1. INFORMATION 

Reissues and revisions are automatically provided to the subscription holders of the manual. 

Additional publications are listed on the web at http://pubs.hawkerbeechcraft.com. For more information on these 

publications, or to check subscription status, contact the Technical Manual Distribution Center (TMDC) at 1.800.796.2665 or 

316.676.8238, fax 316.671.2540, E-mail tmdc@hawkerbeechcraft.com. 

Since a wide variety of avionic components and equipment is available, avionic manufacturers normally supply parts and 

servicing manuals with each set/component. The manufacturer of the equipment should be contacted when additional parts 

or servicing information is required. 

The Interactive Maintenance Library (IML) contains selected Manuals in a digital format. This manual, along with others, is 

available on CD-ROM and online. Optional paper copies of the manuals on CD-ROM are available for purchase. 

Help Line phone support for IML CD and Online Users is available 8:00 AM to 4:30 PM Central Time (US and Canada). 

During off-hours, leave a detailed voicemail message. Calls will be returned within one business day. Contact the Help Line 

at 1.800.240.2959 or 1.316.676.3053, E-mail iml@hawkerbeechcraft.com. 

Comprehensive user guides for the IML CD and Online manuals are available on the Hawker Beechcraft Corporation (HBC) 

Technical Publications website http://pubs.hawkerbeechcraft.com. Illustrated and detailed procedures for using IML Features 

are included in the downloadable user guides. 

A. General 

This Structural Inspection Manual applies to the Hawker Beechcraft Corporation 1900 Airliner (UA Serials), 1900C Airliner 

(UB and UC Serials). The wording MODEL 1900/1900C AIRLINER appearing in the masthead at the top of each page is 

not intended to indicate applicability beyond that noted above. Separate Structural Inspection Manual coverage is 

provided for subsequent models in the 1900 Airliner Series. 

The Model 1900/1900C Airliner Structural Inspection Manual is prepared in accordance with the ATA (Air Transport 

Association of America) Specification 2200 format. It meets the requirements with respect to the arrangement and content 

of the System/Chapters within the designated chapter-numbering system. This manual includes the maintenance 

information required to be available by 14 CFR Part 23. 

In addition to this manual and its subsequent revisions, additional maintenance information is published in the form of 

Hawker Beechcraft Corporation service bulletins. The information contained in these service bulletins is an integral part of, 

and is to be used in conjunction with, the information contained in this manual. 

This Structural Inspection Manual is supplemented by the following publications: 

 Model 1900/1900C Airliner (UA-1 and After, UB-1 and After) Illustrated Parts Catalog, P/N 114-590021-5 

 Model 1900C Airliner (UC-1 and After) Illustrated Parts Catalog, P/N 114-590021-59 

 Model 1900/1900C Airliner (UA-1 and After, UB-1 and After, UC-1 and After) Maintenance Manual, P/N 114-

590021-7 

 Model 1900 Airliner (UA-1 and After) Wiring Diagram Manual, P/N 114-590032-3 

 Model 1900C Airliner (UB-1 thru UB-74) Wiring Diagram Manual, P/N 114-590021-13 

 Model 1900C Airliner (UC-1 and After) Wiring Diagram Manual, P/N 114-590021-61 

 Model 1900 Airliner Series Component Maintenance Manual, P/N 114-590021-11 

 Model 1900 Airliner Series Structural Repair Manual, P/N 114-590021-9 

 Model 1900 Airliner Series Corrosion Control Manual, P/N 114-590021-197 

 Model 1900 Series Airliners Kit Supplement Illustrated Parts Catalog, P/N 129-590000-131 

 Model 1900 Airliner Series Airworthiness Limitation Manual, P/N 129-590000-133 

It shall be the responsibility of the owner/operator to ensure that the latest revision of the publications referenced in this 

manual are utilized during operation, servicing and maintenance of the airplane. 

Current as of Oct 1/12

7/16/2013 1:53:31 PM

Page 1 of 6
Hawker Beechcraft Corporation expressly reserves the right to supersede, cancel and/or declare obsolete any parts, part 

numbers, kits or publications that may be referenced in this manual without prior notice. 

Warning: Use only parts obtained from sources approved by Hawker Beechcraft Corporation, in connection with 

the maintenance and repair of Hawker Beechcraft Corporation airplanes. 

Genuine Hawker Beechcraft Corporation parts are produced and inspected under rigorous procedures 

to insure airworthiness and suitability for use in Hawker Beechcraft Corporation airplane applications. 

Parts purchased from sources other than those approved by Hawker Beechcraft Corporation, even 

though outwardly identical in appearance, may not have the required tests and inspections performed, 

may be different in fabrication techniques and materials, and may be dangerous when installed in an 

airplane. 

Salvaged airplane parts, reworked parts obtained from sources not approved by the Hawker Beechcraft 

Corporation or parts, components or structural assemblies, the service history of which is unknown or 

cannot be authenticated, may have been subjected to unacceptable stresses or temperatures or have 

other hidden damage, not discernible through routine visual or usual nondestructive testing 

techniques. This may render the part, component or structural assembly, even though originally 

manufactured by the Hawker Beechcraft Corporation, unsuitable and unsafe for airplane use. 

Hawker Beechcraft Corporation expressly disclaims any responsibility for malfunctions, failures, 

damage or injury caused by use of parts not approved by the Hawker Beechcraft Corporation. 

Any maintenance requiring the disconnection and connection of flight control cables, plumbing, 

electrical connectors or wiring requires identification of each side of the component being 

disconnected to facilitate correct reassembly. At or prior to disassembly, components should be color 

coded, tagged or properly identified in a way that it will be obvious how to correctly reconnect the 

components. After reconnection of any component, remove all identification tags. Check all associated 

systems for correct function prior to returning the airplane to service. 

B. Qualifications 

All personnel performing Non-destructive Testing Inspections (NDT) in this manual must be qualified and Certified Level II 

or Level III in accordance with NAS 410 in the method in which they are performing. All Inspections must be documented 

and approved by a person who has completed the Model 1900 Airliner Series Cold Expansion Course offered by Hawker 

Beechcraft Corporation, no alternate courses are approved. The Implementation of these test procedures by unauthorized 

personnel will not be considered valid. The Model 1900 Airliner Series Cold Expansion Course information can obtained 

by calling 1.800.429.5372 option 5 then option 1 or 316.676.3140. 

Note: A Certified Level II or Level lII technician in accordance with NAS 410 may perform the NDT requirements 

as directed in this manual having not attended the Hawker Beechcraft Corporation Training, if the 

technician is directed by a person who has completed training. 

C. Correspondence 

If a question should arise concerning the care of your airplane, it is important to include the airplane serial number in any 

correspondence. The serial number appears on the model designation placard. Refer to Chapter 11 in the Model 

1900/1900C Airliner Maintenance Manual for placard location. 

D. Publications Change Request (PCR) 

If an irregularity or missing information is noted, the user of this manual may access a PCR form at 

http://pubs.hawkerbeechcraft.com. Instructions on how to submit a PCR are available on the web page. 

E. Normal Revisions 

Normal Revisions to this manual are issued to provide changes to maintenance information. 

1. Paper Revision 

That portion of text which has been revised by the addition of, or a change in, information is denoted by a solid 

revision bar adjacent to the text. The date printed on the bottom of each page can be compared to the "A" page to 

determine the revision number. Each revised page will ONLY show revision bars for text changed by the revision. 

There will not be a revision bar if text was deleted from the page. 

Revised illustrations will be identified by a revision bar printed on the side of the page. 

7/16/2013 1:53:31 PM

Page 2 of 6
2. CD-ROM Revision 

Normal revised text on the CD-ROM will be highlighted yellow across the revised passage of text. For each revision 

of this manual, a new CD-ROM will be issued. 

The CD-ROM may contain revised illustrations. Revisions to the illustrations are not identified. 

F. Temporary Revisions 

Temporary Revisions to this manual are issued to provide maintenance information in the interim between normal 

revisions. Each temporary revision is issued by the chapter number to which it applies, followed by a sequential number in 

the order of publication (Temporary Revisions 12-1, 12-2, etc.). If relevant, the information in the temporary revision 

should be included in the next normal revision of the manual. 

1. Paper Temporary Revisions 

Temporary Revisions are printed on yellow paper and are to be inserted in the maintenance manual in accordance 

with the instructions provided and adjacent to applicable chapter, section, and subject matter in the manual. 

2. CD-ROM Temporary Revisions 

A new CD-ROM will be issued for each Temporary Revision to this manual. This information is listed in conjunction 

with the applicable chapter, section, subject on the CD-ROM. 

G. Revised Text 

That portion of text which has been revised by the addition of, or a change in, punctuation and/or information is denoted 

by a solid revision bar adjacent to the textual column in the margin of this paragraph. Each page may or may not have 

revision bars. That date printed on the bottom of each page indicates when the information on that page was changed. 

Each page will ONLY show revision bars for punctuation and/or text changed by the current revision. Revised text in IML 

will be denoted by yellow highlighting. 

H. Revised Illustrations 

When an illustration is modified or a new illustration is added, it will be noted by a solid line (revision bar) along the 

outside margin of the illustration. 

I. Warnings, Cautions, and Notes 

 WARNING - Brings attention to an operating procedure, inspection or maintenance practice, which if not correctly 

followed, could result in personal injury or loss of life. 

 CAUTION - Brings attention to an operating procedure, inspection, repair or maintenance condition, which if not 

strictly observed, could result in damage or destruction of equipment. 

 NOTE - Brings attention to an operating procedure, inspection, repair or maintenance condition, which is essential 

to highlight. 

2. MANUAL LAYOUT 

A. Title Page 

A Title page is located at the beginning of the manual and provides the part number of the manual, and lists all aircraft 

models pertaining to this manual and their respective serial numbers. Information throughout this manual is applicable to 

all serial numbers listed on the title page except where specifically stated. 

B. List of Effective Revisions/List of Effective Pages 

The printed manual will have a List of Effective Revisions/List of Effective Pages, ("A" page) following the title page of the 

manual. The List of Effective Revisions page lists the revisions currently effective for the manual. The List of Effective 

Pages section lists the page effectivity for the Title Page(s), "A" page(s) and Introduction chapter. It will also show the 

effective pages for an entire manual if the manual does not have individual Chapter List of Effective Pages. 

C. Record of Revisions Page 

The printed manual will have a Record of Revisions page. The Record of Revisions is provided following the List of 

7/16/2013 1:53:31 PM

Page 3 of 6
Effective Revisions/List of Effective Pages ("A" page). When a revision is inserted, the revision number, the date the 

revision is inserted into the manual, and the initials of the person(s) inserting the revision should be recorded on this page. 

IML CD and Online Manuals do not include a Record of Revisions page. Revisions standard is avalible by a link to the 

catalog Title Page or accessible by clicking Help on the menu bar and selecting "About This IML Book...". 

D. Log of Temporary Revisions Page 

The printed manual will have a Log of Temporary Revisions page. The Log of Temporary Revisions Page is located 

following the Record of Revisions page. The Log of Temporary Revisions page provides a history of each temporary 

revision, including the revision number which incorporated the temporary revision into the manual. 

E. Record of Temporary Revisions Page 

The printed manual will have a Record of Temporary Revisions page. The Record of Temporary Revisions Page is 

located following the Log of Temporary Revisions page. When a temporary revision is inserted or removed from this 

manual, the appropriate information should be recorded on this page. 

F. Introduction 

This section contains general and specific information on how to use this manual. 

G. Chapter List of Effective Page 

The printed manual may have a Chapter List of Effective Pages. The List of Effective Pages follow the Chapter-DividerTab and lists the issue date of each page that is effective for that chapter. 

H. Chapter Table of Contents Pages 

The printed manual may have a Chapter Table of Contents Pages. The Chapter Table of Contents Pages follow the 

Chapter List of Effective Pages and lists the contents of the data for that chapter. 

3. INSPECTION PROCEDURES 

Wherever this manual addresses a specific area or component, it is implied that the inspection will include reasonable 

observation and evaluation of the surrounding area. Airplane components that may have been modified by STC are not the 

responsibility of Hawker Beechcraft Corporation and are not covered by this manual. Inspection of any such component 

affected by this manual must automatically be referred to the STC holder for FAA approval guidelines. 

Note: Any inspection findings, repairs and modifications accomplished must be communicated to Hawker 

Beechcraft Corporation within 10 days in order to access the effectiveness of the recommended inspection 

procedures and time intervals. 

Send all available data, including repairs, photos, sketches, etc., to Hawker Beechcraft Corporation at the address on the 

report form. An example of a report form is provided in the REPORT FORM section of this chapter. Blank report forms for 

each check are provided after the FORMS tab section of this manual for copying and use. Contact Hawker Beechcraft 

Corporation Airline Technical Support at the following numbers for repair information not available in other Hawker 

Beechcraft Corporation publications and for information concerning technical support documents applying to your airplane: 

Telephone: 316.676.7016 or Fax: 316.676.8051. 

A. Inspection Schedule 

The Airworthiness Limitations Manual specifies the time limits for accomplishing the various inspections included in this 

manual. Detailed procedures for each inspection are outlined in the appropriate sections of this manual. 

The initial times and intervals for particular inspections are expressed in flight hours, while the fuselage inspections are 

expressed in both hours and cycles. The inspection times and intervals are considered to be nominal times. If the initial 

inspection is specified as 12,000 hours and the specified interval is 3,000 hours, the nominal inspection times will be at 

12,000 hours, 15,000 hours, 18,000 hours, etc. In order to coordinate these inspections with the Continuous Inspection 

Program outlined in Chapter 5 of the Model 1900/1900C Airliner Maintenance Manual, any inspection specified in the 

inspection schedule may be varied by an amount of time not to exceed 10% of the inspection interval specified in the 

inspection schedule. However, under no circumstances can the interval between any two inspections be allowed to 

exceed 110% of the interval. For example, if a nominal inspection point is 15,000 hours and the specified inspection 

interval is 3,000 hours, that inspection may be performed as early as 14,700 hours or as late as 15,300 hours. The next 

inspection must be performed within 3,300 hours provided the 10% variance about the nominal inspection point is not 

exceeded. Therefore, if the last inspection was completed at 14,700 hours, the next inspection must be performed no later 

7/16/2013 1:53:31 PM

Page 4 of 6
than 18,000 hours. However, if the last inspection was completed at 15,300 hours, the next inspection must be performed 

no later than 18,300 hours. 

It is permissible to perform the initial fuselage or wing inspection early to accommodate fleet scheduling. However the 

subsequent recurring inspections will be set to re-occur at 3,000 hours from the initial time. Example: Initial fuselage 

inspection at 10,500 hours, the next inspection will be due at 13,500 hours. 

The Empennage inspection is expressed in calendar time for the initial inspection while the repetitive inspections are 

expressed in airframe hours. 

B. Inspection Intervals 

The structural inspection intervals for the 1900/1900C airliners are in the Model 1900 Airliner Series Airworthiness 

Limitations Manual, P/N 129-590000-133. 

C. Report Form Example 

An example of a Check Discrepancy Report Form is shown below. 

Note: Complete the appropriate CHECK DISCREPANCY REPORT form each time this inspection is performed. 

Discrepancies revealed during this inspection must be repaired. Applicable repair procedures may be 

found in the Model 1900 Airliner Series Structural Repair Manual. Report each discrepancy found and the 

corrective action taken to clear the discrepancy. If no discrepancies were found, write the word NONE on 

the form. Please mail the completed form to the address indicated at the bottom of the form. If required, 

mark any discrepant areas on a photo and attach it to the report form. 

A blank copy of the various report forms is provided in each section of this manual and after the FORMS

tab section of this manual. Copy the appropriate form as required for the inspection being performed. 

4. CHAPTER/SYSTEM INDEX GUIDE TABLE 

The following System/Chapter, Subsystem/Section Index Guide is prepared in accordance with ATA Specification No. 2200 

for use with maintenance manuals, parts catalogs and wiring diagram manuals. 

Table 1 

"A" CHECK DISCREPANCY REPORT 

AIRCRAFT S/N UC-157 DATE 7 Oct. 1998 PAGE 1 of 1

Aircraft Flight Hours 12,000 Airplane Cycles 15,952

Step Number Discrepancy and Corrective Action 

1 A loose fastener was found at FS 150. It was replaced with equivalent fastener. 

9 Two rivets were missing under the airstair door at FS 145. Rivets were replaced with 

MS470AD5-6 fasteners. 

 

 FORM LENGTH REDUCED FOR THIS EXAMPLE 

 

 

 

Report submitted by Joseph T. Technician Organization Wichita Flying Service Center 

Area Code and Phone Number 1-316-555-1212 

Mail this report to: 

Hawker Beechcraft Corporation, Attn: Airliner Technical Support, P.O. Box 85, Wichita, KS 67201-0085 

System/Chapter Subsystem/Section 

INTRODUCTION 

 

20-00-00 

7/16/2013 1:53:31 PM

Page 5 of 6
 

INSPECTIONS 

 

"A" CHECK "A" Check Procedures 

 

"B" CHECK "B" Check Procedures 

 

"C" CHECK "C" Check Procedures 

 

"D" CHECK "D" Check Procedures 

 

"D1" CHECK "D1" Check Procedures 

 

"D2" CHECK "D2" Check Procedures 

 

"E" CHECK "E" Check Procedures 

 

"F" CHECK "F" Check Procedures 

 

"G" CHECK "G" Check Procedures 

 

"H" CHECK "H" Check Procedures 

 

"I" CHECK "I" Check Procedures 

 

FORMS 

 "A" Check Discrepancy Report 

 "B" Check Discrepancy Report 

 "C" Check Discrepancy Report 

 "D" Check Discrepancy Report 

 "D1" Check Discrepancy Report 

 "D2" Check Discrepancy Report 

 "E" Check Discrepancy Report 

 "F" Check Discrepancy Report 

 "G" Check Discrepancy Report 

 "H" Check Discrepancy Report 

 "I" Check Discrepancy Report 

7/16/2013 1:53:31 PM

Page 6 of 6