# N733PA: Amazon.Com Services MK30

- Status: Valid registration
- Airframe: [Amazon.Com Services MK30](https://openairdocs.org/model/amazon-com-services-mk30) (registry code 06102FK)
- Serial number: 178650105S
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: March 30, 2025
- Expires: March 31, 2032
- Mode S code: A9D776
- Registered owner: [Amazon.Com Services LLC](https://openairdocs.org/faa-owner/AMAZON.COM%20SERVICES%20LLC)
- Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)
- Owner type: LLC
- Owner's area on the map: 47.6306° N, 122.3456° W: Placed by OpenAirDocs at the center of ZIP code 98109, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=733PA
- Page: https://openairdocs.org/aircraft/N733PA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Amazon.Com Services MK30)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N733PA.

## FAA accident and incident reports

None matched to N733PA.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N733PA not matched to an aircraft (176, newest 50)

They name N733PA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SROM2012032000019](https://openairdocs.org/sdr/SROM2012032000019), Jun 19, 2012: DUCT CLAMP. WORN. ON CLIMBOUT, RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. REDUCED POWER ON RIGHT ENGINE LIGHT EXTINGUISHED. RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPLAC
- [SDR SROM201203200018](https://openairdocs.org/sdr/SROM201203200018), Mar 16, 2012: SILL. CORRODED. LEVEL 1 CORROSION FOUND ON L1 DOOR INNER SILL. SECOND BLEND ON THIS PART'S HISTORY.
- [SDR SROM201203200017](https://openairdocs.org/sdr/SROM201203200017), Mar 16, 2012: SILL. CORRODED. LEVEL 1 CORROSION FOUND ON FORWARD SERVICE DOOR SILL CHORD. SECOND BLEND IN THIS PART'S HISTORY.
- [SDR SROM2012032000016](https://openairdocs.org/sdr/SROM2012032000016), Mar 16, 2012: BEAR STRAP. CRACKED. DURING INSPECTION, CRACKS WERE FOUND IN THE BEAR STRAP RE-INFORCEMENT OF THE L1 DOOR, BS 304 S10-13L.
- [SDR SROM201203160002](https://openairdocs.org/sdr/SROM201203160002), Mar 16, 2012: STRINGER. CORRODED. LEVEL 1 CORROSION FOUND ON STRINGER.
- [SDR SROM201203200014](https://openairdocs.org/sdr/SROM201203200014), Mar 16, 2012: SPAR. CORRODED. CORROSION FOUND ON LOWER SPAR CHORD.
- [SDR SROM201203200013](https://openairdocs.org/sdr/SROM201203200013), Mar 16, 2012: SHEAR TIE. DAMAGED. DAMAGED SHEAR TIE FRAME.
- [SDR SROM20120320013](https://openairdocs.org/sdr/SROM20120320013), Mar 16, 2012: STRAP. DAMAGED. STRAP DAMAGED.
- [SDR SROM201203200012](https://openairdocs.org/sdr/SROM201203200012), Mar 16, 2012: FRAME. DAMAGED. DAMAGED FRAME AT BS 867 S26R.
- [SDR SROM201203160001](https://openairdocs.org/sdr/SROM201203160001), Mar 16, 2012: FRAME. DAMAGED. DAMAGE /DRILL START ON FRAME.
- [SDR SROM201203200011](https://openairdocs.org/sdr/SROM201203200011), Mar 16, 2012: FRAME. CRACKED. FRAME CRACKED AT AIR CONDITIONING BRACKET.
- [SDR SROM201203200010](https://openairdocs.org/sdr/SROM201203200010), Mar 16, 2012: FRAME. CRACKED. CRACKED FRAME AT AIR CONDITIONING SUPPORT BRACKET.
- [SDR SROM201203200009](https://openairdocs.org/sdr/SROM201203200009), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 360 S5L.
- [SDR SROM201203200008](https://openairdocs.org/sdr/SROM201203200008), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 400 S18R.
- [SDR SROM201203200007](https://openairdocs.org/sdr/SROM201203200007), Mar 16, 2012: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 500A S19R.
- [SDR SROM201203200006](https://openairdocs.org/sdr/SROM201203200006), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 908 S4R.
- [SDR SROM201203200005](https://openairdocs.org/sdr/SROM201203200005), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 767 S22L.
- [SDR SROM201203200004](https://openairdocs.org/sdr/SROM201203200004), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 907 S21R.
- [SDR SROM201203200003](https://openairdocs.org/sdr/SROM201203200003), Mar 16, 2012: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 706 S13R.
- [SDR SROM201203200002](https://openairdocs.org/sdr/SROM201203200002), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP AT BS 663 S9R IS CRACKED.
- [SDR SROM201203200001](https://openairdocs.org/sdr/SROM201203200001), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP AT BS 663 S10L CRACKED.
- [SDR SROM2012001](https://openairdocs.org/sdr/SROM2012001), Jan 9, 2012: CONTACTOR. BURNED. EXPERIENCED SMOKE IN THE COCKPIT AT THE GATE PRIOR TO DEPARTURE. THE FLIGHT CREW QUICKLY POWERED DOWN THE AIRCRAFT; NO PASSENGERS WERE ON BOARD. MAINTENANCE FOU
- [SDR SROM2010009](https://openairdocs.org/sdr/SROM2010009), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT BELOW STRINGER S-25R, STA BS 885.25 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SE
- [SDR SROM2010015](https://openairdocs.org/sdr/SROM2010015), Apr 26, 2010: SHEAR TIE. CRACKED. REPAIRED SHEAR TIE BETWEEN STRINGERS 20L AND S-21L, STA: BS 907 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010,
- [SDR SROM2010014](https://openairdocs.org/sdr/SROM2010014), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT 0.4 INCHES BELOW STRINGER S-20L, STA: BS 896 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED M
- [SDR SROM2010013](https://openairdocs.org/sdr/SROM2010013), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN SCRIBE LINES LEFT WING TO BODY FAIRING AT STRINGERS S-16L TO 3 INCHES BELOW S-17L, STA: BS 500B - 516 IN ACCORDANCE WITH MESSAGE KFC-ATR-
- [SDR SROM2010012](https://openairdocs.org/sdr/SROM2010012), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-20L, STA: BS 974 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTI
- [SDR SROM2010011](https://openairdocs.org/sdr/SROM2010011), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT 1.6 INCHES ABOVE STRINGER S-23L, STA: BS 926.5 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH
- [SDR SROM2010010](https://openairdocs.org/sdr/SROM2010010), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT ABOVE STRINGER S-26R, STA: BS 838.5 IN ACCORDANCE WITH MESSAGE KFC-ATR-10-0001-01C, DATED MARCH 31, 2010, KFC-ATR-10-0001-05B, 
- [SDR SROM2010008](https://openairdocs.org/sdr/SROM2010008), Apr 26, 2010: SKIN. NICKED. REPAIRED FUSELAGE NICK 3 INCHES ABOVE STRINGER S-20R, STA: BS 914 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 201
- [SDR SROM2010007](https://openairdocs.org/sdr/SROM2010007), Apr 26, 2010: INTERCOSTAL. DAMAGED. REPAIRED STRINGER INTERCOSTAL AT STRINGER S-4L, STA: BS 305 BY REPLACEMENT WITH NEW PART 50-8261-62 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (
- [SDR SROM2010006](https://openairdocs.org/sdr/SROM2010006), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT 1.75 INCHES ABOVE STRINGER S-23R, STA: BS 904.8 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARC
- [SDR SROM2010005](https://openairdocs.org/sdr/SROM2010005), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT THREE INCHES BELOW STRINGER S-25R, STA: BS 775 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH
- [SDR SROM2010004](https://openairdocs.org/sdr/SROM2010004), Apr 26, 2010: BEARING. LOOSE. REPLACED NLG UPPER ATTACH BEARING IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3 NO. 091-1236-10-848, DATED APRIL 01, 2010, ASI ENGINEERING REPORT 5310848-ER, 
- [SDR SROM2010003](https://openairdocs.org/sdr/SROM2010003), Apr 26, 2010: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-23L, STA: BS 897 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SECTION
- [SDR SROM2010002](https://openairdocs.org/sdr/SROM2010002), Apr 26, 2010: FAIRING. DELAMINATED. REPAIRED LEFT AND RIGHT GRAVEL EQUIPPED NOSE LANDING GEAR FILLET FAIRINGS AND DOOR FAIRINGS IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, REV IR, DATED JANUA
- [SDR SROM20090017](https://openairdocs.org/sdr/SROM20090017), Nov 3, 2009: ACTUATOR. INOPERATIVE. NLG WOULD NOT RETRACT AFTER TAKE-OFF. SELECTED GEAR DOWN AND RETURNED TO DEPARTURE AIRPORT. FOUND NOSE GEAR GRAVEL DEFLECTOR ACTUATOR FUNCTIONING IMPROPERLY.
- [SDR SROM20080024](https://openairdocs.org/sdr/SROM20080024), Sep 26, 2008: SLIDE. INOPERATIVE. DURING MINI EVACUATION DEMONSTRATION TRAINING SLIDE DEPLOYED BUT DID NOT INFLATE. WAITING ON TEAR DOWN REPORT FOR FINAL DISPOSITION. 11/20/08 FINAL DISPOSITION.
- [SDR SRO2008F00000](https://openairdocs.org/sdr/SRO2008F00000), Sep 26, 2008: SLIDE. INOPERATIVE. DURING MINI EVACUATION DEMONSTRATION TRAINING SLIDE DEPLOYED BUT DID NOT INFLATE. WAITING ON TEAR DOWN REPORT FOR FINAL DISPOSITION.
- [SDR SROM2008021](https://openairdocs.org/sdr/SROM2008021), Apr 6, 2008: TORQUE BOX. CRACKED. CRACKED APU TORQUE BOX WEB AT STA BS 1115 RBL 2. HFEC CARRIED OUT IN ACCORDANCE WITH BOEING 737 NDT MANUAL 51-00-00, FIGURE 23, PART 6 ON A CUT-OUT ON THE APU T
- [SDR SROM2008020](https://openairdocs.org/sdr/SROM2008020), Apr 6, 2008: FLOORBEAM. CRACKED. CORROSION ON FLOOR I-BEAM AT STA BS 344 LBL 18 THRU RBL 39. REPAIRED FLOOR I-BEAM AT STA BS 344 LBL 18 THRU RBL 39 IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPA
- [SDR SROM2008008](https://openairdocs.org/sdr/SROM2008008), Apr 6, 2008: KEELBEAM. CORRODED. LOWER CHORDS OF KEEL BEAM IN MAIN LANDING GEAR HAS CORROSION AT LOWER FLANGE IN SEVERAL AREAS UPPER & LOWER SURFACES FROM STA BS 663-727 RBL 6.5 & LBL 6.5. REPA
- [SDR SROM2008003](https://openairdocs.org/sdr/SROM2008003), Apr 6, 2008: FLOORBEAM. CORRODED. CORROSION ON UPPER CAP OF FLOORBEAM AT STA BS 294.5 BETWEEN LBL 12 AND RBL 50. CORROSION ON UPPER CAP OF FLOORBEAM AT STA BS 294.5 BETWEEN LBL 12 AND RBL 50 BLE
- [SDR SROM2008019](https://openairdocs.org/sdr/SROM2008019), Apr 6, 2008: FLOORBEAM. CRACKED. LOWER LONGITUDINAL FLOORBEAM CHORD CRACKED AT RBL 24.5 STA BS 663. REPLACED LOWER LONGITUDINAL FLOORBEAM CHORD AT RBL 24.5 STA BS 663 IN ACCORDANCE WITH BOEING 
- [SDR SROM2008012](https://openairdocs.org/sdr/SROM2008012), Apr 6, 2008: SKIN. DAMAGED. LIGHTNING STRIKE AT STA BS 933 STR 25.5R. REPAIRED IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 53-30-03, FIGURE 23 (PERMANENT REPAIR), SECTION
- [SDR SROM2008006](https://openairdocs.org/sdr/SROM2008006), Apr 6, 2008: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT STA BS 760 STR 19L, (NDT CONFIRMED CRACK). REPAIRED FUSELAGE SKIN AT STA BS 760 STR 19L IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAI
- [SDR SROM2008007](https://openairdocs.org/sdr/SROM2008007), Apr 6, 2008: BAR. CRACKED. REPAIR CRACKED SPREADER BARS ON PASSENGER SEATS. REPAIRED CRACKED SPREADER BARS ON PASSENGER SEATS IN ACCORDANCE WITH CPAI EO C007-2525-B737-01 AND FAA DER APPR
- [SDR SROM2008002](https://openairdocs.org/sdr/SROM2008002), Apr 6, 2008: FLOORBEAM. CORRODED. CORROSION ON AFT GALLEY FLOORBEAM AT STA BS 980 RBL 4. BLENDED AND FOUND CORROSION ON AFT GALLEY FLOORBEAM AT STA BS 980 RBL 4 TO BE BEYOND LIMITS. REPAIRED AFT
- [SDR SROM2008018](https://openairdocs.org/sdr/SROM2008018), Apr 6, 2008: FLOORBEAM. CRACKED. LOWER LONGITUDINAL FLOORBEAM CHORD CRACKED AT LBL 24.5 STA BS 663. REPLACED LOWER LONGITUDINAL FLOORBEAM CHORD AT LBL 24.5 STA BS 663 IN ACCORDANCE WITH BOEING 
- [SDR SROM2008017](https://openairdocs.org/sdr/SROM2008017), Apr 6, 2008: BRACKET. CRACKED. LEFT HAND ENGINE TAILPIPE CRACKED AT BRACKET MOUNT (3 O'CLOCK POSITION). REPAIRED LEFT HAND ENGINE TAILPIPE BRACKET MOUNT (3 O'CLOCK POSITION) IN ACCORDANCE WIT

All 176: https://openairdocs.org/aircraft/N733PA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N733PA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N733PA before.

- [Cancelled 2024-09-30](https://openairdocs.org/deregistered/N733PA-2024-09-30): Amazon.Com Services MK27-2, S/N 17868SN000789. Owner: [Amazon.Com Services LLC](https://openairdocs.org/faa-owner/AMAZON.COM%20SERVICES%20LLC), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)
- [Cancelled 1992-05-13](https://openairdocs.org/deregistered/N733PA-1992-05-13): Boeing 747-121, S/N 19640. Exported to Nigeria. Owner: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

## Related

- Other Amazon.Com Services MK30 aircraft: https://openairdocs.org/model/amazon-com-services-mk30/aircraft.md

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