Issued: 31-MAR-1987 | To: FAA | A-87-27 |
ISSUE A GENERAL NOTICE (GENOT) IMMEDIATELY TO ALL UNITED STATES OWNERS AND OPERATORS OF THE CASA C-212 AIR PLANE DESCRIBING THE BACKGROUND AND SIGNIFICANT FINDINGS OF THE RECENT FLIGHT TEST OF THE CASA C-212. THE NOTICE SHOULD PROVIDE AN EVALUATION OF THE EXISTING CASA C-212 STALL CHARACTERISTICS, OPERATIONAL PRECAUTIONS, AND TRAINING PROCEDURES TO PRECLUDE INADVERTENT STALLS UNTIL AN APPROVED ARTIFICAL STALL WARNING SYSTEM IS INSTALLED. (Closed - Acceptable Action) |
Issued: 31-MAR-1987 | To: FAA | A-87-28 |
EXPEDITE THE RULEMAKING ACTION TO REQUIRE INSTALLATION OF AN ARTIFICAL STALL WARNING SYSTEM ON THE CASA C-212 AIRPLANES. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-100 |
COMPLETE AS SOON AS POSSIBLE AND MAKE THE FINDINGS AVAILABLE TO THE SAFETY BOARD THE REPORT ON THE IN-HOUSE REVIEW OF THE BILATERAL AIRCRAFT TYPE CERTIFICATION PROGRAM AND THE CORRECTIVE ACTIONS TAKEN OR CONTEMPLATED AS A RESULT OF THE REVIEW. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-101 |
AMEND TITLE 14 CODE OF FEDERAL REGULATIONS 23.207 AND 25.207 TO REQUIRE A STALL WARNING DEVICE AND ELIMINATE THE USE OF "INHERENT AERODYNAMIC QUALITIES" (AERODYNAMIC BUFFETING) AS A STALL WARNING. (Closed - Unacceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-102 |
AMEND TITLE 14 CODE OF FEDERAL REGULATIONS PARTS 121 AND 135 TO REQUIRE A STALL WARNING DEVICE ON THOSE AIRPLANES THAT CURRENTLY USE "INHERENT AERODYNAMIC QUALITIES" (AERODYNAMIC BUFFETING) AS A STALL WARNING. (Closed - Unacceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-103 |
REQUIRE THE AIRCRAFT EVALUATION GROUP DURING THE TYPE CERTIFICATION PROCESS OF TURBOPROPELLER AIRPLANES TO REVIEW CAREFULLY THE DESIGN OF PROPELLER PITCH CONTROLS IN ORDER TO IDENTIFY AND ESTABLISH APPROPRIATE FLIGHTCREW TRAINING GUIDELINES AND EMPHASIS ON THE PROPER USE OF THESE CONTROLS TO PREVENT INADVERTENT OPERATION IN THE BETA MODE IN FLIGHT WHERE PROHIBITED BY THE AIRPLANE MANUFACTURER. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-104 |
REQUIRE THE PRINCIPAL OPERATIONS INSPECTORS FOR OPERATORS OF TURBOPROPELLER AIRPLANES TO REVIEW CAREFULLY FLIGHTCREW TRAINING PROGRAMS TO VERIFY THAT APPROPRIATE INFORMATION IS PROVIDED BY THE OPERATORS ON THE PROPER USE OF PROPELLER PITCH CONTROLS TO PREVENT INADVERTENT OPERATION IN THE BETA MODE IN FLIGHT. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-105 |
Amend title 14 Code of Federal Regulations 25.1155 and 23.1155 to provide for a positive means to prevent inadvertent operation of the propellers at blade pitch settings below the flight regime in those airplanes where such operation of the propellers is prohibited. (Superseded by A-94-61 through A-94-63) (Closed - Acceptable Action/Superseded) |
Issued: 17-OCT-1988 | To: FAA | A-88-92 |
CORRECT ANY DEFICIENCIES IN COMPLIANCE WITH TITLE 14 CODE OF FEDERAL REGULATIONS 25.8L3 REGARDING THE INSTALLATION OF PASSENGER SEATS ADJACENT TO TYPE II AND III EXITS IN CASA C-212 AIRPLANES WITH 19 SEATS OR LESS. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-93 |
REMEDY THE DEFICIENCIES IN COMPLIANCE WITH TITLE 14 CODE OF FEDERAL REGULATIONS 25.809, .811, AND .813 OF THE SUPPLEMENTAL TYPE CERTIFICATE FOR THE CASA C-212-CC MAIN DOOR REGARDING ACCESSIBILITY TO DOOR CONTROLS DURING EMERGENCY CONDITIONS. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-94 |
REQUIRE IN ACCORDANCE WITH TITLE 14 CODE OF FEDERAL REGULATIONS 25.785(C) ADEQUATE HEAD CLEARANCE BETWEEN PASSENGER SEATS AND BULKHEADS/PARTITIONS INSTALLED IN CASA C-212 AIRPLANES. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-95 |
INSPECT FLIGHTCREW RESTRAINTS IN CASA C-212 AIRPLANES TO VERIFY THE ADEQUACY OF OPERATION, CONVENIENCE, AND COMFORT BASED ON ANTHROPOMORPHIC CRITERIA, AND TAKE APPROPRIATE REMEDIAL ACTION. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-96 |
REQUIRE FIRE-BLOCKING MATERIALS ON ALL PASSENGER AND CREW SEATS ON TITLE 14 CODE OF FEDERAL REGULATIONS PART 21, SPECIAL FEDERAL AVIATION REGULATIONS NO. 41, AND 14 CODE OF FEDERAL REGULATIONS PART 23 COMMUTER CATEGORY AIRPLANES THAT ARE OPERATED UNDER TITLE 14 CODE OF FEDERAL REGULATIONS PART 135. (Closed - Unacceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-97 |
CONDUCT A SPECIAL SURVEILLANCE INSPECTION OF APPROVED HARTZELL PROPELLER OVERHAUL FACILITIES AND OF OTHER PROPELLER MANUFACTURER OVERHAUL FACILITIES AS SERVICE DIFFICULTY HISTORICAL DATA AND EXPERIENCE DICTATE TO DETERMINE THAT THE PROPER QUALITY CONTROL ORGANIZATION AND PROCEDURES ARE IN PLACE AND ARE BEING FOLLOWED. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-98 |
ALERT ALL PRINCIPAL OPERATIONS AND MAINTENANCE INSPECTORS TO EMPHASIZE IN THEIR SURVEILLANCE OF OPERATORS OF TURBO-PROPELLER AIRPLANES THE NEED TO ADHERE TO PRESCRIBED MANUFACTURER INSTRUCTIONS IN MAINTAINING FLIGHT IDLE BLADE ANGLES AND TO EMPHASIZE TO OPERATORS THE CRITICALNESS OF MAINTAINING THEM PROPERLY. (Closed - Acceptable Action) |
Issued: 17-OCT-1988 | To: FAA | A-88-99 |
REISSUE TO OPERATIONS AND MAINTENANCE INSPECTORS FEDERAL AVIATION ADMINISTRATION NOTICE N8320.301 OF SEPTEMBER 17, 1984, PROMPTED BY SAFETY BOARD RECOMMENDATION A-84-15. (Closed - Unacceptable Action) |