Paperwork Reduction Act Burden Statement: This form reports occurrences or detection of each failure, malfunction, or defect in an aircraft.
A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a currently valid OMB Control Number. The OMB Control Number for this information collection is
2120-0663. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, completing and reviewing the
collection of information. All responses to this collection of information are required per 14 CFR Part 135. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to the FAA at:
800 Independence Ave SW, Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200.
                                                                                                                                                                                                          FORM APPROVED
                                                                                                                                                                                                          OMB No. 2120-0663 Exp. 10/31/2020
                                                                          DEPARTMENT OF TRANSPORTATION                                                                                                                 RIS- WS 8070-1
                                                                                  FEDERAL AVIATION ADMINISTRATION
                                                                                                                                                                                                                               Control No.
           U.S. Department
           of Transportation
           Federal Aviation
           Administration
                                                      Service Difficulty Report                                                                                                            ATA                      Code
                                                                                     AERONAUTICAL EQUIPMENT
         MAJOR EQUIPMENT IDENTITY
                         Enter pertinent data                           MANUFACTURER                                    MODEL/SERIES                                  SERIAL NUMBER
                                                                                                                                                                                                              NA16WE
                                                               boeing                                          737-200
                  AIRCRAFT                                                                                                                                        30663
                  POWERPLANT
                  PROPELLER
         PROBLEM DESCRIPTION
                                DATE                                STATUS                      CARRIER                      ATA                        AIRCRAFT TYPE                        N-                                CONTROL NO.
                          03/09/2020
                 TEXT
                  The accident aircraft was HK 0099, Boeing 737-700, serial number 30663; which was impacted on the right plane from the bottom, due to the impact it is necessary to repair the outer flap on the
                  right side, completely removing the lower skin and repairing three ribs of the same flap.
                  Likewise, it was necessary to correct a small dent in the tip of the wing on the right side and remove it to paint it again.
                  The impact to the aircraft caused the destruction of the wingtip, taking into account the magnitude of the work, the operating airline of the aircraft decided to make a modification to the aircraft
                  and install the winglets using STC.
                  SPECIFIC PART CAUSING PROBLEM
                             PART NAME                                                    MFG. PART NUMBER                                             PART CONDITION                                       PART/DEFECT LOCATION
                                                                                                                                                                      Report                               PART TT                    PART TSO
                   COMPONENT/APPLIANCE ABOVE PART INSTALLED ON                                                                                                         whole
                                                                                                                                                                       hours
                                COMP/APPL NAME                                              MANUFACTURER                                             MFG. MODEL/NUMBER                                                SERIAL NO.
         SUBMITTED BY
                   SUBMITTER (Check one)                                                    A            B            C            D             E           F            G           H            I       P. S. L. ALERT               OPER/D.O.
                                                                                         CARRIER        REP          OPER         MECH          AIR         MFG           FAA       OTHER         Spec.
                                                                                                        STA.                                    TAXI
                    PREC. PROC.        NATURE          STAGE       STAT         ROLL                   Frame                             SYS.                     SYS.
                ADDITIONAL COMMENTS
                 FAA Form 8070-1 (11-84) SUPERSEDES PREVIOUS EDITION                                                                                                              Shaded Areas are for FAA USE ONLY
                         All Submitters - Instructions for Completing FAA Form 8070-1
Major Equipment Identity
 TITLE                         ENTRY
 Aircraft                       Identify major equipment related to problem. Enter manufacturer, model, and serial
                                number per FAA/MANUFACTURER type certificate data sheet. If amateur built, use
 Powerplant
                                plan or kit name. Use military model designators when appropriate. Avoid colloquial
 Propeller
                                names and market titles.
 N                             Aircraft Registration Number.
Problem Description
 Date                          Give date problem occurred (i.e., 7-1-84).
 Text                          Whenever possible, describe conditions subsequent to, or leading up to, the reported problem:
                               (a) Identify the cause for malfunction and emergency measures execute. (b) Include com-
                               pliance or noncompliance with Airworthiness Directives, Service Bulletins, STC's, and PMA's.
                               (c) Provide any significant fact you feel may help to reduce or eliminate recurrence (i.e., cycles,
                               landings, and suggested changes).
 Part Name                     Skin, rib, shaft, Venturi, transistor, capacitor, etc. Avoid colloquial names.
 Mfg. Part Number              Alphanumeric part identifiers assigned by manufacturer.
 Part Condition                Cracked, bent, burned, corroded, shorted, etc.
 Part/Defect Location          L.H. alternator, audio, R.H. outboard, range switch, etc.
 Part TT                       Total service time on part in whole hours (i.e., 00531).
 Part TSO                      Service time on part since overhaul in whole hours (i.e., 00200)
 Comp/Appl Name                Fuselage, wing, alternator, carburetor, VOR receiver, etc.
 Manufacturer                  Comp/appl manufacturer: Beech, Cessna, Prestolite, Bendix, Collins, etc.
                               Alphanumeric model and serial numbers or identifiers assigned by comp/appl manufacturer
Mfg. Model/Number,
                               (i.e., ALU8403, NAS3A1, 51 RVII). Do not repeat ''MAJOR EQUIPMENT IDENTITY" in these
Serial Number                  locations.
Submitted By
Submitter                      As noted on form.
FAA District Offices - Refer to FAA Order 8010.2
                                                                                             U.S. GOVERNMENT PRINTING OFFICE: 1984-461-823-21521