We were in there every 200 hour inspection. The airplanes got about 800 hours a year on them. I had a piece of plywood I laid on that baggage shelf to carry my weight to the bulkhead without kinking that light aluminum angle under the front edge of the shelf. Easy to wreck that.
Far 43 Appendix D lists the MINIMUM stuff to be done on an annual, and this sort of thing is there:
Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections
(a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. He shall thoroughly clean the aircraft and aircraft engine.
Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group:
(1) Generally - for uncleanliness and loose equipment that might foul the controls.
(5) Flight and engine controls - for improper installation and improper operation.
((7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment.
(b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group:
Systems and components - for improper installation, apparent defects, and unsatisfactory operation.
(g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation.
Now, I know that this sort of thing is regularly flouted. I found way too much stuff that had been in bad shape for years in places like the tailcone. How does one inspect, for instance, the flight controls back there without getting in there? You can peek though the access hole on the RH side of the tailcone but you can't reach the cables where they pass under the pulleys under that baggage shelf unless you pull the plastic interior out, and you can't check the bulkheads for cracking with that plastic in the way. They do crack, especially the one that carries that light angle. And the pulley bearings seize as the grease in them hardens, and then the cable starts to grind over them and get worn. There are pulleys under the cabin floor and in the aft doorposts that almost never get checked. I have freed them all up and the owners are amazed at the ease and precision of the controls after that.
As I said, it's false economy to ignore that stuff. Seized pulleys wreck both themselves and the cable, an expense that could have been avoided with five minutes effort and some light oil. Bulkheads develop small, repairable cracks that turn into big cracks that require component replacement. Plugged rain holes cause internal corrosion that can trash a lot of structure and the cables, too. Whatever excuse an school or FBO comes up with really doesn't justify such stuff, and it always hurts a lot more in the end.