FAA REGISTRY
N-Number Inquiry Results
Serial Number | 33010 | Status | Valid |
Manufacturer Name | BOEING | Certificate Issue Date | 02/20/2018 |
Model | 737-7ET | Expiration Date | 02/29/2028 |
Type Aircraft | Fixed Wing Multi-Engine | Type Engine | Turbo-fan |
Pending Number Change | None | Dealer | No |
Date Change Authorized | None | Mode S Code (base 8 / Oct) | 50676546 |
MFR Year | 2001 | Mode S Code (Base 16 / Hex) | A37D66 |
Type Registration | LLC | Fractional Owner | NO |
Name | N324CH LLC | ||
Street | 2200 BISCAYNE BLVD | ||
City | MIAMI | State | FLORIDA |
County | DADE | Zip Code | 33137-5016 |
Country | UNITED STATES |
Type Certificate Data Sheet | None | Type Certificate Holder | None |
Engine Manufacturer | CFM INTL | Classification | Standard |
Engine Model | CFM56-7B27/B3 | Category | Transport |
A/W Date | 01/03/2008 | Exception Code | Yes |
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis
for a determination regarding the airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/ |
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Certificate Number | T181147 | Issue Date | 02/20/2018 | Expiration Date | 03/22/2018 |
Mod Code | 28 | Mod Date | 20020128 |
INSTALLED A PATS INC 7 TANK AUXILIARY FUEL SYSTEM,CONFIGURATION 2-3 (2 FWD, 5 AFT) IN ACCORDANCE WITH PATS INC STC ST00936NY DATED 2/24/99AMENDED 6/8/01, AND PATS INC MASTER DRAWING LIST BBJ0007 REV. L DATED 05-29-01, UP TO AND INCLUDING ADCN L20 DATED 11/29/01. REFER TO FAA FORM 8110-3 (2 EACH) DATED 1/28/02 FOR MINOR DEVIATIONS TO THE MDL. REFER TO FAA FORM8110-3 DATD 1/28/02 FOR MINOR DEVIATIONS NOTED UNDER THE FOLLOWING NON-ROUTINES: 4997-0003, -0005, -0008, -0009, -0018, -0024, -0025, -0032, -0033, -0035, -0036, -0039, -0040, AND -0048. W/O4997 & 4997-OOS. FAA APPROVED FLIGHT MANUAL SUPPLEMENT NUMBER 6, DATED 5/20/99, REVISED 6/7/01 WAS INSERTED INTO THE AIRPLANE FLIGHT MANUAL. PERFORMED FOLLOWING FUNCTIONAL TESTS: T.O 915 DISTURBED SYSTEMS RETEST INSTRUCTIONS REV. B DATED 5/13/99. T.O 753 AUX FUEL GROUND FUNCTIONAL TEST PROCEDURES REV. F DATED 8/23/01. THE AIRCRAFT WAS WEIGHED AFTER MODIFICATION AND REVISED WEIGHT AND BALANCE DATA AND EQUIPMENT LISTS WERE PROVIDED. THE INSTALLATION WAS MADE USING THE RECOMMENDATIONS OF AC 43.13-1B CHAPTER 4, SECTION 4, CHAPTER 7, SECTIONS 1,2,3,4, & 7, AND CHAPTER 11, SECTIONS 11,12,15,16,17 & 19. |
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