N706AS
Registered owner: AGRI SPRAY DRONES LLC, MO (owner ≠ operator)
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.
179 reports on file, 2001-03-09 – 2016-06-03.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 55,381 hrs · 31,272 cycles
DURING COMPLETION OF T/C 48133000 "INTERNAL EMERGENCY LIGHTS" FOUND BATTERY PACK M1674 FAILED. ACFT GROUNDED. R & R M1674 BATTERY PACK, REF AMM 33-51-51 & SSM 33-51-00. OPS CHECKS GOOD.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 54,926 hrs · 30,986 cycles
EXIT ROW EXIT SIGN COVER FELL OFF ACFT RT. ACFT GROUNDED. REINSTALLED EXIT SIGN COVER AS REQUIRED, OK FOR SERVICE.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 54,896 hrs · 30,972 cycles
CREW REPORTS RT OVERWING EXIT SIGN COVER FELL OUT. ACFT GROUNDED. SECURED EXIT SIGN COVER.
Part: STRINGER — CRACKED (BS 986) · airframe 54,612 hrs · 30,771 cycles
UPON REMOVAL OF L2 DOOR SILL WEB BS 986-992 FOUND CRACKED STR TIE AT STR 19L, BS 986. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.
Part: WEB — CORRODED (BS 968-986) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
UPON REMOVAL OF R2 MOPSILL FOUND SILL WEB STA 967 TO 986 TO BE CORRODED. ACFT GROUNDED. BLENDED R2 LOWER SILL WEB BS 967 TO 986. MATERIAL REMAINING FOUND TO BE OUT OF LIMITS, R & R SILL WEB IAW SRM 53-60-15-1A-1, FIG 101 AND 51-40-02-0G-0, W 1", 9 .056, R .049, L 3", D .007.
Part: FLOOR PANEL — DELAMINATED (BS 360-380) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2334B HAS AN AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED AREA OF DELAMINATION ON FLOOR PANEL NR 2334 IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 270-312) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL 2331 HAS AN AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED AREA OF DELAMINATION ON FLOOR PANEL NR 2331 IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 270-294) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL 2333 HAS AN AREA OF DELAMINATED. ACFT GROUNDED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 328-360) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2340 HAS AN AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED AREA OF DELAMINATION ON FLOOR PANEL NR 2340 IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 947-986) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2472 HAS AN AREA OF DELAMINATED. ACFT GROUNDED. REPAIRED AREA OF DELAMINED ON FLOOR PANEL NR 2472 IAW SRM 53-00-50-2R-0, PARA 3.B.
Part: FLOOR PANEL — DELAMINATED (BS 270-294) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2334 HAS AN AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED AREA OF DELAMINATION ON FLOOR PANEL NR 2334 IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 294-328) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2336 HAS AN AREA OF DELAMINATION AND A PUNCTURE. ACFT GROUNDED. REPAIRED DELAMINATION AND PUNCTURE ON FLOOR PANEL NR 2336 IAW SRM 53-00-50-2R-0, PARA 3.C, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 312-344) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2337 HAS AN AREA OF DELAMINATION. ACFT GROUNDED. REPAIRED AREA OF DELAMINATION ON FLOOR PANEL NR 2337 IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: FLOOR PANEL — DELAMINATED (BS 986-1000) · airframe 54,612 hrs · 30,771 cycles
FLOOR PANEL NR 2473 HAS AN AREA OF DELAMINATED AND EDGE DAMAGE. ACFT GROUNDED. REPAIRED FLOOR PANEL NR 2473 DELAMINATED AND EDGE DAMAGE IAW SRM 53-00-50-2R-0, PARA 3.B, PG 1.
Part: STRINGER CLIP — CRACKED (BS 500G) · airframe 54,612 hrs · 30,771 cycles
UPON REMOVAL OF TRANSITION PANEL STRINGER CLIP AT BS 500G, STR 26R FOUND TO BE CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.
Part: STRINGER CLIP — CRACKED (BS 500G) · airframe 54,612 hrs · 30,771 cycles
UPON REMOVAL OF TRANSITION PANEL STRINGER CLIP AT BS 500G, STR 26R, FOUND TO BE CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0.
Part: STRINGER — CRACKED (BS 500F) · airframe 54,612 hrs · 30,771 cycles
UPON REMOVAL OF TRANSITION PANEL FOUND STR CLIP AT BS 500F, STR 26R TO BE CRACKED. ACFT GROUNDED. R & R STR CLIP IAW SRM 51-40-02-0G-0.
Part: CUSP WEB — CORRODED (BS 400-420) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
CUSP WEB LT BS 400 TO BS 420 HAS HEAVY CORROSION ON LOWER SIDE. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51-40-02-0G-0, W 1", O .036, R 0, L 2", D .036.
Part: STRINGER — CRACKED (BS 277-291) · airframe 54,612 hrs · 30,771 cycles
STRINGER ANGLE FORWARD OR R1 DOOR WL 253. ACFT GROUNDED. R & R CRACKED ANGLE IAW SRM 51-40-02-0G-0.
Part: STRINGER — CRACKED (BS 277-291) · airframe 54,612 hrs · 30,771 cycles
STRINGER ANGLE FORWARD OF R1 DOOR WL 247. ACFT GROUNDED. R & R CRACKED ANGLE IAW SRM 51-40-02-0G-0.
Part: CUSP WEB — CORRODED (BS 400-420) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
CUSP WEB LT BS 400 TO 420 HAS HEAVY CORROSION ON LOWER SIDE. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51-40-02-0G-0, W 1", O .036", R 0, L 2", D .036.
Part: STRINGER — CRACKED (BS 277-291) · airframe 54,612 hrs · 30,771 cycles
STRINGER ANGLE FORWARD OF R/1 DOOR WL 239. ACFT GROUNDED. R & R CRACKED ANGLE IAW SRM 51-40-02-0G-0.
Part: STRINGER — CRACKED (BS 277-291) · airframe 54,612 hrs · 30,771 cycles
STRINGER ANGLE FORWARD OF R1 DOOR. ACFT GROUNDED. R & R CRACKED ANGLE IAW SRM 51-40-02-0G-0.
Part: STIFFENER — CORRODED (BS 1112-1118) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
APU COMPARTMENT TORQUE BOX ON RT SIDE APU INLET FWD SUPPORT ANGLE AT FS 1115 HAS AREA OF CORROSION. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0, G 0, W 1", O .071" R 0, L 1", D .071.
Part: FLOOR SUPPORT — CORRODED (BS 951-967) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
FLOOR SUPPORT BS 951 TO 967, LBL 50 IS CORRODED. ACFT GROUNDED. CORROSION FOUND TO BE OUT OF LIMITS, R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0, W 1.25", O .080", R .068", L 5.0", D .012".
Part: STIFFENER — CORRODED (BS 1123-1128) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
APU COMPARTMENT RT TORQUE BOX AT APU INLET AFT SUPPORT ANGLE AT FS 1125 HAS SEVERAL AREAS OF HEAVY CORRODED NUT PLATE AREAS ARE BLOWN OUT WITH CORROSION. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0, W 1", O .071", R 0, L 1", D .071.
Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 54,612 hrs · 30,771 cycles
FWD WET AREA FLOOR SUPPORT BS 328 TO 344 LBHL 48 IS CRACKED. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-402-0G-0 AT BS 328 TO 344, LBL 48.
Part: STRINGER — CORRODED (BS 980-990) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
STR 21R IS CORRODED STA 980-990. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS REMOVED DAMAGE STRINGER AND REPLACED WITH NEW STRINGER IAW SRM 51-10-02-0G-0 PAR 14, SRM 53-00-03-1A-1, AND SRM 51-40-02-0G-0.
Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
FWD WET AREA FLOOR SUPPORT, BS 312 TO BS 328, RBL 12 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-A-1 DETA 0. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AT BS 312 TO BS 328, RBL 12, W 1.0, O .080, R .034, L 2.09, D .046.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,612 hrs · 30,771 cycles
FWD WET AREA FLOOR SUPPORT BS 312 TO 328 LBL 48 IS CRACKED. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AT BS 312 TO 328, LBL 48.
Part: CHANNEL — CORRODED (BS 947-1006) · corrosion level 2 · airframe 54,612 hrs · 30,771 cycles
L2 DOOR MOPSILL IS CORRODED. ACFT GROUNDED. CORRODED FOUND TO BE OUT OF LIMITS R & R L2 MOPSILL IAW SRM 51-40-02-0G-0, W 2, O .071, R 0, L 6, D .071.
Part: FRAME — CRACKED (BS 827) · airframe 54,612 hrs · 30,771 cycles
CABIN FRAME AT BS 827 IS CRACKED BETWEEN S8L AND S9L. ACFT GROUNDED. REPAIRED CABIN FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15, FIG 2.
Part: FRAME — CRACKED (BS 727D) · airframe 54,612 hrs · 30,771 cycles
CABIN FRAME AT BS 727D IS CRACKED BETWEEN S8L AND S9L. ACFT GROUNDED. REPAIRED CABIN FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15 FIG 2.
Part: FRAME — CRACKED (BS 787) · airframe 54,612 hrs · 30,771 cycles
CABIN FRAME AT BS 787 IS CRACKED BETWEEN S8L AND S9L. ACFT GROUNDED. REPAIRED CABIN FRAME IAW T/C AD2006209-400-53-107, REV 00, DATED 11SEP15, FIG 2.
Part: FRAME — CRACKED (BS 907) · airframe 54,612 hrs · 30,771 cycles
CABIN FRAME AT BS 907 IS CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED CABIN FRAME IAW T/C AD20062609 -400-53-107, REV 00, FIG 2.
Part: STRAP — CRACKED (BS312) · airframe 54,606 hrs · 30,769 cycles
E & E BAY FAR RT FLOORBEAM STABILIZER STRAP CRACKED ON PREVIOUS REPAIR FS 312. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02-0G-0.
Earlier reports · 2001–2015 · 143 reports
2015
Part: LIGHT — FAILED (PAX CABIN) · airframe 53,558 hrs · 30,076 cycles
F/A REPORTS FWD LT OVERWING EMERGENCY EXIT TRACK LIGHTING LENS WILL NOT STAY ON. ACFT GROUNDED. REPLACED FWD LT OVERWING EMERGENCY EXIT TRACK LIGHTING ASSY. OPS CHECK SAME GOOD.
Part: HOUSING — GOUGED (CRGO DOOR HANDLE) · airframe 52,716 hrs · 29,524 cycles
FWD CARGO DOOR HANDLE HOUSING GOUGED. ACFT GROUNDED. REMOVED HANDLE HOUSING FROM DOOR, REMOVED FLAPPER DOOR FROM HOUSING AND INSTALLED HOUSING DOOR ON NEW HOUSING. LOCATED ALL FASTENER LOCATION ON NEW HOUSING FOR INSTALLATION. REMOVED ALL SHARP EDGES, ALODINED AND PRIMED HOUSING HOLE. LOCATIONS HOUSING READY TO INSTALLED WITH ATTACHING FASTENER IAW SRM 51-40-02. COMPLETED INSTALLATION OF HANDLE HOUSING WITH ATTACHING FASTENERS IAW SRM 51-40-02. APPLIED FILLET SEAL AND ALODINED AND PRIMED ALL BARE METAL OF OUTER SKIN SURFACES. REINSTALLED SAME EXTERIOR AND INTERIOR DOOR HANDLES, OP'S CHECK NORMAL REF AMM 52-31-14-004-054. REINSTALLED DOOR LINER AS REQUIRED.
2014
Part: CARGO TRACK — CORRODED (BS 747-853) · corrosion level 2 · airframe 51,414 hrs · 28,738 cycles
AFTER REMOVAL OF NR 4 FLOOR PANEL, FOUND CARGO TRACK RBL 13.8 CORRODED FROM BS 747 - 853. ACFT GROUNDED. R & R THE CARGO TRACK SECTION IAW SRM 53-00-53-R-2.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 49,207 hrs · 27,412 cycles
OVERWING EXIT SIGN CAME LOOSE. ACFT GROUNDED. REINSTALLED LIGHT COVER, OK FOR SERVICE.
2013
Part: TRACK — DIRTY (SLIDING WINDOW) · airframe 48,429 hrs · 26,941 cycles
CAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. ACFT GROUNDED. CLEANED CAPTAIN`S L2 SLIDING WINDOW TRACK, REPOSITIONED WINDOW BACK IN TRACK. PERFORMED OPS CHECK, IAW AMM 56-12-11 NO ADJUSTMENT MADE. WINDOW OPS NORMAL, NO HISTORY 30 DAYS. OK FOR SVC.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 48,402 hrs · 26,918 cycles
EMERGENCY EXIT LIGHTS L1 UPPER, L2 LOWER AND LT BULLNOSE ROWS 1-10 INOP. ACFT GROUNDED. R & R BATTERY PACK FOR POWER SUPPLY M1674. OPS CKS NORMAL IAW MM 33-51-51.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 47,958 hrs · 26,630 cycles
EMERGENCY EXIT SIGN ABOVE DOOR IN CABIN FELL OFF. ACFT GROUNDED. REPLACED SIGN WITH NEW IAW AMM 33-51-22.
Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,952 hrs · 26,627 cycles
NR 2 SLAT INBD END UPPER CORNER DELAMINATED. REPAIRED NR 2 SLAT INBD AND UPPER CORNER IAW SRM-51-70-10-2R-4, REPAIR 4. (PERMANENT REPAIR)
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 47,952 hrs · 26,627 cycles
LEFT OTBD AFT FLAP UPPER INBD SURFACE DELAMINATED. REPAIRED LT OTBD AFT FLAP UPPER INBD SURFACE IAW SRM 51-70-10-2R-4, REPAIR 4. (PERMANENT REPAIR)
Part: ANGLE — CORRODED (BS 600-630) · corrosion level 2 · airframe 47,952 hrs · 26,627 cycles
LT MLG WW LOWER AFT ANGLE HAS EXFOLIATING CORROSION ONTOP SIDE OF LOWER LIP. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-05 AND 51-40-02.
Part: BRACKET — CRACKED (BS 996) · airframe 47,952 hrs · 26,627 cycles
AFT SILL DRAIN BRACKET, IS CRACKED AT UPPER ATTACH FLANGE FABRICATED AFT SILL DRAIN BRACKET, IAW SRM 51-30-01-0G-0 AND DWG 417A2106.
2012
Part: FRAME — CRACKED · airframe 44,886 hrs · 24,770 cycles
BS 616 STUB BEAM LOWER INNER CHORD CRACKED COMMON TO THE LOWEST 2 FASTENER HOLES. ACFT GROUNDED. REPAIRED INNER CHORD IAW T/C AD 20102506-400-53-7.
Part: FRAME — CRACKED (BS 639) · airframe 44,886 hrs · 24,770 cycles
BS 639 STUB BEAM LOWER INNER CHORD CRACKED COMMON TO THE LOWEST FASTENER HOLE. ACFT GROUNDED. REPAIRED INNER CHORD IAW ASA T/C AD20102506-400-53-9.
Part: FRAME — CRACKED (BS 616) · airframe 44,886 hrs · 24,770 cycles
RT BS 616 STUB BEAM LOWER INNER CHORD CRACKED, COMMON TO THE LOWEST 2 FASTENER HOLES. ACFT GROUNDED. REPAIRED INNER CHORD IAW T/C AD 20102506-400-53-8.
2011
Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 42,942 hrs · 23,612 cycles
L1 DOOR WILL NOT LATCH CLOSED. UPON INSPECTION FOUND JAM NUT BACKED OFF OF GUIDE ARM. ADJUSTED L1 DOOR GUIDE ARM REF MM 52 11 00 705 007 STEPS G.(1) (2)(C). DOOR FLUSHNESS AND DOOR CLEARANCE CHECKED GOOD REF MM 52 11 00 705 007 FIGURE 503. PERFORMED FORWARD ENTRY DOOR TEST REF MM 52 11 00 755 051. OPS CHECK GOOD.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFT GALLEY FLOOR SUPPORT "Z" ANGLE AT BS 992 RBL 42 CORRODED. REMOVED CORRODED ANGLE FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFT PIT LT ZEE CHANNEL CORRODED SEVERAL AREAS FROM SPLICE AFT OF BS 787 TO BS 867. REPAIRED LT ZEE CHANNEL IAW B737 400 SRM 53 60 53 FIG 201 REPAIR 4.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFT PIT SHEAR TIE AT BS 787 BETWEEN STR 27R AND 25R CORRODED. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 3.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
CORROSION AT FRAME BS 727E SHEAR TIE STR 27R TO STR 27L. REPAIRED FRAME SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 3.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
SHEAR TIE BS 787 STR 25R TO 26R CORRODED. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 3.
Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 41,702 hrs · 22,884 cycles
AFT CARGO LT TRANSITION PANEL CORRODED BETWEEN BS 727B AND 727C. REPAIRED TRANSITION PANEL IAW B737 400 SRM 53 60 53 FIG 201 REPAIR 4.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
CORROSION ON WEB AT BS 992 TO BS 1006 RBL 40. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
L1 DOOR GIRT BAR RECEPTACLE FLOOR FITTING SUPPORT CORRODED BS 344 LBL 56. REMOVED AND REPLACED BRACKET IAW B737 400 AMM 20 50 11 912 002.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFT PIT FAIL SAFE CORRODED AFT SIDE BS 794 BETWEEN STR 25R AND 26R. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
L1 DOOR GIRT BAR RECEPTACLE FLOOR FITTING SUPPORT CORRODED BS 313 LBL 56. REMOVED AND REPLACED BRACKET IAW B737 400 AMM 20 50 11 912 002.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
CORROSION ON WEB BS 992 TO BS 1006 RBL 40. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.
Part: CHANNEL — CORRODED (CARGO BAY) · airframe 41,702 hrs · 22,884 cycles
AFT PIT TRANSITION PANEL AFT OF DOOR OPENING FROM BS 847 TO BS 867 ALONG STR 25R CORRODED. REMOVED AND REPLACED TRANSITION PANEL IAW B737 400 SRM 51 40 02.
Part: ANGLE — CRACKED (LT WING) · airframe 41,702 hrs · 22,884 cycles
LEFT WING STIFFENER JUST FORWARD OF THE NR 2 AILERON HINGE IS CRACKED APPROX RSS543. REMOVED AND REPLACED STIFFENER IAW B737 400 SRM 51 40 02.
Part: SKIN — DENTED (HORIZ STAB) · airframe 41,702 hrs · 22,884 cycles
LT HORIZONTAL STABILIZER LEADING EDGE DENTED. DENT IS 5 IN. L X 2.25 IN W X .052 IN DEEP. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 55 10 01.
Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFTER REMOVAL OF RT SHEAR WEB FOUND CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND OUT OF LIMITS. FABRICATED REPLACEMENT WEB AND INSTALLED IAW SRM 53-60-51 AND 51-40-05.
Part: WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
R2 DOOR MOPSILL FOUND CORRODED ON WEB BS 986 TO BS 992 RBL 40. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02 AND 51-40-05.
Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFTER REMOVAL OF LT SHEAR WEB FOUND CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND OUT OF LIMITS. FABRICATED REPLACEMENT WEB AND INSTALLED IAW SRM 53-60-51 AND 51-40-05.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
L2 DOOR MOP SILL WEB BETWEEN BS 947 AND BS 986 AT LBL 40 IS CORRODED. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
L2 DOOR MOP SILL WEB AT BS 966 TO BS 992 LBL 40 IS CORRODED. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.
Part: WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AT R2 DOOR MOPSILL FOUND CORRODED WEB BS 947 TO BS 986 RBL 40. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02 AND 51-40-05.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT OUTBOARD SEAT TRACK GOUGED AND WORN AT BS 520. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 REPAIR 2.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
RT OUTBOARD SEAT TRACK IS GOUGED AND WORN BETWEEN BS 540 BS 663.5 AND BS 685 BS 706. REMOVED DAMAGED SEAT TRACK AND INSTALLED REPLACEMENT PART IAW B737 400 AMM 20 50 11 912 002.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT INBOARD SEAT TRACK GOUGED AND WORN BETWEEN BS 727G BS 747 BS 887. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 REPAIR 4.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
RIGHT OUTBOARD SEAT TRACK GOUGED AND WORN BETWEEN BS 500E AND 520. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 REPAIR 2.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT INBOARD SEAT TRACK GOUGED AND WORN BS 695.5. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT IAW B737 400 SRM 53 00 52.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT INBOARD SEAT TRACK GOUGED AND WORN AT BS 520. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 REPAIR 2.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
RADIAL STIFFENER AT BS 1016 BL 0 IS CORRODED. REMOVED CORRODED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING DWG 65 28106.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
FLOOR SUPPORT STIFFENER AT BS 950 HAS CORROSION AT FASTENER HOLES. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW B737 400 SRM 53 60 51 AND 51 40 02.
Part: RIB — CRACKED (LT WING) · airframe 41,702 hrs · 22,884 cycles
LEFT WING LOWER RIB CHORD IS CRACKED AT WBL 135.5. REPAIRED RIB LOWER CHORD IAW ASA EA 400 57EA 05014.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
INTERCOSTAL AT FORWARD EDGE OF R2 DOOR HAS CORROSION. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.
Part: CARGO TRACK — BENT (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
RIGHT CARGO TRACK AT BS 767 IS BENT ON LOWER FLANGE. REPAIRED IAW B737 400 SRM 53 00 53 FIG 201.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
CUSP WEB BETWEEN BS 907 AND BS 927 RT SIDE CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW SRM 53-60-51, 51-30-01, 51-40-02, 51-20-01 AND SOPM 20-41-02.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
CUSP WEB BETWEEN BS 400 AND BS 420 RIGHT IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 70 13.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT CUSP WEB BETWEEN BS 685 AND BS 695 IS CORRODED. REMOVED WEB FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02.
Part: FRAME — DENTED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 747 FRAME IS DENTED ON UPPER FLANGE. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05095.
Part: FRAME — DENTED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 727A FRAME IS DENTED ON UPPER FLANGE. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05099.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
RIGHT CARGO TRACK IS CORRODED FROM BS 767 TO BS 867. REPAIRED IAW ASA EA 400 53EA 04992.
Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
SIDEWALL SUPPORT AT BS 727G IS BENT AND CORRODED. REMOVED AND REPLACED SUPPORT IAW B737 400 SRM 51 40 02.
Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
RIGHT TRANSITION PANEL IS CORRODED FROM BS 727 TO BS 767. REPAIRED IAW B737 400 SRM 53 60 53.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
CUSP WEB CORRODED BETWEEN BS 807 TO BS 827 RIGHT SIDE. CUT OUT DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-03.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
FLOOR SUPPORT AT RBL 8 BS 937 HAS DRILL STRIKES. REPAIRED IAW B737 400 SRM 53 00 53.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
SIDEWALL SUPPORT ANGLE AT BS 727D IS CORRODED. REMOVED AND REPLACED SUPPORT IAW B737 400 SRM 51 40 02.
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
L2 DOOR CUTOUT FORWARD FRAME CORRODED AT LOWER INBOARD EDGE. REPAIRED FRAME IAW ASA EA 400 53EA 05127.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
AFT PIT BRACKET (CLIP) CRACKED FORWARD SIDE OF BS 807 INBOARD OF STR 25R. REMOVED AND REPLACED BRACKET IAW B737 400 SRM 51 40 22.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BULKHEAD LOWER SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 51 40 02.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
LEFT CUSP WEB JUST FORWARD OF BS 380 IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 70 13.
Part: STRAP — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
CABIN FLOOR SUPPORT TIE STRAP IS CRACKED AT RBL 24 AFT OF BS 312 (SEEN FROM E&E BAY). STOP DRILLED CRACK FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 53 10 51 DETAIL I REPAIR 4.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
AFT PIT REINFORCEMENT ANGLE CORRODED BS 767 STR 27R. REMOVED ANGLE (FAIL SAFE CHORD). FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 00 07 FIG 1.
Part: FRAME — DENTED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 727 FRAME IS DENTED ON UPPER EDGE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05101.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 787 FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 907 FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 400 FRAME BETWEEN STR 8R AND 9R IS CRACKED. REPAIRED FRAME IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 360 FRAME BETWEEN STR 8L AND 9L CRACKED REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: RIB — CRACKED (RT WING) · airframe 41,702 hrs · 22,884 cycles
RIGHT WING RIB LOWER CHORD AT WBL 135.5 CRACKED. REPAIRED RIB LOWER CHORD IAW ASA EA 400 57EA 05014.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 400 FRAME BETWEEN STR 8L AND 9L CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 747 FRAME BETWEEN STR 8L AND 9L CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 747 FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 380 FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 480 FRAME BETWEEN STR 8L AND 9L CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 440 FRAME BETWEEN STR 8L AND 9L CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 867 FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 440 FRAME BETWEEN STR 8R AND 9R CRACKED REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 500A FRAME BETWEEN STR 8R AND 9R CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
BS 867 FRAME BETWEEN STR 8L AND 9L CRACKED. REPAIRED IAW ASA EA AD20062609 400 53 117.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
FORWARD CARGO BULKHEAD LOWER FLOOR SUPPORT BS 500G HAS CORROSION FROM STR 25L TO 25R, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 40 05.
Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
FORWARD CARGO COMPARTMENT LT TRANSITION PANEL ABOVE STR 26L CORRODED FROM BS 515D TO BS 500H. REMOVED CORRODED AND CRACKED TRANSITION PANEL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 30 15.
Part: SILL — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
FORWARD WET AREA RIGHT SIDE MOP SILL CHORD IS CORRODED. REMOVED DAMAGED CHORD FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05105.
Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
VERTICAL STABILIZER LT AFT SKATE (CLOSEOUT) ANGLE AFT END CHAFED. REPAIRED SKATE ANLE IAW B737 400 SRM 53 80 71 REPAIR 1 FIG 201.
Part: SILL — CORRODED (FUSELAGE) · airframe 41,720 hrs · 22,884 cycles
R2 DOOR MOP SILL CORRODED. REMOVED MOP SILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.
Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 41,702 hrs · 22,884 cycles
VERTICAL STABILIZER LT FORWARD SKATE ANGLE CHAFED. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
R1 DOOR CUTOUT SCUFF PLATE SUPPORT ANGLE CORRODED BS 300 TO BS 332. REMOVED AND REPLACED SUPPORT ANGLE IAW B737 400 SRM 53 10 15 FIG 1.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
FORWARD WET AREA LEFT SIDE MOP SILL CORRODED FROM BS 306 TO BS 360. REMOVED MOP SILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.
Part: SKIN — DENTED (HORIZ STAB) · airframe 41,702 hrs · 22,884 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED 63 INCHES FROM INBOARD EDGE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 55 10 01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
FLOORBEAM AT BS 986 UPPER CAP PREVIOUS REPAIR IS CORRODED FROM LBL 49 TO RBL 49. REMOVED PREVIOUS "T" CAP REPAIR FABRICATED NEW REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05061.
Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 41,702 hrs · 22,884 cycles
VERTICAL STABILIZER RT FORWARD SKATE ANGLE CHAFED. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,702 hrs · 22,884 cycles
L2 DOOR MOPSILL IS CORRODED. REMOVED MOPSILL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,702 hrs · 22,884 cycles
DOUBLE DRILLED HOLE THRU SKIN BS 727+10 BETWEEN STR 26R AND 27R. REPAIRED SKIN IAW ASA EA 400 57EA 05092.
Part: PANEL — DAMAGED (RT WING) · airframe 41,702 hrs · 22,884 cycles
RIGHT TRAILING EDGE CLOSE OUT PANEL IS CHAFED AND DENTED. FABRICATED REPLACEMENT PANEL AND INSTALLED IAW B737 400 SRM 51 40 05.
2009
Part: SKIN — DELAMINATED (LE SLAT) · airframe 38,343 hrs · 24,241 cycles
RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED AT O/B UPPER SURFACE. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED REPAIR.
Part: RELAY — FAILED (E&E BAY) · airframe 37,517 hrs · 20,417 cycles
RED NOSE GEAR INDICATION ON APPR. CYCLED 2 TIMES 3RD CYCLE GREEN LIGHT INSPECTED & CYCLED NOSE GEAR. VERIFIED LOCK & POSITION SENSOR (S846 &S845) RESISTANCES. REPLACED NOSE GEAR LOCK SENSOR. PERFORMED SELF TEST FOR THE LANDING GEAR POSITION SWITCHES OPS GOOD. PERFORMED TEST FOR R374 NOSE GEAR LATCHING RELAY FAILS STEP 2F (REQUIRES P/N JLD4A). REPLACED RELAY R374.
2008
Part: SKIN — DENTED (NR 7 SPOILER) · airframe 34,783 hrs · 18,874 cycles
NR 7 SPOILER IS DENTED ABOVE THE ACTUATOR ON THE UPPER SURFACE. REMOVED DAMAGED AREA, FABBED DOUBLER & INSTALLED REPAIR IAW B737 400 SRM 57 70 01 REPAIR 4.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,783 hrs · 18,874 cycles
RT INBOARD FORE FLAP HAS MULTIPLE SMALL DENTS ON LOWER SURFACE ABOVE NR 3 & 4 TIRES 2 DENTS ON PREVIOUS REPAIRS. REMOVED DAMAGED AREA, FABBED FILLERS & DOUBLERS & BONDED REPAIRS IAW B737 400 SRM 51 70 10 REPAIR 4.
Part: SKIN — DENTED (NR 4 SPOILER) · airframe 34,783 hrs · 18,874 cycles
LT WING INBOARD GROUND SPOILER NR 4 HAS SEVERAL DENTS ON THE LOWER SURFACE. PREPARED DAMAGED AREA, FABBED DOUBLERS & BONDED THE REPAIRS IAW B737 400 SRM 51 70 10.
Part: SKIN — DENTED (NR 6 SPOILER) · airframe 34,783 hrs · 18,874 cycles
NR 6 SPOILER HAS SEVERAL DENTS ON TOP. PREPPED DAMAGED AREA, FABBED DOUBLERS 2 EA & BONDED REPAIRS IAW B737 400 SRM 51 70 10.
Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,783 hrs · 18,874 cycles
RT INBOARD AFT FLAP UPPER SURFACE IS CHAFED AT WBL 82. PREPPED DAMAGED AREA, FABBED DOUBLER & BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,783 hrs · 18,874 cycles
LT OUTBOARD T/E AFT FLAP HAS NUMEROUS DENTS ON THE LOWER SURFACE. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER & BONDED THE REPAIR PARTS IAW B737 400 SRM 51 70 10 REPAIR 4.
Part: SKIN — DENTED (BS 911-922) · airframe 34,783 hrs · 18,874 cycles
REF SAD 6250170: FUSELAGE SKIN DENT 6' AFT OF AFT CARGO DOOR. DENT IS CREASED LOCATED AT STA 917 BELOW STR 23R. REMOVED DAMAGED AREA, FABBED DOUBLER & INSTALLED REPAIR IAW ASA EA 5330 02378. REF LG PG 5130588 FOR REINSPECTION INFO. FLIGHT CYCLES AT INSTALL = 18874.
Part: CARGO TRACK — BROKEN (BS 480-500) · airframe 34,783 hrs · 18,874 cycles
FWD CARGO PIT LT CARGO TIE DOWN TRACK HAS A BROKEN LUG FOR THE AFT NET ATTACHMENT. REMOVED DAMAGED SECTION OF TRACK, FABBED REPLACEMENT TRACK & REPAIR PARTS & INSTALLED IAW B737 400 SRM 53 00 53 FIG 201.
Part: SKIN — DENTED (BS 366-377) · airframe 34,783 hrs · 18,874 cycles
REF SAD 6311478: DENT ON RT SIDE OF FUSELAGE AT APPROX STA 370 WL 206. DENT IS COMMON TO STR 17R. REMOVED DAMAGED AREA, FABBED FILLER DOUBLER & TRIPLER & INSTALLED REPAIR IAW ASA EA 5330 02379. REF LG PG 5130589 FOR REINSPECTION INFO. FLIGHT CYCLES AT INSTALL = 18874.
2007
Part: INTERCOSTAL — CORRODED (BS 767-787) · airframe 30,860 hrs · 16,749 cycles
AFT CARGO FLOOR INTERCOSTAL IS CORRODED. CORRODED FLOOR INTERCOSTAL REPLACED WITH FABRICATED REPAIR PART IAW SRM 53-30-01 AND 53-60-15 FIG 11.
Part: SHEAR TIE — CRACKED (NR 2 NACELLE) · airframe 30,860 hrs · 16,749 cycles
NR 2 ENGINE PYLON RIGHT SIDE END PANEL SUPPORT BRACKET IS CRACKED. BRACKET REPLACED WITH NEW PART.
Part: DOOR — CRACKED (MLG) · airframe 30,860 hrs · 16,749 cycles
RIGHT MLG INNER DOOR LOWER T/E CRACKED. REPAIRED GEAR DOOR IAW SRM 53-80-02 REPAIR 2 DETAIL 2.
Part: WEB — CORRODED (BS 787-794) · corrosion level 2 · airframe 30,860 hrs · 16,749 cycles
AFT CARGO PIT INTERCOSTAL FOUND CORRODED. REPLACED INTERCOSTAL WITH FABRICATED REPAIR PART IAW SRM 51-40-02.
Part: SUPPORT BRACKET — CRACKED (BS 664) · airframe 30,860 hrs · 16,749 cycles
SYSTEM B-HYDRAULIC LINE SUPPORT BRACKET ON RIGHT MLG WW FWD BULKHEAD IS CRACKED. BRACKET REPAIRED IAW SRM 51-31-01.
Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 30,860 hrs · 16,749 cycles
AFT CARGO DOOR SURROUNDING WEB FOUND CORRODED. AFT CARGO DOOR SURROUNDING WEB REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-30-01 AND 51-40-05.
Part: SKIN — CRACKED (RT WING) · airframe 30,860 hrs · 16,749 cycles
RIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT CRACKED. RIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT REPAIRED SERVICEABLE IAW SRM 51-70-17.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 30,860 hrs · 16,749 cycles
AFT CARGO DOOR AFT SCUFF PLATE CRACKED. AFT CARGO PIT AFT SCUFF PLATE REPAIRED IAW ASA EA 5320 01456.
Part: FRAME — CORRODED (BS 794) · corrosion level 2 · airframe 30,860 hrs · 16,749 cycles
AFT CARGO PIT FRAME DOUBLER FOUND CORRODED. FRAME REPLACED WITH NEW PART IAW SRM 51-40-05.
Part: STRINGER CLIP — CORRODED (BS 787) · corrosion level 2 · airframe 30,860 hrs · 16,749 cycles
AFT CARGO PIT CLIP CORRODED. REPLACED WITH MADE REPAIR PART IAW SRM 51-40-02.
Part: SKIN — DENTED (RWS 245) · airframe 30,860 hrs · 16,749 cycles
RIGHT WING O/B FORE FLAP DENTED ON UPPER SURFACE. DENT REPAIRED IAW SRM 51-70-10 REPAIR 4.
2006
Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 27,222 hrs · 14,775 cycles
FOUND FLOORBEAM HAS CORROSION AROUND NUTPLATE HOLES. REMOVED COMPLETE UPPER TEE HORIZONTAL FLANGE FABRICATED AND INSTALLED UPPER TEE SPLICE ANGLES SPLICE STRAPS FILLERS AND SHEAR TIES PER ASA EA 5310 02615.
Part: FLOORBEAM — CORRODED (BS 986) · airframe 27,222 hrs · 14,775 cycles
FOUND FLOORBEAM CORRODED AROUND NUTPLATE HOLES. REMOVED COMPLETE UPPER TEE HORIZONTAL FLANGE FABRICATED AND INSTALLED UPPER TEE SPLICE ANGLES STRAPS FILLERS AND SHEAR TIES IAW ASA EA 5310 02615.
Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 27,215 hrs · 14,772 cycles
FOUND LT CARGO TRACK TIE DOWN LUG MISSING JUST FWD OF BSTA 500. REMOVED DAMAGED SECTION OF TRACK FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW ASA EA 5310 02614.
Part: DOUBLER — CRACKED (HORIZONTAL STAB) · airframe 27,215 hrs · 14,772 cycles
FOUND RT HORIZONTAL STAB LE BONDED DOUBLER IS CRACKED AT LE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5510 01236.
Part: SKIN — DAMAGED (L/E SLAT) · airframe 27,215 hrs · 14,772 cycles
NR 1 SLAT DAMAGED IN 2 PLACES ON UPPER SIDE. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.
Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 27,215 hrs · 14,772 cycles
NR 2 SLAT DELAMINATED AT OB TE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PIECES PER SRM 51 70 10.
Part: FRAME — LEAKING (RUDDER) · airframe 27,215 hrs · 14,772 cycles
FOUND RUDDER T/E HAS LIGHTING STRIKE 10" FROM TOP ON LT SIDE. REMOVED DAMAGED CONDUCTIVE FRAME FABRICATED AND INSTALLED REPLACEMENT CONDUCTIVE FRAME PER SRM.
Part: SKIN — DENTED (VERTICAL STAB) · airframe 27,215 hrs · 14,772 cycles
LT VERTICAL STABILIZER LE HAS GROUP OF DENTS AT STAB STA 90. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 55 10 01 FIG 201 REPAIR 2.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 27,215 hrs · 14,772 cycles
LT OB AFT FLAP TE REPAIR AT IB END DELAMINATED. REMOVED PREVIOUS REPAIR PREPPED AREA FABRICATED AND INSTALLED SKIN AND DOUBLER PIECES IAW SRM 51 70 10.
Part: SILL — CORRODED (BS 909-1006) · airframe 27,215 hrs · 14,772 cycles
FOUND R2 DOOR LOWER SILL INNER CHORD IS CORRODED. REMOVED CORRODED INNER CHORD INSTALLED NEW INNER CHORD IAW SRM 51 40 02 AND 51 40 05.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,215 hrs · 14,772 cycles
FOUND R2 DOOR LOWER SILL INNER CHORD IS CORRODED. REMOVED CORRODED INNER CHORD INSTALLED NEW INNER CHORD IAW SRM 51 40 02 AND 51 40 05.
Part: SILL — CORRODED (BS 909-1006) · corrosion level 2 · airframe 27,215 hrs · 14,772 cycles
FOUND L2 DOOR LOWER SILL INNER CHORD IS CORRODED. REMOVED CORRODED INNER CHORD INSTALLED NEW INNER CHORD PER SRM 51 40 02 AND 51 40 05.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 27,215 hrs · 14,772 cycles
FOUND R1 DOOR SURROUND FWD ATTACH ANGLE FROM LWR SILL TO 294.5 FRAME CORRODED. REMOVED CORRODED ANGLE FABRICATED AND INSTALLED ANGLE IAW SRM 51 40 02.
Part: STRUCTURE — CRACKED (ELEVATOR TAB) · airframe 27,215 hrs · 14,772 cycles
FOUND LT ELEVLATOR TAB NR 1 HINGE CUTOUT LE HAS MINOR CRACK. REPAIRED LT ELEVLATOR TAB IAW SRM 51 70 05 REPAIR 11.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,215 hrs · 14,772 cycles
FOUND L1 DOOR CUTOUT LOWER SILL INNER CHORD CORRODED. REMOVED CORRODED CHORD REPLACED WITH NEW CHORD IAW SRM 51 40 05.
Part: FRAME — CRACKED (FUSELAGE) · airframe 27,215 hrs · 14,772 cycles
FRAME IS CRACKED BETWEEN STRINGERS. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-10-02.
Part: FRAME — CORRODED (BS 986 S17R) · airframe 27,215 hrs · 14,772 cycles
FRAME CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.
2005
Part: SWITCH — FAILED (GROUND SAFETY)
PHX - AT 31,000 FEET AFTER 90 MINUTES IN CRUISE, PRESSURIZATION FAILED. AUTO THROTTLE AND TRANSPONDER FAILED AT SAME TIME. AUTO SPEED BRAKE WARNING LIGHT ILLUMINATED ALSO. REPLACED GROUND SAFETY SWITCH S-105, PER AMM 32-09-01. ALSO REFERENCE EA 3209-01001 FOR GROUND SAFETY SWITCH CLARIFICATION. SYSTEM OPS TEST NORMAL IAW AMM 32-09-01 PAGES 501-505. (M)
Part: STRAP — CORRODED (FLOORBEAM) · airframe 24,833 hrs · 13,500 cycles
AFT PIT FLOOR BEAM STRAP HAS CORROSION AS MARKED. REMOVED DAMAGED STRAP, INSTALLED NEW STRAP IAW SRM. (K)
Part: WEB — CORRODED (AFT CARGO BAY) · airframe 24,833 hrs · 13,500 cycles
AFT CARGO DOOR OPENING THRESHOLD WEB IS CORRODED. REMOVED AND REPLACED WEB ASSEMBLY IAW SRM. (K)
Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 24,833 hrs · 13,500 cycles
FWD CARGO DOOR SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM. (K)
Part: SKIN — DEBONDED (LT TE FLAP) · airframe 24,833 hrs · 13,500 cycles
LT OB AFT FLAP PREVIOUSLY INSTALLED REPAIR IS DEBONDING AT IB AFT CORNER. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)
Part: SKIN — DENTED (T/E FLAP) · airframe 24,833 hrs · 13,500 cycles
RT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DENTED AREA OF LOWER SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM. (K)
Part: WEDGE — DENTED (LT MIDFLAP) · airframe 24,833 hrs · 13,500 cycles
LT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS AND INSTALLED REPAIR PIECES IAW SRM. (K)
2004
Part: NOZZLE — DAMAGED (NR 1 TURBINE SEC)
FOUND LEFT NR 1 ENGINE EXHAUST NOZZLE AND PLUG ROTOR AND STATOR HAVE SUSTAINED SEVERE DAMAGE, RIPPED AND TORN BLADE SEGMENTS WITH MISSING MATERIAL. REMOVED AND REPLACED ENGINE PER T/C'S 4855400 AND 48571016. (M)
Part: STARTER — FAILED (NR 2 ENGINE)
OAK - FOUND INSPECTED NR 2 ENGINE, FOUND THE NR 2 STARTER HAD COME APART AND WAS DAMAGED. REMOVED AND REPLACED THE NR 2 ENGINE STARTER PER AMM. (M)
2001
Part: SLIDING WINDOW — BINDING (NR 2)
SEA - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING WINDOW HARD TO OPEN AND CLOSE. REMOVED, REPLACED AND RIGGED, WINDOW IAW MM, OPS NORMAL. (M)
Part: SKIN — PUNCTURED (FUSELAGE)
PAE - DURING LINE CHECK, FOUND PUNCTURE IN SKIN AT BS 363 TO 371, WATER LINE 207 AND STRINGER 17L. REPAIRED IAW EA 5330-01509. (M)