| WHAT DOES NAMDRP STAND FOR | NAVAL AVIATION MAINTANENCE DECREPIENCY REPORTING PROGRAM |
| DISCUSS ENGINEERING INVESTIGATION (EI) | IS A PHYSICAL EXAMINATION OF DISCREPANT MATERIAL CONDUCTED BY THE DESIGNATED FLEET SUPPORT TEAM. TO DETERMIND TO ROOT CAUSE OF DEFECTS AND DEFICIENCES. |
| HOW OFTEN DO YOU UPDATE MAINTENANCE | HOUR BY HOUR MAINTENANCE |
| WHAT ARE THE TYPES OF TD'S | 1. FORMAL CHANGE- AIRFRAME CHANGE
2. INTERIM- INTRIM AIRFRAME CHANGE
3. BULLETIN- ONE TIME INSPECTION TO DETERMIND IF A GIVEN PROBLEM EXISIT
4. RAPID ACTION MINIOR ENGINEERING CHANGE- FLEET SELF HELP |
| WHAT IS THE TD PUBLICATION | 00-25-300 |
| WHAT ARE THE CATIGORTIES OF TD'S #1 | IMMEDIATE- ASSIGNED WHEN UNSAFE CONDITIONS EXISIT DONE BEFORE NEXT FLIGHT |
| WHAT ARE THE CATIGORTIES OF TD'S #2 | URGENT- ASSIGNED WHEN FACTORS OF COMBAT NECESSITY OR POTENTIAL HAZARDOUS CONDITIONS COULD RESULT IN PERSONNEL INJURY OR DAMGE TO VALUABLE PROPERTY |
| WHAT ARE THE CATIGORTIES OF TD'S #3 | ROUTINE- NOT URGENT BUT THE ASSIGNMENT WOULD BE INNAPROPATE. |
| WHAT ARE THE CATIGORTIES OF TD'S #4 | RECORD PURPOSE- TO DOCUMENT CHANGES THAT HAVE BEEN INCORPORTATED IN ALL AFFECTED AIRCRAFT |
| WHO IS OVERALL IN CHARGE FOR MAINTAINING AND IMPLEMENTING THE NAVAIR TD SYSTEM | AIR-6.0 |
| WHERE ARE MELS POSTED | IN THEFLIGHT STATION, ADB, AND A-SHEET |
| WHAT IS A ADDR AND HOW LONG DO YOU HAVE TO SUBMIT | AIRCRAFT DELEVERY DEFICIENCY REPORT- ARE DEFICIENCY FOUND DURING A DEPOT LEVEL MAINTANENCE. ADDRS WILL BE SUBMITTED TO THE SQUADRON RECIEVING THE AIRCRAFT. INITAL ADDR WILL BE SUBMITTIED WITHIN 20 CALENDAR DAYS. SUPPLEMENTAL ADDRS WILL BE SUBMITTED WITHIN 30 DAYS TO THE RECIEVING SQUADRON. |
| WHAT IS A PQDR? | PRODUCT QUALITY DEFICIENCY REPORT- PARTS OR EQUIPMENT THAT DEFICIENCIES WHERE FOUND DURING RECEVING A PART OR FAILED DURING FIRST FLIGHT. |
| WHAT IS THE PQDR CAT 1 | CAT1 WILL BE SUBMITTED FOR DEFICIENCIES THAT COULD CAUSE DEATH, INJURY, OR LOSS OF AIRCRAFT, SUBMITTED WITHIN 24 HOURS. |
| WHAT IS THE PQDR CAT 2 | CAT2 ARE DEFICIENCIES THAT DO NOT AFFECT SAFETY, SUBMITTED WITHIN 3 DAYS. |
| WHAT IS A MESM? WHAT DOES IT DO? | MISSION ESSENTIAL SUBSYSTEM MATRIX- GIVES EOC CODES AND EXPLAINS IF THE SUBSYSTEM IS A DOWNER OR PARTIAL AND IF A MEL IS REQUIRED. |
| WHAT EOC CODES ARE PARTIALS AND WHAT ARE DOWNERS | ALL CODES C-K ARE PARTIALS AND THE ONLY DOWNER CODES IS Z |
| WHAT ARE THE FCF PROFILES? | FCF A- ACCEPTING OF AN AIRCRAFT, 30 NO FLY AND AFTER COMPLETION OF STANDARD REWORK.
FCF B- BOTH ENGINE CHANGES.
FCF C- RERIGING, REMOVAL, AND INSTILLATION OF MOVEABLE FLIGHT CONTROL SURFACES.
FCF D- REPLACEMENT OR INSTALLATION OR BOTH AIR DATA INERITAL REFERENCE UNITS. |
| WHAT IS REQUIRED ON A 30 DAY NO FLY BESIDES FCF A | AIRCRAFT MUST BE FOD FREE BY A QAR OR CDQAR. |
| WHO CAN FLY A FCF? WHO CAN PASS OR FAIL A FCF? | ANY FCF QUALIFIED PILOT. |
| HOW LONG DO WE HOLD FCF PROFILES? | FCFS ARE HELD UNTIL ANOTHER FCF OF THE SAME PROFILE IS COMPLETED. |
| WHEN CAN A FCF B, C, AND D TURN INTO A FCF A | IF THE AIRCRAFT ISNT FLOWN WITHIN 30 DAYS. |
| HOW LONG DOES VP-46 TRACK FOD? HOW LONG DOES THE NAMP SAYS TO TRACK FOD. | VP-46 RETAINS FOD TRENDS FOR 1 YEAR. THE NAMP SAY TO KEEP FOD TRENDS FOR 90 DAYS. |
| WHAT IS A IFE? | IN FLIGHT EVALUATION- INTENTED TO BE PERFORMED ON ANY SYSTEM OR COMPONET THAT CANNOT BE PROPERLY EVALUATED THROUGH FUNCTIONAL OR OPERATIONAL CHECKS ON THE GROUND. |
| HOW MANY IFE ENCLOSURES ARE THERE DURING AN IFE? WHERE ARE THEY LOCATED? | THERE ARE 3 ENCLOSURE 2. LOCATED FIRST IN QA, SECOND IN THE ADB, AND THIRD IN THE WORK CENTER. |
| HOW LONG DO YOU HAVE TO COMPLETE AN IFE? WHO CAN EXTEND IT AND FOR HOW LONG? | IFE SHOULD BE COMPLETED WITHIN 5 FLIGHTS. THE MO CAN EXTEND AN IFE FOR INDEFENTLY |
| WHAT IS A TPDR? | TECHNICAL PUBLICATION DEFICIENCY REPORT. |
| WHAT IS TPDR CAT 1 | SUBMITTED ON SAFETY RELATED TECHNICAL PUBLICATIONS THAT COULD OR RESULTED IN DEATH, INJURY TO PERSONNEL, DAMAGE OR LOSS OF AN AIRCRAFT. DUE TO TECH MANUAL MISSING IMPORTANT SAFETY STEP. |
| WHAT IS TPDR CAT 2 | SUBMITTED ON NON-SAFETY RELATED TECH PUBS THAT CAUSED A DELAY IN MAINTENANCE PROCEDURES OF 8 OR MORE HOURS. |
| WHAT IS TPDR CAT 3 | SUBMITTED FOR NON-SAFETY RELATED PUBS THAT CAUSED A DELAY OF LESS THAN 8 HOURS. |
| WHAT IS TPDR CAT 4 | SUBMITTED FOR NON-SAFETY RELATED PUBS THAT DO NOT CAUSE A DELAY IN MAINTENANCE. SUBMITTED FOR MISSPELLS AND TYPOS |
| DISCUSS ENGINEERING INVESTIGATION (EI) | IS A PHYSICAL EXAMINATION OF DISCREPANT MATERIAL CONDUCTED BY THE DESIGNATED FLEET SUPPORT TEAM. TO DETERMIN TO ROOT CAUSE OF DEFECTS AND DEFICIENCES. |
| DISCUSS EXPLOSIVE MISHAP REPORTING (EMR) | EMRS WILL BE REPORTED EVEN IF A ORDANCE SYSTEM WORKS AS DESIGN AND HUMAN ERROR CONTRIBUTED TO A INCIDENT OR ACCIDENT. REPORTED USING RISK MANAGEMENT INFORMATION. |
| DISCUSS CONVENTIONAL ORDANCE DISCREPANCY REPORT (CODR) | CODRS ARE REPORTED WHEN ORDANCE OR WEAPON SYSTEMS FAIL TO FUNCTION. THIS INCLUDES IMPROPER STORAGE OF AMMUNITION AND EXPLOSIVES. |
| DISCUSS HAZARDOUS MATERIAL REPORT (HMR) | HMRS ARE ALL CAT 1 SAFETY DISCREPANCIES AND COULD BE DUAL REPORTED WITH CODRS
MAILFUNCTION OR FAILURE OF A COMPONET
A CONFIGURATION DEFICIENCY IN AIRCRAFT, ENGINES, OR SUPPORT EQUIPMENT
A DESIGN FLAW THAT ALLOWS INNCORRECT INSTALLATION OF PARTS
IN-FLIGHT OR GROUND LOSS OF AIRCRAFT PARTS |
| WHAT IS A ELAR | ELECTRONIC LOCAL AREA REQUEST- TO REQUEST A CLARIFICATION ON PUBS OR ITEMS. FOUND ON NATEC. |
| DISCUSS THE 5 FACTORS REQUIRED TO ACHIEVE THE BASIC CONCEPT OF QA | 1. THE APPLICATION OF QA FROM START TO COMPLETION OF EACH MAINTENANCE TASK TO PREVENT DEFECTS BEFORE THEY OCCUR.
2. IMPROVE THE QUALITY, UNIFORMITY, AND RELIABILTY OF AIRCRAFT AND EQUIPMENT.
3. IMPROVE THE QUALITY OF MAINTENANCE MATERIALS, TECHNICAL DATA AND PROCESS.
4. IMPROVE THE SKILLS AND CONSISTENCY IN PERFORMANCE OF MAINTENANCE PERSONNEL.
5. ELIMINATE UNNECESSARY MAN-HOURS AND MATERIAL EXPENDITURES. |
| DISCUSS THE BASIC CONCEPTS OF QA | THE PROCESS OF SYSTEMATIC INSPECTIONS AND MONITORING THE VERIFY STANDARDS OF QUALITY ARE BEING MET IN THE NAVY AND MARINE CORPS AIRCRAFT, ENGINE, COMPONETS, AND EQUIPMENT. |
| DISCUSS PURPOSE AND FUNCTION OF THE CDI | CDI's INSPECT ALL WORK AND COMPLY WITH THE REQUIRED QA INSPECTIONS DURING ALL MAINTENANCE ACTIONS PERFORMED BY THEIR PRODUCTION WORK CENTER. CDI's ARE RESPONSIBLE TO THE QAO WHEN PERFORMING QA FUNCTIONS. |
| DISCUSS THE DEFINITION AND PURPOSE OF RECIEVING/SCREENING INSPECTIONS | R/S INSPECTIONS APPLY TO RECIEVING PARTS, EQUIPMENT, LOGS AND RECORDS, CONFIGURATION MANAGEMENT AUTO-LOGS (CM-ALS), AND DOCUMENTS. THE INSPECTION TO IDENTIFY TO CONDITION AND THE ACCURACY OF ACCOMPANYING RECORDS. |
| DISCUSS IN-PROCESS INSPECTION | INPROCESS INSPECTION ARE REQUIRED DURING THE PERFORMANCE OF A MAINTENANCE WHERE SATISFACTORY ACCOMPLISHMENT OF THE TASK CANNOT BE DETERMINED AFTER THE TASK HAS BEEN COMPLETED. REQUIRING FOR INPROS INCLUDED 'QA' STEPS ON MAINTENANCE PROCEDURES. ALSO WHEN TASK CARDS OF SMI's ARE COMPLETED. |
| DISCUSS ZONAL INSPECTIONS | INPECT FOR OBVIOUS DEFECTS SUCH AS LEAKS OR FOREIGN OBJECTS IN THE IMMEDIATE WORK AREA PRIOR TO CLOSING A PANEL OR FINISHING THE JOB. |
| DISCUSS FINAL INSPECTIONS | ARE SPECIFIC QA FUNCTIONS PERFORMED FOLLOWING THE COMPLETION OF A MAINTENANCE TASK. LIKE OP CHECKS AND BIT TESTS. |
| DESCUSS CHAIN OF RESPONSIBILITY FOR THE CDI WHEN PERFORMING INSPECTIONS | CDI- QDQAR- QAR- QALPO- QAS- QAO- MO- CO |
| DISCUSS TYPES OF INSPECTIONS THAT CAN NOT BE PERFORMED BY A CDI | 1. EGRESS, PERSONNEL PARACHUTES, AND FLOTATION DEVICES INPRO AND FINAL INSPECTION.
2. INSPECTIONS ON THEIR OWN WORK.
3. AIRCRAFT SAFETY OF FLIGHT INSPECTIONS.
4. FCF INPROS AND FINAL INSPECTION. |
| HOW MANY TIMES DURING A JOB DOES A CDI CHECK TOOLS | A CDI CHECKS TOOLS 5 TIMES. WHEN SIGNING THE TOOLS OUT, WHEN YOU GET TO THE JOB, OPERATIONAL CHECKS, AFTER JOB IS COMPLETE, AND WHEN CHECKING THEM BACK IN. |
| WHO RECOMMENDS SOMEONE TO BECOME A CDI | THE DIVISION OFFICER WILL ENDORSE THE CDI. |
| WHAT IS OPNAV 5100.23 | NAVY SAFETY AND OCCUPATIONAL HEALTH MANUAL |
| WHAT CHAPTER LETS US USE ULSS | CHAPTER 11 LETS YOU USE ULSS |
| WHAT PROGRAMS DOES QA MANAGE | AIRCRAFT CONFINED SPACE
VIBRATION ANALYSIS
MAINTANENCE SAFETY
AUDITING
NAMDRP
TECHNICAL DATA MANAGEMENT |
| WHAT ARE CH 3,5,7, AND 10 | CH 3- MAINT CONCEPTS
CH 5- MAINT CONTROL
CH 7- QA
CH 10- NAMPSOPS |
| WHAT IS APPENDIX A, B, D, AND E | A- Acronyms, Abbreviations, and Definitions
B- FORMS
D- LOCAL COMMAND PROCEDURES.
E- Maintenance Documentation Codes |
| WHAT IS PMIC? DEFINE A SCHEDULE REMOVAL COMPONET. | PERIODIC MAINTENANCE INFORMATIONAL CARD. SRC IS WHEN A SERIALIZED COMPONET NEEDS TO BE REMOVED +/- 10% OF LIFE OF COMPONET OR HYDRO STRATIC TEST DATE. |
| WHAT IS THE GENERAL IDEA OF THE STATEMENT AT THE BOTTOM OF 4790/12 | THAT I AM RESPONSIBLE TO THE CO WHEN PERFORMING QA FUNCTIONS. THAT I WONT LET ANY JUDGEMENT OR PERSONAL MATTER INTERFER WHEN INSPECTING WORK. ALSO THAT WHEN I SIGN THE CDI BLOCK I CERTIFY THAT THE WORK HAS BEEN INSPECTED IAW THE INSTRUCTIONS. AND THAT I CERTIFY THE WORK IS SAFE FOR FLIGHT. |
| WHAT ARE THE GENERAL WUC 030 AND 040 USED FOR? | 030- IS FOR MAINTENANCE INSPECTIONS, USED FOR ACCEPTANCE, TRANSFER, AND CONDTIONAL REPAIRS.
040- CORROSION PREVENTION, USED FOR UNSCHEDULED CORROSION PREVENTION. |
| DEFINE TRANS CODE 11 | 11- WORK THAT DOESNT INVOLVE REMOVAL OF COMPONETS. |
| DEFINE TRANS CODE 12 | 12- WORK THAT REQUIRES REMOVAL AND REPLACE OF CONSUMABLES
DOCUMENTED AS FAILED PARTS. |
| DEFINE TRANS CODE 16 | 16- REMOVAL OF A NONDEFECTIVE COMPONET TO BE PROSESSED AT AN O-LEVEL EVENT. NONSERIALIZED COMPONETS THE INSTALLED BLOCK SECTION OF THE WO MUST BE A SINGLE ZERO. |
| DEFINE TRANS CODE 17 | 17- INSTALLATION OF A NONDEFECTIVE COMPONET. NONSERIALIZED COMPONETS THE INSTALLED BLOCK SECTION OF THE WO MUST BE A SINGLE ZERO. |
| DEFINE TRANS CODE 23 | 23-REMOVAL AND REPLACEMENT OF DEFECTIVE OR SCHEDULED MAINTENANCE OF A REPAIRABLE COMPONET |
| DEFINE TRANS CODE 41 | 41- TD COMPLIANCE WITH NO PART NUMBER CHANGE OR NON-SERIALIZED COMPONETS. |
| TYPE MAINT CODE B | UNSCHEDULED MAINT |
| TYPE MAINT CODE D | DAILY, TURNAROUND, SPECIAL INSPECTIONS AND PRESERVATION |
| TYPE MAINT CODE G | PHASE INSPECTION |
| TYPE MAINT CODE S | CONDITIONAL INSPECTION |
| TYPE WORK ORDER CODE CP | CORROSION PREVENTION |
| TYPE WORK ORDER CODE CT | CORROSION TREATMENT |
| TYPE WORK ORDER CODE CX | CONDITIONAL INSPECTION SINGLE WORK CENTER |
| TYPE WORK ORDER CODE DF | DAILY, TURNAROUND, PRE/POST FLIGHT DISCREPENCIES |
| TYPE WORK ORDER CODE DM | DISCREPANCY MAINTANENCE |
| TYPE WORK ORDER CODE OM | OTHER TYPE MAINTANENCE |
| TYPE WORK ORDER CODE PF | PHASE FIX PHASE |
| TYPE WORK ORDER CODE TS AND WHEN WOULD YOU USE IT? | TROUBLESHOOTING AND IT IS USE FOR WHEN REMOVING A COMPONET AND INSTALLING IT ON ANOTHER BIRD TO VERIFY IT WORKS, THEN INSTALLING THE COMPONET BACK IN THE ORIGINAL BIRD. |
| WHEN DISCOVER CODE H | BETWEEN FLIGHTS GROUND CREW |
| WHEN DISCOVER CODE J | DAILY INSPECTION |
| WHEN DISCOVER CODE K | TURNAROUND INSPECTIONS |
| WHEN DISCOVER CODE L | SPECIAL INSPECTIONS, PRESERVATION |
| WHEN DISCOVER CODE M | MAJOR OF PHASE INSPECTION |
| WHEN DISCOVER CODE Q | CONDITIONAL INSPECTION |
| WHEN DISCOVER CODE R WHEN WOULD YOU USE IT? | QA INSPECTION. WHEN PERFORMING CDI INSPECTIONS AND THE CDI FINDS A DECREPANCY IS FOUND. THE MAF WOULD BE CUT WITH AN R DC |
| WHEN DISCOVER CODE Y | UPON RECIEPT OR WITHDRAWN FROM SUPPLY |
| WHAT IS THE 01-1A-8 | STRUCTURAL HARDWARE MANUAL- ITS APPLIES BY IDENTIFYING IF MISSING HARDWARE OR TFOA IS CRITICAL OR IS A COMPONENT TO A STRESS PANEL. |
| WHAT IS THE 01-1A-509 | THE 509 CONTAINS ALL OF THE AVIATION CORROSION PUBS USED BY THE NAVY |
| HOW MANY VOLUMES ARE IN THE 509 | THERE ARE 5 VOLUMES. THE 5TH VOLUME IS ONLY USED BY THE AIRFORCE |
| WHAT IS VOLUME 1 OF THE 509 | CORROSION PROGRAM AND CORROSION THEORY |
| WHAT IS VOLUME 2 OF THE 509 | AIRCRAFT CORROSION |
| WHAT IS VOLUME 3 OF THE 509 | AVIONICS AND ELECTRONICS |
| WHAT IS VOLUME 4 OF THE 509 | CONSUMABLE MATERIAL AND EQUIPMENT FOR AIRCRAFT AND AVIONICS. |
| WHAT IS VOLUME 5 OF THE 509 | CONSUMABLE MATERIAL AND EQUIPMENT FOR AIRCRAFT AND AVIONICS. (AIRFORCE) |
| WHAT IS THE 36 INCH RULE | THE 36 INCH RULE IS 36 INCH DIAMETER AROUND YOUR IMMEDIATE WORKAREA. INSPECTING FOR CORRSION |
| WHEN AND WHY WOULD YOU WANT TO MODIFY YOUR TURN-IN WHEN REMOVING PARTS FROM OOMA | WHEN THE SERIAL NUMBERS OF PART NUMBERS DOESNT MATCH IN OOMA. YOU HAVE TO MODIFY IT TO MATCH THE PART REMOVED FROM THE AIRCRAFT |
| WHAT IS THE NAT-04 | A LIST OF ALL ALS TD'S |
| WHAT IS A FOD FASTNER | IT IS A CONPONET ON THE AIRCRAFT, SE, OR IMRLD THAT IS MISSING. |
| WHAT IS THE BIG THING YOU LOOK FOR WHEN RECIEVING REPAIRABLE PARTS | YOU ARE LOOKING FOR THE RFI TAG AND MAKING SURE THE SERIAL NUMBER ON THE TAG MATCHES THE PART. |
| WHAT IS A CERTFICATE OF CONFORMANCE? | IT IS A RFI TAG FROM THE MFR AND COMMERCIAL FACTORY. |
| WHEN SUBMITTING AN EI HOW DOES THE MAF HAVE TO BE LABLED? | 3 INCH RED LETTERS NOT OBSTRUCTING ANYTHING. |
| WHERE IS THE MEL PUB FOUND IF THERE IS NO PAPER COPY AVAILABLE? | CAN BE FOUND ON JTDI AND GROUP SHAREPOINT. |
| WHY DO WE USE THE ULSS FOR THE P-8? | BECAUSE IT IS A COMMERIAL DERIVATIVE AIRCRAFT. |
| WHAT GOES IN THE LOCAL USE BLOCK. | WHEN A SERIALIZED COMPONET HAS BEEN REMOVED FOR FOM MAFS |
| WHAT DOES THE X MEAN IN ALL TYPE WO FOR EXP CX | X MEANS SINGLE WORK CENTER |
| WHAT TYPES OF AUDITS DOES QA PERFORM? | WORK CENTER AUDITS
QA PROGRAM AUDITS
SPECIAL AUDITS
PROGRAM MANGER AUDITS |
