# N772AS: 1993 Boeing 737-4Q8, registration cancelled 2014-12-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 18, 2014
- Exported to: Austria
- Status when cancelled: Valid registration
- 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: 25105
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 27, 1993
- Certificate issued: July 29, 2014
- Last registry action: July 29, 2014
- Mode S code: AA7086
- Owner when cancelled: [V54x-737 LLC](https://openairdocs.org/faa-owner/V54X-737%20LLC)
- Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)
- Owner type: Corporation
- Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N772AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=772AS
- Page: https://openairdocs.org/deregistered/N772AS-2014-12-18

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 (239, newest 50)

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

- [SDR BJNA201304070001](https://openairdocs.org/sdr/BJNA201304070001), Apr 6, 2013: LAMP. INOPERATIVE. FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE.
- [SDR BJNA2013002050001](https://openairdocs.org/sdr/BJNA2013002050001), Jan 29, 2013: SKIN. DAMAGED. DURING A SCHEDULED A-18 CHECK, MECHANICS FOUND THE LT INBD FORE FLAP CONTAINING A LARGE HOLE WITH MISSING CORE HONEYCOMB STRUCTURE. THE DAMAGE DID NOT PROTRUDE 
- [SDR BJNA201211150001](https://openairdocs.org/sdr/BJNA201211150001), Nov 15, 2012: BATTERY. UNSERVICEABLE. FWD CABIN F/A FLASHLIGHT CHARGE INDICATOR INOPERATIVE. R & R SERVICEABLE BATTERY IAW AMM 25-64-06. OPS CHECK GOOD. SECURED WITH SAFETY BREAK AWAY STRAP.
- [SDR ASAA0945366](https://openairdocs.org/sdr/ASAA0945366), Apr 24, 2009: SWITCH. FAILED. REPORTED EMERGENCY LIGHTS WILL NOT SHUTOFF WITH SWITCH IN OFF POSITION FROM "ARM" IN FLT DECK. SUSPECT BAD OVERHEAD SWITCH. COULD DUPLICATE. REMOVED AND REPLACE
- [SDR ASAA0944833](https://openairdocs.org/sdr/ASAA0944833), Mar 16, 2009: SKIN. PUNCTURED. NR 4 SPOILER BLADE SEAL FASTENER PENETRATED THE INSERT AND PUNCTURED THE UPPER SURFACE AND PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABBED FILLED AND DOUBLER A
- [SDR ASAA0944832](https://openairdocs.org/sdr/ASAA0944832), Mar 16, 2009: SKIN. DELAMINATED. RT OUTBOARD FLAP UPPER AND LOWER SURFACES WERE DELAMINATED. REMOVED AND REPLACED RT AFT FLAP IAW AMM 27 51 39.
- [SDR ASAA0944782](https://openairdocs.org/sdr/ASAA0944782), Mar 13, 2009: WEDGE. CHAFED. RT WING I/B FLAP TRAILING EDGE WEDGE HAS TWO CHAFED AREAS IN PREVIOUS REPAIRS. REMOVED DAMAGED DOUBLERS, PREPPED AREAS, FABRICATED FILLER AND DOUBLER, BONDED RE
- [SDR ASAA0944739](https://openairdocs.org/sdr/ASAA0944739), Mar 3, 2009: SKIN. DELAMINATED. FOUND DELAMINATION UNDER I/B ARROW ON UPPER SURFACE NR 4 GROUND SPOILER. REMOVED PREVIOUS REPAIR AND DAMAGED AREA FABRICATED FILLER AND DOUBLER AND INSTALLED RE
- [SDR ASAA0944662](https://openairdocs.org/sdr/ASAA0944662), Mar 2, 2009: INTERCOSTAL. CRACKED. LEFT O/B MID FLAP INTERCOSTAL CRACKED AT I/B FORE FLAP TRACK ROLLER. REMOVED CRACKED INTERCOSTAL, LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW B737 400 SRM
- [SDR ASAA0944660](https://openairdocs.org/sdr/ASAA0944660), Mar 2, 2009: SKIN. DENTED. LEFT INBOARD MID FLAP BULLNOSE DENTED 24 INCHES FROM I/B END. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 57 53 01 FIG 201
- [SDR ASAA0944658](https://openairdocs.org/sdr/ASAA0944658), Feb 27, 2009: FRAME. DENTED. FRAME DENTED STA 727G BETWEEN 26R 25R. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR CHANNEL IAW B737 400 SRM 51 70 11 FIG 1.
- [SDR ASAA0944659](https://openairdocs.org/sdr/ASAA0944659), Feb 26, 2009: SKIN. DAMAGED. RT OUTBOARD AFT FLAP O/B LOWER END DAMAGED. REMOVED DAMAGED SECTION, FABRICATED AND BONDED FILLER AND DOUBLER IAW B737 400 SRM 51 70 10.
- [SDR ASAA0944632](https://openairdocs.org/sdr/ASAA0944632), Feb 26, 2009: SKIN. DENTED. RIGHT I/B AFT FLAP HAS TWO DENTS ON LOWER T/E. REMOVED DAMAGED AREA, FABRICATED AND BONDED REPAIR MATERIAL IAW B737 400 SRM 51 70 10.
- [SDR ASAA0944783](https://openairdocs.org/sdr/ASAA0944783), Feb 24, 2009: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REMOVED DAMAGE, FABRICATED DOUBLER FILLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 00843.
- [SDR ASAA0944657](https://openairdocs.org/sdr/ASAA0944657), Feb 24, 2009: DOUBLER. CRACKED. R1 DOOR AFT LOWER CORNER INNER DOUBLER CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B737 400 SRM 51 40 02.
- [SDR ASAA0944714](https://openairdocs.org/sdr/ASAA0944714), Feb 23, 2009: SKIN. DENTED. LEFT O/B FOREFLAP JUST OUTBOARD OF I/B END HAS 3 DENTS. REPAIRED, BONDED LT O/B FOREFLAP IAW B737 400 SRM 51 70 10.
- [SDR ASAA0944682](https://openairdocs.org/sdr/ASAA0944682), Feb 23, 2009: SKIN. DENTED. LEFT I/B FORE FLAP HAS 2 DENTS AT I/B END LOWER SIDE. PREPPED DAMAGE AREA, FABRICATED REPAIR DOUBLER AND BONDED DOUBLER IAW B737 400 SRM 51 70 10.
- [SDR ASAA0944663](https://openairdocs.org/sdr/ASAA0944663), Feb 23, 2009: DOUBLER. CHAFED. LEFT O/B MID FLAP CHAFED ABOVE I/B AFT FLAP TRACK. REMOVED CHAFED DOUBLER, FABRICATED AND BONDED REPAIR DOUBLER IAW B737 400 SRM 57 53 01.
- [SDR ASAA0944661](https://openairdocs.org/sdr/ASAA0944661), Feb 22, 2009: SLAT. DELAMINATED. RIGHT NR 5 SLAT OUTBOARD T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED AND BONDED REPAIR IAW B737 400 SRM 51 70 10.
- [SDR ASAA0741530](https://openairdocs.org/sdr/ASAA0741530), Mar 12, 2007: ACM. LEAKING. RIGHT PACK TRIP AND CABIN FILLED WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21 00 01. FOUND RT ACM LEAKING BETWEEN TURBINE AND COMPRESSOR SECTIONS. REMOVED AN
- [SDR ASAA0741512](https://openairdocs.org/sdr/ASAA0741512), Mar 9, 2007: ACM. LEAKING. RIGHT PACK TRIP AND FILLED CABIN WITH SMOKE. SMOKE REMOVED FROM CABIN PER AMM 21-00-01. FOUND RIGHT ACM LEAKING BETWEEN TURBINE AND COMPRESSOR SECTIONS. REMOVED
- [SDR ASAA0641192](https://openairdocs.org/sdr/ASAA0641192), Nov 10, 2006: TAB. DAMAGED. RIGHT ELEVATOR TAB HAS COMPOSITE LAYERS DAMAGED AT T/E. PREPPED AREA FOR BONDING, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-17 AND ASA EA 2730 01107.
- [SDR ASAA0641191](https://openairdocs.org/sdr/ASAA0641191), Nov 8, 2006: WEDGE. CHAFED. RIGHT I/B MID FLAP T/E WEDGE IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51-70-10.
- [SDR ASAA0641189](https://openairdocs.org/sdr/ASAA0641189), Nov 8, 2006: SKIN. CHAFED. TRIMMED OUT SKIN DAMAGE AND REPAIR FUSELAGE SKIN. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER ON FUSELAGE SKIN IAW ASA EA 5330 02152.
- [SDR ASAA0641188](https://openairdocs.org/sdr/ASAA0641188), Nov 8, 2006: SKIN. CHAFED. NR 3 SLAT CHAFED AT OB END LWR SURFACE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.
- [SDR ASAA0641187](https://openairdocs.org/sdr/ASAA0641187), Nov 8, 2006: SKIN. DAMAGED. LT IB FORE FLAP HAS NUMEROUS DINGS BELOW CENTERLINE TRACK. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.
- [SDR ASAA0641186](https://openairdocs.org/sdr/ASAA0641186), Nov 8, 2006: SKIN. NICKED. LT OB AFT FLAP TE IS NICKED AND SEPARATING JUST OB OF IB TRACK FAIRING. REMOVED DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 10.
- [SDR ASAA0641185](https://openairdocs.org/sdr/ASAA0641185), Nov 8, 2006: SKIN. CHAFED. NR 3 SLAT IS CHAFED AT LOWER AFT AREA NEAR ACTUATOR. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.
- [SDR ASAA0641184](https://openairdocs.org/sdr/ASAA0641184), Nov 8, 2006: SKIN. CHAFED. LT OB MID FLAP PREVIOUS REPAIR AT NR 2 FLAP TRACK IS CHAFED. REMOVED DAMAGED DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER IAR SRM 51 70 10.
- [SDR ASAA0641183](https://openairdocs.org/sdr/ASAA0641183), Nov 8, 2006: SKIN. DENTED. RT IB FORE FLAP LWR SKIN DENTED. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.
- [SDR ASAA0641182](https://openairdocs.org/sdr/ASAA0641182), Nov 8, 2006: SKIN. DENTED. RT IB TE FLAP LWR SKIN HAS MULTIPLE DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.
- [SDR ASAA0641180](https://openairdocs.org/sdr/ASAA0641180), Nov 8, 2006: SKIN. DENTED. 5 SPOILER LOWER SKIN DENTED. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.
- [SDR ASAA0641179](https://openairdocs.org/sdr/ASAA0641179), Nov 8, 2006: SKIN. DENTED. NR 5 SPOILER UPPER SKIN HAS CLUSTERS OF DENTS. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.
- [SDR ASAA0640411](https://openairdocs.org/sdr/ASAA0640411), Apr 10, 2006: SKIN. GROUND DAMAGE. FOUND L1 UPPER FWD HINGE CUTOUT HAS TORN SKIN FROM JETWAY DAMAGE. INSTALLED REPAIR DOUBLER PER SRM 52 00 01 REPAIR 2.
- [SDR ASAA0540546](https://openairdocs.org/sdr/ASAA0540546), Oct 12, 2005: SHAFT. DAMAGED. SEA - R-1 DOOR HANDLE WILL NOT STAY IS STOWED POSTION. DOOR HANDLE SHAFT AND SLEEVE ASSY WAS REPLACED AND DOOR RIGGED PER AMM. (M)
- [SDR ASAA0540516](https://openairdocs.org/sdr/ASAA0540516), Sep 29, 2005: COMPRESSOR. CONTAMINATED. OKC - FOUND TAKEOFF ROLL POWER SET, COCKPIT FILLED WITH SMOKE. TAKEOFF ABORTED LESS THAN 45 KTS. REMOVED SMOKE FUMES FROM CABIN PER B737-400 AMM 21-00-01 AND AM
- [SDR ASAA0540510](https://openairdocs.org/sdr/ASAA0540510), Sep 26, 2005: SKIN. BENT. OKC - FOUND LEFT OUTBOARD FORE FLAP DENTED, LOWER T/E 21 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51
- [SDR ASAA0540509](https://openairdocs.org/sdr/ASAA0540509), Sep 26, 2005: STRUCTURE. BENT. OKC - FOUND RIGHT INBOARD AFT FLAP OUTBOARD EDGE BENT, LOWER SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)
- [SDR ASAA0540508](https://openairdocs.org/sdr/ASAA0540508), Sep 26, 2005: SKIN. BENT. OKC - FOUND RIGHT INBOARD AFT FLAP T/E BENT. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-90-10. (M)
- [SDR ASAA0540507](https://openairdocs.org/sdr/ASAA0540507), Sep 26, 2005: SKIN. PUNCTURED. OKC - FOUND RIGHT OUTBOARD AFT FLAP HAS PUNCTURE APPROX 44 INCH FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51
- [SDR ASA0540506](https://openairdocs.org/sdr/ASA0540506), Sep 26, 2005: SKIN. DENTED. OKC - FOUND FUSELAGE SKIN DENTED AT BS 1006.5 BETWEEN STRINGER 13-14 RT. REMOVED SKIN, REPLACED WITH NEW SKIN IAW ASA EA 5330-01999 AND 737-400 SRM 51-40-2. (M)
- [SDR ASAA0540505](https://openairdocs.org/sdr/ASAA0540505), Sep 26, 2005: SKIN. DENTED. OKC - FOUND FUSELAGE SKIN DENTED AT BS 1000 .5 INCH BELOW STRINGER 14R. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED LAP REPAIR IAW 737-400 SRM 53
- [SDR ASAA0540504](https://openairdocs.org/sdr/ASAA0540504), Sep 26, 2005: STRAP. GOUGED. OKC - FOUND FUSELAGE SKIN STRAP AT BS 1150 STRINGER 20R GOUGED. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW ASA EA 53
- [SDR ASAA0540512](https://openairdocs.org/sdr/ASAA0540512), Sep 26, 2005: FLOORBEAM. PUNCTURED. OKC - FOUND FLOORBEAM BS 947 CORRODED AROUND FASTENER HOLES AT LBL 45, RBL 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EO 5310-02500. (M)
- [SDR ASAA0540511](https://openairdocs.org/sdr/ASAA0540511), Sep 26, 2005: SKIN. PUNCTURED. OKC - FOUND LEFT OUTBOARD AFT FLAP PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M)
- [SDR ASAA0540514](https://openairdocs.org/sdr/ASAA0540514), Sep 26, 2005: FLOORBEAM. CORRODED. OKC - FOUND FLOORBEAM STATION 986.5 CORRODED ON UPPER CHORD. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02498. (M)
- [SDR ASAA0540513](https://openairdocs.org/sdr/ASAA0540513), Sep 26, 2005: FLOOR SUPPORT. CORRODED. OKC - FOUND FLOOR SUPPORT IN FLIGHT DECK ENTRY WAY IS CORRODED AT STATION 270. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02501. (M)
- [SDR ASAA0540502](https://openairdocs.org/sdr/ASAA0540502), Sep 22, 2005: FLOORBEAM. DAMAGED. OKC - FOUND BS 312 FLOORBEAM UPPER CHORD DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED UPPER CHORD REPAIR PIECES IAW B737-400 SRM 53-10-51 FIG 201. (M)
- [SDR ASAA0540501](https://openairdocs.org/sdr/ASAA0540501), Sep 22, 2005: SPLICE. CORRODED. OKC - FOUND BS 344 UPPER CHORD SPLICE REPAIR CORRODED. REMOVED CORRODED CHORD REPAIR, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02494. (M)
- [SDR ASAA0540500](https://openairdocs.org/sdr/ASAA0540500), Sep 22, 2005: STIFFENER. CORRODED. OKC - FOUND VERTICAL STIFFENER EXFOLIATED RIGHT SIDE OF TORQUE BOX AT BS 1127. REMOVED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 737-400 SRM

All 239: https://openairdocs.org/deregistered/N772AS-2014-12-18/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA00IA019](https://openairdocs.org/ntsb/SEA00IA019), Nov 11, 1999: Boeing 737-400 (N772AS), Portland, OR, incident, minor damage. Probable cause: Arcing in the electrical system wiring for undetermined reasons.

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