 53-00-50-2R-10.
Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 43,114 hrs · 25,940 cycles
RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. REMOVED RIGHT HAND HORIZONTAL STABILIZER FWD UPPER SLIDE SEAL PLATE, IAW AMM 53-31-31-000-802 STEP 2D AND E. 56260U 15OCT20. INSTALLED RT HORIZ STAB FWD UPPER SLIDE SEAL PLATE, IAW AMM 53-31-31-400-802 STEP 3E 56260U 15OCT20.
Part: FASTENER — LOOSE (LT WING TE) · airframe 43,114 hrs · 25,940 cycles
LEFT WING TRAILING EDGE TWO LOOSE FASTENERS ARE CHAFING ON DEFLECTION RIB UPPER ATTACH TAB ORSS279. TRIMMED OUT THE DAMAGE PART OF THE DEFLECTION CONTROL RIB UPPER TAB AND INSTALLED REPAIR PARTS, IAW SRM 57-51-02-2R-4 88920U 30OCT20.
Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 43,114 hrs · 25,940 cycles
LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. REMOVED LT HORIZONTAL STABILIZER FWD UPPER SLIDE PLATE, IAW AMM 53-31-31-000-802 STEP 2D AND E. REPLACED LT HORIZONTAL STABILIZER FWD UPPER SLIDE SEAL PLATE, IAW AMM 53-31-31-400-802 STEP 3E 56260U 15OCT20.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
LT WHEEL WELL VAPOR BARRIER IS CRACKED AT BS 663 LBL 45 WL 152 TO LBL48 WL 149. REPAIRED CRACK ON LT WHEEL WELL VAPOR BARRIER AT BS 663 45L 152 TO LBL 48 WL 149, PER SRM 51-70-04-2R-0 AND SRM 51-70-04-2R-10.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
RT WHEEL WELL VAPOR BARRIER IS CRACKED AT BS 663 RBL 45 WL 152 TO RBL48 WL 149. REPAIRED RT WHEEL WELL VAPOR BARRIER, IAW SRM 51-70-04-2R-10.
Part: SKIN — DENTED (BS 1024) · airframe 43,114 hrs · 25,940 cycles
FUSELAGE SKIN HAS A DENT AT BS 1024 BETWEEN STR 15L-16L. FUSELAGE SKIN DAMAGE AT BS 1024 BETWEEN STR 15L-16L REPAIRED, PER SRM 53-80-01-2R-5. CATEGORY A REPAIR NO FURTHER ACTION REQUIRED.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
RT WHEEL WELL VAPOR BARRIER IS CRACKED AT BS 663 RBL 45 WL 152 TO RBL 48 WL 149 AND REQUIRES PERMANENT REPAIR ACTION. REMOVED AND REINSTALLED RT WHEEL WELL VAPOR BARRIER BS 663 RBL 6 TO RBL 61 FOR PERMANENT REPAIR ACTION, IAW SRM 51-40-02 REF DWG 111A1000 AND DWG 111A1001. 89004U 19OCT20. REPAIRED OF VAPOR BARRIER RT WAS ACCOMPLISHED ON CUSTOMER CARD U238242.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 43,114 hrs · 25,940 cycles
LT WHEEL WELL VAPOR BARRIER IS CRACKED AT BS 663 LBL 45 WL 152 TO LBL48 WL 149 AND REQUIRES PERMANENT REPAIR ACTION. REMOVED AND REINSTALLED LT WHEEL WELL VAPOR BARRIER BS 663 LBL 6 TO LBL 61, IAW SRM 51-40-02 REF DWG 111A1000 DWG 111A1001. VAPOR BARRIER LT WAS REPAIRED ON CUSTOMER CARD U238241 89004U 19OCT20.
Part: SKIN — DENTED (BS 193) · airframe 43,114 hrs · 25,940 cycles
TRANSFERRED FROM CARD X367145=EXTERNAL FUSELAGE SKIN DENTED AT BODY STATION 193 BETWEEN STRINGERS 17 AND 18 RIGHT HAND SIDE=ACTUAL LOCATION IS 188+5.9'; 12.3' BELOW STRINGER 17 RT L=2.1' W=1.7' Y=0.013' W/Y=130. EVALUATED DENT ON BS 188+5.9'; 12.3' BELOW STR 17 RT LENGTH OF 2.1' WIDTH OF 1.7' DEPTH OF .013' W/Y= 130. DAMAGE WITHIN LIMITS, IAW EA 20-153-02072 REV IR AND ER 20-03419 REV IR HFEC AREA NO DEFECTS NOTED, PER NDT MANUAL D6-37239 PART 6 53-30-00 PROC 3. INSTALLED DENT DOT, IAW EA 20-153-02072 REV IR. NO FURTHER INSPECTION OR ACTION REQUIRED, PER REF EA 20-153-02072 REV IR.
Part: SKIN — DENTED (BS 200) · airframe 43,114 hrs · 25,940 cycles
TRANSFERRED FROM CARD X521177=RE-EVALUATE DENT AT STA 200 BETWEEN STR 17 AND STR 18 RIGHT, REF NRC X367146. ACTUAL LOCATION IS BS 196.5 + 2.2' 6.4' BELOW STRINGER 17 RT L=7.3', W=4.5', Y=0.120, W/Y=37. DENT WAS REPAIRED, PER EA 20-153-02072 REV IR AND ER 20-03419 REV IR.
Part: SKIN — DENTED (BS 209) · airframe 43,114 hrs · 25,940 cycles
TRANSFERRED FROM CARD X367147=EXTERNAL FUSELAGE DENT DOT MISSING BODY STATION 20 9 BETWEEN STRINGERS 17 AND 18 RIGHT HAND SIDE, ACTUAL LOCATION IS BS 203.8 + 5.6' 11.8' BELOW STRINGER 17 RT L=2.2'; W=1.6'; Y=0.038' W/Y=42. EVALUATED DENT ON BS 203.8+5.6' 11.8' BELOW STR 17 RT LENGTH OF 2.2 WIDTH OF 1.6', DEPTH OF .038' W/Y=42. DENT WITHIN LIMITS, IAW EA 20-153-02072 REV IR AND ER 20-03419 REV IR HFEC AREA NO DEFECTS NOTED, PER NDT MANUAL D6-37239 PART 6 53-30-00 PROC 23. INSTALLED DENT DOT, IAW EA 20-153-02072 REV IR. NO FURTHER ACTION OR INSPECTION REQUIRED, PER REF EA 20-153-02072 REV IR.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 42,234 hrs · 25,377 cycles
CAPTAIN'S AFT I/B SEAT TRACK FAILED WEAR CHECK. / REMOVED AND REPLACED CAPT'S AFT I/B SEAT TRACK IAW AMM 25-11-01.
Part: PLENUM — DIRTY (APU) · airframe 41,912 hrs · 25,196 cycles
DURING CRUISE HAD ELECTRICAL BURNING ODOR IN COCKPIT NO ODOR IN CABIN. NO SMOKE, FIRE OR ABNORMAL A/C SYSTEMS NOTED. ODOR LASTED FOR APROX 15 MIN. CAPT CDU BLINKED AND REBOOTED AT THE BEGINING OF THE FLIGHT. COMPLIED WITH CONDITIONAL INSP PER M/M 05-51-56 REMOVED #1 AND #2 FMCS CDU INSPECTED VENTS AND FOUND CLEAN AND OPS CKS NORMAL #1 AND #2 PER M/M 34-61-01. INSPECTED APU AIR INLET PLEAAM AND REMOVED DEBRIS PER M/M 49-15-00. CLEANED WX RADAR RT FILTER PER M/M 34-43-09 OPERATED ALL INST PANEL LTS PER M/M 33-11-00 NO DEFECTS NOTED. OK FOR CONTINUED SERVICE.
Part: PLENUM — DIRTY (APU) · airframe 41,912 hrs · 25,196 cycles
DURING CRUISE HAD ELECTRICAL BURNING ODOR IN COCKPIT NO ODOR IN CABIN. NO SMOKE, FIRE OR ABNORMAL A/C SYSTEMS NOTED. ODOR LASTED FOR APROX 15 MIN. CAPT CDU BLINKED AND REBOOTED AT THE BEGINING OF THE FLIGHT. COMPLIED WITH CONDITIONAL INSP PER M/M 05-51-56 REMOVED #1 AND #2 FMCS CDU INSPECTED VENTS AND FOUND CLEAN AND OPS CKS NORMAL #1 AND #2 PER M/M 34-61-01. INSPECTED APU AIR INLET PLEAAM AND REMOVED DEBRIS PER M/M 49-15-00. CLEANED WX RADAR RT FILTER PER M/M 34-43-09 OPERATED ALL INST PANEL LTS PER M/M 33-11-00 NO DEFECTS NOTED. OK FOR CONTINUED SERVICE. WITH MECH 36461
Part: PLENUM — DIRTY (APU BAY) · airframe 41,912 hrs · 25,196 cycles
DURING CRUISE HAD ELECTRICAL BURNING ODOR IN COCKPIT NO ODOR IN CABIN. NO SMOKE; FIRE OR ABNORMAL A/C SYSTEMS NOTED. ODOR LASTED FOR APROX 15 MIN. CAPT CDU BLINKED AND REBOOTED AT THE BEGINING OF THE FLIGHT. / COMPLIED WITH CONDITIONAL INSP PER M/M 05-51-56 REMOVED #1 AND #2 FMCS CDU INSPECTED VENTS AND FOUND CLEAN AND OPS CKS NORMAL #1 AND #2 PER M/M 34-61-01. INSPECTED APU AIR INLET PLEAAM AND REMOVED DEBRIS PER M/M 49-15-00. CLEANED WX RADAR RT FILTER PER M/M 34-43-09 OPERATED ALL INST PANEL LTS PER M/M 33-11-00 NO DEFECTS NOTED. OK FOR CONTINUED SERVICE. WITH MECH 36461
Earlier reports · 2009–2019 · 93 reports
2019
Part: PUMP — FAULTY (NR 2 ENGINE FUEL) · airframe 40,359 hrs · 24,210 cycles
#2 N1 UNABLE TO REACH FULL POWER ON CLIMBOUT. R & R THE NR 2 ENGINE FUEL PUMP PER MT.
Part: BEAM — CRACKED (R1 DOOR) · airframe 40,350 hrs · 24,205 cycles
R1 DOOR #4 BEAM CRACKED IN RADIUS ADJACENT TO FASTENER HOLE CLOSEST TO INNER SKIN. / R&R R1 DOOR PER AMM.
Part: BEAM — CRACKED (R1 DOOR) · airframe 40,350 hrs · 24,205 cycles
R1 DOOR #5 BEAM CRACKED IN RADIUS ADJACENT TO FASTENER HOLE CLOSEST TO INNER SKIN. REPAIRED R1 DOOR PER AMM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
RT HORIZONTAL INSPAR RIB ASSEMBLY STA 120.3 HAD CRACKED HOLE COMMON TO THE #4 STIFFENER, 9TH HOLE FROM AFT OUTBOARD EDGE. REPAIRED RIB IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
CABIN FLOORBEAM CORRODED AT FASTENER HOLES BS. 986.5, LBL 43. R&R FLOORBEAM PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
CABIN FLOORBEAM CORRODED AT FASTENER HOLES BS. 986.5, BETWEEN RBL 12 TO RBL 44. R&R FLOORBEAM PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #5 STAB STA 129.50 CRACKED HOLE COMMON TO THE #4 STIFFENER. REPAIRED RIB ASSEMBLY PER SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
R2 DOOR Z ANGLE CORRODED. R&R Z ANGLE PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #5 STAB. STA. 129.50 CRACKED HOLE COMMON TO #3 STIFFENER. REPAIRED RIB ASSEMBLY PER SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
RT HORIZONTAL STABILIZER #2 RIB, HORIZONTAL STAB STA 120.3 CRACKED 1" ABOVE BOTTOM OF 2ND VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: FLOOR SUPPORT — CRACKED (BS 312) · airframe 40,350 hrs · 24,205 cycles
FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE INTERCOSTAL CRACKED AT FORWARD FASTENER HOLE ATA BS. 312+3, RBL 33. R&R INTERCOSTAL PER SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
RT HORIZONTAL STABILIZER #2 RIB, HORIZONTAL STAB STA 120.3 CRACKED 1" ABOVE BOTTOM OF 3RD VERTICAL STIFFENER, LOOKING AFT. REPAIRED RIB PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
FORWARD GALLEY INTERCOSTAL CRACKED AT NUT PLATE HOLES, BETWEEN BS. 340 TO BS. 360, BL 0. R&R INTERCOSTAL PER SRM.
Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
LT HORIZONTAL INSPAR RIB ASSEMBLY #5 STAB. STA. 129.50, CRACKED #4 STIFFENER. REPAIRED STIFFENER IAW SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
RT HORIZONTAL STABILIZER #2 RIB, HORIZONTAL STAB STA 120.3 CRACKED 1" ABOVE BOTTOM OF 4TH VERTICAL STIFFENER, LOOKING AFT. REPAIRED RIB PER SRM.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 40,350 hrs · 24,205 cycles
FORWARD CARGO FLOOR STRUCTURES CORRODED AT CARGO TIE DOWN AT BS 436, LBL 21. R&R TIE DOWN TRACK PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,350 hrs · 24,205 cycles
LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #5 STAB STA 129.50 CRACKED #3 STIFFENER. REPAIRED RIB ASSEMBLY PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
FORWARD GALLEY AREA INTERCOSTAL CRACKED AT NUT PLATE HOLE AT BS. 277+6, BL 0. R&R INTERCOSTAL PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
STRINGER CLIP CRACKED AT BS. 277, STR. 10R. R&R CLIP PER SRM.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 40,350 hrs · 24,205 cycles
FORWARD OF R1 DOOR CUTOUT LOWER FORWARD CORNER WEB ATTACH ANGLE CRACKED AT BS. 293.5, STR. 17R. R&R ANGLE PER SRM.
Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 40,350 hrs · 24,205 cycles
RT WHEEL WELL VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER PER SRM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,848 hrs · 23,888 cycles
R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 39,819 hrs · 23,867 cycles
R2 DOOR SLIDE "Z" FOLD CAME OUT. REINSTALLED SLIDE PER AMM.
Part: CONTROL MODULE — FAILED (E&E BAY) · airframe 39,290 hrs · 23,540 cycles
AIR TURNBACK, AUTO FAILED AFTER LIFT-OFF. MANUAL STABILIZED PRESSURIZATION. R&R CABIN PRESSURE CONTROL MODULE IAW MM.
2018
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 37,838 hrs · 22,580 cycles
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER SIP.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,152 hrs · 22,146 cycles
R2 SLIDE OUT OF POSITION. R&R SLIDE PER MT.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,152 hrs · 22,146 cycles
L1 DOOR SLIDE OUT OF POSITION. R&R SLIDE PER MT.
2017
Part: COFFEEMAKER — FAULTY (CABIN) · airframe 34,557 hrs · 20,496 cycles
DIVERSION/DECLARED EMERGENCY, FLIGHT ATTENDANTS REPORTED A STRONG "TOXIC CHEMICAL" SMELL COMING FROM THE AFT GALLEY COFFEE POT AREA. R&R NR 1 COFFEEMAKER IAW AMM.
Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 34,557 hrs · 20,496 cycles
DIVERSION/DECLARED EMERGENCY, FLIGHT ATTENDANTS REPORTED A STRONG "TOXIC CHEMICAL" SMELL COMING FROM THE AFT GALLEY COFFEE POT AREA. R&R NR 2 COFFEEMAKER IAW AMM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,247 hrs · 20,299 cycles
BATTERY PACK FAILED A CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW AMM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,247 hrs · 20,299 cycles
BATTERY PACK FAILED A CAPACITY CHECK AT LOCATION M01675. R & R THE BATTERY PACK IAW AMM AND DWG.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 33,967 hrs · 20,112 cycles
LT WHEEL WELL FORWARD MOISTURE BARRIER CRACKED. REPAIRED BARRIER PER EA.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,930 hrs · 20,085 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,930 hrs · 20,085 cycles
LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 32,272 hrs · 19,084 cycles
FLOOR SUPPORT CRACKED AT BS 540, BL 0. R & R THE FLOOR SUPPORT IAW SRM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,272 hrs · 19,084 cycles
EMERGENCY LIGHT FAILED CAPACITY TEST AT M01670. R & R THE BATTERY PACK IAW AMM AND DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,272 hrs · 19,084 cycles
EMERGENCY LIGHT FAILED CAPACITY TEST AT M01668. R & R THE BATTERY PACK IAW AMM AND DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,272 hrs · 19,084 cycles
EMERGENCY LIGHT FAILED CAPACITY TEST AT M01669. R & R THE BATTERY PACK IAW AMM AND DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,272 hrs · 19,084 cycles
EMERGENCY LIGHT FAILED CAPACITY TEST AT M01672. R & R THE BATTERY PACK IAW AMM AND DWG.
2016
Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 31,422 hrs · 18,565 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER SIP.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 30,714 hrs · 18,135 cycles
RIGHT LOWER VERTICAL EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.
Part: SIGN — MISSING (CABIN) · airframe 30,039 hrs · 17,748 cycles
FORWARD GALLEY EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW EA.
Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 30,038 hrs · 17,748 cycles
RIGHT EMERGENCY EXIT SIGN MISSING AT ROW 12. REPLACED THE SIGN IAW AMM.
Part: SIGN — MISSING (CABIN) · airframe 30,039 hrs · 17,748 cycles
AFT RT GALLEY EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW EA.
Part: TRIM MOTOR — FAILED (HORIZ STAB) · airframe 29,522 hrs · 17,456 cycles
AIR TURN BACK & DECLARED EMER. SPEED TRIM FAIL LIGHT ILLUMINATED. THE STAB TRIM FAILED IN ELEC MODE. R & R STAB TRIM MOTOR IAW MM.
Part: LENS — MISSING (EXIT SIGN) · airframe 29,442 hrs · 17,401 cycles
RIGHT LOWER OVERWING EXIT SIGN LENS MISSING. INSTALLED LENS IAW.
2015
Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 27,988 hrs · 16,549 cycles
L2 DOOR EMER EVAC SLIDE PRESS GAUGE OUT OF LIMITS. R & R SLIDE IAW MT.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
LEFT NR 1 WINDOW FRAME CRACKED, IN UPPER OTBD CORNER INTERIOR & EXTERIOR. R & R DOUBLER IAW ACO.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
LEFT HORIZONTAL STABILIZER RIB AT 120.30, THIRD VERTICAL RIB FROM FRONT, CRACKED NEAR BASE. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
LEFT HORIZONTAL STABILIZER RIB AT 120.30, SECOND VERTICAL RIB FROM FRONT CRACKED NEAR BASE. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
LEFT HORIZONTAL STABILIZER RIB AT 92.70, SECOND VERTICAL FLANGE FROM FRONT CRACKED NEAR BASE. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER RIB AT 92.70, SECOND VERTICAL STIFFENER, CRACKED NEAR BASE. REPAIRED RIB IAW SRM.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
R1 DOOR THRESHOLD INBD ATTACH ANGLE CORRODED, BETWEEN BS 312 - 832. R & R ANGLE IAW SRM & DWG.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
SEAT TRACK INBD FLANGE ATTACH HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 45.5 INBD & OTBD AFT END. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
SEAT TRACK INBD & OTBD FLANGE, CRACKED AT BS 727B, LBL 45.5, FWD HOLE OTBD SIDE. REPAIRED FLANGE IAW EA.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,988 hrs · 16,549 cycles
AFT CARGO COMPARTMENT, PANEL SUPPORT ANGLE CRACKED AT BS 727. R & R ANGLE IAW SRM & DWG.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 101.9, 17.5" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER, LOWER IN SPAR SKIN, CRACKED AT STATION 157.10, 7.25" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER, LOWER IN SPAR SKIN CRACKED AT STATION 101.9, 17.5" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 157.10, 13.75" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER, LOWER IN SPAR SKIN, CRACKED AT STATION 157.10, 13.75" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 157.10, 7.25" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED, BETWEEN STATION 96.0 - 99.0 AT REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
LEFT HORIZONTAL STABILIZER, LOWER IN SPAR SKIN CRACKED, BETWEEN STATION 96.5 - 98.0 AT REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN, CRACKED AT STATION 101.9, 8.5" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED, BETWEEN STATION 96.0 - 99.0 AT REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
LEFT HORIZONTAL STABILIZER, LOWER IN SPAR SKIN CRACKED, BETWEEN STATION 96.5 - 98.0 AT REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 138.7, 15.25" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 138.7, 15.25" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,988 hrs · 16,549 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 101.9, 8.5" FROM REAR SPAR. REPAIRED SKIN IAW CCO.
Part: FAN — OVERHEATED (CABIN) · airframe 26,918 hrs · 15,934 cycles
DIVERSION & DECLARED EMER. DURING CRUISE FLIGHT ATTENDANT REPORTED STRONG FUMES AROUND ROW 16. PAXS IN THE AREA REPORTED THE SAME. FOUND WI-FI HPT FAN MOTOR OVERHEATED. R & R WI-FI HPT FAN MOTOR IAW MM.
2014
Part: SIGN — MISSING (CABIN) · airframe 22,196 hrs · 13,242 cycles
RIGHT OVERWING DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW SIP.
2013
Part: DOOR — CRACKED (EXTERNAL POWER) · airframe 21,112 hrs · 12,615 cycles
EXTERNAL POWER DOOR LANDING CRACKED, AFT EDGE. REPAIRED DOOR IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STATION 138.70, 15.25 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 101.90, 17.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SPAR — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT LOWER HORIZONTAL STABILIZER CRACKED AT REAR SPAR BETWEEN STATION 96.0 TO STATION 99.0. REPAIRED STABILIZER IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 157.10, 7.25 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
LT LOWER HORIZONTAL STABILIZER REAR SPAR CRACKED BETWEEN STATION 129.5 TO STATION 98.0. REPAIRED SPAR IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 101.90, 8.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,112 hrs · 12,615 cycles
RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 157.10, 13.75 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 18,846 hrs · 11,330 cycles
RIGHT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 18,846 hrs · 11,330 cycles
LEFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.
2012
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,892 hrs · 10,173 cycles
L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED BULB PER AMM.
Part: COVER — MISSING (CABIN) · airframe 16,461 hrs · 9,878 cycles
LEFT EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
Part: COVER — MISSING (CABIN) · airframe 15,694 hrs · 9,455 cycles
LEFT EEPLS COVER MISSING AT ROW 20. INSTALLED COVER IAW MM.
2011
Part: SIGN — BROKEN (CABIN) · airframe 12,996 hrs · 7,866 cycles
R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: COVER — PUNCTURED (NR 2 ENGINE) · airframe 12,346 hrs · 7,513 cycles
INFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY. LOW OIL QUANTITY WITH LOW OIL PRESSURE. SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED DRIVE PAD COVER PER MM.
2010
Part: COVER — BROKEN (CABIN) · airframe 10,131 hrs · 6,226 cycles
EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: LENS — MISSING (CABIN) · airframe 9,043 hrs · 5,556 cycles
RIGHT AFT EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LENS — MISSING (CABIN) · airframe 9,010 hrs · 5,537 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 7,726 hrs · 4,770 cycles
AFT GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
2009
Part: LIGHT — BROKEN (CABIN) · airframe 6,503 hrs · 4,007 cycles
EEPLS BROKEN AT ROW 1. REPAIRED EEPLS PER SI.