# N784AS: 1996 Boeing 737-4Q8, registration cancelled 2010-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 2010
- Exported to: Turkey
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-4Q8](https://openairdocs.org/model/boeing-737-4q8) (registry code 138447Q)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 28199
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 1996
- Certificate issued: November 19, 1996
- Last registry action: June 16, 2009
- Mode S code: AA9F73
- Owner when cancelled: [International Lease Finance Corporation](https://openairdocs.org/faa-owner/INTERNATIONAL%20LEASE%20FINANCE%20CORPORATION)
- Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles)
- Owner type: Corporation
- Owner's area on the map: 34.0564° N, 118.4137° W: Placed by OpenAirDocs at the center of ZIP code 90067, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N784AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=784AS
- Page: https://openairdocs.org/deregistered/N784AS-2010-02-01

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-4Q8: https://openairdocs.org/model/boeing-737-4q8.md

## Service difficulty reports (107, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASAA0947171](https://openairdocs.org/sdr/ASAA0947171), Dec 29, 2009: INTERCOSTAL. CRACKED. FOUND CRACKED INTERCOSTAL IN E RACK. REMOVED AND REPLACED INTERCOSTAL.
- [SDR ASAA0947157](https://openairdocs.org/sdr/ASAA0947157), Dec 18, 2009: PANEL. CHAFED. PANEL 9220 LOWER SURFACE IS CHAFED. FABRICATED PANEL.
- [SDR ASAA0947156](https://openairdocs.org/sdr/ASAA0947156), Dec 18, 2009: SUPPORT. CRACKED. RIGHT WING FIX T/E INBOARD UPPER PANEL SUPPORT INBOARD OF NR 5 SPOILER CRACKED. REMOVED AND REPLACED RT FIXED T/E UPPER PANEL SUPPORT.
- [SDR ASAA0947162](https://openairdocs.org/sdr/ASAA0947162), Dec 11, 2009: SKIN. DELAMINATED. RIGHT I/B AFT FLAP O/B END IS DELAMINATED. REMOVED EXISTING REPAIR AND ACCOMPLISHED LARGE REPAIR.
- [SDR ASAA0947161](https://openairdocs.org/sdr/ASAA0947161), Dec 11, 2009: SKIN PANEL. CHAFED. PANEL 9503 HAS CHAFING DAMAGE ON THE INNER SURFACE. FABRICATED NEW PANEL.
- [SDR ASAA0947152](https://openairdocs.org/sdr/ASAA0947152), Dec 11, 2009: PANEL. CRACKED. RIGHT WING T/E UPPER SURFACE PANEL O/B OF NR 5 SPOILER HAS A CRACK IN THE RADIUS. REPAIRED UPPER SURFACE OF PANEL.
- [SDR ASAA0947142](https://openairdocs.org/sdr/ASAA0947142), Dec 11, 2009: PANEL. CRACKED. RT WING T/E UPPER SURFACE PANEL O/B OF NR 5 SPOILER HAS A CRACK IN THE RADIUS. REPAIRED UPPER SURFACE PANEL.
- [SDR ASAA0947153](https://openairdocs.org/sdr/ASAA0947153), Dec 9, 2009: SKIN. DELAMINATED. NR NR 1 ENGINE COWL OUTER SURFACE IS DELAMINATED WITH DAMAGED FIBERS AT 1:00 POSITION. REPAIRED PER EA
- [SDR ASAA0947154](https://openairdocs.org/sdr/ASAA0947154), Dec 9, 2009: COWLING. DELAMINATED. NR 1 ENGINE I/B FAN COWL LWR AFT CORNER IS DELAMINATED. REPAIRED NR 1 IB COWL.
- [SDR ASAA0843959](https://openairdocs.org/sdr/ASAA0843959), Dec 1, 2008: GUIDE ARM. STIFF. L1 DOOR HARD TO CLOSE FROM INSIDE FOUND WHILE REPOSITIONING JETWAY AFTER ARRIVAL. ADJUSTED L1 DOOR GUIDE ARM REF M/M 52-11-00-705-007-B00. OPERATED NORMALLY OK 
- [SDR ASAA0843419](https://openairdocs.org/sdr/ASAA0843419), Aug 25, 2008: TAB. GOUGED. LT WING AILERON TRIM TAB T/E GOUGED. LT WING AILERON TRIM TAB T/E GOUGE REPAIRED IAW B737 400 SRM CH 51 70 06.
- [SDR ASAA0843418](https://openairdocs.org/sdr/ASAA0843418), Aug 25, 2008: SKIN. DELAMINATED. LT WING AILERON TRIM TAB HAS DELAM. LT WING AILERON TRIM TAB REPAIRED IAW B737 400 SRM CH 51 70 16.
- [SDR ASAA0843420](https://openairdocs.org/sdr/ASAA0843420), Aug 25, 2008: SKIN. DENTED. DENT 1 AND 2 (WBL 87.5 AND WBL 87.8) FOUND BEYOND ALLOWABLE LIMITS IAW B737 400 SRM 57 53 02. TRANSFERRED FROM MIG5 NR 5106400 LT INBOARD MID FLAP T/E WEDGE. LT
- [SDR ASAA0843414](https://openairdocs.org/sdr/ASAA0843414), Aug 22, 2008: STRINGER CLIP. DAMAGED. AFT CARGO PIT BS 727F STR 26L TIE CLIP DAMAGE. TIE CLIP REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 40 02 AND B DRAWG SPECS 69 35350.
- [SDR ASAA0843421](https://openairdocs.org/sdr/ASAA0843421), Aug 20, 2008: SKIN. DENTED. DENT FOUND AT A C, SKIN AT BS 727F BETWEEN STR 25L AND 26L. REPAIRED IAW ERO 8620 AND EA 5330 02385.
- [SDR ASAA0843413](https://openairdocs.org/sdr/ASAA0843413), Aug 16, 2008: SKIN. DAMAGED. LEFT HORIZONTAL STAB LEADING EDGE PREVIOUS BLEND OUT AT APPROX STAB STA 98.70 HAS NICK IN THE BLEND OUT. NICK BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMIT
- [SDR ASAA0843423](https://openairdocs.org/sdr/ASAA0843423), Aug 12, 2008: SKIN. DAMAGED. LOWER FUSELAGE SKIN DAMAGED AT BS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW CASCADE ERO 8610 AND ASA EA 5330 02383.
- [SDR ASAA0843422](https://openairdocs.org/sdr/ASAA0843422), Aug 12, 2008: SKIN. DENTED. DENT IN EXTERIOR SKIN OF FUSELAGE AT BS 331.5 BETWEEN STR 20R AND 21R. REPAIRED IAW CASCADE ERO 8620 AND EA 5330 02384.
- [SDR ASAA0843416](https://openairdocs.org/sdr/ASAA0843416), Aug 12, 2008: SKIN. DAMAGED. LWR FUSELAGE SKIN DAMAGED AT FS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW ERO 8610 AND EA 5330 02383.
- [SDR ASAA0843415](https://openairdocs.org/sdr/ASAA0843415), Aug 12, 2008: FRAME. CRACKED. FRAME INNER CHORD BS 616 RT BELOW FLOOR IS CRACKED FROM BOTTOM TIP TO THE LWR HOLE. REPAIRED IAW ERO 8605 AND EA 5310 028114
- [SDR ASAA0843417](https://openairdocs.org/sdr/ASAA0843417), Aug 11, 2008: SKIN. DAMAGED. RT ENGINE INLET COWL LIP SKIN AT 6 O'CLOCK POSITION MULTIPLE SCRATCHES. REPAIRED IAW GRO8617 AND EA.
- [SDR ASAA0842538](https://openairdocs.org/sdr/ASAA0842538), Jan 29, 2008: SKIN. DEFORMED. L1 DOOR UPPER AFT CORNER DEFORMED. INSTALLED REPAIR DOUBLER IAW SRM 52 00 01 REPAIR 2. PAINTED PER MM 51 20 99.
- [SDR ASAA0742054](https://openairdocs.org/sdr/ASAA0742054), Sep 16, 2007: LENS. CRACKED. EXIT INDICATOR AT EMERGENCY EXIT DOOR ROW 13 LEFT LENS FELL OFF. FOUND LENS CRACKED DUE OVER TORQUED. REPLACED LENS.
- [SDR ASAA0742011](https://openairdocs.org/sdr/ASAA0742011), Sep 1, 2007: SKIN. DAMAGED. DAMAGE TO LEFT HORIZONTAL STABILIZER TIP DUE TO CONTACT FROM AC PUSHING BACK. REFERENCE SDR ASAA0742008. TEMPORARY REPAIR TO LEFT HAND HORIZONAL STAB TIP REPAIR
- [SDR ASAA0742008](https://openairdocs.org/sdr/ASAA0742008), Aug 27, 2007: SKIN. DAMAGED. DAMAGE TO LEFT HORIZONAL STABILIZER TIP DUE TO CONTACT FROM AIRCRAFT PUSHING BACK INTO ALLEY. INTERM REPAIR PER EA 5510 01303 AIRCRAFT RELEASED FOR FERRY FLIGHT
- [SDR ASAA0741717](https://openairdocs.org/sdr/ASAA0741717), May 30, 2007: SKIN. DENTED. FUSELAGE SKIN SCRATCHED AND DENTED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5330 02212.
- [SDR ASAA0741716](https://openairdocs.org/sdr/ASAA0741716), May 30, 2007: SKIN. DENTED. DENT IN FUSELAGE SKIN. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLERS DOUBLERS AND TRIPLER IAW ASA EA 5330 02211.
- [SDR ASAA0741703](https://openairdocs.org/sdr/ASAA0741703), May 29, 2007: ATTACH FITTING. CRACKED. NR 4 GROUND SPOILER O/B ACTUATOR ATTACH FITTING IS BROKEN IN TWO PIECES. NR 4 GROUND SPOILER REMOVED AND REPLACED IAW AMM 27-62-12.
- [SDR ASAA0741702](https://openairdocs.org/sdr/ASAA0741702), May 29, 2007: SKIN. DELAMINATED. LEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED AT I/B AFT CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.
- [SDR ASAA0741701](https://openairdocs.org/sdr/ASAA0741701), May 27, 2007: FITTING. GOUGED. NR 9 FLIGHT SPOILER FITTING IS GOUGED AT ACTUATOR ATTACH POINT. REMOVED AND REPLACED SPOILER ASSY IAW AMM 27-62-71.
- [SDR ASAA0741700](https://openairdocs.org/sdr/ASAA0741700), May 27, 2007: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED. REMOVED DAMAGED SECTION OF FRAME SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE FILLER AND ANGLE IAW SRM 53-00-07 REPAIR 3.
- [SDR ASAA0741699](https://openairdocs.org/sdr/ASAA0741699), May 27, 2007: FRAME. CRACKED. FRAME SKIN ATTACHMENT ANGLE IS CRACKED AT ATTACHMENT HOLE. REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR SHEAR TIE FILLER AND ANGLE IAW SRM 5
- [SDR ASAA0741698](https://openairdocs.org/sdr/ASAA0741698), May 23, 2007: FRAME. CORRODED. FRAME IS CORRODED. REMOVED CORRODED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR SECTION OF FRAME IAW SRM 53-00-07 REPAIR 3.
- [SDR ASAA0741697](https://openairdocs.org/sdr/ASAA0741697), May 23, 2007: CARGO TRACK. GOUGED. CARGO TIE DOWN IS GOUGED. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW ASA EA 5310 02722.
- [SDR ASAA0741696](https://openairdocs.org/sdr/ASAA0741696), May 23, 2007: FITTING. CORRODED. NR 4 SPOILER INBOARD ACTUATOR MOUNT FITTING HAS FRETTING CORROSION. REMOVED FITTING, INSTALLED NEW FITTING IAW SRM 51-40-02.
- [SDR ASAA0741692](https://openairdocs.org/sdr/ASAA0741692), May 22, 2007: STIFFENER. CORRODED. APU AIR INLET TORQUE BOX OPENING AFT VERTICAL STIFFENER CORRODED AT FASTENER HOLES. REMOVED CORRODED STIFFENER, FABRICATED AND INSTALLED STIFFENER IAW SRM 51-30
- [SDR ASAA0741691](https://openairdocs.org/sdr/ASAA0741691), May 22, 2007: SKIN. CHAFED. NR 4 SLAT IS CHAFED AT INBOARD CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.
- [SDR ASAA0741690](https://openairdocs.org/sdr/ASAA0741690), May 22, 2007: SKIN. DAMAGED. NR 3 SLAT INBOARD TRAILING EDGE HAS COMPOSITE LAYERS SHOWING. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.
- [SDR ASAA0741689](https://openairdocs.org/sdr/ASAA0741689), May 22, 2007: FLOORBEAM. CORRODED. FLOORBEAM UPPER CHORD IS CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAP AND TAPERED SHIMS IAW ASA EA 5310 02721.
- [SDR ASAA0741652](https://openairdocs.org/sdr/ASAA0741652), May 20, 2007: WEB. CORRODED. WEB BELOW R1 DOOR CUTOUT IS CORRODED ON LOWER SURFACE. REMOVED CORRODED WEB, FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-02.
- [SDR ASAA0741655](https://openairdocs.org/sdr/ASAA0741655), May 20, 2007: SKIN. DENTED. LEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10.
- [SDR ASAA0741654](https://openairdocs.org/sdr/ASAA0741654), May 20, 2007: TAB. CRACKED. RIGHT ELEVATOR TAB NR 3 HINGE CUTOUT IS CRACKED. PREPPED DAMAGED AREA, FABRICATED AND BONDED REPAIR IAW SRM 51-70-17 REPAIR 7.
- [SDR ASAA0741639](https://openairdocs.org/sdr/ASAA0741639), May 16, 2007: SILL. CORRODED. R1 DOOR SILL (INNER CHORD) IS CORRODED. REMOVED CORRODED SILL, REPLACED WITH NEW PART IAW SRM 51-40-02.
- [SDR ASAA0741637](https://openairdocs.org/sdr/ASAA0741637), May 16, 2007: SILL. CORRODED. AR AFT MOPSILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02.
- [SDR ASAA0741636](https://openairdocs.org/sdr/ASAA0741636), May 16, 2007: SILL. CORRODED. LEFT AFT MOP SILL CORRODED (INNER CHORD). REMOVED CORRODED SILL, REPLACED SILL WITH NEW PART IAW SRM 51-40-02.
- [SDR ASAA0741635](https://openairdocs.org/sdr/ASAA0741635), May 16, 2007: TAB. DELAMINATED. LEFT AILERON TAB IS DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERION TAB IAW AMM 27-11-21 PG 401.
- [SDR ASAA0741634](https://openairdocs.org/sdr/ASAA0741634), May 14, 2007: WEB. CRACKED. FLOOR WEB BELOW L2 DOOR CRACKED (UNDER MOPSILL). REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-40-2.
- [SDR ASAA0741633](https://openairdocs.org/sdr/ASAA0741633), May 14, 2007: FLOORBEAM. CORRODED. FLOORBEAM CORRODED UPPER CHORD. REMOVED CORRODED SECTION OF UPPER CHORD FABRICATED AND INSTALLED REPLACEMENT CHORD ANGLES AND SHIMS IAW SRM 53-10-51.
- [SDR ASAA0741630](https://openairdocs.org/sdr/ASAA0741630), May 7, 2007: WEB. PUNCTURED. AFT CABIN FLOOR WEB PUNCTURED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-70-13 FIG 1.
- [SDR ASAA0741443](https://openairdocs.org/sdr/ASAA0741443), Feb 6, 2007: CABLE. MISROUTED. EVAC SLIDE NEW FROM STOCK INFLATION CABLE MISROUTED AT GIRT FROM MANUFACTURES OVERAHUL. REROUTED INFLATION CABLE PRIOR TO INSTALLATION.

All 107: https://openairdocs.org/deregistered/N784AS-2010-02-01/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20050730017239I](https://openairdocs.org/incident/20050730017239I), Jul 30, 2005: Boeing 7374Q8 (N784AS), Fairbanks, AK, Substantial damage. (-23) Aircraft was struck by lightning on the left side of radome. The lightning force exited the aircraft via static wicks on the left side of horizontal…

## Other aircraft with N784AS

- [Registered now](https://openairdocs.org/aircraft/N784AS): Piper PA-28R-200, S/N 28R-7235160, built 1972

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