N921WN
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.
115 reports on file, 2008-06-10 – 2020-11-24.
Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 41,934 hrs · 25,250 cycles
G4 GALLEY EXIT SIGN IS DAMAGED. REMOVED G4 GALLEY EXIT SIGN ASSEMBLY WITH DAMAGE AND INSTALLED NEW GALLEY EXIT SIGN ASSEMBLY, IAW AMM 33-51-01-960-801. CHECK GOOD. 59736U 11/30/20.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 41,934 hrs · 25,250 cycles
EMERGENCY EXIT BATTERY BACK M1668 FAILS CAPACITY CHECK. PERFORMED DEEP CYCLE OF BATTERY PACK M1668, PER AMM 33-51-06-600-802. PERFORMED GOOD TEST OF EMERGENCY EXIT STEPS 6D(4)-(6). LIGHT BATTERY PACKS CAPACITY, PER AMM 33-51-06-200-801. 59019U 20NOV20.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,526 hrs · 25,008 cycles
LT OVERWING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT BULB, PER AMM 33-51-04.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 40,643 hrs · 24,456 cycles
BROKEN LAVATORY B BASE EMERGENCY EXIT LIGHT LENS AT AFT GALLEY AREA. / R&R LENS IAW AMM.
Part: ANGLE — BROKEN (BS 540 RBL 13-21) · airframe 40,642 hrs · 24,456 cycles
BROKEN ANGLE LOCATED BS540 BETWEEN RBL13 TO RBL21 AT PASSENGER CABIN (1 EA) / REPLACED ANGLE (PANEL BRAKE ASSY) LOCATED BS540 BETWEEN RBL 13 TO RBL 21 AT PASSENGER CABIN (1EA) AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A0060 REV
Part: LENS — BROKEN (CABIN) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA BASE EMERGENCY LENS BROKEN. / R&R BASE EMERGENCY LENS IAW AMM.
Part: CARGO TRACK — CRACKED (BS 727E-767) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT TRACK CRACKED BETWEEN BS. 727E TO BS. 767, RBL 13.84. / REPAIRED TRACK PER SRM.
Part: STRAP — CORRODED (BS 737-787) · airframe 40,642 hrs · 24,456 cycles
CORROSION STRAP LOCATED BETWEEN BS767 TO BS787 AND BETWEEN STR 25L TO STR 25R AFT CARGO COMPARMENT / REPLACED STRAP LOCATED BETWEEN BS767 TO BS787 AND BETWEEN STR 25L TO STR 25R AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; 51-10-02 PARAGRAPH 9 AND DRAWING # 146A7500 SHEET 61 REV -
Part: STUB FRAME — CRACKED (BS 294) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA STUB FRAME CRACKED AT BS. 294.5, STR. 17R. / R&R STUB FRAME IAW SRM AND DWG.
Part: SUPPORT — CORRODED (BS 727-767) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS. 727 TO BS. 767 AT LEVEL STR. 25R. / R&R SUPPORT ZEE IAW SRM AND DWG.
Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 40,643 hrs · 24,456 cycles
AFT GALLEY AREA FLOOR PANEL 242XF DELAMINATED. / REPAIRED FLOOR PANEL 242XF PER SRM.
Part: SUPPORT — CRACKED (BS 807-827) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT SUPPORT ZEE CRACKED BETWEEN BS. 807 TO BS. 827, STR. 25L. / REPAIRED SUPPORT ZEE IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,643 hrs · 24,456 cycles
FORWARD CARGO COMPARTMENT WEB - INTERCOSTAL CRACKED BETWEEN BS. 500A TO BS. 500B, STR. 26L. / R&R WEB - INTERCOSTAL IAW SRM AND DWG.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,642 hrs · 24,456 cycles
CRACK GUSSET ON BS500D LOCATED STR19L AND STR21L FWD COMPARTMENT (2 EA) / REPLACED GUSSET ON BS500D LOCATED STR 19L AND STR 21; FWD CARGO COMPARTMENT (2EA) IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7902 SHEET 21 REV E (U 074)
Part: GUSSET — CRACKED (BS 500D) · airframe 40,643 hrs · 24,456 cycles
FORWARD COMPARTMENT GUSSET CRACKED AT BS. 500D, BETWEEN STR. 19L TO STR. 21L. / R&R GUSSET IAW SRM & DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 40,643 hrs · 24,456 cycles
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 40,643 hrs · 24,456 cycles
BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA. / R&R LENS IAW AMM.
Part: STRUCTURE — CRACKED (BS 270-360) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA INTERNAL AREA CHORD CRACKED BETWEEN BS. 270 TO BS. 360, STR. 17L. / R&R INNER CHORD IAW SRM AND DWG.
Part: ANGLE — CRACKED (BS 500C) · airframe 40,643 hrs · 24,456 cycles
FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS. 500C, STR. 26R. / R&R ANGLE IAW SRM AND DWG.
Part: SUPPORT — CORRODED (BS 727-767) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT SUPPORT ZEE AFT CORRODED BETWEEN BS. 727 TO BS. 767 AT LEVEL STR. 25L. / REPAIRED SUPPORT ZEE IAW SRM AND DWG
Part: FLOOR PANEL — MISSING (FWD GALLEY) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA MISSING MATERIAL FLOOR PANEL 221GF. / R&R FLOOR PANEL 221GF PER SRM.
Part: ANGLE — CRACKED (BS 291-294) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA FLOOR STRUCTURE ON ANGLE CRACKED BETWEEN BS. 291.5 TO BS. 294.5, STR. 17R. / R&R ANGLE IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 40,643 hrs · 24,456 cycles
ENTRY DOOR ON WEB CRACKED BETWEEN BS. 294.5 TO BS. 303.9, STR. 16L. / R&R INTERCOSTAL IAW SRM AND DWG.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 40,643 hrs · 24,456 cycles
FORWARD GALLEY AREA FLOOR PANEL 221BF DELAMINATED. / REPAIRED FLOOR PANEL 221BF PER SRM.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 40,643 hrs · 24,456 cycles
CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (5 EA) REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (5 EA) IAW AMM 33-51-15-400-802
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,643 hrs · 24,456 cycles
EMERGENCY LIGHT BATTERY PACKS M1675 INOPERATIVE AT PASSENGER CABIN. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,643 hrs · 24,456 cycles
EMERGENCY LIGHT BATTERY PACKS M1674 INOPERATIVE AT PASSENGER CABIN. / R&R BATTERY PACK IAW AMM.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 40,643 hrs · 24,456 cycles
MAIN WHEEL WELL COMPARTMENT VAPOR BARRIER CRACKED AT BS. 663, LBL 30. / REPAIRED VAPOR BARRIER PER SRM.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 140AF CRACKED. / FABRICATED FLOOR PANEL 140AF IAW DWG.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,643 hrs · 24,456 cycles
CRACKED INSPAR RIB LOCATED STAB. STA. 129.5 AND 19 INCH FROM FRONT SPAR AT L/H HORIZONTAL STABILIZER. / REPAIRED INSPAR RIB PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,643 hrs · 24,456 cycles
CRACKED INSPAR RIB LOCATED ON STAB. STA. 129.5 AND 28 INCH FROM FRONT SPAR AT L/H HORIZONTAL STABILIZER. / REPAIRED INSPAR RIB PER SRM.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 40,643 hrs · 24,456 cycles
CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (5 EA) REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (5 EA) IAW AMM 33-51-15-400-802
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,643 hrs · 24,456 cycles
EMERGENCY LIGHT BATTERY PACK M1669 INOPERATIVE AT PASSENGER CABIN. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,643 hrs · 24,456 cycles
EMERGENCY LIGHT BATTERY PACK M1670 INOPERATIVE AT PASSENGER CABIN. / R&R BATTERY PACK IAW AMM.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 40,643 hrs · 24,456 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 140BF CRACKED. / FABRICATED FLOOR PANEL 140BF IAW DWG.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 40,486 hrs · 24,357 cycles
AFT FLIGHT ATTENDANT FLASHLIGHT SAFETY STRAP BROKEN. R&R STRAP PER MM.
Earlier reports · 2008–2019 · 79 reports
2019
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER #4 RIB STA. 120.3, 3RD VERTICAL STIFFENER CRACKED. / REPAIRED #4 RIB IAW SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER STAB. STA. 129.5 #5 IN SPAR RIB CRACKED ON VERTICAL WEB AT LOWER FORWARD CORNER. / REPAIRED RIB IAW EA.
Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL FORWARD SPAR WEB CRACKED ON FORWARD TOP RIB WEB JUST BELOW UPPER FLANGE AT RIB #1 STA. 92.70. / REPAIRED SPAR WEB IAW EA.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER #1 INSPAR RIB STA. 92.7 CRACKED ON THE 2ND VERTICAL STIFFENER. / REPAIRED #1 INSPAR RIB IAW SRM AND DWG.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER #5 INSPAR RIB STA. 129.50 CRACKED ON THE 2ND VERTICAL STIFFENER. / REPAIRED #5 INSPAR RIB IAW SRM & DWG.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER #4 INSPAR RIB STA. 120.30 CRACKED ON THE 2ND AND 3RD VERTICAL STIFFENERS. / REPAIRED #2 STIFFENER IAW SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER INTERNAL STRUCTURE AT THE #1 RIB (STAB. STA. 92.7), 2ND VERTICAL STIFFENER #4 RIB (STA 120.30), 2ND & 3RD STIFFENER, & #5 RIB (S STA 129.50), 2ND VERTICAL STIFFENER CRACKED. / REPAIRED #4 RIB PER EA.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER INTERNAL STRUCTURE AT THE #1 RIB (STAB. STA. 92.7), 2ND VERTICAL STIFFENER #4 RIB (STA 120.30), 2ND & 3RD STIFFENER, & #5 RIB (S STA 129.50), 2ND VERTICAL STIFFENER CRACKED. / REPAIRED #1 RIB PER EA.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,155 hrs · 24,145 cycles
R/H HORIZONTAL STABILIZER INTERNAL STRUCTURE AT THE #1 RIB (STAB. STA. 92.7), 2ND VERTICAL STIFFENER #4 RIB (STA 120.30), 2ND & 3RD STIFFENER, & #5 RIB (S STA 129.50), 2ND VERTICAL STIFFENER CRACKED. / REPAIRED #5 RIB PER EA.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 40,153 hrs · 24,144 cycles
R/H HORIZONTAL STABILIZER #4 INSPAR RIB, STA. 120.30, CRACKED ON THE 2ND AND 3RD VERTICAL STIFFENERS. / REPAIRED 2ND STIFFENERS IAW SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 40,153 hrs · 24,144 cycles
R/H HORIZONTAL STABILIZER #1 INSPAR RIB (STA 92.7) CRACKED ON THE 2ND VERTICAL STIFFENER. / REPAIRED VERTICAL STIFFENER IAW SRM AND DWG.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 40,153 hrs · 24,144 cycles
R/H HORIZONTAL STABILIZER #5 INSPAR RIB (STA. 129.50) CRACKED ON THE 2ND VERTICAL STIFFENER. / REPAIRED SECOND VERTICAL STIFFENER IAW SRM & DWG.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,153 hrs · 24,144 cycles
R/H HORIZONTAL STABILIZER #4 INSPAR RIB, STA. 120.30, CRACKED ON THE 2ND AND 3RD VERTICAL STIFFENERS. / REPAIRED #4 RIB IAW SRM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,013 hrs · 24,061 cycles
L2 DOOR EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER AMM.
Part: SLIDE — OPEN (L2 DOOR) · airframe 37,396 hrs · 22,407 cycles
L2 DOOR EMERGENCY SLIDE OPENED, DID NOT DEPLOY. REPACKED SLIDE PER MT.
Part: LATCH — BROKEN (EVAC SLIDE) · airframe 37,084 hrs · 22,216 cycles
R1 DOOR ESCAPE SLIDE LATCH ASSEMBLY BROKEN. R&R SLIDE ASSEMBLY PER MT.
2018
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 35,660 hrs · 21,265 cycles
R2 DOOR ESCAPE SLIDE GAUGE PRESSURE LOW. R&R SLIDE PER MT.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 34,585 hrs · 20,568 cycles
LEFT WING OUTBOARD MAIN FLAP OUTBOARD TRAILING EDGE LOWER SKIN DELAMINATED. REPAIREDTHE FLAP SKIN IAW SRM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 34,585 hrs · 20,568 cycles
RIGHT WING INBOARD MAIN FLAP OUTBOARD TRAILING EDGE LOWER SKIN DELAMINATED. REPAIRED THE FLAP SKIN IAW SRM.
Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 34,585 hrs · 20,568 cycles
CENTER CABIN CEILING EMERGENCY EXIT LIGHT HOUSING MOUNTS BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 34,585 hrs · 20,568 cycles
REAR VERTICAL PRESSURE BULKHEAD UPPER OUTBOARD COUNTERSINK FASTENER HOLE ABOVE BALL DRAIN HOUSING CUTOUT THE BULKHEAD WEB CRACKED AT LBL 35. REPAIRED THE BULKHEAD WEB IAW EA.
Part: TRUNNION — CORRODED (LT MLG) · airframe 34,585 hrs · 20,568 cycles
LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.
Part: TRUNNION — CORRODED (RT MLG) · airframe 34,585 hrs · 20,568 cycles
RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.
Part: PLATE — CRACKED (RT WING) · airframe 34,585 hrs · 20,568 cycles
RIGHT WING WIGGLE PLATE OUTBOARD OF PANEL 651DB CRACKED AT IRSS. 215. R & R THE WIGGLE PLATE IAW SRM.
Part: LIGHT — CRACKED (CABIN) · airframe 34,585 hrs · 20,568 cycles
FORWARD GALLEY EMERGENCY LIGHT STRIPS CRACKED. R & R THE LIGHT IAW MM.
Part: LAMP — INOPERATIVE (EMEGENCY LIGHT) · airframe 34,236 hrs · 20,336 cycles
LEFT WING AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
2017
Part: LIGHT — DETACHED (MID CABIN) · airframe 33,823 hrs · 20,082 cycles
MIDDLE CABIN EMERGENCY EXIT LIGHT FELL OFF. SECURED THE LIGHT IAW AMM.
Part: LIGHT — LOOSE (CENTER CABIN) · airframe 33,746 hrs · 20,022 cycles
CENTER CABIN EMERGENCY EXIT LIGHT LOOSE AT ROW 11. SECURED LIGHT ASSY PER MM.
Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 33,035 hrs · 19,546 cycles
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP OUT OF POSITON. REPOSITIONED GIRT BAR PER MT.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 32,369 hrs · 19,122 cycles
MID CABIN OVERHEAD EXIT SIGN CAME OFF. REINSTALLED LENS IAW AMM.
Part: LATCH — LOOSE (CABIN) · airframe 31,343 hrs · 18,514 cycles
AFT FLASHLIGHT COMPARTMENT LATCH LOOSE. SECURED LATCH PER MM.
2016
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670. R & R BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R & R THE BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R & R THE BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01668. R & R THE BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01674. R & R THE BATTERY PACK IAW DWG.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 29,496 hrs · 17,421 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R & R THE BATTERY PACK IAW DWG.
Part: SIGN — LOOSE (CABIN) · airframe 28,433 hrs · 16,802 cycles
R2 DOOR EMER EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 27,675 hrs · 16,367 cycles
RIGHT LOWER FUSELAGE EXTERNAL POWER OUTLET, CUT OUT AFT EDGE REPAIR DOUBLER CRACKED. REPAIRED CUT OUT IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,675 hrs · 16,367 cycles
FORWARD CARGO COMPARTMENT, FLOOR STRUCTURE CORRODED AT BS 500A, STRINGER 26R. R & R Z ANGLE IAW SRM & DWG.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,675 hrs · 16,367 cycles
AFT PIT Z CHANNEL, UPPER SURFACE CORRODED, BETWEEN BS 767 - 782, RBL 22. R & R Z ANGLE IAW SRM & DWG.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,179 hrs · 16,070 cycles
R1 DOOR EXTERIOR SLIDE EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
2015
Part: WEB — CRACKED (LT MLG WW) · airframe 26,463 hrs · 15,657 cycles
LEFT MAIN WW WEB CRACKED, BETWEEN BS 54 - 40. REPAIRED WEB IAW EA.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 23,723 hrs · 14,056 cycles
R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
2014
Part: SLIDE — LOOSE (R1 DOOR) · airframe 21,354 hrs · 12,691 cycles
R1 DOOR EMERGENCY EVAC SLIDE CAME LOOSE OUT OF HOLDER. SECURED SLIDE IAW MT.
Part: PLATE — DAMAGED (LT WING) · airframe 20,967 hrs · 12,470 cycles
LEFT WING TE WAFFLE PLATE ASSEMBLY BETWEEN NR 1 & NR 2 FLAP TRACKS DAMAGED. R & R WAFFLE PLATE IAW SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 20,967 hrs · 12,470 cycles
AFT CARGO BULKHEAD STRUCTURE LOWER ANGLE CRACKED AT BS 867. R & R ANGLE IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.50, 10 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 101.90, 10 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 147.90 10 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 157.10, 9 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 184.70, 10 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.70, 8 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,967 hrs · 12,470 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.70, 18 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,612 hrs · 12,282 cycles
LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 17 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,612 hrs · 12,282 cycles
LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 32.5 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
2013
Part: SIGN — LOOSE (CABIN) · airframe 20,035 hrs · 11,948 cycles
CTR OVERWING EMERGENCY EXIT SIGN LOOSE. R & R SIGN IAW MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 19,175 hrs · 11,435 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT ADJUSTMENT. ADJUSTED SLIDE IAW MT.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 18,353 hrs · 10,967 cycles
EXTERIOR GROUND POWER DOOR CUTOUT CRACKED AT AFT LATCH AREA. REPAIRED DOUBLER IAW EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,353 hrs · 10,967 cycles
RT MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW M/M.
2012
Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 16,087 hrs · 9,644 cycles
LEFT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED SEAL PER SRM 51-40-02 AND SRM 51-10-02 AND AMM.
Part: BATTERY — FAILED (CABIN) · airframe 16,087 hrs · 9,644 cycles
ALL SEVEN EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST FWD LT, FWD RT, CTR LT, CTR RT, ROW 16 LT, AFT L/T AFT RT. REMOVED AND REPLACED ALL SEVEN EMERGENCY LIGHT BATTERIES PER MM. FWD LT, FWD RT, CTR LT, CTR RT, ROW 16 LT, AFT LT, AFT RT.
Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 16,087 hrs · 9,644 cycles
RIGHT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. REPLACED SEAL PER SRM 51-40-02 AND SRM 51-10-02, AND M/M.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 15,052 hrs · 8,986 cycles
L2 DOOR EMERGENY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT AND MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,052 hrs · 8,986 cycles
RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,766 hrs · 7,655 cycles
DURING SCHEDULED CV CHECK FOUND, EELPS INOP BETWEEN ROW 20 TO ROW 23. REMOVED AND REPLACED EEPLS PER MM.
Part: COVER — CRACKED (CABIN) · airframe 11,600 hrs · 6,968 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 11,600 hrs · 6,968 cycles
DURING SCHEDULED HC1 CHECK, FWD EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: HMU — FAULTY (NR 1 ENGINE) · airframe 10,905 hrs · 6,560 cycles
DIVERSION -- DURING CRUISE AT FL410, NR 1 ENGINE SOUND OF COMPRESSOR STALL. N1/N2 EGT ROLLED BACK - AUTOTHROTTLE DISCONNECTED N1 APPROX 30 PERCENT N2 APPROX 40 PERCENT EGT AT 300 DEG DECREASING. REMOVED AND REPLACED HMU & FUEL PUMP PER MT.
Part: MECHANISM — FAILED (ELEVATOR TAB) · airframe 9,573 hrs · 5,766 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR TAB CONTROL MECHANISHM I/B FAILED GAP CHECK. REMOVED AND REPLACED LT TAB MECHANISM PER MM.
2010
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 8,902 hrs · 5,365 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT EXTERIOR EMERGENCY EGRESS LIGHT INOP. RELAMPED PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,149 hrs · 4,338 cycles
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: FUSE — BLOWN (CABIN) · airframe 6,816 hrs · 4,136 cycles
DURING SCHEDULED MV2 CHECK, FOUND AFT EXTERNAL LT EMERGENCY EXIT LIGHT FUSE INOP. RELAMPED PER MM.
2009
Part: SIGN — BROKEN (CABIN) · airframe 4,953 hrs · 2,980 cycles
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: TRACK — LOOSE (CABIN) · airframe 2,950 hrs · 1,759 cycles
FWD EEPLS TRACK LOOSE. SECURED EEPLS PER MM.
2008
Part: COVER — MISSING (CABIN) · airframe 2,279 hrs · 1,360 cycles
R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REPLACED LIGHT ASSY PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 1,933 hrs · 1,178 cycles
DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 392 hrs · 222 cycles
LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM.