# N705AA: 1981 Boeing 727-200, registration cancelled 2021-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2021
- Exported to: Kenya
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-200](https://openairdocs.org/model/boeing-727-200) (registry code 138407E)
- Engine: [Pratt & Whitney JT8D-217](https://openairdocs.org/engine/pratt-whitney-jt8d-217) (registry code 51691)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (OpenAirDocs)
- Serial number: 22462
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 12, 2008
- Certificate issued: February 23, 2004
- Last registry action: August 15, 2019
- Mode S code: A96722
- Owner when cancelled: [Aero Micronesia Inc](https://openairdocs.org/faa-owner/AERO%20MICRONESIA%20INC)
- Location: Barrigada, GU, Guam
- Physical address: [Tamuning, GU](https://openairdocs.org/faa-place/GU/Tamuning)
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N705AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=705AA
- Page: https://openairdocs.org/deregistered/N705AA-2021-02-03

From the FAA registry file of October 31, 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 727-200: https://openairdocs.org/model/boeing-727-200.md

## Service difficulty reports (52, newest 50)

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

- [SDR I5PA20200106104](https://openairdocs.org/sdr/I5PA20200106104), Dec 21, 2019: ENGINE. DAMAGED. AFTER DEPARTURE OUT OF ROR, ON CLIMB OUT CREW EXPERIENCED A LOUD BANG FROM ENGINE #3, CREW KEPT ENGINE AT IDLE AND RETURNED AND LANDED SAFELY IN ROR. MAINTENANC
- [SDR I5PA2019030800000](https://openairdocs.org/sdr/I5PA2019030800000), Mar 8, 2019: SMOKE DETECTOR. ACTIVATED. MAIN CARGO SMOKE DETECTOR GOES ON IN FLIGHT.
- [SDR I5PA2018110470501](https://openairdocs.org/sdr/I5PA2018110470501), Nov 4, 2018: SMOKE DETECTOR. UNSERVICEABLE. MAIN CARGO FIRE LIGHT AND BELL CAME ON IN FLIGHT. REPLACED FAULTY SMOKE DETECTOR UNIT.
- [SDR I5PA2017121170501](https://openairdocs.org/sdr/I5PA2017121170501), Dec 10, 2017: INDICATOR. INOPERATIVE. DISCREPANCY: F/O AIRSPEED INDICATOR INOP. CORRECTIVE ACTION: FOUND FOREIGN OBJECT IN AUXILIARY AND F/O PITOT PROBE. FLUSHED PER AMM 34-11-00. OPS CHECK GOOD
- [SDR FY4Y20141006003](https://openairdocs.org/sdr/FY4Y20141006003), Oct 1, 2014: SKIN. CORRODED. DURING CPCP INSPECTION THE INSPECTOR PERFORMED VISUAL INSPECTION & FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN OF BS 950B STRINGER 28L. THE CORROSION THROUGH THE S
- [SDR FY4Y20141006002](https://openairdocs.org/sdr/FY4Y20141006002), Oct 1, 2014: SKIN. CORRODED. DURING INSPECTION THE INSPECTOR PERFORMED VISUAL INSPECTION & FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN OF BS 950D STRINGER 26L. THE CORROSION THROUGH THE SKIN W
- [SDR FY4Y20141006001](https://openairdocs.org/sdr/FY4Y20141006001), Oct 1, 2014: SKIN. CORRODED. DURING CPCP INSPECTION THE INSPECTOR FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN BETWEEN BS 720E & 720F STRINGER 26L. THE CORROSION THROUGH THE SKIN WAS OVER LIMIT
- [SDR FY4Y20141003007](https://openairdocs.org/sdr/FY4Y20141003007), Sep 30, 2014: SKIN. CORRODED. DURING INSPECTION THE INSPECTOR PERFORMED VISUAL INSPECTION & FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN OF BS 950E+4 STRINGER 28L. THE CORROSION THROUGH THE SKIN
- [SDR FY4Y20141003006](https://openairdocs.org/sdr/FY4Y20141003006), Sep 30, 2014: SKIN. CORRODED. DURING CPCP INSPECTION THE INSPECTOR FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN BETWEEN BS 720B & 720C STRINGER 28L & 28R. THE CORROSION THROUGH THE SKIN WAS OVER
- [SDR FY4Y20141003005](https://openairdocs.org/sdr/FY4Y20141003005), Sep 30, 2014: SKIN. CORRODED. DURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING UPPER SKIN FROM WS 611.5 TO WS 613.5. DIMENSIONS OF CORROSION AREA 3 INCHES X 1.25 INCHES. AFTER THE
- [SDR FY4Y20141003004](https://openairdocs.org/sdr/FY4Y20141003004), Sep 30, 2014: PLATE. CORRODED. DURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 520 TO WS 526. DIMENSIONS OF CORROSION AREA 6 INCHES X 1.5 INCH
- [SDR FY4Y20141003003](https://openairdocs.org/sdr/FY4Y20141003003), Sep 30, 2014: PLATE. CORRODED. DURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 701 TO WS 696. DIMENSIONS OF CORROSION AREA 5 INCHES X 1.5 INCH
- [SDR FY4Y20141003002](https://openairdocs.org/sdr/FY4Y20141003002), Sep 30, 2014: PLATE. CORRODED. DURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 726 TO WS 734. DIMENSIONS OF CORROSION AREA 8 INCHES X 2 INCHES
- [SDR FY4Y20141003001](https://openairdocs.org/sdr/FY4Y20141003001), Sep 30, 2014: PLATE. CORRODED. DURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 738.5 TO WS 742. DIMENSIONS OF CORROSION AREA IS 3.5 INCHES X 1
- [SDR I5PA201406010002](https://openairdocs.org/sdr/I5PA201406010002), Jun 25, 2014: ENGINE. LEAKING. NUMBER 3 ENG SHUT DOWN IN FLIGHT DUE TO POSSIBLE COMPRESSOR STALL, FOLLOWED BY OIL LOSS. THE INLET & EXHAUST LOOKED OK, BUT EVIDENCE OF OIL LOSS FROM THE EXHAUS
- [SDR I5PA201406010001](https://openairdocs.org/sdr/I5PA201406010001), Jun 25, 2014: ENGINE. LEAKING. NR 3 ENGINE SHUTDOWN IN FLIGHT DUE TO POSSIBLE COMPRESSOR STALL FOLLOWED BY OIL LOSS. THE INLET & EXHAUST LOOKED OK, BUT EVIDENCE OF OIL LOSS FROM THE EXHAUST. 
- [SDR FY4Y20121122197](https://openairdocs.org/sdr/FY4Y20121122197), Nov 19, 2012: WEB. CORRODED. DURING PERFORMED 7C CHECK, CORROSION WAS FOUND ON CENTER FUEL TANK AFT VERTICAL WEB AT STATION BS 865, LBL 38, 39,WL 165-168 (DIMENSIONS OF CORROSION AREA:2 .37
- [SDR FY4Y20121116197](https://openairdocs.org/sdr/FY4Y20121116197), Nov 13, 2012: SKIN. CORRODED. DURING PERFORMED 7C CHECK, CORROSION WAS FOUND ON FUSELAGE LOWER LOBE SKIN PANEL AT STATION BS 1010, WL 148 BETWEEN S-28R AND S-29R. (DIMENSIONS OF CORROSION AR
- [SDR FY4Y201211130001](https://openairdocs.org/sdr/FY4Y201211130001), Nov 13, 2012: STRUCTURE. CORRODED. DURING PERFORMED 7C CHECK, CORROSION WAS FOUND ON CENTER FUEL TANK AFT LOWER EDGE AT STATION BS 865, LBL 54, WL 169 TO LBL 58 WL 171 ( DIMENSIONS OF CORROSION A
- [SDR FY4Y2012F00244](https://openairdocs.org/sdr/FY4Y2012F00244), Nov 13, 2012: STRUCTURE. CORRODED. PERFORMED 7C CHECK, CORROSION WAS FOUND ON CENTER FUEL TANK AFT LOWER EDGE AT BS 865, LBL 54, WL 169 TO LBL 58, WL 171 (DIMENSIONS OF CORROSION AREA: 3.7500" × 
- [SDR FY4Y20110317](https://openairdocs.org/sdr/FY4Y20110317), Mar 16, 2011: STRAP. CORRODED. HE CORROSION WAS FOUND AT TENSION STRAP OF LT OTBD MID FLAP AT WBL 452 DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE STRAP IS 0.225". AFTER BLEND OUT, THE DIME
- [SDR FY4Y20110315](https://openairdocs.org/sdr/FY4Y20110315), Mar 14, 2011: SPLICE. CORRODED. THE EXFOLIATION CORROSION IS FOUND AT LT I/B MID FLAP CHORD SPLICE AT WBL 193 DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD SPLICE IS 0.072”. AFTER BLENT
- [SDR FY4Y197M20110315E](https://openairdocs.org/sdr/FY4Y197M20110315E), Mar 11, 2011: SEAT TRACK. CORRODED. DURING PERFORMED CPCP CARD NR C53-224-01 PART 1 OF 3 FOR MAIN DECK CARGO COM'P FLOOR STRUCTURE, THE SEAT TRACK AT STA BS 640+3 AND BS 640+10 LBL. 0 WAS FOUND LE
- [SDR FY4Y201103151](https://openairdocs.org/sdr/FY4Y201103151), Mar 11, 2011: SPAR. CORRODED. THE EXFOLIATION CORROSION IS FOUND AT LT INBD MID FLAP AFT SPAR LOWER CHORD AT WBL 82, DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD IS 0.125". AFTER BLE
- [SDR FY4Y197M20110315D](https://openairdocs.org/sdr/FY4Y197M20110315D), Mar 11, 2011: BEAM. CORRODED. RT HORIZONTAL STAB TRAILING LOWER BEAM SURFACE STA 220 TO 222 HAD EXFOLIATION CORROSION. ORIGINAL THICKNESS IS 0.105". AFTER CORROSION REMOVED, THE REMAINED THI
- [SDR FY4Y197M20110315C](https://openairdocs.org/sdr/FY4Y197M20110315C), Mar 11, 2011: BEAM. CORRODED. LT HORIZONTAL STAB TRAILING LOWER BEAM UPPER SURFACE STA 66 TO 70 HAD EXFOLIATION CORROSION. ORIGINAL THICKNESS WAS 0.091". AFTER CORROSION REMOVED, THE REMAINE
- [SDR FY4Y197M20110315B](https://openairdocs.org/sdr/FY4Y197M20110315B), Mar 11, 2011: BEAM. CORRODED. LT HORIZONTAL STAB TRAILING LOWER BEAM LOWER SURFACE STA96 TO 97 HAD EXFOLIATION CORROSION. ORIGINAL THICKNESS IS 0.120". AFTER CORROSION REMOVED, THE REMAINED 
- [SDR FY4Y197M20110315A](https://openairdocs.org/sdr/FY4Y197M20110315A), Mar 11, 2011: SPAR. CORRODED. HEAVY CORROSION ON RT WING INBD MIDFLAP REAR SPAR LOWER CHORD AT WBL142, ORIGINAL THICKNESS 0.121". AFTER CORROSION REMOVED, THE REMAINED THICKNESS WAS 0.051", 
- [SDR FY4Y197M20110315](https://openairdocs.org/sdr/FY4Y197M20110315), Mar 11, 2011: SKIN. CORRODED. HEAVY CORROSION ON RT WING INBD MIDFLAP UPPER EXTERNAL SURFACE, AT WBL128, FWD OF FLAP T/E ABOUT 22.5". ORIGINAL THICKNESS IS 0.054" AFTER CORROSION REMOVE, REM
- [SDR FY4Y197M20110310](https://openairdocs.org/sdr/FY4Y197M20110310), Mar 7, 2011: SKIN PANEL. CORRODED. DURING PERFORMED 6C-CHECK FOUND FUSELAGE EXTERIOR SKIN CORRODED (LEVEL 2) AT BS 1066 BETWEEN S-27L AND S-28L, IAW SRM 53-30-1, PAGE 2A PENETRATED DEPTH OUT OF L
- [SDR I5PA20090805](https://openairdocs.org/sdr/I5PA20090805), Aug 6, 2009: STRUCTURE. CORRODED. DURING 5C CHECK AND INSP, CORROSION WAS FOUND BETWEEN BS 950C AND 950E AND STR 28L AND 28R. REPAIRED IAW EI-727-090705.
- [SDR I5PA20090804](https://openairdocs.org/sdr/I5PA20090804), Aug 6, 2009: SKIN. DAMAGED. DURING 5C CHECK AND INSP, CORROSION WAS FOUND ON THE SKIN INTERNAL SURFACE WHICH WAS UNDER THE PREVIOUS SKIN REPAIR DOUBLER FROM BS 1009 TO BS 1045 AND BETWEEN 
- [SDR I5PA20090803](https://openairdocs.org/sdr/I5PA20090803), Aug 6, 2009: KEELBEAM. CORRODED. DURING 5C CHECK AND INSP, CORROSION WAS FOUND ON RT KEEL BEAM INBD FLANGE AFT OF BS740. AFTER BLENDOUT AND MEASURED ORIGINAL THICKNESS BLEND OUT EXCEED LIMITS. 
- [SDR I5PA20090802](https://openairdocs.org/sdr/I5PA20090802), Aug 6, 2009: SPAR. CORRODED. DURING 5C CHECK AND INSPECTION, CORROSION WAS FOUND ON LT WING REAR SPAR LWR SKIN AT WS706 DIMENSION AREA 1.3 INCH X 1.7 INCH. AFTER CORROSION BLENDOUT FOUND MA
- [SDR I5PA20090801](https://openairdocs.org/sdr/I5PA20090801), Aug 6, 2009: SPAR. CORRODED. DURING 5C-CHECK AND INPS CORROSION WAS FOUND ON RT AND LT WING FRONT SPAR CHORD PLATE LWR SURFACE. AFTER BLEND OUT THE MAX LOSS OF MATERIAL THICKNESS WAS BEYOND
- [SDR 2008FA0000746](https://openairdocs.org/sdr/2008FA0000746), Oct 15, 2008: PUMP. MALFUNCTIONED. CRUISE NR 1 ENG STARTED TO SPOOL DOWN OTHER PARAMETERS ARE NORMAL, PERFORMED IN-FLIGHT START CHECKLIST SEVERAL TIMES INCLUDING RESETTING SWITCHES, NO LIGHT OFF.
- [SDR 2007FA0000946](https://openairdocs.org/sdr/2007FA0000946), Oct 16, 2007: STRINGER. CRACKED. THE AIRCRAFT INPUT FOR 4C CHECK AND CPCP ON SEPT 3, 2007. DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND 5 INCH CRACK BOTH ON LT AND RT FUSELA
- [SDR 20010411CW003](https://openairdocs.org/sdr/20010411CW003), Mar 19, 2001: TRUNNION. DAMAGED. SEVERE DAMAGE TO THE AFT TRUNNION SPUD AREA.
- [SDR AALA991403](https://openairdocs.org/sdr/AALA991403), Sep 18, 1999: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M
- [SDR AALA990684](https://openairdocs.org/sdr/AALA990684), May 7, 1999: SKIN. CORRODED. TUL - FOUND CORROSION ON LOWER CENTER TANK OUTER SKIN STATION 833 RBL 20-24. REMOVED CORROSION AND REPAIRED AREA PER ESO 11697, DATED 5-7-99 PAGES 1/2. (M)
- [SDR AALA981090](https://openairdocs.org/sdr/AALA981090), May 31, 1998: LIGHT. INOPERATIVE. TPA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL O
- [SDR AALA980864](https://openairdocs.org/sdr/AALA980864), Apr 30, 1998: FLOORBEAM. CORRODED. TUL - RT AFT LAV FLOOR OUTBOARD OF FORWARD OUTBOARD TANK CABLE ATTACH LUG IS CORRODED, FORWARD OF INBOARD TANK CABLE ATTACH IS CORRODED. REMOVED CORRODED HAT CH
- [SDR AALA960894](https://openairdocs.org/sdr/AALA960894), Jun 8, 1996: SKIN. CRACKED. TUL - FOUND CRACK IN FUSELAGE SKIN ON CROWN AT STATION 1096, RIGHT SIDE OF STRINGER NR 1 AT FASTENER FOR NR 2 ENG INLET FORWARD ATTACH. INSTALLED DOUBLER PER SB
- [SDR AALA960893](https://openairdocs.org/sdr/AALA960893), Jun 8, 1996: STRINGER. CRACKED. TUL - FOUND STRINGER END CRACKED STRINGER 15R AT THE LIGHT BOX FORWARD SIDE STATION 720B PLUS 4. REMOVED CRACK STRINGER AND SPLICED NEW STRINGER AS PER SRM 53-1
- [SDR AALA960892](https://openairdocs.org/sdr/AALA960892), Jun 8, 1996: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE NEAR DOME NUTS, STATION 700 STRINGER 28L TO 28R. REMOVED SHEAR TIE AND INSTALLED NEW ONE PER SRM 57-10-3 PG 4. (M)
- [SDR AALA960891](https://openairdocs.org/sdr/AALA960891), Jun 8, 1996: STRINGER. CORRODED. FOUND CORROSION IN STRINGER 27R AT STATION 701. REMOVED OUT OF LIMITS STRINGER AND REPAIRED PER SRM 53-10-3. (M)
- [SDR AALA960890](https://openairdocs.org/sdr/AALA960890), Jun 8, 1996: SKIN. CORRODED. TUL - FOUND CORROSION ON BELLY SKIN AND CIRCUMFERENTIAL STRAP, STATION 680 TO 684, INBOARD OF STRINGER 27R. INSTALLED DOUBLER AND FILLER ALODINED, PRIMED, PER S
- [SDR AALA960889](https://openairdocs.org/sdr/AALA960889), Jun 8, 1996: SKIN. CORRODED. TUL - FOUND STRINGER 28 LEFT HAS CORROSION AND SKIN CORRODED STATION 580 TO 595. REMOVED AND REPLACED SECTION OF STRINGER AND SKIN AT STRINGER 28 LEFT STATION 5
- [SDR AALA960888](https://openairdocs.org/sdr/AALA960888), Jun 8, 1996: STRINGER. CORRODED. TUL - FOUND STRINGER 27 LEFT HAS CORROSION STATION 514 TO STATION 525. CUT OUT CORROSION AND REPLACED STRINGER 27L FROM STATION 513 TO STATION 525, PER SRM 53-1
- [SDR AALA960887](https://openairdocs.org/sdr/AALA960887), Jun 8, 1996: ENG INLET. CORRODED. TUL - NR 2 ENGINE INLET CORRODED AT 11:00 POSITION. REMOVED CORRODED AREA AND MADE FLUSH REPAIR PER SRM 54-30-3 PAGE 2A AND 2B. (M)

All 52: https://openairdocs.org/deregistered/N705AA-2021-02-03/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 MIA88LA075](https://openairdocs.org/ntsb/MIA88LA075), Dec 26, 1987: Boeing 727-200 (N705AA), San Juan, PR, substantial damage

## FAA accident and incident reports (6)

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 20120229024959I](https://openairdocs.org/incident/20120229024959I), Feb 29, 2012: Boeing 727-200 (N705AA), GU, No damage. No information regarding this incident and closing this item this date. 10-24-2012.
- [Incident 19891030063529I](https://openairdocs.org/incident/19891030063529I), Oct 30, 1989: Boeing 727200 (N705AA), Atlantic Ocean, FL. Experienced turbulence for a period of seconds. One crewmenber injured.
- [Incident 19890607038309I](https://openairdocs.org/incident/19890607038309I), Jun 7, 1989: Boeing 727200 (N705AA), Dallas-Ft Worth, TX, Minor damage. While taxiing, right wing tip struck a bus parked on right side of taxiway. Minor damage.
- [Accident 19871226074841A](https://openairdocs.org/incident/19871226074841A), Dec 26, 1987: Boeing 727200 (N705AA), San Juan, Puerto Rico, Substantial damage. Struck the wing of N893AA while trying to pass on a taxiway to position for takeoff. Both were Boeing 727S.
- [Incident 19840523023969I](https://openairdocs.org/incident/19840523023969I), May 23, 1984: Boeing 727200 (N705AA), Detroit, MI. Right main gear left the taxiway during a turn. Gear stuck in the ground. No damage to aircraft.
- [Incident 19811214086839I](https://openairdocs.org/incident/19811214086839I), Dec 14, 1981: Boeing 727200 (N705AA), Chicago, IL. Lost all electrical power on approach. Landed on standby power only. #1 generator had failed. Replaced gen panel.

## Other aircraft with N705AA

- [Registered now](https://openairdocs.org/aircraft/N705AA): Anduril Industries ROADRUNNER, S/N 3164

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