N785AS

CESSNA 172M · 1974 · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: A S FLIGHT ACADEMY LLC, FL (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.

154 reports on file, 1998-02-09 – 2009-03-26.

OTHER · 2009-03-26 Matched by certificate designator
ATA 5330

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

SKIN REPAIR OF LT MLG W/W FS 727 AT STR 26L HAS A GOUGE IN TRIPLER. REPAIRED TRIPLER IAW ASA EA 400 53EA 0096 REV NEW.

Source: SDR ASAA0944951
OTHER · 2009-03-24 Matched by certificate designator
ATA 5512

Part: SKIN — DENTED (HORIZ STAB) · airframe 40,959 hrs · 22,600 cycles

RT HORIZONTAL STABILIZER L/E IS DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 55 10 01.

Source: SDR ASAA0944908
OTHER · 2009-03-17 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STRINGER 10L AFT SIDE OF APB HAS ELONGATED BOLT HOLE IN END FITTING. REMOVED END FITTING, FABRICATED, MACHINED NEW FITTING, LOCATED, TREATED AND INSTALLED NEW END FITTING IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944880
OTHER · 2009-03-17 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STRINGER 10L AFT SIDE OF APB HAS ELONGATED BOLT HOLE IN END FITTING. REMOVED END FITTING, MACHINED NEW FITTING, LOCATED, TREATED AND INSTALLED NEW END FITTING IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944847
OTHER · 2009-03-16 Matched by certificate designator
ATA 5753

Part: SKIN — DAMAGED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

RIGHT O/B AFT FLAP DAMAGED. REMOVED PREVIOUS REPAIR AREA, FABRICATED, TREATED ,BONDED NEW SKIN AND DOUBLER REPAIR.

Source: SDR ASAA0944849
OTHER · 2009-03-16 Matched by certificate designator
ATA 5753

Part: SKIN — DAMAGED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

RIGHT WING O/B AFT FLAP DAMAGED. REMOVED PREVIOUS REPAIR AREA, FABRICATED, TREATED AND BONDED NEW SKIN AND DOUBLER REPAIR.

Source: SDR ASAA0944882
OTHER · 2009-03-13 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

R1 DOOR FWD LOWER CORNER STUB FRAME MISDRILLED. REMOVED STUB FRAME, RECEIVED, LOCATED AND INSTALLED NEW STUB FRAME IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944875
OTHER · 2009-03-13 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

R1 DOOR FWD LOWER CORNER STUB FRAME MISDRILLED. REMOVED STUB FRAME, RECEIVED, LOCATED AND INSTALLED NEW STUB FRAME IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944837
OTHER · 2009-03-10 Matched by certificate designator
ATA 5751

Part: AILERON — DELAMINATED (LT WING) · airframe 40,959 hrs · 22,600 cycles

LT AILERON LOWER I/B FORWARD CORNER DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PAINTED AND BALANCED AILERON IAW B737 400 SRM 57 60 02.

Source: SDR ASAA0944840
OTHER · 2009-03-10 Matched by certificate designator
ATA 5751

Part: AILERON — DELAMINATED (LT WING) · airframe 40,959 hrs · 22,600 cycles

LT AILERON LOWER I/B FORWARD CORNER DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PAINTED AND BALANCED IAW B737 400 SRM 57 60 02.

Source: SDR ASAA0944884
OTHER · 2009-03-06 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

ANGLE O/B OF R1 DOOR MOP SILL CORRODED. REMOVED CORRODED ANGLE, LOCATED DRILLED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944631
OTHER · 2009-03-05 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

DRILL MARKS ON INNER FUSELAGE SKIN STA 747 BETWEEN STRINGERS 8 9. BLENDED DRILL MARKS, FABRICATED AND INSTALLED REPAIR DOUBLER AND TEAR STRAP DOUBLER.

Source: SDR ASAA0944910
OTHER · 2009-03-04 Matched by certificate designator
ATA 5753

Part: WEDGE — DAMAGED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

LEFT INBOARD FLAP TRAILING EDGE WEDGE O/B END BENT / CRACKED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944751
OTHER · 2009-03-02 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FRAME STA 727D DENTED AND CORRODED ABOVE STR 25R. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR ANGLE AND FILLER IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944790
OTHER · 2009-02-26 Matched by certificate designator
ATA 5330

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

INTERNAL DOUBLER FOR SKIN SPLICE CORRODED FWD PIT STA 500C STR 26L 26R. REMOVED DOUBLER, FABRICATED, LOCATED AND DRILLED, AND INSTALLED NEW SPLICE DOUBLER IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944665
OTHER · 2009-02-26 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FRAME UPPER SURFACE CORRODED STA 727G LT. REMOVED CORRODED AREA, FABRICATED, TREATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944788
OTHER · 2009-02-26 Matched by certificate designator
ATA 2560

Part: FITTING — CORRODED (GIRT BAR) · airframe 40,959 hrs · 22,600 cycles

L1 DOOR AFT GIRT BAR MOUNT FITTING CORRODED. REMOVED FITTING REVIVED DRILLED AND INSTALLED NEW FITTING ASSY IAW B737 400 MM 20 50 11 912 002.

Source: SDR ASAA0944789
OTHER · 2009-02-25 Matched by certificate designator
ATA 5753

Part: ATTACH FITTING — CORRODED (MIDFLAP) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

RT INBOARD MID FLAP O/B TORQUE TUBE ATTACH FITTING CORRODED. REMOVED FITTING, LOCATED, DRILLED AND INSTALLED NEW ATTACH FITTING IAW 737 400 SRM 51 40 02.

Source: SDR ASAA0944594
OTHER · 2009-02-25 Matched by certificate designator
ATA 5753

Part: CARRIAGE — CORRODED (MIDFLAP) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

RIGHT O/B MID FLAP OUTBOARD CARRIAGE HALVES HAVE CORROSION IN BORES. REMOVED I/B CARRIAGE HALF INSTALLED NEW I/B CARRIAGE HALF IAW MM 27 51 14 O/B HALF CORROSION REMOVED AND IN LIMITS.

Source: SDR ASAA0944664
OTHER · 2009-02-25 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (FOREFLAP) · airframe 40,959 hrs · 22,600 cycles

LT OUTBOARD FOREFLAP DENTED T/ LOWER SURFACE APPROX WBL 360. REMOVED DAMAGED AREA, FABRICATED AND BONDED REPAIR MATERIAL IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944630
OTHER · 2009-02-24 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

INTERCOSTAL AT STA 794 HAS CORROSION. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW B737 400 SRM 51 40 02 INTERCOSTAL REPLACED WITH NEW PART.

Source: SDR ASAA0944568
OTHER · 2009-02-23 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FRAME UPPER SURFACE STA 727C STR 25L CORRODED. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944834
OTHER · 2009-02-23 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME SURFACE STA 727E CORRODED. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944791
OTHER · 2009-02-23 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FRAME UPPER SURFACE STA 727C STR 25L CORRODED. REMOVED DAMAGED AREA, FABRICATED TREATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944872
OTHER · 2009-02-23 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME STA 807 STRINGER 25L CORRODED. REMOVED DAMAGED AREA, INSTALLED NEW REPAIR ANGLE FILLER AND SHIM IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944715
OTHER · 2009-02-22 Matched by certificate designator
ATA 5320

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

AFT PIT SUPPORT ANGLE STA 794 STR 25R 27R CORRODED. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW B737 400 SRM 51 30 01.

Source: SDR ASAA0944738
OTHER · 2009-02-21 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

L1 DOOR LWR HINGE CUTOUT BEARING PLATE FITTING TO HAVE ELONGATED HOLE. REMOVED EXISTING HINGE FITTING AND INSTALLED NEW LOWER L1 DOOR HINGE FITTING IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944717
OTHER · 2009-02-20 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FWD PIT STR 28R CORRODED STA 500D 520. REMOVED CORRODED STRINGER CLIPS, FABRICATED, TREATED, LOCATED, INSTALLED NEW CLIPS IAW B737 400 SRM 53 00 03.

Source: SDR ASAA0944848
OTHER · 2009-02-20 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT STR 28R CORRODED STA 500D 520. REMOVED CORRODED STRINGER CLIPS, FABRICATED, TREATED, LOCATED AND INSTALLED NEW CLIPS IAW B737 400 SRM 53 00 03.

Source: SDR ASAA0944881
OTHER · 2009-02-19 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

INTERCOSTAL WEB HAS TOOLING DAMAGE AT STA 790 845. REMOVED DAMAGED WEB, INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944891
OTHER · 2009-02-18 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

PREVIOUS REPAIR AT STRINGER 25R STA 940 CORRODED. REMOVED CORRODED STRINGER, FABBED, TREATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 40 02 53 00 03.

Source: SDR ASAA0944595
OTHER · 2009-02-18 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FWD PIT FRAME CORRODED STA 500B BETWEEN STR 26R 27L. REMOVED CORROSION, FABBED, DRILLED AND INSTALLED SHEAR TIE REPAIR AW B737 400 SRM 53 00 07 51 20 01.

Source: SDR ASAA0944596
OTHER · 2009-02-18 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT FRAME STA 500E BETWEEN STR 28L 28R CORRODED. REMOVED CORROSION, FABRICATED, TREATED AND INSTALLED REPAIR SHEAR TIE IAW B737 400 SRM 53 00 07.

Source: SDR ASAA0944786
OTHER · 2009-02-18 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB STA 967 986 LBL 48 CORRODED. REMOVED CORRODED WEB, FABRICATED LOCATED AND DRILLED AND INSTALLED NEW SHEAR WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944600
OTHER · 2009-02-18 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB STA 986 992 LBL 45 CORRODED. REMOVED SHEAR WEB, FABRICATED AND INSTALLED NEW SHEAR WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944566
OTHER · 2009-02-17 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB STA 967 987 CORRODED. REMOVED 2 CORRODED SHEAR WEBS, FABRICATED, DRILLED AND INSTALLED NEW SHEAR WEBS IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944602
OTHER · 2009-02-16 Matched by certificate designator
ATA 5754

Part: SKIN — DENTED (LE SLAT) · airframe 40,959 hrs · 22,600 cycles

NR 3 SLAT LOWER SURFACE DENTED 18 INCHES FROM I/B END. REMOVED DAMAGED AREA, FABRICATED, TREATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944838
OTHER · 2009-02-16 Matched by certificate designator
ATA 5754

Part: SKIN — DENTED (LE SLAT) · airframe 40,959 hrs · 22,600 cycles

NR 3 SLAT LWR SURFACE DENTED 18 INCHES FROM I/B END. REMOVED DAMAGED AREA, FABRICATED, TREATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944885
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 5 SPOILER HAS DENT AT CENTER O/B HINGE AT T/E. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944540
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DELAMINATED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 6 SPOILER TRAILING EDGE DELAM. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944569
OTHER · 2009-02-16 Matched by certificate designator
ATA 5320

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT THRESHOLD WEB CORRODED STA 468 495. REMOVED CORRODED WEB, FABRICATED, TREATED, PRIMED, TOP COATED AND INSTALLED NEW THRESHOLD WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944878
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 6 SPOILER DENTED AT I/B HINGE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REP 2.

Source: SDR ASAA0944542
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 5 SPOILER HAS DENT ABOVE I/B HINGE ON T/E. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944541
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 5 SPOILER HAS CLUSTER OF 6 DENTS AROUND O/B HINGE. REMOVED DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.

Source: SDR ASAA0944538
OTHER · 2009-02-16 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 5 SPOILER HAS DENT AROUND O/B HINGE. REMOVED DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.

Source: SDR ASAA0944539
OTHER · 2009-02-16 Matched by certificate designator
ATA 5320

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT THRESHOLD WEB CORRODED STA 468 495. REMOVED CORRODED WEB, FABRICATED, TREATED, PRIMED, TOPCOATED AND INSTALLED NEW THRESHOLD WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944851
OTHER · 2009-02-15 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FLOORBEAM STA 344 LBL 50 CORRODED. REMOVED CORROSION, FABRICATED, DRILLED AND INSTALLED REPAIR STRAP IAW ASA EA 400 53EA 00780.

Source: SDR ASAA0944601
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 480 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944928
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 787L IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944932
OTHER · 2009-02-14 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

RIGHT I/B AFT FLAP LOWER SURFACE IS DENTED 2 PLACES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.

Source: SDR ASAA0944537
OTHER · 2009-02-14 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STRINGER CLIP CRACKED STA 663 STR 10L. REMOVED CRACKED CLIP INSTALLED NEW CLIP IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944545
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 480 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944929
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 907 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944931
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 787 IS CRACKED JUST BELOW STRINGER 8R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00946.

Source: SDR ASAA0944912
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 827 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944915
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 727D IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944930
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 440 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944914
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 500A IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944917
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 727B IS CRACKED JUST BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944913
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 500A IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944926
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 747 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944921
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 827 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944925
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 380 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944922
OTHER · 2009-02-14 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STIFFENER ANGLE CRACKED AT FS 294 BELOW STRINGER 9. REMOVED DAMAGED STIFFENER ANGLE FS 294 BELOW STRINGER 9 IAW B737 400 SRM 51 40 2, INSTALLED REPLACEMENT STIFFENER ANGLE.

Source: SDR ASAA0944784
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 500C IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944918
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 480 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944923
OTHER · 2009-02-14 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

SHEAR CLIP CRACKED AT FS 380 STRINGER 8R. REMOVED EXISTING STRINGER CLIP, LOCATED, DRILLED AND INSTALLED NEW STRINGER CLIP IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944536
OTHER · 2009-02-14 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STIFFENER ANGLE CRACKED AT FS 294 BELOW STRINGER 11. REMOVED DAMAGED STIFFENER ANGLE FS 294 BELOW STRINGER 11 IAW B737 400 SRM 51 40 2, INSTALLED REPLACEMENT STIFFENER ANGLE.

Source: SDR ASAA0944785
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 400 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944924
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 400 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944919
OTHER · 2009-02-14 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

STIFFENER ANGLE CRACKED AT FS 294 BELOW STRINGER 12. REMOVED DAMAGED STIFFENER ANGLE, LOCATED, DRILLED AND INSTALLED STIFFENER ANGLE IAW SRM 51 40 02.

Source: SDR ASAA0944711
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 500C IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944927
OTHER · 2009-02-14 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB STA 1016 WL 208 RBL 15 CORRODED. REMOVED CORRODED WEB, LOCATED, DRILLED AND INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944597
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 907L IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944933
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

R1 DOOR UPPER FWD STUB FRAME IS CRACKED. REMOVED CRACKED STUB FRAME, INSTALLED NEW STUB FRAME IAW B737 400 SRM 51 40 0.

Source: SDR ASAA0944902
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 867 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944916
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 747 IS CRACKED JUST BELOW STRINGER 8R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00946.

Source: SDR ASAA0944911
OTHER · 2009-02-14 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (FOREFLAP) · airframe 40,959 hrs · 22,600 cycles

LEFT O/B FORE FLAP DENTED ON UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Source: SDR ASAA0944548
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — BENT (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT UPPER FLANGE OF FRAME AT STA 727B BENT STR 21L 22L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944666
OTHER · 2009-02-14 Matched by certificate designator
ATA 5320

Part: STRAP — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE STA 312 RBL 24 HAS CRACKED STABILIZER STRAP. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 13.

Source: SDR ASAA0944892
OTHER · 2009-02-14 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FUSELAGE FRAME STA 440 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948.

Source: SDR ASAA0944920
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

R1 DOOR MOP SILL CORRODED. REMOVED CORRODED MOP SILL, INSTALLED NEW SILL IAW B737 400 SRM 51 40 03.

Source: SDR ASAA0944868
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

ZEE ANGLE EXTRUSION IS CORRODED STA 994 LBL 32 44 WL 208. REMOVED EXISTING ZEE ANGLE EXTRUSION, LOCATED, DRILLED, INSTALLED NEW ZEE ANGLE EXTRUSION IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944688
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB UPPER SURFACE CORRODED STA 987 LBL 32 48 WL 208. REMOVED LT SHEAR WEB, LOCATED, DRILLED, INSTALLED NEW SHEAR WEB IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944689
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

INTERCOSTAL CRACKED AT STA 500G+4 BL 0. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW INTERCOSTAL ANGLE IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944547
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: SKIN — CHAFED (FOREFLAP) · airframe 40,959 hrs · 22,600 cycles

RIGHT O/B FORE FLAP I/B LEADING EDGE CHAFED. REMOVED DAMAGED SECTION OF LEADING EDGE SKIN FABRICATED AND INSTALLED REPLACEMENT SECTION OF LEADING EDGE SKIN IAW B DWG 65C35705.

Source: SDR ASAA0944871
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

ZEE ANGLE STA 994 RBL 32 44 WL 208 CORRODED. REMOVED CORRODED ZEE ANGLE, LOCATED, DRILLED INSTALLED NEW ZEE ANGLE IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944712
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

NR 7 FLAP TRACK PITTED. REMOVED FLAP TRACK RECEIVED NEW TRACK AND INSTALLED IAW ASA EA 400 57EA 006617.

Source: SDR ASAA0944850
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

INTERCOSTAL STA 927 947 RBL 22 WL 208 CRACKED. REMOVED CRACKED ANGLE, FABRICATED LOCATED AND INSTALLED NEW INTERCOSTAL ANGLE IAW B737 400 SRM 51 40 2.

Source: SDR ASAA0944787
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

LEFT O/B AFT FLAP OUTBOARD TRAILING EDGE CORNER SPLIT AND DELAMINATED. REMOVED PREVIOUS REPAIR, FABRICATED AND BONDED DOUBLER AND SKIN REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Source: SDR ASAA0944734
OTHER · 2009-02-13 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

L1 DOOR UPPER HINGE FITTING CRACKED. REMOVED CRACKED FITTING INSTALLED NEW HINGE FITTING B737 400 SRM 51 40 02.

Source: SDR ASAA0944546
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

SHEAR WEB CORRODED STA 986 RBL 31 WL 208. REMOVED CORRODED WEB, RECEIVED, LOCATED, DRILLED, INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944736
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (TE FLAP) · airframe 40,959 hrs · 22,600 cycles

LEFT O/B AFT FLAP DENTED 31 INCHES FROM OUTBOARD EDGE LOWER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Source: SDR ASAA0944735
OTHER · 2009-02-13 Matched by certificate designator
ATA 5522

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 40,959 hrs · 22,600 cycles

LT ELEVATOR UPPER SURFACE HAS HOLE. REMOVED DAMAGE, INSTALLED RESIN AND REPAIR PLIES TO ELEVATOR SURFACE IAW B737 400 SRM 55 20 01 51 70 02 REP 2.

Source: SDR ASAA0944549
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: FLAP TRACK — DAMAGED (TE FLAP) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

NR 7 FLAP TRACK PITTED. REMOVED FLAP TRACK, RECEIVED NEW TRACK AND INSTALLED IAW 400 57EA 00617.

Source: SDR ASAA0944883
OTHER · 2009-02-13 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

L1 DOOR MOP SILL CORRODED. REMOVED CORRODED MOP SILL, INSTALLED NEW SILL IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944869
OTHER · 2009-02-13 Matched by certificate designator
ATA 5753

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

NR 1 FLAP TRACK HAS PITTING CORROSION ON ROLLER CONTACT AREA. REMOVED AND REPLACED NR 1 FLAP TRACK IAW B737 400 MM 27 51 49.

Source: SDR ASAA0944909
OTHER · 2009-02-12 Matched by certificate designator
ATA 5754

Part: WEDGE — DENTED (LE SLAT) · airframe 40,959 hrs · 22,600 cycles

NR 3 SLAT LOWER SURFACE T/E WEDGE IS DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.

Source: SDR ASAA0944544
OTHER · 2009-02-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT LOWER FLANGE OF FRAME HAS SEVERAL AREAS OF CORROSION AT STA 500F BETWEEN STR 26R 26L. REMOVED DAMAGED SHEAR TIE SECTION OF FRAME, FABRICATED, DRILLED INSTALLED SHEAR TIES IAW B737 400 SRM 53 00 07.

Source: SDR ASAA0944685
OTHER · 2009-02-12 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

L2 MOP SILL INNER CHORD IS CORRODED IN SEVERAL AREAS. REMOVED L2 MOP SILL INNER CHORD, LOCATED, DRILLED INSTALLED INNER CHORD IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944686
OTHER · 2009-02-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD FRAME LOWER FLANGE STA 500C STR 28L 28R CORRODED. REMOVED CORRODED ARE, FABRICATED, TREATED AND INSTALLED REPAIR DOUBLER TRIPLER IAW ASA EA 400 53EA 00934.

Source: SDR ASAA0944901
OTHER · 2009-02-12 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

R2 DOOR MOP SILL INNER CHORD CORRODED. REMOVED CORRODED CHORD, LOCATED, DRILLED, INSTALLED NEW CHORD IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944713
OTHER · 2009-02-12 Matched by certificate designator
ATA 5755

Part: SKIN — DENTED (SPOILER) · airframe 40,959 hrs · 22,600 cycles

NR 4 SPOILER HAS DENTS ON UPPER SURFACE. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REP 2.

Source: SDR ASAA0944543
OTHER · 2009-02-12 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

STA 986.5 FLOORBEAM UPPER FLANGE CORRODED. REMOVED ENTIRE UPPER FLANGE, FABRICATED AND INSTALLED REPLACEMENT UPPER FLANGE CHORD SPLICE ANGLES AND SPLICE STRAPS IAW EA 400 53EA 00794.

Source: SDR ASAA0944867
OTHER · 2009-02-12 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

FLOORBEAM UPPER FLANGE CORRODED STA 947 LBL 6 TO RBL 6. REMOVED FLOORBEAM UPPER CAP FABRICATED AND INSTALLED SPLICE REPAIR IAW EA 400 53EA 007.

Source: SDR ASAA0944737
OTHER · 2009-02-12 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

INTERCOSTAL CORRODED STA 947 967 STR 27R. REMOVED CORRODED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW B DWG 65 49679.

Source: SDR ASAA0944870
OTHER · 2009-02-12 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

LT MOP SILL IS CORRODED IN SEVERAL AREAS. REMOVED LT MOP SILL INNER CHORD, LOCATED, DRILLED, INSTALLED INNER CHORD IAW B737 400 SRM 51 40 05.

Source: SDR ASAA0944716
OTHER · 2009-02-12 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

L1 DOOR LWR HINGE CUTOUT BEARING PLATE FITTING HAS ELONGATED HOLE. REMOVED EXISTING HINGE FITTING AND INSTALLED NEW LOWER L1 DOOR HINGE FITTING IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944687
OTHER · 2009-02-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

FWD PIT LOWER FLANGE OF FRAME AT STA 500G CORRODED AT STR 26R 27R. REMOVED DAMAGED SHEAR TIE SECTION OF FRAME, FABRICATED, DRILLED, INSTALLED FRAME REPAIR IAW B737 400 SRM 53 00 07.

Source: SDR ASAA0944684
OTHER · 2009-02-11 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT WEB CORRODED STA 787 847 STR 25R 26R. REMOVED CORRODED WEB, RECEIVED, LOCATED, TREATED AND INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944841
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME UPPER FLANGE BENT STA 747 ABOVE STR 25R. REMOVED DAMAGED AREA, FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944839
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME UPPER FLANGE BENT STA 747 ABOVE STR 25R. REMOVED DAMAGED AREA, FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944876
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME STA 727A UPPER FLANGE CREASED. REMOVED DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 11 FIG 1.

Source: SDR ASAA0944550
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — BENT (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME AT STA 727 UPPER FLANGE BENT AT STR 24R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED PART IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944683
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME UPPER FLANGE BENT STA 727B STR 24L 25L. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944835
OTHER · 2009-02-11 Matched by certificate designator
ATA 5310

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

AFT CARGO DOOR LOWER CUTOUT SUPPORT ANGLE CORRODED STA 794.3 STR 24R 25R. REMOVED CORRODED ANGLE, FABRICATED, LOCATED, TREATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944836
OTHER · 2009-02-11 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

AFT PIT WEB CORRODED STA 787 847 STR 25R 26R. REMOVED CORRODED WEB, RECEIVED, LOCATED, TREATED AND INSTALLED NEW WEB IAW B737 400 SRM 51 40 02.

Source: SDR ASAA0944877
OTHER · 2009-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT PIT FRAME UPPER FLANGE BENT STA 727B STR 24L 25L. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED FRAME REPAIR IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944873
OTHER · 2009-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,959 hrs · 22,600 cycles

AFT CARGO DOOR LOWER CUTOUT SUPPORT ANGLE CORRODED STA 794 STR 24R 25R. REMOVED CORRODED ANGLE, FABRICATED, LOCATED, TREATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 51 70 11.

Source: SDR ASAA0944874
OTHER · 2009-02-11 Matched by certificate designator
ATA 5522

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 40,959 hrs · 22,600 cycles

RT ELEVATOR LOWER T/E IS SEPARATING. REMOVED DAMAGED PLIES, REPLACED DAMAGED PLIES AND INSTALLED TWO ADDITIONAL PLIES IAW ASA 400 55EA 00914.

Source: SDR ASAA0944890
OTHER · 2009-02-11 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,959 hrs · 22,600 cycles

AFT PIT CARGO DOOR CUTOUT WEB AFT FRAME CORRODED. REMOVED EXISTING REPAIR DOUBLER, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER.

Source: SDR ASAA0944535
OTHER · 2009-02-10 Matched by certificate designator
ATA 5754

Part: WEDGE — CHAFED (LE SLAT) · airframe 40,959 hrs · 22,600 cycles

NR 3 SLAT T/E WEDGE WORN THIN I/B AFT LOWER CORNER. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED NEW SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.

Source: SDR ASAA0944893
Earlier reports · 1998–2006 · 32 reports

2006

OTHER · 2006-09-05 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (BS 747 S27-28R) · airframe 33,494 hrs · 18,383 cycles

AFT CARGO PIT HAS CORROSION ON FRAME AT FWD AND AFT SIDES. CORRODED FRAME REPAIRED IAW SRM 53-00-07 FIG 201.

Source: SDR ASAA0640930
OTHER · 2006-09-05 Matched by certificate designator
ATA 5511

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,494 hrs · 18,383 cycles

LEFT HORZ STAB L/E ONE INNER RIB CRACKED AT STAB STATION. CRACK FOUND AT AFT L/E ASSY REMOVED. CRACKED L/E INNER RIB REPLACED WITH NEW PART IAW SRM 51-40-02.

Source: SDR ASAA0640935
OTHER · 2006-09-05 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (RT AFT FLAP) · airframe 33,494 hrs · 18,383 cycles

RIGHT INBOARD AFT FLAP L/E SKIN DENTED. REPLACED DENTED SKIN WITH FABRICATED REPAIR PARTS IAW SRM 50-30-01 AND 51-40-02.

Source: SDR ASAA0640938
OTHER · 2006-09-05 Matched by certificate designator
ATA 5753

Part: SKIN — CHAFED (WS 639) · airframe 33,494 hrs · 18,383 cycles

LEFT INBOARD T/E FLAP EXHAUST GATE UPPER SKIN IS CHAFED AT FWD O/B CORNER. REPLACED EXHAUST GATE IAW AMM 27-51-05.

Source: SDR ASAA0640939
OTHER · 2006-09-05 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 986) · airframe 33,494 hrs · 18,383 cycles

FLOORBEAM UPPER CAP CORRODED AT CLIP NUT LOCATION. CORRODED FLOORBEAM UPPER CAP REPAIRED IAW SRM 53-60-51 FIG 201.

Source: SDR ASAA0640934
OTHER · 2006-09-05 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CORRODED (BS 795 S29R) · airframe 33,494 hrs · 18,383 cycles

AFT PIT TIE CLIP CORRODED. REPLACED WITH FABRICATED PART IAW SRM 51-30-01 AND 51-40-02.

Source: SDR ASAA0640932
OTHER · 2006-09-05 Matched by certificate designator
ATA 5330

Part: SKIN — GOUGED (BS 328-344) · airframe 33,494 hrs · 18,383 cycles

E&E COMPARTMENT DOOR EXTERNAL SKIN GOUGED 5 INCHES AFT OF FWD EDGE RIGHT SIDE. REPAIRED IAW SRM 53-00-01 FIG 201.

Source: SDR ASAA0640931
OTHER · 2006-09-05 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CORRODED (BS 807) · airframe 33,494 hrs · 18,383 cycles

AFT PIT TIE CLIP CORRODED. AFT PIT CORRODED TIE CLIP REPLACED WITH FABRICATED PART IAW SRM 51-30-01 AND 51-40-02.

Source: SDR ASAA0640940
OTHER · 2006-09-05 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 33,494 hrs · 18,383 cycles

AFT PIT TIE CLIP CRACKED. REPLACED CRACKED TIE CLIP WITH FABRICATED REPAIR PART IAW SRM 51-30-01 AND 51-40-01.

Source: SDR ASAA0640933
OTHER · 2006-09-05 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (BS 500) · airframe 33,494 hrs · 18,383 cycles

CORROSION ON FRAME TO SKIN ATTACH ANGLE. CORRODED FRAME TO SKIN ATTACH ANGLE REPAIRED IAW SRM 53-00-07 FIG 201.

Source: SDR ASAA0640936
OTHER · 2006-09-05 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (BS 500B) · airframe 33,494 hrs · 18,383 cycles

CORROSION ON SKIN TO FRAME ATTACH ANGLE IN FWD CARGO PIT. REPAIRED IAW SRM 53-00-07.

Source: SDR ASAA0640937

2005

OTHER · 2005-06-05 Matched by certificate designator
ATA 5753

Part: SKIN — DENTED (T/E FORE FLAP)

DENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)

Source: SDR ASAA0540293

2004

OTHER · 2004-04-26 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND FLOORBEAM UPPER CAP IS CORRODED AT CLIP FROM RBL 24-49. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR, TREATED AND PRIMED AND INSTALLED, REF 737 SRM 53-00-51. (M)

Source: SDR ASAA0440114
OTHER · 2004-04-25 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIPNUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND RELACED UPPER CAP AT STATION 986 RBL 24 TO RBL 49. (M)

Source: SDR ASAA0440118
OTHER · 2004-04-20 Matched by certificate designator
ATA 5512

Part: SKIN — DENTED (HORIZONTAL STAB)

GYR - FOUND DEN ON HORIZ STAB LEADING EDGE APPROX 50 INCHES FROM INBOARD EDGE MEASURED 1 INCH DIAMETER .040 DEEP. REPAIRED DENT IAW SRM 55-10-01 AND REPAIRED RIB PER SRM 55-10-09. (M)

Source: SDR ASAA0440108
OTHER · 2004-04-20 Matched by certificate designator
ATA 5512

Part: SKIN — DENTED (HORIZONTAL STAB)

FOUND TWO EACH DENTS ON HORIZONTAL STABILIZER LEADING EDGE, ONE AT 13 INCHES FROM INBOARD PLUS 1.25 INCHES BY .875 BY .020 DEEP, ONE AT 50 INCHES FROM INBOARD EDGE REF LOG PAGE 5755154. REPAIRED DENTES ON RIGHT HORIZONTAL STABILIZER LEADING EDGE PER SRM 55-10-01. (M)

Source: SDR ASAA0440109
OTHER · 2004-04-20 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE)

FOUND DENT IN FUSELAGE SKIN, AFT OF L1 DOOR, 8 INCHES ABOVE VERT. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGER 17L AND 18L REF SRM 53-00-01 FIG 201. (M)

Source: SDR ASAA0440116
OTHER · 2004-04-15 Matched by certificate designator
ATA 5712

Part: RIB — CRACKED (LT WING)

GYR - FOUND LEFT WING INTERNAL RIB AT WING STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOEWR CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M)

Source: SDR ASAA0440115
OTHER · 2004-04-13 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSLEAGE)

GYR - FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIP NUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND REPLACED UPPER CAP AT STATION 986 RBL 24 TO RBL 49. (M)

Source: SDR ASAA0440104
OTHER · 2004-04-12 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE)

GYR - AFT CARGO DOOR OUTER SKIN DENTED AND GOUGED IN NUMEROUS PLACES. REPLACED THE AFT CARGO DOOR OUTER SKIN. (M)

Source: SDR ASAA0440126
OTHER · 2004-04-07 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE)

FOUND FS 360 AT STRINGER 8L FRAME IS CRACKED AT SIDEWALL LIGHT ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT STRINGER 8L. (M)

Source: SDR ASAA0440117
OTHER · 2004-04-07 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE)

GYR - FOUND STATION 360 AT 8L FRAME IS CRACKED AT SIDEWALL ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT 8L. (M)

Source: SDR ASAA0440100
OTHER · 2004-04-05 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE)

GYR - FOUND AFT PIT STRINGER 25R IS EXFOLIATED AT STATION 940. CUTOUT DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PART AND INSTALLED REPAIR IAW SRM 53-00-03 FIG 201. (M)

Source: SDR ASAA0440113
OTHER · 2004-04-04 Matched by certificate designator
ATA 5312

Part: BULKHEAD — DAMAGED (FUSELAGE)

FOUND BULKHEAD STATION 178 HAS WEB DAMAGED WL 219, LBL 18.1, PART NR 65-16300-511. REPAIR DAMAGED WEB IAW ASA EA 5310-02343 PAGE 3 STEP 3. (M)

Source: SDR ASAA0440119

2003

NO TEST · 2003-03-17 Matched by certificate designator
ATA 5410

Part: STRUCTURE — CHAFED (RT PYLON)

PAE - DURING C-CHECK, FOUND WEB OUTBOARD OF RIGHT PYLON IN AFT FLAP WELL IS CHAFED. REPAIRED IAW SRM. (M)

Source: SDR ASAA02401AA
NO TEST · 2003-03-17 Matched by certificate designator
ATA 5753

Part: FLAP TRACK — WORN (LT WING)

PAE - DURING C-CHECK, FOUND LEFT OUTBOARD FOR FLAP TRACKS ARE WORN INBOARD TRACK. REPAIRED IAW SRM. (M)

Source: SDR ASAA02401AB

2002

NO TEST · 2002-03-12 Matched by certificate designator
ATA 3397

Part: WIRE — LOOSE (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 14-15. RECONNECTED LOOSE WIRES, OPS CHECK NORMAL. (M)

Source: SDR ASAA0240029

2001

NO TEST · 2001-02-09 Unresolved
ATA 3397

Part: WIRE — BROKEN (CABIN)

SEA - WHILE PERFORMING A LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 1 INOPERATIVE, WIRE BROKEN. REMOVED AND REPLACED EMERGENCY FLOOR ASSEMBLY. OPS CHECKED GOOD. (M)

Source: SDR ASAA0140022

2000

NO TEST · 2000-12-20 Unresolved
ATA 3397

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK INSPECTION, FOUND FLOOR EMERGENCY EXIT LIGHTING INOPERATIVE AT LEFT OVERWING EXIT. RECONNECT WIRE, OPS CHECK NORMAL. (M)

Source: SDR ASAA0040155
NO TEST · 2000-05-25 Unresolved
ATA 3397

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-15 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Source: SDR ASAA0040070

1999

OTHER · 1999-04-17 Matched by certificate designator
ATA 5240

Part: MECHANISM — LACK OF LUBE (L-2 DOOR)

ANC - FLT 88 - L-2 DOOR DIFFICULT TO OPEN AND CLOSE, MAKES METAL GRINDING NOISE. LUBED DOOR ARMS AND ROLLER TRACKS, AND DOOR OPERATED NORMALLY. (M)

Source: SDR ASAA9940092

1998

OTHER · 1998-02-09 Matched by certificate designator
ATA 5610

Part: ROLLER — LOOSE (LT COCKPIT)

SEA - FLT 84 - PRIOR TO FLIGHT, THE CAPTAIN'S SLIDING WINDOW COULD NOT BE CLOSED. SECURED LOOSE ROLLER AT BOTTOM AFT SIDE OF WINDOW AND WINDOW OPERATED NORMALLY. (X)

Source: SDR ASAA9840028