N923DN
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.
177 reports on file, 2008-03-22 – 2019-10-06.
Part: FITTING — CRACKED (MLG ACTUATOR) · airframe 51,073 hrs · 33,937 cycles
DUE VERIFICATION FLIGHT DUE TO LT MLG UNSAFE LIGHT. VERIFICATION OF LANDING GEAR OPERATION FAILS. WHEN GEAR HANDLE SELECTED DOWN GOT 3 GREEN AND AMBER DOOR LIGHT. PERISCOPE CONFIRMED GEAR DOWN AND LT DOOR OPEN. SLOWED DOWN TO 180KTS - DOOR LIGHT GOES OUT. AFTER SHUTDOWN LEFT DOOR STARTS OPENING. FOUND CRACK IN INNER DOOR SKIN AT ACTUATOR ATTACH FITTING. REMOVED LT MLG DOOR IAW MD90 AMM 32-10 (252122). INSTALLED NEW LT MLG DOOR PER MD90 AMM 32-10. PERFORMED GEAR SWINGS, ALL GEAR INDICATIONS NORMAL PER MD90 AMM 32-32 (LP5772918)
Part: ARM — LOOSE (LT MLG UPLOCK) · airframe 51,073 hrs · 33,937 cycles
LANDING GEAR UNSAFE. GEAR HANDLE UP. LEFT GEAR UNSAFE IN UP POSITION. RAN QRH GEAR DOOR LIGHT DID NOT EXTINGUISH UPON LOWERING GEAR. COMPLETED PROCEDURE AND LANDED IN ATL. NO FURTHER ISSUES. RAN ALTERNATE GEAR EXTEND PERFORMED PER QRH. C/W NO GO ODI PREVENTION MAIN GEAR INDICATION. FOUND LT MLG DOOR UPLOCK ARM LOOSE. RESECURED/ ADJUSTMENT OPS CK GOOD. REPLACED LT & RT MLG DOOR RUBSTRIPS. PERFORMED GEAR SWING OPS CK GOOD. OK FOR SERVICE. (LP5772912)
Part: LINE — LEAKING (APU FUEL) · airframe 50,292 hrs · 33,430 cycles
STRONG SMELL OF OIL POSSIBLY FUEL FROM START TO CLIMBING OUT OF 10000 (10 MINS). FA'S DID NOT NOTICE SMELL IN CABIN. FOUND APU FUEL NOZZLE HARD LINE LEAKING. REPLACED APU PER FORCAST NBR 92-4910-9-0010.(LP#5899748)
Part: FUEL CONTROL — LEAKING (APU) · airframe 50,258 hrs · 33,405 cycles
FUEL ODOR IN CABIN AFTER STARTING APU ON TAXI IN. APU AIR SWITCH ON. CONFIRMED FUEL SMELL IN CABIN(AFT). FOUND APU FUEL CONTROL LEAKING FUEL AT LOWER FITTING. TIGHTENED FUEL LINE MD88 IPC 49-31-00 FIG 1(SHEET 2) ITEM # 265. LEAK CK OK. NO FUEL LEAKS NOTICED. C/W FULL DUCT BURNOUT REF MD90 AMM 21-53 AND CHANGED SOCKS AND WASHED APU INLET REF AMDS W/C 4900-18. (LP# 5899738)
Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 49,843 hrs · 33,117 cycles
INITIAL INSPECTION: CORROSION ON DOOR JAMB LOWER AREA. AT AFT CARGO COMPARTMENT. CORROSION ON DOOR JAMB LOWER AREA WAS REPAIRED (AS PERMANENT REPAIR) PER MD90 VOL I SRM 53-60-02 FIG 9 A, ER/A 577398-14 REV ORIGINAL AND ETI90-19-020 REV 2 ASSOCIATED ER/A 00-577398 ADDED FOR AC 9223. (LP# 1037344)
Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 49,843 hrs · 33,117 cycles
DURING REMOTION OF RETAINERS WAS FOUND CORROSION ON INTERNAL PRODUCTION DOUBLER AT LOWER DOOR JAMB OF AFT CARGO COMPARTMENT SUMMARY: OF NRC 00180 ON INTERNAL PRODUCTION DOUBLER AT LOWER DOOR JAMB OF AFT CARGO COMPARTMENT (CCT) WAS REPAIRED (PERMANENT REPAIR) PER ER/A 577195-14 REV ORIGINAL AND ETI-90-19-019 REV.3 . GENERAL VISUAL INSPECTION ON REPAIR WILL BE PERFORMED EVERY 8000 CYCLES UNDER L.P. 1035029 PER ERA 577195-14 REV ORIGINAL. SECTION II. ASSOCIATED ER/A 00-577195 ADDED FOR AC 9223. (LP# 1037648)
Part: SKIN — CRACKED (BS 1437) · airframe 49,843 hrs · 33,117 cycles
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. Y=1437 AND BTW LONGERONS 12RH AND 13RH. SUMMARY OF NRC 00058 FUSELAGE SKIN STA Y=1437 AND BTW LONGERONS 12RH AND 13RH WAS REPAIRED (AS PERMANENT REPAIR) PER ER/A 577191-14 REV ORIGINAL AND ETI-90-19-015 REV 2.
Part: SKIN — CRACKED (NLG DOOR AREA) · airframe 49,843 hrs · 33,117 cycles
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN ON AFT NLG DOOR AFT HINGE RH SIDE. FUSELAGE SKIN ON AFT RH NLG DOOR AFT HINGE, WAS REPAIRED (AS PERMANENT REPAIR) PER VOL I SRM 53- 30-01 FIG 17. (LP# 1036617)
Part: SKIN — CRACKED (BS 1494) · airframe 49,838 hrs · 33,113 cycles
CRACK ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE. PERMANENT REPAIR SCTION I WAS PERFORMED ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE. PER ETI- 90-19-016 REV. 1 AND ER/A 577192-14 REV. ORIGINAL. PERFORM WITHIN EVERY 3,000 CYCLES AFTER INSTALLATION OF SECTION I PERMANENT REPAIR: LOG 1032923 PER ER/A 577192-14 REV. ORIGINAL.
Part: SPAR — CORRODED (LT WING) · airframe 49,834 hrs · 33,112 cycles
REAR SPAR LOWER CHORD / BS 161 / LEFT WING / CORROSION REMOVAL PSE 57.11.02.2 - PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION OF ER/A 525623-14AD IS REV. C. RESULTS OF STAGE II DTE/DTA HAVE BEEN COMPLETED AND INCORPORATED AT THIS REVISION LEVEL. ACCOMPLISH SECTION IV: PERMANENT REPAIR : REMOVED TANK PLATES 520CB & 520DT REF. MD90AMM 28-00-00(426619) INSTALLED TANK PLATES 520CB & 520DT REF. MD90AMM 28-00-00 PERFORMED LEAK CHECK. NO LEAKS NOTED REF. MD90AMM 28-00-00 (933739) C/W ERA 525623-14AD REV D SECTION IV. NO DEFECTS NOTED. (LP#0972552)
Part: GROMMET — DEFECTIVE (WIPER MOTOR) · airframe 49,649 hrs · 32,999 cycles
CAPT PFD INOP CB POPPED. ELECTRICAL BURN SMELL EVIDENT. REPOSITIONED CAPTS INSTRUMENT PANEL AND INSP AREA NO LEAKS NOTED. APPLIED WATER TO CAPT WINDSHIELD AND WIPER MOTOR AREA. NO LEAKS FOUND. PRESSURIZED A/C FOUND CAPT WIPER MOTOR LEAKS FROM PLATE AND GROMMET. R/R CAPT'S WIPER GROMMET PER AMM 30-43. R/R CAPTS PFD PER AMM 34-23. OK FOR SVC. (LP# 3787964)
Part: TERMINAL — LOOSE (WINDOW) · airframe 49,607 hrs · 32,972 cycles
SMOKE STARTED COMING FROM FWD WINDOW RIGHT SIDE OF COCKPIT STOPPED WHEN WINDSHIELD ANTI ICE SWITCH ON RT WAS TURNED OFF. WINDSHIELD DEACTIVATED PER MEL 30-41-01B C/W M PROCEDURES. FOUND LOOSE TERMINAL ON TERMINAL BLOCK OPS CK NML AFTER TIGHTENING. (LP# 3787948)
Part: CABLE — SEVERED (TAILCONE) · airframe 49,360 hrs · 32,796 cycles
TAILCONE JETTISON BOTLLE TRIGGER CABLE SEVERED IN HALF ONE HANGING. REMOVED AND REPLACED TAILCONE DISPLACEMENT SYST BALL VALVE CABLE. OK FOR SERVICE. (LP#5310303)
Earlier reports · 2008–2018 · 164 reports
2018
Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 48,383 hrs · 32,151 cycles
RIGHT MAIN LANDING GEAR FORWARD DOOR FRAME CHANNEL WAS CRACKED. REMOVED, DRILLED THE REPLACEMENT FRAME IAW DWG 5930584-503. INSTALLED THE DOOR FRAME IAW DWG 5930584.
Part: WIRE — BROKEN (AC BAY) · airframe 47,983 hrs · 31,917 cycles
AFT ACCESSORY COMPARTMENT LT SIDE OF CATWALK HAS INOP EMERGENCY LIGHT. IDENTIFIED FIXTURE AS L2-845. RANG FROM P1-1211 TO R5-3803, R5-3804. FOUND R5-3803 OPEN, INSPECTED FURTHER AND FOUND WIRE BROKEN IN AMPHENOL CONNECTER. RETERMINATED WIRE AND REINSERTED INTO CONNECTER. OK FOR SERVICE.
Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 47,788 hrs · 31,799 cycles
LOW HYD QTY LT SYSTEM. RAN QRH & TURNED OFF LT HYD PUMP. SYSTEM DID NOT REPRESSURIZE ON LANDING. FOUND THE LT LOWER INBOARD SLEEVE ACTUATOR LEAKING FROM THE SHAFT ON THE INSIDE OF THE LOWER THRUST REVERSER. R & R THE LOWER INBD NON-LOCKING ACTUATOR. AN EMERGENCY LANDING WAS MADE.
Part: CABLE — FRAYED (TAILCONE) · airframe 47,767 hrs · 31,784 cycles
TAIL CONE DISPLACEMENT SYSTEM ACTUATION PULL CABLE WORN/FRAYED. TAIL CONE DISPLACEMENT SYSTEM ACTUATION PULL CABLE REMOVED AND REPLACED IAW AMM 53-52.
Part: BOTTLE — LOW PRESSURE (TAILCONE) · airframe 47,613 hrs · 31,688 cycles
DURING A SERVICE CHECK, FOUND THE TAILCONE NITROGEN BOTTLE OUT OF RANGE FOR TEMP. SERVICED THE TAILCONE BOTTLE IAW AMM 12-18-01.
2017
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 46,486 hrs · 31,000 cycles
CATWALK EMERGENCY LIGHT INOPERATIVE. RESET A PIN IN THE CONNECTOR IAW SWPM. OPS CHECKED GOOD. (LP# 4020528)
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,476 hrs · 30,993 cycles
FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,498 hrs · 30,421 cycles
WHILE LOADING PASSENGERS, THE FLIGHT CREW REPORTED AN ODOR IN THE CABIN. ALSO NOTED ODOR IN COCKPIT. THE APU HAD INGESTED HYDRAULIC FLUID INTO THE APU INLET. ISOLATED LEAK TO CRIMP AT ELBOW TEE TO HYDRAULIC FILTER. PERFORMED ALTERNATE DUCT BURNOUT.
Part: RETAINER — DAMAGED (GIRT BAR) · airframe 44,960 hrs · 30,121 cycles
BRACKET THAT HOLDS GIRT BAR AT R1 DOOR HAS A SPLIT IN IT AND GIRT BAR DROPS DOWN. INSTALLED NEW RETAINER ASSEMBLY. OPERATION CHECKED OK.
Part: BUSHING — SCRATCHED (HORIZONTAL STAB) · airframe 44,863 hrs · 30,065 cycles
HORIZONTAL STABILIZER SCRATCHED ON RIGHT BUSHINGS,XE49, XE103, AN XE157. REPLACED THE BUSHINGS IAW ERA 549239-14, REV O.
Part: BUSHING — SCRATCHED (HORIZONTAL STAB) · airframe 44,863 hrs · 30,065 cycles
SCRATCHES ON HINGE BUSHINGS. NEW BUSHINGS INSTALLED IAW ERA 556356-14, REV O.
Part: BUSHING — SCRATCHED (HORIZONTAL STAB) · airframe 44,863 hrs · 30,065 cycles
HORIZONTAL STABILIZER SCRATCHED ON RIGHT BUSHINGS. NEW BUSHINGS INSTALLED IAW ERA 549239-14, REV O.
Part: INTERCOSTAL — CORRODED (BS 1269-1288) · airframe 44,863 hrs · 30,065 cycles
AFT CARGO BAY CORRODED ON THE INTERCOSTAL, BS 1269 - 1288, LONGERON 29L. REPLACED THE INTERCOSTAL IAW SRM 51-30-05.
Part: FRAME — CRACKED (BS 962) · airframe 44,863 hrs · 30,065 cycles
CRACKED ON OVERWING FRAME, BS 962, LEFT. REPLACED THE FRAME IAW SRM 51-30-02 AND 51-30-05.
Part: SPAR — DAMAGED (LEFT WING) · airframe 44,863 hrs · 30,065 cycles
BENT DIAPHRAGM AND ELONGATED RIVET HOLE ON LEFT WING REAR SPAR, XRS 457. REPAIRED IAW SRM 51-10-05 AND 57-00-01.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON BARREL NUT HOLES NR 10, 12, AND 13 LEFT SIDE, XH=7 HORIZONTAL STABILIZER. COMPLIED WITH ERA 556327-14.
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON HORIZONTAL STABILIZER SKIN. REPAIRED IAW ERA 556326-14, REV O.
Part: FUEL TANK — CORRODED (BS 926) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CENTER FUEL TANK BS 926, LBL 56. REPAIRED IAW ERA 555641-14AD.
Part: LONGERON — CORRODED (BS 168-218) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON LONGERON 30 BETWEEN BS 168 AND 218 E/E COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 51-30-02, 53-10-01 AND 51-30-05.
Part: FUEL TANK — CORRODED (BS 898-902) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CENTER FUEL TANK, BETWEEN BS 898 AND 902, LBL 56. REPAIRED IAW ERA 555641-14AD.
Part: DOUBLER — CORRODED (BS 1395) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON PRODUCTION DOUBLER AT AFT PRESSURE BULKHEAD BETWEEN LONBERONS 28L AND 28R, BS 1395. REPLACED IAW SRM 51-10-03 AND 51-30-05.
Part: FRAME — CRACKED (BS 1508) · airframe 44,863 hrs · 30,065 cycles
CRACKED FRAME ANGLE, BS 1508 BETWEEN LONGERON 4R - 4L AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-02 AND DWG 9911860.
Part: FRAME — CRACKED (BS 1508) · airframe 44,863 hrs · 30,065 cycles
CRACKED FRAME BS 1508. REPLACED IAW SRM 51-10-05 AND DWG 9911860-3.
Part: FRAME — CRACKED (BS 1443) · airframe 44,863 hrs · 30,065 cycles
CRACK ON FRAME BS 1443.. REPAIRED IAW SRM 53-10-02. (LP# 2937224)
Part: CUSP WEB — CORRODED (BS 1212-1269) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON RIGHT CUSP WEB BETWEEN BS 1212 AND 1269, RBL 54 AND 60. REPAIRED IAW SRM 53-20-02, 51-30-01, 51-30-02, AND 51-30-05.
Part: WEB — CRACKED (BS 1520) · airframe 44,863 hrs · 30,065 cycles
CRACK ON WEB AFT FACE, BS 1520 AT THE 10 O'CLOCK POSITION. REPLACED WEB AND STIFFENERS IAW SRM 53-10-04 AND 51-30-05.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 44,863 hrs · 30,065 cycles
AFT ACCESSORY COMPARTMENT CRACK ON LONGERON 12 L STA 1494. REPAIRED IAW SRM 53-10-01.
Part: FLOORBEAM — CORRODED (BS 1364) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOORBEAM, BS 1364, RBL 16 TO LBL 16. FOUND TO BE OUT OF LIMITS. REPLACED SUPPORT IAW SRM 53-10-03, 51-30-05, AND 51-10-03.
Part: FLOOR SUPPORT — CORRODED (BS 1364-1404) · airframe 44,863 hrs · 30,065 cycles
CORRODED FLOOR SUPPORT BS 1364 - 1404 RBL 18. REPLACED IAW SRM 51-30-01 AND DWG 9936656.
Part: CUSP WEB — CORRODED (BS 1227-1238) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CUSP WEB, BS 1227-1238, RBL 54 TO 60. REMOVED AND INSTALLED IAW SRM 53-20-02 AND 51-30-01.
Part: INTERCOSTAL — CRACKED (BS 984) · airframe 44,863 hrs · 30,065 cycles
CRACK ON INTERCOSTAL, BS 984, RBL 44, Z=-6. REPAIRED IAW SRM 51-70-01.
Part: WEB — CORRODED (BS 180-200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON DIAPHRAGM FROM BS 180-200, RBL 9 TO 44 AND LBL 9 TO 44. REPAIRED IAW SRM 51-11-01.
Part: FLOOR SUPPORT — CORRODED (BS 160-196) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT BS 160 - 196, LBL 54. REPLACED IAW SRM 51-30-01 AND 51-30-05.
Part: CUSP WEB — CORRODED (BS 386-589) · airframe 44,863 hrs · 30,065 cycles
CORRODED ON RIGHT CUSP WEB, BS 386 - 430 AND 589, RBL 54 - 60. REPAIRED IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 385-394) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CUSP WEB, BS 385-394, RBL 54 - -60. REPAIRED IAW SRM 53-20-02.
Part: FLOOR SUPPORT — CORRODED (BS 200-256) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT BS 200 - 256, LBL 16. REPLACED THE FLOOR SUPPORT IAW SRM 53-10-01, 51-10-05, 51-30-02, AND 51-30-05.
Part: FLOORBEAM — CORRODED (BS 200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOORBEAM BS 200, RBL 9 AND 46 . REPLACED IAW SRM 51-30-02, 51-305 AND 51-10-01.
Part: FLOOR SUPPORT — CORRODED (BS 200-256) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT BS 200 - 256, LBL 16. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-10-01, 51-10-05, AND 51-30-02.
Part: WEB — CORRODED (BS 148-200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON DIAPHRAGM FROM BS 148-200, RBL 8 TO LBL 8. REPAIRED IAW SRM 51-11-01.
Part: CUSP WEB — CORRODED (BS 712-750) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CUSP WEB BETWEEN BS 712 - 750, RBL 54 - 60. REPAIRED IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 510-628) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON CUSP WEB BS 510 AND 618-628, LBL 54 - 60 ON UPPER AND LOWER SURFACE. REPAIRED IAW SRM 53-20-02 AND 51-30-02.
Part: HOUSING — WORN (CARGO DOOR) · airframe 44,863 hrs · 30,065 cycles
WEAR INSIDE OF HANDLE HOUSING ON THE CARGO DOOR. REPAIRED IAW SRM 51-30-02, AND 51-30-05.
Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT BS 148-200, X=8 . REPLACED THE FLOOR SUPPORT IAW SRM 51-30-01.
Part: SEAT TRACK — CORRODED (BS 299-317) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON SEAT TRACK BS 299 - 302 AND 317, RBL 54. REPAIRED IAW SRM 53-40-01, AND 51-10-03.
Part: CUSP WEB — PUNCTURED (BS 945) · airframe 44,863 hrs · 30,065 cycles
PUNCTURE ON CUSP WEB, BS 945 BETWEEN LBL 54 TO 60. PLUGGED IAW SRM 53-00-01.
Part: ANGLE — CRACKED (BS 883) · airframe 44,863 hrs · 30,065 cycles
CRACKED ANGLE ON INTERCOSTAL, BS 883, RBL 42, Z=-6. REPAIRED IAW SRM 51-30-05 AND ERA 498192-14MA.
Part: FLOORBEAM — CORRODED (BS 180) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOORBEAM BS 180 BETWEEN RBL 9 TO 44. FOUND TO BE OUT LIMITS. REMOVED AND REPLACED IAW SRM 51-10-05.
Part: FLOOR SUPPORT — CORRODED (BS 160-196) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT BS 160 AND 196 BETWEEN LBL 54. REPLACED IAW SRM 53-10-01 AND 51-10-05.
Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 44,863 hrs · 30,065 cycles
CORRODED ON FLOOR SUPPORT BS 148-200, BETWEEN RBL 8. REPLACED IAW SRM 51-30-05.
Part: CUSP WEB — CRACKED (BS 218) · airframe 44,863 hrs · 30,065 cycles
CRACK ON CUSP WEB, BS 218, RBL 44. REPAIRED IAW SRM 53-20-02.
Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FLOOR SUPPORT, BS 160 - 200 RBL 44 AND 52. REPLACED IAW SRM 51-30-02 AND 51-30-05.
Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 44,863 hrs · 30,065 cycles
ELONGATED HOLES ON ACCESS PLATES 620CB AND 620PB. REPLACED THE ACCESS PANELS.
Part: FLOOR SUPPORT — CORRODED (BS 195-200) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON THE FLOOR SUPPORT BS 195-200 LBL 15. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-02 AND 51-30-05.
Part: PAN — WORN (CARGO DOOR) · airframe 44,863 hrs · 30,065 cycles
WEAR ON AFT EDGE INNER PAN BETWEEN BEAMS 1 AND 2 AT FORWARD CARGO DOOR. REPAIRED IAW SRM 52-30-02.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FUEL ACCESS PANEL 520DT. REPLACED THE ACCESS PANEL.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON FUEL TANK ACCESS PANEL 620DT. REPLACED THE ACCESS PANEL.
Part: BEAM — CRACKED (L1 DOOR) · airframe 44,863 hrs · 30,065 cycles
L1 DOOR CRACKED MID SECTION ON BEAM NR 6. DAMAGED AREA TRIMMED OUT AND REPAIRED IAW ERA 498178-14 MA, REV O.
Part: FLOORBEAM — CORRODED (BS 196) · airframe 44,863 hrs · 30,065 cycles
FORWARD WET AREA CORROSION ON FLOORBEAM BS 196 BETWEEN LBL 16 TO 44, REPLACED THE FLOORBEAM IAW SRM 51-30-02.
Part: LONGERON — CRACKED (BS 256) · airframe 44,863 hrs · 30,065 cycles
CRACKED LONGERON 17L AT BS 256. REPAIRED IAW SRM 53-10-01.
Part: FLOOR SUPPORT — CORRODED (BS 196) · airframe 44,863 hrs · 30,065 cycles
FORWARD WET AREA, CORROSION FOUND ON FLOOR SUPPORT, BS 196, LBL 44 AND 54. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-02.
Part: BEAM — CRACKED (L1 DOOR) · airframe 44,863 hrs · 30,065 cycles
L1 DOOR CRACKED AT AFT EDGE ON BEAM NR 7. REPAIRED THE BEAM IAW SRM 52-10-02.
Part: WEB — CORRODED (E/E BAY DOOR) · airframe 44,863 hrs · 30,065 cycles
CORROSION ON WEB DOOR E/E. FOUND TO BE OUT OF LIMITS PER ERA 511165. REPAIRED IAW SRM 52-00-01, AND ERA 5111165.
Part: SKIN — DAMAGED (BS 70) · airframe 44,863 hrs · 30,065 cycles
FUSELAGE PREVIOUS BLEND OUT ON EXTERNAL SKIN, BS 70, LONGERON 24L. REPAIRED IAW ERA 511165.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,860 hrs · 30,064 cycles
EMERGENCY OVERHEAD LIGHTS BETWEEN 1DE TO 11CDE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND EMERGENCY POWER SUPPLY B5-227 IAW MM. OPERATION CHECKS GOOD.
Part: UNKNOWN — ODOR (CABIN) · airframe 44,843 hrs · 30,055 cycles
ELECTRICAL OR RUBBER ODOR NOTED BY FLIGHT CREW UPON ENTERING AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND LEFT APU DOOR BLANKET SOILED. NO ACTIVE LEAK. CLEANED INLET. REMOVE AND REPLACED COALESCE BAGS AND PERFORMED DUCT BURNOUT.
2016
Part: ACCESS PANEL — CRACKED (RT WING) · airframe 42,898 hrs · 28,920 cycles
CRACK ON COUNTERSINK AREA AT FUEL ACCESS PLATE NR 620DT, RT WING. REPLACED IAW SRM 57-00-09.
Part: WIRE — BROKEN (L1 DOOR SLIDE) · airframe 42,893 hrs · 28,918 cycles
L1 SLIDE HAS BROKEN WIRES ON LANYARD. SLIDE WAS REPLACED IAW MM.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 42,893 hrs · 28,918 cycles
CRACK ON RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE AT DORSAL FIN AREA. REPLACED SAME IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 42,893 hrs · 28,918 cycles
CRACK ON UPPER AREA, ON RT FORWARD OVERWING EMERGENCY DOOR JAMB. REPAIRED IAW SRM 53-60-02, FIG 4.
Part: CHANNEL — CRACKED (LT MLG WW) · airframe 42,893 hrs · 28,918 cycles
CRACK AFT INBD CHANNEL, BS 983, X 8 AT LT MLG WHEEL WELL DOOR FRAME AREA. R & R CHANNEL IAW SRM 530-02 AND DWG 5930584.
Part: BEAM — CRACKED (L1 DOOR) · airframe 42,893 hrs · 28,918 cycles
CRACKED BEAM, NR 1, AT L1 DOOR, FORWARD AND AFT SECTION. REPAIRED SECTION IAW SRM 52-10-02. HFEC, 2 CRACKS WERE FOUND ON BEAM NR 1.
Part: CHANNEL — CRACKED (MLG DOOR FRAME) · airframe 42,893 hrs · 28,918 cycles
CRACK AFT INBD CHANNEL, BS 983, X -8, RT MLG WHEEL WELL DOOR FRAME AREA. R & R CHANNEL IAW SRM 51-30-02, 51-30-05, 51-10-03 AND DWG 5930574, REV BY.
Part: CHANNEL — CRACKED (RT MLG WW) · airframe 42,893 hrs · 28,918 cycles
CRACK AFT INBD CHANNEL , BS 983, X=-8, RT MLG WHEEL WELL DOOR FRAME AREA. R & R CHANNEL IAW SRM 51-30-02, 51-30-05, 51-10-03 AND DWG 5930574, REV BY.
2015
Part: BOLT — MISSING (CATWALK) · airframe 41,580 hrs · 28,132 cycles
AFT VENTRAL STAIRS CATWALK HANGS DOWN 6" WITH STAIRS DOWN. FOUND BOLT MISSING ON RT CABLE TENSION CRANK ARM. REPLACED SAME. OPS CHECKS OK.
Part: TURNBUCKLE — BROKEN (AIRSTAIR) · airframe 40,818 hrs · 27,679 cycles
DURING SERVICE CHECK, FOUND CABLE AND TURNBUCKLE ASSY ON RT SIDE OF VENTRAL CATWALK BROKEN. REPLACED TURNBUCKLE ON RT SIDE. OPS CHECKED GOOD.
Part: STRAP — DISENGAGED (TAILCONE SLIDE) · airframe 39,827 hrs · 27,074 cycles
LEFT TAILCONE SLIDE HOLD DOWN STRAP DISENGAGED FROM WALKWAY CLIP. ATTACHED LEFT TAILCONE EVACUATION SLIDE HOLD DOWN STRAP TO WALKWAY IAW AMM.
Part: NONE — HANDLER ERROR (NONE) · airframe 39,827 hrs · 27,074 cycles
LEFT WINGTIP SUSTAINED EXTENSIVE DAMAGE FROM ANOTHER ACFT. R & R WINGTIP IAW PRI 533962-14.
2014
Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 37,558 hrs · 25,630 cycles
NOSE WHEEL WELL FORWARD AVIONICS DOOR FRAME PAN CRACKED AT AFT LOWER RADIUS. REPAIRED ERA 52607-14 REV O.
Part: SPAR — CORRODED (LT WING) · airframe 37,558 hrs · 25,630 cycles
LEFT WING REAR SPAR LOWER ANGLE CORRODED AT XRS 164, REPAIRED IAW ERA 525623-14, REV O.
Part: SKIN — CRACKED (BS 1520) · airframe 37,558 hrs · 25,630 cycles
TAIL INTERIOR FUSELAGE SKIN DOUBLER HAS A ONE INCH LONG CRACK, BS 1520. REPAIRED IAW SRM 53-10-03, FIG 20.
Part: SPAR — CORRODED (LT WING) · airframe 37,604 hrs · 25,661 cycles
CORROSION FOUND ON THE LOWER SURFACE OF THE LEFT WING REAR SPAR, LOWER ANGLE. AREA WAS BLENDED IAW ERA 92-525623.
Part: SKIN — WORN (VERTICAL STAB) · airframe 37,529 hrs · 25,619 cycles
VERTICAL STABILIZER L/E PANEL AT UPPER END OF ZFS52.267 HAS 14 EA FASTENERS WORN IN SKIN. HFEC HOLES. FABRICATED BUSHING ON N/R 14 IAW DWG SG09530004. INSTALLED REPAIR BUSHINGS.
Part: BUSHING — CORRODED (MLG ACTUATOR) · airframe 37,529 hrs · 25,619 cycles
LT MLG RETRACT ACTUATOR INBD SUPPORT BUSHING BOSS, CORROSION PITS ON INBD LOWER SURFACE NEAR EDGE. MACHINED ACTUATOR IAW CARD 5740-01140-0101.
Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD DEICE) · airframe 37,075 hrs · 25,336 cycles
DURING DESCENT, CENTER WINDSHIELD, RT POST APPEARED TO OVERHEAT. GAVE OFF A STRONG BURNING ODOR AND SMALL PUFF OF SMOKE. FLIGHT CREW TURNED OFF WINDSHIELD ANTI-ICE. ODOR DISSIPATED. WIRES IN WINDSHILED BURNED. R & R CENTER WINDSHIELD IAW AND ANTI-ICE CONTROLLER. CHECKED GOOD.
2013
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,346 hrs · 24,880 cycles
DURING SERVICE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESET AFT BATTERY RACK. OPS CHECKED GOOD.
Part: SLIDE — LOOSE (TAILCONE) · airframe 36,068 hrs · 24,715 cycles
DURING TAIL CONE DROP, AFT ESCAPE SLIDE CAME UNPACKED. REPLACED AFT ESCAPE SLIDE IAW WC 2500-4332 & AMM 53-52-01-420-801.
Part: RELEASE CABLE — BROKEN (TAILCONE) · airframe 36,068 hrs · 24,715 cycles
DURING TAILCONE DROP, CABLE PRESSURE RELEASE PULL CABLE BROKE OFF. R & R PRESSURE RELEASE CABLE FOR ASSIST BOTTLE IAW AMM 53-52.
2012
Part: CABLE — MISINSTALLED (COCKPIT DOOR) · airframe 34,081 hrs · 23,591 cycles
DURING SERVICE CHECK, MX FOUND COCKPIT DOOR EMERGENCY EGRESS HINGE CABLE HALF WAY OUT. REINSTALLED HINGE CABLE IAW MM. OK FOR SERVICE.
Part: CABLE — OUT OF RIG (TAIL) · airframe 33,943 hrs · 23,521 cycles
DURING INSPECTION AND RIG CHECK OF CATWALK, MX FOUND CABLE TENSIONS LOW. ADJUSTED LIFT CABLES IAW AMM. OPS CHECKS GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,847 hrs · 23,461 cycles
DURING SERVICE CHECK, MX FOUND L2 DOOR FORWARD EXIT LIGHT INOPERATIVE. MX TROUBLESHOT IAW WDM. FOUND EMERGENCY BATTERY POWER SUPPLY B5-241 BAD. R & R EMERGENCY POWER SUPPLY IAW AMM. OPS CHECKED GOOD.
Part: BOLT — BROKEN (CATWALK) · airframe 33,664 hrs · 23,345 cycles
DURING SERVICE CHECK, MAINTENANCE FOUND CATWALK IS DOWN WHEN AFT STAIRS ARE DOWN AND WILL NOT GO UP IN STOWED POSTION. REPLACED BROKEN BOLT AND TORQUE TUBE ADAPTER PER AMM.
Part: LANYARD — DETACHED (COCKPIT DOOR) · airframe 32,388 hrs · 22,655 cycles
FLIGHT CREW FOUND COCKPIT DOOR EMERGENCY EGRESS LANYARD DETACHED (RED ROUND RING). MAINTENANCE RE-ATTACHED LANYARD. OPERATION CHECKS NORMAL. DOOR HINGE RELEASE HANDLE ASSEMBLY OK FOR SERVICE.
2011
Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 30,465 hrs · 21,696 cycles
DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM COCKPIT SWITCH. MAINTENANCE REMOVED AND REPLACED S1-177 EMERGENCY LIGHT SWITCH, SLAVED IN AUXILIARY EMERGENCY POWER RELAY R2-680 AND MWCC B5-98, BUT THE SYSTEM REMAINED INOPERABLE. RESET EMERGENCY LIGHT ARM CHARGE CIRCUIT BREAKER. SYSTEM OPERATION NOW CHECKS GOOD.
Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 FWD CARGO STA 484-503 LONG 30 FASTENERS RUSTY. REPLACED LONGERON SPLICE AND FASTENERS PER SRM 51-30-05.
Part: LONGERON — CORRODED (BS 484-503 L30) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO COMPT BETWEEN STA 484 AND STA 503, STR 30 FASTENER WITH RUST (MK11-25) COMPLIED WITH ON NON-ROUTINE W/O 2003107, ZONE 1000, ITEM 0135. R & R LONGERON 30 SPLICE AND HARDWARE AT FWD CARGO BETWEEN STA 484 TO STA 503 IAW SRM 51-30-05.
Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 FWD CARGO COMP BETWEEN 484-503 STR 29LT CORROSION ON FASTENERS. REPAIRED/REPLACED LONGERON 29LT SPLICE AND FASTENERS PER SRM 51-30-05.
Part: LONGERON SPLICE — CORRODED (BS 484-503) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO COMPT BETWEEN STA 484 AND STA 503, STR 29 LT FASTENER WITH RUST (MK11-26). COMPLIED WITH ON NON-ROUTINE W/O 2003107, ZONE 1000, ITEM 0136. R & R LONGERON SPLICE AND HARDWARE AT FWD CARGO BETWEEN STA 484 AND STA 503, LONGERON 29 LT IAW SRM 51-30-05.
Part: FRAME — MISREPAIRED (BS 1364) · airframe 29,883 hrs · 21,436 cycles
FRAME REPAIR AT STA 1364 SPLICE PLATES WITH NO ED COMPLIED WITH COMPARTMENT STA 1364 BETWEEN L 28L AND 29L AND AT LONG 29R AS PER MD 90 SRM 51-30-05- SRM 53-10-02 SRM 51-10-04 AND 51-20-00.
Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO COMPT LT TIE DOWN TRACK FROM STA 1060 TO STA 1155, WITH SURFACE CORROSION. COMPLIED WITH W/O 2003107 ITEM 0091. REMOVED AFT CARGO COMPT LT TIE DOWN TRACK FROM STA 1060 TO STA 1155. REF SRM 51-30-05. INSTALLED NEW TIE DOWNTRACK AND SPLICE REF SRM 51-30-05 AND 53-40-01.
Part: FRAME — MISINSTALLED (BS 1344) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO COMPARTMENT STA 1344 BETWEEN L 29R AND 29LT CIRCUMFERENTIAL REPAIR WENT IN DRY, NO SHIMS INSTALL IN THE BOW REPAIR AND FASTENERS HAVE NO EDGE DISTANCE DOT- 30-01. COMPLIED WITH W/O 2003107 ITEM 0326. INSTALLED CIRCUMFERENTIAL REPAIR WITH SHIMS AND SEALANT CARGO COMP STA 1344 BETWEEN L 29RT AND 29 LT PER SRM 53-10-02 SRM 51-30-02 SRM 51-30-05 AND SRM 51-20-00.
Part: FRAME — MISREPAIRED (BS 1328) · airframe 29,883 hrs · 21,436 cycles
REPAIR IN AFT CARGO COMP STA 1328 BETWEEN STR 28R AND 28L CIRCUMFERENTIAL NOT PERFORMED PER SRM 53-10-02 PAR 27 ITEM 8 AND SRM 51-20-00 DID NOT USR SEALER O0N REPAIR PARS. COMPLIED WITH AT AIR MIAMI ON W/O 2003107 ITEM 0325 REMOVED REPAIR (2 SECTIONS) AND APPLIED PRY AND REINSTALL AT AFT CARGO COMP STA 1328 BETWEEN STR 29R AND 28L CIRCUMFERENTIAL PER SRM 53-10-02 PAR 27 ITEM 8 AND SRM 51-20-00.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPT BETWEEN STA 636 AND STA 655 LT TIE DOWN TRACK WITH CORROSION. COMPLIED WITH ON W/O 2003107 ITME 0026.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPT. BETWEEN STA 636 AND STA 655 LT TIE DOWN TRACK WITH CORROSION (MK 11-11). COMPLIED WITH W/O 2003107 ITEM 0026.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 CTR CARGO COMP STA 655 LT TIE DOWN TRACK CORRODED. REPLACED TRACK STA 598-845 LT PER SRM 51-30-03.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO COMPT. TIE DOWN TRACK HAS SIX CORROSION SPOTS AND IS DIRTY. DOT 80-33 LOCATED AT 28R STA 1212 TO STA 1145. COMPLIED WITH W/O 2003107 ITEM 0232.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 29,883 hrs · 21,436 cycles
HMV2 CABIN FLOOR PANEL CRACKED PNL NR 221XF. PANEL REPAIR PER SRM 51-10-03 AND TIMCO DWG 09T229MO42.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO COMPARTMENT STA 1344 BETWEEN STR 29RT AND STR 29 LT CIRCUMFERENTIAL WITH CORROSION (KM 11-16). COMPLIED WITH AT AAR MIAMI ON W/O 2003107 ITEM 0106.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPT STA 598, CENTER FLOOR SUPPORT PANEL, WITH CORROSION (MK 11-09), COMPLIED WITH W/O 2003107 ITEM 0024. REMOVED CORROSION FLOOR SUPPORT 2 MATERIAL FOUND OUT OF LIMITS3. REMOVED FLOOR SUPPORT 4 DRILLED AND LOCATED HOLES NEW PART5 INSTALLED FLOOR SUPPORT ALL THE STEPS AS PER B MD90 SRM 51-10-03, 53-00-01, 51-10-05, 51-30-05.
Part: FRAME — CORRODED (RT MLG WW) · airframe 29,883 hrs · 21,436 cycles
HMV2 RT WHEEL WELL FWD CUTOUT FRAME CORRODED. REPLACED FRAME PER SRM 51-30-02.
Part: WEB — CRACKED (RT MLG WW) · airframe 29,883 hrs · 21,436 cycles
HMV2 RT MLG WHEEL WELL CUTOUT WEB CRACKED. REPLACED WEB PER SRM 51-30-02
Part: WEB — CRACKED (RT MLG WW) · airframe 29,883 hrs · 21,436 cycles
RT WHEEL WELL CUTOUT WEB OTBD FWD HAS CRACK BELOW UPLOCK SENSOR SWITCH MKD DOT 024. COMPLIED WITH AT AAR MIAMI ON W/O 2003107 ITEM 0013. REMOVED AND REPLACED WEB AS PER SRM 51-30-02.
Part: FRAME — CORRODED (RT MLG WW) · airframe 29,883 hrs · 21,436 cycles
RT WW FWD CUTOUT FRAME AND BRACKETS HAVE CORROSION AT INBD AREA. COMPLIED WITH ON NON-ROUTINE W/O 2003107, ZONE1000, ITEM 0159. R & R FRAME IAW 51-30-2.
Part: SKIN — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
LOWER FUSELAGE VHF 1 ANTENNA MOUNTING SURFACE CORRODED. COMPLIED WITH AT W/O 2003107, ITEM 0298. REMOVED CORROSION AT LOWER FUSELAGE VHF 1 ANTEN IAW SRM 51-10-03, MAX MATERIAL FOUND 0.60, MIN MAT FOUND 0.580, MAT LOSS 0.020, FOUND WITHIN LIMITS IAW SRM 53-00-01. TREATED AREA IAW SRM 51-10-03.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPT BETWEEN STA 522 AND STA 541, LT TIE DOWN TRACK, WITH CORROSION (MK 11-02) COMPLIED WITH W/O 20033107 ITEM 0017. REMOVED CORROSION AT CENTER CARGO COMPT BETWEEN STA 522- 541 LT TIEDOWN TRACK, FOUND OUT OF LIMITS PER RF 53-00-01. REMOVE DAMAGE TIE DOWN SRM 51-30-01, 51-30-05, PREPARATION OF HOLE AT NEW TIE DOWN TRACK, PRIMED AND TOP COATING NEW TIE DOWN TRACK REF SRM 51-10-05, 51-10-03 AND INSTALLED NEW TIE DOWN TRACK REF 51-30-01, 51-30-05.
Part: SKIN — CORRODED (FS 946-952) · airframe 29,883 hrs · 21,436 cycles
CTR WING BOTTOM SKIN LWR SURFACE HAS IG CORROSION SPOTS FS 946-952, RBL14-19. COMPLIED WITH AT W/O 2003107, ITEM 0155. REMOVED SURFACE CORROSION IAW SRM 51-10-03 AT SKIN, FS946-952, RBL14-19, MAX MAT FOUND 0.220, MIN MAT FOUND 0.188, MAZ LOSS 0.032, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01, TREATED IAW SRM 51-10-03.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 CTR CARGO COMP LT TIE DOWN TRACK STA 522-541 CORRODED. REPLACED TRACK PER SRM 51-30-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
LOWER FUSELAGE SKIN HAS CORROSION AT RAD/ALT ANTENNA STA 779. COMPLIED WITH W/O 2003107 ITEM 0115.
Part: SKIN — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
LOWER FUSELAGE SKIN HAS CORROSION RAD/ATL ANTENNA STA 665. COMPLIED WITH W/O 2003107 ITEK 0112.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO COMP RT TIE DOWN TRACK FROM STA 1060 TO 1155. WITH SURFACE CORROSION (MK). COMPLIED WITH W/O 20033107 ITEM 0045. REMOVED CORROSION REF MD90 SRM 51-10-05 AND FOUND OUT OF LIMITS, REF MD90 SRM 53-40-001. REMOVED RT TIE DOWN TRACK FROM STA 1060 TO DTA 1155 REF MD90 SRM 51-30-001 AND 51-30-02 LOCATED AND DRILLED NEW TIE DOWN TRACK FROM STA 1060 TO 1155 RT REF MD90 SRM 51-30-05. INSTALLED NEW TIE DOWN TRACK FROM STA 1060 TO STA 1155 RT REF MD90 SRM 51-30-01 AND 51-30-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 CTR CARGO STA 598 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-10-03.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 FWD CARGO FLOOR SUPPORT CORRODED STA 218. REPLACED FLOOR SUPPORT PER SRM 51-30-01.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO COMPT STA 218 LOWER SUPPORT FLOOR PANEL WITH CORROSION (MK 11-20). REMOVED CORRODED PART, DRILLED NEW FLOOR SUPPORT AND INSTALLED NE FLOOR SUPPORT AT FWD CARGO COMPT STA 218 LOWER REF MD90 SRM 51-30-01,51-10-05.
Part: TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 FWD CARGO STA 218-370 LT TIE DOWN TRACK CORRODED. REPLACED TRACK PER SRM 53-00-01.
Part: CARGO TRACK — CORRODED (BS 218-370) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO COMP FROM STA 218 TO 370 LT TIE DOWN TRACK WITH SURFACE CORROSION. REMOVED CORROSION AT FWD CARGO COMP LT TIE DOWN TRACK FOUND OUT OF LIMITS REF SRM 51-10-03, 53-00-01 PREPARTION OF THE HOLE IN NEW TIE DOWN BEFORE INSTALL REF 51-10-05, REMOVE DAMAGED TIE DOWN TRACK REF 51-10-01,53-10-02 TREATED PRIMED AND TOP COATED HOLE AND INSTALLED NEW TIE DOWN TRACK.
Part: ANGLE — CORRODED (BS 218 BULKHEAD) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO AT FWD BULKHEAD STA 218 T-ANGLE BELOW FLOOR SUPPORT CORRODED. R & R T-ANGLE, DRILLED NEW T-ANGLE, TREATED AND PRIMED . HOLE AND AREA AND INSTALLED NEW T-ANGLE AT FWD CARGO AT FWD BULKHEAD STA 218. REFSRM 51-30-02,51-10-05, AND 51-10-03.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 FWD CARGO FWD BULKHEAD T-ANGLE CORRODED. REPLACED T-ANGLE PER SRM 51-30-02.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
FWD CARGO AT FWD BULKHEAD STA 218 T ANGLE BELOW FLOOR SUPPORT CORRODED. COMPLIED WITH W/O 2003107 ITEM 0301. REMOVED DAMAGED T ANGLE. DRILLED NEW T ANGLE TREATED AND PRIMED. HOLE AND AREAS AND INSTALLED NEW T ANGLE AT FWD CARGO AT FWD BULKHEAD STA 218. REF MD90 SRM 51-30-02, 51-10-05, 51-10-03.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPT BETWEEN STA 579 AND STA 598 STR 28 LT WITH CORROSION AND HARDWARE HAS EVIDENCE OF RUST (MK 11-04). REMOVED HARDWARE, MATERIAL FOUND OUT OF LIMITS, TREATED AND PRIME AND TOP COAT. INSTALLED HARDWARE PRIOR STEP, REMOVED CORROSION ALL THE STEPS AS PER B-MD90 SRM 51-10-03, 53-00-01 AND 51-30-05.
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO DOOR LOWER STOP CUTOUT CRACKED. REPAIR PER SRM 52-30-02.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 - CTR CARGO STA 693 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-05.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 - CTR CARGO BETWEEN STA 750-845 RT TRACK CORRODED. REPLACED TRACK PER 51-30-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
MAIN CABIN RT FWD OTBD SEAT TRACK INBD SIDE TRACK AND FLANGE HAVE CORROSION BETWEEN STA 200-237 MKD-DOTS 021. COMPLIED WITH W/O 2003107 ITEM 0042. REMOVE CORROSION AS PER MD90 SRM 51-10-03 FOUND TO BE OUT OF LIMITS AS PER MD90 SRM 53-40-01. CUT OUT DAMAGE SECTION AND INSTALLED NEW REPAIR AS PER MD SRM 53-40-01 PG 10.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 E/E COMP LONG 28R STA 168 CORRODED. REPAIRED PER SRM 53-10-01 FIG 12.
Part: LONGERON — CORRODED (BS 168 L28R) · airframe 29,883 hrs · 21,436 cycles
E & E COMPARTMENT STA 168, CORROSION UNDER LONGERON 28R, COMPLIED WITH AT W/O 2003107B, ITEM 0084. REMOVED DAMAGED SECTION OF LONGERON IN REF WITH SRM 51-30-02 AND 53-10-01. FABRICATED SPLICE IN REF WITH SRM 53-10-01. INSTALLED NEW LONGERON SECTION AND SPLICE IN REF WITH SRM 53-10-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,883 hrs · 21,436 cycles
HMV2 CABIN RT FWD SEAT TRACK STA 200-237 CORRODED. REPAIR PER SRM 53-40-01.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
CENTER CARGO COMPARTMENT BETWEEN STA 750 AND STA 845 RT TIE DOWN TRACK WITH SURFACE CORROSION (MK 11-20). COMPLIED WITH W/O 2003107 ITEM 0035.B. REMOVED AND REPLACED TIE DOWN TRACK BETWEEN STA 750 THRU 845 RT SIDE AS PER MD90 SRM 51-30-01.
Part: FLOOR SUPPORT — CORRODED (BS 693) · airframe 29,883 hrs · 21,436 cycles
CTR CARGO COMPARTMENT, STA 693, CTR FLOOR SUPPORT PANEL WITH CORROSION AND HARDWARE HAS EVIDENCE OF RUST (MK 11-14). COMPLIED WITH W/O 2003107, ITEM 0029. R & R FLOOR SUPPORT PN 5936597U505 AT STA 693 BETWEEN L28R- L28L IAW SRM 51-30-05 AND SRM 51-30-02.
Part: SEAL — DENTED (HORIZ STAB) · airframe 29,883 hrs · 21,436 cycles
HMV2 RT HORIZ STAB REAR SPAR SEAL DENTED. REPAIR PER ERA 487468-14.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO COMP TIE DOWN TRACK CORRODED STA 1212-1145 RT. REPLACED TRACK PER SRM 51-30-01.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO COMP RT TIE DOWN TRACK STA 1269-1307 CORRODED. REPLACED TRACK PER SRM 51-30-01.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 29,883 hrs · 21,436 cycles
INNER DORSAL FIN JOINT ANGLE RT FOUND CRACKED / DAMAGED ANGLE WAS REPLACED REF SRM 51-10-05, 51-30-02 AND 51-30-05. FUSELAGE SKIN CRACK FOUND AT STA 1475 DAMAGED AREA WAS CUT OUT AND REPAIR INSTALLED PER ERA 487464-14AD REF N/R S/N 499893.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
CABIN FLOOR SUPPORT CORRODED STA 1364-1395. REPLACED FLOOR SUPPORT IAW SRM 51-30-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO STA 1328 BETWEEN 28RT AND 26LT FRAME CORRODED. REPLACED FRAME PER SRM 51-30-02.
Part: LONGERON — CORRODED (BS 1344-1364 L30) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO STA 1344-1364, LONGERON 30 CORRODED. REPAIR LONGERON 30 IAW SRM 53-00-01, 51-30-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO STA 1344 BETWEEN 29RT AND 29LT FRAME CORRODED. REPAIR FRAME PER SRM 53-10-02.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO STA 1307 BETWEEN STGR 30 AND 28LT FRAME CORRODED. REPAIR IAW SRM 53-10-02, 51-30-05.
Part: FRAME — CORRODED (BS 1364 S29L/R) · airframe 29,883 hrs · 21,436 cycles
AFT CARGO STA 1364 BETWEEN STGR 29RT AND 29LT FRAME CORRODED. REPAIR IAW SRM 53-00-01 51-30-05.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO COMP LT TIE DOWN TRACK STA 1060-1155 CORRODED. REPLACED TIE DOWN TRACK PER SRM 51-30-05.
Part: LONGERON — CORRODED (BS 168 L28R) · airframe 29,883 hrs · 21,436 cycles
CORROSION ON L28R, STA 168. REPAIR L28R, STA 168 IAW 53-10-01, 51-30-02.
Part: WEB — CRACKED (LT MLG WW) · airframe 29,883 hrs · 21,436 cycles
HMV2 LEFT WHEEL WELL CUTOUT FWD WEB CRACKED 3 PLACES. REPLACED WEB PER SRM 51-30-02.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO COMP LT TIE DOWN TRACK STA 1155-1227 CORRODED. REPLACED TRACK PER SRM 51-30-05.
Part: HINGE FITTING — CHAFED (SPOILER) · airframe 29,883 hrs · 21,436 cycles
HMV2 RT WING INBD FLT SPOILER CENTER FITTING FOUND WITH HEAVY CHAFING. REPLACED FITTING PER SRM 51-30-01.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO RT TIE DOWN TRACK STA 1060-1155 CORRODED. REPLACED TRACK PER SRM 51-30-01.
Part: PAN — CORRODED (CARGO DOOR) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO DOOR INNER PAN CORRODED. REPLACED PAN PER SRM 51-10-03 52-00-01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT ACCY COMP AFT AIRSTAIR CUTOUT RT STA 1469 CANT 1542 CORRODED.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO COMP STA 1364 BETWEEN STR 29RT AND 29LT FRAME CORRODED. REPAIRED FRAME PER SRM 53-10-02.
2010
Part: LONGERON — CORRODED (FUSELAGE) · airframe 29,883 hrs · 21,436 cycles
HMV2 AFT CARGO LONG 28 RT CORRODED STA 1184-1288. REPLACED LONGERON 28R PER SRM 51-30-05.
2008
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65065097 CORROSION ON FITTING OF RIGHT TRACK BETWEEN STA 1136 STA 1155 IN AFT CARGO COMPARTMENT. REPLACE PER SRM VOL 1 53-40-01 FIG 7, C/W TASK CARD 65065097.
Part: FITTING — CORRODED (FUSELAGE) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65064988, CORROSION OF FITTING OF RIGHT TRACK BETWEEN STA 579 AND STA 598 IN FWD CARGO COMPARTMENT. REPLACE PER SRM VOL 1 53-40-01 FIG 7, C/W TASK CARD 65064988.
Part: TEE FITTING — CRACKED (RT MLG WW) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65065033 CRACK ON RIGHT MAIN LANDING GEAR AFT JAMB TEE. INSTALL DOUBLER PER SRM VOL 1 53-60-02 FIG 8, C/W TASK CARD 65065033.
Part: TEE FITTING — CRACKED (LT MLG WW) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65065034 CRACK ON LEFT MAIN LANDING GEAR AFT JAMB TEE. INSTALL DOUBLER PER SRM VOL 1 53-60-02 FIG 8, C/W TASK CARD 65065034.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 15,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65064990, CORROSION ON RIGHT TRACK BETWEEN STA 579 AND STA 693 IN FWD CARGO COMPARTMENT. SPLICE REPAIR PER SRM VOL 1 53-40-01 FIG 7, C/W TASK CARD 65064990.
Part: PAN — CORRODED (FUSELAGE) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65064962 CORROSION ON FWD LOWER CARGO DOOR JAMB PAN. REPAIR PER DRAWING J060228-1, C/W 65064962.
Part: FITTING — CORRODED (FUSELAGE) · airframe 25,414 hrs · 17,983 cycles
PERFORMED TASK CARD 65064968 CORROSION ON FITTING OF RIGHT TRACK BETWEEN STA 503 AND STA 522 IN FWD CARGO COMPARTMENT. REPLACE PER SRM VOL 1 53-40-01 FIG 7, C/W TASK CARD 65064968.